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Airworthiness Directive

AD 2016-14-05 81 FR 44207 Active

Federal Aviation Administration · 14 CFR part 39

We are superseding Airworthiness Directive (AD) 2008-15-06 for certain Textron Aviation Inc.

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

FR document
2016-15866
Amendment
39-18586
Published
2016-07-07
Effective
2016-08-11
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2016-14-05 · 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

2016-14-05

FR doc 2016-15866 · 81 FR 44207

AD 2016-14-05Published 2016-07-07Effective 2016-08-11

Supersedes 2008-15-06

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.

We are superseding Airworthiness Directive (AD) 2008-15-06 for certain Textron Aviation Inc.

Full official abstract

We are superseding Airworthiness Directive (AD) 2008-15-06 for certain Textron Aviation Inc. Models 175 and 175A airplanes (type certificate previously held by Cessna Aircraft Company). AD 2008-15-06 required checking the airplane logbook to determine if the original engine mounting brackets had been replaced. If the original engine mounting brackets were still installed, the AD required repetitively inspecting those brackets for cracks and replacing any cracked engine mounting bracket until all four original engine mounting brackets were replaced. Replacing all four original engine mounting brackets terminated the actions required in AD 2008-15-06. Since we issued AD 2008-15-06, we have determined that the applicability needs to be changed to add one serial number and remove another. This new AD retains the actions required in AD 2008-15-06 and changes the Applicability section. We are issuing this AD to correct the unsafe condition on these products.

More directives for Cessna 175 Skylark

  1. AD 2011-10-09 Airworthiness Directives; Cessna Aircraft Company Models 150, 152, 170, ... Effective 2011-06-17
  2. AD 2008-26-10 Airworthiness Directives; Cessna Aircraft Company 172, 175, 177, 180, 18... Effective 2009-01-05
  3. AD 2008-15-06 Airworthiness Directives; Cessna Aircraft Company Models 175 and 175A Ai... Effective 2008-09-02
  4. AD 2008-10-02 Airworthiness Directives; Cessna Aircraft Company 172, 175, 180, 182, 18... Effective 2008-05-12
  5. AD 2004-19-01 Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 150, F... Effective 2004-11-01

All Cessna 175 Skylark 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