Airworthiness Directive

AD 97-02-14 62 FR 4001 Active

Federal Aviation Administration · 14 CFR part 39

Requires installation of an improved throttle governor; an adjustment to the low RPM warning unit threshold to increase the revolutions-per-minute (RPM) at which the warning horn and caution light activate; and revisions to the…

FR document
97-1702
Amendment
39-9899
Published
1997-01-28
Effective
1997-03-04
Models covered
1

Last live check: 2026-08-19

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AD

97-02-14

FR doc 97-1702 · 62 FR 4001

AD 97-02-14Published 1997-01-28Effective 1997-03-04

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 installation of an improved throttle governor; an adjustment to the low RPM warning unit threshold to increase the revolutions-per-minute (RPM) at which the warning horn and caution light activate; and revisions to the R22 Rotorcraft Flight Manual that prohibit flight with the improved throttle governor selected off, except in certain situations.

Supersedes an earlier directive. See the official text.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to Robinson Helicopter Company (Robinson) Model R22 helicopters, that currently requires installation of an improved throttle governor; an adjustment to the low RPM warning unit threshold to increase the revolutions-per-minute (RPM) at which the warning horn and caution light activate; and revisions to the R22 Rotorcraft Flight Manual that prohibit flight with the improved throttle governor selected off, except in certain situations. This amendment requires the same actions required by the existing AD, as well as requires an insertion of procedures for the improved throttle governor into the Normal and Emergency sections of the R22 Rotorcraft Flight Manual and corrects the applicability section of the existing AD. This amendment is prompted by the need to insert normal and emergency procedures for the improved throttle governor into the flight manual, and expand the applicability statement of this AD to include all Robinson Model R22 helicopters. The actions specified by the proposed AD are intended to minimize the possibility of pilot mismanagement of the main rotor (M/R) RPM, which could result in unrecoverable M/R blade stall 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

Applies to 1 model in our index