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c) ELECTRIC MASTER ................... OFF, pull out key
d) ENGINE MASTER ..................... check OFF
e) ECU SWAP .......................... check AUTOMATIC
f) Emergency fuel valve................... locked, in NORMAL position
g) Front canopy & rear door................ clean, undamaged,
check locking mechanism function
h) All electrical equipment ................. OFF
i) Circuit breakers ....................... set in (if one has been pulled, check
reason)
j) Power lever .......................... check condition, freedom of movement
and full travel
k) Power lever .......................... IDLE
l) ELECTRIC MASTER ................... ON
m)Fuel quantity ......................... check, use alternate mean
% NOTE
% If the Long Range Tank is installed and the fuel quantity % indicator reads 15 US gal, the correct fuel quantity must be % determined with the fuel quantity measuring device. If this % measurement is not carried out, the fuel quantity available % for flight planning is 15 US gal.
n) Position lights, strobe lights (ACL) ......... check
o) ELECTRIC MASTER ................... OFF
p) Foreign objects ....................... check
q) Controls and trim ...................... free and correct
r) Baggage ............................ stowed and secured
Doc. No. 6.01.05-E Revision 2 30-Apr-2003 Page 4A - 3
II. Walk-around check, visual inspection
CAUTION
A visual inspection means: examination for damage, cracks, delamination, excessive play, load transmission, correct attachment and general condition. In addition control surfaces should be checked for freedom of movement.
CAUTION
In low ambient temperatures the airplane should be completely cleared of ice, snow and similar accumulations.
CAUTION
Prior to flight, remove such items as control surfaces gust lock, Pitot cover, tow bar, etc.
%
Doc. No. 6.01.05-E Revision 1 03-Mar-2003 Page 4A - 4
1. Left main landing gear:
a) Landing gear strut or fairing .............. visual inspection
b) Wheel fairing ......................... visual inspection
c) Tire inflation pressure (2.5 bar/36 psi) ...... check
d) Wear, tread depth of tire ................ check
e) Tire, wheel, brake ..................... visual inspection
f) Brake line connection .................. check for leaks
g) Slip marks ........................... visual inspection
h) Chocks.............................. remove
2. Left Wing:
a) Entire wing surface .................... visual inspection
b) Step ................................ visual inspection
c) Air intake on lower surface .............. visual inspection
d) Openings on lower surface ............... check for foreign objects and for traces
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