MAINTENANCE MANUAL
SAVANNAH S
Doc. No.:
MM-SVNH-EN
Revision:
07
Rev. Date:
07/11/2022
Proj. Ref.:
SVNH S
A/C:
Savannah S
Applies to Generic Serial Number:
yy-mm-54-xxxx
Page:
45/132
DOC
FMM00
Structure /
System
N°
Inspection item
Action / Description
Flight Control
System
11.06
Rudder cables
Check cable tension is 11-15 [lbs] (5-7
[kg]) with dedicated instrument.
Verify cable integrity and terminal fitting
(nicopress, cable redance). Verify nonio
tender closed.
Verify pulleys round, safety pin installed
and plastic fairleads hole not ovalized.
Clean and lubricate passages and joint if
necessary
11.07
Brake pedals
Verify brake pumps are correctly
supported and connected to the pedals.
Verify no leakage from pipes and fittings;
on pumps cup small sign of oil is
acceptable
Main landing
gear
12.01
Support structure
Verify integrity of landing gear
attachments. Verify vertical bolt and nut
correctly closing the spring with red
rubber (vulcolan) and lower plate in
correct position and integrity
12.02
Spring
Verify landing gear spring no damages,
no unsymmetrical shape (within
tolerances)
12.03
Axle
Verify ring nut with teeth washer closed,
both on the spring and on the wheel side
12.04
Brakes
Verify brakes caliper free play along
wheel axis and blots closed. Verify no oil
leakage and brake pipes integrity. Verify
brake pads consumption (change if
required or friction material is less than 3
[mm])
12.05
Wheel
Verify visually that wheel rim is round
and disc fixed
12.06
Tyre
Verify tyre consumption (replace if
necessary). Verify pressure from 1.5 to
2.5 [bar], as required by the wheel type
12.07
Fairing
Verify wheel fairings rigidly supported
and not damaged
Table 19g