AD 98-12-27
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | ATP | Airworthiness Directives; British Aerospace BAe Model ATP Airplanes |
Unsafe Condition
Cracking of the splined operating shaft of the internal door handle on the forward passenger door, rear passenger door, and rear baggage door could result in failure of the internal door handle, inability to operate the door during an emergency evacuation, and consequent injury to airplane occupants.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a magnetic particle inspection to detect cracking of the splined operating shaft of the internal door handles on specified doors, or replace the shaft with a new one per the service bulletin. Repeat inspections at intervals not exceeding 1,000 flight cycles after initial inspection or replacement.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 2,000 flight cycles on the splined operating shaft 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
BAe Model ATP airplanes, constructor’s numbers 2002 through 2067 inclusive; certificated in any category.
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.