AD 2006-22-11

final rule
Data completeness: 80%

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

AD Number
2006-22-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25332
FR Citation
71 FR 62902

Applicability

TypeManufacturerModelDetails
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

Unsatisfactory initial elevator trim actuator greasing may lead to the icing of the elevator trim and generate an untrimmed nose-up attitude after an autopilot disconnection.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Lubricate the elevator trim tab actuator rods without removal, within the next 25 hours time-in-service after December 1, 2006. Follow EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB70-124, Amendment 1, ATA No. 27, dated January 2005.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 25 hours time-in-service after December 1, 2006.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

EADS SOCATA Model TBM 700 airplanes, serial numbers 1 through 32, 34, 36 through 69, 71 through 76, 79, 81 through 92, 96 through 98, 101, 102, 107 through 109, 112 through 114, 116, 118 through 124, 126 through 130, 132 through 135, 137, 138, 140 through 145, 148 through 155, 157, 158, 161 through 268, and 270 through 304.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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