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· A/C Pack Valves
· PACK TRIP OFF Lights
APU
· APU Operation ( >>@ start attempts not recommended above
25,000 ft.)
Communications
· Flight Interphone System
· Passenger Address System
· VHF No.1
· Audio Selector Panels
Electrical
· External Power Control
· APU & Engine Generator Power Control
· STANDBY POWER OFF Light
· TRANSFER BUS OFF Light
· GEN OFF BUS Light
>>@
· OFF BUS Light
BCD
· SOURCE OFF Light
ELECTRICAL
Sec. 2.6 Page 10
Rev. 11/15/02 #41
Continental
737
Flight Manual
Emergency Equipment
· Flight Crew Oxygen
· Passenger Oxygen
Fire Protection
· APU & Engine Fire Ext. Bottles
· APU & Engine Fire Detection System
Flight Instruments
· Standby Airspeed / Altimeter
· Standby Horizon Indicator
· Clocks
· Magnetic Compass
· Captain’s RDMI
>
· Captain’s ADI & HSI
BCD
· Captains Inboard Display Unit
· Altimeter, Vertical Speed
· Indicator, Navigation Display
· Captain’s Outboard Display Unit
Mach / Airspeed Indicator, Attitude Indicator, Altimeter, Vertical Velocity
Indicator, HSI
· Standby RMDI
· Left EFIS Control Panel
Fuel
· Crossfeed Valve
· Engine Fuel Shutoff Valve
· Fuel Quantity Indicator
· Fuel FILTER BYPASS Light
>>@
· FUEL VALVE CLOSED Light
BCD
· Spar fuel Shutoff Valve
· SPAR VALVE CLOSED Light
· ENG VALVE CLOSED Light
737
Flight Manual
Continental
ELECTRICAL
Sec. 2.6 Page 11
Rev. 11/15/02 #41
Hydraulic Power
· Engine Hydraulic Shutoff Valve
· Standby Rudder Shutoff Valve
Landing Gear
· Inboard Antiskid System
· ANTISKID INOP Light
· Parking Brake
· Landing Gear Position Lights
Navigation / Flight Management
· Left IRS
· VHF No. 1
>>@
· ADF No. 1
BCD
· Left GPS
· Left FMC
· Left CDU
· Marker Beacon
Pneumatics
· BLEED TRIP OFF Lights
Pressurization
· Manual Pressurization Control
· Altitude Warning Horn
Engines
· Thrust Reversers
· Starter Valves
· Right Igniters
>>@
· N1 & EGT Indications
· Indications
· LOW OIL PRESSURE Light
· START VALVE OPEN Light
ELECTRICAL
Sec. 2.6 Page 12
Rev. 11/15/02 #41
Continental
737
Flight Manual
BCD
· Upper display unit
N1, N2, fuel flow, EGT, fuel quantity, oil pressure, oil temperature, oil
quantity, hydraulic pressure, hydraulic quantity
Warnings
· Stall Warning System
· Aural Warnings
· Master Caution Light Recall
737
Flight Manual
Continental
ELECTRICAL
Sec. 2.6 Page 13
Rev. 11/15/02 #41
LOSS OF BOTH ENGINE GENERATORS CHECKLIST
Loss of both engine driven generators is indicated by instrument warning flags,
master caution system, and by illumination of:
>>@ TRANSFER BUS OFF, BUS OFF, and GEN OFF BUS lights.
BCD TRANSFER BUS OFF, SOURCE OFF, and GEN OFF BUS lights.
Upon the failure of all generators, the electrical system will automatically switch
to standby power when airborne. The Captain's essential radios, navigation
equipment, and flight instruments are powered through the standby system.
Note: With main tank fuel pumps inoperative above 30,000 feet, thrust
deterioration or engine flameout may occur.
BCD Note: Reversion to Standby power may cause the Barometric
setting to revert to Standard. Reset as necessary.
Bus Transfer Switch...................................................................................OFF
Prevents high electrical loads during attempts to restore power.
Electric Hydraulic Pump Switches...........................................................OFF
Prevents high electrical loads during attempts to restore power.
No. 2 Generator Switch................................................................................ON
No. 1 Generator Switch................................................................................ON
IF One Or Both >>@ BUS OFF BCD SOURCE OFF Lights
Remain ON:
　
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