AD 2003-14-09

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 767 Series Airplanes

AD Number
2003-14-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-395-AD
FR Citation
68 FR 42573

Applicability

TypeManufacturerModelDetails
aircraft Boeing 767 Airworthiness Directives; Boeing Model 767 Series Airplanes

Unsafe Condition

Failure of the collar fittings, which could result in separation of the inboard trailing edge flap and consequent reduced controllability of the airplane.

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

Required Actions

Inspect both inboard trailing edge flaps for cracked, corroded, or stained collar fittings, torque tube, and splined bushings. Perform follow-on and corrective actions as necessary. Revise the Accomplishment Instructions of Revision 3 of the service bulletin for corrosion removal and rework procedures.

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

Compliance Time

Before further flight

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

Affected Aircraft

Boeing Model 767 series airplanes, as specified in the referenced service bulletin.

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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