P92 Classic
Deluxe
NORMAL PROCEDURES
F
LIGHT MANUAL
1
st
edition – 23
th
March 2009 Doc. n° 92-13-030-00
4-4
H Horizontal tail and tab: check integrity and unhindered movement.
I Vertical tail and rudder: check integrity and unhindered movement.
L Check integrity of right side main landing gear, tire pressure (1.6 bar), condition and
alignment; check fuselage skin condition.
M Right flap and hinges: check integrity.
N Right aileron: check integrity and unhindered movement.
O Leading edge and wing skin: check integrity
P Check right side tank cap is fastened and blow-out plug is unobstructed.
Q Check right side static vent is unobstructed, do not blow inside vents (read note).
R Check integrity of nose landing gear strut, tire inflation (1.0 bar) and condition; check
condition of rubber shock absorbers.
S Propeller and spinner condition: check for nicks and fastening.
T Open engine cowling and perform the following checklist:
I.
Check no foreign objects are present.
II.
Check the cooling circuit for losses from tubing, check coolant reservoir lev-
el, insure radiator honeycomb cooling fins are unobstructed.
III.
Check lubrication circuit for losses from tubing, check oil reservoir level, in-
sure radiator honeycomb cooling fins are unobstructed
IV.
Open both fuel taps, inspect fuel circuit for losses from tubing, check integri-
ty of fireproof protection braids, drain circuit using a container to collect fuel
activating the specific drainage tap located on the firewall, shut fuel taps.
Check for absence of water or other contaminants.
Drainage operation must be carried out with aircraft parked on level
surface.
V.
Check integrity of silent-blocks.
VI.
Check firmness and integrity of air intake system, check externally that ram
air intake is unobstructed.
VII.
Check that all parts are secure or safetied.
U Close engine cowling.
V Check left side static port is unobstructed
WARNING !
