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CAUTION
In low ambient temperatures the airplane must be completely cleared of ice, snow and similar accumulations. For approved de-icing fluids refer to Section 8.7 - GROUND DE-ICING.
CAUTION
Prior to flight, remove such items as control surfaces gust lock, Pitot cover, tow bar, etc.
CONTINUED
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 4A - 11
1. Left main landing gear:
a) Landing gear strut and lock .............. visual inspection, sufficient height (typical visible length of bare piston: at least 4 cm/1.6")
b) Down and Uplock switches (3x) .......... visual inspection
c) Wear, tread depth of tire ................ visual inspection
d) Tire, wheel, brake ..................... visual inspection
e) Brake line connection .................. check for leaks
f) Slip marks ........................... visual inspection
g) Chocks ............................. remove
h) Landing gear door..................... visual inspection
2. Left engine nacelle:
a) 3 air inlets / 2 air outlets ................ clear b) Engine oil level ....................... check dipstick (inspection hole in the upper cowling) c) Gearbox oil level ...................... check visually (inspection hole in
the lower cowling)
d) Cowling ............................. visual inspection
e) Gascolator / air inlet ................... drain off to check for waterand
sediment (drain until no water
comes out) / clear
f) Venting pipe ......................... check for blockage
g) Exhaust ............................. visual inspection
WARNING
The exhaust can cause burns when hot.
CONTINUED
Page 4A - 12 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
h) Propeller ............................ visual inspection
WARNING
Never move the propeller by hand while the ENGINE MASTER switch is ON! Also do not move the propeller by hand while the ENGINE MASTER is OFF immediately after operation (remaining pressure in the injection system rail). Serious personal injury may result.
% i) De-Icing boots on propeller (if O.M 42-053
% or/and O.M 42-054 carried out) .......... check for de-bonding j) Nacelle underside..................... check for excessive contamination particularly by oil, fuel, and other fluids k) Auxiliary tank vent outlet on lower surface . . visual inspection l) Auxiliary tank drain .................... drain off to check for water and sediment (drain until no water comes out) / visual inspection m) Auxiliary tank filler ..................... visual inspection, tank filler closed
3. Left wing:
a) Entire wing surface .................... visual inspection
b) Tank air outlet on lower surface .......... visual inspection
c) Tank drain/tank air inlet ................ drain off to check for water and
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