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37 Cards in this Set

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  • Back
WHAT ARE THE COMPONENT PARTS OF THE ENGINE
1- STARTER
2- FUEL CONTROL
3- POWER LEVEL CONTROL QUADRANT
4- ENGINE OIL SYSTEM
5- FIRE OVERTEMPERATURE DETECTION SYSTEM
6- ENGINE INDICTING SYSTEM
WHAT IS THE FUNCTION OF ENGINE STARTER
TURNS ENGINE OVER DURING START
WHAT IS THE FUNCTION OF THE ENGINE FUEL CONTROL SYS
LIGHTWEIGHT HYDROMECHANICAL HIGH CAPACITY FUEL FLOW METERING UNIT-PERMITS SELECTION OF ENGINE THRUST LVL- PROVIDES AUTOMATIC COMPENSATION FOR AMBIENT OPERATING CONDITIONS
WHAT IS THE FUNCTION OF ENGINE PWR LVL CNTRL QUADRANT
ENGINE CONTROL,
AUTOMATICALLY SEQUENCE IGNITION AND FUEL DURING STARTING CYCLE
WHAT IS THE FUNCTION OF ENGINE ENGINE OIL SYS
SUPPLIES OIL UNDER PRESSURE
LUBRICATES MAIN BEARINGS, ENGINE, AND ACCESORY DRIVE
WHAT IS THE FUNCTION OF FIRE OVERTEMPERATURE DETECTION SYS
COCKPIT INDICATION OF FIRE OR OVERTEMP IN ENGINE COMPARTMENT, AFTE EQUIPMENT BAY, NWW
WHAT ARE THE PARTS OF THE ENGINE INDICATING SYS
1- OIL PRESSURE INDICATOR
2- FUEL FLOW INDICATOR
3- ENGINE SPEED (RPM) INDICATOR
4- EXHUAST GAS TEMP (EGT) INDICATOR
WHERE IS THE ENGINE STARTER LOCATED
CENTER FRT ACCESORY DRIVE PAD ON GENERATOR
WHERE IS THE ENGINE FUEL CONTROL LOCATED
LEFT REAR PAD OF ACCESSORY GERA BOX
WHERE IS THE ENGINE POWER LVL CNTRL QUADRANT LOCATED
FWD COCKPIT PILOTS LEFT HAND CONSOLE
WHERE IS THE ENGINE OIL SYS LOCATED
MAIN GEARBOX
HOW DOES THE OIL PRESSURE INDICATOR WORK
RECIEVES SIGNAL FROM OIL PRESSURE XMITTER INDICATING OPERATING PRESSURES
HOW DOES THE FUEL FLOW INDICATOR WORK
RECIEVES A SIGNAL FROMT HE FUEL FLOW XMITTER DISPLAY IN PPH POUND PER HOUR
HOW DOES THE rpm INDICATOR WORK
ENGINE SPEED INDICATOR - TACHOMETER GENERATOR SENDS SIGNAL TO INDICATOR- READS IN PERCENTAGES
HOW DOES THE EGT INDICATOR WORK
EXHUAST GAS TEMPERATURE- 6 THERMOCOUPLES ON EXHUST CASE SENSE TEMP SEND IT TO MOUNTED GAUGE
WHERE IS THE OIL PRESSURE INDICATOR LOCATED
PILOTS INSTRUMENT PNL LWR LFT SIDE
WHERE IS THE FUEL FLOW INDICATOR LOCATED
PILOTS INSTRUMENT PNL RT HAND SIDE
WHERE IS THE ENGINE SPEED INDICATOR LOCATED
PILOTS INSTRUMENT PNL LFT HAND SIDE
WHERE IS THE EXHUAST GAS TEMP INDICATOR LOCATED
PILOTS INSTRUMENT PNL LEFT HAND SIDE
WHAT ARE THE COMPONENT PARTS OF THE FUEL SYSTEM
1- FWD FUEL CELL
2- MID FUEL CELL
3- AFT FUEL CELL
4- WING TANKS
5- AERO 1D DROP TANKS
DESCRIPTION AND COMPONENTS FWD FUEL CELL
SELF SEALING-
392 GALLONS=2.666LBS

DUAL SEAT SHUTOFF VALVE
NON MODUALTING PILOT VALVE
TRANSFER AND DUMP PUMP
TWO FUEL QTY PROBES
FLOAT VENT VALVE
ACCELERATION CHECK VALVE
CATAPULT CHECK VALVE( INERTIA)
CATAPULT VENT CHECK VALVE
DESCRIPTION AND COMPONENTS MID FUEL CELL
BLADDER TYPE-
256 GALLON=1741 LBS

PILOT VALVE
TWO FUEL QTY UNITS
CATAPULT VENT CHECK VALVE
DESCRIPTION AND COMPONENTS AFT FUEL CELL
SELF SEALING TYPE-
643 GALLONS=4372 LBS

DUAL SEAT SHUT OFF VALVE
PILOT VALVE
TRANSFER AND DUMP PUMP
FUEL BOOSTER PUMP
DEFUELING CHECK VALVE
TWO FUEL PROBES
FWD BAFFLE CHECK VALVE
AFT BAFFLE CHK VALVE
DESCRIPTION AND COMPONENTS WING TANKS
STRUCTRULLY INTEGRAL TANKS

TWO OUTBOARD TANKS
ONE INBOARD TANK
DESCRIPTION AND COMPONENTS AERO-1D DROP TANK
300 GALLONS-295 USABLE
INSTALLED ON FUSELAGE STATIONS TO PROVIDE EXTRA FUEL
WHERE IS THE FWD FUEL CELL LOCATED
AFT REAR COCKPIT DIRECTLY UNDER TB#1
WHERE IS THE MID FUEL CELL LOCATED
DIRECTLY BEHIND FWD FUEL CELL
WHERE IS THE AFT FUEL CELL LOCATED
DIRECTLY BEHIND MID FUEL CELL UNDER TB #3
WHERE IS THE WING TANKS LOCATED
OUTBOARD WING TANKS- OUTBOARD WING FOLD EACH WING
INBORAD WING TANKS- INBOARD WING FOLD RUNS THROUGH FUSELAGE ONE WING TO OTHER.
WHERE IS THE DROP TANKS LOCATED
ANY OF THE 5 STATION PYLONS
THE MAX LIMITS OF ATTEMPTED ENGINE STARTS IS
1- 1 MIN ON 1 MIN OFF
2- 1 MIN ON 1 MIN OFF
3- 1 MIN ON 30 MIN OFF
THE MAX LIMITS OF DROP TANK CAPACITY IN GALLONS IS
300 GALLONS 295 USABLE
THE MAX LIMITS OF INTERNAL FUEL TANK CAPACITY IN GALLONS IS
WINGS- 977 GALLONS
MAIN BAGS- 1291 GALLONS
TOTAL- 2268 GALLONS
HOW DOES ENGINE BLEED AIR INTERFACE WITH ENGINE STARTING
CROSS BLEEDING

EITHER ENGINE CAN BE STARTED WITH ENGINE BLEED AIR
SAFETY PRECAUTIONS OF ENGINE GROUND TURN UP
STAY CLEAR OF DANGER AREAS- INTAKES EXHUAST STARTER ROTATION LINE ENGINE TURBINE BLADES

EAR AND EYE PROTECTION WORN
SAFETY PRECAUTIONS FOR FUELING
HOT PUMP-WINGS FOLDED, NO FUEL (FIRE HAZARD)

GROUNDED A/C, PPE

NO RADIO/RADAR ACTIVITY 100 FT A/C
SAFETY PRECAUTIONS FOR DEFUELING
GROUNDED A/C
PPE
NO RADIO ACTIVITY 100 FT
NO RADAR ACTIVITY 300 FT