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FLIGHT DESIGN CT - 05-20.2.5 Propulsion System Inspection

FLIGHT DESIGN CT
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Document Title Document No. Revision
Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS
AF 0480 0011 00 05-Aug-12 05-20-3
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Check fuel valve off function
Notes:
05-20.2.4 Post Run-Up, Pre-inspection and Preparations
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Airframe, engine, propeller
Perform a walk around to detect damage, fluid
leaks or other abnormalities,
Check visual the installation geometry between
fuselage/ wing/ empennage and engine/ propeller/
cowling
Check leveling of aircraft on ground.
Pilot/Owner
Engine cowling
Remove engine cowling.
Refer to Section 71-00.3.1
Pilot/Owner
Spinner
Remove spinner as defined in the basic aircraft
AMM
Pilot/Owner
Make record of all malfunctions and abnormalities
Pilot/Owner
05-20.2.5 Propulsion System
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Cleaning. Clean the engine as required in the
Maintenance Manual for ROTAX
®
Engine Type
912 Series.
Pilot/Owner
Engine. Conduct 100 hrs inspection as per
Maintenance Manual for
ROTAX
®
Engine Type 912 iS Series.
A&P

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