AD 2014-16-07

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Bombardier, Inc. Airplanes

AD Number
2014-16-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0129
FR Citation
79 FR 48968

Applicability

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

Unsafe Condition

Failure of the main landing gear (MLG) alternate extension system (AES) cam mechanism, which may lead to improper operation or rupture of the door release cable, resulting in loss of control of the airplane during landing.

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

Required Actions

Conduct new repetitive inspections for proper operation of the MLG AES cam mechanism assembly. Replace the MLG AES cam mechanism assembly with a new assembly to terminate repetitive inspections.

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

Compliance Time

Within 12 months of the effective date (September 23, 2014).

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

Affected Aircraft

Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes with specific MLG AES cam mechanism assembly part numbers.

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

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