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Master Warning Light Panel
L/R OIL PRESS
Oil pressure < 15 psi
- 1. Check Gauge & Throttle position
- 2. Advance throttle to restore pressure
- 3. If pressure can't be restored within limits - Shut down engine
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Master Warning Light Panel
L/R ENG HOT
Cooling Air > 860° F
BOLDFACE (On Ground)- 1. THROTTLE - IDLE P
- 2. FUEL COCK - SHUT P
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Master Warning Light Panel
GND SPOILER
- INFLIGHT
- 1. 1 or both Ground Spoiler Panels extended w/ Speed Brake not EXTENDED
- 2. Primary Control Valve failure
- 3. Secondary Control Valve failure
- 4. Primary or Secondary Nutcracker Relay failure
- ON GROUND
- 1. Primary Control Valve failed w/ throttles out of Idle
- 2. Unlocked Ground Spoilers w/ throttles at Take Off Power
- 1. Ground Spoiler Switch OFF
- 2. Pull Ground Spoiler CB (P, C9)
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Master Warning Light Panel
REV UNLOCK
Thrust Reverser Overcenter Links have moved Overcenter towards Deploy position
- 1. Throttle - Idle
- 2. Reverser Lever - Stow
- 3. Reverser Switch - Restow
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Master Warning Light Panel
L/R FUEL PRESS
Fuel pressure < 15 psi at inlet of HP Pump
- Due to:
- 1. Boost Pump failure
- 2. Crossflow and Boost Pump mismanagement
- 3. Fuel Leak
Check Boost Pumps & Crossflow Valve
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Master Warning Light Panel
L/R PYLON HOT
Pylon Air > 325° F
Possible Bleed Air leak
- BOLDFACE
- 1. BLEED AIR SWITCHES - OFF P
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Master Warning Light Panel
AFT EQUIP HOT
Aft Equipment Compartment temperature > 200° F
- 1. HP Duct has blown off
- 2. Fire is in progress
- BOLDFACE
- 1. BLEED AIR SWITCHES - OFF P
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Master Warning Light Panel
CABIN DOORS
Main and/or Baggage Door Not Locked
- Reduce Cabin Pressure Differential
- - Cabin Altitude < 10,000 Feet
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Master Warning Light Panel
CAB PRESS LO
Cabin Altitude > 9,250 ±750 Feet
- 1. Check Cabin Pressure Indicator and Controls
- 2. Descend as Necessary
- 3. Use Oxygen as Appropriate
- 4. Select Emergency Pressurization
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Master Warning Light Panel
CABIN PRES MAN
Pressure Controller in Manual Mode
- Occurs if:
- 1. AUTO/MAN Switch to MANUAL
- 2. Depressurization Rate Limiting Occurs
- 3. Phase A CB on PDB is open
- 4. Battery only operation
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Master Warning Light Panel
L/R FUEL FILT
Fuel filter clogged and DP of .3 across filter is sensed
- Shut down engine if FUEL FLOW begins to FLUCTUATE
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Master Warning Light Panel
L/R BLEED HT
Bleed Air after Precooler > 550° F
- Turn Affected Side Bleed Air Switch OFF
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Master Warning Light Panel
BATT SW OFF
BATT 1 and/or BATT 2 Switch is Off
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Master Warning Light Panel
CAB OXY ON
- Cabin Altitude > 13,500 Feet
- Oxygen Masks Deployed
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Master Warning Light Panel
BLEED PRESS
Bleed Air > 90 psi
Probably a failure of a HP regulator valve
- Select Bleed Air Switch OFF for Engine w/ Lowest EPR & Highest TGT
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Master Warning Light Panel
FUEL LOW LVL
Fuel in Either Fuel Hopper is < approximately 700 lbs
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Master Warning Light Panel
L/R CONV HT
Converter Temperature > 220° F
- Power Master Switch - OFF
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Master Warning Light Panel
AV INV 1 FAIL
- 1. Avionics Inverter #1 Failed
- Or
- 2. Essential DC Power Loss
- Equipment now powered by Essential AC Bus
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Master Warning Light Panel
AV INV 2 FAIL
- 1. Avionics Inverter #2 Failed
- Or
- 2. Right Main DC Bus Power Loss
Equipment now powered by Right Main AC Bus
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Master Warning Light Panel
L/R DC PWR
DC Converter Output Offline
- Power Master Switch – OFF / ON
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Master Warning Light Panel
L/R ALTNTR HT
Alternator Case Temperature > 250° F
- Power Master Switch for respective alternator - OFF
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Master Warning Light Panel
L/R PITOT HT
Pitot Heat not Energized
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Master Warning Light Panel
L/R AC PWR
AC Converter Output Offline
Power Master Switch - OFF/ON
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Master Warning Light Panel
T/R HT
Transformer Rectifier Temperature > 374° F
- 1. Check Cooling Fan Screen
- 2. Reduce L/R DC load to < 250 amps
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Master Warning Light Panel
APU ALT HT
APU Alternator Case Temperature > 300° F
Aux Power Master Switch - OFF
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Master Warning Light Panel
TONE GEN
Tone Generator Failed
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Master Warning Light Panel
TRANS/RECT
Transformer Rectifier Selected ON but there is not TRU Output
Ensure L/R Main AC Bus is powered
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Master Warning Light Panel
AUX AC PWR
AUX/APU Power Source Offline
Aux Power Switch OFF then ON
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Master Warning Light Panel
COMB HYD HT
Combined Hydraulic Fluid Temperature > 220° F
Proceed w/ flight, investigate after landing
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Master Warning Light Panel
FLT HYD HT
Flight Hydraulic Fluid > 200° F
Proceed w/ flight, investigate after landing
- If Utility Hydraulic System is needed, Flight Hydraulic System Switch must be in OVERRIDE
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Master Warning Light Panel
AUX MASTER WARN CB
- Loss of Power to:
- 1. 1 or more of the 16 AUX MAST WARN CBs
- 2. Either Master Warning 1 or 2 Power CBs
Check CBs (P, L2 & M2)
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Master Warning Light Panel
EPMP PS
- 1 of the 4 Power Sources has failed:
- 1. EDC Bus (2)
- 2. BATT 1
- 3. BATT 2
Check CBs (CP, F3 & F4)
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Master Warning Light Panel
COMB HYD
Combined Hydraulic System Pressure < 800 psi
- No Fluid Loss:
- Check Flight Hydraulic System pressure at 3000 psi (if not, pull Flight Hyd CB (P, B9))
- Fluid Loss:
- 1. If flaps suspected, pull Manual Flap Control CB (P, G9)
- 2. Check Flight Hydraulic System pressure at 3000 psi (if not, pull Flight Hyd CB (P, B9))
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Master Warning Light Panel
FLT HYD
Flight Hydraulic System Pressure < 800 psi
Check Combined Hydraulic System pressure at 3000 psi (if not pull Combined Hyd CB (P, D10))
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Master Warning Light Panel
AUX HYD HT
Aux Hydraulic System Case Temperature > 300° F
Limit use of pump
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Master Warning Light Panel
RADIO RACK HT
Radio Rack Area Temperature > 200° F
Check Cooling Fan Screen
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Master Warning Light Panel
STAB-FLAP
Flaps Up, Stab is Not
Refer to Stab/Flap Interconnect Failure
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Master Warning Light Panel
TRIM OFF
Electric Trim Inoperable
Check Pitch Trim Switch
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Master Warning Light Panel
ANTI-SKID
System Failure
Anti-Skid Switch OFF then ON
- On Ground:
- 1. MIN EPR Take Off
- 2. Anti-Ice OFF (Eng & Wing)
- 3. Flaps 20° Take Off
- 4. Adjust TOLD
- 5. Ground Spoilers Operable
- 6. Switch - ON for Take Off / OFF for Taxi
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Master Warning Light Panel
UTIL HYD OFF
Switch is Off
Set to NORMAL or OVERRIDE as required
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Master Warning Light Panel
L/R WING HT
Wing Anti-Ice Duct Temperature > 180° F
Affected side Wing Anti-Ice Switch OFF & time for 2 minutes
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Master Warning Light Panel
STALL BARR VLV NO 1/2
Respective Stall Barrier Valve is Open
- 1. Press and Hold Autopilot Disconnect Button
- 2. Turn Stall Barrier Switch OFF
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Master Warning Light Panel
L/R MAIN FUEL
Main Boost Pump Failure (< 15 psi)
Select Alternate Boost Pump ON
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Master Warning Light Panel
COOL TURB HT
Discharge Temperature of the Turbine Cooling Compressor > 400 ± 15° F
- Inflight - Manually shutdown AC System
- 1. CABIN PRESS Switch EMER
- Or
- 2. CABIN AIR Switch RAM
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Master Warning Light Panel
BATT ON BUS
Essential DC Bus on Battery Power
Verify Left and/of Right Main DC Buses are powered
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Master Warning Light Panel
SERVICE DOOR
- Fuel, Lav, Water or Aft Equipment Door Unlocked
- Check security of all doors on the ground
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Master Warning Light Panel
L/R ALT FUEL
- Alternate Boost Pump Failed
- Select Main Boost Pump - ON
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Master Warning Light Panel
L/R CONV FAILED FAN
Converter cooling fan has failed (1 out of 5 fans)
- Record the time (25 hours allowed with 1 fan out)
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Master Warning Light Panel
FLT RECORD
Recorder Inoperable
Check CB (CP, B7)
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