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L or R ELEV PITOT Light:
Inputs to the elevator feel computer may be affected resulting in the
illumination of the FEEL DIFF PRESS light.
L or R ALPHA VANE Light:
Angle-of-Attack input to the stall warning system, autothrottle, and/or
autopilot may be affected.
TEMP PROBE Light:
Inputs to ADC 1 or ADC 2 may be affected. The TAT indicator may be
unreliable.
F/O P/S, 2 AUX STATIC Light:
Inputs to the First Officer’s Mach / Airspeed indicator, altimeter, and IVSI
may be unreliable. Alternate static source inputs to ADC 2 are not affected.
CAPT STATIC, 1 AUX P/S Light:
Inputs to the flap load limit airspeed switch, pressurization control, cabin
altitude indicator, and cabin differential pressure indicator may be affected.
* * * *
737
Flight Manual
Continental
ANTI-ICE, RAIN
Sec. 2.3 Page 5
Rev. 11/15/02 #41
OR
BCD TAI INDICATION
This condition is recognized by an amber TAI indication. This indicates that
the cowl valve is in disagreement with the engine anti-ice switch position.
IF Open Position:
IF Total Air Temperature Is Above 10°C:
Limit thrust of the affected engine to 80% N1 or less if possible.
* * * *
IF Closed Position:
Avoid icing conditions.
* * * *
WINDOW OVERHEAT
The OVERHEAT light illuminated indicates that the window heat has automatically
been removed from the window.
Window Heat Switch (Affected Window)................................................OFF
Positioning the WINDOW HEAT switch to OFF extinguishes the OVERHEAT light
and resets the system.
After 2 to 5 Minutes:
Window Heat Switch....................................................................................ON
IF The Window OVERHEAT Light Re-Illuminates:
Window Heat Switch...........................................................................OFF
Limit airspeed to 250 knots maximum below 10,000 feet.
Windshield Air Controls ..................................................................PULL
Vents conditioned air to the inside of the windshield for defogging.
* * * *
ANTI-ICE, RAIN
Sec. 2.3 Page 6
Rev. 11/15/02 #41
Continental
737
Flight Manual
WING ANTI-ICE VALVE FAILURE
This condition is recognized by the L and/or R VALVE OPEN lights illuminated
bright blue in flight. This indicates that the left and/or right wing anti-ice
valve is in disagreement with the wing anti-ice switch position.
IF Open Position And OAT (ground) – TAT (airborne) Is Above
10°C/50°F And No Visible Moisture:
Isolation Valve Switch............................................................CLOSE
Prevents the isolation valve from opening in the following
procedural step.
Pack Switch (Affected Side) .......................................................OFF
Engine Bleed Air Switch (Affected Side) ..................................OFF
Prevents unwanted wing anti-ice operation.
* * * *
IF Closed Position:
Avoid icing conditions.
* * * *
OR
737
Flight Manual
Continental
AUTOMATIC FLIGHT
Sec. 2.4 TOC-1
Rev. 11/15/02 #41
2.4 – AUTOMATIC FLIGHT
TABLE OF CONTENTS
AUTOPILOT DISENGAGE..................................................................... 1
AUTOTHROTTLE DISENGAGE............................................................ 1
AUTOMATIC FLIGHT
Sec. 2.4 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
AUTOMATIC FLIGHT
Sec. 2.4 Page 1
Rev. 11/15/02 #41
AUTOMATIC FLIGHT
AUTOPILOT DISENGAGE
Condition: The flashing red A/P light illuminated and the aural tone sounding
indicates the autopilot has disengaged.
Fly the aircraft manually or re-engage an autopilot.
AUTOTHROTTLE DISENGAGE
Condition: The flashing red A/T light illuminated indicates the autothrottle
has disengaged.
Fly the aircraft manually or re-engage the autothrottle.
AUTOMATIC FLIGHT
Sec. 2.4 Page 2
Rev. 11/15/02 #41
Continental
737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
COMMUNICATIONS
Sec. 2.5 TOC-1
Rev. 11/15/02 #41
2.5 – COMMUNICATIONS
TABLE OF CONTENTS
ACARS ELECTRICAL POWER LOSS .................................................. 1
ACARS MU FAIL OR CU FAIL ............................................................... 1
COMMUNICATIONS
Sec. 2.5 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
　
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