AD 2014-19-02

final rule
Data completeness: 80%

Airworthiness Directives; Bombardier, Inc. Airplanes

AD Number
2014-19-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0144
FR Citation
79 FR 56264

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier, Inc. Airplanes

Unsafe Condition

Rudder bearings falling out of the fore rudder hinge bracket during assembly due to improper application of adhesive compound and lack of sealant, leading to abnormal wear, increased freeplay in the rudder system, airframe vibration, and potential compromise of flutter margins.

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

Required Actions

Perform a proof load test for slippage and freeplay. Conduct detailed inspections of the bearing for damage, corrosion, and dimension conformity, and of the fitting bore of the fore rudder hinge bracket for wear, damage, corrosion, and dimension conformity. Install a new bearing, ream, or repair the bearing as necessary.

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

Compliance Time

Before further flight

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

Affected Aircraft

Bombardier Model DHC-8-400, -401, and -402 airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.