FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 23 > Section 1155 - Turbine engine reverse thrust and propeller pitch settings below the flight regime
section 23.1153 |
section 23.1157
For turbine engine installations, each control for reverse thrust and for propeller pitch settings below the flight regime must have means to prevent its inadvertent operation. The means must have a positive lock or stop at the flight idle position and must require a separate and distinct operation by the crew to displace the control from the flight regime (forward thrust regime for turbojet powered airplanes).
[Amdt. 23-7, 34 FR 13096, Aug. 13, 1969]
   
Current page: FARs > Part 23 > Section 1155 - Turbine engine reverse thrust and propeller pitch settings below the flight regime
section 23.1153 |
section 23.1157
page stats: viewed 3292 unique times - last change 07-Jan-2005
» DOWNLOADING (PARTS OF) THIS WEBSITE AUTOMATICALLY IS NOT ALLOWED! «
THIS IS NO OFFICIAL SOURCE --
[DISCLAIMER]
[FAA WEBSITE]
See also:
AIM | ATC | FSS | NOTAMS | PCG | |
![[FAR Part § 23.1155: Turbine engine reverse thrust and propeller pitch settings below the flight regime -- FAA FARS, 14 CFR] -- Flightsim Aviation Zone - Number 1 Flight Simulation and Aviation Resource! Information, Tools, Downloads, Databases, FAQ, Aviation Humour, Glossaries, Directory, FS2006, Multimedia, Screenshots, Free Flight Planner, Weather Reports](/images/gui/header_logo.gif){kind=logo}
add
to favorites
Link
to this!