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Airworthiness Directive

AD 2021-07-15: Airbus Helicopters

Airworthiness Directives; Airbus Helicopters

Effective
May 7, 2021
Published
Apr 2, 2021
Registered aircraft
363

Models this AD may apply to

AI-extracted — verify against original

Matched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.

Aircraft

  • Only with: With a tail rotor drive shaft bearing P/N 593404, 6007-2RS1MT47CA, P9107NPP7, 83A851BC3, or 83A851B-1C3, or MP/N 704A33-651-010, 704A33-651-111, 704A33-651-143, or 704A33-651-181 installed.
  • Only with: With a tail rotor drive shaft bearing P/N 593404, 6007-2RS1MT47CA, P9107NPP7, 83A851BC3, or 83A851B-1C3, or MP/N 704A33-651-010, 704A33-651-111, 704A33-651-143, or 704A33-651-181 installed.

Applicability

From the AD text
This airworthiness directive (AD) applies to Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters, certificated in any category, with a tail rotor (TR) drive shaft bearing (bearing) part number (P/N) 593404, 6007-2RS1MT47CA, P9107NPP7, 83A851BC3, or 83A851B-1C3, or manufacturer part number (MP/N) 704A33-651-010, 704A33-651-111, 704A33-651-143, or 704A33-651-181, installed.

Related ADs

Supersedes or revises AD 82-20-05.

Read the AD in the Federal RegisterReport an error on this page