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Jabiru Aircraft
Pilot Operating Handbook
Model J170-D
JP-FM-13
Revision:
0
1
2
3
4
28 Feb 2020
Page 4-36
Aileron and elevator cables & fasteners....CHECK
Rudder and nose wheel steerage linkage .CHECK
Rudder centring springs ...........................CHECK
Controls (all) .............................................CHECK full travel, free movement.
Harnesses & Seats...................................CHECK CONDITION
Windshield ...............................................CLEANLINESS
Cockpit area .............................................GENERAL CONDITION
Loose objects ...........................................SECURE
Cockpit Doors/Latches .............................CONDITION & OPERATION
POH .........................................................AVAILABLE
Instruments
Heading indicator .....................................Check
Engine Instruments ..................................Confirm normal operation
Interior / Map / Instrument Lights
Lights .......................................................Check operation
4. Left Undercarriage
Mount bolts ..............................................CHECK SECURE*
Tyre ..........................................................CHECK CONDITION / INFLATION
* - Lock the hand brake on, then pull the aircraft forwards. Some flexing of the undercarriage legs
is normal, but there should be no movement of the top of the leg relative to the fuselage.
5. Static Source
Static Source ............................................CHECK FOR BLOCKAGE
6. Empennage
Tail tie-down .............................................DISCONNECT
Control surfaces .......................................CHECK Security & Full & Free Movement
Rudder, Elevator & Trim Cables ...............CHECK Security & Full & Free Movement
7. Right Wing
– Trailing Edge
Aileron ......................................................CHECK Security & Full & Free Movement
Flap ..........................................................CHECK Security
Control rods & cables ...............................CHECK Security. Check rod ends for
freedom of rotation & excess movement.
8. Right Wing
Wing Tie-Down .........................................DISCONNECT
Wing Strut Mount Bolts .............................CHECK Security**
Wing Root Mount Bolts .............................CHECK Security***
Pitot Tube .................................................REMOVE COVER, CHECK for blockage.
** - Wing strut bolts must not be tightened. Nut should just bear on washer.
*** - Holding the wingtip, push the tip up & down, forwards & backwards. If a wing / strut attachment
is degrading, slop will be felt.
9. Nose