AD 97-12-03

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747 Series Airplanes

AD Number
97-12-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-NM-70-AD
FR Citation
(Federal Register: June 09, 1997 (Volume 62, Number 110))

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, corrosion, and fracturing of the lower and upper horizontal clevis legs of the strut midspar fittings due to stress corrosion, which could result in drooping of the strut at the strut-to-wing interface and separation of the engine and strut from the airplane.

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

Required Actions

Inspect for cracking, corrosion, and fracturing of the lower and upper horizontal clevis legs of the strut midspar fittings, replace discrepant parts with new parts or rework as necessary, and remove broken sealant from the clevis and fasteners following Boeing Alert Service Bulletin 747-54A2179, Revision 1.

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

Compliance Time

Effective June 24, 1997.

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

Affected Aircraft

Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, and other 747 series airplanes as specified in the AD, with affected midspar fittings and engine types (Pratt & Whitney JT9D, Rolls Royce RB211, General Electric CF6-45/-50).

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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