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:
47/132
DOC
FMM00
Structure /
System
N°
Inspection item
Action / Description
Tail landing
gear
(if configured
with)
13b.
01
Spring
Verify integrity of spring, no crack, no
scratches, lower structural plate of
attachments with its bolt, properly closed.
Verify tail fuselage reinforcement and
bulkheads rivets all present. Verify spring
rubber pad (red vulcolan) in position
13b.
02
Tail wheel
Verify tail wheel attachment bolt closed
and rotating castle nut fixed with cotter
pin. Verify tail wheel steering horn free to
rotate with rudder and wheel. Verify tail
wheel disengage from directional control
system for excessive angle defection
13b.
03
Cables
Verify rudder to steering horn and
steering horn to tail wheel cables are in
tension and springs present
13b.
04
Alignment
Verify rudder aligned with tail wheel
13b.
05
Lubrication
Lubricate with white grease all the
rotating points
Engine
cowling
14.01
Integrity
Remove the upper and lower cowling
and verify all the parts of the cowling,
internal and external, upper part
14.02
Attachments
Verify cowling to fuselage attachments
and connections between the lower and
upper part. DZUS bolt and its spring
close in same
14.03
Match
Verify the upper and lower part match
correctly, DZUS bolts with plastic washer
and their spring are closing firmly.
At the end of maintenance, re-install the
engine cowling.
Verify intake Naca is almost aligned to
the airbox intake cold air opening and not
obstructed
Propeller
15.01
Prop. Maintenance Manual
Apply manufacturer approved
documentation for Maintenance and
Service Bulletin
15.02
Blades
Verify blades rigidity around rotation and
traction axis at the blade tip, all coherent
and rigid. Verify blades shape and
leading edge integrity, dents and cracks
absent
Table 19i
