AD 2002-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Turbomeca | S | Airworthiness Directives; Turbomeca S.A. Makila Models 1A, 1A1, and 1A2 Turboshaft Engines |
Unsafe Condition
Modification TU 200A exhaust pipes cracking at several of the ejector attachment tabs, which could result in the ejector becoming loose from the exhaust pipe.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect exhaust pipes for cracks and tears upon completion of the last flight of each day. Replace cracked or torn exhaust pipes before further flight. Remove modification TU 200A exhaust pipes from service at the next shop visit or by a specified date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date of the AD.
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Affected Aircraft
Turbomeca S.A. Makila Models 1A, 1A1, and 1A2 turboshaft engines with exhaust pipes incorporating modification TU 200A.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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