Airworthiness Limitations - Lycoming TEO-540-C1A Maintenance Manual

TEO-540-C1A Engine Maintenance Manual
TEO-540-C1A Engine Maintenance Manual
1. General
This Airworthiness Limitations chapter sets forth each mandatory replacement time,
inspection interval, and related procedure required for type certification. The
Airworthiness Limitations section is FAA approved and specifies maintenance required
under 14 CFR §§ 43.16 and 91.403 of the Federal Aviation Regulations (FAR) unless an
alternative program has been FAA-approved.
2. Mandatory Inspection - Exhaust Valve and Guide
At every 1000 hours of operation for TEO-540-C1A engines, examine the exhaust valve
and guide conditions. Refer to the section "Exhaust Valve and Guide Inspection" in
Chapter 72-30.
3. Mandatory Inspection – EECS NTO Faults
Take-off is prohibited with Electronic Engine Control System No Take-Off Faults
annunciated. The NTO annunciator indicates engine control fault(s) exists that exceed 14
CFR Part 33 limitations; the engine is not airworthy with the NTO annunciator
illuminated. The fault(s) must be identified, the condition corrected, and the fault(s)
cleared before take-off.
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November 2018

AIRWORTHINESS LIMITATIONS

Airworthiness Limitations
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