[b[)[iUBDrJU
11m
DUAL
GENERATOR
FAILURE
(CONT)
3-10
•
On
aircraft 35-107, 35-113 and subsequent, and 36-032
and subsequent,
the emergency pressurization valves
will
reposition
to
emergency. Bleed-air for wing, windshield, and
stabilizer anti-ice as
well
as temperature control
will
not be
available. Pressurization AUTO mode
will
not
be
affected.
e. Autopilot
and
yaw dampers
will
be inoperative.
f.
The
jet
pwnps
wiD
supply fuel
to
the engines. Fuel system
valves
will
remain in their last position.
g. Fuel Quantity, Fuel Row,
and
Fuel Counter indicators
wiD
be
inoperative.
h. Mach Trim
and
stick puller will be inoperative.
Do
not
exceed
MMo
(0.74
MJ).
i.
All
AC electrical
systems
will
be
inoperative.
j. Spoilers.will
be
inoperative.
k.
stan
warning system
will
be
inoperative. Maintain adequate
margin above
stall
speed by reference
to
the airspeed indicator.
l.
Engine fire detect and extinguishing systems
wiD
be
inoperative.
m. Nose
wheel
steering and anti-skid
wiD
be inoperative for
land-
ing. Refer
to
Section V for increased landing distance
requirements.
FAA
APPROVED
4-30-76
REISSUED
2-25-81. CHANGE
10
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