Tecnam P2002 JF - Page 146

Page 3 2
nd
Edition – Rev 0
O6-10
INSPECTION CAPS
INSPECTION CAPS AND REMOVABLE PARTS
No
ACCESS TO
Q.TY
W1
Aileron differential bellcranck
2 – LH and RH
W2
Wing tank outlet, main spar and torque box
2 – LH and RH
W17
Flap control rod and wing rear fitting point
2 – LH and RH
W18
Main spar fittings and fuel tank outlet
2 – LH and RH
W19
Main spar fittings
2 – LH and RH
W20
Main spar fitting
2 – LH and RH
F3
Gascolator
1
F4
Fuel return tank
1
F5
Fuel selector valve
1
F6
MLG spring leaves fitting bolts
2 – LH and RH
F7
Stabilator push-pull rod; vertical tail; attachment,
structure and rudder control cable
2
F8
Instrument panel
2 – LH and RH
F9
Battery and its connections
1
F10
Stabilator torque tube, its attachments and control rod;
vertical tail rear spar; rudder bellcrank, trim actuator and
its connecting rods
1
F22
Tail cone structure
1
C11
Parking brake valve (lever brake configuration); rudder
control cables
1
C12
Instrument panel and radio equipment
1
C15
Tail cone structure; tail cone to cabin fitting points;
intermediate bellcranck of the stabilator control system;
rudder control cables and pulleys; flap electric actuator
1
C16
Turnbuckles and cables of the aileron’s circuit and stick
leverages; brake pump; wing carrythrough.
E13
Engine and its systems; nose landing gear and steering
system
1
E14
Propeller hub and fitting bolts
1
E21
Engine
2- LH and RH