AD 89-14-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | ATR - GIE Avions de Transport R gional | ATR42-300 | Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes |
| aircraft | ATR - GIE Avions de Transport R gional | ATR42-320 | Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes |
Unsafe Condition
Failure of the emergency exit frame
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Accomplish modification of the fuselage emergency exit frame in accordance with Aerospatiale Service Bulletin ATR42-53-0024, Revision 2. An alternate means of compliance or adjustment of the compliance time may be used if approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 12,000 landings or within 60 days after the effective date of this AD, whichever occurs later
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
AEROSPATIALE Model ATR42-300 series airplanes, Serial Numbers 003 through 052
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.