• Home
  • Download PDF
  • Order CD-ROM
  • Order in Print
GO AROUND WITH BOTH PILOTS' TRIM SYSTEM INOPERATIVE
PRESSURIZATION SYSTEMS.

Operator and Crewmember Checklist for C-26E Aircraft
Page Navigation
  58    59    60    61    62  63  64    65    66    67    68  
img
TM 1-1510-253-CL
NOTE
With SAS servo turned off, stick pusher
will be inoperative. Stall warning will still
be provided by activation of stickshakers
5 to 10 knots above stall speed. Angle of
attack should be immediately reduced to
provide an adequate margin above stall
speed. If angle of attack isinadvertently
allowed to increase, stall recovery should
be initiated at first natural or SAS indica-
tion of stall (glareshield stall light and/or
stall horn).
1. ELEVATOR -- Overpower
2. MASTER DISCONNECT -- Press and
Hold
3. SAS SERVO SWITCH -- OFF
4. MASTER DISCONNECT -- Release
INADVERTENT STALL WARNING
Stick Shaker or stall warning at speeds well above
normal stall warning speeds
NOTE
Pressing either stall light module will
remove power immediately from re-
spective SAS computer and render
SAS pusher servo inoperative. Pilot's
stall light module controls left SAS
computer and copilot's light module
controls right SAS computer.
Both stall warning stick shakers, stall
horn, and glareshield STALL lights for
operating SAS computer will be oper-
ational. Stick pusher will not operate
with either SAS computer off.
1. STALL LIGHT MODULE (either SAS) --
Press OFF
E-40


Privacy Statement
Press Release
Contact

© Copyright Integrated Publishing, Inc.. All Rights Reserved.