Jabiru Aircraft Pty Ptd Aircraft Service Manual Jabiru J160 / J170
Contents
1. ALO 2530 ON Lid WALI H3NNIdS 0917 aqogsalvey L alld SNINSNY H3NNIdS 0917 000681 zi M3HSvM vrz ZLlO SEIEV AGHOS 3NIHOV ISOE69TZSW L viva O 43438 S 9 17089 VI TNV 9 9 IAN M2O01AN Szv S9 0zSW 8p S3HSVM 3TIIATTT38 NglovrHd 9 S S doud 6 INNOW dONd 39 Ezcleor ONDOVE 5 0917 00068 LI vC AW 3S2 XdVl HOHONY 90169012SW VV NOILIAS 3j9NY Jj SNLLNDIOW LJYHSONYHO Wiad 335 NOLIYTTWLSNI LNN MOHONY 304 Lc pe NOULO3PO3d 3W23S LON GO 534 34 NI SNOISN3MHIQ Ald HO3lAv 40 LN3SNOD LhOHLIA 031909 38 JON ISNA ONY LHORAdOO SI SIHL Figure 50 Propeller Installation e u N uw 5 lt 02 a 2 o 2 Ke CN 2 5 9 o 2 x g files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM L Mfiles Technical_manuals J160_J170 J160_ amp _J170_workin Jabiru Aircraft me Instruction amp Maintenance Manual Jabiru 2200 Aircraft Engine IMPORTANT The Spinner is an important and integral part of the propeller Assembly It is essential to ensure adequate engine cooling The air2. NOLLO3POMd JOS LON OG SIHLIANIN NI SNOISNINIG 031909 38 LON 5 ONY LHSIYAdOS SI ONIAWHO SIHL Figure 49 VHF Antenna Installation Ww 5 A 02 tn 2 o 0 Ko 2 9 o 2 x g_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM L files Technical_manuals J160_J170 J160_ amp _J170_workin Jabiru Aircraft me Aircraft Service Manual Jabiru J160 7 7170 Variants 14 SECTION 15 PAINTING amp FINISHING 14 4 INTERIOR The interior is painted with BERGER Matt Vinyl Standard colour 15 Fumosus A154 Grey 14 2 EXTERIOR 14 2 1 PAINTING The following painting procedure as used at the Jabiru factory had proven successful in ensuring good presentation of the aircraft 2 part paint should be used for best results Due to the variation between different paints we recommend carefully following the pack recommendations relating to surface preparation and safety Use a bare minimum of undercoat preferably white or cream and topcoat to keep weight down If you have had no previous painting experience a short course may be available from TAFE NOTE It is very easy to dramatically increase the weight of the aircraft with a heavy paint job Care must be taken to use the absolute minimum amounts of filler undercoat
3. EN e N oh RES Gh 9 BRS safe amp 8 p 5 mb ul 4 Won c e 5 5 S5 id OIO O OO 0 0 O 989 Wlad 335 Ww C1 5 A 02 tn 2 o 0 Ko 2 Figure 44 Instrument Panel Layout Basic Panel V TVLIA 335 G310N SSIINN o I5 H3N3ISv4 Ty o I 1 T s 5 2 aos S 2 2 E p 3Nruno TaNVd e m x o e wo 3198 LON S3ML3WFIIN NI SNOISN3HIG eese MM REVISION files J160_ amp _J170_Tech doc L Miles Technical_manuals J160_J170 J160_ amp _J170_workin Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 12 2 3 INSTRUMENT REMOVAL Most instruments are secured to the panel with screws inserted through the panel face To remove an instrument disconnect wiring or pluming to the instrument remove mounting screws and take instrument out from behind or in some cases from the front of the panel In all cases when an instrument is removed disconnected lines or wires should be protected Cap open lines a
4. Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 11 4 FUEL SHUT OFF VALVE See Figure 46 or 47 depending on model variant 11 4 1 DESCRIPTION The fuel shut off valve is a two position ON OFF valve which is located in front of the main longitudinal beam 11 4 2 FUEL VALVE REMOVAL amp INSTALLATION 16 Turn OFF both taps between wing tanks and header tank Cover both tank vents 2 Remove fuel shut off valve cover Remove shut off valve handle 4 Remove cover plate 5 Disconnect and cap fuel lines at shut off valve 6 Remove shut off valve 7 Reverse the preceding steps for installation WARNING Fuel valves between wing tanks and header tanks must be in the ON position during flight CS VLA variants must have these taps wired ON using electrical fuse wire Ensure wing tank cap vent covers are removed 11 5 FUEL FILTERS 11 5 1 CS VLA FILTER DESCRIPTION The fuel filter is of the in line type and is located inside the header tank enclosure behind the seats 11 5 2 NON CS VLA MODEL VARIANT FILTER DESCRIPTION The fuel filter is of the in line type and is located just inside the cabin above the rudder pedals 11 5 3 CS VLA MODEL FUEL FILTER REMOVAL amp INSTALLATION 1 Turn fuel valves between wing tanks and header tank to OFF Cover wing tank vents 2 Try to kink to main fuel line above the fuel filter being careful not to
5. assuming that the altimeter has been tested and inspected in accordance with the current Regulations 5 Ensure the static system is free from entrapped moisture and restrictions 2 Ensure no alternations of airframe surface have been made which would effect the relationship between air pressure in the static pressure system and truce ambient static air pressure for any flight configuration Attach source of suction to static pressure source opening Figure 50 shows method of obtaining suction 4 Slowly apply suction until the altimeter indicates a 1000 foot increase in altitude revision Dated July 2005 Issued By RAS Page 125 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft mm Aircraft Service Manual Jabiru J160 J170 Variants CAUTION When applying or releasing suction do not exceed the range of either vertical speed indicator or airspeed indicator 5 Cut off suction source to maintain a closed system for one minute Leakage shall not exceed 100 feet altitude loss as indicated on the altimeter 6 If leakage rate is within tolerance slowly release suction source NOTE If leakage rate exceeds maximum allowable first tighten all connections then repeat leakage test If leakage rate still exceeds maximum allowable use the following pr
6. 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 12 3 7 TROUBLE SHOOTING AIRSPEED INDICATOR Table 10 Trouble Shooting Airspeed Indicator Trouble Probable Cause Remedy Pitot pressure connection not Test line and connections for leaks Repair or replace praperiy connecisd t damaged line tighten Hand fails to response pressure line from pitot tube 9 gt Ug connections Pitot or static lines clogged obstructions Blow out lines Test lines and connections for leaks Repair or replace Leak in pitot or static lines damaged lines tanten Incorrect indication or 9 mild connections Substitute known good Defective mechanism or d goor indicator and check reading leaking diaphragm Replace instrument Check panel shock mounts Excessive vibration Replace defective shock mounts Hand vibrates Check clamps and line connections for security Excessive tubing vibration Tighten clamps and connections replace tubing with flexible hose 12 3 8 TROUBLE SHOOTING ALTIMETER Table 11 Trouble Shooting Altimeter Trouble Probable Cause Remedy Static line plugged Check line for obstructions Blow out lines Instrument fails to f operate Substitute known good Defective mechanism altimeter and check reading Replace instrument Hands not carefully set Reset
7. 3 Replace Gauge 12 8 EXHAUST GAS TEMPERATURE GAUGE OPTION The Exhaust Gas Temperature Gauge is a Thermo couple instrument and is not connected to the aircraft electrical system See Wiring Diagram Figure 51 Should the instrument fail to operate 1 Check loose terminal connections and damage to wiring 2 Replace thermo couple 12 9 HOURMETER The Hourmeter is an electronic instrument An optional Airspeed Switch may be fitted Should the instrument fail to operate Ti Check 10amp instrument fuse and replace if necessary 2 Check 30amp main fuse and replace if necessary Remove Instrument Panel see Paragraph 13 2 3 and check cable terminals for security 4 Replace Gauge 12 10 MAGNETIC COMPASS The Magnetic Compass is liquid filled with expansion provisions to compensate for temperature changes It is equipped with compensating magnets adjustable from the front of the case No maintenance is required on the compass except an occasional check on a compass rose for adjustment and compensation REVISION Dated July 2005 Issued By RAS Page 134 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 12 11 GYRO INSTRUMENT PACKAGE OPTION A vacuum pump driven Art
8. 5 OIL PRESSURE GAUGE The Oil Pressure Gauge is an electronic instrument Should the instrument fail to operate 1 2 5 6 Check 10 instrument fuse and replace if necessary Check 30amp main fuse and replace if necessary Remove Instrument Panel see Paragraph 13 2 3 and check cable terminals for security Check wiring at Sender for security Replace Sender Replace Gauge 12 6 OIL TEMPERATURE GAUGE The Oil Temperature Gauge is an electronic instrument Should the instrument fail to operate 1 Check 10 instrument fuse and replace if necessary 2 Check 30amp main fuse and replace if necessary 3 Remove Instrument Panel see Paragraph 13 2 3 and check cable terminals for security REVISION Dated July 2005 Issued By RAS 133 of 156 L MilesYTechnical manuals160 J1701J160 amp J170 working files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 4 Check wiring at Sender for security 5 Replace Sender 6 Replace Gauge 12 7 CYLINDER HEAD TEMPERATURE GAUGE The Oylinder Head Temperature Gauge is a Thermo couple instrument and is not connected to the aircraft electrical system See Wiring Diagram Figure 51 Should the instrument fail to operate 1 Check for loose terminal connections and damage to wiring 2 Replace thermo couple
9. Aircraft me Instruction amp Maintenance Manual Jabiru 2200 Aircraft Engine 19 8 PROPELLER BALANCING PROCEDURE Propeller balance should be checked by locating a 16mm tube to firmly fit the centre mounting hole of the Propeller and balancing on knife edges Tolerances e Imbalance shall not exceed the following limit whatever the position of the Propeller in the plane of rotation 750 mm gms approximately 1 gm at the tip The balance may only be corrected by the application of epoxy paint Any other method of securing balance is PROHIBITED Propellers outside these limits should be rejected as unserviceable or returned to JABIRU for assessment and possible repair REVISION Dated June 2005 Issued By RAS 155 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me struction amp Maintenance Manual Jabiru 2200 Aircraft Engine 20 APPENDIX V AIRWORTHINESS LIMITATIONS 20 1 GENERAL This Section sets forth each mandatory replacement time structural inspection interval and related structural inspection procedure 20 2 MANDATORY REPLACEMENT TIME The following components MUST be replaced at the intervals described hereunder Table 17 Mandatory Replacement Times Description Part No Interval Hours Rud
10. By RAS Page 144 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 15 2 COCKPIT CONTROL DECALS Table 14 Cockpit Control Decals Decal Detail Preview Loading Limitations P No 5098894 Fit to right side of fuselage between window and beam Trim Position P No5024094 NOSE DOWN NEUTRAL TRIM NOSE UP BRAKE ON 4 Fitted on the Top of the Main Beam Beside the trim control Fuel Tap Position P No 502319N FAN om Fue OFF Fitted on the Main Beam in front of the Fuel SELECTOR Valve Fuel Tap Position P No 502329N OFF on FUE Fitted on the rear of the fuselage beam next to the wing tank valves Choke Cable P No5051094 CHOKE PULL ON REVISION lo Dated July 2005 Issued By RAS Page 145 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft pty pta 7 sro Aircraft Service Manual Jabiru J160 J170 Variants Decal Detail Preview Fitted at the base of the choke cable Carby Heat P No 5026194 CARB HEAT C PULL ON Fitted at the base of the CARBY Heat Cable 15 3 EXTERNAL FUS
11. UBE STRAIGHT PITO WING STRUT ASSY ITEM PART DESCRIPTION QTY PITOT ASSEMBLY Figure 45 Pitot Assembly revision Dated July 2005 Issued By RAS 130 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft pty pta 22 un Aircraft Service Manual Jabiru J160 J170 Variants E pen eel EF C Co 00 Co Les JAE era EH g mum h th s E SS qu E a o z a z pu z gt 3 2 219 19 e gt e I jam n z D r ea m TI up e es gt A COTTON FLOCK amp EPOXY TUBE TAIL FIN ENSURE TUBE IS ALIGNED WITH TOP OF FIN AND FUSELAGE Figure 46 Static Probe System Assembly Revision Dated July 2005 Issued By RAS Page 131 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft pty pta AMEN un Aircraft Service Manual Jabiru J160 J170 Variants SURGICAL TUB P d MA THICK WAI URGICAL TUBE THICK WA APPLY SUCTION Squeeze air bulb suct
12. be applied to horizontal upper surfaces REVISION lo Dated July 2005 Issued By RAS Page 143 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft pty pta srno Aircraft Service Manual Jabiru J160 J170 Variants 15 SECTION 16 PALCARDS 15 1 COCKPIT PLACARDS GENERAL Table 13 General Cockpit Decals Decal Detail Preview J160 Warning Placard P No 5A011A0D g is PROHIB Noise level at full power 95 dB A Ear KIT JABIR amp Manufactured JABIRU AIRCRAFT LTD 3UNDABERG Q Fitted on the rear Face of the Forward Wing Spar Carry D 4670 J170 Warning Placard P No 5A015A0D through Beam in the Cabin Ceiling Fitted on the rear Face of the Forward Wing Spar Carry through Beam in the Cabin Ceiling Owners Manual FLIGHT OWNERS MANUAL P No 5036194 Fitted to Inside of RH Door above the Door Pocket Door Open LHS Fitted to the Outsides of LH Door Above the Door Catch Lever Door Open RHS P No 5028094 Fitted to the outside of RH Door Above the Door Catch Level Door String Placard 5026094 PULL OPEN Fitted on Inside of both Doors Above Door Handle Fuel Contents Fitted to sight glasses of wing fuel tanks REVISION Dated July 2005 Issued
13. close opposite end of tubing and slowly roll up tube until airspeed indicator registers in the cruise range Secure tube and after a few minutes recheck airspeed indicator Any leakage will have reduced the pressure in the system resulting in a lower airspeed indication Slowly unroll tubing before removing it so pressure may be released gradually revision Dated July 2005 Issued By RAS Page 126 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 7 7170 Variants Otherwise instrument may be damaged If the test reveals a leak in the system check all connections for tightness 12 3 4 BLOWING OUT LINES Condensation may collect at points in the pitot system and produce a partial obstruction To clear line disconnect airspeed indicator Using low pressure air blow from indicator end of line toward pitot tube CAUTION Never blow through pitot or static lines towards the instruments Like pitot lines static lines may be kept clear and connections tight When necessary disconnect static line at first instrument to which it is connected then blow line clear with low pressure air Check all static pressure lines for tightness If hose or hose connections are used check for general condition and clamps for security Replace hose which h
14. damage 3 Place a cloth beneath the filter to collect any fuel which may be split during removal of the filter REVISION Dated July 2005 Issued By RAS Page 121 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 4 Disconnect the fuel lines at both ends of the filter 5 Remove filter 6 Reverse the preceding steps for installation Ensure waste cloth is removed WARNING Fuel valves between wing tanks and header tanks must be wired in the ON position using electrical fuse wire during flight Ensure wing tank cap vent covers are removed The fuel filter must only be installed in one direction arrow on the side of the filter marks the fuel flow direction Ensure this arrow is pointed towards the Firewall and Engine 11 5 4 NON CS VLA MODEL FUEL FILTER REMOVAL amp INSTALLATION 7 Turn main fuel on the cabin main beam OFF 8 Place a cloth beneath the filter to collect any fuel which may be split during removal of the filter 9 Disconnect the fuel lines at both ends of the filter 10 Remove filter 11 Reverse the preceding steps for installation Ensure waste cloth is removed WARNING The fuel filter must only be installed in one direction An arrow on the side of the filter marks the
15. fuel flow direction Ensure this arrow is pointed towards the Firewall and Engine 11 6 FUEL PUMPS 11 6 1 PRIMARY PUMP The Primary Fuel Pump is located on the Starboard rear of the Engine Refer to engine Maintenance amp Instruction Manual for details 11 6 2 CS VLA SECONDARY PUMP A secondary electronic pump is mounted inside the header tank enclosure behind the seats This pump is a back up to the Primary Pump is recommended that the Secondary Pump be engaged at least during take off and landing 11 6 3 NON CS VLA SECONDARY PUMP A secondary electronic pump is mounted inside the centre console above the rudder pedals This pump is a back up to the Primary Pump It is recommended that the Secondary Pump be engaged at least during take off and landing REVISION lo Dated July 2005 Issued By RAS Page 122 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 12 SECTION 12 INSTRUMENTS amp INSTRUMENT SYSTEMS 121 GENERAL This Section describes the typical instrument installation and its operating system Emphasis is placed on trouble shooting and corrective measures only It does NOT deal with specific instrument repairs as this usually requires special equipment and data and should be handled by instrument speci
16. hands with knob Substitute known good incorect indicato Leaking diaphragm altimeter and check reading Replace instrument Compare reading with known Pointers out calibration good altimeter Replace instrument Check lines for obstruction or Hand oscillates Static pressure irregular leaks Blow out lines tighten connections Revision Dated July 2005 Issued By RAS Page 128 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft pty pta 7 __ Aircraft Service Manual Jabiru J160 J170 Variants Trouble Probable Cause Remedy Leak in airspeed or vertical speed indicator installations Check other instruments and system plumbing for leaks Blow out lines tighten connections 12 3 9 Table 12 Trouble Shooting Vertical Speed Indicator Option TROUBLE SHOOTING VERTICAL SPEED INDICATOR OPTION Trouble Probable Cause Remedy Instrument fails to operate Static line plugged Check line for obstructions Blow out lines Static line broken Check line for damage connections for security Repair or replace damaged line tighten connections Incorrect indication Partially plugged static line Check line for obstructions Blow out lines Ruptured diaphragm Substitute known good
17. propellers with cracks or splits or any delamination of the composite sheath in the case of sheathed Propellers must be either Rejected as unserviceable or returned to JABIRU Aircraft Pty Ltd or our local approved agent for assessment and possible repair In composite leading edges nicks of a size described above may be repaired by filling with epoxy resin and Fibreflock using the procedure outlined below Propeller Repair Kit is available from JABIRU as Part No PP0049N 1 Remove Propeller as per Paragraph 5 2 Sand nick with abrasive paper to remove any fractured particles Mix resin carefully and thoroughly equal parts resin and hardener and thicken with Fibreflock to form a paste 4 Apply paste to sanded nick and allow to cure in low moisture environment for 24 hours 5 Lightly and carefully sand excess cured resin to a smooth surface matching exactly the previous aerofoil 6 Refurbish with clear Epoxy paint JABIRU Part PPOO69N 7 Rebalance Propeller see Paragraph 8 8 Reassemble and replace Propeller and Spinner see Paragraph 6 9 Check Propeller tracking and Spinner balance see Paragraph 6 10 Damaged urethane leading edges should be referred to Jabiru Aircraft Pty Ltd for repair REVISION lo Dated June 2005 Issued By RAS Page 154 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru
18. 15 08 2005 10 25 00 AM Jabiru Aircraft pty pta Aircraft Service Manual Jabiru J160 J170 Variants c m E gt z In E 4 1 c 2 a D 8 ga Ko na E E Q o 5 i Eaj 1 a Jf Figure 48 Wiring Diagram revision Dated July 2005 Issued By RAS 137 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft mm Aircraft Service Manual Jabiru J160 J170 Variants 13 3 BUS BARS Electrical power for electrical equipment and installations is supplied through Bus Bars The bus bars are mounted at the rear of the lower instrument panel Access is gained by removing the main instrument panel see Paragraph 13 2 3 13 3 1 MASTER SWITCH When using a key switch the Master Switch activates a relay which in turn powers the bus bars When using a toggle switch it activates the power direct from the battery Refer to Wiring Diagram at Figure 51 13 4 BATTERY POWER SYSTEM Refer also to Wiring Diagram at Figure 51 13 4 1 BATTERY The battery is 12 volts and appro
19. 70 SP Jabiru 2200 C000 a x A Not above 3300 RPM Jabiru J170 SPC Jabiru 2200 C000 ae 1 Not above 3300 RPM Jabiru J170 UL Jabiru2200 C000 1 a i Not above 3300 RPM 19 2 IDENTIFICATION STAMPINGS Each propeller is marked with the particulars indicated below 1 The Propeller Drawing 2 The diameter and pitches in metres proceeded by the letters respectively The type of engine for which the propeller has been designed 4 Manufacturing Serial No DWG D 1524 P 1346 JABIRU 2200 J J 4 0001 LC Jabiru Jabiru 4 Stroke Serial No Leading Edge Composite Prop Engine Protection Sheath 19 3 DESCRIPTION The Propellers are constructed from 3 laminations of approved species timber and are manufactured in accordance with the relevant approved Drawing They are single piece 2 blade propellers with an inlaid leading edge urethane Jabiru Aircraft me Instruction amp Maintenance Manual Jabiru 2200 Aircraft Engine The propeller finish is a composite sheath and clear epoxy paint JABIRU Part No PPOO39N WARNING In countries other than Australia different registration requirements will apply It is the owner s responsibility to become fully aware of the particular maintenance requirements and limitations applicable to the appropriate registration WARNING ENSURE IGNITION SYSTEM IS OFF BEFORE COMMENCING ANY WORK O
20. Check Spinner for balance by locating a fixed object on a flat floor to just clear the lower edge of the front dome of the Spinner Rotate the propeller by hand and check that the Spinner runs true Correct any imbalance by loosening and retightening Machine Screws REVISION lo Dated June 2005 Issued RAS Page 153 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Instruction amp Maintenance Manual Jabiru 2200 Aircraft Engine 19 7 SERVICING AND REPAIRS Any service or repair must take account of the risk of subsequent Propeller failure Therefore repairs are limited to the filling of small nicks in the Propeller Maximum size of nicks approved for repair is Those in Leading Edge 4mm deep x 20mm long Those across the drive Face flat sides 2mm deep x 6mm diameter scratches not more than 0 5mm deep Repairs must also take account of the changes to balance of the Propeller and therefore the Propeller should be removed in accordance with the procedure described above It must be checked for balance see Paragraph 8 prior to refitting see Paragraph 6 checked for tracking after reassembly see Paragraph 6 4 and the Spinner checked for balance after reassembly see Paragraph 6 7 Only nicks within the size tolerances described above may be repaired All
21. ELAGE Table 15 External Fuselage Decals Decal Detail Preview P No 5043094 Attach to LHS of Vertical Fin in line with Static Tube Electrical Earthing EARTH ON NOSE LEG oo Attach above the Earthing Pole adjacent to the Fuel Filler Cap Fuel Grade P No 5091344 AVGAS 100 RE CAPACITY EARTH ON POS Attach to top skin of wing adjacent to Fuel Filler Cap Wing Bolt Tightening P No 5039094 Qty 8 Required DANGER DO NOT TIGHTEN Attach to the fuselage and wings beside each wing and lift strut attachment fitting REVISION Dated July 2005 Issued By RAS Page 146 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft mm Aircraft Service Manual Jabiru J160 J170 Variants 16 APPENDIX I JABIRU 2200 ENGINE Appendix 1 of this Manual is the Instruction and Maintenance Manual for the Jabiru 2200 engine Please insert your copy of the INSTRUCTION AND MAINTENANCE MANUAL that comes with your engine into this section if you are printing this out THIS PAGE IS INTENTIALLY LEFT BLANK REVISION lo Dated July 2005 Issued By RAS Page 147 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft
22. N PROPELLER DO NOT RUN ENGINE WITH PROPELLER DISCONNECTED OR ENGINE DAMAGE WILL RESULT 19 4 INSTALLATION Refer to Figure 52 The Propeller is bolted to the Propeller Drive Flange with 6 x aircraft grade bolts attaching to Nyloc Nuts There are 8 Belleville Washers between the Aluminium Propeller Flange and each nut These Belleville washers must be fitted in pairs as shown in the attached drawing Bolts should be torqued to 6 nm 72 inch lbs in a standard torque sequence REVISION lo Dated June 2005 Issued By RAS Page 151 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM ircraft pty A ion amp Ma ine ircraft Eng iru 2200 A Jab tenance Manual in Instruct ASSY 5 8 Iv L3 nun 4 OL WALI J NYI dOMd ANDYOL LOAYYOD 404 AYM SIHL 38 LSNW 7 SNOLLO3MId 3ilSOddO NI 3974 SH3HSV A 3LON Tu W3NNIdS NI SJ10H 3Tlhd 3uUd Ag 0317901 SLNN HOHONY Z G e a p 517109 HiTl3dOHd SNIN3IHSIL 404 JONANOAS 21036 74891 SY 1703134 00768 6 982 010 ane ON OMG 1 9 HO3IAV Need 3lvQ SSI 37905 NOIIVTIVISNI LON 1130
23. al maintenance is not considered removable Access to instruments etc is gained by removing the panel facia containing the instruments from the facia T Unscrew amp remove the facia retaining screws from around the perimeter if the panel 2 Remove the front facia It is normally best to lie the facia on a cushion or similar while working to reduce the risk of damaging the instruments or facia 3 Take care not to strain connections on wires or tubes 4 Assembly is the reverse of the above procedure 12 2 2 INSTRUMENTS Refer to Figure 44 Revision Dated July 2005 Issued By RAS Page 123 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru J160 170 Variants ircraft pty A Aircraft Service Manual 30 133 5 3915 1095 D VIDVA T3NVd LNIWNULSNI _ rp f ON Wd HO31AV Sq pu SINO LND LTY 18 SSI Z V AGIA Y 5 9 31928 27725 20601 z 91 S3ovid 8 cio un 856 SZZ S3ovld TS 08 E 082 A ch o gu gt pep N NN N
24. alists Malfunctioning instruments should be either returned to JABIRU AIRCRAFT Pty Ltd or sent to an approved instrument overhaul and repair station for servicing Our concern here is with preventive maintenance on the various instrument systems and correction of system faults which will result in instrument malfunctions The descriptive material maintenance and trouble shooting information in this Section is intended to help the owner or mechanic determine malfunctions and correct them up to the defective instrument itself at which point an instrument technician should be called in Some instruments such as Oil Temperature and Pressure Gauges are simple and relatively inexpensive and repairs will usually cost more than a new instrument Flight instruments on the other hand are usually well worth repairing The words replace instrument in the text therefore should be taken only in the sense of physical replacement in the aircraft Whether replacement is to be with a new instrument an exchange one or an original instrument is to be repaired must be decided on the basis of the individual circumstances 12 2 INSTRUMENT PANEL The instrument panel assembly consists of a stationary panel The lower part of the panel contains switches and circuit breakers which are not sensitive to vibration The instruments are screw mounted to the panel 12 2 1 INSTRUMENT PANEL REMOVAL amp INSTALLATION The panel is secured to the Firewall and for norm
25. and topcoat Certain brands of filler are significantly lighter that others checking densities and using lighter materials can save around 5kg on a typical Jabiru airframe 14 2 2 MATERIALS RECOMMENDED 14221 PAINTS FILLERS e Top Coat 5 Lts MUST BE WHITE e Base Coat 4115 Ensure compatibility with top coat e Polyester Filler 4kg e Spot Putty 1 Ib tube Claw Glaze recommended 14 2 2 2 SANDPAPER Note aluminum oxide type most effective 1st all over sand 150 grit 20 3M Brand e Bog Sand 120 grit 20 3M Brand e Spot Putty Sand 180 grit 20 3M Brand e Final Sand 320 grit 20 3M Brand 14 2 3 PAINTING EQUIPMENT REQUIRED e Random Orbital Sander approximately A 70 00 e Gas Mask e Compressor REVISION Dated July 2005 Issued By RAS Page 141 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants e Spray Gun 14 2 4 PAINTING PROCEDURE T Wash all parts to remove release agent Note Prepare all parts separately and paint separately 2 Completely sand all outside surface area with 150 grit to give paint adhesion The factory uses a Random Orbital Sander and 150mm Stickit discs Note Ensure that glass is not cut into in the sanding process 3 Grind excess resin from joints being careful not to grind into fib
26. as cracked hardened or shows signs of deterioration 12 3 5 REMOVAL amp INSTALLATION OF COMPONENTS To remove pitot mast remove the two rivets fastening it to the wing strut and pull it out from the strut far enough to disconnect the pitot line The static mast is fixed and cannot be removed To gain access to disconnect the static tube from the static mast remove the VHF antenna cover at the tope of the fin Pitot and static tubing is removed in the usual manner Installation of tubing will be simplified if a guide wire is drawn in as the tubing is removed When replacing tubing and fittings tighten connections firmly but avoid overtightening and distortion of fittings or tubing 12 3 6 TROUBLE SHOOTING PITOT STATIC SYSTEM Table 9 Trouble Shooting Pitot Static System Trouble Probable Cause Remedy Low or sluggish Test pitot tube and line for airspeed indication Pitot tube obstructed leak or leaks or obstructions Blow normal airspeed and obstruction in pitot line out tube and line repair or vertical speed replace damaged line Incorrect or sluggish Tm Test ina for leaks and Leaks or obstruction in static obstructions Repair or line replace line blow out instruments obstructed line revision Dated July 2005 Issued By RAS Page 127 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005
27. craft must not be flown with the Spinner removed 19 5 10 TO REMOVE EXISTING PROPELLER Remove Machine Screws and Tinnerman Washers from Spinner Remove Spinner Unbolt Propeller Bolts 6 off Remove Bolts Spinner Flange Aluminium Propeller Flange Belleville Washers and Propeller TO ASSEMBLE AND REPLACE PROPELLER ASSEMBLY Ensure that Propeller drive bushes 6 off are in place in the Crankshaft Propeller Flange Fit the rear spinner backing plate to the flange Fit propeller to flange Ensure that the drive pins are snug fit in the propeller Loose pins can cause propeller fretting and engine damage Fit Propeller Bolts 6 off Fit front spinner backing plate to front of propeller The fit Aluminium Propeller Flange Belleville Washers 42 off 8 per Bolt assembled in pairs as shown Progressively tighten bolts ensuring equal distribution of load and in a normal criss cross torque sequence Using Torque Wrench tighten Bolts to 6nm 72 inch Ibs Check tracking of Propeller by locating a fixed object on a flat floor so that it just clears the Propeller tips when rotating the Propeller by hand Check that each blade clears the object by the same amount f the Propeller is outside the approved tolerance refer to JABIRU Aircraft Pty Ltd or a JABIRU Approved Service Centre Maximum Tracking Error Tolerance is 2mm Locate Spinner on Spinner Flange and fix with Machine Screws through tinnerman Washers
28. der Cable PC01714 2 2500 Elevator Cable 1814 1 2500 Aileron Cable 2 PC01614 2 2500 20 3 STRUCTURAL INSPECTION INTERVALS A visual inspection should be conducted each 100 hours in accordance with the Inspection Schedules detailed at Paragraph 2 3 of the Service Manual e This inspection should identify the commencement of any structural deterioration which will be evidenced by cracking of the paintwork whiting of unpainted areas movement of wing attachments and threaded bushes movement of undercarriage attachments loosening of firewall engine attachments e Wing struts should be inspected for loose rivets excessive clearance in wing strut attachments or corrosion e Cable clamps should be inspected for evidence of movement and security 20 4 INSPECTION PROCEDURES All inspection is by visual means Refer Paragraph 3 above and Paragraph 3 3 of the Service Manual REVISION lo Dated June 2005 Issued By RAS Page 156 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM
29. erglass layers Take care not to grind into the horn of any control surfaces 4 A clean wire brush is used to search out any crab holes or pinholes Give the entire aircraft a good scrub all over especially around corners etc 5 Wear a breathing respirator with painting cartridges right from initial sanding through to painting Hint Body Filler sets quickly in high temperatures particularly when larger mixes are necessary Use cold packs under the Body Filler board to extend setting time 6 Follow instructions carefully and experiment with setting times T On large radius e g sides of fuselage an extra large homemade spatula 9 thin tin plate is very handy when applying Body Filler 8 When filling up to window edges grind chamfer onto edge of window to give depth for bog adhesion WARNING THE GEL COAT IS MICRO THIN SO SANDING 15 ALWAYS A CAREFUL PROCEDURE IF GEL COAT IS INADVERTENTLY PENETRATED DO NOT CONTINUE SANDING INTO STRUCTURAL GLASS 9 With the surface satisfactorily prepared white primer is required only on the discolored areas i e Body Filled areas Pin holes become evident after the primer is applied so use spot putty to fill Be careful and meticulous to find all pin holes because primer and top coat will not fill holes 10 Your final product can only be as good as your preparation Remember paint does NOT cover a multitude of sins 11 The factory uses a low pressure pot gun for spraying at pres
30. have a limited effect on the length of time of radio transmissions and no effect on aircraft performance as the engine electrical system is totally isolated from the power supply and is self sustaining The battery is only used to crank the engine for starting 13 9 RADIO WIRING DIAGRAM OPTION The optional aircraft radio system diagram is provided with the radio manuals 13 9 1 VHF ANTENNA INSTALLATION The VHF antenna used consists of two aluminium bars permanently bonded in place inside the spar channel of the vertical fin Figure 49 shows the position details of the two bars REVISION lo Dated July 2005 Issued By RAS Page 139 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM ircraft pty A Aircraft Service Manual Jabiru J160 170 Variants d0 13985 OoH38vNna NOLVZINVIOd 143A 1 WOO 4H F IH es Visas m ds mm Me viia 031419395 SSIINN S O ava ssi LL 28901 2102 NOIVNIWH3I 318VO dWIMO 03M 318vo Xvoo n 296 9M S e HOYI 310H eile si ER piza i 510909 We X 499 SL
31. ificial Horizon and Directional Gyro together with an electric Turn Coordinator is available as an option Where this option is provided a different instrument panel facia is fitted Repair should only be performed by an approved instrument workshop revision Dated July 2005 Issued By RAS Page 135 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 13 SECTION 14 ELECTRICAL SYSTEMS 13 1 ELECTRICAL POWER SUPPLY SYSTEM Electrical energy for the aircraft is supplied by a 14 volt direct current single wire negative ground electrical system A 12 volt battery supplies power for starting and furnishes a reserve source of power in the event of electrical power system failure An engine driven Alternator is the normal source of power during flight and maintains a battery charge controlled by a voltage regulator The following paragraphs provide brief descriptions of the elements of the electrical system They should be read in conjunction with the Wiring Diagram at Figure 51 13 2 WIRING DIAGRAM The Wiring Diagram is shown at Figure 51 REVISION lo Dated July 2005 Issued By RAS Page 136 of 156 L MilesYTechnical manuals160 J1701J160 amp J170 working files J160_ amp _J170_Tech doc Print Date
32. indicator and check reading Replace instrument Pointer off zero Reset pointer to zero Pointer oscillates Partially plugged static line Check line for obstructions Blow out lines Leak in static line Test lines and connections for leaks Repair or replace damaged lines tighten connections Leak instrument case Substitute known good indicator and check reading Replace instrument Hand vibrates Excessive vibration Check shock mounts Replace defective shock mounts Defective diaphragm Substitute known good indicator and check for vibration Replace instrument 12 3 10 Refer to Figure 48 PITOT TUBE ALIGNMENT For correct airspeed indication pitot tube must be properly aligned Open end of tube must be perpendicular to longitudinal axis of the aircraft Refer to Figure 48 for alignment details REVISION Dated July 2005 Issued By RAS Page 129 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft pty pta me Cr E Aircraft Service Manual Jabiru J160 J170 Variants 230 Hh _ 4 9 o0449N UBE BENT PIIOI 8 CLAMP MS8242 2 IOSE COUPLING 6 TUBE 1 4 ID RIVET 2 3 MOUNT PLATE PITOT TUBE 2
33. ion hose f 4 After amount c indicator TO APPLY PRESSURE nawing 9017093 1 STATIC 5 QUIPMENT 9017095 ATIC TES EQUIPMEN Figure 47 Static System Test 12 4 TACHOMETER The tachometer is electronic and driven from a magnetic pick up Should the tachometer fail to operate f Check 10amp instrument fuse and replace if necessary 2 Check 30amp main fuse and replace if necessary Revision Dated July 2005 Issued By RAS Page 132 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants Remove Instrument Panel see Paragraph 13 2 3 and check cable terminals for security Check wiring see Wiring Diagram Figure 51 Check correct installation of magnetic sensor on engine Refer to engine Instruction amp Maintenance Manual Should the instrument give incorrect readings jJ 2 Check 10amp instrument fuse and replace if necessary Check 30amp main fuse and replace if necessary Check correct installation of magnetic sensor on engine Refer to engine Instruction amp Maintenance Manual Refer to an Authorised Service Centre to have Alternator and Regulator checked Refer instrument to VDO Service Centre or JABIRU AIRCRAFT Pty Ltd for inspection and possible repair 12
34. me Aircraft Service Manual Jabiru J160 J170 Variants 17 APPENDIX II JABIRU ENGINE PARTS BOOK Please insert your copy of the INSTRUCTION AND MAINTENANCE MANUAL that comes with your engine into this section THIS PAGE IS INTENTIALLY LEFT BLANK REVISION lo Dated July 2005 Issued By RAS Page 148 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 18 APPENDIX 111 ENGINE INSTALLATION MANUAL Please insert your copy of the INSTALLATION MANUAL that comes with your engine into this section THIS PAGE IS INTENTIALLY LEFT BLANK REVISION lo Dated July 2005 Issued By RAS Page 149 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM 19 APPENDIX IV PROPELLER SERVICE MANUAL 19 1 APPROVED INSTALLATIONS The following combinations are approved Table 16 Approved Propeller Installations Airframe Engine Propeller Dia x Pitch Remarks Limits Jabiru J160 Jabiru 2200 C000 1924 x 1117 Mot above 3300 RPM 60 x 44 Jabiru J160 C Jabiru2200 000 2 los Not above 3300 RPM Jabiru J170 Jabiru2200 1924 x 1117 Not above 3300 RPM 60 x 44 Jabiru J1
35. nd cover pressure connections on instrument to prevent thread damage and entrance of foreign matter Wire terminals should be insulated or tied up so that accidental ground or short circuiting will not occur 12 2 4 INSTALLATION Generally the installation procedure is the reverse of the removal procedure Ensure mounting screws and nuts are tightened firmly but do not over tighten particularly on instruments having plastic cases The same rule applies to connecting plumbing and wiring 12 3 amp STATIC SYSTEMS Refer to Figures 48 and 49 The pitot system conveys ram air pressure to the airspeed indicator The static system vents vertical speed indicator if fitted altimeter and airspeed indicator to atmospheric pressure through plastic tubing connected to a static port 12 3 1 PITOT STATIC SYSTEM MAINTENANCE Proper maintenance of pitot and static system is essential for proper operation of the altimeter airspeed indicator and vertical speed indicator if fitted Leaks moisture and obstructions in the pitot system will result in false airspeed indications while static system malfunctions will affect readings of all three instruments Cleanliness and security are the principal rules for system maintenance The pitot tube and static ports MUST be kept clean and unobstructed 12 3 2 STATIC PRESSURE SYSTEM INSPECTION amp LEAKAGE TEST The following procedure outlines inspection and testing of the static pressure system
36. ocedure Ti Disconnect static pressure lines from airspeed indicator and vertical speed indicator 2 Use suitable fittings to connect lines together so that the altimeter is the only instrument still connected into the static pressure system 3 Repeat leakage test to check whether static pressure system or the bypassed instruments are the cause of the leakage If instruments are at fault they must repaired by an appropriately authorised repair station or replaced If static pressure system is at fault use the following procedure to locate the leakage 4 Attach a source of positive pressure to the static source opening Figure 50 shows one method of obtaining positive pressure CAUTION Do not apply positive pressure with airspeed indicator or vertical speed indicator connected to the static pressure system 5 Slowly apply positive pressure until altimeter indicates 500 foot decrease in altitude and maintain this altimeter indication while checking for leaks Coat line connectors and static course flange with solution of mild soap and water watching for bubbles to locate leaks 6 Tighten leaking connections Repair or replace parts found to be defective 7 Reconnect airspeed and vertical speed indicators into static pressure systems and repeat leakage test steps 3 through 6 12 3 3 PITOT SYSTEM INSPECTION amp LEAKAGE TEST To check pitot system for leaks place a piece of rubber or plastic tubing over pitot tube
37. ry terminals and the entire surface of the battery with a clean cloth moistened with a solution of bicarbonate of soda baking soda and water 3 Rinse with clear water wipe off excess water and allow battery to dry 4 Brighten up cable ends and battery terminals with emery cloth or a wire brush 5 Install the battery in accordance with the preceding paragraphs 6 Coat the battery terminals with petroleum jelly or an ignition spray product to reduce corrosion 13 4 5 BATTERY BOX The battery box is located on the firewall in the engine compartment 13 5 STARTER SOLENOID The starter solenoid is a sealed unit Service is limited to inspection of terminals for security and replacement of the unit 13 6 VOLTAGE REGULATOR The voltage regulator is a sealed unit Service is limited to inspection of terminals for security and replacement of the unit 13 7 STROBE SYSTEM OPTION A white strobe light may be installed in the rear lower fuselage or in the cabin roof The power source for the strobe light is located behind the fuel tank WARNING The strobe system is a high voltage device Do Not remove or touch tube assembly while in operation Wait at least 5 minutes after turning off power before commencing any activity near the strobe light 13 8 ELECTRICAL LOAD ANALYSIS As this aircraft is only certified for VFR Daylight only operations an Electrical Load Analysis is not required as failure of the electrical generation system would
38. sures from 60 100 psi 12 Itis mandatory that exterior color is WHITE only broken if desired by pin strips on the vertical surfaces i e Sides of fuselage but not horizontal surfaces i e top of wings or fuselage as the heat build up under the tape in hot sun is considerable REVISION lo Dated July 2005 Issued By RAS Page 142 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 13 14 15 16 After filling all pinholes spray another coat of primer on the discolored areas An all over primer coat is not required over the gel coat as gel coat is a sufficient undercoat The final rub is with 320 grit all over and if satisfied with the surface preparation remember paint will simply change color not hide lumps bumps scratches and holes blow off the dust and give an all over wipe with a tack cloth to pick up the final dust particles Wash down the floor of the spray area to settle dust and proceed to spray as per your selected technique You are now ready to spray final coat GOOD LUCK WARNING The Jabiru aircraft is only approved to be painted in basic White colour so as to minimise the effects of heat and ultra violet light to the aircraft structure In addition colour including stripes etc must not
39. ximately 20 ampere hour capacity The battery is mounted in the engine compartment and is vented overboard 13 4 2 BATTERY TROUBLE SHOOTING Trouble Shooting is limited to inspection of wiring and terminals battery charge condition and battery solenoid 13 4 3 REMOVAL AND INSTALLATION T Disconnect the battery security strap 2 Disconnect battery drain 3 Disconnect the ground cable from the negative battery terminal black insulation WARNING When installing or removing battery always observe the proper polarity with the aircraft electrical system negative to ground Reversing the polarity even momentarily may result in failure of semi conductor devices alternator diodes radio protection diodes and radio transistors 4 Disconnect the cable from the positive battery terminal 5 Lift the battery out of the battery box 6 To replace the battery reverse this procedure 13 4 4 CLEANING THE BATTERY For maximum efficiency the battery and connections should be kept clean at all times T Remove the battery and connections in accordance with the preceding paragraph REVISION lo Dated July 2005 Issued By RAS Page 138 of 156 L Miles Technical_manuals J160_J170 J160_ amp _J170_working_ files J160_ amp _J170_Tech doc Print Date 15 08 2005 10 25 00 AM Jabiru Aircraft me Aircraft Service Manual Jabiru J160 J170 Variants 2 Wipe the battery cable ends batte
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