Airworthiness Directives; Fokker Model F.27 Mark 050 Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2009-03-24 · Effective 2009-04-08 · 74 FR 12238
Document
Document number
E9-5958
Federal Register citation
74 FR 12238
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Fokker Model F.27 Mark 050
Publication date
2009-03-24
Effective date
2009-04-08
FAA docket
Docket No. FAA-2009-0224
Abstract
The FAA is superseding an existing airworthiness directive (AD) that applies to certain Fokker Model F.27 Mark 050 airplanes. The existing AD currently requires repetitive visual checks for oil leaks of both engines between the spinner and the engine cowling, and directly behind the heated intake lip of the engine; repetitive inspections for oil leaks at the feathering pump on both engines; and corrective actions if necessary. This new AD retains the requirements of the existing AD. This AD also requires replacing the outlet port (high-pressure) bobbin with a new, improved outlet port (high-pressure) bobbin, which terminates the repetitive visual checks and inspections. This AD results from reports of oil leakage at the engine feathering pump. We are issuing this AD to prevent oil loss from the feathering pump, which could cause the engine to shut down in flight.