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STC, Installation and Service Manual

1. 1251 LG 305mm 7108020 18AWG 12 1 LG 28VDC White 18GA Ground Black 18GA MIL W 22759 43 01 0771080 30 1 7108020 Wire 18 12 LG Ground Black 28VDC White 5 79 06 147 MFG Label 44mm 2 31 i 59mm MTG Gasket Model 7108020 7108030 Series Parts List REF QTY QTY ITEM PART NUM BER DESCRIPTION EN E Connector 01 0771080 20 Model 7108020 EC Style 28V MIL C 38999 Series II P 01 0771080 30 Model 7108030 EC Style 28V 20FA98PN 1 1 01 0271848 00 Assy 28V LED Anti Collision Light 71080 1 1 2 07 771393 110 Plate Adapter EC Style Complete 1 3 11 450845 300 Housing Connector Machined LED A C LT 8 4 4 14 0050505 14 Screw 4 40 x 5 16 PPHMS MS51957 14 4 5 13 0050517 04 Nut 4 40 Self Lock Red Hex MS21042 04 4 6 13 0050513 44 Nut 4 40 Plain Hex SS MS35649 244 8 4 7 16 0050506135 Washer 4 Lock Spring MS35338 135 4 4 8 14 0050503123 Screw 6 32 x 9 16 PPHMS SS MS51957 123 4 4 9 16 0050506136 Washer 6 Lock Spring MS35338 136 1 1 10 38 0250885 00 Gasket Lens Model 71055 1 1 11 68 4971082A30 Lens Clear LED Anti Collision Hard coat VIEW PRIOR TO REV K 1 1 12 19 171047 100 Retainer Lens lridite Complete 1 14 10 0331058 01 Label Conn A 28
2. qp Nut for shipping 96 24mm purposes only 96 Tut purposes only I Drain Hole Drain Hole gt 1 13 gt lt 1 13 29 29mm 29mm 9 1 2 229 1 71 43 ZA L lt J 6 152mm 1 20 AWG WIRES MIL 22759 43 20 AWG WIRES MIL 22759 43 POS 1 14VDC RED POS1 14VDC RED POS 2 GROUND BLACK POS2 GROUND BLACK Mounting Detail Model L 7155411 1 23 31mm 9 125 32mm 2 Places Model 7155412 0 875 22mm 01 23 31mm 1 1 750 WE an 44mm dl 125 32mm 2 Places Dimensions and Mounting Detail 28 VDC Model 71554 Series Figure 47b Exploded View Parts HORIZONTAL VERTICAL Figure 47a 01 0771554 01 01 0771554 02 HORIZONTAL VERTICAL 4 40X1 2 4 40X1 2 Je 551957 17 2X LA MS51957 17 2X 60mm Nut for shipping 69mm qpe Nut for shipping 96 24mm purposes only 96 purposes only Drain Hole X Drain Hole 1 13 143 29mm 29mm 9 1 N 947 229mm 5 229mm 55mm ZS 1717 K e KE 152mm 1 e 152mm 1 20 AWG WIRES MIL 22759 43 20 AWG WIRES MIL 22759 43 POS1 28VDC WHITE POS1 28VDC WHITE POS2 GROUND BLACK POS2 GROUND BLACK Mounting Detail Model i
3. 01 0750206 00 60 Cable Kit HDT390 01 0750205 00 90 Cable Kit 01 0750216 00 Install Kit Only No Cable REPLACEMENT CONNECTORS Model Number Part Number Description A441 01 0430011 00 3 Position Male Connector with Pins 442 01 0410823 00 3 Position Female Connector with Sockets 444 02 0230007 00 2 Position Male Connector with Pins 446 02 0230085 00 2 Position Female Connector with Sockets 2015 Whelen Engineering Company Inc Document 05131 Rev D 5 STROBE POWER SUPPLY INSTALLATION INSTALLATION PROCEDURES Location 1 Consider areas or locations designated by the aircraft man ufacturer Do not mount the strobe power supply closer than three 3 feet of the ADF loop 2 For alternate locations consider areas such as the cabin baggage compartment the floor under the seat nonstruc tural bulkheads firewalls etc 3 H necessary fabricate support brackets or shelves and attach them to the aircraft structure to provide a mounting surface that will withstand the inertia forces stipulated in chapters 1 amp 3 of AC 43 13 2A 4 An IA or other representative of the FAA must approve documentation of structural integrity of the fabricated instal lation 5 When installing the strobe light power supply in an inverted position drill a 3 16 diameter hole in the lowest corner o
4. QTY QTY ITEM PART NUMBER DESCRIPTION 01 0771080 07 Model 7108007 Upper 28V 01 0771080 17 Model 7108017 Lower 28V 01 0271848 00 Assy 28V LED Anti Collision Light 71080 38 0250885 00 Gasket Lens Model 71055 Series 68 4971082A30 Lens Clear LED Anti Collision Hard coat 68 4971082A31 Lens Clear LED Anti Collision with Drain Hard coat 07 571361 100 Adapter Mounting 3 3 4 16 0050506135 Washer 4 Lock Spring MS35338 135 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 N 26 0715260 11 Shrink Tubing 1 8 Dia X 1 2 O OQ Ww Pp 39 5903711 25 Conn Pin MS3102E10SL 3P Rework 4 11 450845 300 Housing Connector Machined LED A C Lt 07 750976 100 Plate Nut Model 90520 w Helicoils i N 14 0050503 34 Screw 6 32 X 1 PPHMS MS51957 34 k Co 10 0331058 02 Label Conn A 28VDC C GND i 14 0050503 28 Screw 6 32 X 3 8 PPHMS 55 MS51957 28 k 16 0050506136 Washer 6 Lock Spring 535338 136 MS3102R10SL 3P o View Prior to Rev K 2015 Whelen Engineering Company Inc Document 05131 Rev D 25 Models 7108008 7108018 Dimens
5. r p d 1 COMPANY INC Engineers for the Aviation Warning Industry ANTI COLLISION LIGHT SYSTEMS INSTALLATION 2998 AND SERVICE MANUAL May 2015 Approved under STC SA6NE STC SA21NE STC SA615EA STC SA800EA ISO 9001 Registered QMS 2015 Whelen Engineering Company Inc Document 05131 Rev D HIN DEX PAGE 11 12 13 14 15 16 21 22 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 Table Of Contents Company Information Strobe System Requirements Aircraft not specifically mentioned on the eligibility list Strobe System Wiring Strobe Power Supply Installation Orion 500 LED Light Assemblies Orion 650 LED Light Assemblies Orion 650E LED Light Assemblies Strobe Power Supplies HDACF A490ATSC A490TCF A490TCCF LED Light Assemblies 90520 Series LED Light Assemblies 71080 Series Self Contained Light Assemblies 70900 Series Self Contained Light Assemblies 71055 Series Self Contained Light Assemblies HRCFA Series Models SACF amp A440 Strobe Lighthead Assemblies A470A Series Model A450 H102 amp H103 Strobe Lighthead Assemblies A650PG PR Series LED Light Assemblies 71110 Series Strobe Lighthead Assemblies A610 Series A612 Series Strobe Lighthead Assemblies A625 Series S
6. 7101113 Model 71011 Series Parts List QTY ITEM PART NUMBER DESCRIPTION 01 0771011 02 MODEL 7101102 LED TAIL POSITION LIGHT FINAL ASSEMBLY 28VDC 01 0771011 03 MODEL 7101103 LED TAIL POSITION LIGHT FINAL ASSEMBLY 28VDC 01 0771011 12 MODEL 7101112 LED TAIL POSITION LIGHT FINAL ASSEMBLY 14VDC d 01 0771011 13 MODEL 7101113 LED TAIL POSITION LIGHT FINAL ASSEMBLY 14VDC 1 1a 01 0290307 02 ASSY LED VERTICAL MOUNT TAIL POSITION LIGHT 28V 1 1b 01 0290307 03 ASSY LED VERTICAL MOUNT TAIL POSITION LIGHT 28V 1 1c 01 0290307 12 ASSY LED HORIZONTAL MOUNT TAIL POSITION LIGHT 14V 1 1d 01 0290307 13 ASSY LED HORIZONTAL MOUNT TAIL POSITION LIGHT 14V 1 2 38 0231061 00 GASKET LENS LED TAIL POSITION LIGHT 1 3 68 3970991 30 LENS CLEAR TAIL POSITION LIGHT 1 4 19 0150350 03 RETAINER MASK 635 TALL 2 5 14 0050505 18 SCREW 4 40 x 5 8 PPHMS MS51957 18 2 6 13 040130 040 NUT 4 40 x 1 4 HEX BRASS for shipping 1 7 46 0750898 00 28V PIGTAIL ASSEMBLY 6 BLK WHT 1 8 46 0750898 01 14V PIGTAIL ASSEMBLY 6 BLK RED 2015 Whelen Engineering Company Inc Document 05131 Rev D 45 LED LIGHT ASSEMBLIES MODEL 71554 SERIES LED TAIL POSITION LIGHT ASSEMBLY 71554 Series in our newest LED Tail Position Light Exact Footprint for Whelen Models A555A and 71011 Taillights Available in horizontal or vertical mount Model 71554
7. POS 1 RED ANODE POS 1 BLUE POS 2 BLACK CATHODE POS 2 BLUE GROUND POS 3 WHITE TRIGGER Model A500A Parts List QTY QTY QTY QTY QTY QTY QTY QTY ITEM PART NUM BER DESCRIPTION 01 0770024 00 Tail Pos amp Strobe LT Assy A500A V 14 01 0770024 01 Tail Pos amp Strobe LT Assy A500A V 28 01 0770024 02 Tail Pos amp Strobe LT Assy A500A H 14 01 0770024 03 Tail Pos amp Strobe LT Assy A500A H 28 01 0770024 04 Tail Pos amp Strobe LT Assy A500A V D 14 01 0770024 05 Tail Pos amp Strobe LT Assy A500A V D 28 01 0770024 06 Tail Pos amp Strobe LT Assy A500A H D 14 4 01 0770024 07 Tail Pos amp Strobe LT Assy A500A H D 28 N A 4 40 x 1 2 Phillips PHMS MS51957 17 19 0150350 01 Retainer Mask Horizontal 19 0150350 02 Retainer Mask Vertical 68 4270002 30 Clear Glass Plain Dome A457A 38 0230002 00 Gasket A455 34 0412070 63 Lamp Erc Halogen 14 Volt A508 14 34 0428070 64 Lamp Esg Halogen 28 Volt A508 28 N A Hex Nut 4 40 X 1 4 A F Brass 1 1 1 1 12 02 0350034 00 Flash Tube And Socket Assy A506 1 1 1 1 14 02 0350375 00 Flash Tube And Socket Assy A506D 1 1 1 1 15 68 4270002 34 Lens RFI Coated A457AC l _ 19 02 0350375 01 Flash Tube And Socket Assy A506DM 1 1 1 1 1 1 1 1 32 46 0750698 00 Pigt
8. 68 3950902A30 LENS CLEAR FWD POSITION LIGHT HARD COAT 38 0130107 00 GASKET A427 4 1 4 THICK 36 0050626 01 ASS Y FLASHTUBE 6 00 LEADS W GROMMET 68 2290005 34 LENS CLEAR COATED A612 19 171122 200 RETAINER LENS MODEL 71110 SERIES 14 0050508 27 SCREW 6 32 5 16 PFHMS 551959 27 01 0271757 03 ASSY POSITION STROBE LIGHT 28V GRN 71110 i 01 0271 757 04 ASSY POSITION STROBE LIGHT 28V RED 71110 OPEN HOLE IN LABEL FOR DRAIN HOLES 2 PLACES 2015 Whelen Engineering Company Inc Document 05131 Rev D 39 INSTALLATION OF MODEL A612 with an A610 Flash Tube A612 glass lens and A610 flash tube are used for installing wing tip strobes in single engine Cessna s 1972 and later The existing position light retainer is modified to accommodate the lens and the flash tube is mounted directly behind The unique magnifying design of the A612 lens increases the light intensity by two to three times in the horizontal plane These items may be used for custom instal lations or as spare parts for existing light assemblies The A612 lens is available in Aviation Red and an RFI coated version Lenses meet material requirements of MIL C 7989B Class B A612 Model A612 Specifications Model Part A612 68 2290005 30 2290005 30 Standard ClearLens Clear Lens A612C 68 2290005 34 s o shie
9. Aircraft for which type certificate was applied for after April 1 1957 to August 10 1971 These anti collision systems must produce a minimum of 100 effective candela in Aviation Red or White REF FAR 23 1397 360 around the aircraft s vertical axis 30 above and below the horizontal plane REF FAR 23 1401 Aircraft for which type certificate was applied for after August 11 1971 to July 18 1977 These anti collision systems must produce a minimum of 400 effective candela in Aviation Red or White REF FAR 23 1397 360 around the aircraft s vertical axis 30 above and below the horizontal plane REF FAR 23 1401 Aircraft for which type certificate was applied for after J uly 18 1977 These anti collision systems must produce a minimum of 400 effective candela in Aviation Red or White REF FAR 23 1397 360 around the aircraft s vertical axis 75 above and below the horizontal plane REF FAR 23 1401 The position lights must be wired independently of anti collision lights GENERAL AVIATION MINIMUM POSITION LIGHTING REQUIREMENTS For compliance to FAR Part 23 1385 through 23 1397 VFR flight rule night requirements on a General Aviation aircraft you must have a TSO d Aviation Red forward position light on the left and an Aviation Green forward position light on the right See Figure 7 page 4 These are normally mounted on the most outward extremity of the airframe so they can project their light directly in
10. Lens Clear LED Anti Collision with Drain 68 4971082A31 Hardcoat 07 571361 100 3 3 4 Adapter Mounting 71106005 amp 7108015 AWG TEEN EC 28 VDC White 18GA 16 0050506135 Washer 4 Lock Spring MS35338 135 Ground Black 18GA 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 MIL W 22759 43 10 0315069 14 Label Voltage ID 28V 46 0750898 01 Ass y 14V Pigtail 6 Blk Red 127 305mm 1 LG 28VDC White Wire 18GA 12 LG 7108005 amp 7108015 18AWG 12 1 LG 28VDC White 18GA Ground Black 18GA 4 MIL W 22759 43 4 1 CO OO N O a RWIN 24 Document 05131 Rev Models 7108007 7108017 Exploded View Parts Figure 25a Dimensions Figure 25b 03 67 93mm Q 125 3mm DRAIN HOLE LOWER MNT ONLY 1 1 6 32 Mounting Holes M ount hg 6 32 x 5 16 Suggested Figure 25C Screw Length 3 092 2 06 100mm 5 43 x 06 138mm Suggested Mounting Pattern Wi rl ng Connector Figure 25d Trim Wires To 3 5 Before Soldering White Black O B MS Connector Wiring Rear View Figure 25e 28VDC N C GND LED MODULE Wiring Diagram Model 7108007 7108017 Series Parts List
11. Specifications Model Part LED Operational Input 7155401 01 0771554 01 28 VDC 7155411 01 0771554 11 14 VDC 7155412 01 0771554 12 Operating Instructions EQUIPMENT LIMITATIONS An approved tail position light assembly should be mounted as far aft on the aircraft as practicable on a ther mally conductive surface The baseplate must be mounted parallel to the vertical and horizontal centerlines of the aircraft to project the patterns properly Certain types of installations may require additional testing CONTINUED AIRWORTHINESS The 71554 series LED tail position light assembly is designed with 6 LEDs Should any one LED fail the unit must be repaired or replaced Note To reduce eye strain use an optical filter such as dark glasses or a Blue covering dome during LED inspection Inspect the lens Replace if there is excessive scratching pitting discoloration or cracking INSTALLATION PROCEDURES The following information is to assist you in installing a Whelen LED tail position light 1 Choose the appropriate 71554 light assembly 2 Using the mounting detail information provided prepare the aircraft for means to secure the LED light assembly 3 Connect the position light inputs according to the chart shown Connect the power lead to an appropriate sized breaker Connections to be in accordance with FAA approved methods 4 Remove and discard the two screws and nuts holding the retain er to the unit Carefu
12. 01 0790725 11 OR6502G Wingtip Position Anti Collision Light 28V Green 14 0050581 05 Screw 44 40 x 7 16 P100FH CSNK MS24693 C5 01 0790725 12 OR6502R Wingtip Position Anti Collision Light 28V Red 19 151088 000 Retainer Lens Model 90725 14 0050581 05 Screw 4 40 x 7 16 P100FH CSNK MS24693 C5 01 0251094 00 Lens Assy 2 Gasket 19 151088 000 Retainer Lens Model 90725 01 0251094 01 Lens Assy 1 Gasket 01 0251094 00 Lens Assy 2 Gasket 38 0231382 00 Gasket Lens Model 90725 38 0231382 00 Gasket Lens Model 90725 14 005058 1 02 Screw 4 40 x 1 4 P100FH CSNK MS24693 C2 14 0050581 02 Screw 4 40 x 1 4 P100FH CSNK MS24693 C2 01 0290729 01 Sub Assy Model OR6501G 14VDC Green 01 0290729 11 Sub Assy Model OR6502G 28VDC Green 01 0290729 02 Sub Assy Model OR6501R 14VDC Red 01 0290729 12 Sub Assy Model OR6502G 28VDC Red OON O Q WN 07 551089 100 Adapter Mounting Heli Coils Installed CMPL ANO WIN 07 551089 100 Adapter Mounting Heli Coils Installed CMPL Document 05131 Rev D ORION 650E LED LIGHT ASSEMBLIES MODELS 086501 0 096501 RE pa OR6502GE OR6502RE LED Wingtip Position Anti Collision Lighthead Assembly All LED self contained wingtip mounted Position Anti Collision system El
13. 4 4 Before with Quartz Light After with Remote Strobe Light Model A470A Installation The A450 and A470A remote anti collision strobe lighthead assemblies are direct replacement for the quartz type flasher using the original or the H102 B mounting adapter The H102 B mounting adapter is mounted in the aircraft s structure with four 4 MS 20470 AD4 rivets or four 4 6 32 screws and self locking nuts 21 625 21 250 Drill out the center hole in the skin to allow access to the strobe head connector BOLT CIRCLE BOLT CIRCLE 34 Document 05131 Rev D Vertical Fin and Rudder Mounting of Anti Collision Strobe Lights Rudder mounted anti collision lights should be located top center of the rudder hinge center line or rudder balance must be established after installation Refer to AC 43 13 2A Chapter 4 Paragraph 55 e Rudder Installation The rudder or fin cap is excellent for shadowing the prop and cabin area if the light is mounted far enough back NOTE Mounting an A450 or A470A strobe lighthead assembly on a vertical fin or rudder can be accomplished by fabricating a mounting adapter similar to the ones shown in illustrations Round or streamline tubing cut to fit 40 thick disc Reference AC 43 13 1B Chapter 2 Section 2 A470A Dimensions Exploded View Figure 35c
14. 7155401 01 23 31mm 9 125 32mm 2 Places Model 7155402 0 875 22mm 91 23 31mm 1 750 E 44mm 0 125 32 7 2 Places Position 1 28VDC White Position 2 Ground Black Model 71554 Series Parts List QTY QTY QTY QTY ITEM PART NUMBER DESCRIPTION u 01 0771554 01 Final 28V LED Tail Pos Light Horizontal 01 0771554 02 Final 28V LED Tail Pos Light Vertical 01 0771554 11 Final 14V LED Pos Light Horizontal 01 0771554 12 Final 14V LED Tail Pos Light Vertical 1 1 01 0271552 01 Assy 28V LED Tail Pos Light Horizontal 2 01 0271552 02 Assy 28V LED Tail Pos Light Vertical 3 38 0231260 00 Gasket Lens 90296 Housing 4 68 3970991 30 Lens Clear Hard coat Tail Position Light 1 1 5 19 0150350 06 Retainer Mask Horizontal 6 7 8 19 0150350 07 Retainer Mask Vertical 2 2 2 2 14 0050505 18 Screw 4 40 x 5 8 PPHMS MS51957 18 2 2 2 2 13 040130 040 Nut 4 40 x 1 4 Hex Brass 1 1 1 1 10 46 0750898 00 Ass y 28V Pigtail 6 Blk Wht 1 11 01 0271552 11 Assy 14V LED Tail Pos Light Horizontal 1 m 12 01 0271552 12 Assy 14V LED Tail Pos Light Vertical 1 1 1 1 13 46 0750898 01 Ass y 14V Pigtail 6 Blk Red 2015 Whelen Engineering Company Inc Document 05131 Rev D 47 MODEL A600 PG PR SERIES INSTALLATION A600
15. Dimensions Exploded View A625 Strobe Light Assembly Figure 41a Figure 41b The A625 strobe lighthead assembly fits into a 1 1 inch hole The mounting screws are 1 75 inch center to center It protrudes 1 7 inch outside the air craft s skin and 1 1 inch inside the aircraft When installing an A625 strobe lighthead assembly on the rudder refer to the aircrafts MAINTENANCE and or SERVICE MANUAL for accepted procedures for balancing the rudder before returning the aircraft to service Mount the anti collision strobe lighthead assembly as close to the stabilizer center line as practical to eliminate backscatter as much as possible for the horizontal surface When installing the A625 strobe lighthead assembly in an enclosed area like a Beech enclosed wingtip or tail cone maintain at least 0 060 inch clearance around the lens to the plastic cover The A625 mounts conveniently just behind the forward position light on Cessna s conical camber wingtip Make sure that the navigation light pattern is not interrupted when installing the A625 strobe light head on a wingtip The A612 lens is not considered an obstruction 5 50 50 E LEAD LENGTH CONNECTOR WIRING POS 1 RED ANODE POS 2 BLACK CATHODE POS 3 WHITE TRIGGER A625 INSTALLATION IN CESSNA 300 OR 400 SERIES WINGTIP TANKS The A625 fits just under the navigation light on an adapter plate of 0 032 inch aluminum approximately 2 3 8 inches x 3 1 2 inches Fit
16. and mounting hori zontal or vertical must be specified when ordering ia VERTICAL HORIZONTAL x MOUNTING MOUNTING Model A500A Specifications umbers Number Color Voltage Diameter wwe 5 wwe 3 _ wwe _ wwe 3 _ wwe _ Horizontal Mount Molex Connector Mount Molex Connector voo ow ow Vertical Mount with MS Connector A500ABV2 01 0770024 15 Beach Special 28 VDC Vertical Mount with MS Connector A500ABV1 01 0770024 16 Beech Special 14 VDC Vertical Mount 50 cables A500ASP2 01 0770024 25 no connectors Beech Special 28 VDC Operation Installation Combination Strobe Tail Navigation Light used when the wingtip Anti 1 Remove the Model S tail position light by removing the two 2 Collision lights are mounted in an enclosure and can t provide 360 of retainer ring screws strobe coverage It is a direct replacement for the standard Tail Position light Available in a radio shielded version Voltage 14 or 28 and mount ing horizontal or vertical must be specified when ordering Dimensions 2 17 42 2 44mm 2 This unit fits directly in place of the Grimes Model S tail position light It is however sometimes necessary to open the mounting hole in the aircraft fairing to 1 10 inch to clear the body of the A500A The body protrudes 1 40 inch into the tail fairing 3 Establish the proper light pattern of t
17. tighten firmly When necessary seal the light to the aircraft Apply sealant around the perimeter of the base Do not cover the drain hole Check all avionics systems for interference from this installation A flight check should be performed by a properly certi fied pilot Update aircraft records complete Form 337 and obtain FAA field approval for installation if required Dimensions 1 79 4 500 13mm Figure id A 1 000 25mm 29 800 20mm 72 18mm 9 E 175 3x 150 4mm 44mm for 6 Screw Cx 100 C sink oo Mounting Detail 1031 0 25cm 20AWG MIL 22759 43 Wire Document 05131 Rev D 9 Model OR6501G OR6501R 14V Series Exploded View Parts Figure 10a Lens P N 01 0251094 00 Shown For ReferenceOnly Drain Hole Model OR6501G amp OR6501R Series Parts List Model OR6502G OR6502R 28V Series Exploded View Parts Figure 10b Drain Hole QTY QTY ITEM PART NUMBER DESCRIPTION Model OR6502G amp OR6502R Series Parts List 01 0790725 01 OR6501G Wingtip Position Anti Collision Light 14V Green QTY QTY ITEM PART NUM BER DESCRIPTION 01 0790725 02 OR6501R Wingtip Position Anti Collision Light 14V Red
18. 0790520 04 Model 9052004 28V Upper 01 0790520 14 Model 9052014 28V Lower 1 1 1 01 0290522 00 Assy 28V 1 1 2 38 0250885 00 Gasket Lens 1 3 68 4971082A30 Lens Clear 1 4 68 4971082A31 Lens Clear 1 1 5 38 0250225 00 Seal 1 1 6 07 571304 100 Adapter 5 Hole Lens Retainer 4 4 7 16 0050506135 Washer 4 Lock Spring MS35338 135 4 4 8 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 Mounting Figure 18c 75 6 32 Flat Head 100 Countersink typ 5 x 6 32 MTG holes on a 4 656 118mm bolt circle GROUND BLACK Dimensions Figure 18b 5 14 131mm 260 66mm NOTE RED LEDs TO THE FRONT i Olle 3 64 GIS 92mm Olle Mounting ge Gasket 4 2 T MFG LABEL 18AWG 12 1 0 28VDC WHITE 18AWG 12 1 0 Models 9052005 9052015 Exploded View Parts Figure 19a 2015 Whelen Engineering Company Inc 9052055 QTY QTY QTY ITEM PART NUMBER DESCRIPTION 01 0790520 05 Model 9052005 28V Upper j 01 0790520 15 Model 9052015 28V Lower i 01 0790520 55 Model 9052055 14V Upper 1 1 1 1 01 0290522 00 Assy 28V 1 2 01 0290522 50 Assy 14V 1 1 1 3 38 0250885 00 Gasket Lens 1 4 68 4971082A30 Lens Clear 1 1 B 68 4971082A31 Lens Clear 1 1 1 6 07 571361 100 Adapter Mounting 4 4 4 7
19. 16 0050506135 Washer 4 Lock Spring MS35338 135 4 4 4 8 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 Mounting Figure 19c 3x 6 32 Mounting Holes 6 32 x 5 16 8mm suggested screw length Heli Coil Insert 3 Suggested Mounting Hole Pattern Dimensions Figure 19b 3 60 91mm NOTE RED LEDs TO FRONT 0 125 DRAIN HOLE LOWER MOUNT ONLY 3 92 100mm a i O MFG LABEL GROUND BLACK 20AWG 14VDG 6 x1 0 18AWG 28VDC 12 x1 0 14VDC RED 20AWG 6 31 0 or 28VDC WHITE 18AWG 12 1 0 Document 05131 Rev D 1 Q Models 9052007 9052017 Exploded View Parts Figure 20a DESCRIPTION Model 9052007 28V Upper QTY QTY ITEM PART NUMBER T 01 0790520 07 m 01 0790520 17 Model 9052017 28V Lower 01 0290522 00 Assy 28V 1 1 2 38 0250885 00 Gasket Lens 1 3 68 4971082A30 Lens Clear 1 4 68 4971082A31 Lens Clear 1 1 5 07 571361 100 Adapter Mounting 4 4 6 16 0050506135 Washer 4 Lock Spring MS35338 135 4 4 7 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 Mounting Figure 20c 3x 6 32 Mounting Holes 6 32 x 5 16 8mm suggested screw length Heli Coil Insert 3 S
20. 3 68 4971082A30 Lens Clear LED Anti Collision Hard coat 1 4 68 4971082A31 Lens Clear LED Anti Collision with Drain Hard coat 4 4 5 16 0050506135 Washer 4 Lock Spring MS35338 135 4 4 6 14 0050505 14 Screw 4 40 x 5 16 PPHMS MS51957 14 4 4 7 26 0715260 11 Shrink Tubing 1 8 Dia x 1 2 1 1 8 39 5903711 25 Conn Pin MS3102E10SL 3P Rework 1 1 9 11 450845 300 Housing Connector Machined LED A C LT 1 1 10 07 750976 100 Plate Nut Model 90520 w Helicoils 4 4 11 14 0050503 34 Screw 6 32 X 1 PPHMS MS51957 34 1 1 12 07 571304 100 Adapter 5 Hole Lens Retainer Iridite 1 1 14 10 0331058 02 Label Conn A 28VDC C GND 1 1 15 38 0250225 00 Seal HR LT Series 4 4 16 14 0050503 28 Screw 6 32 X 3 8 PPHMS SS 551957 28 4 4 17 16 0050506136 Washer 6 Lock Spring MS35338 136 Models 7108020 7108030 Exploded View Parts Figure 27b Figure 27a Dimensions Wiring Diagram Figure 27d 30 Wiring Diagram 28VDC A LED GND B MODULE N C C MS Connector Wiring Rear View Mounting Figure 27c 01 0771080 20 2 475 Suggested Mounting Pattern Models 7108020 amp 7108030 MTG GASKET REF MFG LABEL
21. 3 N A 416 32 X 1 2 PHILLIPS PHMS MS51957 30 1 4 01 0450685 00 CLAMP RING 6 50 1 5 68 4230044 30 LENS Clear 1 6 N A 416 32 X 5 16 SS HEX NUT MS35649 264 2015 Whelen Engineering Company Inc Figure 35b Metal bracket shaped to fit the vertical fin or rudder or vertical fin welded to 2 12 OD rudder with 2 1 2 OD 040 thick disc riveted in place Reference AC 43 13 1B Chapter 2 Fabrication and installation of these mounting brackets are referenced in this approved installation manual and AC 43 13 1B and 2A Documentation of structural integrity of the fabricated installation must be approved by an or other representative of the FAA Conformity inspections will be performed with reference to approved techniques and procedures specified in this manual see page 3 THRU Document 05131 Rev D 35 MODEL A650PG PR SERIES WINGTIP STROBE ANTI COLLISI ON POSITION LIGHT ASSEMBLY A650 PG PR Series wingtip with Anti Collision amp Forward Position lights can be used to convert non Whelen Position lights into a Position Anti Collision light system The small size allows for mounting into a wing tip enclosure Available in 14 or 28 VDC and in a radio shielded version The forward position lamp is 26 watts Model A650PG PR Specifications A650PG1 01 0770054 00 0770054 00 Position Red AGSOPGDM 01 0770054 14 Radio
22. 4 3 14 0050503123 SCREW 6 32 X 9 16 PPHMS MS51957 123 4 4 4 16 0050506136 WASHER 6 LOCK SPRING MS35338 136 1 1 5 38 0250885 00 GASKET LENS MODEL 71055 SERIES 1 1 6 68 497 1046 30 LENS CLEAR MODEL 71055 SERIES 1 1 7 19 171047 100 RETAINER LENS MODEL 71055 SERIES 4 4 8 14 0050505 14 SCREW 4 40 X 5 16 PPHMS 551957 14 4 4 9 16 0050506135 WASHER 4 LOCK SPRING MS35338 135 1 1 10 10 0315069 13 LABEL VOLTAGE ID 14V 1 14 01 0271829 01 ASSY 28V LED ANTI COLL LT 2015 Whelen Engineering Company Inc Document 05131 Rev D 31 MODEL HRCFA SERIES SELF CONTAINED STROBE ANTI COLLISION LIGHT ASSEMBLY HRCFA series is a self contained CometFlash strobe Anti Collision light The unique polycarbonate optic lens and reflector design re directs stray light rays into the horizontal plane to provide maximum 360 of uniform light coverage Available in three different lens colors aviation Red aviation White and split aviation Red White and in radio shielded configurations FAA approved as a direct replacement for any rotating beacon that uses a 3 3 4 95mm dia mounting hole Can be installed the vertical fin or the fuselage Fuselage installation requires the A440 mounting adapter Operates between 10 to 30 VDC Model HRCFA Specifications Model Part Polycarbonate Input Current Split Red White Split Red White MODEL SACF SELF CONTAINED STROBE ANTI COLLISION LIGHT ASSEMBLY Standard Assembly 3 3 4 95mm
23. 40c 3 Scribe the A612 lens profile as shown in illustration Figure 40c left the object being to have the strobe light centered over the position light base plate 4 Trim or fit an opening to the scribe line to fit the A612 lens Due to the uneven surface of the Cessna lens retainer the A612 will contact only the front and rear radius profile 5 Place the sponge rubber pad supplied under the A610 flash tube to firm the assembly RTV is recommended to secure lens in the modified retainer 6 The flash tube interconnecting cable is routed through square holes in the rear bulkhead of the position light area T Install the modified position light lens retainer A610 flash tube and A612 lens using original hardware 40 Document 05131 Rev D MODEL A625 SERIES INSTALLATION A625 series has many different applications It can be used for aircraft with tip tanks with enclosed position lights under a fairing or as an add on strobe on the wing or the tail Available in a radio shielded version Model A625 Specifications Model Part LENS ADGFOUMIS Input Current Exposed Numbers Number Color PP Operational Voltage Height A625 01 0770058 03 Clear FAA PMA 03 only ear White A625D 01 0770058 13 Radio shielded 1 ependant on strobe s Red lens power supply used 0 2 lbs 919m 1 7 43mm A625DR 01 0770058 14 Radio shielded red lens Radio shielded 3 c cable Radio shielded 24 3 c White
24. 7090005 Exploded View Parts Figure 29a Lens P N 68 4990257 30 Screw P N 14 062216 05M Before LED installation Gasket P N 38 0250843 00 Model 70900 series after LED installation LED Module P N 14V 01 0270918 01 P N 28V 01 0270918 03 Model 70900 series after LED installation RTV required after hardware installation for inverted bottom mounted units Mounting 3 6 32 x 3 8 Figure 29b 1 00 Clearance for wires Typical Mounting Hole Pattern 2015 Whelen Engineering Company Inc Document 05131 Rev D 29 SELF CONTAINED LIGHT ASSEMBLIES MODEL 71055 SERIES LED BEACON ANTI COLLISION LIGHT ASSEMBLY 50 9 CLASS IIl 71055 series beacons are FAA TSO compliant self contained LED Anti Collision lights They are designed to replace existing quartz halogen flasher beacons installed as original equipment on single engine Cessna s from 1967 and later contact factory for details They can also replace remote mounted strobe lights ref Whelen A470 series allowing for removal of the strobe power supply Internal mounting plate provided with choice of mounting holes to retrofit most existing mounting patterns STC SA615EA approved Model 71055 Specifications Model Part LED Operational Peak Input Flash 0 48 Polycarbonate 21 4 0 Amps 0 55 7105500 01 0771055 00 14 VDC 9 14 VDC 0 75 Amp Avg ACL ely 249gm 45 5 FPM
25. A470ADR A470ADW MODEL A450 REMOTE STROBE FUSELAGE VERTICAL A450 series remote strobe assembly is compatible with all Whelen power supplies It can be installed on the fuselage i TT or the vertical fin The Pyrex9 Glass lens Clear only makes the assembly suitable for use in severe vibration chemical and moisture conditions i e agricultural aircraft Requires either the model H102 or model H103 mounting adapter Model A450 Specifications Exposed Model Part Input Current Lens Approvals Height Clear Pyrex amp Glass lens _ 7 Standard assembly installed i Dependant on strobe 2 25 A450 01077005200 the fuselage or the vertical fin m FAA PMA power supply used 0 3 lbs 13 MODELS H102 amp H103 MOUNTING ADAPTERS Designed for the Model A470A or Model A450 series remote strobe lighthead assemblies The Model H102 allows flush mounting of the lighthead to the skin of the fuselage or the vertical stabilizer on later model Cessna Single engines The H103 is designed for strobe assemblies to be installed in the standard 3 3 4 95mm dia rotating beacon mounting hole Model A440 Specifications Model Part H102 07 730068 000 Flush mount adapter FAA PMA I 1 For standard 3 3 4 95mm dia H103 11290079000 rotating beacon mounting hole H102 Mounting Quartz Type Flasher Replacements Adapter pu 1507 M Figure 34a 1 i 22 485 4
26. FRONT Wiring Diagram Figure 21d LOWER MOUNT ONLY WHITE BLACK C O Q O B 0 125 DRAIN HOLE MS CONNECTOR WIRING REAR VIEW CONNECTOR MS3102R10SL 3P 2015 Whelen Engineering Company Inc Document 05131 Rev D 21 LED LIGHT ASSEMBLIES MODEL 71080 SERIES LED BEACON Red LED s LED Flashing Anti Collision Light Assembly 150 eff Cd 14 VDC amp 28 VDC 71080 series LED beacons are FAA TSO compliant Self Contained LED Anti Collision lights Ref Class 150 effective candlepower They are designed to replace a range of products Refer to models and descriptions below ELECTRICAL Models 01 04 05 14 15 20 51 55 Ship with 12 Flying Leads Models 07 17 08 18 MS3102R10SL 3P Connector MECHANICAL Models 04 14 08 18 are designed to replace existing beacons utilizing a 5 Hole mounting pattern on a 4 656 diameter bolt circle Whelen 70285 series 7090501 series or 70900 with A440 adapter Models 05 15 07 17 are 3 4 opening designed to fit inside an A440 mounting adapter mounting holes to fit in place of rotating beacons Whelen Model HRCFA or 7090004 05 series LED beacons Model 71080 LED Rotorcraft Beacon Specifications Lens Voltage LED Color Approvals Input Current Mount Hole Pattern Model Numbers Part Number 7108001 01 0771080 01 A470A Mount 5 Hole Adapter Flying Leads 3 75 Adapter Flying Leads 7108004 01 0771080 04 7108005 01 0771080 05 7
27. Hole 1 2 01 0290522 00 Assy 28V 1 3 01 0290522 50 Assy 14V 4 4 4 16 0050506136 Washer 6 Lock Spring MS35338 136 4 4 5 14 0050503 30 Screw 6 32 X 1 2 PPHMS SS MS51957 30 1 1 6 38 0250885 00 Gasket Lens 1 1 7 68 4971082 30 Lens Clear AI 1 1 8 19 171047 100 Retainer Lens 4 4 9 16 0050506135 Washer 4 Lock Spring MS35338 135 3 74 4 4 10 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 95mm i 4 x 6 32 MTG holes equally Mounting spaced on a 1 625 bolt circle Figure 17c i 1 00 25mm MFG 4 x 6 32 MTG holes LABEL equally spaced on a 1 250 38mm bolt circle Front BLACK GROUND 28VDC 18AWG 12 1 0 14 VDC 20AWG 6 0 1 0 316 32 Flat Head 100 Countersink typ WHITE 28VDC 18AWG 12 1 0 RED 14VDC 20AWG 6 1 0 7 2015 Whelen Engineering Company Inc Document 05131 Rev D 1 7 Models 9052004 9052014 Exploded View Parts Figure 18a 1 8 Document 05131 Rev D Model 9052004 amp 9052014 Parts List QTY QTY ITEM PART NUMBER DESCRIPTION d 01
28. PG PR series wing tip anti collision forward position and tail position lights all in one compact unit Tail position light eliminates the need for a tail mounted position light Available in 14 or 28 VDC and in a radio shielded version The forward position lamp is 26 watts and the taillight lamp is 25 watts Model A600 PG PR Specifications Model Numbers Part Number A600PG1 01 0790006 00 Position Green Green A600PG2 01 0790006 01 Position Green A600PR1 01 0790006 02 Position Red A600PR2 01 0790006 03 Position Red FAA TSO C30b Position Green Radio shielded Position Green Radio shielded Position Red Radio shielded Position Red Radio shielded FAA PMA A600PGD1 01 0790006 04 Green A600PGD2 01 0790006 05 A600PRD1 01 0790006 06 A600PRD2 01 0790006 07 D e o 2 Wingtip anti collision forward position and tail position lights all in one compact unit Tail position light eliminates the need for a tail mounted position light Available in 14 or 28 volts and in a radio shielded version The forward position lamp is 26 watts and the taillight lamp is 25 watts Installation The A600 Series must be properly mounted to comply with FAR Part 91 205 c 2 amp c 3 The light assembly must be mounted so that the light distribution pattern is not obstructed by any parts of the aircraft A limited amount of obstruction is permitted Ref FAR Part 23 1401 for anti collisio
29. Position Anti Collision Light 28V Green 01 0790701 12 OR6502RE Wingtip Position Anti Collision Light 28V Red 07 771790 100 Mounting Plate Model 90701 Heli Coils CMPL 14 0050505 14 Screw 4 40 x 5 16 PPHMS MS51957 14 01 0290714 11 Sub Assy Model OR6502GE 28 VDC GRN 01 0290714 12 Sub Assy Model OR6502RE 28 VDC RED 1 4 1 oja 1 2 Document 05131 Rev D MODEL HDACF STROBE POWER SUPPLY ASSEM BLY FAA PMA APPROVED Specifications Model Number HDACF Part Number 01 0770028 05 Current Draw 7 0 Amps Q 14 VDC 3 5 Amps 28 VDC Weight 2 1 Ibs Length 5 50 Height 2 01 Operation This power supply will operate up to 3 strobe lighthead assemblies When operating two lights in the alternating mode 42 joules of power are produced for each light While in simultaneous mode power to each light is 21 joules When operating 3 lights strobe outlet 1 pro duces 42 joules of power and alternates with strobe outlets 2 amp 3 producing 21 joules each that flash simultaneously see Figure 13b Jumper to be inserted in trigger selector outlet Outlet Outlet Outlet 1 2 3 STROBE OUTLETS 1 2 3 N C Connector for input power cable STROBE HOOK UP PIN 1 RED ANODE PIN 2 BLACK CATHODE Figure 13a 3 WHITE TRIGGER Trigger Function Jumping pins 1 and 2
30. RING 3 38 0230946 00 GASKET 4 02 0350053 00 SA406 FLASH TUBE ASSEMBLY 5 N A 6 32 x 3 8 PPHMS MS51957 28 6 N A 86 32 x 5 16 SS HEX NUT MS35649 264 7 01 0770619 00 POWER SUPPLY HR CF 14 28V 8 19 130074 100 A440 MOUNTING FLANGE OPTIONAL 9 N A 6 INT TOOTH L W MS 35333 71 10 N A 36 32 x 1 2 PPHMS MS51957 30 T 18 00 1 00 i WHITE BLACK GROUND 2015 Whelen Engineering Company Inc Document 05131 Rev D 33 STROBE LIGHTHEAD ASSEMBLIES MODEL A470A SERIES A470A series remote strobe light assembly is compatible with all Whelen power supplies It can be installed on the fuselage or the vertical fin The unique polycarbonate optic lens and reflector design re directs stray light rays into the horizontal plane to provide the maximum 360 of uniform light coverage possible Available in three different lens colors Aviation Red Aviation White and split Aviation Red White Available in radio shielded configurations All assemblies require either the model H102 or H103 mounting adapter Model A470A Specifications Exposed Part I Polycarbonate Input Current Number Optic Lens Approvals Operational Voltage ven Masa m 01 0770019 18 01 0770019 20 Split Red White SE Dependant enne Tm 3 75 Comm 01 0770019 21 o Rd power supply used 2 5 64mm 01 077001922 Rado Shielded A470ADS 01 0770019 23 Split Red White Model Numbers A470AR A470AW 01 0770019 19 A470AS
31. con Position 1 28VDC White nected by FAA approved techniques using approved hardware Position 2 Ground Black 5 Make sure the existing system is equipped with an appropriate 171 x orizonta oun sized breaker u 7101103 7101113 6 Remove two 44 40 screws from taillight assembly Save these I m Model 7101103 shown for reference screws 3 46 35mm I 7 Install the light assembly and insure that all the leads are clear of CT dame any obstructions and ty wrap as required Secure light assembly 2 2 16 T iue using approved vibration resistant hardware methods 53mm Mounting Sonawa g Note Top marking on the unit 200 8 Re mount the lens and retainer onto the assembly Attach the T TYP 2 PLCS i 225 lens and retainer with mounting screws provided 20AWG Teflon Wire 9 Check all avionics systems for interference from this installation 8 203mm _ 1 00 25mm 95 24mm Square 10 When waterproofing the assembly to the aircraft apply aviation approved single part silicone RTV or equiva Position 1 14VDC Red lent around the periphery with caution Do not fill the dS 44 Document 05131 Rev D Model 71011 Series Exploded View Parts Figure 45a Model 7101102 2 Places e 2 Places 2 Places Model 7101103 2 Places 2 Places Model 7101112
32. designed to fit inside an A440 mounting adapter mounting holes to fit in place of rotating beacons Whelen model HRCFA or 7090004 05 series LED beacons Model 90520 LED Flashing Beacon Specifications Model Part Numbers Number 28 VDC Operation The Model 90520 series LED Flashing Split Anti Collision Light Assembly meets the requirements of FAR 91 205 c 3 CONTINUED AIRWORTHINESS The 90520 series LED Flashing Split Anti Collision Light Assembly is designed with 4 vertical columns consisting of 4 red LEDs each and 4 vertical columns consisting of 3 white LEDs each Should any one LED or any vertical column fail the unit must be repaired or replaced Inspect the lens and replace if there is excessive scratching discoloration or cracking INSTALLATION PROCEDURES The following information is to assist in the installation of a Whelen LED Flashing Split Anti collision Light System 1 The installation procedure described in the following text will be confined to a single light installation but is identical for multiple light installations 2 Using the suggested mounting hole pattern prepare the aircraft for means to secure the LED Flashing Split Anti collision Light assembly Remove any existing mounting adapters 3 75 Adapter Clear LED Red White 9052015 91 0 90920 19 Flying Leads Lower Polycarbonate 1 6 Document 05131 Rev D TSO C96a CLASS III APPROVED 9052001 51 9052005 15 55 Mount 0
33. front of the aircraft 0 degree to 110 degrees left and right horizontally and 180 degrees up and down vertically unobstructed by any part of the aircraft The tail position light must project its Aviation White light toward the rear of the aircraft 70 degrees horizontally left and right from 0 degree straight back behind the aircraft 180 degrees up and down 0 04 Steradian 131 36 sq degrees interference is allowable reference FAR Part 23 1387 c More than one light is acceptable 2015 Whelen Engineering Company Inc POSITION LIGHTS AND ANTI COLLISION LIGHT DISTRIBUTION PATTERNS REQUIREM ENTS An approved anti collision An approved anti collision strobe light system must proj strobe light system must proj ect light 360 around the air ect light or 30 above and craft s vertical axis One or below the horizontal plane of more strobe lights can be used the aircraft One or more strobe lights can be used The or 75 projected light is required since July 18 1977 Approved light pattern in the horizontal plane The anti collision wingtip mounted lights must converge within 1200 feet directly in front and rear of the aircraft on center line If the wingtip strobe light convergence is greater than 1200 ft in back of the aircraft a 3rd light is necessary LOCATIONS ON THE AIRCRAFT FOR ANTI COLLISION STROBE LIGHTS TO COMPLY TO THE LIGHT PATTERN REQUIREM ENTS WINGTIP Two wingtip strobe lights
34. modified the Type E Series Wingtip Navigation Light by cutting off the back 1 3 inch and designed their wingtip to fit in closer to the light it will be necessary to do a little fiberglass work when completing this installation The A650 can be installed on these Cessnas in the manner below and instructions above 1 Remove the wingtip and the navigation light assembly 2 Take a complete Model W1285 navigation light with an A650 head assembly installed or an A650 PR or PG and place it in position on the wingtip Mark around the navigation light base plate to get an outline of the navigation light profile on the wingtip 3 File or trim away the excess wingtip material to allow the navigation light and the A650 strobe light assembly to fit neatly in place Allow at least 0 060 inch clearance around the A650 strobe head assembly and the wingtip To fill in the hole in the wingtip made by this trimming and to provide a platform for the navigation and strobe light assembly mount the naviga tional light base plate on the wingtip using the two 2 forward screws with a sheet of polyvinyl between the wingtip and the base plate for a parting agent Tape the polyvinyl back over the wingtip to form a seal so it is pos sible to apply a polyester resin putty or epoxy putty like Bondo on the inside of the tip Build up the trimmed area with this putty as to have about 1 4 inch of material under and in back of the base plate Prepare th
35. the light assembly and lens 5 Check all avionics systems for interference from this installation GROUND BLACK 18GA T TEFLON WIRE 12 1 L 6 A flight check should be performed by a properly certified pilot 7 All inverted bottom mounted units shall require waterproofing of the flasher base assembly to the aircraft Note Drill a 1 8 hole in the center of the lens for bottom mount units 14VDC RED 18GA 28VDC WHITE 18GA 8 Update aircraft records complete Form 337 and obtain FAA field TEFLON WIRE 12 1 LG TEFLON WIRE 12 1 LG approval for installation If not covered under STC eligibility list on MODEL 7105500 on MODEL 7105501 30 Document 05131 Rev D Models 7105500 7105501 Exploded View Parts Figure 31a GROUND BLK TEFLON WIRE 18GA 12 LG Model 71055 series LED installation 14VDC RED TEFLON WIRE 18GA 12 LG 116 32 Flat Head ES 100 Countersink a Mounting Figure 31b 4x 6 32 Mounting Holes Equally Spaced on a 01 625 Bolt Circle typ 4x 6 32 Mounting Holes Equally Spaced on A 01 250 Bolt Circle Suggested Mounting Hole Pattern Model 71055 Series Parts List QTY QTY ITEM PART NUM BER DESCRIPTION j 01 0771055 00 MODEL 7105500 14V 01 0771055 01 MODEL 7105501 28V 1 1 01 0271843 00 LED MODULE ASSEMBLY 6 SIDED 14V 1 1 2 07 771051 100 ADAPTER PLATE MODEL 71055 SERIES 4
36. this plate between the navigation light and its mounting surface and locate the A625 strobe head below the navigation light Spare Parts QTY ITEM PART NUMBER DESCRIPTION j 01 0770058 03 STROBE LIGHT ASSY MODEL A625 01 0770058 13 STROBE LIGHT ASSY MODEL A625D 2 2 1 N A 14 40 X 1 2 PPHMS 551957 17 Bend and trim the adapter plate as necessary so that the A625 clears the 1 3 68 2290005 30 LENS CLEAR A612 transparent window that covers the navigation light area 0 060 inch minimum 1 1 4 38 0250074 00 GASKET The conduit for the navigation light wire is very small To get the necessary 1 1 5 02 0370338 00 A627 FLASHTUBE ASSY wires to operate the strobe light and the navigation light through this conduit use a 20 gauge wire with less that 0 060 inch OD It has been found that the 2 2 6 N A 4 40 HEX NUT BRASS Belden 8502 or 8308 has an 0 058 inch OD 1 8 68 2290005 34 LENS RFI COATED A612C 2015 Whelen Engineering Company Inc Document 05131 Rev D 41 MODEL A500A SERIES INSTALLATION _ e lt gt A500A Series Combination Strobe Tail Navigation light used when the wingtip Anti Collision lights are is mounted in an enclosure and can t provide 360 of strobe coverage It is a direct replacement for the gt standard Tail Position light Available in a radio shielded version Voltage 14 or 28
37. to change any of the existing wiring or circuit breakers The light assembly must be properly mounted to comply with FAR Part 91 205 c 2 amp c 3 When necessary such as fuselage installation the Whelen model A440 mounting adapter must be used Mounting 1 Remove the existing beacon 2 Make the necessary wiring connections using the existing wiring Positive to the WHITE wire and Ground to the BLACK wires protruding from the light assembly All connections must use FAA approved techniques Note It is recommended to ground the unit to the buss bar or the battery Using the airframe as ground may produce EMI RFI interference 3 Remove the three 3 6 32 x 3 8 mounting screws from the light assembly Do not use longer screws damage to the unit may occur 4 Insert light assembly into mounting location and attach using screws as mentioned in step 3 There are two sets of mounting screw locations on the unit for installation versatility unit may be sealed around periphery with RTV or equivalent 5 If the A440 mounting adapter is used attach light assembly to adapter 32 Document 05131 Rev D using screws as mentioned in step 3 unit may be sealed around periphery with RTV or equivalent 6 If light assembly is mounted in an inverted position drill a 1 8 diameter hole in lens as indicated on the lens label For the model SACF series remove the RTV plug from the hole in the lens T When installing the li
38. 0 40 LENS GREEN W1284 G 6 68 4230020 50 LENS RED W1284 R y 19 170049 009 LENS RETAINER A606 8 02 0350260 00 SOCKET ASSY A507 9 N A 6 32 X 5 16 PHILLIPS FHMS MS51959 27 10 34 0412070 63 LAMP 14V A508 14 11 34 0428070 64 LAMP 28V A508 28 12 68 4250066 30 LENS TAIL POSITION A615 13 38 0230021 00 GASKET W1283 14 38 0130090 00 GASKET A616 16 68 2290005 34 LENS RFI COATED A612C 17 38 0130107 00 GASKET A427 4 18 68 2290005 30 LENS CLEAR A612 ZAT y N Model A600 Installation 2015 Whelen Engineering Company Inc Document 05131 Rev D 49 MODEL A650 SERIES INSTALLATION A650 series converts W1285 position lights into a position anti collision system by removing the existing retainer amp replacing it with the A650 assembly Radio shielded version available Model A650 Specifications Model Part ud Exposed A650 01 0770053 00 Standard Unit m White FAA PMA 0 2 Ibs 91gm 2 4 61mm A650D 01 0770053 13 Radio shielded A650 Operation Converts existing Whelen W1285 position lights into a position anti collision light system by removing the existing retainer and replacing it with the A650 assembly Available in a radio shielded version A650 Wingtip Strobe Light To install the Whelen A650 strobe lighthead assembly on the aircraft proceed with the following instructions Remove the wingtip navigation light a
39. 0 8 lbs 363gm 5 63 143mm power supply 1 7 43mm Observe the following strobe color coding PIN 1 RED Anode PIN 2 BLACK Cathode PIN 3 WHITE Trigger Caution When pins 1 amp 2 or pins 2 amp 3 are reversed the system will appear to operate normally however this condition will cause pre mature flash tube failure 2 Connect the forward position light wires as follows RED 14 or 28 volts depending on aircraft voltage BLACK Ground 3 The tail position light has no polarity as noted by both wires being BLUE Connect one BLUE wire to 14 or 28 volts depending on aircraft voltage Connect the other BLUE wire to ground see Figure 48b Dimensions 5 63 Figure 48b 143mm 4 1 83 D mm 1 66 42mm 15 4mm TAIL LIGHT WIRES BLUE NO POLARITY POS 3 WHITE TRIGGER POS 2 BLACK CATHODE POS 1 RED ANODE RED 14 or 28VDC X BLACK GROUND 1 35 34mm 18 AWG TEFLON DIA LEAD LENGTH 6 00 1 00 Model A600 SERIES Exploded View Parts Figure 49a 9 Model A600 Series Replacement Parts List T T ITEM PART NUMBER DESCRIPTION 1 02 0350259 00 BASEPLATE ASSY A605 EE SO rid 2 02 0250276 00 FLASH TUBE ASSEMBLY A610 3 34 0414020 65 LAMP 14V W1290 14 4 34 0428020 65 LAMP 28V W1290 28 5 68 423002
40. 1 13 46 0750898 01 Ass y 14V Pigtail 6 Blk Red 1 14 01 0271848 01 Assy 28V LED Anti Collision Light 71080 1 15 07 771051 200 Plate Adapter Model 4 Hole 2015 Whelen Engineering Company Inc Document 05131 Rev D 23 Dimensions Models 7108004 7108014 5X 156 Thru Suggested Mounting Fiaure 24 Exploded View Parts Figure 24a C SINK to 9 281 x 100 Pattern gure 24b spaced as shown on 84x 24 656 Bolt Circle 25 7 4 D 5 6 B Mounting Figure 24c Q 125 1 Drain Hole NC Lower Mount Only 02 60 oie 66mm 131mm Q 1 VIEW PRIOR TO REV 2 73 06 e 3 64 92mm 9 Model 7108004 7108014 Series Parts List QTY QTY ITEM PART NUMBER DESCRIPTION 01 0771080 04 Model 7108004 28V Upper bi 01 0771080 14 Model 7108014 28V Lower 1 1 1 01 0271848 00 Assy 28V LED Anti Collision Light 71080 Mfg Label 1 1 2 38 0250885 00 Gasket Lens Model 71055 Series 1 3 68 4971082A30 Lens Clear LED Anti Collision Hard coat 42 44 1 4 68 4971082A31 Lens Clear LED Anti Collision with Drain Hard coat 309mm 1 1 5 07 571304 100 5 Hole Adapter Lens Retainer lridite 1 1 6 38 0250225 00 S
41. 108006 01 0771080 06 A470A Mount 3 75 Adapter MSConn Lower 5 Hole Adapter MSConn 5 Hole Adapter Flying Leads Lower 3 75 Adapter Flying Leads Lower 3 75 Adapter MSConn Lower 5 Hole Adapter MSConn Lower EC120 130 135 Adapter EC120 130 135 Adapter MSConn A470A Mount Mate N Lock 3 75 Adapter Flying Leads 7108007 01 0771080 07 7108008 01 0771080 08 Clear 7108014 01 0771080 14 7108015 01 0771080 15 7108017 01 0771080 17 7108018 01 0771080 18 7108020 01 0771080 20 7108030 01 0771080 30 7108051 01 0771080 51 7108055 01 0771080 55 roos Operation The Model 71080 series LED Anti Collision light assembly meets the requirements of FAR 91 205 c 3 CONTINUED AIRWORTHINESS The 71080 series LED anti colli sion light assembly is designed with 8 vertical columns consist ing of 4 LEDs each Should any one LED or any vertical column fail the unit must be repaired or replaced Inspect the lens and replace if there is excessive scratching discoloration or cracking INSTALLATION PROCEDURES The following information is to assist in the installation of a Whelen LED Flashing Anti collision Light System 1 The installation procedure described in the following text will be confined to a single light installation but is identical for multiple light installations 2 Using the suggested mounting hole pattern prepare the aircraft for means to secure the LED Fla
42. 6 A427 A427 4 A428 A428C A428D A435 A440 A441 A442 A443 A444 A446 A455 A457A A457AD A457BDH A457BDV A469A A469B A469D A469DK A504 A506 A507 A50814 A50828 A605 A606 A610 A612 A612D A615 A616 A626 01 0450685 00 68 2170504 50 68 2170504 60 68 2170504 30 11 430005 100 19 130000 100 19 0150350 01 19 0150350 02 19 190000 009 02 0250274 00 38 0130107 00 68 4290001 30 02 0350033 00 02 0350057 00 02 0350054 00 19 130074 009 01 043001 1 00 01 0410823 00 02 0230081 00 02 0230007 00 02 0230085 00 38 0230002 00 68 4270002 30 02 0350038 35 02 0350038 37 02 0350038 36 01 0770044 00 01 0770044 02 01 0770044 01 01 0710834 00 06 150058 001 02 0350034 00 02 0350260 00 34 0412070 63 34 0428070 64 02 0350259 00 19 170049 009 02 0250276 00 68 2290005 30 02 0350071 35 68 4250066 30 38 0130090 00 19 170052 009 Description Clamp Ring Assy A626D Optic Lens Red Optic Lens Split Red White aie Optic Lens White Taillight Mounting Cup SA402 Taillight Lens Retainer SA406 Retainer Horizontal Mount SA4181 Retainer Vertical Mount W1282 Retainer for A428 Lens W1283 Strobe Tube Assy W1284G Gasket Spacer for A428 Lens W1284R Lens W12852 Lens Radio shielded W129014 Lens Retainer Assy Radio shielded W129028 Strobe Tube Assy A430 Series Mounting Adapter Ring Kit 3 Pin Connector amp contacts Kit 3 Socket Connector amp contacts Trigger Jumper Plug for HDACF Kit 2 Pin Connector a
43. 67 amps 3 0 amps peak average 9 3 seconds 9 6 lbs 272gm 1 34 amps 6 0 amps peak average 3 seconds 0 65 Ibs 295gm 0 8 Ibs 363gm FAA TSO C96a Class 111 0 67 amps 3 0 amps peak average 3 seconds 0 75 Ibs 340gm 0 8 Ibs 363gm 1 34 amps 6 0 amps peak 14 or 28 VDC and ground leads equipped with an appropriate sized breaker to be supplied to the LED Flashing oplit Anti Collision Light Assembly System Both leads must be connected by an approved FAA connection Insure that the wire leads are clear of any obstructions and ty wrap as required Install the light assembly by securing to the aircraft using appropriate approved hardware Refer to page 2 All inverted bottom mounted units shall require waterproof ing of the flasher base assembly to the aircraft Check all avionics systems for interference from this installa tion A flight check should be performed by a properly certified pilot Update aircraft records as required Update aircraft records complete Form 337 and obtain FAA field approval for installa tion if not covered under STC eligibility list Models 9052001 9052051 Exploded View Parts Dimensions Figure 17a Figure 17b Model 9052001 amp 9052001 Parts List QTY QTY ITEM PART NUM BER DESCRIPTION 01 0790520 01 Model 9052001 28V 01 0790520 51 Model 9052051 14V 07 771051 100 Adapter Plate 8
44. 8 D 9 14 VDC 1 32 m Clear pan 0 72 Amp Avg ACL 9 TSO ETSO C30c yr II Hard coaled White 45 5 Polycarbonate OR5002V 01 0771774V02 28 VDC Whi I 1 0 10 Amp Position FAA Eo C96a Class 11 8 III Field 22 32 VDC t 20 Ibs Replaceable 0 36 Amp Avg ACL 32gm TSO ETSO C30c Eo Operation Operation cont d EQUIPMENT LIMITATIONS 7 A flight check should be performed by a properly An approved position lighting system consists of three lights one certified pilot located the tail and one on each wingtip Model OR500 is a tail 8 Update aircraft records complete Form 337 and obtain position and anti collision light The assembly should be mounted as FAA field approval for installation if required far aft on the aircraft as practicable on a thermally conductive sur face The baseplate must be mounted parallel to the vertical and Dimensions and Mounting Detail horizontal centerlines of the aircraft to project the patterns properly Figure 7a Certain types of installations may require additional testing uM 43mm CONTINUED AIRWORTHINESS The tail position light is designed with 4 LEDs The anti collision light is designed with 18 LEDs If any one LED fails the unit must be repaired or replaced Inspect the lens replace if there is excessive scratching pitting discoloration or cracking Note To reduce eye strain use an optical filter such as dark glasses or a blue covering dome during LED inspection INS
45. BE ASSEM BLY 71110 series is a wing tip mounted strobe anti collision position light assembly utilizing LED s for the forward position lights The LED s pro vide a significant reduction in current draw over conventional position light bulbs The strobe light lens assembly is radio shielded for maximum EMI RFI protection Direct replacement exact footprint for the Whelen Model A650PG PR series without replacing the current strobe power supply Navigation light portion is wired with flying leads Model 71110 Specifications TSO C30c TYPE APPROVED TSO C96a CLASS APPROVED Nav Light Model Part LED Operational Exposed mons 0771110 01 Strobe Color White Aviaion Green Green FAA TSO C96a Class II TSO C30c Type II 14 VDC mt Coated 7111002 01 0771110 02 Heat Tel Shielded Lens Aviation Red FAATSO C96a Class Il TSO C30c Type 14 VDC Clear Polycarbonate 7111004 01 0771110 04 Hard coated Lens Operation EQUIPMENT LIMITATIONS An approved lighting system consists of two lights one located on each wingtip The baseplate must be mounted parallel to the vertical and horizontal centerlines of the air craft to project the patterns properly The strobe tube assembly must be connected to a strobe power supply such as Whelen model 70888 70879 or other approved models CONTINUED AIRWORTHINESS The 71110 series LED wingtip posi tion light assembly is designed with 3 LED s If any one LED fail
46. Do not cover the drain hole or the back Red 12VDC ACL White 28VDC ACL of the unit Orange 12VDC POS Orange 28VDC POS 6 Check all avionics systems for interference from this ee 5 installation 2015 Whelen Engineering Company Inc Document 05131 Rev D 7 ORION Model OR5001V 12V Series Exploded View Parts Figure 8a CAUTION DO NOT TOUCH THE LED LENS SURFACE WITH EITHER FINGERS OR SHARP OBJECTS THIS COULD SOIL AND OR DAMAGE THE LENS AND EFFECT THE OPTICAL PERFORMANCE OF THE LEDs e epe lt 4 sx 3 Model OR5001V Parts List SD QTY ITEM PART NUMBER DESCRIPTION x 01 0771774 01 ORION 500 Model OR5001V 12 VDC 2 2 1 14 040216 160 Screw 4 40 x 1 PPHMS SS 2 2 19 151080 100 Retainer lridite 1 3 68 3951061 A31 Lens Model 90667 No Drain Slot Hardcoat 1 For shipping purposes 1 4 38 0131364 00 Gasket VHB Seal 1 5 01 0290717 00 Sub Assy ORION 500 Model OR5001V 12 VDC 2 6 13 040130 040 Nut 444 40 X 1 4 Hex Brass ORION Model OR5002V 28V Series Exploded View Parts Figure 8b CAUTION DO NOT TOUCH THE LED LENS SURFACE WITH EITHER FINGERS OR SHARP OBJECTS THIS COULD 2 SOIL AND OR DAMAGE THE LENS 9 AND EFFECT THE OPTICAL gt PERFORMANCE OF THE LEDs 225 ee 2 O 7 4 3 Mode
47. Document 05131 Rev D ESTABLISHING SOLID ANGLE BLOCKAGE WITH REFERENCE TO AC 43 13 2A CHAPTER 4 1 To determine the vertical angles to use with reference to Figure 7 and 8 of the aforementioned chapter 4 attach a long string to the subject light source location 2 Fix navigational type plotter or protractor to the string with weighted thread fixed to the center of the scale for a plumb bob 3 Level the aircraft or determine the offset angle 4 Pull the string over the point of solid angle blockage Ref Fig 6 page 4 Any angles greater than 75 degrees vertical are not a factor 5 Apply the vertical and horizontal angles to the graph paper Ref Fig 4 8 and instructions in text of paragraph b6 amp c of Chapter 4 A flight test will be performed by properly certified pilot with reference to paragraph 52 a b of Chapter 4 COMPLETING THE ANTI COLLISION LIGHT INSTALLATION 1 Check all avionics systems for interference from this installation reference AC 43 13 2A Chapter 4 Paragraph 52 b 2 A flight check will be performed by a properly certificated pilot with reference to AC 43 13 2A Paragraph 52 a and b 3 If a solid angle blockage document must be established it should be performed after all masking has been installed and all flight test ing is completed See page 3 of this manual 4 WATERPROOFING OF STROBE LIGHT INSTALLATIONS When necessary to waterproof the installation of a strobe light
48. FAA TSO C96a Class Ill Clear 7105501 01 0771055 01 28 VDC 22 32 VDC 0 56 Amp Avg ACL gos subs Operation TSO C96a Class Ill approved The conditions and tests Equipment Limitations The Model 71055 Series LED anti collision iuba for TSO approval of this article are 1 light assembly meets or exceeds the requirements of FAR 23 1401 performance standards It is the responsibility of those and FAR 91 205 c 3 installing this article either on or within a specific type or s u DIE class of aircraft to determine that the aircraft installation Continued Airworthiness The 71055 Series LED anti collision light conditions are within the TSO standards TSO articles assembly IS designed with 6 vertical columns consisting of 2 or 3 must have separate approval for installation in aircraft LED s each Should any one LED or any vertical column fail the unit The article may be installed only if performed under 14 must be repaired or replaced Periodically inspect the lens and CFR part 43 or the applicable airworthiness require replace if there is excessive scratching discoloration or cracking ments Installation Procedures The Model 71055 is a self contained flash ing beacon that requires no external flasher or power supply In some Dimensions installations it may be necessary to remove several existing compo Figure 30a nents When replacing flashing halogen beacon assemblies the flasher box and ballast resistor if present and ass
49. Figure 35d QTY QTY QTY QTY QTY QTY ITEM PARTNUMBER DESCRIPTION 01 0770019 18 Strobe Assy Red A470A R d 01 0770019 19 Strobe Assy White A470A W 3 50 01 0770019 20 Strobe Assy Red White A470A R W 89mm 01 0770019 21 Strobe Assy R S Red A470A D R 01 0770019 22 Strobe Assy S WHITE A470A D W 01 0770019 23 Strobe Assy R S R W A470A D R W 1 1 68 2170504 50 Lens Assy Red 1 2 68 2170504 30 Lens Assy White 1 3 68 2170504 60 Lens Assy Red White 1 4 68 2170504R50 Lens Assy R S Red 1 5 68 2170504R30 Lens Assy R S White 1 6 68 2170504R60 Lens Assy R S Red White 66mm DIA 1 1 1 1 1 1 8 01 0450685 00 Clamp Ring 2 50 A470A 1 1 1 9 38 0250429 00 Gasket Shielded 1 1 1 1 1 1 10 01 0770044 02 Flashtube Assy A469B 1 1 1 1 1 11 N A 6 32 x 1 2 Phillips PHMS MS51957 30 Ex 1 1 1 12 38 0230840 00 Gasket 1 1 1 1 1 1 15 N A 6 32 x 5 16 SS Hex Nut MS35649 264 17 02 0350600 01 Lens Assy Masked White SACF Dimensions Exploded View Figure 35e Figure 35f REMOVE RTV WHEN UNIT IS MOUNTED IN AN INVERTED POSITION QTY ITEM PART NUMBER DESCRIPTION s 01 0770032 00 A450 STROBE LIGHT HEAD ASSEMBLY 1 1 02 0350053 00 FLASH TUBE ASSY 1 2 38 0230946 00 GASKET LENS 046 THK 1
50. NUMBER DESCRIPTION 01 0770053 00 01 0770053 13 A650 STROBE ASSY A650 D STROBE ASSY SHIELDED CLEAR 68 2290005 30 LENS CLEAR A612 68 2290005 34 LENS RFI COATED A612C 19 170052 009 RETAINER LENS A626 02 0250276 00 FLASHTUBE ASSEMBLY A610 N 38 0130106 00 A427 3 GASKET STROBE POWER SUPPLY CROSS REFERENCE REPLACEMENT LISTING Old Part Number Old Model Number Description Current Replacement p p es ee PN 01 0770029 HR DFA 14 28 Self Contained Strobe DoubleFlash 14 or 28 VDC A402A lens 2015 Whelen Engineering Company Inc Document 05131 Rev D 51 CONTINUED AIRWORTHINESS FLOW CHART Inspect Lens Excessive scratches discolorations or cracking Yes Replace Lens No Check Lens Mounting Loose or missing hardware Yes Tighten or Replace No Check Operation Improper Operation m Check wiring and connections Refer to trouble shooting procedures for No strobe lights Complete 52 Document 05131 Rev D STROBE SYSTEM TROUBLE SHOOTING TROUBLE SHOOTING PROCEDURES FOR AVIATION ANTI COLLISION STROBE LIGHT SYSTEMS WHEN REPAIRING WHELEN ANTI COLLISION STROBE LIGHT SYSTEMS USE ONLY WHELEN FAA APPROVED HARDWARE BE CAREFUL OF STROBE LIGHT PARTS THAT ARE SIMILAR IN APPEARANCE The Whelen Aviation Strobe Light is a condenser discharge strobe light system A condenser is ch
51. Shielded Molex A650PRDM 01 0770054 15 Position Red Red Position Green Green Position Green Standard Assembly Position Red Position Red Position Green Position Green Radio Shielded Position Red Installation The A650 Series must be properly mounted to comply with FAR Part 91 205 c 2 amp c 3 The light assembly must be mounted so that the light distribution pattern is not obstructed by any parts of the aircraft A limited amount of obstruction is permitted Ref FAR Part 23 1401 for anti collision lights and PAR 23 1387 for position lights The baseplate must be mounted parallel to the vertical and horizontal centerlines of the aircraft to project the patterns properly These assemblies are interchangeable with the Grimes model A1285 position light Mounting 1 If necessary fabricate the mounting pattern using dimensions found in Figure 16b Note A 1 diameter hole is needed for the connector to pass through 2 Make the necessary wiring connections using 18 gauge wire for the posi tion lights and Whelen 16 gauge 3 c cable for the strobe lights All connec tions must use FAA approved techniques 3 Remove the 6 32 x 312 retainer mounting screw and retainer 4 Attach the base assembly to the wingtip using 3 46 32 counter sunk screws unit may be sealed around periphery with RTV or equivalent 5 Re attach lens retainer Wiring 1 The strobe connector should plug into the Whelen 16 gaug
52. T NUM BER DESCRIPTION I 1 68 2170504 50 LENS A402AR 2 68 2170504 30 LENS A402AW x gt 3 68 2170504 60 LENS A402AS 3 67 DIA X9 93mm 4 68 2170504R50 LENS A402ADR 5 68 2170504R30 LENS A402ADW Mounti ng EN 6 68 2170504R60 LENS A402ADS Figure em OI SLE x 14 15 7 6 32x1 2 PPHMS MS51957 30 8 01 0450685 00 CLAMP RING BAN 9 N A 6 32 X 5 16 SS HEX NUT MS35649 264 10 38 0230840 00 GASKET 11 38 0250429 00 RFI GASKET i XN 12 01 0770044 02 A469B FLASH TUBE ASSY Ws 13 01 0770619 00 POWER SUPPLY ASSEMBLY NES 14 6 32x3 8 PPHMS MS51957 28 15 6 INT TOOTH LW MS35333 71 6 18 00 50 16 19 130074 100 A440 MOUNTING FLANGE OPTIONAL 5 00 4 65 DIA B C BLACK GROUND WHITE 14 28V Exploded View Figure 33e Dimensions Figure 33d Shown Rotated for Illustration of Parts as i 7 2 97 S 1 75 44mm LOCATION y I 3 67 DIA 93mm Mounting Figure 33f 5 HOLES 75 75 5 00 DIA ee 4 65 DIA B C 8 ES y T E um p Model SACF Parts List ITEM PART NUM BER DESCRIPTION 1 68 4230044 30 SA402 LENS CLEAR 2 01 0450685 00 CLAMP
53. TALLATION PROCEDURES The following information is to assist you in installing a Whelen light system A N 125 32mm Dia 44mm 1 Choose the appropriate light assembly TT 1 125 2 Using the mounting detail information provided prepare the omy aircraft for means to secure the light assembly d 3 Connect the light inputs according to the chart shown Connect Wire 20AWG the power lead to an appropriate sized breaker Connections to be A in accordance with FAA approved methods Note SYNC is a low Drain Passage on both sides power bi directional control signal Connecting to the synchro Suggested Mounting Detall nize signal of any Whelen LED anti collision assembly to another Whelen anti collision assembly will cause the lights to flash at the same time If synchronization is not necessary the connection M may be left open 1 150 29mm 4 Proper installed orientation is achieved with the drain hole down 1 75 Note The arrow on the label must point up Install the light SD ies assembly on to the aircraft Insure that all leads are clear of any 22mm obstructions and secured as required p 5 When necessary waterproof the light base to aircraft Apply single part Silicone RTV or equivalent around any open area WIRING 12V WIRING 28V where water could get in
54. VDC B GRD 1 15 10 0315069 14 Label Voltage ID 28V 1 1 16 38 0271394 00 Gasket Adapter LED Beacon EC Style 1 17 01 0271848 03 Assy 28V LED Anti Collision Light 71080 2015 Whelen Engineering Company Inc Document 05131 Rev D 27 SELF CONTAINED LIGHT ASSEMBLIES MODEL 70900 SERIES TSO C96a CLASS FLASHING ANTI COLLISION LIGHT ASSEM BLY APPROVED 70900 series are FAA TSO compliant self contained anti collision lights for fixed wing aircraft An external power unit is not required Conservative lab life results greater than 20 000 hours No EMI or RFI produced All units meet the minimum requirements stated in FAR Parts 23 amp 25 for anti collision light systems used on fixed wing aircraft Ref Class 111 100 effective candela of SAE AS8017a minimum performance standards STC SA615EA approved Models 7090004 amp 7090005 are designed to replace existing light assemblies with the 3 3 4 95mm dia mount ing pattern Ref Whelen HRCFA series 90081 series and old style rotating beacons It has the same mounting hole pattern No modification to the aircraft is required Model 70900 Specifications Model Part LENS 7090004 01 0770900 04 3 3 4 dia mount 2 1 7090005 01 0770900 05 Aviation Red Operation Equipment Limitations The Model 70900 series LED anti collision light assembly meets the requirements of FAR 23 1401 25 1401 and 91 205 c 3 If certification for n
55. WG 6 00 1 00 MIL W 22759 43 7108051 CONNECTOR WIRING AMP 1 480319 0 7108001 18AWG 12 1 LG 7108006 18 AWG 24 1 LG POS 1 RED 28VDC WHITE 18GA 28VDC WHITE 18GA Po amp 1 9 RED GROUND BLACK 18GA GROUND BLACK 18GA 7108001 18AWG 12 1 LG MIL W 22759 43 MIL W 22759 43 22VDC WHITE 18GA GROUND BLACK 18GA MIL W 22759 43 Model 71080 Series Parts List d E SEC x Za 112 pM LG QTY QTY QTY ITEM PART NUM BER DESCRIPTION 01 0271080 01 Model 7108001 28V i 01 0271080 51 Model 7108051 14V 01 0271080 06 Model 7108006 28V 1 1 01 0271848 00 Assy 28V LED Anti Collision Light 71080 01 0271848 50 Assy 14V LED Anti Collision Light 71080 07 771051 100 Plate Adapter Model 8 Hole 16 0050506136 Washer 6 Lock Spring MS35338 136 7108006 18AWG 24 1 LG 4 4 4 22VDC WHITE 18GA 4 4 GROUND BLACK 18GA MIL W 22759 43 38 0250885 00 Gasket Lens Model 71055 Series 68 4971082A30 Lens Clear LED Anti Collision Hard coat 2 3 4 5 14 0050503123 Screw 6 32 X 9 16 PPHMS SS 551957 123 6 7 8 GROUND BLK 28VDC WHT WIRE 18GA 24 LG WIRE 18GA 24 LG 1 1 19 171047 100 Retainer Lens Iridite Complete 4 4 4 9 16 0050506135 Washer 4 Lock Spring MS35338 135 4 4 4 10 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 1 1 12 10 0315069 14 Label Voltage ID 28V
56. ail ONO AA WIN Model A500A Installation 2015 Whelen Engineering Company Inc Document 05131 Rev D 43 LED LIGHT ASSEMBLIES MODEL 71011 SERIES LED TAIL POSITION LIGHT ASSEMBLY 71011 series are LED tail position lights designed to replace the existing old style tail lights typically seen mounted on most general aviation corporate and helicopter applications They have all the advantages associated with using LED s as a light source improved reliability and reduced operating costs and are available with horizontal or vertical mounts with 14 Volt or 28 Volt versions TSO C30c TYPE III APPROVED Model 71011 Specifications Mounting Model Part LED Operational Input Exposed 7101102 01 0771011 02 28 VDC 7101103 01 0771011 03 0 3 Amps Aviation FAATSO C30c lll 22 30 VDC 0 2 Ibs 91gm 1 36 35mm 1 75 45mm 7101112 01 0771011 12 14 VDC 0 5 Amps 7101113 01 0771011 13 Operation Operation cont d Equipment Limitations The approved tail position light assembly drain holes at bottom of unit RTV should never be used should be mounted vertically and as far aft on the aircraft as possible between the rear surface of the light assembly and its on a thermally conductive surface mounting surface Continued Airworthiness The LED tail position light assembly is 11 Update aircraft records a
57. arged to approximately 450 volts DC then discharged across a xenon flash tube at controlled intervals The con denser is parallel across the xenon flash tube that is designed to hold off the 450 volts DC applied until the flash tube is triggered by an external pulse This pulse is generated by a solid state timing circuit in the power supply When trouble shooting a strobe light system first determine if the trouble is with the flash tube or the power supply This can be accom plished by replacing the flash tube assembly with a good operating flash tube or with the use of a Whelen Strobe Check unit Whelen s power supplies are protected against a short or open circuit on the output In either case the power supplies will effectively turn themselves off when subjected to a shorted output of a xenon flash tube that refuses to flash WARNING Strobe light power supplies are meant to be used not to remain in an inactive state Use them at all times this will improve their proper functioning Any strobe light power supply that has been out of service for a long period of time is subject to failure because the elec trolytic condenser loses the polarity formation A strobe light power supply not having been used for one year or longer is vulnerable to failure applies to 1993 amp older units If this is the case it is recommended to start operating the system on a voltage that is reduced by 25 percent for 10 to 15 minutes before putting the po
58. can develop a leak through eggshelling of the glass or a leak can develop around the seal of the wire to the glass This is caused by hot and cold cycling of normal operating of the system They can go into self ionization continuously glow a light Blue thus rendering the entire system non operational until flash tube is replaced This most likely occurs when the input voltage is highest This can be checked by turning the system off When turning the system back on it generally will operate normally for a few flashes before going back into self ionization ANY OF THE ABOVE MENTIONED CONDITIONS ARE REASONS FOR REPLACEM ENT OF THE XENON FLASH TUBE NOTE Installing one new flash tube in any multi head strobe light system will sometimes cause the remaining old flash tube to misfire or skip This signifies that the old flash tube is nearing the end of it s service life However to check the questionable flash tube install it in a system and apply a reduced voltage approximately 20 percent to the input to the power supply If the flash tube will operate at this reduced level it still has a great deal of service life in it N Jen WHELEN S CometFlash Strobe Light System con sists of four high energy pulses per burst of light 45 bursts of light per light NOTE Whelen Engineering does not recommend attempting to repair their strobe light power supplies in the field It is recommended to take advantage o
59. ctions The acceptable distance for the two wingtip anti collision strobe lights to converge in front and back of the aircraft on center line is 1200 feet If both wingtip anti collision strobe lights can be seen at 1200 feet or less directly in front and back of the aircraft it is considered a point of light source therefore a third light is not necessary The wingtip anti collision light must be located in such a way that it will project light 75 degrees above and below the horizontal axis of the aircraft and the summation of the 2 or 3 lights will project light 360 degrees around the vertical axis PILOT AND CREW INTERFERENCE In some installations it will be necessary to mask the strobe lighthead assembly to reduce pilot annoyance This interference problem varies from one aircraft to another of the same model due to paint schemes and colors The Navigation Light Detector will be a source of reflection and should be reduced in size or masked as necessary A small aluminum or plastic plate mounted between the navigation light and the wingtip protruding up or down as required like some plastic navigation light detectors and trimmed to shadow the objectionable reflected area is simple and very effective The solid angle blockage must be reviewed after installing any masking that will disturb the 360 degrees by 75 degrees pattern The afore mentioned type masking used on wingtip lighting seldom interferes with this pattern 4
60. diameter mounting hole in the vertical fin or the fuselage Radio Shielded RFI Shielded ith wi MS Connector SACF series self contained CometFlash strobe anti collision light which utilizes the same power supply amp housing as 3 2 amps 14 VDC 1 6 amps 28 VDC FAA PMA 1 5 lbs 680gm Split Red White the model HRCFA It uses an aviation White glass lens only ideal for agricultural applications where chemicals are 1 used Because the lens has no optics built in it produces 300 effective candlepower It uses a 3 3 4 dia mounting t hole Fuselage installation requires the A440 mounting adapter Operates between 10 to 30 VDC Input Current Height 3 2 Amps 14 VDC amp The model A440 Mounting Adapter is for fuselage installations for the HRCFA series and the SACF series Model Specifications Model Part Mom o lms ser oo d 3 3 4 dia mounting hole Glass A SACF 01 0770030 01 A440 MOUNTING ADAPTER he A440 mounting adapter Aviation White Model A440 Specifications Mounting Adapter for HRCFA amp SACF Series for fuselage installations A440 19 130074 009 Model Part Outside vem 140 Installation The HRCFA amp SACF self contained strobe light assemblies are interchangeable with Rotating Beacons on any aircraft with a 3 75 inch diameter fairing or mount ing adapter It is not necessary
61. e aircraft to project the patterns properly This Dimensions and Mounting Detail assembly must be mounted behind a Clear lens Certain types of Figure 11a installations may require additional testing 3x Q 150 CONTINUED AIRWORTHINESS ertet PLE oue x The forward position light is designed with Green or Red LEDs The anti collision light is designed with 24 white LEDs If any one LED 1 00 25mm fails the unit must be repaired or replaced Note To reduce eye x EE Scam dome during LED inspection EC j strain use an optical filter such as dark glasses or a Blue covering INSTALLATION PROCEDURES The following information is to assist you in installing a Whelen light system 1 Choose the appropriate light assembly 2 Using the mounting detail information provided prepare the aircraft for means to secure the light assembly 3 Carefully remove the 4 phillips head screw qty 4 Remove the light assembly from the baseplate CAUTION Do not touch the LED with either fingers or sharp objects This could soil and or damage the lens and affect the optical performance of the LEDs 4 Using the appropriate hardware install the baseplate to the aircraft 5 Route the wires through the opening in the baseplate Connect the light inputs according to the chart shown Connect the power lead to an appropriately sized breaker Connections to be accord ing to FAA approved methods Note SYNC is a low power bi directional control s
62. e inter connect ing cable or a Whelen strobe power supply Observe the following strobe color coding PIN 1 RED Anode PIN 2 BLACK Cathode PIN 3 WHITE Trigger Caution When pins 1 amp 2 or pins 2 amp 3 are reversed the system will appear to operate normally however this condition will cause pre mature flash tube failure 2 Connect the forward position light wires as follows using 18 gauge approved aviation wire or cable RED 14 or 28 volts depending on aircraft voltage BLACK Ground 36 Document 05131 Rev D Model Part Lens Peak Input Approvals FAA PMA Nav Light Input Current Height 2 0 Amps 14 VDC Dependant on strobe power supply used 1 0 4 0 Amps 28 VDC 28 VDC 1 0 Amps 28 VDC Dimensions ud 98mm Figure 36a 1 75 19mm Figure 36b Pin 1 RED Anode Pin 2 BLACK Cathode Pin 3 WHITE Trigger RED 14 28 VDC BLACK GROUND Mounting Diagram BOTTOM VIEW Figure 36c 1 00 13mm Length Width 25mm 140 DIA 3 MTG HOLES 280 DIA X 100 DIMPLE OPP SIDE A650 Replacement Parts Exploded View Figure 37a Before After With Modified Wingtip A650 Wingtip Strobe Light Installation on Later Model Cessna Wingtips with Shortened Light Base Because Cessna has
63. e surface and the putty material in accordance with the putty manufacturer s instruc tions to assure a good bond to the wingtip Remove the navigation light base plate and parting agent To improve the appearance of this installation fill the indentation on the outside of the wingtip with the aforementioned putty and file the excess material to a clean profile before painting Drill the third mounting screw hole for the navigation light and complete the installation reference the enclosed information ov SOS SS ee 552552255 2 SOS 55252505052 25 2525 550505 A gt DL 209 9 255 LER 0505 PART NUMBER DESCRIPTION 1 02 0350072 35 LENS CLEAR A626D 2 68 4230020 50 LENS RED W1284R 3 68 4230020 40 LENS GREEN W1284G 4 34 0428020 65 LAMP 28V W1290 28 5 34 0414020 65 LAMP 14V W129014 6 38 0230021 00 GASKET LENS W1283 7 38 0130106 00 GASKET FLASHTUBE A427 3 8 02 0350003 01 BASE PLATE ASSEMBLY W1285 2 10 N A 6 32 X 5 16 PHILLIPS FHMS MS51 959 27 11 19 170052 009 RETAINER LENS A626 12 68 2290005 30 LENS FLASHTUBE A612 13 02 0250276 00 FLASH TUBE ASSEMBLY A610 14 02 0250276 03 FLASH TUBE ASSEMBLY MOLEX CONNECTOR 2015 Whelen Engineering Company Inc Document 05131 Rev D 37 LED LIGHT ASSEMBLIES 71110 SERIES WING TIP LED FORWARD POSITION LIGHT STRO
64. eal HR LT Series 18AWG 12 1 Ground Black 28VDC White 4 4 7 16 0050506135 Washer 4 Lock Spring MS35338 135 28VDC White 18GA Wire 18GA Wire 18GA Ground Black 18GA 12 LG 12 LG 4 4 8 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 MIL W 22759 43 1 1 9 10 0315069 14 Label Voltage ID 28V Y Models 7108005 7108015 7108055 Dimensions Exploded View Parts Figure 24 Mounting Figure 24f Suggested Mounting Pattern 6 32 Mounting Holes 6 32 x 5 16 Suggested Screw Length Q 125 3mm Drain Hole Lower 3 66 Mount Only o 7108055 CONNECTOR WIRING AMP 1 480319 0 POS 1 1AVDC RED VIEW PRIOR TO REV K POS 2 GROUND 3 92 06 100mm Model 7108005 7108015 and 7108055 Series Parts List QTY QTY QTY ITEM PARTNUMBER DESCRIPTION 01 0771080 05 Model 7108005 28V Upper 01 0771080 15 Model 7108015 28V Lower i 01 0771080 55 Model 7108055 14V 46 32 01 0271848 00 Assy 28V LED Anti Collision Light 71080 HELI COIL insert 01 0271848 50 Assy 14V LED Anti Collision Light 71080 i 38 0250885 00 Gasket Lens Model 71055 Series 68 4971082A30 Lens Clear LED Anti Collision Hard coat
65. ed to ground The radiation of RF energy is reduced to a minimum by properly terminating the shield at one end or the other generally the power supply end but which ever proves the quietest ground Do not terminate both ends When installing a strobe light system provide a good ground and a low impedance source to the strobe light power supply Eliminate ground loops in audio circuits by using a centrally located ground point for all audio grounds Whelen Engineering has available RF shielded flash tubes and strobe lighthead assemblies to suppress the trigger pulse or clicking some times heard in the radios If noise problems persist and the procedures described have not cleared them up please contact the Whelen Engineering Company for assistance STROBE SYSTEM TESTER Description A strobe system tester designed to determine the reason the strobe light system is not working properly This kit contains an instruction sheet and a trouble shooting procedure sheet Test power supplies and interconnecting cables It also comes with an adapter for testing Grimes and Hoskins strobe light systems Model Number Part Number Description 6542600 01 0765246 00 Strobe System Tester Please Order Part Number 01 0765246 00 Photos Show Typical Installations 54 Document 05131 Rev D PARTS BREAKDOWN AIRCRAFT STROBE BEACONS Model Number Part Number 5068500 A402AR A402AS A402AW A424 A425 A425AH A425AV A42
66. er A490TCCF Part Number 01 0770006 09 Specifications Both Models Current Draw 1 7 Amps 14 VDC 0 85 Amps 28 VDC Weight 1 2 Ibs Length 5 00 Width 9 12 Height 200 Operation MODEL A490TCF This model operates one strobe lighthead It is our most compact unit and can be mounted in the wingtip and or the tail adjacent to the lighthead It produces an accumulated 19 joules of power t will only meet 400 ECP when used with the A470A W This unit can not be synchronized This power supply operates gt from 10 to 30 volts Not approved for use with Red strobe light RED ANODE POSITION 1 WHITE 14 28 VDC BLACK CATHODE POSITION 2 BLACK GROUND WHITE TRIGGER POSITION 3 Dimensions 2 00 Figure 15a 20 00 51cm 2 00 Output Cable 20 00 51cm 2 00 Input Cable White 14 28V Black Ground 342 00 79mm 127mm M Mounting Holes 191 bmm DIA 4 Places 2 38 60mm i 080 6 18 2mm 157mm Mounting 5 562 E uw DIA Figure 15b EM utn 4 PLACES 938 T 24mm Ue SUGGESTED MOUNTING PLAN STANDARD 2015 Whelen Engineering Company Inc Operation MODEL A490TCCF SERIES This model is the same as the A490TCF but has Ma a mounting plate with additional p 22 holes that directly replaces t factory installed sy
67. escribed on these pages may be obtained free of charge from the Whelen Engineering Company Inc Chester Connecticut 06412 2015 Whelen Engineering Company Inc Document 05131 Rev D 55 PARTS BREAKDOWN AIRCRAFT STROBE BEACONS on 4 Oe amp SA402 A457B D A628 D OPTIONAL OPTIONAL O A457A 7 A402A 01 0450685 00 455 4 C gt D 01 0450685 00 x NC di 9 Z A508 gt Z A457A QUON uae amp NL A506 eee A627 A467 SA406 A469B 1 444 625 441 441 450 A470A When ordering models A500A and A555A or lens assembly part number A457B D make sure to SPECIFY HORIZONTAL OR VERTICAL 606 A612 D A626 D A626 A626 D OPTIONAL OPTIONAL OPTIONAL W1284 W1284 A612 A612 gt o 5 N gt 2 N A610 vt A427 3 A441 A615 A600 PR A650 PR A650 W1285 PR A600 PG A650 PG W1285 PG 56 Document 05131 Rev D NOTES 2015 Whelen Engineering Company Inc Document 05131 Rev D 57 NOTES 58 Document 205131 Rev D WHELEN LED amp STROBE TECHNOLOGY FOR YOUR AIRCRAFT FROM WHELEN ENGINEERING THE LEADER IN AVIATION LIGHTING Model 71141 For a complete look at Whelen and it s line of Aviation Automotive and Mass Notification Products Please visit us on the WEB at Model 710 odel 71055 www whelen com wa Whelen Prod
68. f the cover to provide for moisture drainage Care must be taken not to let the drill protrude into the power supply for it will inflict damage to the electronic components 6 Specifically call out the location of the strobe light power supply on FAA form 337 Important Note Your new strobe power supply has an additional circuit built in to prevent self ionization steady glowing of the strobe tubes In some cases when replacing older power supplies the bare shield wire in the existing harness is pinned together at each end with the black wire The following modification must be made to ensure proper operation 1 At the strobe tube end of the cable cut the shield wire and tape it off DO NOT CUT THE BLACK WIRE 2 At the power supply end of the cable cut the shield wire and connect it to a good ground DO NOT CUT THE BLACK WIRE 3 This must be done for each strobe light connection See Figure 6a 6 Document 05131 Rev D Wiring WARNING STROBE LIGHT POWER SUPPLIES ARE POLARITY SENSITIVE REVERSING THE INPUT POLARITY WILL CAUSE SEVERE DAMAGE TO THE POWER SUPPLY Steps below Ref AC 43 13 1B Chapter 11 Sections 1 2 3 amp 7 1 Choosing wire size of A input lead refer to Paragraph 444 Electric Wire Chart Figure 11 7 amp 11 7a with reference to Strobe Light Model Current requirement chart on page 6 amp 11 and Wire and Circuit Protection Chart Figure 11 1 2 Shielded wire
69. f our 48 hour Repair Service Document 05131 Rev D 53 R F l and Problems Radio Noise Whelen Engineering strobe light power supplies are designed with a low pass filter built in to keep R Fl and down to a minimum however sometimes there will be interference in the radios by the strobe light system Most always this is an installation problem not a strobe light power supply problem The power supply should acquire its power from a low impedance source such as the alternator or generator end of the electrical buss Historically the rotating beacon or strobe light circuit breaker is added on the electrical buss at the opposite end with the radio in between the strobe breaker and the low impedance end of the electrical buss Any noise generated by the power supply will be transmitted into the radio through the A input lead to the radio Most of the new radio equip ment manufactured today has inadequate input filtering and any noise on the electrical buss is amplified in the radio and produced through the speaker and or head phones loud and clear Two things can be done to alleviate the problem 1 Connect the strobe light circuit breaker to the low impedance end of the electrical buss using a 16 gauge jumper as close to the battery as possible 2 Install additional filtering in the radio A line or provide an iso lated A source for the radios by installing a filter choke in series with the radio input
70. ght assembly in a rudder mount location rudder balance must be checked with reference to the aircraft s service manual The weight and balance should equal the original rotating beacon 8 Check all avionics systems for interference from the installation with reference to AC 43 13 2a Chapter 4 paragraph 52 b 9 Label all switches and breakers install pilot warning placard 10 Update aircraft records complete Form 337 and obtain FAA field approval for installation if not covered under STC eligibility list Flash Tube Replacement 1 When a flash tube failure occurs remove the 6 Phillips head screw on the clamp ring Be careful not to lose the 6 hex nut Remove the clamp ring Lift the lens assembly amp gasket off the strobe tube Lift the strobe tube and carefully unplug the connector Replace with new strobe tube assembly Attach all parts required See parts breakdown for replacement part numbers Dimensions Note Exploded View Align Reflectors Figure 33a 222 Figure 33b 2 33 DIA 59mm Optional Mounting Adapter Positions 7 01 03 mm 178mm Before with Rotating Beacon After with Strobe Light us Model HRCFA Parts List 9 PAR
71. he A5004 tail position light The retainer shield must be located so that the bottoms of the V notches are vertical parallel to the rudder to shadow the light so it will produce a horizontal light pattern of 70 degrees left amp right of straight back of aircraft Mounting Figure 42b Connecting Wiring of the A500A to the MIRE EATARES HORIZONTAL VERTICAL MOUNTING A441 Amp 3 Position Pin Connector a SURFACE Housing and the A444 Amp 2 Position Ka Pin Housing Connector EE Anode RED wire Pin 1 of M41 5mm 1 40 Cathode BLACK wire Pin 2 of A441 1 06 27mm DIA 99mm Trigger WHITE wire Pin 3 of M41 Position Light BLUE wire Pin 1 of A444 Position Light Ground BLUE wire Pin 2 of M44 POSITION LIGHT PATTERN REQUIREMENTS 42 Document 305131 Rev D Model A500A SERIES A500AVD1 01 0770024 04 A500AVD2 01 0770024 05 Exploded View Parts A500AHD1 01 0770024 06 Figure 43a A500AHD2 01 0770024 07 A500VDM1 01 0770024 08 E 8 0 A500VDM2 01 0770024 09 A500HDM1 01 0770024 10 A500HDM2 01 0770024 11 x x A500ABV2 01 0770024 15 moo A500ABV1 01 0770024 16 A500ASP2 01 0770024 25 12 00 305mm 1 00 LEADS BONDING BRAID 6 00 152mm 1 00 S A500AV14 A500AV28 A500AH14 A500AH28 01 0770024 00 01 0770024 01 01 0770024 02 01 0770024 03 J2 CONNECTOR WIRING J1 CONNECTOR WIRING
72. he shroud with each notch equadistant to the centerline 8 Check all avionics systems for interference from the installation 38 Document 05131 Rev D 0 50 Ibs 0 25 Amps 227gm FAA TSO C96a Class Il TSO C30c Type II 28 VDC Nominal FAA TSO C96a Class Il TSO C30c Type I 28 VDC 9 A flight check should be performed by a properly certified pilot 10 Update aircraft records as required Dimensions Figure 38a 14V amp 28V Models 14V Models 4mm POS 3 WHITE TRIGGER POS 2 BLACK CATHODE POS 1 RED ANODE RED 14VDC BLACK GROUND 28V Models POS 3 WHITE TRIGGER POS 2 BLACK CATHODE POS 1 RED ANODE WHITE 28VDC BLACK GROUND Figure 38c Models 7111001 7111002 7111003 7111004 Exploded View Parts Figure 39a Mounting Figure 39b 1 31 33mm DIA 1 00 Model 71110 Series Parts List 3 x 0 140 Dia Mounting Hole For 226 32 Screws QTY QTY QTY QTY ITEM PART NUMBER DESCRIPTION 01 0771110 01 FINAL ASSY POS STROBE LIGHT 14V GRN 71110 01 0771110 02 FINAL ASSY POS STROBE LIGHT 14V RED 71110 01 0771110 03 FINAL ASSY 28V POS STROBE LIGHT GRN 71110 01 0771110 04 FINAL ASSY 28V POS STROBE LIGHT RED 71110 01 0271757 01 ASSY POSITION STROBE LIGHT 14V GRN 71110 01 0271757 02 ASSY POSITION STROBE LIGHT 14V RED 71110 38 0230021 00 GASKET W 1283 W 1285 A650
73. he vertical and horizontal centerlines of the aircraft to project the patterns properly Certain types of installations may require additional testing CONTINUED AIRWORTHINESS The forward position light is designed with Green or Red LEDs The anti collision light is designed with 18 White LEDs If any one LED fails the unit must be repaired or replaced Inspect the lens replace if there is excessive scratching pitting discoloration or cracking Note To reduce eye strain use an optical filter such as dark glasses or a Blue covering dome during LED inspection INSTALLATION PROCEDURES The following information is to assist you in installing a Whelen light system 1 Choose the appropriate light assembly 2 Using the mounting detail information provided prepare the aircraft for means to secure the light assembly 3 Carefully remove the 4 phillips head screw and lens retainer Remove the lens from the light assembly by lifting the rear of the lens approximately 1 2 Now slide the lens rearward approxi mately 1 4 and lift upwards to remove CAUTION To avoid potential damage do not touch the LEDs with either fingers or sharp objects Remove the 3 Phillips head screws securing the baseplate to the light assembly Remove baseplate 4 Using the appropriate hardware install the baseplate directly to the aircraft 5 Route the wires through the opening in the baseplate Connect the light inputs according to the chart show
74. housing If it is not possible to get a good grip it is recommended that the pins and sockets be soldered to prevent burning of the wires INSTALLATION CABLE KITS Intermixing Strobe Light System Equipment Observe Color and Pin Numbers Cables Connecting Strobe Lights MUST BE Connected Correctl y Whelen Engineering and Aero flash wiring between light assemblies and remote power supplies are identical as pictured below in Figure 5b Figure 5b Grimes and SDI Hoskins wiring between light assemblies and remote power supplies are identical as pictured below in Figure 5c Figure 5c Both Grimes and SDI connectors Position A RED Anode Position B WHITE or BLUE Trigger Position C Cathode BLACK or YELLOW sometimes use MS Cannon Type All Kits include required connectors for hooking up the strobe light to the power supply only and warning placards Cable is 16 gauge 3 c shielded The cable diameter is 275 The weight is 050 Ibs per linear foot Kits do not include switches or breakers In order to maintain the integrity of the installation one of the following installation kits must be used If the installer chooses to use different cable it must have the same or better electrical characteristics V Model Number Part Number Description 4 HS5 01 0750215 00 5 Cable Kit EIO o scires 01 0750218 00 10 Cable Kit H9390 01 0750214 00 30 Cable Kit _ HD60
75. ight operations is requested the airplane must have an anti collision light system that consists of one or more approved anti collision lights located so that their light will not impair the flight crew members vision or detract from the con spicuity of the position lights Continued Airworthiness The 70900 series LED anti collision light assembly is designed with 10 vertical columns consisting of 3 LEDs each Should any one LED or any vertical column fail the unit must be repaired or replaced Installation Procedures The following information is to assist in the installation of a Whelen LED Flashing Anti Collision Light System 1 The installation procedure described in the following text will be confined to a single light installation but is identical for multiple light installations 2 Prepare the aircraft for means to secure the LED Flashing Anti Collision Light assembly see reference AC 43 13 2A Ch 4 3 14 and 28 VDC and ground leads equipped with an appro priate sized breaker to be supplied to the LED Flashing Anti Colli sion Light Assembly System Both leads must be connected by an approved FAA connection Insure that the wire leads and the pressure venting tube are all clear of any obstructions and ty wrap as required The pressure venting tube may be trimmed to minimum length of 1 from base 4 Install the light assembly by securing to aircraft using 46 32 x 3 8 maximum length approved hardware Note Le
76. ignal 12 VDC ACL ORANGE 12 VDC POS Connecting to the synchronize signal of any Whelen LED anticol 10 0 25cm 1 0 lision assembly to another Whelen anti collision assembly will 20AWG MIL 22759 43 cause the lights to flash at the same time If Synchronization is not necessary the connection may be left open 6 Re install the light assembly on to the baseplate and insure that all leads are clear of any obstructions and secured as required 7 Check all avionics systems for interference from this installation 2015 Whelen Engineering Company Inc Document 05131 Rev D 1 1 Model OR6501GE OR6501RE 12V Series Exploded View Parts Figure 12a Gr Model OR6501GE OR6501RE Series Parts List QTY QTY ITEM PART NUM BER DESCRIPTION 01 0790701 01 OR6501GE Wingtip Position Anti Collision Light 12V Green 01 0790701 02 OR6501RE Wingtip Position Anti Collision Light 12V Red 07 771790 100 Mounting Plate Model 90701 Heli Coils CMPL 01 0290714 01 Sub Assy Model OR6501GE 12 VDC GRN 01 0290714 02 Sub Assy Model OR6501RE 12 VDC RED 14 0050505 14 Screw 4 40 x 5 16 PPHMS MS51957 14 Model OR6502GE OR6502RE 28V Series Exploded View Parts Figure 12b Gr AA Model OR6502GE OR6502RE Series Parts List QTY QTY ITEM PART NUM BER DESCRIPTION i 01 0790701 11 OR6502GE Wingtip
77. iminates the need for external power supplies and reduces current draw and provides thousands of hours of operation Model OR650E Specifications Model Part LED Numbers Voltage Color Aviation OR6501GE 01 0790701 01 12 VDC OR6501RE 01 0790701 02 Aviation Red Aviation OR6502GE 01 0790701 11 d 28 VDC OR6502RE 01 0790701 12 L A Anti Collision Operational LED Voltage Flash Rate Approvals Lenses Color FAA TSO ETSO C96a Class II 030 Position TSO ETSO C30c Type II 9 14 VDC 0 7 Amp Avg Anti Collision FAA TSO ETSO C96a Class II Aviation 26 Ibs TSO ETSO C30c Type White 118gm FAA TSO ETSO C96a Class II 0 15 Amp Position TSO ETSO C30c Type II 22 32 VDC 35 Amp Avg Input Current Anti Collision FAA TSO ETSO C96a Class II TSO ETSO C30c Operation Operation cont d EQUIPMENT LIMITATIONS 8 A flight check should be performed by a properly certi An approved forward position lighting system consists of three fied pilot lights one located on the tail and one located on each wingtip Model 9 Update aircraft records complete Form 337 and obtain OR650 is a wingtip position and anti collision light The assembly FAA field approval for installation if required should be mounted as far outboard on the aircraft as practical The baseplate must be mounted parallel to the vertical and horizontal centerlines of th
78. ions Exploded View Parts Figure 26b Figure 26a 9 125 3mm Drain Hole Lower 05 14 131mm Mount Only 75 75 72 lt lt lt 75 75 Mounting Figure 26c 5x 2 156 4mm thru C SINK to 2 281 7mm x 100 spaced as shown on ff i 4 656 118mm Bolt Circle ST o gt Wm Wo mio D ms jm of e o 0 GASKET REF 5 43 1 06 138mm LN 22 60 66mm MFG LABEL Suggested Mounting Pattern CONNECTOR MS3102R10SL 3P Wiring Figure 26d Wiring Diagram Figure 26e TRIM WIRES TO 3 5 BEFORE SOLDERING J1 28VDC A LED N C B MODULE GND c Goe eld MS Connector Wiring Wiring Diagram VIEW PRIOR TO REV K 26 Document 05131 Rev D Rear View Model 7108008 7108018 Series Parts List QTY QTY ITEM PART NUMBER DESCRIPTION i 01 0771080 08 Model 7108008 Upper 28V 01 0771080 18 Model 7108018 Lower 28V 1 1 1 01 0271848 00 Assy 28V Led Anti Collision Light 71080 1 1 2 38 0250885 00 Gasket Lens Model 71055 Series 1
79. is not generally necessary but has proven effective in reducing the possibility of radio interference 3 The power supply shall acquire its power from a low imped ance source such as the alternator or generator end of the electrical buss as close to the battery as possible Do not ground power supply to airframe This can attenuate emi rfi noise to airframe causing it to act as an antennae for inter ference in aircraft audio amp electrical systems 4 For penetrating pressure hull refer to the aircraft service manual 5 Check all avionics systems for interference Figure 6a PIN 1 RED ANODE PIN 2 BLACK CATHODE PIN 3 WHITE TRIGGER SHIELD RFI DRAIN TO GROUND 3 POS PIN HSG 3 POS SOCKET HSG 3 CONDUCTOR SHIELDED CABLE 1 STROBE SUPPLY 2 2 TUBE END 31 4 END X SHIELD WIRE CUT AND TAPE SHIELD WIRE AT STROBE TUBE END GROUND SHIELD WIRE A AT POWER SUPPLY END ONLY ORION 500 LED LIGHT ASSEMBLIES MODEL OR5001V amp OR5002V LED Tail umm 49 Position Anti Collision Lighthead Assembly All LED self contained tail mounted Position Anti Collision system Eliminates the need for external power supplies and reduces current draw and provides thousands of hours of operation Model OR500 Specifications Anti Model Part LED Collision Operational Flash Color OR5001V 01 0771774V01 12 VDC Aviation 0 20 Amp Position FAA yr C96a Class II amp III 0 2
80. l OR5002V Parts List QTY ITEM PART NUMBER DESCRIPTION ii 01 0771774V02 ORION 500 Model OR5002V 28 VDC 2 1 14 040216 160 Screw 4 40 x 1 PPHMS SS 2 2 2 19 151080 100 Retainer lridite 1 3 68 3951061 A31 Lens Model 90667 No Drain Slot Hardcoat 1 he For shipping purposes only 1 4 38 0131364 00 Gasket VHB Seal 1 7 01 0290717 01 Sub Assy ORION 500 Model OR5002V 28 VDC 2 6 13 040130 040 Nut 44 40 x 1 4 Hex Brass 8 Document 205131 Rev D ORION 650 LED LIGHT ASSEMBLIES MODELS OR6501G OR6501R OR6502G OR6502R LED Wingtip Position Anti Collision Lighthead Assembly All LED self contained wingtip mounted Position Anti Collision system Eliminates the need for external power supplies and reduces current draw and provides thousands of hours of operation Model 650 Specifications Anti Collision Operational LED Voltage Color 11 15 VDC OR6501R Aviation Model Part LED Numbers Voltage Color d Aviation OR6501G 01 0790725 01 Gian 14 VDC 01 0790725 02 Re Aviation 01 0790725 11 ae 28 VDO 01 0790725 12 nun Red Operation EQUIPM ENT LIMITATIONS An approved forward position lighting system consists of three lights one located on the tail and one located on each wingtip Model OR650 is a wingtip forward position and anti collision light The assembly should be mounted as far outboard on the aircraft as prac tical The baseplate must be mounted parallel to t
81. lation if not covered under STC eligibility Model 71080 Series Class helicopter beacon Red only can now replace Model 70905 beacon now available with new style mounts and electrical connections 28 amp 14 VDC 0 65 Ibs 295gm 0 80 Ibs 363gm 0 75 lbs 340gm 2 0 amps peak Models 7108001 7108006 4x 6 32 Mounting Holes Equally 4x 6 32 Mtg Holes Equally 71 08051 Spaced a 1 625 Bolt Circle Spaced on a 1 750 Bolt Circle Exploded View Parts CA p Suggested Suggested I gt Figure 23a 14V Mounting 28V Mounting dis E Hole Pattern s Hole Pattern Q 59 4x 6 32 Mounting Holes Equally I Spaced on a 21 250 Bolt Circle M ounting Figure 23c Dimensions Figure 23b o OJ OJOJIOGIe 3 74 06 95mm 7108051 14 Volt 28 Volt id MFG MFG 5 5 5 LG 7108001 140mm LABEL 12 41 LG LABEL 305mm 7108006 dS 24 1 5 610mm 20A
82. lded Clear Coated Lens 0 08 Ibs 36gm A612RC 68 2290005 54 Rfi Coated Aviation Red Lens Before MODEL A610 46 0 flash tube Model A610 Specifications Model Part Input Current Flash Tube A610 02 0250276 00 Standard unit 6 leads unit Standard unit 6 leads leads A610M 02 0250276 03 Molex connector 6 leads Dependant on strobe 0 09 Ibs 41gm 5027601 02 0250276 01 14 leads power supply used 5027602 02 0250276 02 A610 Style with 12 1 2 Leads After Operation The Model A610 flash tube and the Model A612 glass lens are used for installing wingtip strobes in single engine Cessna s 1972 and later The existing posi tion light retainer is modified to accommodate the lens and the flash tube is mounted directly behind The unique magnifying design of the A612 lens increases the light intensity by two to three times in the horizontal plane Lenses meet material requirements of MIL C 7989B class B A610 Dimensions Figure 40a Late Model Single Engine Cessna Wingtip Strobe Light Installation of A610 and A612 Figure 38d CONNECTOR WIRING POS 1 RED ANODE POS 2 BLACK CATHODE POS 3 WHITE TRIGGER A612 Dimensions Figure 40b Remove the position light lens retainer being careful Green lens 2 Establish a center line on the Cessna lens retainer referencing to the lens retainer center mounting screw and position light base plate rear A612 Lens Profile Figure
83. lly remove the lens retainer and lens from the assembly CAUTION Do not touch the LED surface with either fingers or sharp objects This could soil or damage the lens and effect the optical performance of the LEDs 5 Install light assembly and insure that all leads are clear of any obstructions Note that proper orientation is achieved with the drain hole down 6 Reinstall the lens and confirm proper gasket fit T Install the lens retainer Using appropriate hardware secure as required Secure light assembly using vibration resistant thread ed fasteners 8 When necessary waterproof the light base to aircraft Apply single part silicone RTV or equivalent around any open area where water could get in Do not cover drain hole 9 Check all avionics systems for interference from this installation 10 A flight check should be performed by a properly certified pilot 46 Document 05131 Rev D FAA TSO C30c ETSO C30c Type III TSO C30c TYPE Ill APPROVED Exposed Hole 1 36 35mm 1 75 45mm 22 30 VDC 0 125 Amps 0 17 lbs 91gm 11 15 VDC 0 25 Amps Operation cont d 11 Update aircraft records complete Form 337 and obtain FAA field approval for installation as necessary Dimensions and Mounting Detail 14 VDC Figure 46a VERTICAL 01 0771554 12 4 40 1 2 MS51957 17 2x HORIZONTAL 01 0771554 11 i 4 40x1 2 Nut for shipping 60mm
84. mounting to the aircraft apply GE silicone rubber RTV 102 or equivalent around the open area where water could get in 5 Label all switches and breakers install Pilot Warning Placard 6 Up date aircraft records and complete form 337 STROBE SYSTEM WIRING Interconnecting Cable 1 The Whelen interconnecting cable shall be secured in place with approved aviation techniques 2 The cable shall not parallel ADF Gyro or Flux Gate compass leads closer than 12 inches 3 Reference should be made to AC 43 13 1B Chapter 11 Sections 3 and 7 when routing and fishing the interconnecting cable 4 Leave a service loop at the strobe lighthead end to allow access to the connector for flash tube replacement without having to dis assemble the aircraft 5 CABLE COLORING CODE PIN 1 RED Anode PIN 2 BLACK Cathode flash tube ground PIN 3 WHITE Trigger SHIELD Ground at the power supply end only Caution When pins 1 and 2 or pins 2 and 3 are reversed the system will appear to operate normally however this condition will cause pre mature flash tube failure CLIP SHIELD Figure 5a ED A441 PINS POWER SUPPLY END R A442 SOCKETS FLASH TUBE END Observe Color and Pin Numbers The retaining clip on the side of each pin or socket of the A441 and A442 connector assemblies must be bent out Reference illustration Figure 5a shown above so that they positively snap into the AMP 3 position socket nylon connector
85. mp contacts Kit 2 Socket Connector amp contacts Gasket A457A Lens Lens Lens Shielded Lens Retainer Assy Radio shielded Vertical Mounting Lens Retainer Assy Radio shielded Horizontal Mounting Strobe Tube Assy non reflective base Strobe Tube Assy Radio shielded Strobe Tube Assy Radio Shielding Kit for A469A Disc Lamp Socket for A555A Series Strobe Tube Socket Assy For A500A Lamp Socket for A555A Series Halogen Lamp 14V 25 Watt Halogen Lamp 28V 25 Watt Base Plate Assy For A600 Series Retainer for A600 Series Strobe Tube Magnifying Lens for A610 Lens Retainer Assy Radio shielded used on A600 Series Taillight Lens used on A600 Series Gasket for A615 Taillight Lens Retainer for A650 Series Model Number Part Number 02 0350072 35 07 730068 000 11 230079 000 68 4230044 30 02 0350053 00 38 0230104 00 19 150002 009 38 0230021 00 68 4230020 40 68 4230020 50 02 0350003 01 34 0414020 65 34 0428020 65 Description Lens Retainer Assy for A650 Series Radio shielded Mounting Adapter for A470A Series Mounting Adapter for A470A Series 3 3 4 dia mounting pattern Lens Clear for SACF amp A450 Series Strobe Tube for SACF amp A450 Series Gasket for SA402 Lens Lens Retainer for W1285 Series Gasket for W1284 Lens Position Light Lens Green Position Light Lens Red Base Plate Assy Position Light Lamp 14V Position Light Lamp 28V A copy of the Whelen warranty regarding products d
86. n Connect the power lead to an appropriately sized breaker Connections to be accord ing to FAA approved methods Note SYNC is a low power bi directional control signal Connecting to the synchronize signal of any Whelen LED anticollision assembly to another Whelen anti collision assembly will cause the lights to flash at the same time lf synchronization is not necessary the connection may be left open Aviation hite OR6502G 22 32 VDC 24 A OR6502R 2015 Whelen Engineering Company Inc AMD Avg Anti Collision Flash Input Current ED Approvals Lenses 0 20 Position 0 56 Amp Avg Anti Collision 0 17 Amp Position 10 11 1 1 TSO ETSO C96a Class III TSO ETSO C30c Type II FAA TSO ETSO C96a Class Ill Clear 0 3 Ibs TSO ETSO C30c Hard coated 45 5 FPM 136 m Polycarbonate 9 FAA TSO ETSO C96a Class III Field TSO ETSO C30c Type II Replaceable FAA TSO ETSO C96a Class III TSO ETSO C30c Type I Operation cont d 6 Re install the light assembly on to the baseplate and insure that all leads are clear of any obstructions and secured as required Note that proper orientation is achieved with the drain hole down Install lens in the reverse order as removal and return the lens retainer to its installed location Note Visually confirm that the lens and retainer are fully and prop erly seated Re insert 4 phillips head screw and
87. n lights and PAR 23 1387 for position lights The convergence of the two wingtip tail position must occur within 1200 feet directly behind the aircraft to comply with field of coverage requirements The baseplate must be mounted parallel to the vertical amp horizontal centerlines of the aircraft to project the patterns properly Mounting 1 If necessary fabricate the mounting pattern using dimensions found Figure 40a 2 Make the necessary wiring connections using 18 gauge wire for the posi tion lights and Whelen 16 gauge 3 c cable for the strobe lights All connec tions must use FAA approved techniques 3 Remove the two 6 32 x 312 retainer mounting screws and retainer 4 Attach the base assembly to the wingtip using 3 46 32 counter sunk screws unit may be sealed around periphery with RTV or equivalent 5 Re attach lens retainer see Figure 48a 140 4mm DIA 3 MOUNTING HOLES FOR 6 32 SCREWS Figure 48a 25mm Wiring 1 The strobe connector should plug into the Whelen interconnecting cable or a Whelen strobe power supply 48 Document 05131 Rev D 4 0 amps 14 VDC 2 0 amps 28 VDC 4 0 amps 14 VDC 2 0 amps 28 VDC Dependant on strobe 4 0 amps 14 VDC used 2 0 amps 28 VDC 4 0 amps 14 VDC 2 0 amps 28 VDC LENS ADDrovals Nav Light Input Current Strobe Input Exposed Height Color Operational Voltage Current Length Width 2 4 61mm
88. nd wingtip when necessary Install the nylon three position AMP pin connectors A441 on the end of the flash tube wires RED in pin 1 BLACK in pin 2 and WHITE in pin 3 Assemble the navigation light assembly on the wingtip using the A650 strobe light assembly as the navigation light lens retainer Install the rubber pad supplied in kit on the position light base plate under the A610 flash tube if necessary to make the lens firm in its mounting In some installations it will be necessary to mask the A650 strobe light to reduce pilot annoyance The Navigation Light Detector will be a source of reflection and should be reduced in size or masked as necessary A small aluminum or plastic plate mounted between the navigation light and the wingtip protruding up or down as required like some plastic navigation light detectors and trimmed to shadow the objectionable reflected area is most effective This reflection problem varies from one aircraft to another due to aircraft design and paint color scheme and must be checked on every installation ND e Before After with Modified Wingtip 50 Document 05131 Rev D Dimensions Figure 50a TOP VIEW LEADS ARE A650 Spare Parts Exploded View Figure 50b CONNECTOR WIRING POS 1 RED ANODE POS 2 BLACK CATHODE POS WHITE TRIGGER Model A650 Series Parts List QTY QTY ITEM PART
89. ns mount ing screws installed at 5 7 in Ibs of torque 5 Check all avionics systems for interference from this installation 6 A flight check should be performed by a properly certified pilot T All inverted bottom mounted units shall require waterproofing of the unused mounting holes An application of single part sili cone RTV or equivalent applied into mounting holes is recom mended see illustration on page 11 Fig 11A Inverted and or standard mounted units when necessary may require water proofing around any open area where water could get in opecifically the lens to the flasher base assembly and the flash er base assembly to the aircraft 8 Update aircraft records complete Form 337 and obtain FAA field approval for installation If not covered under STC eligibility list 28 Document 05131 Rev D FAA TSO C96a Class 111 Input Current Operational Peak Input mine Current Voltage Diameter 0 85 amps 4 5 Amps 14 VDC 0 25 Seconds 1 1 lbs 499gm 0 425 amps 2 25 Amps 28 VDC 25 Seconds Dimensions Figure 28a 3 1 78mm 2 8 71mm IST DOC S DDO OG P e S DDO OC lt 14VDC Red 18GA Teflon Wire 18 LG or 28VDC White 18GA Teflon Wire 18 LG Ground Black 18GA Teflon Wire 18 LG MFG Label Teflon Tube 18GA Pressure Venting Models 7090004
90. ociated wiring need to be removed When replacing strobe light assemblies the strobe power supply must be removed In both cases 18 gage DC voltage wires A amp Ground must be continued from the location of the previous box flasher or power supply to the location of the new LED beacon The following information is to assist in the installation of a Whelen LED Flashing Anti Collision Light System 1 The installation procedure described in the following text will be confined to a single light installation but is identical for multiple light installations 2 Using the suggested mounting hole pattern prepare the aircraft for means to secure the LED Flashing Anti Collision Light assembly Remove any existing mounting adapters 3 14 28 VDC and ground leads equipped with an appropriate sized breaker to be supplied to the LED Flashing Anti Collision Light Assembly System Both leads must be connected by an approved VIEW PRIOR TO REV D FAA connection Insure that the wire leads and the pressure venting tube are all clear of any obstructions and ty wrap as required ADAPTER PLATE 4 Install the light assembly by first removing the lens Remove the MEG LABEL adapter plate Attach the adapter plate to the aircraft mounting holes Refer to page 2 Reinstall
91. on the trigger plug will provide an alternating flash pattern between strobe outlet 1 and strobe outlet s 2 and or 3 Installing a switch in series with the jumper will allow strobe outlets 2 amp 3 to be turned off while strobe outlet 1 remains on see Figure 13b Switch normally closed 1 10 amp rated Jumper inserted into trigger selector outlet 14V or 28V STROBE OUTLETS TRIGGER POWER SELECTOR IN OUTLET Figure 13b 2015 Whelen Engineering Company Inc Dimensions 5 03 128mm 6 56 5 40 167mm 137mm POWER INPUT TRIGGER 4 28V E STROBE OUTPUTS SELECTION A 187 5mm DIA 4 PLACES 18G WIRES RED 14 28V BLACK GROUND PIN 3 N C Figure 13c Mounting 203 DIA 4 PLACES 6 00 152mm 9 2 50 64mm 9 9 Suggested Mounting Plan Figure 13d Document 05131 Rev D 1 3 MODEL A490ATSC STROBE POWER SUPPLY FAA PMA APPROVED Specifications Model Number A490ATSC Part Number 01 0770062 03 Position Lights Current Draw 4 0 Amps Q 14 VDC 2 0 Amps Q 28 VDC Weight 1 7 Ibs Length 5 00 Width 212 Height 3 06 Operation This power supply will operate ONE strobe lighthead assembly at 34 joules of power It is equi
92. power lead and a filter adapter to ground and reference all radios to their filter This will also improve the radio system from other line noises REF 2200 mfd 950V Capacitor Frequently the noise is not on the A lead but is conducted through the ground circuit Alternator electrical motor fuel pumps and strobe light power supplies draw heavy current through the ground circuit of the aircraft s frame Any voltage drop in the ground circuit between the battery ground and the radio ground can look like a signal to the radios When the speaker head phone and microphone use the aircraft s ground for return to the radios one will always experience some inter ference The amount of interference depends upon how much potential difference there is between the two ground points Isolating the audio grounds from the airplane ground at the speaker head phone and microphone junctions and grounding the aforementioned with the radio at one central ground point will eliminate the majority of all ground inducted radio noise Do not parallel any audio leads with any power lead supplying energy to a noise generator i e alternator electric motor or DC choppers such as inverters and strobe light power supplies The interconnecting cable between the power supply and the remote strobe lighthead assembly radiate very little for the output circuit of the power supply is very low impedance They can radiate RF like an antenna if the shield is not terminat
93. pped to flash up to five 5 other like units simultaneously when an 18 gauge wire is connected to outlet 3 on the input power connector a h POWER 1543 2 SYNC OUTPUT 1 Anode 2 Cathode 3 Trigger POS 1 RED POS 2 BLACK POS 3 SYNC Figure 14a Looking at the power supply connectors with the mounting plate flat on a bench the left connector is the strobe outlet The right connector is the power input and synchronization Left Connector Power Output Pin 1 Top RED wire anode Pin 2 Center BLACK wire cathode Pin 3 Bottom WHITE wire trigger Right Connector Power Input Pin 1 Top RED wire 13 to 30 volt positive input Pin 2 Center BLACK wire ground Pin 3 Bottom Synchronization pin lf synchronization is desired connect an 18 gauge wire between pin 3 on each power supply 1 4 Document 05131 Rev D Dimensions Figure 14b 6 25 159mm 500 127 1 ANODE 2 CATHODE 3 TRIGGER Mounting Figure 14c 5 675 144mm eg 5 562 141mm MTG 1 600 938 41mm 24mm MTG MTG 187 5mm DIA 8 MOUNTING HOLES MODEL A490TCF STROBE POWER SUPPLY FAA PMA APPROVED Model Number A490TCF Part Number 01 0770006 08 MODEL A490TCCF STROBE POWER SUPPLY FAA PM A APPROVED Model Numb
94. robe lights meet the requirements as specified in AC 43 13 2A Chapter 4 PAR 51 a and b 1 STC SA615EA covers replacement of original equipment STC SA800EA and STC SA21NE cover installation of new anti collision light systems Vertical fin mounted anti collision strobe beacons will conform to the FAR 23 1401 0 5 steradian 1642 sq degrees maximum solid angle blockage requirements on most standard configurations CAM 3 and FAR Part 23 high or low wing type aircraft An aver age solid angle blockage for an installation of this type is 1324 sq degrees Fuselage mounted anti collision light systems require two 2 anti collision strobe beacons to get the 75 degrees required Two lights mounted in this manner exceed the steradian requirements of 21 600 sq degrees total coverage c eo Fuselage mounted anti collision lights should be located on the fuselage center line to reduce reflection on the wings as much as possible They should be mounted near the trailing edge of the wing to reduce cockpit reflection APPROVED METHOD OF DETERMINING ADEQUATE COVERAGE OF WING AND TAIL STROBE LIGHT INSTALLATIONS The most practical system is the approved wingtip anti collision strobe light system These systems consist of two or more lights to complete the anti collision light requirement There is no question as to their complying to the field of coverage when the installation is completed Reference to the following instru
95. s the unit must be repaired or replaced Inspect the lens Replace if there is excessive scratching discolor ation or cracking INSTALLATION PROCEDURES The following information is to assist in the installation of a Whelen 71110 LED Forward Position Light strobe System 1 Choose appropriate 71110 series replacement light assembly 2 The installation procedure described in the following text will be confined to a single light installation but is identical for multiple light installations 3 Remove the old light locate and save the existing VDC lead and ground lead Clean and prep ends as required 4 Make sure the existing system is equipped with an appropriate sized breaker Connect the existing 14 28 VDC lead to the POSITIVE wire on the input cable assembly supplied with the light assembly Connect the existing ground lead to the GROUND wire on the input cable assembly or use the supplied connector as shown in the illustrations Both leads must be connected by an approved FAA connection Insure that the wire leads are clear of any obstructions and ty wrap as required Connect the strobe J1 to the strobe power supply as shown in the figure 5 Remove the shroud from the light assembly 6 Position the base of the new light assembly onto the mounting surface Insert three 3 46 32 pan head screws into the mount ing hole and tighten firmly 7 Reinstall the lens so that the two notches are positioned under t
96. s required and obtain FAA field designed with 6 LED s If any one LED fails the unit must be repaired approval for installation if not covered under STC or replaced Inspect the lens Replace if there is excessive scratching eligability list discoloration or cracking Installation Procedures The following information is to assist you in Dimensions and Mounting Detail installing a Whelen tail position light Figure 44a 1 Choose the appropriate model light assembly which is most Vertical Mount Models applicable to your aircraft 7101102 7101112 2 Remove the old light locate and save the existing 28VDC lead eR 136 elu and ground lead 7101102 amp 7101103 Clean and prep ends 9 my are vice 2 x 4 40 x 5 8 16 m 3 Use the existing mounting holes and hardware 2 10 i MS51957 18 CU G mm 4 For Model 7101101 secure the existing connector onto the base pom E dE 22mm of the light assembly For Models 7101102 amp 7101103 connect 51mm Drain Hole 2 x 9 125 the existing 28 VDC lead to the White 20 AWG lead on the input Ld iioc MN cable assembly supplied with light assembly Connect the exist 40 ing ground lead to the Black 20 AWG wire on the input cable 1 I U I 1 00 25mm 95 24mm Square assembly If a chassis ground wire exists on the aircraft connect it to the chassis ground wire assembly Both leads must be
97. shing Anti Collision Light assembly Remove any existing mounting adapters 3 28 VDC and ground leads equipped with an appropriate sized breaker to be supplied to the LED Flashing Anti Collision Light Assembly System Both leads must be connected by an 22 Document 05131 Rev D polycarbonate hard coat LED Red FAA TSO C96a Class amp III 150 ecp FAA TSO C96a Class FAA TSO C96a Class amp III 150 ecp 0 45 amps average 0 65 Ibs 295gm 0 87 Ibs 395gm 0 80 Ibs 363gm 0 75 Ibs 340gm 0 45 amps 2 0 amps I peak average 0 87 Ibs 395gm 0 75 Ibs 340gm FAA TSO C96a Class 0 87 Ibs 395gm 0 65 Ibs 295gm FAA TSO C96a Class amp III 150 ecp 0 75 lbs 340gm approved FAA connection Insure that the wire leads are clear of any obstructions and ty wrap as required 4 nstall the light assembly by first removing the lens Remove the adapter plate Attach the adapter plate to the aircraft mounting holes Refer to page 2 Reinstall the light assembly and lens 5 All inverted bottom mounted units shall require waterproof ing of the flasher base assembly to the aircraft Note Drill a 1 8 hole in the center of the lens for bottom mount units 6 Check all avionics systems for interference from this installa T A flgh check should be performed by a properly certified 8 pt aircraft records as required amp obtain FAA field for instal
98. stems on single engine Cessna s Aero Commanders and Grumman Americans RED ANODE POSITION 1 BLACK CATHODE POSITION 2 WHITE TRIGGER POSITION 3 WHITE 14 28 VDC BLACK GROUND A490TC UNITS Dimensions PLATE BOTTOM VIEW Figure 15c OUTPUT CABLE 3 750 MOUNTING HOLES 187 DIA 4 PLACES Mounting Iumamm Figure 15d T 3 250 Asa Z 87 DIA 4 PLACES SUGGESTED MOUNTING PLAN FOR OPTIONAL BASE Document 05131 Rev D 1 5 LED LIGHT ASSEMBLIES MODEL 90520 SERIES LED FLASHING BEACON Red amp White LED s 90520 series LED beacons are FAA TSO compliant self contained LED anti collision lights Ref Class 111 100 effective candlepower They are designed to replace strobe lightheads as small as the A470A with available models to replace HR self contained beacons HRCFA or our legacy 70900 LED beacon Mounting plate included with assembly Refer to models and descriptions below ELECTRICAL Models 01 04 05 14 15 51 55 Ship with 12 Flying Leads Models 07 17 08 18 MS3102R10SL 3P Connector MECHANICAL Models 04 14 08 18 55 are 3 4 opening designed to fit inside an A440 mounting adapter mounting designed to replace existing beacons utilizing a 5 Hole mounting pattern on 4 656 diameter bolt circle Whelen 70285 series 7090501 series or 70900 with A440 adapter Models 05 15 07 17 are 3 94 opening
99. that protrude beyond the wingtip their light converging in front and back of the aircraft within 1200 ft is an approved anti collision strobe light system VERTICAL FIN One anti collision strobe light mounted on the vertical fin will meet the minimum require ments on most aircraft A half red and half white lens is re commended FUSELAGE In a fuselage mounted anti collision strobe light system a minimum of two strobe lights are necessary to get the ENCLOSED WINGTIP Enclosed wingtip anti collision strobe lights require a third strobe light on the tail or verti cal fin to fill in the required light envelope This is an required vertical coverage approved anti collision sys This is an approved anti colli tem sion system Document 05131 Rev D AIRCRAFT NOT SPECIFICALLY MENTIONED ON THE ELIGIBILITY LIST ANTI COLLISION LIGHT INSTALLATION PROCEDURES STC SA800EA STC SA615EA STC SA21NE The following information is to assist in the installation of a custom Whelen anti collision strobe light system on any aircraft and how to return the aircraft back to service with compliance to FAR Part 91 205 c 3 1 Choose the anti collision light system which is most applicable to the aircraft NO With reference to the STC s Limitation and Conditions for field of coverage requirements Check the field of coverage of the pro posed location These STC s document that Whelen s anti collision st
100. trobe Lighthead Assemblies A500A Series LED Light Assemblies 71011 Series LED Light Assemblies 71554 Series A600 PG PR Series A650 Series Strobe Power Supply Replacement Cross Reference Listing Continued Airworthiness Flow Chart Strobe System Trouble Shooting Parts Breakdown Aircraft Strobe Beacons Notes Whelen LED amp Strobe Ad Visit Whelen at www whelen com view our products amp contact us We can be e mailed at aviation whelen com Corporate Pilots Corporate Manufacturing Facilities in Chester CT and Charlestown NH 2 Document 205131 Rev D ENGINEERING COMPANY INC 51 WINTHROP ROAD CHESTER CT 06412 0684 PHONE 860 526 9504 e FAX 860 526 2009 Makers of Aviation Automotive and Industrial Safety Lighting since 1953 The Finest Designed Assembled Tested Aviation Warning Products Manufactured In the U S A To view our products and contact us visit Whelen at www whelen com or we can be emailed at aviation whelen com Whelen Aviation Staff Greg Jeff Bryan Sharon Jessica Trish INTRODUCTION TO WHELEN ANTI COLLISION STROBE LIGHTING SYSTEMS STC SA800EA STC SA615EA STC SAGNE STC SA21NE Whelen s Anti Collision Strobe Light Systems are approved under STC SA615EA STC SA800EA STC SA6NE and STC SA21NE manufactured under PMA as an approved anti collision light for all aircraft when installation is accomplished in accordance
101. ucts are proudly made in the U S A Background Photo Courtesy of Cessna Flyer Magazine December 2008 2015 Whelen Engineering Company Inc Document 05131 Rev D 59 ENGINEERING COMPANY INC 51 WINTHROP ROAD CHESTER CT 06412 0684 PHONE 860 526 9504 FAX 860 526 2009 www whelen com WARRANTY amp SERVICE REPAIR STATION SERVICE REPAIR STATIONS UNITED STATES CANADA OVERSEAS Whelen Engineering Company Inc Wright Instruments Ltd Allen Group International 51 Winthrop Road 2762 Slough Street Kruisweg 705 Chester CT 06412 0684 Mississauga Ontario P O Box 52 Tel 860 526 9504 Canada L4T 1G3 Hoofddorp Netherlands 2130 AB Fax 860 526 2009 Tel 905 677 7161 Tel 31 20 6552213 www whelen com Fax 905 677 2188 Fax 31 20 6533991 aviation whelen com 377 gt ISO 9001 Registered QMS 2015 Whelen Engineering Company Inc Part Number 04 0105131 00 Document 05131 Rev D
102. uggested Mounting Hole Pattern Wiring Diagram Figure 20d WHITE BLACK C SNC O B MS CONNECTOR WIRING REAR VIEW 20 Document 05131 Rev D LED MODULE CONNECTOR MS3102R10SL Dimensions Figure 20b NOTE RED LEDs TO FRONT 0 125 DRAIN HOLE LOWER MOUNT ONLY e J K e e 3 92 100 Q rej 1 51 38mm MS3102 CONNECTOR Models 9052008 9052018 Dimensions Exploded View Parts p Figure 21b Figure 21a _ 5 442 131 2 60 QTY QTY ITEM PART NUMBER DESCRIPTION 91 mm 5 01 0790520 08 Model 9052008 28V Upper 01 0790520 18 Model 9052018 28V Lower 1 1 1 01 0290522 00 Assembly 28V 1 1 2 38 0250885 00 Gasket Lens 1 3 68 4971082A30 Lens Clear 1 4 68 4971082A31 Lens Clear with Drain 1 1 5 38 0250225 00 Seal 1 1 6 07 571304 100 Adapter 5 Hole Lens Retainer NOTE 4 4 7 16 0050506135 Washer 4 Lock Spring MS35338 135 RED LEDs 4 4 8 14 0050505 14 Screw 4 40 X 5 16 PPHMS MS51957 14 Mounting Figure 21c 138mm s QQ Mounting Gasket 6 32 Flat Head 100 Countersink typ 5 x 6 32 MTG holes on a 4 656 118mm bolt circle NOTE RED LEDs TO
103. wer supply is in working condition and the problem may be with the interconnecting cables 2015 Whelen Engineering Company Inc CABLE CONTINUITY CHECK PROCEDURES If pins 1 and 3 are reversed or if there is a short between pins 1 and 2 of the interconnecting cable the power supply will be rendered non operable until the short is cleared A short of this type will not cause any permanent damage to the power supply However a discharge of the condenser across pin 1 and pin 3 will destroy the trigger circuit in the power supply 1 Check for continuity between the connectors of each interconnect ing cable Pin 1 to pin 1 red wire anode Pin 2 to pin 2 black wire flash tube ground Pin 3 to pin 3 white wire trigger 2 Check for shorts between pins 1 and 2 pins 1 and 3 and pins 2 and 3 of the interconnecting cable NOTE When pins 1 and 2 or pins 2 and 3 are reversed the system will appear to operate normally but these conditions will cause early flash tube failure and void the flash tube warranty XENON FLASH TUBE PROCEDURES 1 A xenon flash tube can be very photosensitive One will flash nor mally when exposed to an external light source but may become hard to fire when subjected to darkness They will become hard firing with age or when exposed to a very high temperature A hard firing tube will sometimes operate with the engine running but will fail when operated on a low battery They
104. wer supply into normal service This will prevent over heating of the condenser while they reform If the power supply after a long period of non use is operated at full voltage immediately there is an excellent possibility that the condenser will become overheated POWER SUPPLY TEST PROCEDURES THE POWER SUPPLY IS A HIGH VOLTAGE DEVICE LET THE POWER SUPPLY BLEED DOWN FOR 10 MINUTES AFTER TURNING OFF POWER BEFORE HANDLING WARNING Reverse polarity of the input power for just an instant will permanently damage the power supply This dam age is sometimes not immediately apparent but will cause failure later on External trigger switching is not provided on the A413A HDA DF Strobe Light Power Supply Reference A413 T3 DF old style strobe light power supply outlet 1 Do not short out high voltage for extended length of time it will cause overheating of the output diodes and cause possible failure A normal operating power supply emits an audible tone If there is no sound emitted investigate 1 Determine that there is a proper input voltage at the power supply If this test is positive go to step 2 2 Clear all possible shorts at the power supply by disconnecting the output cables from the power supply outlets and connect an oper ating strobe lighthead assembly or a strobe check unit directly to the power supply outlet then apply the required voltage to the power supply input If this application proves positive the po
105. with the following instructions Whelen s Anti Collision Strobe Light Systems are designed and approved spe cifically for General Aviation Aircraft to comply to FAR 91 205 c 3 visual flight rule night requirements Whelen s approved Anti Collision Strobe Light Systems can be installed on all aircraft by completing the installation with reference to this Installation and Service Manual and the appropriate technical data listed below ADVISORY CIRCULAR 43 13 1A Chapter 11 Sections 1 2 3 and 7 Electrical Systems ADVISORY CIRCULAR 43 13 2A Chapters 1 and 2 Radio Installations ADVISORY CIRCULAR 43 13 2A Chapter 4 Anti Collision Light Installations ADVISORY CIRCULAR 20 21 12 3 64 Application of Glass Fiber Laminates in Aircraft ANTI COLLISION AND POSITION LIGHT REQUIREMENTS LOCATIONS amp DISTRIBUTION PATTERNS All aircraft must have an approved anti collision light and position light system for nighttime operations The position lights consist of an Aviation Red on the left side an Aviation Green on the right and an Aviation White taillight REF FAR 23 1389 The anti collision lighting system is required under FAR PART 91 205 c 3 There are different requirements affecting different aircraft These aircraft are categorized by the date of application for type certificate Home built aircraft are determined by the date of issuance of the Experimental Operating Limitations The different categories are as follows

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