Airworthiness Directive

AD 2012-18-01 77 FR 54787 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-21536
Amendment
39-17177
Published
2012-09-06
Effective
2012-09-21
Models covered
1
Last live check
2026-09-30
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AD

2012-18-01

FR doc 2012-21536 · 77 FR 54787

AD 2012-18-01Published 2012-09-06Effective 2012-09-21

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 repetitively inspecting the left and right forward (main) and aft spar wing-to-fuselage attach fittings for cracks and replacing any cracked fitting.

Full official abstract

We are adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), SA227-AT, and SA227-TT airplanes. This AD requires repetitively inspecting the left and right forward (main) and aft spar wing-to-fuselage attach fittings for cracks and replacing any cracked fitting. This AD also requires reporting certain inspection results to the FAA. This AD was prompted by reports of fatigue cracking in the left and right forward (main) spar wing-to-fuselage attach fittings. We are issuing this AD to correct the unsafe condition on these products.

More directives for Fairchild SA226/SA227 Metro

  1. AD 2021-01-02 Airworthiness Directives; M7 Aerospace LLC Airplanes 2021-01-22
  2. AD 2017-07-01 Airworthiness Directives; M7 Aerospace LLC Models Airplanes 2017-03-31
  3. AD 2016-25-12 Airworthiness Directives; M7 Aerospace LLC 2016-12-08
  4. AD 2016-15-02 Airworthiness Directives; M7 Aerospace LLC Airplanes 2016-07-22
  5. AD 2016-10-01 Airworthiness Directives; M7 Aerospace LLC Airplanes 2016-05-11

All Fairchild SA226/SA227 Metro directives

Applies to 1 model in our index