AD 69-12-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-28R-180 | Airworthiness Directives; Piper Models PA-28R-180 Series and PA-28R-200 Series Airplanes |
| aircraft | Piper Aircraft Inc. | PA-28R-200 | Airworthiness Directives; Piper Models PA-28R-180 Series and PA-28R-200 Series Airplanes |
Unsafe Condition
Deterioration, broken or frayed cord wrapping, collapsed hose, reinforcement wire slippage, or improper wire bonding in the engine air induction system's inlet hose (Piper P/N 63633-43) could restrict air flow.
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Required Actions
Within 10 hours' time in service after the effective date, inspect the air induction inlet hose for specified defects. If defects are found, replace with an approved hose or install Piper Kit 760 328. Install Piper Kit 760 328 within 50 hours' time in service. Repeat inspections every 10 hours until the kit is installed.
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Compliance Time
Within the next 10 hours' time in service after the effective date of this airworthiness directive (for initial inspection) and within the next 50 hours' time in service for kit installation. Inspections must be repeated every 10 hours until the kit is installed.
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Affected Aircraft
Piper Models PA-28R-180 (Serial Numbers 28-30004 through 28-31092) and PA-28R-200 (Serial Numbers 28-35000 through 28-35237, 28-35239 through 28-35251, and 28-35253 through 28-35256).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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