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Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes

airworthiness · Rule · Final rule. · Published 2005-04-07 · Effective 2005-05-12 · 70 FR 17594

Document

Document number
05-6687
Federal Register citation
70 FR 17594
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-04-07
Effective date
2005-05-12
FAA docket
Docket No. FAA-2005-20222

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and-315 airplanes. This AD requires revising the airplane flight manual to include applicable procedures to follow when the flightcrew receives abnormal indications of airspeed, altitude, or vertical airspeed. This AD also requires modifying the static system. This AD is prompted by a report of a leak in the static pressure system, which could result in loss of the static systems and consequent erroneous data displayed on the pilot's flight instruments. We are issuing this AD to advise the flightcrew of applicable procedures in the event of abnormal indications of airspeed, altitude, or vertical airspeed; and to prevent leaks in the static system, which could result in the loss of critical flight information that could result in reduced controllability of the airplane or controlled flight into terrain.

Source

Authoritative
Federal Register document
Machine
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