AD 92-10-04

final rule
Data completeness: 70%

Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes

AD Number
92-10-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-NM-261-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. BH.125 Series 400A Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. BH.125 Series 600A Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A-522 Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A/R-522 Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 1A/S-522 Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 3A Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 3A/R Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 3A/RA Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes
aircraft Textron Aviation Inc. DH.125 Series 400A Airworthiness Directives; BRITISH AEROSPACE Model DH/BH/HS 125 Series Airplanes

Unsafe Condition

Reduced structural integrity of the wings due to corrosion beneath the boundary layer fence on the wing upper skins.

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

Required Actions

Visually inspect left and right wing upper skins for corrosion beneath the boundary layer fence within 3 months after the effective date. Repair corroded parts within specified limits per SB 57-73 prior to further flight; repair exceeding limits requires an approved method. Submit inspection findings report within 10 days post-inspection.

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

Compliance Time

Within 3 months after the effective date of this AD

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

Affected Aircraft

Model DH/BH/HS 125 series airplanes excluding Model 125-700A, -800A, and -1000A series, as listed in British Aerospace Service Bulletin S.B. 57-73 dated July 30, 1991.

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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