AD 69-22-01

final rule
Data completeness: 70%

Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Models BAC 1-11 200 and 400 Series Airplanes

AD Number
69-22-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus SAS BAC 1-11 200 Series Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Models BAC 1-11 200 and 400 Series Airplanes
aircraft Airbus SAS BAC 1-11 400 Series Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Models BAC 1-11 200 and 400 Series Airplanes

Unsafe Condition

Malfunction of the ventral stairway door due to looseness or insecurity of the starboard hinge bolt (M.M. 52-10).

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the ventral stairway starboard hinge bolt (M.M. 52-10) within the next 100 hours' time in service after the effective date unless already accomplished within the last 550 hours' time in service. Thereafter, repeat inspections at intervals not exceeding 650 hours from the last inspection. If the bolt is insecure or loose, secure it before further flight per BAC 1-11 Alert Service Bulletin 52-A-PM 3701 or FAA-approved equivalent.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the next 100 hours' time in service after the effective date of this AD unless already accomplished within the last 550 hours' time in service

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

BRITISH AIRCRAFT CORPORATION Models BAC 1-11 200 and 400 Series Airplanes

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

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