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Airworthiness Directive

AD 95-19-07 60 FR 47687 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires repetitively inspecting, using ultrasonic methods, the left-hand and right-hand MLG yokes and the NLG yokes for stress corrosion cracking, and, if any cracked yokes are found that exceed certain limits, either replacing…

Superseded by AD 96-19-05Federal Register (opens in a new tab)

FR document
95-22646
Amendment
39-9369
Published
1995-09-14
Effective
1995-09-28
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/95-19-07 · 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

95-19-07

FR doc 95-22646 · 60 FR 47687

AD 95-19-07Published 1995-09-14Effective 1995-09-28

Superseded by 96-19-05

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 repetitively inspecting, using ultrasonic methods, the left-hand and right-hand MLG yokes and the NLG yokes for stress corrosion cracking, and, if any cracked yokes are found that exceed certain limits, either replacing the cracked yoke, the yoke/cylinder combination, or the affected MLG or NLG assembly.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Fairchild Aircraft SA226 and SA227 series airplanes equipped with certain main landing gear (MLG) and nose landing gear (NLG). This action requires repetitively inspecting, using ultrasonic methods, the left-hand and right-hand MLG yokes and the NLG yokes for stress corrosion cracking, and, if any cracked yokes are found that exceed certain limits, either replacing the cracked yoke, the yoke/cylinder combination, or the affected MLG or NLG assembly. Several reports of landing gear failures on the affected airplanes that have the affected MLG or NLG yokes installed prompted this action. The actions specified by this AD are intended to prevent MLG or NLG failure caused by stress corrosion cracks in the yokes, which, if not detected and corrected, could result in loss of control of the airplane during landing operations.

More directives for Fairchild SA226/SA227 Metro

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  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) Search DRS manually for AD 95-19-07 (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