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 05-20-2
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
05-20.2.2 Aircraft Records
This chapter of AMM is not affected by this Supplement
05-20.2.3 Run-Up
▲Warning: Run-up shall be performed before any inspection.
▲Warning: Run-up shall continue until all temperatures are acceptable for take-off.
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Engine and engine compartment
Clean for leakage check
Pilot/Owner
Run up of engine: Conduct per following checklist,
fill pre-inspection values only:
Pilot/Owner
Systems Pre-inspection Post-inspection
Engine oil. Check the level of oil and follow the Operator’s
Manual for all versions of ROTAX
®
912 iS or SECTION 12-10.
Brakes and parking brake. Check for proper operation
Starter. Smooth operation, starting properties
Oil pressure. 3…5 bar / 44…73 PSI
bar/PSI
bar/PSI
Engine Instruments. Check engine parameters
Ignition ground test. (See Operator’s Manual for ROTAX
®
912 iS)
Oil temperature. 90…110°C /190…230°C
°C/ °F
°C/ °F
▲Warning: Ensure that cylinder head temperature (CHT) and oil temperature are within limits.
Cabin heat
Idle RPM. Tachometer should read 1400 RPM
RPM
RPM
Engine full power RPM. Tachometer should read 4900 to
5000RPM
RPM
RPM
Ignition check. Set RPM to 4000.
Turn “OFF” LANE selector switch A. Record rpm drop. Must
not be more than 180.
Turn “ON” LANE selector switch A.
Turn “OFF” LANE selector switch B. Record rpm drop. Must
not be more than 180.
Turn “ON” LANE selector switch B.
RPM
RPM
RPM
RPM
Directional stability of nose gear
▲Warning: Allow engine to cool down to 149°C (300°F) (CHT) be fore shutdown. Shut down the
engine, set the ignition switch and the master switch to the off position. Remove
ignition key from the aircraft.
Check for fuel and exhaust odors in cabin
Check for fuel stains on floor
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