AD 2011-18-18

final rule
Data completeness: 70%

Airworthiness Directives; Bombardier, Inc. Model DHC-8-400 Series Airplanes

AD Number
2011-18-18
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0471
FR Citation
76 FR 55785

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier, Inc. Model DHC-8-400 Series Airplanes
aircraft Aviat Various Airworthiness Directives; Bombardier, Inc. Model DHC-8-400 Series Airplanes

Unsafe Condition

Loose rivets in the torque tube assemblies cause relative motion between the crank arms and torque tubes, leading to excessive wear and significant backlash in the driving crank arms. This condition degrades the controllability of the airplane.

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

Required Actions

Inspect the part numbers of the left and right elevator torque tube assemblies. Replace the elevator torque tube assembly or the elevator torque tube rivets if necessary, and re-identify the assemblies.

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

Compliance Time

Within the compliance times specified in the AD, unless the actions have already been performed.

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; certificated in any category; serial numbers 4001 through 4305 inclusive.

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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