3. PRE-FLIGHT INSPECTIONS
Before each flight, it is necessary to carry out a complete aircraft check compris-
ing an external inspection followed by a cockpit inspection as below detailed.
3.1.
CABIN INSPECTION
A
Weight and balance: calculate (ref. this AFM sect. 6) check within limits
B
Safety belts: connected to hard points, check condition
C
Magnetos: OFF, keys extracted
D
Master switch: ON
E
Voltmeter: check (10-12 V); Ammeter check (red).
F
Lights (if installed): all ON, check operation
G
Acoustic stall warning: check operation
H
Master switch: OFF
I
Baggage: check ELT, luggage stowage and fastened with restraint net.
3.2.
AIRCRAFT WALK-AROUND
To perform the aircraft walk-around, carry out the checklist according to the sta-
tion shown in Figure 4-1.
Visual inspection is defined as follows: check for defects, cracks,
detachments, excessive play, unsafe or improper installation as
well as for general condition. For control surfaces, visual inspec-
tion also involves additional check for freedom of movement and
security. Red lubber lines on bolts and nuts shall be intact.
Fuel level indicated by the avionics system indication should be
verified by visual check of actual fuel quantity embarked in the
tanks.
Fuel drainage operation must be carried out with the aircraft
parked on a level surface. Set Cockpit Fuel Selector Valve to open
prior to drain fuel circuit nose section valve.
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