AD 94-15-17

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747 Series Airplanes

AD Number
94-15-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
93-NM-212-AD
FR Citation
(Federal Register: August 03, 1994 (Volume 59, Number 148))

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 skin around the fasteners in the upper row of the longitudinal lap joints of Stringer S-12L and S-12R from station 520 to station 741.1 can lead to rapid decompression of the airplane.

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

Required Actions

Perform an external high frequency eddy current inspection to detect skin cracking, repair any cracking found, replace countersunk fasteners with protruding head fasteners, and conduct follow-up inspections post-replacement.

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

Compliance Time

Prior to the accumulation of 15,000 total flight cycles or within 1,000 flight cycles after the effective date of this AD, whichever occurs later for inspections; prior to the accumulation of 20,000 total flight cycles or within 4 years after the effective date for fastener replacement.

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

Affected Aircraft

Boeing Model 747 series airplanes with line numbers 201 through 230 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 8, 2026

Rights: U.S. Government Public Domain

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