Airplane Flight Manual XA42
AFM-XA42-0040-002-A.01
Page 3
Page date :
Chapter 04
24.01.2011
CAUTION
Tyre wear
CHECK
G) Right rear fuselage
Fuselage skin for damage
CHECK
Static port clean?
CHECK
H) Right wing trailing edge
Spade and spade arm
CHECK
Aileron linkage
CHECK
Wing trailing edge and skin for damage
CHECK
Aileron trailing- leading edge and skin for damage
CHECK
Aileron hinges
CHECK
Freedom of movement and play
CHECK
I) Right wing leading edge
Wing leading edge and skin for damage
CHECK
Fuel cap and fuel capacity
CHECK
Right wing tank
DRAIN WATER
J) Right main gear
Main gear strut to damage
CHECK
Tyre to pressure and wear
CHECK
Tire and wheel slip mark
CHECK
K) Right front fuselage
Fuselage skin for damage
CHECK
L) Engine
Oil quantity
CHECK
All items of this check below this line must be performed every 20 Flights!
Cowling
OPEN
Engine core to cracks
CHECK
Baffling to cracks
CHECK
Engine mount to cracks
CHECK
Exhaust system to cracks
CHECK
Exhaust system fixtures
CHECK
Cables and hoses to chafing
CHECK
Summary of Contents for XA42
Page 2: ......
Page 4: ......
Page 6: ......
Page 12: ......
Page 14: ......
Page 16: ......
Page 18: ......
Page 22: ......
Page 24: ......
Page 26: ......
Page 28: ......
Page 34: ......
Page 36: ......
Page 40: ......
Page 44: ......
Page 46: ......
Page 48: ......
Page 50: ......
Page 56: ......
Page 62: ......
Page 64: ......
Page 66: ......
Page 68: ......
Page 70: ......
Page 72: ......
Page 74: ......
Page 76: ......
Page 78: ......
Page 80: ......
Page 84: ......
Page 86: ......
Page 88: ......
Page 92: ......
Page 94: ......
Page 98: ......
Page 100: ......
Page 102: ......
Page 106: ......
Page 112: ......
Page 114: ......
Page 116: ......
Page 118: ......
Page 120: ......
Page 122: ......
Page 124: ......