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227 Cards in this Set
- Front
- Back
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WHAT PART IS THE 45 CERTIFIED UNDER?
|
CFR FAR PART 25, \
\ TRANSPORT CATEGORY |
|
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WHAT KINDS OF OPERATIONS IS THE 45 APPROVED FOR?
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VFR, IFR, DAY, NIGHT, ICING
|
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THE 45 IS STAGE _____ NOISE COMPLIANT
|
3\
FAR 36 |
|
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WHAT ENGINES AND HOW MUCH THRUST IS ON THE 45
|
TWO AlliedSignal TFE731-20 ENGINES\
3500# AT SEA LEVEL |
|
|
WHAT AVIONICS ARE IN THE 45
|
PRIMUS 1000\
\ UNIVERSAL UNS-1(x) |
|
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WHAT INTEGRATED AVIONICS COMPUTER (IAC) CONTROLS THE AP
|
YD, AND RUDDER BOOST?,IAC #2, COPILOT
|
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WHEN DOES LOW BANK AUTOMATICALLY ENGAGE ON THE AP?
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>41,600', IT AUTOMATICALLY CLEARS WHEN <41,400'
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WHAT AP MODES WILL LOW BANK NOT ENGAGE FOR?
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FMS NAV, APP, or ROLL
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WHAT ARE THE FLC PROFILES?
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NORMAL CLIMB, HS CLIMB, NORMAL DESCENT, HS DESCENT
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WHAT IS THE FLC NORMAL CLIMB PROFILE?
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250 KIAS TO 0.70M
|
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WHAT IS THE FLC HS CLIMB PROFILE?
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250 KIAS TO 10,000', THEN 275 KIAS TO 0.73M
|
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WHAT IS THE FLC NORMAL DESCENT PROFILE?
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0.76 TO 300 KIAS TO 12,500', THEN 250 KIAS <10,500'
|
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WHAT IS THE FLC HS DESCENT PROFILE?
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0.79M TO 320 KIAS TO 14,500', THEN 250 KIAS < 10,500'
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WHAT APU IS IN THE 45?
|
ALLIED SIGNAL RE100 APU WITH AUTOMATIC PROTECTIONS
|
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WHEN WILL THE APU OIL LEVEL BE ANNUNCIATED ON THE APU MX CONTROL PANEL?
|
ONLY DURING AN OIL TEST
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WHAT MUST BE "ON" IN ORDER TO DO AN APU OIL TEST?
|
THE RIGHT BATTERY
|
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CAN THE APU BE OPERATED WITH AN "APU FAN FAIL" CAS?
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YES: IF THE OUTSIDE TEMP IS <100 DEGREES F (38C)
|
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WHAT IS THE APU POWER RATING?
|
300amps AT 30v DC.
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IF A GPU IS CONNECTED WHEN THE APU IS ON WHAT HAPPENS?
|
THE APU DROPS OFFLINE IF THE GPU IS SELECTED
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WHERE DOES THE APU GET ITS FUEL FROM AND HOW MUCH DOES IT USE?
|
THE RIGHT WING TANK VIA THE RH STBY PUMP AND BURNS 150# PER HR (22GAL)
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HOW WOULD YOU KNOW THERE WAS AN APU FIRE?
|
"APU FIRE" CAS AND LIGHT, APU SHUTDOWN, FIRE HORN/SIREN IN THE NOSE AVIONICS BAY.
|
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WHEN IS THE APU FIRE HALON BOTTLE DISCHARGED?
|
1) WHEN THE "APU FIRE" SWITCH IS PRESSED\
2) 10sec AFTER THE "APU FIRE" SWITCH INDICATOR IS ILLUMINATED |
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WHAT IS THE NORMAL OIL LEVEL OF THE APU
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2qt
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HOW MANY STATIC WICKS ARE ON THE 45?
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19
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HOW MANY BATTERIES ARE IN THE 45?
|
2 MAIN BATTS AND 1 EMER BATT
|
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WHEN WILL THE BATT OVHT LIGHT CAS COME ON?\
\ *Ni-Cad only |
> 60c AMBER, > 70c RED
|
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WHAT IS A DEEC?
|
DIGITAL ELECTRONIC ENGINE CONTROL
|
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WHAT ARE THE STARTER GENERATORS RATED AT?
|
400amp 30vDC, CONTROLLED BY 2 GEN CONTROL UNITS (GCU)
|
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WHAT DO THE GCUs DO?
|
1) REGULATE VOLTAGE\
2) LIMIT CURRENT TO 28v\ 3) STARTER CUTOFF\ 4) STARTER ABORT\ 5) UNDER AND OVER VOLTAGE PROTECTION\ 6) OVERSPEED PROTECTION (runaway start) |
|
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WHY IS THERE AN EMER BATT AND HOW IS IT CHARGED?
|
TO POWER THE ESSENTIAL COMPONENTS DURING DUAL GEN FAIL.\
\ CHARGED BY THE R GEN BUS OR A GPU |
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WHEN DO THE PAX OX MASK AUTO DEPLOY?
|
AT 14,500' CABIN ALT
|
|
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CREW AND PAX MASK ARE NOT APPROVED ABOVE______?
|
FL400
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WHAT DOES "HI FLOW" DO?
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RESETS THE PACK (AIR CYCLE MACHINE) VALVE TO REGULATE AT HIGHER PRESSURE FOR MAXIMUM COOLING OF THE CABIN
|
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WHERE ARE THE 2 OUTFLOW VALVES?
|
ON THE FORWARD PRESSURE BULKHEAD
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WHAT IS THE NORMAL DELTA P PRESSURE AND HIGHEST ALTITUDE IN THE PRESSURIZATION SYSTEM?
|
9.3psi OR 8,000' CABIN ALT AT FL510
|
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WHAT HAPPENS IF BOTH CHANNELS FAIL IN THE PRESSURIZATION CONTROLLER?
|
1) "LR CAB PRESS FAIL" CAS\
\ 2) CABIN DIFFERENTIAL CLIMBS FROM 9.3 TO 9.7\ \ 3) EMER DEPRESS IS NOT AVAILABLE\ \ 4) PACK MUST BE SELECTED OFF \ BEFORE LANDING TO PREVENT LANDING PRESSURIZED |
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WHAT ARE THE MODES OF THE AUTO PRESSURIZATION SYSTEM?
|
GROUND, T/O, CLIMB, CRUISE, DESCENT, LANDING
|
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WHAT HAPPENS IN THE AUTO PRESS SYSTEM GROUND MODE
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CABIN ALT IS ZERO, OUTFLOW VALVES ARE FULL OPEN
|
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WHAT HAPPENS IN THE AUTO PRESS SYSTEM T/O MODE
|
IT STARTS WHEN THE LEFT TL IS ADVANCED TO MCR OR HIGHER, OR A/S <150 KIAS. \
\ IT PRESSURIZES CABIN 150 BELOW T/O ELEVATION |
|
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WHAT HAPPENS IN THE AUTO PRESS SYSTEM CLIMB MODE
|
IT STARTS AT LIFT-OFF OR >150KTS. \
\ THE CABIN ALT INCREASES AT NO MORE THAN 600fpm UNTIL THE REACHING THE PROGRAMMED ALT. |
|
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WHAT HAPPENS IN THE AUTO PRESS SYSTEM CRUISE MODE
|
IT STARTS WHEN THE A/C ALT HAS STABALIZED AT +/- 100' OF CHANGE FOR 1MIN. \
\ CABIN ALT IS HELD CONSTANT UNTIL A FLIGHT ALT CHANGE OF 200' OR MORE. |
|
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WHAT HAPPENS IN THE AUTO PRESS SYSTEM DESCENT MODE
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IT STARTS WHEN THE A/C DESCENDS 1,000'. \
\ CABIN ALT DESCENDS AT A RATE NOT EXCEEDING 375fpm. |
|
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WHAT HAPPENS IN THE AUTO PRESS SYSTEM LANDING MODE
|
IT STARTS WHEN THE A/S DECREASES BELOW 65 KIAS AND THE LEFT TL IS BELOW MCR OR THE A/C LANDS. \
\ UPON LANDING THE CABIN EQUALIZES WITH FIELD ELEVATION AT -300 TO +500 fpm. |
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WHAT ABNORMAL MODES PROTECT THE AUTO PRESS SYSTEM
|
1) T/O ABORT\
2) EMER RETURN FROM CLIMB \ 3) T/O AFTER LANDING FOR TOUCH AND GOES\ 4) HIGH T/O AND L/D |
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EMER PRESS CAN BE ________ OR _________ SELECTED
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AUTOMATICALLY SELECTED WHEN CABIN ALT INCREASES TO 9,500' OR 14,500'. \
\ MANUALLY |
|
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HOW CAN YOU PURGE THE CABIN OF SMOKE OR FUMES?
|
EMERGENCY DEPRESS. \
\ OPENS BOTH OURFLOW VALVES TO FULL OPEN BUT IS LIMITED TO 13,700' IF BLEED AIR IS FLOWING INTO THE VESSEL |
|
|
WHAT FIRE PROTECTION IS ON THE 45?
|
1) PORTABLE HALON FIRE EXTINGUISHERS IN THE CABIN\
\ 2) APU HALON FIRE EXTINGUISHER\ \ 3) 2 HALON FIRE EXTINGUISHERS FOR THE ENGINES\ \ 4) A FIRE DETECTION SYSTEM |
|
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WHAT DOES PUSHING THE FIRE BUTTON DO?
|
1) CLOSES BLEED AIR VALVES\
\ 2) CLOSES FUEL SOV\ \ 3) CLOSES HYDRAULIC SOV\ \ 4) CLOSES THE TR ISOLATION VALVE\ \ 5) ARMS FIRE BOTTLE SQUIBS\ \ 6) INHIBITS ENGINE IGNITORS\ \ 7) DISCONNECTS GEN AND ALT\ \ 8) DISABLES THE ONSIDE WINDSHIELD HEAT |
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THE AP USES THE _______ TRIM SYSTEM
|
SECONDARY
|
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WHEN THE SPOILERS ARE ARMED WHAT MUST HAPPEN FOR THEM TO AUTO DEPLOY?
|
1) SPOILER LEVER IN ARM POSITION\
\ 2) BOTH SQUAT SWITCHES IN GROUND MODE\ \ 3) EITHER WHEEL SPEED IS ABOVE 60 KTS |
|
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DOES THE SPOILER HANDLE MOVE IF THE SPOILERS ARE AUTO DEPLOYED?
|
NO, BUT THE SPOILERS REMAIN EXTENDED UNTIL RETRACT IS SELECTED \
\ **UNLESS A TL IS ADVANCED ABOVE IDLE THEN THEY AUTO RETRACT FOR GO AROUND |
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WHEN AIRBORNE SHOULD THE SPOILERS AND FLAPS BE USED TOGETHER?
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NO
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ON THE GROUND SPOILERS FULLY EXTEND TO ______ DEGREES
|
IN THE AIR THEY CAN BE SELECTED FROM ____ TO ____ DEGREES,60\
\ 15 TO 60\ *60 IS ONLY AVAILABLE WHEN BELOW 175kts |
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AT WHAT AOA DOES THE SHAKER ACTIVATE?
|
0.8 AOA
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HOW IS BANK CONTROLLED WHEN THE ROLL DISC LEVER IS PULLED?
|
PILOT: BY SPOILERONS ONLY\
\ COPILOT: AILERONS ARE STILL CONTROLLED |
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HOW IS PITCH CONTROLLED WHEN THE ELEV DISC HANDEL IS PULLED
|
PILOT: LEFT ELEVATOR ONLY\
\ COPILOT: RIGHT ELEVATOR ONLY |
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WHEN IS THE RUDDER BOOST SYSTEM ARMED AND THEN ACTIVATED?
|
1. FLAPS EXTENDED BEYOND 3 DEGREES\
2. A/S BELOW 180 KIAS\ 3. ACTIVATED WHEN 50lb OF FORCE IS APPLIED TO A RUDDER OR COMBINATION |
|
|
YAW DAMPING IS AUTO _______ WHEN RUDDER BOOST IS ACTIVE
|
INHIBITED
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HOW DO YOU TRIM PITCH OR ROLL WHEN THE AP IS DISENGAGED?
|
TRIM BARREL AND BUTTON ON CONTROL WHEEL (HAT)
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HOW DO YOU TRIM PITCH OR ROLL WHEN THE AP IS ENGAGED?
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TRIM BARREL ONLY ON CONTROL WHEEL
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WHERE DOES PITCH TRIM COME FROM AND WHAT CONTROLS IT?
|
A VARIABLE-INCIDENCE HORIZONTAL STAB\
\ MOVED BY AN ELECTRIC SCREW-JACK ACTUATOR WITH PRIMARY AND SECONDARY MOTORS |
|
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THE PRIMARY PITCH TRIM MOTOR RESPONDS TO?
|
MANUAL TRIM COMMANDS FROM CONTROL WHEEL SWITCHES
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THE SECONDARY PITCH TRIM MOTOR RESPONDS TO?
|
MANUAL TRIM COMMANDS FROM SEC SWITCHES ON THE PEDESTAL OR AP
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WHAT TYPE OF FLAPS ARE ON THE 45?
|
SINGLE-SLOT FOWLER FLAPS\
\ OPERATED BY 2 SCREW-JACK ACTUATORS AND A HYDRAULIC FLAP POWER UNIT |
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WHAT DEGREES ARE SELECTABLE FOR THE FLAPS?
|
0, 8, 20, 40
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HOW LONG DOES IT TAKE TO EXTEND THE FLAPS FULLY NORMALLY?
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NO MORE THAN 10sec
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HOW LONG DOES IT TAKE TO EXTEND THE FLAPS TO 20 WHEN USING THE AUX PUMP AND XFLOW?
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UP TO 60sec
|
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HOW MANY FUEL TANKS DOES THE 45 HAVE AND WHAT ARE THEIR QUANTITIES?
|
3: 2 WING AND 1 FUSELAGE TANKS.\
\ 6292# TOTAL AND 6062# USABLE |
|
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HOW DO YOU FUEL THE 45
|
VIA SINGLE POINT CONNECTION OR GRAVITY FILLER PORT THAT FILLS THE FUSELAGE TANK AND THEN IS PLUMMED TO THE MAIN WING TANKS
|
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HOW DOES THE FUEL SYSTEM WORK
|
A FUSELAGE BLADDER TANK IS FILLED AND THEN FEEDS 2 WING TANKS. THE WING TANKS FEED THE RESPECTIVE ENGINE, THE WING TANKS ARE SEPARATED INTO 2 TANKS PLUMED TOGETHER. THE TANKS HAVE FLAPPER VALVES, SCAVENGE PUMPS AND A COLLECTOR BAY TO PREVENT FUEL SLOSH AND TO ENSURE POSITIVE PRESSURE AND SUBMERSION OF THE MAIN EJECTOR PUMPS. RAM AIR AND VENTS ENSURE POSITIVE PRESSURE IN THE WING TANKS. A TRANSFER SYSTEM ENABLES FUEL TO BE TRANSFERRED BETWEEN WING TANKS AS NEEDED.
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WHAT HAPPENS TO THE FUEL XFLOW VALVE WHEN DC POWER IS LOST?
|
IT FAILS IN THE POSITION IT WAS IN WHEN THE POWER WAS LOST.
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WHAT ARE THE STBY FUEL PUMPS USED FOR?
|
1. ENGINE START\
\ 2. AS A BACK UP FOR MAIN EJECTOR PUMPS\ \ 3. FOR WING TO WING TRANSFER |
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HOW MANY FUEL FILTERS ARE ON THE 45 AND WHAT IF IT GETS CLOGGED?
|
4: 2 PER WING \
\ THERE IS A BYPASS FOR EACH FILTER WHICH WILL TRIGGER A CAS MESSAGE |
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WHAT HAPPENS TO THE FWSOVs WHEN DC POWER IS LOST?
|
IT FAILS IN THE POSITION IT WAS IN WHEN THE POWER WAS LOST.
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DURING NORMAL START WHEN DOES THE STARTER AND ELECT FUEL PUMP CUTOUT?
|
APPROX 50% N2
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WHEN WILL THE FUEL IMBALANCE CAS OCCUR?
|
WHEN > 500# WITH THE FLAPS RETRACTED OR 200# WITH THE FLAPS EXTENDED\
\ ** 200# DIFFERENCE IN FLIGHT W/SB 45-28-8 |
|
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WHEN WILL THE FUEL QTY LOW CAS OCCUR?
|
WHEN THE FUEL QUANTITY IN THE CORRESPONDING REACHES 350# OR LESS
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HOW MANY FUEL QUANTITY PROBES ARE IN THE 45?
|
17: 8 IN EACH WING TANK AND ONE IN THE FUSELAGE TANK
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WHAT ARE THE ISSUES WITH GRAVITY FUELING
|
1. THE WINGS FILL UP SLOWER THAN THE FUSELAGE TANK SO STOP AT 4500# AND WAIT 5MIN THEN FUEL TO 6000#. \
\ 2. THE VENT LINES MUST BE DRAINED BEFORE GRAVITY REFUELING OR THE WINGS WONT FILL COMPLETELY BECAUSE TRAPPED AIR. |
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WHERE ARE THE FUEL VENT LINES ACCESSED?
|
IN THE R/L WING ACCESS DOORS ON THE BELLY
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WHAT IS OPERATED BY HYDRAULICS?
|
1. GEAR \
\ 2. GEAR INBOARD DOORS\ \ 3. FLAPS\ \ 4. SPOILERS / SPOILERONS\ \ 5. WHEEL BREAKS\ \ 6. TRs |
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HOW MANY HYDRAULIC SYSTEMS DOES THE 45 HAVE?
|
2: A MAIN SYSTEM POWERED BY ENGINE DRIVEN PUMPS AND AN AUX SYSTEM POWERED BY DC ELECTRIC MOTOR. \
\ BOTH SHARE A SPLIT RESERVOIR. |
|
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WHAT HAPPENS IF BOTH HYDRAULIC SYSTEMS FAIL?
|
A HYDRAULICALLY CHARGED PNEUMATIC ACCUMULATOR CAN STILL OPERATE EMER WHEEL BRAKES.
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WHAT IS THE NORMAL HYD SYSTEM PRESSURE?
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3000psi
|
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HOW MANY FILTERS ARE IN THE HYD SYSTEM AND HOW DO YOU KNOW IF IT IS BLOCKED?
|
2: AN LED ON THE GROUND SERVICE PANEL\
\ * NO CAS |
|
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WHAT ARE THE FUNCTIONS OF THE AUX HYD SYSTEM?
|
1. HYD PRESSURE TO CHARGE THE BREAK ACCUMULATOR\
\ 2. BACKUP POWER FOR THE BRAKES, FLAPS AND GEAR IF THE MAIN SYSTEM MALFUNCTIONS\ \ 3. POWER FOR GROUND SERVICING |
|
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WHICH HYD SYSTEM POWERS THE BRAKES MAIN OR AUX?
|
THE SYSTEM WITH THE MOST PRESSURE VIA THE BRAKE SYSTEM SHUTTLE VALVE
|
|
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WHAT DOES THE BRAKE ACCUMULATOR DO?
|
AN INDEPENDENT SYSTEM THAT IS CHARGED BY THE AUX HYD SYSTEM TO 3000psi CAN BE USED FOR UP TO 6 EMER BRAKE APPLICATIONS OR TO PRESSURIZE THE PARKING BRAKE FOR 48hrs
|
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WHEN DOES THE AUX HYD PUMP OPERATE AUTOMATICALLY?
|
DURING NORMAL GEAR DOWN OPERATION\
*SELECTING GEAR UP DEACTIVATES THE SYSTEM |
|
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THE AUX HYD SYSTEM WILL NOT OPERATE WHAT SYSTEMS?
|
1) SPOILERS\
\ 2) TRs\ \ 3) **FULL 40 DEGREES OF FLAPS |
|
|
HYD XFLOW VALVE CONNECTS WHAT SYSTEMS?
|
THE MAIN AND THE AUX HYD SYSTEMS\
\ IF THE MAIN SYSTEM FAILS THE AUX SYSTEM CAN OPERATE THE GEAR AND FLAPS. |
|
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HOW MUCH FLUID DOES THE HYD RESERVOIR HOLD?
|
2gal
|
|
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WHAT ELECTRIC ANTI-ICE PROTECTION IS ON THE 45?
|
1) PITOT HEAT\
\ 2) TOTAL AIR TEMP PROBE\ \ 3) ENGINE INLET AIR TEMP AND PRESSURE PROBES\ \ 4) STALL WARNING VANES\ \ 5) WINDSHIELDS |
|
|
WHAT BLEED-AIR ANTI-ICE PROTECTION IS ON THE 45?
|
LEADING EDGES ON:\
1) WING\ \ 2) HORIZONTAL STAB\ \ 3) NACELLE |
|
|
OTHER THAN A VISUAL INSPECTION HOW CAN YOU TELL IF YOU ARE ACCUMULATING ICE IN THE 45?
|
ICE DETECTION CAS FROM THE ICE DETECTOR LOCATED IN THE LOWER LEFT NOSE AREA
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WHAT SYSTEM IS INOP IF YOU LOSE THE L OR R ALTERNATOR?
|
THE CORRESPONDING SIDE WINDSHIELD HEAT IS INOP
|
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LOSS OF ELECTRICAL POWER CAUSES THE NACELLE PRESSURE REGULATING SOV TO FAIL ________.
|
OPEN
|
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LOSS OF ELECTRICAL POWER CAUSES THE WING AND STAB ANTI-ICE SOV TO FAIL ________.
|
CLOSED
|
|
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WHICH WAY DOES THE NOSE GEAR RETRACT?
|
FORWARD
|
|
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HOW ARE THE MAIN GEAR HELD IN THE DOWN POSITION?
|
DOWNLOCK MECHANISM
|
|
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HOW ARE THE MAIN GEAR HELD IN THE UP/RETRACTED POSITION?
|
BY THE MAIN GEAR INBOARD DOOR THAT IS MECHANICALLY LATCHED BY AN UPLOCK MECHANISM\
\ WHICH IS RELEASED BY A HYDRAULIC ACTUATOR OR MANUAL EMERGENCY RELEASE. |
|
|
THE INBOARD GEAR DOORS ARE ONLY OPEN WHEN?
|
DURING GEAR OPERATION, THEY ARE CLOSED WHEN THE GEAR IS LOCKED UP OR DOWN.
|
|
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WHAT KEEPS THE NOSE-WHEEL FROM TURNING WHILE IN THE AIR BUT EXTENDED?
|
1) A CENTERING CAM\
\ 2) THE NOSE-WHEEL STEERING SYSTEM |
|
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HOW CAN THE GEAR BE LOWERED IF THE MAIN HYDRAULIC SYSTEM FAILS?
|
THE AUX HYDRAULIC SYSTEM CAN LOWER THE GEAR IN APPROX 30 SEC
|
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HOW CAN THE GEAR BE LOWERED IF THE MAIN AND AUX HYDRAULIC SYSTEMS FAIL?
|
AN EMERGENCY FREE FALL SYSTEM THAT USES GRAVITY AND AIRFLOW TO LOWER THE GEAR.
|
|
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WHAT IS THE DIFFERENCE IN GEAR CAUTION AND GEAR WARNING?
|
CAUTION CAN BE MUTED, WARNING CANNOT
|
|
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WHAT CAUSES THE GEAR WARNING INDICATORS TO ACTIVATE?
|
1) 1 OR MORE GEAR IS NOT DOWN AND THE FLAPS ARE LOWERED BEYOND 25 DEGREES\
\ 2) 1 OR MORE GEAR IS NOT DOWN AND BOTH TLs ARE BELOW 82% AND THE RADIO ALT IS BELOW 500' |
|
|
WHAT EXTRA PROTECTIONS ARE IN THE BRAKE SYSTEM?
|
1) ANTI-SKID\
\ 2) TOUCHDOWN\ \ 3) LOCKED WHEEL |
|
|
HOW MUCH EXTRA THRUST DOES THE AUTOMATIC PERFORMANCE RESERVE (APR) GIVE AN ENGINE?
|
150#
|
|
|
HOW IS THE ACCESSORY GEARBOX (AGB) DRIVEN?
|
BY THE HP ROTO (N2) VIA THE TOWER SHAFT
|
|
|
WHAT COMPONENTS ARE DRIVEN BY THE AGB?
|
1) HYDRAULIC PUMP\
\ 2) FUEL PUMP AND FUEL CONTROL UNIT\ \ 3) DC STARTER/GENERATOR\ \ 4) AC ALTERNATOR\ \ 5) OIL PRESSURE AND SCAVENGE PUMPS\ \ 6) AUX MOTIVE FUEL PUMP |
|
|
WHAT IS A DEEC?
|
DIGITAL ELECTRONIC ENGINE CONTROL
|
|
|
WHAT DO THE DEECs DO?
|
PROVIDES:\
1) AUTO START SEQUENCING\ \ 2) ROTOR SPEED AND TEMP LIMITS\ \ 3) SURGE FREE \ ACCELERATION/DECELERATION\ \ 4) AUTO IGNITION\ \ 5) ENGINE SYNC\ \ 6) APR |
|
|
WHAT DO THE DEECs USE TO DETERMINE ENGINE OPERATION PARAMETERS?
|
1) TOTAL INLET PRESSURE AND TEMP FROM PT2 AND TT2 PROBES\
\ 2) INTERSTAGE TURBINE TEMP (ITT)\ \ 3) N1 SPEED\ \ 4) N2 SPEED\ \ 5) POWER LEVER ANGLE (PLA)\ \ 6) AIRFRAME INPUTS - WOW |
|
|
HOW CAN YOU TAKE THE WEATHER RADAR OUT OF FORCED STANDBY MODE ON THE GROUND?
|
PUSH STAB BUTTON 4 TIMES, PRESS BOTH RANGE BUTTONS TO EXIT
|
|
|
IF A DEEC FAILS OR IS IN THE MAN OR OFF POSITION THE SURGE BLEED VALVE IS _______ OPEN.
|
1/3
|
|
|
WHAT PREVENTS FUEL ICING?
|
THE FUEL HEATER / OIL COOLER
|
|
|
WHEN IS ULTIMATE OVER-SPEED PROTECTION NOT AVAILABLE?
|
WHEN ENG CMPTR SWITCH IS OFF
|
|
|
WHAT TRIGGERS THE APR THRUST?
|
A DIFFERENCE OF 15% N2 BETWEEN THE ENGINES
|
|
|
WHAT IS MPR?
|
MANUAL PERFORMANCE RESERVE, LIKE APR BUT AVAILABLE REGARDLESS OF THE OTHER ENGINE SPEED.
|
|
|
WHAT ENGINE/DEEC IS THE MASTER FOR ENGINE SYNC?
|
LEFT
|
|
|
BELOW WHAT TEMP SHOULD THE ENGINES BE PRE-WARMED BEFORE START?
|
-40C/F
|
|
|
ENGINE RPM SHOULDNT BE INCREASED ABOVE IDLE WHEN OIL TEMP IS BELOW ______ DEGREES
|
30c
|
|
|
DURING NORMAL START AT WHAT SPEED DOES THE DEEC COMMAND IGNITION ON AND THEN OFF AFTER STARTED?
|
7% N2, 70% N1
|
|
|
WHEN IS THE APU OR A GPU RECOMMENDED FOR START? (TEMP)
|
BELOW 32F
|
|
|
AT _____ N2 THE STARTER IS CUTOUT DURING A NORMAL START?
|
50%
|
|
|
WHAT ARE THE STARTER LIMITATIONS?
|
1) 1MIN\
2) 2MIN\ 3) 30MIN\ \ *1min continuous |
|
|
WHEN WOULD THE AUTOMATIC THRUST LEVER RETARD SYSTEM REDUCE THE ENGINE TO IDLE?
|
WHEN A TR DEPLOY SEQUENCE IS INITIATED AND THE POWER IS NOT AT IDLE
|
|
|
HOW MANY CHIMES DOES A WARNING CAS AND CAUTION CAS GET?
|
TRIPLE, SINGLE
|
|
|
HOW MUCH FUEL DOES THE APU BURN?
|
ABOUT 150 pph
|
|
|
WHAT ARE THE APU STARTER LIMITATIONS?
|
1) 1MIN\
2) 2MIN\ 3) 15MIN |
|
|
DURING PREFLIGHT WHAT DO YOU CHECK ON THE APU?
|
CHECK THE APU MAINT PANEL FOR PROPER OIL LEVEL.\
\ PRESS OIL TEST BUTTON- NO INDICATION MEANS THE OIL LEVEL IS WITHIN NORMAL RANGE |
|
|
WHAT CABIN ALT WILL THE OUTFLOW VALVES CLOSE AT EVEN DURING EMER DEPRESS?
|
13,700'
|
|
|
DURING ELEVATOR DISCONNECT WHAT SEAT CONTROLS WHAT ELEVATOR?
|
PILOT - LEFT ELEVATOR\
COPILOT - RIGHT ELEVATOR\ \ *AP WILL NOT ENGAGE |
|
|
ALLOW THE OPERATING GEN AMPS TO DROP BELOW _______ BEFORE ATTEMPTING CROSS GEN START
|
300 AMP
|
|
|
WHEN DOES APR AUTOMATICALLY COME ON?
|
WHEN ARMED WITH 15% DIFFERENCE OF N2.\
\ GIVES 150# ADDITIONAL THRUST. |
|
|
WHAT HELPS THE 45 WITH LOW SPEED AND STABILITY?
|
1) DROOPING LEADING EDGE - STABILITY AT LOW SPEED\
\ 2) SAWTOOTH - CREATE VORTICIES\ \ 3) VORTILONS - DELAY STALL AT WING TIP\ \ 4) 4 TRIANGLES - PREVENT FLOW DETACHMENT AT HIGH AOA |
|
|
WHAT DOORS GIVE CAS?
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1) MAIN DOOR\
\ 2) BAGGAGE DOOR\ \ 3) TAILCONE EQUIPMENT BAY |
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HOW DO YOU TURN ON THE RADAR ON THE GROUND OR EXIT FORCED STBY MODE?
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PRESS STAB 4X
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WHAT COMPUTER GIVES YOU THE ORAL WARNINGS AND CHIMES?
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CWP - CREW WARNING PANEL
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WILL YOU GET ORAL OR CWP LIGHTS IF ON EMER BATT ONLY?
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NO - NOT ON EMER BATT BUS
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WHAT IS THE IDEAL AMP FOR A GPU?
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1000-1100amp, 1500 MAX
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HOW CAN YOU TELL IF THE APU OR GPU ARE POWERING THE A/C FROM OUTSIDE THE COCKPIT?
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LOGO LIGHTS- ARE ON THE NON-ESSENTIAL BUS\
\ IF APU/GPU FALL OFFLINE THE LIGHTS WILL GO OUT |
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WHAT DO THE EMER BATTS POWER DURING STARTS?
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1) AVIONICS BUSES\
\ 2) ESSENTIAL BUSES\ \ 3) EMER BUS |
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WHAT PUSHES FUEL FROM FUSELAGE TANK TO WINGS?
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1) GRAVITY\
\ 2) MOTIVE FLOW PUMP\ \ 3) NACA SCOOP RAM AIR PRESSURE |
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WHAT DO YOU NEED TO DRAIN BEFORE GRAVITY REFUELING?
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DRAIN VENT LINES
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HOW MANY FUEL FILTERS ARE ON THE 45?
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4: 2 PER SIDE
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HOW MANY FUEL PROBES CAN BE INOP IN THE WING TO STILL GIVE QUANTITY?
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1
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HOW MANY FUEL PROBES ARE IN THE WINGS AND FUSELAGE?
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8 PER WING TANK AND 1 IN THE FUSELAGE TANK
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WHEN DO THE IGNITIONS AUTOMATICALLY COME ON DURING NORMAL START SEQUENCE?
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6-7% N2
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WHEN IS FUEL INTRODUCED DURING START?
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10% N2
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WHEN SHOULD THE IGN CUTOUT AFTER START?
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45% N2
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WHEN SHOULD THE STARTER CUTOUT DURING START?
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50% N2
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WHEN WILL THE APR COME ON?
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AUTOMATICALLY BY THE DEEC WHEN THERE IS A 15% DIFFERENCE IN ENGINE N2 IF ARMED OR BY SETTING IT ON THE THRUST LEVER
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WHAT ENGINE DEEC IS MASTER DURING SYNC?
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LEFT
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HOW CAN YOU TELL IF THE NOSE WHEEL IS DOWN?
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IF THE NOSE WHEEL STEERING WILL ENGAGE
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HOW CAN YOU TELL IF THE MAIN GEAR ARE DOWN
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IF THE TAXI LIGHT WILL COME ON - WATCH GEN AMPS DURING DAYLIGHT
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IS MIXING APPROVED OILS APPROVED?
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YES
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THE ENGINES SHOULD BURN NO MORE THAN 1QT OF OIL EVERY _______ HOURS?
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25
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WHAT SYSTEM OPERATES THE TRs?
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MAIN HYD SYSTEM ONLY\
\ NOT AUX |
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AT HIGH POWER SETTINGS THE PACK USES ______ BLEED AIR AND AT LOW POWER SETTINGS IT USES _____ BLEED AIR.
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LOW PRESSURE,\
\ HIGH PRESSURE |
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ABOVE WHAT ALTITUDE IS THE ACM BYPASSED?
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40,000'
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WHAT TYPE OF BATTERY IS THE EMER BATT?
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24V LEAD ACID BATT IN THE NOSE
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WHAT ARE THE GEN CONTROL UNIT (GCU) FUNCTIONS?
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1) VOLTAGE REGULATION \
\ 2) CURRENT LIMITING\ \ 3) BACKUP STARTER CUTOFF\ \ 4) LINE CONTACTOR CONTROL\ \ 5) OVER VOLTAGE PROTECTION\ \ 6) UNDER VOLTAGE PROTECTION\ \ 7) OVERSPEED (STARTER RUN AWAY) \ PROTECTION \ \ 8) STARTER ABORT OPERATION\ \ 9) DIFFERENTIAL CURRENT \ PROTECTION |
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WHAT TRIGGERS THE AUTO APR?
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15% DIFFERENCE IN N2's
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HI FLOW MUST BE OFF WHEN?
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1) T/O\
\ 2) L/D\ \ 3) > 30,000'\ \ 4) WHEN USING ANTI-ICE |
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WHAT REGULATES HP AND LP IN THE ECS?
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ECS VALVE CONTROLLER
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DOES EMER PRESS FAIL OPEN OR CLOSED?
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CLOSED
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ABOVE WHAT ALTITUDE IS THE ACM BYPASSED?
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40,000'
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HOW MANY OUTFLOW VALVES ARE THERE?
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2 - CONNECTED VIA A SLAVING LINE
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NACELLE HEATS FAIL OFF OR ON?
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ON
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WILL NACELLE HEAT WORK IF BLEEDS ARE OFF?
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YES
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HOW MANY FILTERS ARE IN THE MAIN AND AUX HYDRAULIC SYSTEMS?
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4: 2 IN HE MAIN AND 2 IN THE AUX
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WHAT DETERMINES THE TRIM SPEED?
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THE FLAP POSITION
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WHEN WILL YOU HEAR THE TRIM "CLACKER"?
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DURING AUTOPILOT TRIM MORE THAN 2-3SEC
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WHERE IS THE ROLL TRIM TAB?
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ON THE LEFT AILERON
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WHEN IS THE RUDDER BOOST ARMED?
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1) WHEN THE RUDDER BOOST SWITCH IS SELECTED\
\ 2) < 180 KIAS\ \ 3) FLAPS EXTENDED MORE THAN 3 DEGREES |
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WHAT DO THE AUTO SPOILERS NEED TO OPERATE?
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1) ARMED\
\ 2) WOW\ \ 3) TLs AT IDLE OR CUTOFF |
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WHAT LIMITS SPOILER EXTENSION RANGE?
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AIRSPEED, < 175kts FOR FULL EXTENSION
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HOW DO YOU KNOW IF THE FIRE BOTTLE DISCHARGED OR THE SQUIB FIRED?
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WHEN THE "ARMED" EXTINGUISHER LIGHT GOES OUT
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DURING FIRE TEST WHEN SHOULD YOU HEAR THE ORAL APU FIRE SIREN? WHY SHOULD YOU BE CAUTIONS?
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15sec YOU SHOULD HEAR THE SIRE\
\ IF YOU HOLD IT FOR 30sec YOU WILL INITIATE THE APU FIRE SHUTDOWN PROCESS THAT DISCHARGES FIRE BOTTLE |
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WHAT ARE THE ABORTED T/O SPEED AND TIME LIMITS?
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1) < 40KT: NONE\
\ 2) 40-80KT: 20 MIN, VISUAL INSPECTION\ \ 3) > 80KT UNDER MAX BRAKE ENERGY T/O WT: 1HR, VISUAL INSPECTION\ \ 4) > 80KT OVER MAX BRAKE ENERGY T/O WT: MX HIGH ENERGY STOP INSPECTION\ \ *Do not attempt a third takeoff after two rejected takeoffs without a 4-hour waiting period and another visual inspection |
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WHY DO YOU SET T/O TRIM?
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ITS SET FOR THE BEST SINGLE ENGINE CLIMB PER A/C WEIGHT
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WHAT WOULD GIVE YOU A T/O CONFIGURATION ALERT?
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1) PITCH TRIM BIAS NOT AT ZERO\
\ 2) SPOILERS EXTENDED\ \ 3) PITCH, AILERON, OR RUDDER TRIM NOT SET T/O\ \ 4) PITCH TRIM MISCOMPARE \ \ 5) PARKING BRAKE SET\ \ 6) TR UNLOCK OR DEP |
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WHAT DOES THE #2 IAC CONTROL?
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1) A/P\
\ 2) YAW DAMPER\ \ 3) RUDDER BOOST\ \ 4) INDEPENDENT FD |
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HOW MANY MAIN GEAR NEED TO BE DOWN TO DEPLOY TRs?
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ONLY ONE MAIN WHEEL SQUAT SWITCH
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CAN THE GENS COME ONLINE IF A GPU IS CONNECTED AND ON?
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NO, YOU MUST DESELECT THE GPU FIRST
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HOW IS THE OXY QUANTITY INDICATED?
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IN LITERS
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WHAT HELPS PREVENT COMPRESSOR STALLS AND SURGES?
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THE DEEC(S)
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WHEN THE DEECS ARE IN MANUAL MODE WHAT HELPS PREVENT COMPRESSOR STALLS AND SURGES?
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SURGE BLEED VALVE STAYS 1/3 OPEN
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WHY SHOULD YOU NOT T/O WITH "APU FAIL" CAS?
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APU FUEL SHUTOFF VALVE MAY NOT BE CLOSED
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WHAT SHOULD THE CABIN ALT BE WHEN AT THE MAX A/C ALT IN AUTO MODE?
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8,000 CABIN ALT @ FL510
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HOW LONG IS THE T/O FIELD ELEVATION KEPT IN THE CABIN PRESS MEMORY FOR EMER RETURN?
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10MIN, IF THE FLIGHT ALT HAS NOT EXCEEDED 6,000 ABOVE THE T/O FIELD ELEVATION
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WHEN IS THE RUDDER BOOST ARMED?
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1) FLAPS EXTENDED BEYOND 3 DEGREES\
\ 2) < 180 KTS |
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WHAT DOES THE PITCH TRIM BIAS DO?
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DURING A JAMMED STABALIZER IT BIASES OR OFFSETS THE FORCE IMPOSED BY THE UP-DOWN SPRING
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WHAT ARE THE TEMPERATURES FOR "ICING"?
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+10 TO -40 C WITH VISIBLE MOISTURE
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WHAT IS A "WET" RUNWAY?
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IT HAS A SHINY APPEARANCE DUE TO THIN LAYER OF WATER
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WHAT IS A "CONTAMINATED" RUNWAY?
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> 0.125in (3mm) OF STANDING WATER
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HOW DO YOU COMPUTE LANDING DISTANCE WITH A CONTAMINATED RUNWAY?
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MULTIPLY THE DRY RUNWAY DISTANCE TIMES THE CONTAMINANT FACTOR
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HOW LONG WILL THE EMER BATT LAST WITH BOTH GENS AND BOTH BATTS FAILED?
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~ 1HR
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WHAT IS THE NON-STANDARD WAY TO SHUT THE APU DOWN DURING THE EMER EVAC?
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APU WILL SHUT DOWN WHEN THE RIGHT BATT IS SELECTED OFF
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WHAT IS THE BEST GLIDE SPEED WITH BOTH ENGINES INOP
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160 KTS
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WHAT IS THE GLIDE RATIO IF AT BEST GLIDE SPEED- 160KTS WITH BOTH ENGINES INOP
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2nm PER 1,000'
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WHAT WILL CAUSE A "CONFIGURATION" AURAL WARNING FOR TAKEOFF?
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WHEN EITHER TL IS ADVANCED TO MCR OR ABOVE WHILE THE PLANE IS ON THE GROUND AND:\
1) FLAPS NOT AT 8 OR 20\ \ 2) TRs NOT STOWED\ \ 3) PARKING BRAKE NOT RELEASED\ \ 4) ANY TRIM NOT IN T/O BAND\ \ 5) SPOILERS NOT RETRACTED\ \ 6) PITCH TRIM BIAS NOT AT ZERO |
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WHAT SPEED SHOULD YOU SLOW TO IF YOU HAVE A TR UNLOCK OR DEPLOY IN FLIGHT?
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160 KTS OR BELOW AS REQUIRED TO MAINTAIN FLIGHT
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WHAT DOORS HAVE PRESSURE SWITCHES THAT WILL GIVE A CAS MESSAGE?
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1) MAIN CABIN DOOR\
\ 2) EMERGENCY EXIT\ \ 3) BAGGAGE DOOR\ \ 4) TAILCONE ACCESS DOOR |
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WHAT BATTERY TYPE WILL OVERHEAT?
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Ni-Cad
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WHAT PUMPS WILL CONTINUE TO OPERATE WITH A WINDMILLING ENGINE
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1) FUEL\
2) HYDRAULIC\ \ **don't press the engine FIRE switch unless a fuel or hydraulic leak or fire is suspected to prevent pump damage |
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WHAT N1 SETTING IS REQUIRED FOR ANTI-ICING SYSTEMS OPERATION ON A SINGLE ENGINE?
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75% N1 OR HIGHER
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WHEN WILL THE "FUEL QTY LOW" CAS COME ON?
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350 # IN RESPECTIVE TANK
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ARE THE TRs AVAILABLE AFTER A SINGLE ENGINE LANDING?
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YES, IDLE REVERSE ON THE OPERATIVE ENGINE IS AVAILABLE
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WHAT DOES A ROLLING T/O DO TO THE T/O FIELD LENGTH?
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ADDS 300'
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WHAT APPROACH CATEGORY MINIMA IS THE 45 DURING A CIRCLING APPROACH?
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CATEGORY C\
\ 1.7NM RADIUS PROTECTED AIRSPACE |
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WHAT TYPE OF BATTERY IS THE EMER BATT?
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SEALED LEAD ACID
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WILL THE BUS-TIE CLOSE ON BATTERY POWER?
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NO
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HOW CAN YOU TELL IF YOU HAVE A BAD BATTERY?
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GEN AMPS HIGH ON CORRESPONDING SIDE BECAUSE THE GEN IS WORKING HARD ATTEMPTING TO RECHARGE IT
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WHERE IS THE AILERON TRIM TAB?
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LEFT AILERON
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SHOULD YOU MOVE THE AC WITH THE DOOR UNLOCKED?
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NO, THE BOTTOM HALF OF THE DOOR IS PART OF THE MAIN STRUCTURE SO TAXIING/TOWING CAN CAUSE DAMAGE
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HOW DO YOU TURN OFF THE DUs?
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DUs 1, 3, 4: AVIONICS MASTER\
DU 2: ROTARY KNOB |
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WHY SHOULD YOU TURN ON THE FMS(s) WHEN YOU TURN ON THE AVIONICS MASTERS?
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SO THE GPWS TESTS ACCURATELY, IF THEY/IT ARE NOT ON YOU WILL GET "TERRAIN INOP"
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WHEN IN FLIGHT HOW CAN YOU TEST IF YOU ARE IN "AIR" OR "GROUND" MODE FOR THE SQUAT SWITCHES?
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PRESS AND HOLD THE ROTARY TEST KNOB ON THE DISPLAY CONTROLLER. IF YOU ARE IN GROUND MODE YOU WILL SEE THE TEST PAGE ON THE DUs, IF YOU ARE IN AIR MODE IT WILL ONLY TEST THE RADAR ALTIMETER
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DOES THE AP USE PRIMARY OR SECONDARY TRIM SERVOS?
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SECONDARY (slower)
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CAN AP BE ON WITHOUT THE YD?
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NO
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CAN THE YD BE ON WITHOUT THE AP?
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YES
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CAN YOU TURN OFF THE FD IF THE AP IS ON?
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NO
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WHAT DISENGAGES THE AP AUTOMATICALLY?
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1) AP FAULTS\
2) SECONDARY PITCH TRIM FAULTS\ 3) POWER LOSS TO AP SERVOS\ 4) FAILURE OF EITHER IC600\ 5) AHRS FAILURE\ 6) STICK SHAKER\ 7) EXCESS: 35 DEGREES OF BANK, 25 DEGREES NOSE UP, 15 DEGREES NOSE DOWN |
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WHAT AIRCRAFT CONFIGURATION IS REQUIRED BEFORE YOU CAN ERASE THE CVR?
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1) BRAKE SET\
2) WEIGHT ON WHEELS |
