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Harmonization of Airworthiness Standards for Transport Category Airplanes-Landing Gear Retracting Mechanisms and Pilot Compartment View

other · Rule · Final rule. · Published 2012-01-11 · Effective 2012-03-12 · 77 FR 1614

Document

Document number
2012-360
Federal Register citation
77 FR 1614
Type
Rule
Action
Final rule.
Category
other
Publication date
2012-01-11
Effective date
2012-03-12
FAA docket
Docket No. FAA-2010-1193

Abstract

The Federal Aviation Administration amends the airworthiness standards for transport category airplanes on landing gear retracting mechanisms and the pilot compartment view. For the landing gear retracting mechanism, this rulemaking adopts the 1-g stall speed as a reference stall speed instead of the minimum speed obtained in a stalling maneuver and adds an additional requirement to keep the landing gear and doors in the correct retracted position in flight. For the pilot compartment view, this rulemaking revises the requirements for pilot compartment view in precipitation conditions. This action eliminates regulatory differences between the airworthiness standards of the U.S. and the European Aviation Safety Agency (EASA), without affecting current industry design practices.

Source

Authoritative
Federal Register document
Machine
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