AD 2003-11-16

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 767 Series Airplanes

AD Number
2003-11-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-142-AD
FR Citation
68 FR 32968

Applicability

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

Unsafe Condition

Missing, loose, or cracked bolts on the inboard and outboard support of the inboard main flap could result in loss of the inboard main flap, which could lead to loss of control of the airplane.

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

Required Actions

Inspect for missing bolts on the inboard and outboard support of the inboard main flap. If no bolts are missing, inspect for gaps indicating loose bolts. If any bolt is missing or a gap is found, remove all bolts in the subject area and replace them with new or serviceable bolts. Eventually, replace existing titanium bolts with steel bolts.

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

Compliance Time

Within 90 days after August 27, 2002, for the initial inspection. Before further flight for follow-on actions.

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

Affected Aircraft

Boeing Model 767 series airplanes, including Model 767-400ER series airplanes, line numbers 1 through 879 inclusive, 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 6, 2026

Rights: U.S. Government Public Domain

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