AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2008-15-06 73 FR 43845 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E8-16583
Amendment
39-15618
Published
2008-07-29
Effective
2008-09-02
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/2008-15-06 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2008-15-06

FR doc E8-16583 · 73 FR 43845

AD 2008-15-06Published 2008-07-29Effective 2008-09-02

Superseded by 2016-14-05

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 you to check the airplane logbook to determine if the original engine mounting brackets have been replaced.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 175 and 175A airplanes. This AD requires you to check the airplane logbook to determine if the original engine mounting brackets have been replaced. If the original engine mounting brackets are still installed, this AD requires you to repetitively inspect those brackets for cracks and replace any cracked engine mounting bracket. After replacing all four original engine mounting brackets, no further action will be required by this AD. This AD was prompted by a report that the engine became detached from the firewall during landing on one of the affected airplanes. We are issuing this AD to detect and correct cracks in the engine mounting brackets, which could result in failure of the engine mounting bracket. This failure could lead to the engine detaching from the firewall.

More directives for Cessna 175 Skylark

  1. AD 2016-14-05 Airworthiness Directives; Textron Aviation Inc. Airplanes 2016-07-07
  2. AD 2011-10-09 Airworthiness Directives; Cessna Aircraft Company Models 150, 152, 170, ... 2011-05-13
  3. AD 2008-26-10 Airworthiness Directives; Cessna Aircraft Company 172, 175, 177, 180, 18... 2008-12-24
  4. AD 2008-10-02 Airworthiness Directives; Cessna Aircraft Company 172, 175, 180, 182, 18... 2008-05-02
  5. AD 2004-19-04 Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 150, F... 2004-09-17

All Cessna 175 Skylark directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2008-15-06 (opens in a new tab)

Applies to 1 model in our index