AD 2007-06-14

final rule
Data completeness: 80%

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

AD Number
2007-06-14
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2006-26180
FR Citation
72 FR 12548

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

Discovery of propeller control cables with defective crimping. Two cable ends were found uncrimped at the factory after an engine run-up test, and one cable end was also found uncrimped on the first 100-hour time-in-service aircraft maintenance check. If not corrected, an incorrect crimping of the propeller control lever cable could generate a decrease of the propeller revolutions per minute which could result in loss of power.

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

Required Actions

Inspect for the batch number identification and replace defective control cables as necessary in accordance with the paragraph B. of the 'ACCOMPLISHMENT INSTRUCTIONS' of EADS SOCATA TBM Aircraft Mandatory Alert Service Bulletin SB 70-123, dated October 2004.

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

Compliance Time

Within the next 50 hours time-in-service (TIS) after April 20, 2007 (the effective date of this AD).

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 285 through 304 and 307, 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 4, 2026

Rights: U.S. Government Public Domain

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