AD 98-12-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA | TBM 700 | Airworthiness Directives; SOCATA Groupe Aerospatiale Model TBM 700 Airplanes. |
Unsafe Condition
Cracks in the elevator trim tab fittings could result in separation of the elevator trim tab and loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the left- and right-hand elevator trim tab fittings for cracks using a dye penetrant aerosol method per SB 70-079-55. Replace any cracked parts with improved design assemblies prior to further flight. Do not install elevator trim tab assemblies manufactured between January 1, 1993 and February 29, 1996.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 100 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
SOCATA Groupe Aerospatiale Model TBM 700 airplanes, serial numbers 83, and 93 through 109
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.