AD 2001-03-10

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747-100, -200, -300, -400, and 747SR Series Airplanes

AD Number
2001-03-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-NM-206-AD
FR Citation
66 FR 10951

Applicability

TypeManufacturerModelDetails
aircraft Boeing 747-100 Airworthiness Directives; Boeing Model 747-100, -200, -300, -400, and 747SR Series Airplanes

Unsafe Condition

Installation of H-11 steel bolts as attach and support bolts at the trailing edge flap transmissions, which could lead to loss of a flap transmission and reduce lateral controllability of the airplane.

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

Required Actions

Inspect all airplanes to determine whether H-11 steel bolts are installed as attach and support bolts at the trailing edge flap transmissions. Replace any H-11 steel bolt with an Inconel bolt. Operators of airplanes with line number (L/N) 872 and subsequent may inspect maintenance records instead of performing the physical inspection, provided no major repair or replacement of a flap transmission or flap track has been done.

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

Compliance Time

Within 18 months of the effective date (March 28, 2001).

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

Affected Aircraft

All Boeing Model 747-100, -200, -300, -400, and 747SR 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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