Jabiru Aircraft Pty. Ltd. Final Inspection Checklist J200/400. Firewall forward components

Transcription

1 Jabiru Aircraft Pty. Ltd. Final Inspection Checklist J200/400 Registration No: Aircraft Checklist Pre Ground Test Model: Aircraft Serial No: Firewall forward components Propeller: Prop Size: 60 x 53 Other: Propeller Serial No: Prop Bolts: 1. Check Torque (6 ft/lbs) 2. Check Tracking 3. Torque seal nuts 4. Visual check prop for serviceability Spinner: 1. Spinner screws secure 2. Check Spinner/spinner backing plate has been indexed correctly & marked on spinner & spinner flange. 3. Check spinner tracking with engine running Engine: Engine Serial No: Engine Mount bolts secure: 1. Firewall 2. Engine 3. Thrust washer in place & correct Fuel hose secure: 1. Carburettor to pump 2. pump to bulkhead 3. clamped and tied 4. breather hose a. carburettor to hot air mixer box b. fuel pump to firewall \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 1 of 11

2 Spark Plugs/Coil leads: 1. Check plugs are secure 2. terminal nuts secure 3. CHT sender (12mm terminal) 4. leads secure on plugs 5. leads secure on distributor cap gauge earth wire secure and clipped into coil Ram Air Ducts: 1. Baffles in place 2. Bolts secure x 4 3. springs in place 4. spring lock-wire correct and secure x 2 5. Check Alignment of rubber with top cowl 6. Air Ducts not touching top cowl 7. Cooling tubes directed onto coils Oil: 1. Level correct (4 cylinder 2.4) (6 cylinder 3.4) 2. sump plug wired 3. cooler bracket secure to engine 4. cooler secured to bracket 5. air dam in place 6. check hose route 7. cooler hose clamps secure x 4 8. fire sleeve secure 9. filter secure 10. oil breather hose & bottle secure Throttle cable: 1. cable lock nuts secure on both ends 2. cable end free in carburettor link 3. split pins secure 4. 2 x 5/16 washers between cable and carburettor link 5. cable alignment correct with outer at both ends 6. cable adjustment a) full throttle b) idle Choke Cable: 1. Lock nuts secure both ends 2. cable end free in carburettor link 3. split pin secure 4. cable alignment correct with outer 5. operational Carburettor Heat Cable: 1. Lock nuts secure both ends 2. cable end free in carburettor link 3. split pin secure \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 2 of 11

3 4. cable alignment correct with outer 5. operational Scat Hose: 1. carburettor to hot box a) hose clamps secure b) not bunched up under carburettor c) smooth route 2. hot box to NACA duct a) hose clamps secure b) smooth route 3. hot box to heat muff a) hose clamps secure b) smooth route Nose leg & housing: 1. Tyre pressure checked 20 psi 2. wheel - ease of rotation 3. leg lubricated and ease of rotation 4. assembly all bolts secure in nose leg 5. Housing bolts secure a) ¼ washers on head of bolt 6. rod end secure both sides 7. safety hole within limits 8. Jam nuts secure 9. air valve grommet in place 10. spats screws secure 11. Spring does not become coil bound full deflection Electrical: 1. battery tie down secure 2. battery terminals secure 3. battery earth secure on firewall 4. starter solenoid locknuts & wires secure 5. regulator wires secure & correct 6. temp sender wires secure x 3 (oil & CHT) 7. all wiring cable tied and secure 8. oil pressure wire correct & secure (G terminal) Cowls: 1. Top & Bottom Cowl Alignment (no gaps) 2. Retained Nuts secure & correct 3. Oil Door operational 4. Pin Bent in Oil Door hinge 5. Spinner not touching front of cowl & Propeller 6. Oil Cooler not touching bottom cowling 7. Cylinder Heads not touching Top & Bottom Cowling 8. NACA duct secure with no sharp edges 9. Cam Locks Secure & operational \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 3 of 11

4 Interior Fuel system: 1. filters secure & flow direction correct 2. fuel line secure a) bulk head to fuel pump b) fuel pump to selector valve c) fuel selector valve to gascolator left & right d) gascolator left & right to fuel gauge e) gascolator left & right to rear fuel pickup in wing root f) Fuel Gauge forward fuel line in wing root 3. check hose route (a) (f) 4. check valve operation left & right Check left wing fuel line is attached to left hand side fuel tap. Check right wing fuel line is attached to right hand side fuel tap 5. check valve cover and mount secure to console 6. check finger filters secure Fuel Breather: a. Check breather hose clamps and breather route b. Wing Breather tube to wing root secure c. Wing root breather tube to sharks fin Left & Right hand side secure d. Sharks fin to overflow secure e. Sharks fin secure on fuselage f. Check gauze is not blocked g. Check 1/8 holes have been drilled & clear h. Check Fuel breather tube is secure to body fuel filler i. Fuel Breather check has been conducted: Please note: you must be able to hear air in all three outlets independently by a) Removing filler cap in left wing & blow into sharks fin bocking 1/8 holes b) Removing filler cap in right wing & blow into sharks fin bocking1/8 holes c) With both filler caps in body fuel filler listen to breather outlet under fuselage Fuel Gauge Left & Right: 1. Secured to fuselage 2. Check for leaks 3. Add one litre of fuel to each tank & mark fuel level ensure fuselage is level. 4. Fuel decal in place left & right Fuel Flow Test: 1. Add 20lts of fuel to left & right hand tank 2. check Fuel taps have been indexed i.e. on is on off is off 3. Select left tank only & measure fuel flow a) Fuel pump off lts per minute b) fuel pump on lts per minute 4. Select Right tank only & measure fuel flow a) Fuel pump off lts per minute \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 4 of 11

5 b) fuel pump on lts per minute Controls Rudder: 2. pedal mount bolts secure x 2 3. Rudder peddle keepers secure & correct a) 2 x ¼ bolt secure b) 2 x 5/16 bolts secure c) check jam nuts on push rods secure x 2 d) check safety within limits on push rods x 2 f) check rod end free play at full deflection, both directions 3. Rudder cable a) anchor secure and correct position in clamp b) rod end secure in pedal with ¼ washer c) safety within limits d) jam nuts secured e) rod end free play at full deflections, in both directions f) rudder stoppers adjusted and secure (check 98mm travel left & right) Trim: Brake: 1. handle secure 2. lever pivot secure and split pin 3. friction correct & secure 4. rod end secure 5. check safety hole within limits 6. jam nuts secure 7. cable position in clamp correct & anchor secure 8. operation 9. spring not coil bound with elevator fully deflected up 10. decal fitted and correct 1. handle assembly correct and secure 2. lever pivot secure and split pin (no fee play side to side) 3. rod end secure 4. Pushrod not binding in centre console 5. check safety hole within limits 6. jam nuts secure 7. operation 8. free play 9. fluid level full 10. stainless striker in place 11. handbrake correct and operational \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 5 of 11

6 Throttle: 1. cable anchor secure 2. cable alignment correct 3. cable end free in output lever 4. output lever secure 5. input lever x 2 secure 6. bearing blocks x 2 secure 7. throttle stop correct and secure Horizontal shaft: 1. control stick pivot secure 2. yolk secure (no free play) 3. rod end secure 4. safety hole within limits 5. jam nuts secure 6. elevator cable anchor secure and correct position in clamp 7. cable clear of centre console in all positions (Elevator UP & Aileron to Right Hand Side) 8. rod end free at full deflections 9. bell crank plate secure Aileron Cable: 1. cable anchor - wedges i. left ii. right - R clip i. left ii. right - rivets x 3 TLR i. left ii. right 2. rod ends secure x 2 3. safety within limits x 2 4. jam nuts secure x 2 5. aileron stoppers secure (cannot over centre aileron bellcrank) Seat Belts: 1. check bolts are through nyloc and buckle has free play i. Left ii. Right 2. Operation 3. belts not twisted 4. seat belt anchor secure (lower and upper) 5. Door Frame Compression struts fibreglasses in place with no sharp edges. Headsets: hook secure \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 6 of 11

7 Instrument Panel: 1. secure & level 2. instruments square (Check turn coordinator / slip skid ball is centred). 3. balance ball air bubble not visible 4. switches secure 5. choke cable decal square 6. registration number p-touch on panel 7. Switch decals in place & correct 8. mag guard in place and square with rounded edges 9. all instruments fitted as per order 10. instrument markings correct 11. altimeter QNH correct 12. all instruments operational 13. cigarette lighter installed 14. all avionics as per order and operational Flap handle: Upholstery: Decals: 1. pivot bolt secure & torqued 2. pivot bolt split pin 3. locater bolt secure 4. ease of location in all three positions 5. rod end bolt secure handle - input shaft 6. push rod not binding in all three position 7. safety hole within limits x 2 8. jam nuts secure x 2 9. visual on input lever 10. visual on bearing blocks Check nuts are in safety 1. fitted & clean 2. correct as per order 3. seat covers 4. map pockets 1. warning 2. baggage 3. loading Stall warning: 1. operation correct (suck to ensure reed is correct) 2. gauze and stainless plate installed correctly and clear Doors: LEFT RIGHT 1. operation 2. restraining straps secure and correct length 3. hinge and pin secure 4. catches secure and freely operating 5. visual on door jam \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 7 of 11

8 LEFT RIGHT 6. visual on door seal 7. visual on rope handle 8. visual on top catch 9. decals Do not lean on door Exit Open Owners Manual EXTERIOR Wings: LEFT RIGHT 1. route bolts inspected ( correct tension) x 2 2. strut bolts x 2 inspected, correct tension 3. warning decals x 2 (Do not Tighten) 4. speed fairing secure and clear of strut 5. flap/deflections a) first stage b) second stage c) neutral 6. flaps a) hinge points secure with pivot bolts in safety b) push rod ends secure and not binding in 3 positions c) safety hole within limits d) jam nuts secure e) push rod not fowling on cover strip f) drive shaft output secure g) drain holes have been drilled h) wing route cover strips secure i) top wing strut fairings secure 7. Aileron Deflections a) neutral (level with lower wing skin) b) up deg c) down deg 8. Ailerons a) Hinge pin and retainer secure b) Rod ends secure c) Safety hole within limits d) Jam nuts secure e) Cable anchor secure and correct position in clamp f) Drain holes 9. wing drain hole in trailing edge 10. inspection window secure \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 8 of 11

9 RIGHT 11. Pitot a) secure b) operation c) cover Main Undercarriage: LEFT RIGHT 1. tyre pressure 25 psi 2. ease of rotation 3. calliper secure 4. stub axle secure 5. hubs secure 6. discs secure 7. stub axle extension is secure 8. legs secure x 2 9. spat a) screws secure b) clear of tyre a) retain nuts b) outer edge c) air valve grommet in place d) no step decal in place Fuel cap: 1. filler cap secure 2. Earth wire secure 3. Quick drain a) operation b) lock wired 4. decals in place & correct Elevator Deflections 1. up deg 2. down deg 3. 2mm clearance to stops on fuse Elevator: 1. hinge pins and retainers secure 2. rod ends secure 3. safety within limits 4. jam nuts secure 5. cable anchor secure and correct position in clamp 6. drive plate secure 7. rod end free play at full deflections 8. end-plug not touching end-cap full deflection down \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 9 of 11

10 Trim: Trim Cable: Ventral Fin: Rudder: Static Vent: a) pivots secure b) spring rod a) split pins secure b) springs lubricated c) black block secure and free d) rod ends secure e) safety hole within limit f) jam nuts secure g) rod end free at full deflections a) cable anchor secure and correct position in clamp b) rod ends secure c) safety within limits d) jam nuts secure e) rod end free at full deflections. a) Retained nuts in fuselage secure b) Elevator horn not hitting Cut-out in Ventral (full up deflection.) c) Inspection holes drilled d) Drain holes drill e) Ventral fin secure onto fuselage 1. Deflection a) left mm b) right mm c) 2mm clearance to stops on fuse 2. hinge pin and retainers secure 3. 5mm off set to right 4. rod end secure 5. safety within limits 6. jam nuts secure 7. cable anchor secure and correct position in clamp 8. rod end free at full deflections 1. tip secure 2. holes clear 3. decal in place 4. Suction Test with no leaks (Block second hole in static vent & suck until ASI reads 100kts, hold until stabilised.) \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 10 of 11

11 AIRCRAFT REGISTRATION: S/N# DATE: DEFECT: CORRECTED BY: \\Gateway\library\files\forms\Pre & Flight Testing\Final Inspection Cecklist J doc 13 June 2003 Page 11 of 11