AD 98-07-06

final rule
Data completeness: 70%

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

AD Number
98-07-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-NM-163-AD
FR Citation
This information is not available.

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-RJ 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-RJ 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-RJ 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-RJ 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-RJ 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-RJ Series Airplanes

Unsafe Condition

Reduced structural integrity of the stabilizer attachment brackets due to intergranular corrosion, which could result in reduced controllability of the airplane.

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

Required Actions

Perform repetitive inspections of the attachment brackets between the horizontal and vertical stabilizers to detect intergranular corrosion, following British Aerospace Service Bulletin SB.55-15. If corrosion is found, blend out corrosion and re-protect areas, or repair if beyond limits. Apply additional surface protection after inspections. Repeat inspections every 12,000 flight cycles or 4 years, whichever comes first.

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

Compliance Time

Within 20, 32, or 44 months after May 4, 1998, depending on the airplane's constructor number as specified in the service bulletin. Repeat inspections at intervals not exceeding 12,000 flight cycles or 4 years after the initial inspection, whichever occurs first.

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 Avro 146-RJ70A, -85A, -100A airplanes with constructor numbers: BAe 146 models (all), Avro 146-RJ70/70A up to E1267, Avro 146-RJ85/85A up to E2300, and Avro 146-RJ100/100A up to E3301.

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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