Airworthiness Directive
AD 2003-01-04: Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B and 212 Helicopters
Airworthiness Directives; Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B and 212 Helicopters
- Effective
- Jan 30, 2003
- Published
- Jan 15, 2003
- Registered aircraft
- 124
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
- Bell 204-B
- Bell 205A
- Bell 205A-1
- Bell 205A-1
- Bell 205B
- Bell 212
- Bell 212
- Only with: Main rotor grip P/N 204-011-121-005, -009, -113, -117, or -121 installed depending on model (205B: -005, -009, -113, -117, -121; 212: -009, -121; 204B: -005 if ever installed on a 205B, or -117; 205A/205A-1: -005 or -113 if ever installed on a 205B, or -117; 205A-1: -009 or -121 modified per STC SH5132NM).
- Only with: Main rotor grip P/N 204-011-121-005, -009, -113, -117, or -121 installed depending on model (205B: -005, -009, -113, -117, -121; 212: -009, -121; 204B: -005 if ever installed on a 205B, or -117; 205A/205A-1: -005 or -113 if ever installed on a 205B, or -117; 205A-1: -009 or -121 modified per STC SH5132NM).
Applicability
From the AD textThe following model helicopters with the listed part number (P/N) installed, certificated in any category: Model With main rotor grip (Grip) P/N (1) 205B 204-011-121-005, -009, -113, -117, or -121. (2) 212 204-011-121-009 or -121. (3) 204B 204-011-121-005 if the grip was ever installed on a Model 205B helicopter. (4) 205A and 205A-1 204-011-121-005 or -113 if the grip was ever installed on a Model 205B helicopter. (5) 204B, 205A, and 205A-1 204-011-121-117. (6) 205A-1 204-011-121-009 or -121 modified in accordance with Supplemental Type Certificate (STC) SH5132NM.
Related ADs
Superseded or revised by AD 2014-12-04.
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