AD 2002-08-06

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes

AD Number
2002-08-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-38-AD
FR Citation
67 FR 37975

Applicability

TypeManufacturerModelDetails
aircraft Boeing 777-200 and -300 Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes

Unsafe Condition

Inadequate torque of bolts attaching pivot fittings to the horizontal stabilizer through upper and lower titanium straps.

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

Required Actions

Inspect the torque of the bolts attaching pivot fittings to the horizontal stabilizer. Submit a report as required by paragraph (d) of the AD, with an option for a 30-day grace period.

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

Compliance Time

Within 30 days for report submission (optional grace period).

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

Affected Aircraft

Boeing Model 777-200 and -300 series airplanes.

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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View Official Source ↗ Find More ADs for Boeing 777-200 and -300

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Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes Equipped With Rolls-Royce RB211-TRENT 800 Series Engines

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