AD 89-14-52

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model DHC-8 Series Airplanes

AD Number
89-14-52
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Inc. DHC-8-101 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-102 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-103 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-106 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-201 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-202 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-301 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-311 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes
aircraft Bombardier Inc. DHC-8-315 Airworthiness Directives; Boeing Model DHC-8 Series Airplanes

Unsafe Condition

Asymmetric flap deployment due to chafing damage/wear exceeding 0.010 inch in depth or 180 degrees of the circumference on flap drive primary torque tubes, and interference between cooling ducts and torque tubes.

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

Required Actions

Within 25 hours time-in-service after the effective date, visually inspect torque tubes for wear/damage and replace if exceeding limits; inspect cooling ducts for interference, reposition to provide 0.3 inch clearance, repair broken reinforcement wires and replace within 30 days; perform torque sensor operational check per Maintenance Program Task 2750/11. Submit findings report within 7 days. Alternate compliance may be approved.

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

Compliance Time

Within the next 25 hours time-in-service after the effective date of this AD

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

Affected Aircraft

De Havilland Model DHC-8 series airplanes, Serial Numbers 3 and subsequent

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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