Airworthiness Directive
AD 2004-22-03: Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes
- Effective
- Dec 3, 2004
- Published
- Oct 29, 2004
- Registered aircraft
- 432
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
- Embraer EMB-135
- Embraer EMB-135BJ
- Embraer EMB-135BJ
- Embraer EMB-135ER
- Embraer EMB-135KL
- Embraer EMB-135LR
- Embraer EMB-145
- Embraer EMB-145EP
- Embraer EMB-145ER
- Embraer EMB-145EU
- Embraer EMB-145LR
- Embraer EMB-145LU
- Embraer EMB-145MP
- Embraer EMB-145MR
- Embraer EMB-145XR
- Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002
Applicability
From the AD text(c) This AD applies to EMBRAER Model EMB-135 and -145 series airplanes, as listed in EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002; certificated in any category. Unsafe Condition (d) This AD was prompted by a report indicating that trunnion fittings of the wings have been manufactured with a web fillet radius smaller than the minimum required by the design data, which may induce the occurrence of fatigue cracks at the root of the trunnion fillet radius and adjacent structures (e.g., spar and ribs). We are issuing this AD to detect and correct fatigue cracking of the wing trunnion fittings or adjacent structure, which could result in failure of the main landing gear, consequent damage to surrounding structure, and possible loss of control of the airplane during landing.
Read the AD in the Federal RegisterReport an error on this page