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Airworthiness Directive

AD 97-10-13 62 FR 26223 Active

Federal Aviation Administration · 14 CFR part 39

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FR document
97-12517
Amendment
39-10025
Published
1997-05-13
Effective
1997-07-08
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/97-10-13 · 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

97-10-13

FR doc 97-12517 · 62 FR 26223

AD 97-10-13Published 1997-05-13Effective 1997-07-08

Supersedes 96-21-05

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 the following on certain Fairchild Aircraft, Inc.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 96-21- 05, which currently requires the following on certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes that do not have a certain elevator torque tube installed: drilling inspection access holes in the elevator torque tube arm, inspecting the elevator torque tube for corrosion, replacing any corroded elevator torque tube, and applying a corrosion preventive compound. AD 96-21-05 resulted from several reports of corrosion found in the elevator torque tube area on the affected airplanes. This AD retains the actions required by AD 96- 21-05, and adds certain Fairchild Model SA227-BC airplanes to the Applicability section of that AD. The actions specified by this AD are intended to prevent failure of the flight control system caused by a corroded elevator torque tube, which could result in loss of control of the airplane.

More directives for Fairchild SA226/SA227 Metro

  1. AD 2021-01-02 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2021-02-26
  2. AD 2017-07-01 Airworthiness Directives; M7 Aerospace LLC Models Airplanes Effective 2017-05-05
  3. AD 2016-25-12 Airworthiness Directives; M7 Aerospace LLC Effective 2017-01-12
  4. AD 2016-15-02 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2016-08-26
  5. AD 2016-10-01 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2016-06-15

All Fairchild SA226/SA227 Metro 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