Airworthiness Directive

AD 96-09-08 61 FR 19540 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-10477
Amendment
39-9584
Published
1996-05-02
Effective
1996-05-20
Models covered
1
Last live check
2026-09-30
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AD

96-09-08

FR doc 96-10477 · 61 FR 19540

AD 96-09-08Published 1996-05-02Effective 1996-05-20

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 longerons aft of the rear cabane struts for cracks, and if cracked, prior to further flight, repairing the cracks.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Aviat Aircraft Inc., Models S-2A, S-2B, and S-2S airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes). This action requires inspecting the longerons aft of the rear cabane struts for cracks, and if cracked, prior to further flight, repairing the cracks. Reports of longeron failure caused by fatigue aft of the rear cabane struts prompted this action. The actions specified by this AD are intended to prevent cracking and subsequent failure of the longerons resulting in possible loss of control of the airplane.

More directives for Aviat/Pitts Special

  1. AD 96-12-03 R2 Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S... 1998-10-01
  2. AD 97-26-20 Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2... 1997-12-30
  3. AD 97-17-07 Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S... 1997-08-22
  4. AD 96-09-08 R1 Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2... 1996-07-09
  5. AD 96-12-03 Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S... 1996-06-06

All Aviat/Pitts Special directives

Applies to 1 model in our index