Airworthiness Directive

AD 99-23-01 64 FR 59613 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-28655
Amendment
39-11397
Published
1999-11-03
Effective
1999-12-08
Models covered
1
Last live check
2026-10-01
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AD

99-23-01

FR doc 99-28655 · 64 FR 59613

AD 99-23-01Published 1999-11-03Effective 1999-12-08

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires removing and replacing the pilot's cyclic control grip assembly (grip assembly) with an airworthy grip assembly.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to Robinson Model R44 helicopters, that currently requires removing and replacing the pilot's cyclic control grip assembly (grip assembly) with an airworthy grip assembly. This amendment requires the same actions as the current AD but would change a part number (P/N) referenced in the current AD. This amendment is prompted by the discovery of an error in the P/N of the current AD. The actions specified by this AD are intended to prevent use of a grip assembly that may crack, resulting in failure of the grip assembly and subsequent loss of control of the helicopter.

More directives for Robinson R44

  1. AD 2025-11-07 Airworthiness Directives; Robinson Helicopter Company Helicopters 2025-06-06
  2. AD 2024-23-01 Airworthiness Directives; Robinson Helicopter Company 2024-12-03
  3. AD 2024-20-03 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-10-24
  4. AD 2024-19-11 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-09-26
  5. AD 2024-04-02 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-02-27

All Robinson R44 directives

Applies to 1 model in our index