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135 Cards in this Set

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WHAT ARE THE EMERGENCY PROCEDURES FOR SMOKE AND FUME REMOVAL?
CREW OXEGEN MASK & GOGGLES ON.
ESTABLISH CREW COMMUNICATION.
MANUAL DUMP VALVE – AS REQUIRED.
OXEGEN SYSTEM BYPASS VALE – ON.
MEMORY ITEMS FOR SINGLE ENGINE GO-AROUND.
MAXIMUM THRUST.
APPROACH CLIMB SPEED (APPROX. 9 DEG. PITCH UP.
FLAPS – 12 DEG.
POSITIVE RATE – GEAR UP.
AT 400 FEET (MIN) – FLAPS UP.
ACCELERATE TO VFS SPEED.
MEMORY ITEMS FOR ENGINE FAILURE DURING TAKEOFF ABOVE V1 SPEED.
CONTINUE TAKE OFF.
MAXIMUM THRUST.
POSITIVE RATE – GEAR UP.
ACCELERATE TO V2.
AT 400 FEET (MIN.) – FLAPS UP.
ACCELERATE TO VFS.
MEMORY ITEMS FOR ENGINE FIRE IN FLIGHT.
AFFECTED ENGINE.
TRUST LEVER TO IDLE.
IF INDICATIONS OF FIRE PRESIST.
THRUST LEVER TO CUT OFF.
FIRE WARNING PUSH BUTTON – PUSH.
AFTER 5 SECONDS.
FULL/EMPTY PUSH BUTTON – PUSH.
MEMORY ITEMS FOR AN ENGINE FIRE DURING TAKE OFF ABOVE V1 SPEED.
MAXIMUM THRUST
POSITIVE RATE – GEAR UP.
ACCELERATE TO V2
400 FEET (MIN.) – FLAPS UP
ACCELERATE TO VFS.
PERFORM ENGINE FIRE IN FLIGHT PROCEDURE.
MEMORY ITEMS FOR RAPID DECOMPRESSION.
CREW O2 MASK ON.
ESTABLISH CREW COMMUNICATION.
CABIN AIR SELECTOR – EMERGENCY.
CABIN LIGHTS SWITCH – BELS/NO SMOKEING.
O2 BYPASS VALVE – ON.
ENSURE PASSANGERS ARE RECEIVING O2.
MEMORY ITEMS FOR ENGINE FIRE DURING TAKE OFF ROLE BEFORE V1 SPEED.
ABORT TAKE OFF!!!
THRUST LEVERS – IDLE.
BRAKES – MAXIMUM.
LD’S – DEPLOY.
TR’S – DEPLOY.
CONTROL TOWER – CALL.
MEMORY ITEMS FOR ABORTED TAKE OFF.
THRUST LEVERS – IDLE.
BRAKES – MAXIMUM.
LD’S – DEPLOY.
TR’S – DEPLOY.
CONTROL TOWER – CALL.
MEMORY ITEMS FOR SMOKE OR FUME REMOVAL.
CREW O2 MASK & GOGGLES – ON.
ESTABLISH CREW COMMUNICATIONS.
MANUAL DUMP VALVE – ON.
O2 SYSTEM BYPASS VALE – ON.
MEMORY ITEMS FOR A FAN BLADE FAILURE.
NOTE: ENGINE DOES NOT RESPOND TO THRUST LEVER MOVEMENT ON N1 OR N2.
AFFECTED ENGINE.
IDENTIFY.
THRUST LEVER – IDLE POSITION.
MEMORY ITEMS FOR INADVERTANT TR DEPLOYMENT (UNSAFE LIGHT ON)
DURING TAKE OFF ABOVE V1.
TAKE CONTROL OF FLIGHT CONTROLS.
PULL CIRCUIT BREAKERS.
BELOW V1.
ABORT TAKE OFF.
WHAT IS THE MAXIMUM TAKEOFF WEIGHT?
23,500 POUNDS.
WHAT IS THE MAXIMUM RAMP WEIGHT?
23,650 POUNDS.
WHAT HEATS THE FUEL?
FUEL HEATER WHICH IS HEATED BY HOT OIL.
HOW DO YOU KNOW IF FUEL IS IN THE TIP TANKS?
BLUE LIGHT
HOW DO YOU TRANSFER FUEL OUT OF TIP TANKS?
BY THE 3 POSITION SWITCH.
MANUAL OR AUTO.
CAN YOU LAND WITH FUEL IN THE TIP TANKS?
NO
WHEN WILL THE AUTOMATIC TRANSFER BEGIN TO TRANSFER FUEL FROM THE TIP TANKS TO THE WING TANKS?
AS THE LEVEL DROPS BELOW 6600 TO 6700 LBS.
WHAT WILL YOU SEE IN FUEL TRANSFER?
IN TRANSIT LIGHTS.
WHAT DO THE FUEL INTERCONNECT VALVES DO?
ALLOW FUEL TO FLOW TO THE LOWER FUSELAGE TANK THAT CONTAINS LESS FUEL TILL THE 2 TANKS ARE EQUAL.
WHEN WILL THE FUEL DUMP AUTOMATICALLY STOP?
WHEN 1960 LBS. OF FUEL REMAINS.
WHAT IS THE MINIMUM VOLTAGE REQUIRED TO CLOSE BATT. CONTACTOR?
22 VOLTS.
CAN YOU CHARGE THE BATTERIES ON THE GROUND?
YES.
WHAT BUS IS CONNECTED TO THE GENERATOR?
THE GENERATOR BUSS.
WHAT CONSUMERS ARE OFF THE BATTERY BUSS?
FLAPS.
MEMORY ITEMS FOR AN ENGINE FIRE DURING GROUND START OR SHUTDOWN.
AFFECTED ENGINE.
THRUST LEVER – CUT OFF.
START SWITCH – MOTOR TILL FIRE IS OUT.
IF FIRE DOES NOT EXTINGUISH.
FIRE WARNING BUTTON – PRESS.
FULL EMPTY BUTTON – PRESS.
MEMORY ITEMS FOR EMERGENCY DECENT.
THRUST LEVERS – IDLE.
SPEED BRAKES SWITCH – EXTEND.
DECLARE AN EMERGENCY.
DECENT SPEED - .8 MACH OR 365 KTS.
WHAT IS THE ITT MAX TEMP FOR START ?
907 DEG. CELCIUS.
WHAT IS THE ITT MAX TEMP/TIME FOR TAKE OFF ?
907 DEG CELCIUS FOR 5 MIN.
WHAT IS THE ITT MAX TEMP/TIME FOR TAKE OFF TRANSIENT ?
907 DEG C – 939 DEG C FOR 10 SEC.
WHAT IS THE MAX CONTINUIOUS ITT TEMP/TIME ?
885 DEG. C FOR 30 MIN.
WHAT IS THE ITT MAX TEMP FOR CRUISE ?
849 DEG. CELCIUS.
WHAT IS THE MINUMUN FLIGHT WEIGHT ?
12,000 POUNDS.
WHAT IS THE BASIC EMPTY WEIGHT ?
13,500 POUNDS.
WHAT IS THE FORWARD BAGGAGE WEIGHT LIMIT?
820 POUNDS.
WHAT IS THE AFT BAGGAGE WEIGHT LIMIT?
250 POUNDS.
WHAT IS THE USABLE FUEL IN POUNDS AND GALLONS?
8910 POUNDS.
1330 GALLONS.
WHAT IS THE NORMAL CLIMB ITT TEMPERATURE?
870 DEG. CELCIUS.
IF THE FUEL LEVEL LOW LIGHT COMES ON HOW MUCH FUEL IS LEFT IN THE TANK?
415 LBS.
WHAT ITEMS ARE HOT WIRED TO THE BATTERY?
BAGGAGE LIGHTS
STEP AND ENTRANCE LIGHT.
BATTERY VOLT METER.
SINGLE POINT REFULING.
WHY DO YOU HAVE TO TURN THE ANTI-SKID OFF TO PARK THE AIRPLANE?
IT CLOSES THE ANTI-SKID CONTROL VALVE AND TRAPS HYDRAULIC PRESSURE.
NO BRAKES ON LANDING WHAT DO YOU DO?
TURN OFF THE ANTI-SKID.
MAX TR’S. IF NEEDED.
WHAT ARE SPEED BRAKE LIMITATIONS?
NONE EXCEPT NOT TO BE USED FOR TAKE OFF OR LANDING.
WHAT ARE THE LIFT DUMPER LIMITATIONS?
ONLY TO BE USED ON THE GROUND!
WHAT PANELS ARE THE LD’S?
3 PANELS PER SIDE. THE SPEED BRAKES DEPLOY.
WHAT PANELS ARE THE SB’S?
THE OUT BOARD PANEL ON EACH WING.
WHAT PREVENTS THE LD’S TO DEPLOY IN-FLIGHT?
SQUAT SWITCH.
HOW DO YOU USE THE SECONDARY TRIM SYSTEM?
PRESS THE TRIM DISCONNECT BUTTON ON THE RIGHT SIDE OF THE YOKE AND USE THE TOGGLE SWITCH.
WHAT PRECAUTION MUST BE TAKEN WHEN USING THE SECONDARY TRIM SYSTEM?
NO PROTECTION ON THE MOTOR.
WHAT DO YOU DO IF YOU GET A SPLIT FLAP (FLAP IMBALANCE)?
DON’T USE FLAPS.
WHAT POSITION SHOULD THE OUTFLOW SAFETY VALVES BE IN DURING WALK AROUND?
CLOSED.
GENERATOR OFF LIGHT COMES ON WHAT DO YOU LOOSE?
NOTHING.
WHAT ITEMS WOULD YOU CONSIDER TO LOAD SHEAD?
COFFEE POT, LIGHTS, GALLEY POWER, BAGGAGE HEAT, ETC...
WHAT ARE THE FUNCTIONS OF THE GCU.?
CONTROLS THE STARTER GENERATOR DURING START CYCLES.
PROVIDES VOLTAGE REGULATION.
PROTECTS THE AIRCRAFT ELECTRICAL SYSTEM FROM GENERATOR FAULTS DURING OPERATION.
IF THE #1 OR #2 AC BUSS LIGHT COMES ON WHAT IS THIS TELLING YOU?
THE 115V AC BUSS IS LESS THAN 100 VOLTS AC.
WHAT TYPE OF HYDRAULIC FLUID DOES THE WESTWIND USE?
SKYDROL OR EQUIVALENT.
WHAT PSI DOES THE MAIN HYDROLIC SYSTEM PROVIDE?
2000 PSI.
WHAT PSI DOES THE EMERGENCY HYDRAULIC SYSTEM PROVIDE?
750 –1,300 PSI.
WHAT IS THE PURPOSE OF THE EMERGENCY HYDRAULIC SYSTEM?
IT PROVIDES 750 – 1,300 PSI TO THE EMERGENCY BRAKE SYSTEM.
WHAT IS THE HYDRAULIC FLUID CAPACITY?
1.2 GALLONS.
WHAT IS THE CAPACITY OF THE STANDPIPE?
1 PINT.
WHAT SYSTEMS ARE HYDRAULICALLY OPERATED?
LANDING GEAR
BRAKES.
ANTI-SKID.
NOSE WHEEL STEARING.
LD’S & SB’S.
TR’S.
WHAT SUPPLES POWER TO THE EMERGENCY BRAKES?
EMERGENCY HYDROLIC SYSTEM.
WHAT IS IDLE THRUST?
250 LBS.
WHEN MUST YOU PRE HEAT THE ENGINES?
TEMBERATURES LESS THAN 40 DEG. C.
IS THE A/C PRESSURIZED IF THE SWITCH IS IN THE EMERGENCY POSITION? WHAT ARE THE PRECAUTIONS?
YES.
CABIN HEAT IS DIRECTLY CONTROLLED BY THRUST SETTING ON THE RT. ENGINE.
ON THE GROUND, HOW DO YOU INCREASE THE AIR CONDITIONING?
TURN CABIN AIR SELECTOR TO RIGHT ENGINE AND ADVANCE THE RIGHT THRUST LEVER
HOW MUCH ICE SHOULD YOU ALLOW TO BUILD PRIOR TO USING THE BOOTS?
APPROX. ½ INCH.
WHAT WILL CAUSE THE DE-ICE LIGHT TO COME ON? 
TO MUCH OR NOT ENOUGH VACUUM OR PRESSURE.
IF THE DE-ICE LIGHT COMES ON IN-FLIGHT WHAT DON’T YOU WANT TO DO?
DON’T USE THE DE-ICE SYSTEM AS IT MOST LIKELY A HIGH PRESSURE ISSUE.
HOW MUCH FUEL SHOULD REMAIN PRIOR TO MANUAL TRANSFER?
6500 LBS.
WHAT TYPE ENGINES ON ON THE WESTWIND?
GARRETT TFE-731-3-1G
HOW MUCH THRUST DO THE GARRETT 731-3-1G SUPPLY AT SEA LEVEL?
3700 LBS PER SIDE.
HOW MANY VOLT AMPS ARE THE INVERTERS RATED AT?
1000 VA PER INVERTER.
HOW MANY VOLTS DO THE INVERTERS PROVIDE?
115 VAC
26 VAC
WHAT TYPE OF FLAPS DOES THE WESTWIND HAVE?
HIGH LIFT, DOUBLE - SLOTTED FOWLER FLAPS.
WHAT IS THE MAXIMUM TIRE SPEED?
200 MPH OR 174 KTS.
MAX ALT FOR THE CABIN AIR TO BE IN THE RAM POSITION.
13000 FEET.
MINIMUM FIELD ELEVATION FOR TAKE OFF.
-2,000 FEET.
MAXIMUM FIELD ELEVATION FOR TAKE OFF.
10,000 FEET.
LOAD LIMITS FLAPS AND GEAR UP.
2.8 TO –1.0 G’S.
LOAD LIMITS FLAPS AND GEAR DOWN.
+2.0 TO –0.0 G’S.
MAX TAILWIND COMPONENT.
10 KTS.
WHAT IS LOWEST ALTITUDE YOU MAY USE THE AUTOPILOT DURING TAKE OFF OR LANDING?
CATEGORY 1 LANDING MINIMUMS.
WHAT IS THE MAXIMUM RUNWAY SLOPE?
2% UP
START CYCLE LIMITATIONS.
15 SECONDS ON 20 SECONDS OFF FOR 3 CYCLES, THAN 20 MIN OFF.
WHAT IS THE MAXIMUM CABIN DIFFERENTIAL PRESSURE?
9.0 PSI
MAY YOU TAKE OFF WITH ONLY ONE OF THE STABILIZER TRIM SYSTEMS WORKING.
NO.
WHAT IS THE MAXIMUM FUEL IMBALANCE FOR TAKE OFF?
300 POUNDS.
WHAT IS THE MAXIMUM FUEL IMBALANCE FOR IN FLIGHT?
800 POUNDS.
AT WHAT ALTITUDE MUST THE CREW USE OXYGEN?
41,000 FEET.
WHERE DO THE BOOST PUMPS GET THERE POWER FROM?
THE LEFT MAIN AND RIGHT ALT GET THERE POWER FROM THE #2 MAIN BUSS.
THE RIGHT MAIN AND LEFT ALT GET THERE POWER FROM THE #1 MAIN BUSS.
WHEN WILL YOU GET A FUEL PRESSURE LOW INDICATOR?
WHEN FUEL PRESSURE IN THE SUPPLY LINE DROPS BELOW 7 PSI.
WHAT 5 INPUTS GO INTO THE ELECTRONIC ENGINE CONTROL?EEC’S)
N1
N2
ITT
PLA (POWER LEVEL ANGLE
PT2/ TT2
OIL SHOULD BE CHECKED WITHIN HOW MANY MINUITS FROM SHUTDOWN?
15 MINUITS.
WHAT SHOULD YOU SEE WHEN YOU PUSH THE TR FAULT TEST BUTTON?
NO LIGHTS.
HOW MANY FUEL TANKS ARE THERE?
12 FUEL TANKS, 6 PER SIDE.
WHAT PSI IS THE SURFACE DE-ICE REGULATED TO?
18 PSI.
WHAT TYPES BATTERIES ARE IN THE WESTWIND?
TWO 24 VOLT NICAD BATERIES CONNECTED IN PARRELL RATED AT 36 AMP/HRS.
WHEN THE BATTERY SWITCH IS TURNED ON HOW MANY BUSSES COME ONLINE?
7.
WHAT DOES THE GCU PROVIDE DURING STARTING?
FIELD WEAKING.
START TERMINATION.
ANTI-RUNAWAY PROTECTION.
WHAT DOES THE GCU PROVIDE DURING GENERATION OF POWER?
VOLTAGE REGULATION
REDUCTION OF CHARGING RATE
LOAD SHARING.
CURRENT LIMITING.
PROTECTION DURING EXTERNAL POWER START. (RCR STAYS OPEN).
GENERATOR OUTPUT REGULATION.
LOAD SHARING.
WHAT SHOULD THE GPU BE SET TO FOR A EXTERNAL POWER START?
28 V / 1000 AMPS.
THRUST REVERSERS SHOULD BE LIMITED TO TO WHAT TIMES?
1 MINUTE
OR 3 CYCLES IN 15 MINUTES
IF N1 OR N2 EXCEED 105% WHAT MUST BE DONE?
ENGINE REMOVAL.
START TIMES FROM:
10% N2 TILL LIGHTOFF.
LIGHTOFF TILL IDLE.
10 SECONDS FROM 10% N2-LIGHTOFF.
50 SECONDS FROM LIGHTOFF-IDLE.
WHAT ARE THE STARTER GENERATERS RATED AT?
30 VOLTS DC YET REGULATED TO 28.5 VOLTS DC.
WHAT IS THE PURPOSE OF THE WINGLETS ON THE WESTWIND 2?
REDUCE DRAGE AND PROVIDE BETTER FUEL CONSUMPTION.
WHAT IS A PROBLUM CAUSED BY THE WINGLETS?
THEY CAUSE A DUTCH ROLL TENDENCY.
WHY ARE BOTH AC SWITCHES SET TO ALT FOR SHUTDOWN?
TO DE-POWER THE INVERTERS.
IF BOTH GENERATORS FAIL APPROXIMATLY HOW LONG TILL BATTERYS GO DEAD?
15 MINUTES, IF CURRENT IS NOT REDUCED.
WHEN WILL THE ENGINE FIRE DETECTION LIGHT COME ON?
A 800 DEG. F HOT SPOT OR 400 DEG. F OVERALL TEMP.
WHAT HAPPENS WHEN YOU PUSH THE ILLUMINATED FIRE SWITCH?
IT CLOSES THE FUEL SHUTOFF VALVE ON THE AFFECTED ENGINE
CLOSES THE HYDROLIC SHUTOFF VALVE TO THE AFFECTED ENGINE.
ARMS THE CARTRIDGE.
ILLUMINATES THE FULL LIGHT.
WHAT HAPPENS WHEN YOU PUSH THE FULL/EMPTY SWITCH?
DETONATES THE CHARGE ON THE APPROPRIATE SQUIB.
RELEASES HALON IN ONE CYLENDER.
ILLUMINATES THE EMPTY LIGHT.
WHAT DOES THE FUEL STORAGE SYSTEM CONSIST OF?
FUSELAGE TANKS
WING TANKS
WING TIP TANKS
OPIONAL AUX TANK.
WHAT DOES THE FUEL DISTRIBUTION SYSTEM CONSIST OF?
PUMPS
VALVES
PLUMBING
WHAT DOES THE FUEL QUANTITY INDICATION SYSTEM CONSIST OF?
FUEL INDICATORS
ANNUNCIATORS
PROBES AND SENSORS
FOR TRIP PLANNING WHAT SHOULD BE USED FOR FUEL BURN IN POUNDS FOR THE 1ST, 2ND AND 3RD HOUR.
1ST – 1800 LBS
2nd – 1500 LBS.
3RD – 1400 LBS.
WHAT TRANSFERS FUEL FROM THE WING TIP TANKS TO THE WING TANKS?
GRAVITY
JET PUMPS LOCATED IN EACH TIP TANK.
WHAT TRANSFERS FUEL FROM THE WING TIP TANKS TO THE WING TANKS?
GRAVITY
JET PUMPS LOCATED IN EACH TIP TANK.
WHAT TRANSFERS FUEL FROM THE WING TIP TANKS TO THE WING TANKS?
GRAVITY
JET PUMPS LOCATED IN EACH TIP TANK.
WHAT TRANSFERS FUEL FROM THE WING TIP TANKS TO THE WING TANKS?
GRAVITY
JET PUMPS LOCATED IN EACH TIP TANK.
HOW MANY BOOST PUMPS ARE THERE AND WHERE ARE THEY LOCATED?
4 BOOST PUMPS.
2 IDENTICAL PUMPS IN EACH LOWER FUSELAGE TAKE. NOTE:1 MAIN AND 1 ALT PER SIDE.
WHAT ARE THE TWO TYPES OF FUEL DUMPING?
GRAVITY.
BOOSTED.
HOW IS A GRAVITY DUMP PERFORMED AND AT WHAT RATE IS FUEL DUMPED?
PRESS THE DUMP PUSHBUTTON.
200 PPM PER SIDE OR 400 PPM TOTAL.
HOW IS A BOOSTED DUMP PERFORMED AND AT WHAT RATE IS FUEL DUMPED?
PRESS THE DUMP PUSHBUTTONS.
TRANSFER SWITCH OPEN.
INTERCONNECT SWITCH OPEN.
333 PPM PER SIDE OR 666 PPM TOTAL.
NOTE: ONCE THE TIP TANKS ARE EMPTY FUEL DUMPS AT 133 PPM PER SIDE OR 266 PPM TOTAL TIL DUMP BUTTON IS DE-ENERGIZED.
WHAT IS IDICATED BYA A MAIN BOOST PUMP FAILURE?
MOMENTARY FUEL PESSURE LOW LIGHT.
STEADY ALT BOOST PUMP ON ANNUNCIATOR.
WHAT TRANSFERS FUEL FROM THE WING TIP TANKS TO THE WING TANKS?
GRAVITY
JET PUMPS LOCATED IN EACH TIP TANK.
WHAT TRANSFERS FUEL FROM THE WING TIP TANKS TO THE WING TANKS?
GRAVITY
JET PUMPS LOCATED IN EACH TIP TANK.
WHAT TRANSFERS FUEL FROM THE WING TIP TANKS TO THE WING TANKS?
GRAVITY
JET PUMPS LOCATED IN EACH TIP TANK.
HOW MANY BOOST PUMPS ARE THERE AND WHERE ARE THEY LOCATED?
4 BOOST PUMPS.
2 IDENTICAL PUMPS IN EACH LOWER FUSELAGE TAKE. NOTE:1 MAIN AND 1 ALT PER SIDE.
WHAT ARE THE TWO TYPES OF FUEL DUMPING?
GRAVITY.
BOOSTED.
HOW IS A GRAVITY DUMP PERFORMED AND AT WHAT RATE IS FUEL DUMPED?
PRESS THE DUMP PUSHBUTTON.
200 PPM PER SIDE OR 400 PPM TOTAL.
HOW IS A BOOSTED DUMP PERFORMED AND AT WHAT RATE IS FUEL DUMPED?
PRESS THE DUMP PUSHBUTTONS.
TRANSFER SWITCH OPEN.
INTERCONNECT SWITCH OPEN.
333 PPM PER SIDE OR 666 PPM TOTAL.
NOTE: ONCE THE TIP TANKS ARE EMPTY FUEL DUMPS AT 133 PPM PER SIDE OR 266 PPM TOTAL TIL DUMP BUTTON IS DE-ENERGIZED.
WHAT IS INDICATED BY A MAIN BOOST PUMP FAILURE?
MOMENTARY FUEL PESSURE LOW LIGHT.
STEADY ALT BOOST PUMP ON ANNUNCIATOR.