Quick reference handbook 737

What are you looking for? Preferences Community Newsletters Log Out. Download Now. The Handbook is an interactive technical guide for pilots which provides a quick reference for sim or interview preparation from initial type rating to command upgrade. The app features interactive schematics, photos and videos with unique content. The information is sorted in different levels from most essential information on the page to in-depth information in pop-up windows.

This enables you to choose the way you want to learn. Should you require quick reference you can go through the main text in the chapter. Should you, however, wish to explore the systems more in-depth you can do so by opening different pop-up windows, text and playing around with fully interactive schematics.

Try it out yourself! Push 3. Condition: A duct overheat occurs. Temperature selector…………… Select cooler temperature 2. Condition: The equipment cooling supply or exhaust fan is failed. Condition: The high altitude landing system is inoperative. Temperature selectors all ……….. Select warmer temperature 2. Descend to the lowest safe altitude, or 10, feet. Monitor cabin altitude and rate. Pressurization mode selector……………………………MAN 6. OPEN 7. AUTO 8. Condition: A pack overheat occurs. Pressurization mode selector……………………………MAN.

Condition: An overheat from a bleed duct leak occurs. CLOSE 2. R PACK switch………………………………………… OFF 4. BLEED 2 air switch…………………………………… OFF 5. L PACK switch………………………………………… OFF 7.

BLEED 1 air switch…………………………………… OFF 8. ON L PACK switch………………………………………. AUTO CLOSE BLEED 1 air switch……………………………………. L PACK switch…………………………………………. OFF Temperature selector…………….. Select a cooler temperature 2. Condition: An engine cowl anti-ice duct overpressure occurs.

If flight conditions allow: Autothrottle if engaged …………………………. Condition: One or more probe heats are failed. Avoid icing conditions. OFF 2. Wait 2 - 5 minutes. Condition: The wing anti-ice valve is not in the commanded position. Condition: All autopilots are disengaged. The red light flashes and the aural tone sounds. Fly the airplane manually or re—engage an autopilot. Condition: The autothrottle is disengaged. The red light flashes. Control thrust manually or re—engage the autothrottle.

Condition: A generator drive malfunction occurs. Condition: A standby power or DC system fault occurs. Condition: The transfer bus is not powered by the last selected source. Engine GEN switch affected side ……………………….. Only one main AC power source remains. Condition: One or more transformer rectifiers are failed.

Do not use the AFDS approach mode. Condition: The transfer bus is not energized. Condition: An APU malfunction occurs. APU switch………………………………………………. Condition: The APU oil pressure is low. Condition: An EEC operates in the alternate control mode.

Autothrottle if engaged ……… Thrust levers both Retard to mid position 3. EEC mode switches one at a time ……………………. Condition: An engine control system fault occurs. Do not takeoff. Autothrottle if engaged ………………………… Disengage 2. Thrust lever affected engine …………………………..

Close 3. PACK switch affected side …………………………….. Balance fuel as needed. AUTO 9. Thrust lever affected engine …………………………. Condition: An engine start is needed……………… Check the In-Flight Start Envelope. Starts are not assured outside of the in-flight start envelope. Thrust lever affected engine ………………………… Engine start lever affected engine ……………… IDLE detent 6.

AUTO Transponder mode selector………………………… Condition: Landing must be made with one engine inoperative. Plan a flaps 15 landing. Set VREF 15 3. Use engine anti-ice on the operating engine only. Condition: A fault occurs in the thrust reverser system. Expect normal reverser operation after landing. Condition: Fire is detected in the APU. APU fire switch……………………………………Pull, rotate 2. OFF 3. Condition: Fire is detected in the Engine 1.

Autothrottle if engaged ………………………. Engine start lever affected engine …………….. Engine fire switch affected engine …………… Rotate to the other side 6. CLOSE 7. Condition: An overheat is detected in the engine. Condition: Fire is detected in the related cargo compartment. Condition: Flap load relief occurs. Check flap position and maintain the appropriate airspeed. Condition: Hydraulic system pressure to the ailerons, elevators and rudder is low. Condition: The yaw damper is disengaged.

Condition: A display in the common display system is failed. As needed 3. If the DEU fails on the same side as the engaged autopilot: Select the opposite autopilot. Condition: An alert message is in the FMC scratchpad. Take action as needed by the message.