AD 82-12-02 R1

final rule
Data completeness: 70%

Airworthiness Directives; BRITISH AEROSPACE (HAWKER SIDDELEY) Model HS/BH/DH 125 Airplanes

AD Number
82-12-02 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Unsafe Condition

Structural failure of the flap due to cracks in the flap outboard hinge nose ribs.

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

Required Actions

Visually inspect the flap outboard hinge nose ribs for cracks per SB No. 57-58, Rev 3. If cracks exceed criteria, reinspect at intervals not exceeding 40 hours time in service or replace flap/contact manufacturer for permanent repair before further flight. Allow special flight permits under FAR 21.197/21.199.

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 June 17, 1985, or before 600 hours time in service on the airplane, whichever is later.

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

Affected Aircraft

British Aerospace Model HS/BH/DH 125 up to and including series 700 airplanes except those with Modification 252772.

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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View Official Source ↗