PULSELITE STARLIGHT INSTALLATION MANUAL MODELS 1151
Contents
1. ru pris vac 7 9 Dc GND PULSE CONTROL 9 NOTUSED NOTUSED 0 STEADYON 82 1o Norustb NOTUSED DCGND PULSECONTROL 11 115 vac ACINPUT Liz C sreabvon ns vac _ oceno 1 TT eoe como j CONTROL f 1 INPUT De GND AC ONLY L7 oceno sorsmm TT TT 1 oceno TCAS ENABLE I O 19 z vc CONTRoLpoweR o 20 NOTUSED NOTUSED NN voe DC INPUT 28 VDC DC OUTPUT 28 VDC DC INPUT 82 28 VDC DC OUTPUT MATING CONNECTOR MATING CONNECTOR MS24266R16B24SN MS24266R22B19SN AC IN OUT 2 10 FIGURE PINOUT TABLE REVISION 10 17 98 PAGE 2 15 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 CONNECTOR 125 2 11 FIGURE CONNECTOR CONFIGURATION REVISION 10 17 98 PAGE 2 16 L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT INC 631 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 3 TESTING 3 1 INSTALLATION TESTING The following test procedure will e2. fastener location to insure proper ground 2 5 2 Mechanical installation Switches A The switch s should be located near the existing Aircraft Landing Light switches B Individual lights can be controlled by ground the appropriate pin on the Pulselite unit See Figure 2 8 REVISION 10 17 98 2 9 L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 p 2 6 FIGURE PHYSICAL DIMENSIONS REVISION 10 17 98 PAGE 2 10 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT INC 631 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 2 7 ELECTRICAL INSTALLATION All wiring should be secured to prevent chafing and faulty connections Refer to Advisory Circular 43 13 2A NOTE Precise Flight recommends that Mil W 22759 wiring be utilized in the Pulselite installation DO NOT USE ALUMINUM WIRE NOTE Wiring precautions A Observe proper cable routing 1 e avoid tie wrap
3. 1 CH A1 PULSE ON 2 CH ATI UIGHT ON CH C2 OUT 12 CRAFT EXTERNAL LIGHT T 3 CH BTEPULSE ON AFT BUS ULSELITE 4 CH BI LIGHT ON 5 CH CILPULSE ON CH QUT 4 CRAFT EXTERNAL LIGHT T VOLT AC CH B2 OUT 10 EXTERNAL LIGHT 11 c2 Puts on J 12 CH C2 FLIGHT ON CH B1 OUT 22 RAFT EXTERNAL LIGHTS OLT DC MODEL 1152 ONLY 14 PULS CH B2 OUT 2 18 TCAS ENABLE S ANNUN INPUT 16 17 SOFT START 2 8 FIGURE BLOCK DIAGRAM REVISION 10 17 98 PAGE 2 12 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 2 8 1 Determine the amperage on individual channels Proper wire and circuit protection should be observed SEE Fig 2 9 CU WIRE AN CIRCUIT FUSE GAUGE BREAKER 22 amps 2 9 FIGURE WIRE TABLE Approved wire specification is MIL W 22759 16 or equivalent Fuse specification is MIL F 15160 or equivalent Circuit breaker specification is MIL C 5809 or equivalent To protect the Pulselite control unit and insure proper installation it is important to check that ground terminal connector 1 pin 13 of the control unit is properly grounded to the aircraft frame with a No 20 gauge wire or
4. 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC PRECISE FLIGHT INC 6312 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 2 5 1 Mechanical installation Pulselite Control Unit 2 5 2 Mechanical installation Switches 2 6 FIGURE PHYSICAL DIMENSIONS 2 7 ELECTRICAL INSTALLATION 2 7 1 Electrical Installation 2 8 FIGURE BLOCK DIAGRAM 2 8 1 Determine the amperage on individual channels 2 9 FIGURE WIRE TABLE 2 10 FIGURE PINOUT TABLE 2 11 FIGURE CONNECTOR CONFIGURATION 3 TESTING 3 1 INSTALLATION TESTING 3 2 EMI RFI TESTING 3 2 1 Procedures 3 2 2 Communications 3 2 3 Ground Navigation Systems 3 2 4 Weather Radar 3 2 5 Autopilot and Flight Director 3 2 6 Conclusion 4 OPERATION 4 1 NORMAL OPERATION 5 DOCUMENTATION 5 1 DOCUMENTATION 5 2 RETURN AUTHORIZATION 5 3 WARRANTY SERVICE REVISION 10 17 98 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC 2 8 2 9 2 10 2 11 2 11 2 12 2 13 2 13 2 15 3 1 3 1 3 2 3 3 3 3 3 4 3 6 3 6 3 7 4 1 4 1 5 1 5 1 iii PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 6 APPENDIX A 6 2 6 1 1 PARTS LIST 6 2 REVISION 10 17 98 PAGE iv L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC ae FLIGHT INC 63120 PO
5. Lamp brightness REVISION 1 95 pounds 0 88 kilograms Radiation and Convection 5 45 in W 7 63 in D 2 18 in H 13 84 W 19 38 cm D 5 54 H 28 VDC Control Voltage 11 29 VDC 115VAC Switching Voltage Model 1151 amp 1152 28 VDC Switching Voltage Model 1152 0 05 amps 600 Watt AC 200 Watt DC Model 1151 6 Amps 115 VAC Model 1152 6 Amps 115 VAC amp 7 Amps 28VDC 6 Less than 200 ft AGL at Night amp IMC Conditions 5 to 158 F 15 C to 70 43 48 Pulses per minute 3 lights On 3 lights off Full power during Pulse 50 in Dim Mode AC Circuits only Slight resistance through Pulselite Control Unit 10 17 98 PAGE 1 2 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT INC 631 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 1 5 UNITS AND ACCESSORIES SUPPLIED Pulselite Model 1151 or Model 1152 Kit including a Pulselite Control Unit b Copy of the Supplemental Type Certificate c Switches or Switch Specification d Wire Harness or Wiring Harness Drawing e Installation Wiring Diagrams f Installation Drawing 1 6 INSTALLATION APPROVAL BASIS The person who performs or supervises the installation of the Pulselite Model 1151 or Model 1152 may be required to prepare FAA form 337 See Fig 1 7 for a Sample Description of Work Accomplished Data that can be used as a ba
6. equivalent ground strap Chassis of unit should be mounted to airframe and interfaces burnished to ensure a good ground Power input for the Pulselite Control Unit are through Connector 1 Pin 19 One 3 Amp circuit breaker is required between the aircraft bus and this pin This pin provide internal control voltage for the Pulselite Control Unit The switching capability for each lighting channel is handled through pins 1 through 12 on Connector 1 Use at least 22 gauge wire for these circuits The Pulselite circuit breaker s should be located in the existing aircraft circuit breaker panel However if this is not possible they may be located within the Pulselite switch panel REVISION 10 17 98 PAGE 2 13 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 CONNECTOR 1 CONNECTOR 2 PULSELITE CONNECTOR PINOUT TABLE CONNECTOR 1 SHELL SIZE 16 CONNECTOR 2 SHELL SIZE 22 MS24264R16B24PN MS24264R22B19PN PIN VOLTAGE FUNCTION ____ CHNL PIN VOLTAGE FUNCTION 1 DCGND_ PULSE CONTROL 1 115 VAC ACINPUT L2 DC GND STEADYON ___ 2 115 VAC AC OUTPUT 3 DCGND PULSE CONTROL 3 115VAC AC INPUT 4 DC GND STEADY ON 4 115 VAC AC OUTPUT 5 DC GND PULSE CONTROL 5 115 VAC AC INPUT 6 DC GND STEADY ON 6 115 AC O
7. results including any discrepancies note The ground test results shall be recorded in the permanent aircraft records by the installing mechanic or a mechanic with the proper ratings 3 2 1 Procedures During the following tests the aircraft shall be supplied with adequate aircraft power at or above the minimum bus voltage for the aircraft The airplane should be located for proper radio reception and radar operation usually outside 3 2 2 Communications A Select Comm 1 to a local frequency in the lower end of the COMM frequency band Check for clarity of reception and background noise with all Pulselite equipment operating Repeat for all Comm radios Remarks B Select Comm to a local frequency in the upper end of the COMM frequency band Check for clarity of reception and background noise with all Pulselite equipment operating Repeat for all Comm radios Remarks REVISION 10 17 98 PAGE 3 3 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 C Verify that the intercom is free from noise and interference caused by the Pulselite installation Remarks 3 2 3 Ground Navigation Systems A VOR DME 1 Select VOR 1 receiver to a local frequency center CDI needle of HSI with TO indication Listen for background noise 2 Switch Pulselite equipment on and of
8. C 631 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 C Magnetic Compass With Pulselite equipment OFF note compass heading Turn Pulselite equipment ON and compare compass heading THIS TEST MUST BE REPEATED WITH THE AIRCRAFT HEADED IN FOUR DIRECTIONS APPROXIMATELY 90 DEGREES APART Compass Readings PulseliteON Puselite OFF ET Remarks 3 2 4 Weather Radar CAUTION USE CAUTION WHEN OPERATING RADAR FOLLOW RADAR MANUFACTURERS RECOMMENDATIONS FOR SAFETY A Select WxRadar ON After proper warm up time select TEST mode confirm proper operation Select MAP mode and note display Turn on Pulselite equipment and note any changes Remarks 3 2 5 Autopilot and Flight Director Turn on autopilot and perform ground check per the autopilot manufacturers instructions in the flight manual Turn on the Pulselite equipment and again perform check Note any discrepancies Remarks REVISION 10 17 98 PAGE 3 6 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 3 2 6 Conclusion EMI Test Data Record Date 1 Location _ _ _ O Comments REVISION 10 17 98 PAGE 3 7 L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT INC 631 20 PO
9. INSTALLATION REPORT NO 8034 Serial Number PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE STARLIGHT INSTALLATION MANUAL MODELS 1151 amp 1152 esU NS THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION ON THE PRECISE FLIGHT INC COMPANY AND ITS RECEIPT OR POSSESSION DOES NOT CONVEY ANY RIGHTS TO REPRODUCE DISCLOSE ITS CONTENTS OR TO MANUFACTURE USE OR SELL ANYTHING IT MAY DESCRIBE REPRODUCTION DISCLOSURE OR USE WITHOUT SPECIFIC WRITTEN AUTHORIZATION OF THE PRECISE FLIGHT INC COMPANY IS STRICTLY FORBIDDEN REVISION 10 17 98 PAGE L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC ae FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 TABLE OF CONTENTS TABLE OF CONTENTS ii LIST OF ACTIVE PAGES V REVISIONS vi 1 GENERAL INFORMATION 1 1 1 1 INTRODUCTION 1 1 1 2 PRODUCT DESCRIPTION 1 1 1 3 TECHNICAL CHARACTERISTICS 1 2 1 4 FACTORY SETTINGS 1 2 1 5 UNITS AND ACCESSORIES SUPPLIED 1 3 1 6 INSTALLATION APPROVAL BASIS 1 3 1 7 FIGURE FAA FORM 337 1 4 1 8 ENVIRONMENTAL QUALIFICATIONS 1 5 1 9 FIGURE ENVIROMENTAL TEST TABLE 1 5 1 10 AIRCRAFT CERTIFICATION 1 6 2 INSTALLATION 2 7 2 1 GENERAL 2 7 2 2 UNPACKING AND INSPECTION 2 7 2 3 INITIAL BENCH CHECK 2 7 2 4 COOLING 2 8 2 5 MECHANICAL INSTALLATION 2 8 REVISION 10 17 98 PAGE ii L FAA Inventory PULSELIT 1
10. ON MANUAL MODEL 1151 P N dated insert current revision date of manual and guidance in FAA Advisory Circulars 43 13 1A chapter 11 and 43 13 2A Chapter 1 amp 2 electrical load analysis was performed and the revised continuous load of the alternator generator or other supply does not exceed 80 of capacity D A complete operational test was performed according to PULSELITE 1150 Installation Manual P N 8034 date ____ The equipment performed satisfactorily and did not adversely affect existing components or systems in the aircraft as required by FAR 23 1301 FAR 23 1431 or FAR 25 1301 FAR 25 1431 FAR 27 1301 FAR 27 1431 FAR 29 1301 or FAR 29 1431 as applicable E The aircraft equipment list was revised to reflect these changes weight and balance data was revised and placed in the aircraft records A Precise Flight Inc PULSELITE Aircraft Flight Manual Supplement dated was placed in the aircraft 1 7 FIGURE FAA FORM 337 REVISION 10 17 98 PAGE 1 4 L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 1 8 ENVIRONMENTAL QUALIFICATIONS NOMENCLATURE PULSELITE MODEL NUMBER 1150 MANUFACTURER SPECIFICATION PULSELITE PERFORMANCE REQUIREMENTS MANUFACTURER PRECISE FLIGHT INC 63120 POWELL BUTTE RD BEND OR 97701 CONDITIONS DO160D DESCRIPTION OF TESTS CONDUC
11. Pulselite requires 24 28VDC The six separate controlled power circuits of the 1151 Model are to pulse six AC Powered aircraft lamps The Model 1152 controls four AC Powered aircraft lamps and two DC powered lamps Pulsing the landing lights enhances the aircraft flight path recognition quality and may be utilized any time the pilot desires By flashing the landing taxi and recognition lights approx 46 times per minute in a variety of patterns the Pulselite Control Unit creates an illusion of exaggerated motion that other pilots can immediately recognize and avoid Precise Flight recommends that the landing lights be turned on steady full time when the aircraft is within 200 AGL at night Due to possible disorientation the Pulselite should not be operated in clouds at night or on the ground The landing lights may be turned on steady rate by simply switching the original landing taxi recognition lights on REVISION 10 17 98 PAGE 1 1 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 1 3 TECHNICAL CHARACTERISTICS Weight Cooling Dimensions Operating Voltages Operating Current Maximum Load per Switching Circuit Number of circuits Usage limitations Ambient operating range Limited by output pin 1 4 FACTORY SETTINGS Pulse rate Sequence normal
12. TED SECTION _______ _____ ______ __ __________ HUMDTY 60 ____________ __ _____ CRASH SAFETY EXPLOSION ___90 ____80 EXPLOSION WATERPROOFNESS CATEGORY W FLUIDS SUSCEPTIBILITY NOT REQUIRED SAND AND DUST NOT REQUIRED CONDUCTED SUSCEPTIBILITY SUSCEPTIBILITY RADIO FREQUENCY 20 0 CATEGORY A SUSCEPTIBILITY RADIO FREQUENCY EMISSION CATEGORY B _ d 1 9 FIGURE ENVIROMENTAL TEST TABLE REVISION 10 17 98 PAGE 1 5 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 1 10 AIRCRAFT CERTIFICATION Unless otherwise provided the Pulselite Model 1151 amp Model 1152 is approved by the following STC s 1 2 3 REVISION Type of Certification Supplemental Type Certificate Certification Number SA2622NM amp ST00717SE Certification Basis Approved Model Listing Certification Date Sept 1 1999 amp July 13 1999 10 17 98 PAGE L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC 1 6 7 PRECISE FLIGHT INC 631 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 2 INSTALLATION 2 1 GENERAL The Pulselite Model 1151 or Model 1152 should be installed according to this manual and AC 43 13 1A and 2A Cable harnesses and mechanical supports must be
13. UTHORIZATION In order to expedite repair of units call the factory for a return authorization number before returning equipment for service 5 3 WARRANTY SERVICE Precise Flight warrants products in accordance with the warranty statement in effect at the time of equipment registration All repairs are performed at the factory Contact Precise Flight Inc for a warranty return authorization All requests for warranty payment must be submitted on a standard warranty claim form accompanied by the dealer invoice Authorized warranty work performed by the dealer will be limited to removal and re installation of units on an exchange basis Precise Flight Inc will bear the cost of warranty returns both ways via UPS surface delivery only Precise Flight reserves the right to use reconditioned parts in repairing the product or to use reconditioned units as warranty replacements For technical information and service call 1 800 547 2558 REVISION 10 17 98 PAGE 5 1 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 6 APPENDIX A 6 1 1 PARTS LIST REVISION 10 17 98 6 2 L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC
14. UTPUT 7 DCGND PULSE CONTROL 7 115 AC INPUT 8 DCGND STEADY ON 8 115 AC OUTPUT 9 DC GND PULSE CONTROL 9 115 VAC AC INPUT 10 DCGND STEADY ON 10 115 VAC AC OUTPUT 11 DC GND PULSE CONTROL C2 11 115 VAC AC INPUT C2 12 DCGND STEADY ON jee __ 115 VAC OUTPUT 13 DC GND UNIT GROUND eee 41 11 CONTROL e mn _ ___ ___ _ INPUT 16 DCGND 19 06 en Teosta 18 DCGND TCASENABLE 1 19 28 0 T ie MG d a A MATING CONNECTOR MATING CONNECTOR MS24266R16B24SN MS24266R22B19SN REVISION 10 17 98 PAGE 2 14 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC ae FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 PULSELITE 1152 CONNECTOR PINOUT TABLE CONNECTOR 1 SHELL SIZE 16 CONNECTOR 2 SHELL SIZE 22 MS24264R216B24PN DC CONTROL MS24264R22B19PN AC IN OUT amp DC INOUT PIN VOLTAGE FUNCTION gt CHNL PIN T VOLTAGE FUNCTION CHNL 771 DCGND PULSECONTROL 1 15902 ACINPUT gt _ __ gt 1 5 vac ac oUTPUT s De GND PULSE CONTROL 3 USED NOT USED 4 oceno STEADYON B Norustb NOTUSED _ 5 PULSE CONTROL c 5 c _ STEADYON ___ C s 1 5 vac__ Ac oUrPUT 2
15. WELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 4 OPERATION 4 1 NORMAL OPERATION Pulsing the landing lights tend to enhance the aircraft flight path recognition quality and may be utilized any time the pilot desires By flashing the landing taxi and recognition lights approx 46 times per minute in a variety of patterns Pulselite creates an illusion of exaggerated motion that other pilots can immediately recognize and avoid While the Pulselite has been tested throughout the entire landing phase of flight Precise Flight recommends that the landing lights be turned on steady full time when the aircraft is within 200 AGL at night The Pulselite system should not be operated in clouds at night or in the close proximity of other aircraft on the ground due to possible disorientation The landing lights may be turned on steady at any time by simply switching the original landing taxi recognition lights on The Pulselite will remain active until the Pulselite switch is turned OFF REVISION 10 17 98 PAGE 4 1 L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC r PRECISE FLIGHT INC 631 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 5 DOCUMENTATION 5 1 DOCUMENTATION To ensure technical updates and notifications fill out and return the warranty document and a copy of the 337 if appropriate 5 2 RETURN A
16. WELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 LIST OF ACTIVE PAGES ORIGINAL ADDED PAGES PAGE REV REV PAGE REV PAGE REV m REVISION 10 17 98 PAGE v L FAA Inventory PULSELIT I 151 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 REVISIONS REV NO PAGE DESCRIPTION DATE REVISION 10 17 98 PAGE vi L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 1 GENERAL INFORMATION 1 1 INTRODUCTION This manual contains information regarding the physical mechanical and electrical characteristics as well as installation information pertaining to the Precise Flight Pulselite Model 1151 amp 1152 Control Unit For maintenance and repair information contact Precise Flight Inc 1 2 PRODUCT DESCRIPTION The Pulselite Model 1151 amp 1152 Control Units are a compact set of electrical components that will apply regulated pulsing power to the landing taxi or recognition lights instead of the normal steady on The Pulselite connects easily to an aircraft s external lighting system and may be installed on a wide variety of aircraft with differing light sequence combinations The control circuit of the
17. f check for interference and needle deviation 3 Repeat for all other VHF NAV radios 4 Tune VOR Nav 1 to a local VORTAC station with Pulselite equipment off Note distance on DME and listen for noise Turn Pulselite equipment on and compare distance readings and background noise Repeat for all other VHF NAV radios Remarks Loran 1 Observe Loran self test responses and signal to noise ratios Turn Pulselite equipment on and recycle Loran and compare results Remarks REVISION 10 17 98 PAGE 3 4 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 C RNAV 1 VOR MODE Set to VHF on a local frequency center CDI and pilots HSI turn on Pulselite equipment and check for interference Remarks 2 DME MODE With Pulselite equipment off set to local VHF frequency and note DME reading Turn on Pulselite equipment and compare DME reading Verify reading with known distance Remarks 3 RNAV MODE With Pulselite equipment off set local VHF frequency set waypoint bearing to 180 and waypoint distance to 25 miles Center CDI and note RNAV readings Turn Pulselite equipment on and note any changes in RNAV readings Remarks REVISION 10 17 98 PAGE 3 5 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT IN
18. fabricated by the installing agency to these requirements or supplied by Precise Flight for specific aircraft installations This section contains interconnect diagrams mounting dimensions and other information pertaining to a Pulselite installation 2 2 UNPACKING AND INSPECTION Exercise care when unpacking the equipment Make a visual inspection of the unit for evidence of damage incurred during shipment If a claim for damage is to be made save the shipping container to substantiate the claim The claim should be filed with the transportation company Retain the container and packaging material after the equipment has been removed should equipment storage or reshipment become necessary 2 3 INITIAL BENCH CHECK Every Pulselite Model 1151 amp Model 1152 has been checked for operation before shipment The installing agency can insure Pulselite operation before final installation by utilizing Paragraph 3 1 for this procedure REVISION 10 17 98 PAGE 2 7 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 2 4 COOLING Elevated operating temperatures reduce reliability Forced air cooling is not required however allow approx 1 of space around the control unit for adequate convective cooling Space is most critical on the unit sides so that the heat sink fins may dissipate heat at the pr
19. joining power lines to antenna leads intercom or radio leads B Be sure that all connections are sound i e avoid frayed or split conduit ends C Avoid sharp bends or undue strain on cables 2 7 1 Electrical Installation A After the Pulselite Control Unit has been properly mounted determine the lighting pulse mode Find the total wattage of the lamp s connected to the Pulselite Control Unit Divide the highest total wattage by the voltage The result will be the highest amperage rating on the Pulselite Control Unit Amperages should not exceed 6 amps per channel or 600 Watts per channel AC or 7 amps per channel or 200 Watts DC See Example below 400 Watts 115 Vac 347_Amps REVISION 10 17 98 PAGE 2 11 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 ULSELITE CONTROL UNIT MODEL 1151 or 1 EXT LTS a 2 3 10 e E ls TT LTS T N 10 e 5 CH Cf l gg PWR IN MODEL 1151 ONLY OUT 8 gt DC PWR IN MODEL 1152 ONLY 32 120 VOLT AC 221 M Ty AIRCRAFT EXTERNAL LIGHTS 19 UNIT POWER UNIT GND AFT EXTERNAL LIGHT VATT 00 HZ 115 VOLT AC CH EXTERNAL LICHT 20 VOLT AC BOX REF
20. oper rate 2 5 MECHANICAL INSTALLATION Listed below are considerations to be examined before installing the Pulselite Model 1151 or 1152 Close attention to these suggestions will assure optimum performance when completed 2 5 1 Mechanical installation Pulselite Control Unit A Select a location for the Pulselite Control Unit which is suitably ventilated for avionics CAUTION The standard Pulselite Model 1151 or Model 1152 is not approved for use in a potentially explosive environment refer to AC 43 13 2A Chapter 2 Radio Installation Locate Pulselite away from fire hazard zones highly explosive or corrosive areas potentially hazardous fluid areas e g water fuel hydraulic fluid or oxygen units etc B The Pulselite Control Unit must be installed in a structurally substantiated location A typical wiring diagram and physical installation is provided in Appendix A C Allow adequate space for installation of cables and connectors D The Pulselite Control Unit should be installed in an avionics bay or other suitable location REVISION 10 17 98 PAGE 2 8 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC 7 PRECISE FLIGHT INC 631 20 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 E Although the Pulselite Control Unit can be installed in any axis the preferred orientation is with the fins vertical Use 4 10 32 pan head screws Burnish one
21. repair station rated in the equipment involved or an FAA Avionics Inspector for applicable test procedures The evaluation will be with a series of equipment checks on the ground to determine that no detrimental EMI RFI effects are introduced into the aircraft by the Pulselite system The electrical systems installed in the aircraft will be referred to as the Pulselite system in this procedure The following tests should performed by personnel familiar with both aircraft systems and proper operation as well as the Pulselite equipment and its proper operation Any and all discrepancies shall be noted Any discrepancies noted during these procedures must be reported to Precise Flight Inc and evaluated for cause extent and as to what corrective action should be taken to correct the problem The aircraft may not be flown after discrepancies are found unless the Pulselite system is disconnected at the aircraft bus until such time as the problems have been corrected and the aircraft has successfully passed the ground portion of this test Only then may the aircraft be flown to complete this test REVISION 10 17 98 PAGE 3 2 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 A record of this test shall be recorded in the aircraft logbook The entry should include date aircraft time and
22. sis for approval for return to service are A AC 43 13 1A Acceptable Methods Techniques and Practices Aircraft Inspection and Repair B AC 43 13 2A Acceptable Methods Techniques and Practices Aircraft Alterations C FAA approved Manufacturer s Installation Instructions Equipment installation procedures do not differ significantly among various aircraft The installation and operation of the Pulselite Model 1150 does not materially affect the aircraft operation or performance The Sample Description of Work Accomplished Figure 1 7 is suggested language provided as a convenience to the installing agency The information and wording should be modified to correctly describe the particular installation Precise Flight Inc can assume no responsibility for the alteration of the airframe or electrical system REVISION 10 17 98 PAGE 13 L FAA Inventory PULSELIT 1 15 1 8034 1151 amp 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 8 Description of Work Accomplished If more space is required attach additional sheets Identify with aircraft nationality and registration mark and date work completed A The following components were installed PULSELITE UNIT MODEL 1151 or MODEL 1152 S N SWITCH Switch P N B The Unit was installed in position in the aircraft according to instructions in the PRECISE FLIGHT INSTALLATI
23. valuate the installation in the aircraft 1 Check wiring amp connections before applying power 2 Switch the Pulselite Unit to ON and verify that the appropriate Landing Taxi Recognition Lights are flashing on the aircraft 3 Switch the appropriate Landing Taxi Recognition Lights ON utilizing the existing switches and verify that the lights remain on without flashing 4 Switch to DIM if installed and Pulselite Unit to ON notice lights flash with reduced intensity 5 TCAS TEST TO BE DETERMINED 6 Switch the Pulselite Control Unit off and the existing Landing Taxi Recognition Light switches are off and verify that the Landing Taxi Recognition Lights are OFF REVISION 10 17 98 PAGE 3 1 L FAA Inventory PULSELIT 1 15 1 8034 1151 1152 INSTALL MANUAL DOC m PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 1151 amp MODEL 1152 3 2 EMI RFI TESTING The following is an outline for determining that no detrimental Electro Magnetic Interference EMI or Radio Frequency Interference RFI is caused by the installation of a Precise Flight Pulselite product per FAR 23 1431 25 1431 27 1431 or 29 1431 These procedures are not necessarily all encompassing in that they may not include all of the equipment installed in the airplane If electronic and navigation equipment is installed which is not included in this document consult the equipment manufacturer an FAA approved
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