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Airworthiness Directive

AD 2015-13-10 80 FR 38391 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2015-16171
Amendment
39-18197
Published
2015-07-06
Effective
2015-07-21
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/2015-13-10 · 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

2015-13-10

FR doc 2015-16171 · 80 FR 38391

AD 2015-13-10Published 2015-07-06Effective 2015-07-21

Supersedes 2011-17-07

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 and replacing the primary flight control rudder cables, repetitively replacing all other primary flight control and trim tab cables, and checking/setting the flight control cable tension.

Full official abstract

We are superseding Airworthiness Directive (AD) 2011-17-07 for certain M7 Aerospace LLC (type certificate previously held by M7 Aerospace LP) Models SA226-T, SA226-T(B), SA226-TC, and SA226-AT airplanes. AD 2011-17-07 required repetitive replacement and inspection of certain elevator, rudder, aileron, and aileron-to-rudder interconnect primary control cables, and checking and setting of flight control cable tension. This AD requires repetitively inspecting and replacing the primary flight control rudder cables, repetitively replacing all other primary flight control and trim tab cables, and checking/setting the flight control cable tension. This AD was prompted by a report of extensive damage found on the left hand primary flight control rudder cable located under the cockpit floor on one of the airplanes affected by AD 2011-17-07. We are issuing this AD to correct the unsafe condition on these products.

More directives for Fairchild SA226/SA227 Metro

  1. AD 2021-01-02 Airworthiness Directives; M7 Aerospace LLC Airplanes 2021-01-22
  2. AD 2017-07-01 Airworthiness Directives; M7 Aerospace LLC Models Airplanes 2017-03-31
  3. AD 2016-25-12 Airworthiness Directives; M7 Aerospace LLC 2016-12-08
  4. AD 2016-15-02 Airworthiness Directives; M7 Aerospace LLC Airplanes 2016-07-22
  5. AD 2016-10-01 Airworthiness Directives; M7 Aerospace LLC Airplanes 2016-05-11

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)

Applies to 1 model in our index