AD 91-06-03

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Model 747 Series Airplanes

AD Number
91-06-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-152-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-100B Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-100B SUD Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200B Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200C Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200F Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-300 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400D Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400F Series Airworthiness Directives; BOEING Model 747 Series Airplanes

Unsafe Condition

Cracking of the Section 42 fuselage frame web at the stringer cutout from body station 540 to BS 920, Stringer 8L to S-8R could result in sudden cabin pressure loss.

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

Required Actions

Perform a detailed visual inspection for cracks of the Section 42 fuselage frame web within the next 500 flight cycles after the effective date or prior to 12,000 total flight cycles, whichever is later. Repeat inspections at intervals not exceeding 3,000 flight cycles. If cracking is found, repair the frame web per Boeing SRM Section 53-10-04, Figures 4 or 35, or an approved method before further flight.

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

Compliance Time

Within the next 500 flight cycles after the effective date of this AD, or prior to the accumulation of 12,000 total flight cycles, whichever occurs later

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

Affected Aircraft

Boeing Model 747 series airplanes, line numbers 001 through 045, 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 8, 2026

Rights: U.S. Government Public Domain

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