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37 Cards in this Set
- Front
- Back
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WHAT ARE THE COMPONENT PARTS OF THE ENGINE
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1- STARTER
2- FUEL CONTROL 3- POWER LEVEL CONTROL QUADRANT 4- ENGINE OIL SYSTEM 5- FIRE OVERTEMPERATURE DETECTION SYSTEM 6- ENGINE INDICTING SYSTEM |
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WHAT IS THE FUNCTION OF ENGINE STARTER
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TURNS ENGINE OVER DURING START
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WHAT IS THE FUNCTION OF THE ENGINE FUEL CONTROL SYS
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LIGHTWEIGHT HYDROMECHANICAL HIGH CAPACITY FUEL FLOW METERING UNIT-PERMITS SELECTION OF ENGINE THRUST LVL- PROVIDES AUTOMATIC COMPENSATION FOR AMBIENT OPERATING CONDITIONS
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WHAT IS THE FUNCTION OF ENGINE PWR LVL CNTRL QUADRANT
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ENGINE CONTROL,
AUTOMATICALLY SEQUENCE IGNITION AND FUEL DURING STARTING CYCLE |
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WHAT IS THE FUNCTION OF ENGINE ENGINE OIL SYS
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SUPPLIES OIL UNDER PRESSURE
LUBRICATES MAIN BEARINGS, ENGINE, AND ACCESORY DRIVE |
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WHAT IS THE FUNCTION OF FIRE OVERTEMPERATURE DETECTION SYS
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COCKPIT INDICATION OF FIRE OR OVERTEMP IN ENGINE COMPARTMENT, AFTE EQUIPMENT BAY, NWW
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WHAT ARE THE PARTS OF THE ENGINE INDICATING SYS
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1- OIL PRESSURE INDICATOR
2- FUEL FLOW INDICATOR 3- ENGINE SPEED (RPM) INDICATOR 4- EXHUAST GAS TEMP (EGT) INDICATOR |
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WHERE IS THE ENGINE STARTER LOCATED
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CENTER FRT ACCESORY DRIVE PAD ON GENERATOR
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WHERE IS THE ENGINE FUEL CONTROL LOCATED
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LEFT REAR PAD OF ACCESSORY GERA BOX
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WHERE IS THE ENGINE POWER LVL CNTRL QUADRANT LOCATED
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FWD COCKPIT PILOTS LEFT HAND CONSOLE
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WHERE IS THE ENGINE OIL SYS LOCATED
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MAIN GEARBOX
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HOW DOES THE OIL PRESSURE INDICATOR WORK
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RECIEVES SIGNAL FROM OIL PRESSURE XMITTER INDICATING OPERATING PRESSURES
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HOW DOES THE FUEL FLOW INDICATOR WORK
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RECIEVES A SIGNAL FROMT HE FUEL FLOW XMITTER DISPLAY IN PPH POUND PER HOUR
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HOW DOES THE rpm INDICATOR WORK
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ENGINE SPEED INDICATOR - TACHOMETER GENERATOR SENDS SIGNAL TO INDICATOR- READS IN PERCENTAGES
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HOW DOES THE EGT INDICATOR WORK
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EXHUAST GAS TEMPERATURE- 6 THERMOCOUPLES ON EXHUST CASE SENSE TEMP SEND IT TO MOUNTED GAUGE
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WHERE IS THE OIL PRESSURE INDICATOR LOCATED
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PILOTS INSTRUMENT PNL LWR LFT SIDE
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WHERE IS THE FUEL FLOW INDICATOR LOCATED
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PILOTS INSTRUMENT PNL RT HAND SIDE
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WHERE IS THE ENGINE SPEED INDICATOR LOCATED
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PILOTS INSTRUMENT PNL LFT HAND SIDE
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WHERE IS THE EXHUAST GAS TEMP INDICATOR LOCATED
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PILOTS INSTRUMENT PNL LEFT HAND SIDE
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WHAT ARE THE COMPONENT PARTS OF THE FUEL SYSTEM
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1- FWD FUEL CELL
2- MID FUEL CELL 3- AFT FUEL CELL 4- WING TANKS 5- AERO 1D DROP TANKS |
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DESCRIPTION AND COMPONENTS FWD FUEL CELL
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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 |
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DESCRIPTION AND COMPONENTS MID FUEL CELL
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BLADDER TYPE-
256 GALLON=1741 LBS PILOT VALVE TWO FUEL QTY UNITS CATAPULT VENT CHECK VALVE |
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DESCRIPTION AND COMPONENTS AFT FUEL CELL
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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 |
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DESCRIPTION AND COMPONENTS WING TANKS
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STRUCTRULLY INTEGRAL TANKS
TWO OUTBOARD TANKS ONE INBOARD TANK |
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DESCRIPTION AND COMPONENTS AERO-1D DROP TANK
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300 GALLONS-295 USABLE
INSTALLED ON FUSELAGE STATIONS TO PROVIDE EXTRA FUEL |
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WHERE IS THE FWD FUEL CELL LOCATED
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AFT REAR COCKPIT DIRECTLY UNDER TB#1
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WHERE IS THE MID FUEL CELL LOCATED
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DIRECTLY BEHIND FWD FUEL CELL
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WHERE IS THE AFT FUEL CELL LOCATED
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DIRECTLY BEHIND MID FUEL CELL UNDER TB #3
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WHERE IS THE WING TANKS LOCATED
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OUTBOARD WING TANKS- OUTBOARD WING FOLD EACH WING
INBORAD WING TANKS- INBOARD WING FOLD RUNS THROUGH FUSELAGE ONE WING TO OTHER. |
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WHERE IS THE DROP TANKS LOCATED
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ANY OF THE 5 STATION PYLONS
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THE MAX LIMITS OF ATTEMPTED ENGINE STARTS IS
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1- 1 MIN ON 1 MIN OFF
2- 1 MIN ON 1 MIN OFF 3- 1 MIN ON 30 MIN OFF |
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THE MAX LIMITS OF DROP TANK CAPACITY IN GALLONS IS
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300 GALLONS 295 USABLE
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THE MAX LIMITS OF INTERNAL FUEL TANK CAPACITY IN GALLONS IS
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WINGS- 977 GALLONS
MAIN BAGS- 1291 GALLONS TOTAL- 2268 GALLONS |
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HOW DOES ENGINE BLEED AIR INTERFACE WITH ENGINE STARTING
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CROSS BLEEDING
EITHER ENGINE CAN BE STARTED WITH ENGINE BLEED AIR |
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SAFETY PRECAUTIONS OF ENGINE GROUND TURN UP
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STAY CLEAR OF DANGER AREAS- INTAKES EXHUAST STARTER ROTATION LINE ENGINE TURBINE BLADES
EAR AND EYE PROTECTION WORN |
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SAFETY PRECAUTIONS FOR FUELING
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HOT PUMP-WINGS FOLDED, NO FUEL (FIRE HAZARD)
GROUNDED A/C, PPE NO RADIO/RADAR ACTIVITY 100 FT A/C |
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SAFETY PRECAUTIONS FOR DEFUELING
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GROUNDED A/C
PPE NO RADIO ACTIVITY 100 FT NO RADAR ACTIVITY 300 FT |
