AD 2008-19-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Socata | TBM 700 | Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes |
Unsafe Condition
Rupture of the alternator and vapor cycle cooling system pulley drive assembly, compressor drive shaft, and cracks on the standby-alternator and compressor support.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove the compressor drive belt and torque limiter temporarily. Conditionally replace the pulley drive shear shaft. Perform repetitive inspections for cracks on the pulley drive assembly and alternator/compressor support. Replace the original pulley drive assembly with a time-limited assembly of a new design.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 flight hours after the effective date of this AD.
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Affected Aircraft
EADS SOCATA Model TBM 700 airplanes, all serial numbers beginning with 434, certificated in any category.
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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