AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 95-19-15 60 FR 48628 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-23219
Amendment
39-9377
Published
1995-09-20
Effective
1995-11-17
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/95-19-15 · 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

95-19-15

FR doc 95-23219 · 60 FR 48628

AD 95-19-15Published 1995-09-20Effective 1995-11-17

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 wing attach shoulder bolts for fretting, scoring, wear, or enlarged or elongated mounting holes (known as damage from hereon), and replacing any damaged parts and repairing any damaged areas; and…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to American General Aircraft Corporation (American General) Models AA-5, AA-5A, AA-5B, and AG-5B airplanes. This action requires inspecting the wing attach shoulder bolts for fretting, scoring, wear, or enlarged or elongated mounting holes (known as damage from hereon), and replacing any damaged parts and repairing any damaged areas; and inspecting the wing spar at the center spar clearance gap for excessive clearance, and shimming the spar if excessive clearance is found. The actions specified by this AD are intended to prevent wing attach shoulder bolt failure, which, if not detected and corrected, could lead to structural damage to the wing/fuselage to the point of failure.

More directives for Grumman AA-5

  1. AD 2021-14-12 Airworthiness Directives; True Flight Holdings LLC Airplanes 2021-07-12
  2. AD 95-19-15 R1 Airworthiness Directives; Tiger Aircraft LLC Models AA-5, AA-5A, AA-5B, ... 2005-08-22

All Grumman AA-5 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