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MAINTENANCE MANUAL

SAVANNAH VG AND

SAVANNAH XL

Doc. No.:

MM-SVNH-VG&XL-EN

Revision:

Rev. Date:

28/12/2022

Proj. Ref.:

Savannah Model 51

A/C: Savannah VG&XL

Applies to Generic Serial Number: yy-mm-51-xxx

Page: 9/24

OC FMM00

Horizontal tail

 Stabiliser: Integrity of the rear connection, integrity of the holding brackets of the

hinges;

 Elevator: integrity of the trailing edge, and of the holding brackets of the hinges;

 Elevator hinges: presence of split pins and absence of play;

 Elevator control: verify for the integrity between the connection of the control rod and

the elevator operation lever.

Vertical tail

 Fin: Integrity of the rear connection, integrity of the holding brackets of the hinges;

 Rudder: integrity of the trailing edge and of the holding brackets of the hinges;

 Rudder hinges: presence of split pins and absence of play;

 Rudder control: verify for the integrity between the connection between the cables and

the bracket.

Rh half wing

 Wing – fuselage front connection: check the integrity of the connection;

 Wing – fuselage rear connection: check the integrity of the connection;

 Strut – fuselage connection: check the integrity of the connection;

 Connection of the strut to the wing: check the integrity of the connection;

 Wing: check the integrity of leading edge, nose, the absence of rivets or cracks near

holes, and the presence of the vortex generators;

 Flaperon hinges: check for the presence of split pins, integrity of the hinge and

absence of play;

 Flaperon: Check for the integrity of the flaperon nose, for no cracks to be present in

correspondence with the riveting and of the through slots of the holding plates; check

for the trailing edge not to be damaged;

 Flaperon control: verify for the integrity of the connection between the control rod and

control lever;

 Flaperon control: verify for the connection between the control rod and the fixing

brackets to the spar to be sound.

 Cap: verify for the tank cap to be tight;

 Verify that the retun line pipe of fuel is not obstructed.

Rh main undercarriage

 Tyres: wear and related inflation pressure;

 Wheel fairing (if installed): for it to be fixed to its connections;

Brand	ICP
Model	SAVANNAH XL
Category	Aircrafts
Language	English

ICP SAVANNAH XL User Manual

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ICP SAVANNAH XL Specifications

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