B737 FC TRAINING FLASHCARDS

Lenght : 129ft 6inches (39.5m)

Height : 41ft 3inches (12.5m)

Span: 112ft 7inches (34.4m)

Min width to turn the airplane is aprox 77ft (23m)

MZFW : 136,000 lbs 

MTW : 156,000 lbs

MTOW : 155,500 lbs

MLW : 144,000 lbs

CFM56-7

Hight by-pass ration, Electronice Engine control system, EEC

• 22,000 - 26,000 lb thrust
• 90kVA generators
• 61 inch fan diameter

Short to Medium range

41,000 ft 

0.82 Mach 

• Electrical power to 41,000
• Bleed air to 17,000
• Both to 10,000 

• 3 tanks
• no.1 main -8630 lb
• no2. main -8630 lb
• Center -28,000 lb
• Total : 46,063 lb 

• 184 Pax one class
• 160 Pax mixed class 

• VHF
• HF Optional
• Data Link 

25hr of last Operation 

BEFORE&AFTER START, BEFORE TO, SHUTDOWN,

• SECURE Chekclists - FO challenges, CPT responds
• AFTER TO, DESCENT-APP, LANDING Checklists - Pilot Not Flying PNF Challenges and responds
• When a CL stops you say - HOLDING AT.... 

• Priority of Actions
• 1) Control airplane
• 2) Stop aural warning
• 3) Examine the situation
• 4) Reset master caution system
• 5) Make sure steps completed correctly
• 6) Start the checklist
• 7) Say \"Checklist Complete\" 

• Flight crew enters the fault description and fault code. Includes :
• -Cabin faults, Observed faults, Front matter 

The maintenance crew uses FIM, to isolate and correct the faults 

Before using FRM , flight crew must do all the applicable non-normal checklist procedures 

Air condt. Pneumatic Syst. Electrical Syst. 

Crew Oxygen, IDG oil, Engine oil, Fuel, Hydraulic, Potable Water, waste water, APU oil 

All landing gear downlock pins must be installed when parked or towed. The nose landing gear steering must be depressurized before towing. 

115V 400Hz for aircraft systems, 115V 60Hz for cabin systems 

The reservoir servicing can be done between 5-30 mins after engine shutdown. (Reserv. on the right side of eng cowling)IDG is on the left side of eng cowling 

737 Fueled and defueled at the single-point station on the right wing 

Nose wheel steering is depressurised with the towing lever. Downlock pins are ery important. 

• Have 2 Packs, same type. Even one would be enough for cabin by itself.
• Warm air from bleed air -> Heat Exchangers -> Air Cycle Machine 

• The ram air doors are fully open while on ground and during slow flight with flaps extended. (For heat exchange)
• It has own light illumination on air condt panel 

To control the bleed air that goes into pack, you use the pack switches on air condt panel 

• The air from left pack first goes to the Flight Deck and rest goes to mix manifold.
• The air from right pack goes to mix manifold.
• From the mix manifold air goes to FWD and AFT Pax cabin

• Temperature control of 3 zones : Flight deck, FWD and AFT
• Pax cabin
• Trim air sys uses warm bleed air from upstream of the pack to warm up pack air for related zones 

Supply fan collects the cool air from Pax cabin and supllies it to cocpit displays and E&E bayExhaust fan collects the warm air from cocpit displays, CBs and E&E bay. On the GND its open and discards warm air. During flight it sends the warm air to cargo bay 

If downstream air temp from packs is too high we see the illumination : ZONE TEMP on the related Temp Controller/ We choose a colder selection and chechk the temperature change 

-Has an outflow valve on aft fuselage-2 digital cabin press. controllers in E&E bay-Adjust the cruise and landing ALT on overhead Press Panel before T/O

-Off-Schedule Descent-Diversion to Alternate Airport-Single controller failure-Dual cont fail-Cabin ALT higher then limits