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Airworthiness Directive

AD 2013-03-04 78 FR 9789 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the aft fuselage assembly in the area around the attachment point of the horizontal stabilizer, including the paint, for a crack.

Federal Register (opens in a new tab)

FR document
2013-02583
Published
2013-02-12
Effective
2013-03-19
Models covered
1

Last live check: Not yet checked

Printed from https://aircraftdirectives.com/ad/2013-03-04 · 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

2013-03-04

FR doc 2013-02583 · 78 FR 9789

AD 2013-03-04Published 2013-02-12Effective 2013-03-19

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 inspecting the aft fuselage assembly in the area around the attachment point of the horizontal stabilizer, including the paint, for a crack.

Full official abstract

We are adopting a new airworthiness directive (AD) for the Schweizer Aircraft Corporation (Schweizer) Model 269D and Model 269D Configuration A helicopters. The type certificate for these models is currently held by Sikorsky Aircraft Corporation (Sikorsky). This AD requires inspecting the aft fuselage assembly in the area around the attachment point of the horizontal stabilizer, including the paint, for a crack. This AD also requires inspecting the tailboom interior support structure, and if necessary, installing an inspection panel kit in the aft fuselage assembly, and installing doublers in the stabilizer support brackets. This AD is prompted by reports of loose horizontal stabilizers and cracks in the stabilizer support structure for the extruded tailboom. The actions are intended to prevent separation of the horizontal stabilizer from the helicopter and subsequent loss of control of the helicopter.

More directives for Schweizer 269 / 300

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  2. AD 2015-23-01 Airworthiness Directives; Sikorsky Aircraft Corporation (Type Certificat... Effective 2015-12-15
  3. AD 2015-11-09 Airworthiness Directives; Sikorsky Aircraft Corporation (Type Certificat... Effective 2015-07-14
  4. AD 2011-12-16 Airworthiness Directives; Schweizer Aircraft Corporation (Schweizer) Mod... Effective 2011-07-21
  5. AD 2010-16-08 Airworthiness Directives; Schweizer Aircraft Corporation (Schweizer) Mod... Effective 2010-08-20

All Schweizer 269 / 300 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2013-03-04 (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