Airworthiness Directive
AD 2005-15-08: Boeing Model 747-100B SUD, -200B, -300, -400, and -400D Series Airplanes
Airworthiness Directives; Boeing Model 747-100B SUD, -200B, -300, -400, and -400D Series Airplanes
- Effective
- Aug 30, 2005
- Published
- Jul 26, 2005
- Registered aircraft
- 5
Models this AD may apply to
AI-extracted — verify against originalMatched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.
Aircraft
- Boeing 747-100B
- Boeing 747-100B-SUD
- Boeing 747-200B
- Boeing 747-300 SERIES
- Boeing 747-400
- Boeing 747-400BCF
- Boeing 747-400D
- Boeing 747-400ERF
- Boeing 747-400F
- Boeing 747-400M
- Boeing 747-400SF
- Boeing 747-400UF
- Serial numbers per Boeing Alert Service Bulletin 747-53A2484, dated June 26, 2003
Applicability
From the AD text(c) This AD applies to certain Boeing Model 747-100B SUD, -200B, -300, -400, and -400D series airplanes; certificated in any category; as listed in Boeing Alert Service Bulletin 747-53A2484, dated June 26, 2003. Unsafe Condition (d) This AD was prompted by findings of cracking in fuselage stringers 8L, 8R, 10L, and 10R at body station 460, 480, and 500 frame locations. We are issuing this AD to detect and correct fatigue cracking in the specified fuselage stringers, which, if left undetected, could result in fuselage skin cracking that reduces the structural integrity of the skin panel, and consequent rapid depressurization of the airplane.
Related ADs
Superseded or revised by AD 2010-01-02.
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