AD 95-08-05

final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A, and Model Avro 146-RJ70A, -RJ85A, and -RJ100A Series Airplanes

AD Number
95-08-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
94-NM-152-AD
FR Citation
Federal Register: April 18, 1995 (Volume 60, Number 74)

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited Avro 146-RJ100A Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A, and Model Avro 146-RJ70A, -RJ85A, and -RJ100A Series Airplanes
aircraft BAE Systems (Operations) Limited Avro 146-RJ70A Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A, and Model Avro 146-RJ70A, -RJ85A, and -RJ100A Series Airplanes
aircraft BAE Systems (Operations) Limited Avro 146-RJ85A Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A, and Model Avro 146-RJ70A, -RJ85A, and -RJ100A Series Airplanes
aircraft BAE Systems (Operations) Limited BAe 146-100A Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A, and Model Avro 146-RJ70A, -RJ85A, and -RJ100A Series Airplanes
aircraft BAE Systems (Operations) Limited BAe 146-200A Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A, and Model Avro 146-RJ70A, -RJ85A, and -RJ100A Series Airplanes
aircraft BAE Systems (Operations) Limited BAe 146-300A Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A, and Model Avro 146-RJ70A, -RJ85A, and -RJ100A Series Airplanes

Unsafe Condition

Fuel leaks from bolt positions on the rear spar attachment fitting at wing rib 2, leading to a subsequent fire.

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

Required Actions

Visually inspect for integrity of nuts, tightness of bolts, and fuel leaks of the outboard vertical row of fasteners at the left- and right-hand rear spar root joint attachment fittings. Repeat inspections at intervals not exceeding 4,000 landings. Repair suspect or leaking fasteners and reinstall fairing panels as specified in the service bulletin.

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

Compliance Time

Within 12 months after the effective date of this AD (May 18, 1995) for airplanes under paragraph (b). For airplanes under paragraph (a), within 12 months after May 21, 1990, with repeat inspections at intervals not exceeding 4,000 landings.

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

Affected Aircraft

British Aerospace Model BAe 146-100A, -200A, -300A, and Model Avro 146-RJ70A, -RJ85A, -RJ100A series airplanes listed in Avro International Aerospace Service Bulletin S.B. 57-33, Revision 3, dated September 16, 1994.

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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