CHAPTER
4
AIRWORTHINESS LIMITATIONS
This Airworthiness Limitations section has been FAA approved and specifies maintenance required
under
95
43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has
been FAA approved. Federal Aviation Regulations
§§
43.16 and 91.403 require ownerloperator
compliance with all maintenance limitations in this section concerning mandatory replacement times,
inspection intervals and other related procedures that are specific to this engine. Any such
limitations listed below are part of the design limits of the engine and the engine was type certificated
based upon required
ownerloperator compliance with the limitations.
1.
Mandatow Re~lacement Times.
Subject to additional information contained in FAA Airworthiness Directives (AD) issued after the
date of certification, the engines covered in this manual do not contain any components having
mandatory replacement times required by type certification.
2. Mandatow lnssectisn Intervals.
Subject to additional information contained in FAA Airworthiness Directives (AD) issued after the
date of certification, the engine does not require specific intervals of inspection pursuant to type
certification.
3.
Other Related Procedures
Subject to additional information contained in the Airworthiness Directives
(AD)
issued after the
date of certification, there are no other related procedures required pursuant to the type
certification for this engine.
4.
Distribution of Changes to Airworthiness Limitations.
Changes to the Airworthiness Limitations section constitute changes to the type design of this
engine and require FAA approval. Such changes will be published in FAA Airworthiness
Directives (AD).
NOTE
The limitations in this section apply only to specific limitations which are part of the engine design.
Under the Federal Aviation Regulations numerous other additional limitations are applicable to this
engine and it's accessories. For example Federal Aviation Regulation Parts 91 and 43, among other
parts, define inspection criteria, maintenance requirements and procedures that are applicable to
this engine. It is the responsibility of the owner
/
operator to maintain the engine in an airworthy
condition by complying with all applicable Federal Aviation Regulations and by performing
maintenance in accordance with TCM
lnstructions for Continued Airworthiness, which consist of
TCM publications and service documents.
REVISED
OCT 97 4-00-01
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