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