AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 95-12-23 60 FR 31241 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-14404
Amendment
39-9275
Published
1995-06-14
Effective
1995-07-30
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/95-12-23 · 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

95-12-23

FR doc 95-14404 · 60 FR 31241

AD 95-12-23Published 1995-06-14Effective 1995-07-30

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 initially inspecting the wing structure for cracks, modifying any cracked wing structure, and, if not cracked, either repetitively inspecting or modifying the wing structure.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Twin Commander Aircraft Corporation (Twin Commander) Models 690C and 695 airplanes. This action requires initially inspecting the wing structure for cracks, modifying any cracked wing structure, and, if not cracked, either repetitively inspecting or modifying the wing structure. Results of full-scale fatigue testing that indicated areas in the wing that are subject to fatigue cracks prompted this action. The actions specified by this AD are intended to prevent wing damage caused by fatigue cracking, which, if not detected and corrected, could progress to the point of structural failure.

More directives for Twin Commander (Aero Commander)

  1. AD 2013-09-05 Airworthiness Directives; Twin Commander Aircraft LLC Airplanes 2013-05-14
  2. AD 2009-25-02 Airworthiness Directives; Twin Commander Aircraft LLC Models 690, 690A, ... 2009-12-04
  3. AD 2006-15-01 Airworthiness Directives; Twin Commander Aircraft Corporation Models 690... 2006-07-17
  4. AD 2003-07-03 Airworthiness Directives; Twin Commander Aircraft Corporation Models 690... 2003-04-03
  5. AD 98-08-25 R1 Airworthiness Directives; Twin Commander Aircraft Corporation 500, 680, ... 1999-01-05

All Twin Commander (Aero Commander) 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