AD 2013-22-08

Recurring final rule
Data completeness: 70%

Airworthiness Directives; BAE Systems (Operations) Limited Airplanes

AD Number
2013-22-08
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2013-0631
FR Citation
78 FR 65204

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited Airworthiness Directives; BAE Systems (Operations) Limited Airplanes

Unsafe Condition

Cracked pick-up bracket of the forward outboard pylon of the number 1 engine due to stress corrosion, which could result in the engine pylon separating from the wing.

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

Required Actions

Perform repetitive inspections with a videoscope of the flanges of the Rib 10 forward pylon pick-up bracket for cracking, corrosion, and other defects. Repair or replace the bracket if any defects are found.

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

Compliance Time

Within 6 months after the effective date of the AD, or within 20 months if both forward pylon pick-up brackets have been replaced since first flight.

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

Affected Aircraft

BAE Systems (Operations) Limited Model BAe 146-100A, -200A, and -300A airplanes; and Model Avro 146-RJ70A, 146-RJ85A, and 146-RJ100A airplanes, all serial numbers.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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