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:
65/132
DOC
FMM00
Structure /
System
N°
Inspection item
Action / Description
Elevator
07.10
Elevator hinge horns
Replace hinges angle (SA087-2)
07.11
Elevator control system horns
Replace the control system horns
(SE028, SE029)
Trim Tab
08.04
Trim control
Replace the push-pull rods and uniball
08.05
Trim actuator
Check the actuator lever without cracks
or local deformation when push-pull rod
has been disassembled. If any problem
observed, replace the actuator
Vertical Tail
(Fin)
09.08
Attachments
Check front spar with its attachment and
rivnuts. Check rear spar with attachment
holes within tolerance of 0.2 [mm] in
respect of the nominal bolt diameter
09.09
Rudder hinge
Replace all the rudder hinge horns
SG013 and SG010 (which is on fuselage
assembly)
Rudder
10.09
Hinge horns
Replace all the rudder hinge horns
(SA087-3, SA087-4)
10.10
Control system horn
Check the rudder control system horn
plate holes within tolerance of 0.2 [mm]
in respect of the nominal bolt diameter
(ST508)
Flight Control
System
11.17
Pulley
Replace the cables pulley, its safety
cotter pins and bolts/nuts
11.18
Cables
Replace the control cables and bulkhead
fairleads
11.19
Joints
Replace all the bushings and bearings of
control system joints. Replace all the
push-pull rod uniball including the ones
of steering
11.20
Torque tube
Replace the torque tube front aluminium
bushing and the rear plastic bushing
Main landing
gear
12.11
Spring bolts
Replace the spring fixing bolts and nuts
12.12
Bearings
Replace wheels bearings
12.13
Brake discs
Replace brake discs
12.14
Oil brakes
Bleeds and change oil brakes
Main landing
gear tail
dragger (if
configured
with)
12b.
02
Brace rods
Replace the brace rods, uniball and
connecting bolts/nuts
Table 23b