AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 95-06-03 60 FR 31236 Active

Federal Aviation Administration · 14 CFR part 39

Requires an inspection and modification of the main rotor (M/R) gearbox.

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
95-14445
Amendment
39-9276
Published
1995-06-14
Effective
1995-06-29
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/95-06-03 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

95-06-03

FR doc 95-14445 · 60 FR 31236

AD 95-06-03Published 1995-06-14Effective 1995-06-29

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 an inspection and modification of the main rotor (M/R) gearbox.

Full official abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-06-03 which was sent previously to all known U.S. owners and operators of Robinson Helicopter Company (Robinson) Model R22 helicopters by individual letters. This AD requires an inspection and modification of the main rotor (M/R) gearbox. This amendment is prompted by a report of an incident involving a Model R22 helicopter in which the two M/R mast spanner nuts (nuts) became loose, resulting in failure of the M/R mast support structure. The actions specified by this AD are intended to prevent M/R separation and subsequent loss of control of the helicopter.

More directives for Robinson R22

  1. AD 2024-20-03 Airworthiness Directives; Robinson Helicopter Company Helicopters Effective 2024-11-29
  2. AD 2024-04-02 Airworthiness Directives; Robinson Helicopter Company Helicopters Effective 2024-04-02
  3. AD 2022-12-08 Airworthiness Directives; Robinson Helicopter Company Helicopters Effective 2022-06-29
  4. AD 2014-23-16 Airworthiness Directives; Robinson Helicopter Company Helicopters Effective 2015-01-09
  5. AD 2013-19-06 Airworthiness Directives; Robinson Helicopter Company (Robinson) Effective 2013-11-05

All Robinson R22 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index