AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 97-24-05 62 FR 62514 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitively inspecting the aft wing break connectors for arcing damage, deposits between contacts, and looseness of contacts; and removing deposits between contacts, tightening any loose contacts, and replacing any aft…

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
97-30719
Amendment
39-10212
Published
1997-11-24
Effective
1998-01-06
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/97-24-05 · 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

97-24-05

FR doc 97-30719 · 62 FR 62514

AD 97-24-05Published 1997-11-24Effective 1998-01-06

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 aft wing break connectors for arcing damage, deposits between contacts, and looseness of contacts; and removing deposits between contacts, tightening any loose contacts, and replacing any aft wing break connectors with arcing damage.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Aerospace Technologies of Australia Pty Ltd. (ASTA) Models N22B, N22S, and N24A airplanes. This AD requires repetitively inspecting the aft wing break connectors for arcing damage, deposits between contacts, and looseness of contacts; and removing deposits between contacts, tightening any loose contacts, and replacing any aft wing break connectors with arcing damage. This AD results from several reports of uncommanded flap extensions and displays of incorrect stall warning indications on the affected airplanes. The actions specified by this AD are intended to prevent contamination in the aft wing break connectors, which could result in uncommanded flap extensions and incorrect stall warning indications with consequent loss of airplane control.

More directives for GAF Nomad N22 / N24

  1. AD 2010-11-06 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Mo... Effective 2010-07-06
  2. AD 2009-26-08 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Mo... Effective 2010-02-01
  3. AD 2006-21-12 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... Effective 2006-11-08
  4. AD 2005-10-24 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... Effective 2005-06-30
  5. AD 2004-06-10 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Ai... Effective 2004-04-28

All GAF Nomad N22 / N24 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (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