AD 87-14-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | DHC-8-101 | Airworthiness Directives; DEHAVILLAND Models DHC-8-101 and DHC-8-102 Series Airplanes |
| aircraft | Bombardier Inc. | DHC-8-102 | Airworthiness Directives; DEHAVILLAND Models DHC-8-101 and DHC-8-102 Series Airplanes |
Unsafe Condition
Failure of the main landing gear yoke pin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect both main landing gears to determine the yoke pin part number and reidentify the shock strut as necessary. Replace yoke pin P/N 10150-3 with P/N 10150-5 prior to specified flight limits based on model.
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Compliance Time
Within 25 landings after the effective date of this AD. For Model DHC-8-101 airplanes: prior to the accumulation of 5,500 flights since installation of the yoke pin. For Model DHC-8-102 airplanes: prior to the accumulation of 4,700 flights since installation of the yoke pin.
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Affected Aircraft
Bombardier Inc. Models DHC-8-101 and DHC-8-102 series airplanes, serial numbers 3 through 83.
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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