Airworthiness Directive

AD 2017-10-20 82 FR 24030 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitive inspections to detect cracks in the bulkhead and any necessary repairs.

FR document
2017-10407
Amendment
39-18894
Published
2017-05-25
Effective
2017-06-29
Models covered
1

Last live check: 2026-08-19

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AD

2017-10-20

FR doc 2017-10407 · 82 FR 24030

AD 2017-10-20Published 2017-05-25Effective 2017-06-29

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 repetitive inspections to detect cracks in the bulkhead and any necessary repairs.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, and PA-31-350 airplanes. This AD was prompted by fatigue cracking in the fuselage station (FS) 332.00 bulkhead common to the horizontal stabilizer front spar attachment. This AD requires repetitive inspections to detect cracks in the bulkhead and any necessary repairs. This AD also provides an optional modification if no cracks are found that will greatly reduce the likelihood of the specified cracks. We are issuing this AD to correct the unsafe condition on these products.

More directives for Piper PA-31 Navajo/Cheyenne

  1. AD 2017-02-06 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2017-02-22
  2. AD 2016-08-18 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2016-06-06
  3. AD 2016-05-01 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2016-04-15
  4. AD 2015-24-05 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2016-01-12
  5. AD 2014-23-03 Airworthiness Directives; Piper Aircraft, Inc. Effective 2014-12-18

All Piper PA-31 Navajo/Cheyenne directives

Applies to 1 model in our index