AD 89-21-09

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Model 747 Series Airplanes

AD Number
89-21-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-56-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

Fatigue cracks in the skin at body station (BS) 460 just above left and right number 1 main entry doors could cause cabin pressure loss.

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

Required Actions

Conduct high frequency eddy current (HFEC) inspections of fuselage skin along specified fasteners at intervals not exceeding 3,000 landings. If cracks are found, modify the splice per Boeing Service Bulletin or perform internal HFEC inspections and repairs per the 747 Structural Repair Manual. Alternate compliance may be approved by the FAA.

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

Compliance Time

Prior to the accumulation of 10,000 landings, or within the next 1,000 landings after the effective date of this AD, 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 listed in Boeing Service Bulletin 747-53-2289, Revision 1, dated January 26, 1989.

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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