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Airworthiness Directive

AD 2004-19-09 69 FR 56688 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-21269
Amendment
39-13803
Published
2004-09-22
Effective
2004-10-07
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2004-19-09 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2004-19-09

FR doc 04-21269 · 69 FR 56688

AD 2004-19-09Published 2004-09-22Effective 2004-10-07

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 track-and-balancing certain main rotor blades (blades), replacing blades, and determining the age of each blade and revising the component history card or equivalent maintenance record.

Full official abstract

This amendment supersedes an existing emergency airworthiness directive (AD) for the Robinson Helicopter Company (Robinson) Model R22, R22 Alpha, R22 Beta, and R22 Mariner helicopters, that currently requires track-and-balancing certain main rotor blades (blades), replacing blades, and determining the age of each blade and revising the component history card or equivalent maintenance record. This amendment requires the same actions, but changes the applicability and adds clarifying language. It also prohibits the issuance of special flight permits, which the existing AD allows. This amendment is prompted by the need to clarify the existing AD language. The actions specified by this AD are intended to prevent a fatigue crack, blade failure, and subsequent loss of control of the helicopter.

More directives for Robinson R22

  1. AD 2024-20-03 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-10-24
  2. AD 2024-04-02 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-02-27
  3. AD 2022-12-08 Airworthiness Directives; Robinson Helicopter Company Helicopters 2022-06-14
  4. AD 2013-19-06 Airworthiness Directives; Robinson Helicopter Company (Robinson) 2013-10-01
  5. AD 2011-12-10 Airworthiness Directives; Robinson Helicopter Company Model (Robinson) R... 2011-06-17

All Robinson R22 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index