Limitations

Question 1

CERTIFICATION STATUS

-THIS CITATION LATITUDE IS CERTIFIED IN ACCORDANCE WITH 14 CFR PART____

Answer 1

CERTIFICATION STATUS

-THIS CITATION LATITUDE IS CERTIFIED IN ACCORDANCE WITH 14 CFR PART-25

Question 2

WEIGHT LIMITS
MAXIMUM DESIGN
RAMP WEIGHT\_\_\_\_\_
TAKEOFF WEIGHT\_\_\_\_\_
LANDING WEIGHT\_\_\_\_\_
ZERO FUEL WEIGHT\_\_\_\_\_
MAXIMUM TAIL CONE BAGGAGE WEIGHT\_\_\_\_\_

Answer 2

WEIGHT LIMITS
MAXIMUM DESIGN
RAMP WEIGHT-31,050 POUNDS
TAKEOFF WEIGHT-30,800 POUNDS
LANDING WEIGHT-27575 POUNDS
ZERO FUEL WEIGHT-21430 POUNDS
MAXIMUM TAIL CONE BAGGAGE WEIGHT-1000 POUNDS

Question 3

FUEL LIMITS
THE CORRESPONDING ELECTRIC FUEL BOOST PUMP SWITCH MUST BE TURNED_____WHEN THE AMBER FUEL LEVEL LOW AND/OR R CAS MESSAGE IS DISPLAYED AT_____POUNDS OR LESS OF INDICATED FUEL IN EITHER TANK.

MAXIMUM ASYMMETRIC FUEL DIFFERENTIAL FOR NORMAL OPERATIONS_____

A LATERAL FUEL IMBALANCE OF_____POUNDS HAS BEEN DEMONSTRATED FOR EMERGENCY RETURN

Answer 3

FUEL LIMITS
THE CORRESPONDING ELECTRIC FUEL BOOST PUMP SWITCH MUST BE TURNED-ON WHEN THE AMBER FUEL LEVEL LOW AND/OR R CAS MESSAGE IS DISPLAYED AT-600 POUNDS OR LESS OF INDICATED FUEL IN EITHER TANK.

MAXIMUM ASYMMETRIC FUEL DIFFERENTIAL FOR NORMAL OPERATIONS-400 POUNDS

A LATERAL FUEL IMBALANCE OF-800 POUNDS HAS BEEN DEMONSTRATED FOR EMERGENCY RETURN

Question 4

SINGLE POINT REFUELING

• SINGLE POINT REFUELING OPERATIONS MUST BE ACCOMPLISHED PER THE PROCEDURES CONTAINED ON THE PLACARDS INSTALLED ON THE SINGLE POINT REFUELING_____
• REFUELING PRESSURE RANGE_____
• DEFUELING PRESSURE RANGE_____

Answer 4

SINGLE POINT REFUELING

• SINGLE POINT REFUELING OPERATIONS MUST BE ACCOMPLISHED PER THE PROCEDURES CONTAINED ON THE PLACARDS INSTALLED ON THE SINGLE POINT REFUELING-ACCESS DOOR
• REFUELING PRESSURE RANGE-10-55PSI
• DEFUELING PRESSURE RANGE-0-10PSI

Question 5

TAKEOFF AND LANDING OPERATIONAL LIMITS
-MAXIMUM ALTITUDE LIMIT (CONFIGURATION AD)_____

• MAXIMUM ALTITUDE LIMIT (CONFIGURATION AE)_____
• MAXIMUM TAILWIND COMPONENT_____
• PASS OXY KNOB MUST BE SET TO_____PRIOR TO TAKEOFF IF CARRYING PAX

Answer 5

TAKEOFF AND LANDING OPERATIONAL LIMITS
-MAXIMUM ALTITUDE LIMIT (CONFIGURATION AD)-14,000FT (HI ELEVATION MODE)

• MAXIMUM ALTITUDE LIMIT (CONFIGURATION AE)-8000FT (NORMAL MODE)
• MAXIMUM TAILWIND COMPONENT-10KTS
• PASS OXY KNOB MUST BE SET TO-AUTO PRIOR TO TAKEOFF IF CARRYING PAX

Question 6

TAKEOFF AND LANDING OPERATIONAL LIMITS

• THE AUTOPILOT AND YAW DAMPER MUST BE DISENGAGED FOR_____
• THE LAVATORY DOORS MUST BE LATCHED_____FOR TAKEOFF AND LANDING
• TAKEOFF AND LANDINGS ARE LIMITED TO_____RUNWAY SURFACES
• EXCEPT WHERE OTHERWISE SPECIFIED BY AFM PROCEDURES, SPEEDBRAKES MUST BE STOWED PRIOR TO_____ FEET AGL FOR LANDING
• TAKEOFF IS LIMITED TO THE FLAPS_____ CONFIGURATION WHEN TYPE II,III,IV ANTI ICE FLUID HAS BEEN APPLIED TO THE AIRPLANE

Answer 6

TAKEOFF AND LANDING OPERATIONAL LIMITS

• THE AUTOPILOT AND YAW DAMPER MUST BE DISENGAGED FOR-TAKEOFF AND LANDING.
• THE LAVATORY DOORS MUST BE LATCHED-OPEN FOR TAKEOFF AND LANDING
• TAKEOFF AND LANDINGS ARE LIMITED TO-PAVED RUNWAY SURFACES
• EXCEPT WHERE OTHERWISE SPECIFIED BY AFM PROCEDURES, SPEEDBRAKES MUST BE STOWED PRIOR TO-500 FEET AGL FOR LANDING
• TAKEOFF IS LIMITED TO THE FLAPS-1 CONFIGURATION WHEN TYPE II,III,IV ANTI ICE FLUID HAS BEEN APPLIED TO THE AIRPLANE

Question 7

TAKEOFF AND LANDING OPERATIONAL LIMITS
-TAKEOFF MAY NOT BE INITIATED WITH A_____ MESSAGE DISPLAYED. TAKEOFF MAY NOT BE INITIATED WITH AN_____MESSAGE DISPLAYED UNLESS THE ASSOCIATED SYSTEM OR COMPONENT HAS BEEN DEFERRED PER AN APPROVED MINIMUM EQUIPMENT LIST (MEL). TAKEOFF MAY NOT BE INITIATED WITH A_____MESSAGE IF THE PROCEDURE ASSOCIATED WITH THAT MESSAGE REQUIRES MEL ACTION,UNLESS THAT SYSTEM OR COMPONENT HAS BEEN DEFERRED PER THE MEL. WHEN DISPATCHING IN THIS MANNER,IF THE PROCEDURE ASSOCIATED WITH THER MESSAGE INCLUDES “LAND AS SOON AS PRACTICAL” AS A STEP, THE STEP MAY BE IGNORED.

Answer 7

TAKEOFF AND LANDING OPERATIONAL LIMITS
-TAKEOFF MAY NOT BE INITIATED WITH A-RED MESSAGE DISPLAYED. TAKEOFF MAY NOT BE INITIATED WITH AN-AMBER MESSAGE DISPLAYED UNLESS THE ASSOCIATED SYSTEM OR COMPONENT HAS BEEN DEFERRED PER AN APPROVED MINIMUM EQUIPMENT LIST (MEL). TAKEOFF MAY NOT BE INITIATED WITH A-WHITE MESSAGE IF THE PROCEDURE ASSOCIATED WITH THAT MESSAGE REQUIRES MEL ACTION,UNLESS THAT SYSTEM OR COMPONENT HAS BEEN DEFERRED PER THE MEL. WHEN DISPATCHING IN THIS MANNER,IF THE PROCEDURE ASSOCIATED WITH THER MESSAGE INCLUDES “LAND AS SOON AS PRACTICAL” AS A STEP, THE STEP MAY BE IGNORED.

Question 8

ENROUTE OPERATIONAL LIMITS

MAXIMUM OPERATING ALTITUDE_____

FOR OPERATIONS ABOVE FL410 THE FOLLOWING CONDITIONS MUST BE MET:
-BOTH ENG BLD AIR KNOBS MUST BE SELECTED TO____OR_____ AND BOTH ENGINE BLEED AIR SOURCES MUST BE AVAILABLE.
THE PRESS SOURCE KNOB MUST BE SELECTED TO_____

MAXIMUM ALTITUDE WITH FLAPS OR GEAR EXTENDED_____

Answer 8

ENROUTE OPERATIONAL LIMITS

MAXIMUM OPERATING ALTITUDE-FL450

FOR OPERATIONS ABOVE FL410 THE FOLLOWING CONDITIONS MUST BE MET:
-BOTH ENG BLD AIR KNOBS MUST BE SELECTED TO-NORM OR-HP AND BOTH ENGINE BLEED AIR SOURCES MUST BE AVAILABLE.
THE PRESS SOURCE KNOB MUST BE SELECTED TO-NORM

MAXIMUM ALTITUDE WITH FLAPS OR GEAR EXTENDED-FL180

Question 9

ENROUTE OPERATIONAL LIMITS

WHEN THE AIRPLANE HAS BEEN EXPOSED TO PROLONGED TEMPERATURES BELOW -30C THE CABIN MUST BE WARMED TO AT LEAST_____*C AS INDICATED ON MFD GTC HOME,AIRCRAFT SYSTEMS,TEMP PAGE BEFORE FLIGHT ABOVE_____ WITH ANY OCCUPANTS IN THE PASSENGER CABIN.

Answer 9

ENROUTE OPERATIONAL LIMITS

WHEN THE AIRPLANE HAS BEEN EXPOSED TO PROLONGED TEMPERATURES BELOW -30C THE CABIN MUST BE WARMED TO AT LEAST-21*C AS INDICATED ON MFD GTC HOME,AIRCRAFT SYSTEMS,TEMP PAGE BEFORE FLIGHT ABOVE-FL250 WITH ANY OCCUPANTS IN THE PASSENGER CABIN.

Question 10

REDUCED VERTICAL SEPARATION MINIMUMS

THE FOLLOWING EQUIPMENT MUST BE OPERATING NORMALLY UPON ENTERING RVSM AIRSPACE.

A_____
B_____
C_____
D_____

MINIMUM AIRSPEED IN RVSM AIRSPACE IS_____KIAS

Answer 10

REDUCED VERTICAL SEPARATION MINIMUMS

THE FOLLOWING EQUIPMENT MUST BE OPERATING NORMALLY UPON ENTERING RVSM AIRSPACE.

A-PILOT AND CO-PILOT PRIMARY ALTIMETERS
B-AUTOPILOT
C-ALTITUDE ALERTER
D-ATCRBS TRANSPONDER

MINIMUM AIRSPEED IN RVSM AIRSPACE IS-160 KIAS

Question 11

APPROVED OILS

MAXIMUM OIL CONSUMPTION IS 1 QT PER_____FLIGHT HOURS.

OIL TYPES OR_____MAY NOT BE MIXED UNLESS SPECIFICALLY APPROVED IN THE PW306D1 MAINTENANCE MANUALS.

Answer 11

APPROVED OILS

MAXIMUM OIL CONSUMPTION IS 1 QT PER-8 FLIGHT HOURS.

OIL TYPES OR-BRANDS MAY NOT BE MIXED UNLESS SPECIFICALLY APPROVED IN THE PW306D1 MAINTENANCE MANUALS.

Question 12

POWERPLANT LIMITS

CONTINUOUS GROUND STATIC OPERATION OF THE ENGINE AT TAKEOFF THRUST IS LIMITED TO A MAXIMUM OF_____ MINUTES.

ATTEMPTING AN ENGINE START IS PROHIBITED WITH A TAILWIND COMPONENT GREATER THAN_____KNOTS. WHEN STARTING WITH A QUARTERING TAILWIND THE DOWNWIND ENGINE MUST BE STARTED FIRST AND THE AIRPLANE TURNED INTO THE WIND PRIOR TO STARTING THE SECONF ENGINE.

THE ENGINE MUST BE OPERATED AT IDLE FOR AT LEAST_____MINUTES PRIOR TO SHUTDOWN. SMALL THRUST INCREASES FOR TAXI ARE ACCEPTABLE.

TO PRECLUDE LOW OIL PRESSURE,INTENTIONAL UNCOORDINATED FLIGHT OF GREATER THAN_____SLIP/SKID INDICATOR BAR WIDTH FOR LONGER THAN _____SECONDS IS PROHIBITED.

Answer 12

POWERPLANT LIMITS

CONTINUOUS GROUND STATIC OPERATION OF THE ENGINE AT TAKEOFF THRUST IS LIMITED TO A MAXIMUM OF-2 MINUTES.

ATTEMPTING AN ENGINE START IS PROHIBITED WITH A TAILWIND COMPONENT GREATER THAN-10 KNOTS. WHEN STARTING WITH A QUARTERING TAILWIND THE DOWNWIND ENGINE MUST BE STARTED FIRST AND THE AIRPLANE TURNED INTO THE WIND PRIOR TO STARTING THE SECONF ENGINE.

THE ENGINE MUST BE OPERATED AT IDLE FOR AT LEAST-2 MINUTES PRIOR TO SHUTDOWN. SMALL THRUST INCREASES FOR TAXI ARE ACCEPTABLE.

TO PRECLUDE LOW OIL PRESSURE,INTENTIONAL UNCOORDINATED FLIGHT OF GREATER THAN-1 SLIP/SKID INDICATOR BAR WIDTH FOR LONGER THAN -20 SECONDS IS PROHIBITED.

Question 13

ENGINE OPERATING LIMITS
STARTING:

MAX OBSERVED ITT *C_____

THE TOTAL TIME DURING WHICH TAKEOFF THRUST CAN BE USED IS LIMITED TO _____MINUTES PER FLIGHT. THE 5 MINUTE TIME LIMIT COMMENCES WHEN THE THROTTLE IS FIRST INCREASED to TO. THIS TIME MAY BE EXTENDED TO_____MINUTES FOR ONE ENGINE INOPERATIVE OPERATION.

AFTER COMPLETING A START UNDER COLD CONDITIONS AND ACHIEVING A STABILIZED GROUND IDLE,IT IS ACCEPTABLE TO RUN THE ENGINE UP TO_____%N1 TO DECREASE THE TIME REQUIRED FOR THE OIL TO REACH THE MINIMUM OPERATING TEMPERATURE OF_____*C

AFTER INITIATION OF THE START CYCLE,OIL PRESSURE MUST INDICATE AN INCREASE WITHIN_____SECONDS OF ENGINE LIGHT UP INDICATED BY A RISE IN ITT.

Answer 13

ENGINE OPERATING LIMITS
STARTING:

MAX OBSERVED ITT -950*C

THE TOTAL TIME DURING WHICH TAKEOFF THRUST CAN BE USED IS LIMITED TO -5 MINUTES PER FLIGHT. THE 5 MINUTE TIME LIMIT COMMENCES WHEN THE THROTTLE IS FIRST INCREASED to TO. THIS TIME MAY BE EXTENDED TO-10 MINUTES FOR ONE ENGINE INOPERATIVE OPERATION.

AFTER COMPLETING A START UNDER COLD CONDITIONS AND ACHIEVING A STABILIZED GROUND IDLE,IT IS ACCEPTABLE TO RUN THE ENGINE UP TO -82% N1 TO DECREASE THE TIME REQUIRED FOR THE OIL TO REACH THE MINIMUM OPERATING TEMPERATURE OF-16*C

AFTER INITIATION OF THE START CYCLE,OIL PRESSURE MUST INDICATE AN INCREASE WITHIN-20 SECONDS OF ENGINE LIGHT UP INDICATED BY A RISE IN ITT.

Question 14

START CYCLE LIMITS

ENGINE STARTER LIMIT
THE REST PERIODS BETWEEN ENGINE STARTS IS_____MINUTES AFTER THE FIRST START ATTEMPT,_____MINUTES AFTER THE SECOND, AND_____MINUTES AFTER THE THIRD.

                                                                NOTE THE ENGINE STARTER LIMIT IS INDEPENDENT OF STARTER POWER SOURCE (I.E., BATTERY, GENERATOR-ASSISTED CROSS START, AUXILIARY POWER UNIT, OR EXTERNAL POWER) AND ALSO APPLIES TO DRY AND WET MOTORING OF THE ENGINE.

Answer 14

START CYCLE LIMITS

ENGINE STARTER LIMIT
THE REST PERIODS BETWEEN ENGINE STARTS IS-2 MINUTES AFTER THE FIRST START ATTEMPT,-5 MINUTES AFTER THE SECOND, AND-30 MINUTES AFTER THE THIRD.

                                                                NOTE THE ENGINE STARTER LIMIT IS INDEPENDENT OF STARTER POWER SOURCE (I.E., BATTERY, GENERATOR-ASSISTED CROSS START, AUXILIARY POWER UNIT, OR EXTERNAL POWER) AND ALSO APPLIES TO DRY AND WET MOTORING OF THE ENGINE.

Question 15

START CYCLE LIMITS

ENGINE STARTER MOTORING LIMIT (NOT ENGINE START)
BATTERIES ONLY_____
BATTERIES WITHOUT GENERATOR ASSIST_____
EXTERNAL POWER (1000 AMPS)_____
EXTERNAL POWER (1500 AMPS)_____

APU STARTER LIMIT.
THREE APU STARTS PER_____MINUTES.
THREE STARTS WITH A_____SECOND REST PERIOD BETWEEN STARTS.

BATTERY START LIMIT
_____ENGINE BATTERY STARTS PER HOUR.
_____APU BATTERY STARS PER HOUR.

Answer 15

START CYCLE LIMITS

ENGINE STARTER MOTORING LIMIT (NOT ENGINE START)
BATTERIES ONLY-20 SECONDS
BATTERIES WITHOUT GENERATOR ASSIST-15 SECONDS
EXTERNAL POWER (1000 AMPS)-15 SECONDS
EXTERNAL POWER (1500 AMPS)-7 SECONDS

APU STARTER LIMIT.
THREE APU STARTS PER-30 MINUTES.
THREE STARTS WITH A-90 SECOND REST PERIOD BETWEEN STARTS.

BATTERY START LIMIT

• THREE ENGINE BATTERY STARTS PER HOUR.
• NINE APU BATTERY STARTS PER HOUR.

Question 16

START CYCLE LIMITS
NOTE
_____ENGINE EXTERNAL POWER STARTS (AVAILABLE EXTERNAL POWER CURENT GREATER THAN OR EQUAL TO 1000AMPS) ARE EQUIVALENT TO ONE ENGINE BATTERY START.

_____ENGINE EXTERNAL POWER START (AVAILABLE EXTERNAL POWER CURRENT LESS THAN 1000AMPS)IS EQUIVALENT TO ONE ENGINE BATTERY START.

_____GENERATOR-ASSISTED CROSS STARTS ARE EQUIVALENT TO ONE ENGINE BATTERY START.

_____APU BATTERY STARTS ARE EQUIVALENT TO ONE ENGINE BATTERY START.

Answer 16

START CYCLE LIMITS
NOTE
-3 ENGINE EXTERNAL POWER STARTS (AVAILABLE EXTERNAL POWER CURENT GREATER THAN OR EQUAL TO 1000AMPS) ARE EQUIVALENT TO ONE ENGINE BATTERY START.

• 1 ENGINE EXTERNAL POWER START (AVAILABLE EXTERNAL POWER CURRENT LESS THAN 1000AMPS)IS EQUIVALENT TO ONE ENGINE BATTERY START.
• 3 GENERATOR-ASSISTED CROSS STARTS ARE EQUIVALENT TO ONE ENGINE BATTERY START.
• 3 APU BATTERY STARTS ARE EQUIVALENT TO ONE ENGINE BATTERY START.

Question 17

EXTERNAL POWER LIMITS

MAXIMUM CURRENT_____
MAXIMUM VOLTAGE_____

Answer 17

EXTERNAL POWER LIMITS

MAXIMUM CURRENT-1500AMPS
MAXIMUM VOLTAGE-30VDC

Question 18

SPEED LIMITS

MAXIMUM OPERATING MACH NUMBER
Mmo ABOVE 29,833 FEET_____

MAXIMUM OPERATING KNOTS Vmo
8000 feet to 29,833 feet_____
Below 8000 feet_____

                                                                        Note    The maximum speed limits are lower for certain equipment failures.

Answer 18

SPEED LIMITS

MAXIMUM OPERATING MACH NUMBER
Mmo ABOVE 29,833 FEET-Mach0.80 (INDICATED)

MAXIMUM OPERATING KNOTS Vmo
8000 feet to 29,833 feet-305 KIAS
Below 8000 feet-270KIAS

                                                                        Note    The maximum speed limits are lower for certain equipment failures.

Question 19

SPEED LIMITS
WARNING
AVOID RAPID AND LARGE ALTERNATING CONTROL INPUTS,ESPECIALLY IN COMBINATION WITH LARGE CHANGES IN_____,ROLL OR YAW (E.G. LARGE SIDESLIP ANGLES), AS THEY MAY RESULT IN STRUCTURAL FAILURES AT ANY SPEED, INCLUDING BELOW Va.
NOTE
FULL APPLICATION OF RUDDER AND AILERON CONTROLS, AS WELL AS MANEUVERS THAT INVOLVE ANGLES OF ATTACK NEAR THE STALL, SHOULD BE CONFINED TO SPEEDS BELOW_____SPEED.

Answer 19

SPEED LIMITS
WARNING
AVOID RAPID AND LARGE ALTERNATING CONTROL INPUTS,ESPECIALLY IN COMBINATION WITH LARGE CHANGES IN-PITCH, ROLL OR YAW (E.G. LARGE SIDESLIP ANGLES), AS THEY MAY RESULT IN STRUCTURAL FAILURES AT ANY SPEED, INCLUDING BELOW Va.
NOTE
FULL APPLICATION OF RUDDER AND AILERON CONTROLS, AS WELL AS MANEUVERS THAT INVOLVE ANGLES OF ATTACK NEAR THE STALL, SHOULD BE CONFINED TO SPEEDS BELOW-MAXIMUM MANEUVERING AIRSPEED.

Question 20

SPEED LIMITS

MAXIMUM FLAP EXTENDED SPEED-Vfe
FLAPS 1 _____
FLAPS 2_____
FLAPS FULL_____

MAXIMUM LANDING GEAR.
OPERATING/EXTENDED SPEED- Vle/Vlo_____

MAXIMUM TURBULENT AIR PENETRATION SPEED_____

MAXIMUM SPEED BRAKE EXTENSION SPEED_____

Answer 20

SPEED LIMITS

MAXIMUM FLAP EXTENDED SPEED-Vfe
FLAPS 1 -250KIAS
FLAPS 2 -200KIAS
FLAPS FULL- 175KIAS

MAXIMUM LANDING GEAR.
OPERATING/EXTENDED SPEED- Vle/Vlo-210KIAS

MAXIMUM TURBULENT AIR PENETRATION SPEED-225KIAS/MACH.73

MAXIMUM SPEED BRAKE EXTENSION SPEED-NO LIMIT

Question 21

SPEED LIMITS

MINIMUM SPEED BRAKE EXTENDED SPEED (10 PANELS).
(EXCEPT AS REQUIRED BY AFM PROCEDURE)_____

MINIMUM SINGKE ENGINE ENROUTE CLIMB SPEED-Vfto_____

MAXIMUM TIRE GROUND SPEED_____

MINIMUM SPEED FOR SUSTAINED FLIGHT IN ICING CONDITIONS
(EXCEPT TAKEOFF,APPROACH AND LANDING)_____

Answer 21

SPEED LIMITS

MINIMUM SPEED BRAKE EXTENDED SPEED (10 PANELS).
(EXCEPT AS REQUIRED BY AFM PROCEDURE)-Vref +15 KIAS

MINIMUM SINGKE ENGINE ENROUTE CLIMB SPEED-Vfto- 180KIAS

MAXIMUM TIRE GROUND SPEED-182KIAS

MINIMUM SPEED FOR SUSTAINED FLIGHT IN ICING CONDITIONS
(EXCEPT TAKEOFF,APPROACH AND LANDING)-180KIAS

Question 22

MINIMUM CREW
MINIMUM FLIGHT CREW FOR ALL OPERATIONS_____

                                    OPERATIONS AUTHORIZED:
THIS AIRPLANE IS APPROVED FOR DAY AND NIGHT\_\_\_,AND\_\_\_OPERATIONS, AND FLIGHT INTO KNOWN ICING CONDITIONS.

THIS AIRPLANE IS___CERTIFIED FOR DITCHING UNDER 14 CFR PART 25.801

THIS AIRPLANE IS___FOR AOVER WATER OPERATIONS WITH APPLICABLE EQUIPMENT SPECIFIED IN THE APPROPRIATE OPERATING RULES.

Answer 22

MINIMUM CREW
MINIMUM FLIGHT CREW FOR ALL OPERATIONS- 1 PILOT, 1 CO-PILOT

                                    OPERATIONS AUTHORIZED:
THIS AIRPLANE IS APPROVED FOR DAY AND NIGHT-VFR AND-IFR OPERATIONS, AND FLIGHT INTO KNOWN ICING CONDITIONS.

THIS AIRPLANE IS-NOT CERTIFIED FOR DITCHING UNDER 14 CFR PART 25.801

THIS AIRPLANE IS-ELIGIBLE FOR AOVER WATER OPERATIONS WITH APPLICABLE EQUIPMENT SPECIFIED IN THE APPROPRIATE OPERATING RULES.

Question 23

LOAD FACTOR

MAXIMUM LANDING SINK RATE\_\_\_\_\_

MANEUVER LIMITS

AEROBATIC MANEUVERS,INCLUDING SPINS ARE____

INTENTIONAL STALLS ARE PROHIBITED ABOVE_____, INTENTION FULL STALLS ARE LIMITED TO IDLE THRUST ONLY.

Answer 23

LOAD FACTOR

MAXIMUM LANDING SINK RATE-600 FEET PER MINUTE

MANEUVER LIMITS

AEROBATIC MANEUVERS,INCLUDING SPINS ARE-PROHIBITED

INTENTIONAL STALLS ARE PROHIBITED ABOVE-FL180, INTENTION FULL STALLS ARE LIMITED TO IDLE THRUST ONLY.

Question 24

MAXIMUM ALLOWABLE FLIGHT TIME TO A SUITABLE AIRPORT

FLIGHT MUST REMAIN WITHIN_____MINUTES OF A SUITABLE AIRPORT FOR LANDING. THIS LIMITATION IS DUE TO:

1. STANDBY FLIGHT INSTRUMENTS BACK-UP BATTERY ENDURANCE TIME.
2. BAGGAGE/CARGO COMPARTMENT FIRE PROTECTION.

Answer 24

MAXIMUM ALLOWABLE FLIGHT TIME TO A SUITABLE AIRPORT

FLIGHT MUST REMAIN WITHIN-180 MINUTES OF A SUITABLE AIRPORT FOR LANDING. THIS LIMITATION IS DUE TO:

1. STANDBY FLIGHT INSTRUMENTS BACK-UP BATTERY ENDURANCE TIME.
2. BAGGAGE/CARGO COMPARTMENT FIRE PROTECTION.

Question 25

ELECTRICAL POWER SYSTEMS THE BATTERY TEMPERATURE SYSTEM MUST BE OPERATIONAL. A. THE MINIMUM BATTERY TEMPERATURE FOR APU START IS_____ B. THE MINIMUM BATTERY TEMPERATURE FOR THE ENGINE START IS_____

Answer 25

ELECTRICAL POWER SYSTEMS THE BATTERY TEMPERATURE SYSTEM MUST BE OPERATIONAL. A. THE MINIMUM BATTERY TEMPERATURE FOR APU START IS -20*C B. THE MINIMUM BATTERY TEMPERATURE FOR THE ENGINE START IS-10*C

Question 26

ELECTRICAL POWER SYSTEMS FOR GENERATOR COOLING DURING GROUND OPERATION, THE ENGINE ,UST BE OPERATED AT IDLE (SMALL THRUST INCREASES FOR TAXI ARE ACCEPTABLE) WITH THE GENERATOR LOAD LESS THAN_____AMPS FOR 4 MINUTES PRIOR TO RNGINE SHUTDOWN. OTHERWISE, A______MINUTE COOLING PERIOD AFTER ENGINE SHUTDOWN IS REQUIRED PRIOR TO ATTEMPTING A RESTART. TRU MUST BE USED ONLY IN ACCORDANCE WITH AN APPLICABLE AFM PROCEDURE. MAXIMUM CURRENT LIMIT FOR EACH TRU IS_____AMPS.

Answer 26

ELECTRICAL POWER SYSTEMS FOR GENERATOR COOLING DURING GROUND OPERATION, THE ENGINE ,UST BE OPERATED AT IDLE (SMALL THRUST INCREASES FOR TAXI ARE ACCEPTABLE) WITH THE GENERATOR LOAD LESS THAN_75AMPS FOR 4 MINUTES PRIOR TO RNGINE SHUTDOWN. OTHERWISE, A-35 MINUTE COOLING PERIOD AFTER ENGINE SHUTDOWN IS REQUIRED PRIOR TO ATTEMPTING A RESTART. TRU MUST BE USED ONLY IN ACCORDANCE WITH AN APPLICABLE AFM PROCEDURE. MAXIMUM CURRENT LIMIT FOR EACH TRU IS-100AMPS.

Question 27

ELECTRICAL POWER SYSTEMS GENERATOR LIMITS STATUS. ENGINE LIMIT. APU LIMIT GROUND. ______AMPS. ______AMPS AIR. ______AMPS. ______AMPS BELOW FL350. ______AMPS. ______AMPS

Answer 27

ELECTRICAL POWER SYSTEMS GENERATOR LIMITS STATUS. ENGINE LIMIT. APU LIMIT GROUND. - 300AMPS. -275AMPS AIR. - 300AMPS. -275AMPS BELOW FL350. -275AMPS. NOT APPLICABLE

Question 28

AUXILIARY POWER UNIT (APU) THE MAXIMUM ALTITUDE FOR APU START IS_____ THE MAXIMUM AIRSPEED FOR APU STARTS IS____KIAS THE MAXIMUM OPERATING ALTITUDE FOR THE APU IS_____ _____APU START ATTEMPT IS PERMITTED AFTER A DUAL GENERATOR FAILURE FOLLOWING SHUTDOWN FOR ANY REASON AN APU RESTART MUST NOT BE ATTEMPTED UNTIL_____SECONDS AFTER THE RPM INDICATOR READS_____% APPLYING DE-ICE/ANTI-ICE FLUID OF ANY TYPE IS_____WHEN THE APU IS OPERATING.

Answer 28

AUXILIARY POWER UNIT (APU) THE MAXIMUM ALTITUDE FOR APU START IS-FL200 THE MAXIMUM AIRSPEED FOR APU STARTS IS-305 KIAS THE MAXIMUM OPERATING ALTITUDE FOR THE APU IS-FL300 -1 APU START ATTEMPT IS PERMITTED AFTER A DUAL GENERATOR FAILURE FOLLOWING SHUTDOWN FOR ANY REASON AN APU RESTART MUST NOT BE ATTEMPTED UNTIL-30 SECONDS AFTER THE RPM INDICATOR READS-0% APPLYING DE-ICE/ANTI-ICE FLUID OF ANY TYPE IS-PROHIBITED WHEN THE APU IS OPERATING.

Question 29

AUXILIARY POWER UNIT (APU) UNATTENDED OPERATION OF THE APU IS_____ OPERATING THE COCKPIT AND CABIN TEMPERATURE CONTROLS IN MANUAL IS PROHIBITED WHILE MAX COOL AND BLEED AIR. ARE SELECTED_____. A_____SECOND WAITING PERIOD IS REQUIRED AFTER SELECTING MAX COOL TO OFF BEFORE OPERATING COCKPIT AND CABIN TEMPERATURE CONTROLS IN MANUAL. THE APU COMPARTMENT MUST BE_____FOLLOWING AUTOMATIC SHUTDOWN OF THE APU.

Answer 29

AUXILIARY POWER UNIT (APU) UNATTENDED OPERATION OF THE APU IS-PROHIBITED OPERATING THE COCKPIT AND CABIN TEMPERATURE CONTROLS IN MANUAL IS PROHIBITED WHILE MAX COOL AND BLEED AIR. ARE SELECTED-ON A-30 SECOND WAITING PERIOD IS REQUIRED AFTER SELECTING MAX COOL TO OFF BEFORE OPERATING COCKPIT AND CABIN TEMPERATURE CONTROLS IN MANUAL. THE APU COMPARTMENT MUST BE-INSPECTED FOLLOWING AUTOMATIC SHUTDOWN OF THE APU.

Question 30

FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) | EXCEEDING THE TIME INTERVAL (125 HOURS) FOR A WHITE ENGINE DISPATCH LIM L AND OR R CAS MESSAGE IS____

Answer 30

FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) | EXCEEDING THE TIME INTERVAL (125 HOURS) FOR A WHITE ENGINE DISPATCH LIM L AND OR R CAS MESSAGE IS-PROHIBITIED

Question 31

HYDRAULIC POWER SYSTEM THE USE OF THE AUXILIARY HYDRAULIC PUMP IN FLIGHT IS_____. THE AUXILIARY HYDRAULIC PUMP, WHEN USED ON THE GROUND IN ACCORDANCE WITH THE PROCEDURES IN SECTION III, IS LIMITED TO A TOTAL OF_____MINUTES OF OPERATION(EITHER CONTINUOUS, OR IN SUCCESSIVE EVENTS OF SHORTER DURATION),AND MUST BE FOLLOWED BY A_____MINUTE REST PERIOD PRIOR TO FURTHER OPERATION.

Answer 31

HYDRAULIC POWER SYSTEM THE USE OF THE AUXILIARY HYDRAULIC PUMP IN FLIGHT IS-PROHIBITED THE AUXILIARY HYDRAULIC PUMP, WHEN USED ON THE GROUND IN ACCORDANCE WITH THE PROCEDURES IN SECTION III, IS LIMITED TO A TOTAL OF-2 MINUTES OF OPERATION(EITHER CONTINUOUS, OR IN SUCCESSIVE EVENTS OF SHORTER DURATION),AND MUST BE FOLLOWED BY A-15 MINUTE REST PERIOD PRIOR TO FURTHER OPERATION.

Question 32

ICE AND RAIN PROTECTION IN ICING CONDITIONS, THE AIRPLANE MUST BE OPERATED, AND IT’S ICE PROTECTION SYSTEMS_____BE USED,AS DESCRIBED IN SECTION III, NORMAL PROCEDURES, ANTI-ICE SYSTEMS. SPECIFIC OPERATIONAL SPEEDS AND PERFORMANCE INFORMATION MUST BE USED WHERE ESTABLISHED FOR SUCH CONDITIONS. EXCEPT FOR THE GROUND PREFLIGHT CHECK,MAXIMUM SAT FOR OPERATION OF BLEED AIR ANTI-ICE WITH THE THROTTLES ABOVE IDLE IS_____*C

Answer 32

ICE AND RAIN PROTECTION IN ICING CONDITIONS, THE AIRPLANE MUST BE OPERATED, AND IT’S ICE PROTECTION SYSTEMS-MUST BE USED,AS DESCRIBED IN SECTION III, NORMAL PROCEDURES, ANTI-ICE SYSTEMS. SPECIFIC OPERATIONAL SPEEDS AND PERFORMANCE INFORMATION MUST BE USED WHERE ESTABLISHED FOR SUCH CONDITIONS. EXCEPT FOR THE GROUND PREFLIGHT CHECK,MAXIMUM SAT FOR OPERATION OF BLEED AIR ANTI-ICE WITH THE THROTTLES ABOVE IDLE IS +20*C.

Question 33

ICE AND RAIN PROTECTION THE ENGINE/STAB ANTI-ICE BUTTONS MUCT BE SELECTED ON BETWEEN THE TEMPERATURE OF_____*C TO _____*C WHEN IN VISIBLE MOISTURE EXCEPT DURING DEICING/ANTI-ICING PROCEDURES AS SPECIFIED IN SECTION VII, ADVISORY INFORMATION,USE_____FOR GROUND OPERATIONS_____FOR IN FLIGHT. THE WING ANTI-ICE BUTTONS MUST BE SELECTED ON BETWEEN_____*C AND _____*C WHEN IN VISIBLE MOISTURE. THE WING ANTI-ICE BUTTONS MUST BE SELECTED_____FOR OPERATIONS ABOVE FL410. LIMIT THE GROUND OPERATION OF THE PITIT-STATIC HEAT TO______MINUTES TO PRECLUDE DAMAGE TO THE PITOT TUBES AND ANGLE-OF-ATTACK VANES. ANTI-ICE SYSTEMS MUST NOT BE USED TO DE-ICE SURFACES PRIOR TO______.

Answer 33

ICE AND RAIN PROTECTION THE ENGINE/STAB ANTI-ICE BUTTONS MUCT BE SELECTED ON BETWEEN THE TEMPERATURE OF - +10*C TO- -35*C WHEN IN VISIBLE MOISTURE EXCEPT DURING DEICING/ANTI-ICING PROCEDURES AS SPECIFIED IN SECTION VII, ADVISORY INFORMATION,USE-SAT FOR GROUND OPERATIONS-RAT FOR IN FLIGHT. THE WING ANTI-ICE BUTTONS MUST BE SELECTED ON BETWEEN -+5*C AND -35*C WHEN IN VISIBLE MOISTURE. THE WING ANTI-ICE BUTTONS MUST BE SELECTED -OFF FOR OPERATIONS ABOVE FL410. LIMIT THE GROUND OPERATION OF THE PITIT-STATIC HEAT TO-2 MINUTES TO PRECLUDE DAMAGE TO THE PITOT TUBES AND ANGLE-OF-ATTACK VANES. ANTI-ICE SYSTEMS MUST NOT BE USED TO DE-ICE SURFACES PRIOR TO-TAKEOFF.

Question 34

BOUNDARY LAYER ENERGIZERS ALL BOUNDARY LAYER ENERGIZERS (_____PER WING) AND STALL STRIPS (_____PER WING) MUST BE PRESENT FOR TAKEOFF. CABIN PRESSURE LIMITS PRESSURE DIFFERENTIAL DIGITAL DISPLAY GREEN RANGE______

Answer 34

BOUNDARY LAYER ENERGIZERS ALL BOUNDARY LAYER ENERGIZERS (-7 PER WING) AND STALL STRIPS (-2 PER WING) MUST BE PRESENT FOR TAKEOFF. CABIN PRESSURE LIMITS PRESSURE DIFFERENTIAL DIGITAL DISPLAY GREEN RANGE-0.0 TO 10.2 PSID

Question 35

PASSENGER COMPARTMENT FOR TAXI,TAKEOFF AND LANDING, THE FOLLOWING ITEMS MUST BE CONFIGURED ACCORDINGLY: THE LAVATORY DIVIDER DOOR LATCHED_____,CABIN DOOR CURTAIN____,SEAT BACKS FULLY_____,HEADRESTS_____,SEAT CONTROLS_____,SEAT TRACKED AWAY FROM THE TABLE AND THEN_____.AND PASSENGER SEAT BELTS AND SHOULDER HARNESSES (IF EQUIPPED) FASTENED. MAXIMUM SEATING THE MAXIMUM NUMBER OF SEATS APPROVED FOR THE AIRPLANE IS_____INCLUDING CREW SEATS.

Answer 35

PASSENGER COMPARTMENT FOR TAXI,TAKEOFF AND LANDING, THE FOLLOWING ITEMS MUST BE CONFIGURED ACCORDINGLY: THE LAVATORY DIVIDER DOOR LATCHED-OPEN, CABIN DOOR CURTAIN-STOWED, SEAT BACKS FULLY- UPRIGHT, HEADRESTS-EXTENDED, SEAT CONTROLS-INBOARD, SEAT TRACKED AWAY FROM THE TABLE AND THEN-OUTBOARD, AND PASSENGER SEAT BELTS AND SHOULDER HARNESSES (IF EQUIPPED) FASTENED. MAXIMUM SEATING THE MAXIMUM NUMBER OF SEATS APPROVED FOR THE AIRPLANE IS-11 INCLUDING CREW SEATS.

Question 36

BAGGAGE COMPARTMENT THE TAILCONE BAGGAGE COMPARTMENT SMOKE DETECTION AND FIRE EXTINGUISHING SYSTEMS MUST BE_____ IF BAGGAGE IS CARRIED IN THE COMPARTMENT. THE MAXIMUM TOTAL WEIGHT IN THE TAILCONE BAGGAGE COMPARTMENT IS_____POUNDS. TOTAL WEIGHT INCLUDES BAGGAGE IN THE FORWARD AND AFT COMPARTMENTS PLUS ANY ON THE COAT ROD. THE MAXIMUM FLOOR LOADING DISTRIBUTION IS_____POUNDS PER SQUARE FOOT.

Answer 36

BAGGAGE COMPARTMENT THE TAILCONE BAGGAGE COMPARTMENT SMOKE DETECTION AND FIRE EXTINGUISHING SYSTEMS MUST BE-OPERATIONAL IF BAGGAGE IS CARRIED IN THE COMPARTMENT. THE MAXIMUM TOTAL WEIGHT IN THE TAILCONE BAGGAGE COMPARTMENT IS-1000 POUNDS. TOTAL WEIGHT INCLUDES BAGGAGE IN THE FORWARD AND AFT COMPARTMENTS PLUS ANY ON THE COAT ROD. THE MAXIMUM FLOOR LOADING DISTRIBUTION IS-150 POUNDS PER SQUARE FOOT.

Question 37

SUPPLEMENTAL OXYGEN SYSTEM CREW OXYGEN MASKS ARE NOT APPROVED FOR SUSTAINED OPERATION AT A CABIN ALTITUDE GREATER THAN_____FEET. PASSENGER OXYGEN MASKS ARE NOT APPROVED FOR SUSTAINED OPERATION AT A CABIN ALTITUDE GREATER THAN_____FEET. THE PRESSURE-DEMAND CREW OXYGEN MAST MUST BE PROPERLY STOWED IN THEIR CONTAINERS TO QUALIFY AS A______MASK. FOR AIRPLANES EQUIPPED WITH THE EROS MLD20-505 OXYGEN MASKS,CREW MEMBERS____FAMILIARIZE THEMSELVES WITH PROPER USE OF THE SMOKE GOGGLE CLIP ON PROCEDURE.

Answer 37

SUPPLEMENTAL OXYGEN SYSTEM CREW OXYGEN MASKS ARE NOT APPROVED FOR SUSTAINED OPERATION AT A CABIN ALTITUDE GREATER THAN-40,000 FEET. PASSENGER OXYGEN MASKS ARE NOT APPROVED FOR SUSTAINED OPERATION AT A CABIN ALTITUDE GREATER THAN-25,000 FEET. THE PRESSURE-DEMAND CREW OXYGEN MAST MUST BE PROPERLY STOWED IN THEIR CONTAINERS TO QUALIFY AS A-QUICK-DONNING MASK. FOR AIRPLANES EQUIPPED WITH THE EROS MLD20-505 OXYGEN MASKS,CREW MEMBERS-MUST FAMILIARIZE THEMSELVES WITH PROPER USE OF THE SMOKE GOGGLE CLIP ON PROCEDURE.

Question 38

THRUST REVERSERS A SATISFACTORY PREFLIGHT CHECK OF THE THRUST REVERSERS MUST BE ACCOMPLISHED IN ACCORDANCE WITH SECTION III, NORMAL PROCEDURES ON THE_____OF THE DAY AND ON______THAT IS PREDICATED ON THE USE OF THRUST REVERSERS FOR PERFORMANCE OR THE FIRST FLIGHT AFTER_____ACTION HAS BEEN PERFORMED ON THE AIRPLANE. REVERSE THRUST MUST BE DECREASED TO THE IDLE POSITION______KIAS ON LANDING ROLL.

Answer 38

THRUST REVERSERS A SATISFACTORY PREFLIGHT CHECK OF THE THRUST REVERSERS MUST BE ACCOMPLISHED IN ACCORDANCE WITH SECTION III, NORMAL PROCEDURES ON THE-FIRST FLIGHT OF THE DAY AND ON-ANY FLIGHT THAT IS PREDICATED ON THE USE OF THRUST REVERSERS FOR PERFORMANCE OR THE FIRST FLIGHT AFTER-ANY MAINTENANCE ACTION HAS BEEN PERFORMED ON THE AIRPLANE. REVERSE THRUST MUST BE DECREASED TO THE IDLE POSITION-65 KIAS ON LANDING ROLL.

Question 39

THRUST REVERSERS DEPLOYMENT OF THE THRUST REVERSERS FOR MORE THAN_____SECONDS WITH THE APU OPERATING IS PROHIBITED. STATIC GROUND OPERATION OF THE ENGINES IS LIMITED TO_____ IF THE THRUST REVERSERS ARE DEPLOYED. THE USE OF THRUST REVERSERS IS_____DURING TOUCH AND GO LANDINGS. THE USE OF THRUST REVERSERS TO BACK THE AIRPLANE IS_____.

Answer 39

THRUST REVERSERS DEPLOYMENT OF THE THRUST REVERSERS FOR MORE THAN-30 SECONDS WITH THE APU OPERATING IS PROHIBITED. STATIC GROUND OPERATION OF THE ENGINES IS LIMITED TO-IDLE IF THE THRUST REVERSERS ARE DEPLOYED. THE USE OF THRUST REVERSERS IS-PROHIBITED DURING TOUCH AND GO LANDINGS. THE USE OF THRUST REVERSERS TO BACK THE AIRPLANE IS-PROHIBITED.

Question 40

ANGLE-OF-ATTACK AND STICK SHAKER SYSTEM THE ANGLE-OF-ATTACK SYSTEM CAN BE USED AS A REFERENCE FOR APPROACH SPEED (Vref) AT ALL AIRPLANE WEIGHTS,CG LOCATIONS AND FLAP POSITIONS. Vref IS INDICATED BY APPROXIMATELY_____ON THE AOA GAUGE AND BY THE_____ON THE PILOTS AND CO-PILOTS AIRSPEED INDICATORS. STANDBY FLIGHT DISPLAY THE STANDBY FLIGHT DISPLAY (INCLUDING PRE-FLIGHT TEST, ATTITUDE,HEADING,ALTITUDE AND AIRSPEED) MUST BE_____PRIOR TO TAKEOFF.

Answer 40

ANGLE-OF-ATTACK AND STICK SHAKER SYSTEM THE ANGLE-OF-ATTACK SYSTEM CAN BE USED AS A REFERENCE FOR APPROACH SPEED (Vref) AT ALL AIRPLANE WEIGHTS,CG LOCATIONS AND FLAP POSITIONS. Vref IS INDICATED BY APPROXIMATELY-.6 ON THE AOA GAUGE AND BY THE-GREEN CIRCLE ON THE PILOTS AND CO-PILOTS AIRSPEED INDICATORS. STANDBY FLIGHT DISPLAY THE STANDBY FLIGHT DISPLAY (INCLUDING PRE-FLIGHT TEST, ATTITUDE,HEADING,ALTITUDE AND AIRSPEED) MUST BE-FUNCTIONING PRIOR TO TAKEOFF.

Question 41

GARMIN G5000 AVIONICS SYSTEM SOFTWARE-GENERAL TAKEOFF WITH A DISPLAY UNIT IN REVERSIONARY MODE IS_____. TAXIING THE AIRPLANE IS_____UNTIL AHRS ALIGNMENT IS COMPLETE. ATTITUDE PITCH LIMIT INDICATOR (PLI) MUST_____BE USED AS A SOLE MEANS OF STALL AVOIDANCE. CATEGORY II ILS APPROACHES ARE______AUTHORIZED.

Answer 41

GARMIN G5000 AVIONICS SYSTEM SOFTWARE-GENERAL TAKEOFF WITH A DISPLAY UNIT IN REVERSIONARY MODE IS-PROHIBITED. TAXIING THE AIRPLANE IS-PROHIBITED UNTIL AHRS ALIGNMENT IS COMPLETE. ATTITUDE PITCH LIMIT INDICATOR (PLI) MUST-NOT BE USED AS A SOLE MEANS OF STALL AVOIDANCE. CATEGORY II ILS APPROACHES ARE-NOT AUTHORIZED.

Question 42

GARMIN G5000 AVIONICS SYSTEM SOFTWARE-GENERAL FOR CONTINUOUS GROUND OPERATION WITH ELECTRICAL POWER ON WHEN AMBIENT TEMPERATURES ARE AT OR ABOVE_____*C, CONDITIONED AIR MUST BE SUPPLIED TO THE CABIN WITH APU OR ENGINE BLEED AIR AND THE CABIN DOOR MUST BE KEPT CLOSED EXCEPT FOR PASSENGER BOARDING.

Answer 42

GARMIN G5000 AVIONICS SYSTEM SOFTWARE-GENERAL FOR CONTINUOUS GROUND OPERATION WITH ELECTRICAL POWER ON WHEN AMBIENT TEMPERATURES ARE AT OR ABOVE-ISA+26*C, CONDITIONED AIR MUST BE SUPPLIED TO THE CABIN WITH APU OR ENGINE BLEED AIR AND THE CABIN DOOR MUST BE KEPT CLOSED EXCEPT FOR PASSENGER BOARDING.

Question 43

GARMIN G5000 AVIONICS SOFTWARE-GENERAL AFTER MAKING A MODIFICATION TO THE FLIGHT PLAN, WAYPOINTS OR VNAV CONSTRAINTS, THE FLIGHT PLAN MUST BE REVIEWED TO VERIFY ALL_____AND_____ ARE CORRECT. BOTH PILOT MUST BE USING_____WHEN THE OVERHEAD COCKPIT SPEAKER IS DESELECTED. USE OF THR SET DEFAULT PROFILE BUTTON ON THE SYSTEM MAINTENANCE PAGE IS_____.

Answer 43

GARMIN G5000 AVIONICS SOFTWARE-GENERAL AFTER MAKING A MODIFICATION TO THE FLIGHT PLAN, WAYPOINTS OR VNAV CONSTRAINTS, THE FLIGHT PLAN MUST BE REVIEWED TO VERIFY ALL-WAYPOINTS AND-CONSTRAINTS ARE CORRECT. BOTH PILOT MUST BE USING-HEADSETS WHEN THE OVERHEAD COCKPIT SPEAKER IS DESELECTED. USE OF THR SET DEFAULT PROFILE BUTTON ON THE SYSTEM MAINTENANCE PAGE IS-PROHIBITED.

Question 44

GARMIN G5000 AVIONICS SYSTEM SOFTWARE-GENERAL (SOFTWARE 2009.22,CONFIG AI OR SOFTWARE 2009.24 CONFIG AH) PRIOR TO THE FAF, MAKE SURE THAT THR_____OR_____AUTO-SELECTED COURSE (AS APPROPRIATE) MATCHES THE FINAL APPROACH COURSE ON THE PUBLISHED APPROACH. USE OF AUTOPILOT OR FLIGHT DIRECTOR COUPLED LDA APPROACHES WITH A GS IS_____.

Answer 44

GARMIN G5000 AVIONICS SYSTEM SOFTWARE-GENERAL (SOFTWARE 2009.22,CONFIG AI OR SOFTWARE 2009.24 CONFIG AH) PRIOR TO THE FAF, MAKE SURE THAT THE-ILS OR-VOR AUTO-SELECTED COURSE (AS APPROPRIATE) MATCHES THE FINAL APPROACH COURSE ON THE PUBLISHED APPROACH. USE OF AUTOPILOT OR FLIGHT DIRECTOR COUPLED LDA APPROACHES WITH A GS IS-PROHIBITED.

Question 45

SYNTHETIC VISION TECHNOLOGY (SVT) SVT IS PROVIDED AS A SITUATIONAL AWARENESS TOOL AND MUST NOT BE USED FOR TACTICAL NAVIGATION AROUND TERRAIN, OBSTACLES OR _____. AIRPLANE NAVIGATION MUST_____BE PREDICTED SOLEY ON SVT RUNWAY PRESENTATION GRAPHICS. APPROACH PATH ANGLE AND DISTANCE MUST BE CONFIRMED BY OTHER SOURCES.

Answer 45

SYNTHETIC VISION TECHNOLOGY (SVT) SVT IS PROVIDED AS A SITUATIONAL AWARENESS TOOL AND MUST NOT BE USED FOR TACTICAL NAVIGATION AROUND TERRAIN, OBSTACLES OR-TRAFFIC. AIRPLANE NAVIGATION MUST-NOT BE PREDICTED SOLEY ON SVT RUNWAY PRESENTATION GRAPHICS. APPROACH PATH ANGLE AND DISTANCE MUST BE CONFIRMED BY OTHER SOURCES.

Question 46

SYNTHETIC VISION TECHNOLOGY SVT AIRPORT SURFACE MARKING AND FEATURES_____AGREE WITH THE ACTUAL SURFACE MARKING AND PREVAILING NOTAMS IN EFFECT FOR THE PARTICULAR AIRPORT. SVT MUST NOT BE USED AS THE SOLE MEANS OF NAVIGATION ON THE AIRPORT SURFACE. TCAS INTRUDER TRAFFIC THAT IS BELOW____FEET AGL MAY NOT APPEAR ON SVT OR MAY ONLY PARTIALLY APPEAR.

Answer 46

SYNTHETIC VISION TECHNOLOGY SVT AIRPORT SURFACE MARKING AND FEATURES-MAY NOT ALWAYS AGREE WITH THE ACTUAL SURFACE MARKING AND PREVAILING NOTAMS IN EFFECT FOR THE PARTICULAR AIRPORT. SVT MUST NOT BE USED AS THE SOLE MEANS OF NAVIGATION ON THE AIRPORT SURFACE. TCAS INTRUDER TRAFFIC THAT IS BELOW-500 FEET AGL MAY NOT APPEAR ON SVT OR MAY ONLY PARTIALLY APPEAR.

Question 47

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) AUTOPILOT: A._____PILOT MUST REMAIN SEATED, WITH THE SEATBELT FASTENED, DURING ALL AUTOPILOT OPERATIONS. B. AUTOPILOT OPERATION IS_____WHEN ANY COMPARISON MONITOR MESSAGE IS DISPLAYED AND APPROPRIATE SENSOR REVERSION HAS NOT BEEN SELECTED.

Answer 47

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) AUTOPILOT: A-ONE PILOT MUST REMAIN SEATED, WITH THE SEATBELT FASTENED, DURING ALL AUTOPILOT OPERATIONS. B. AUTOPILOT OPERATION IS-PROHIBITED WHEN ANY COMPARISON MONITOR MESSAGE IS DISPLAYED AND APPROPRIATE SENSOR REVERSION HAS NOT BEEN SELECTED.

Question 48

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) ``` AUTOPILOT MINIMUM USE HEIGHT: 1 ENROUTE AND DESCENT_____ 2 PRECISION APPROACH (ILS/LPV)_____ 3 NON-PRECISION APPROACH_____ 4 TAKEOFF,CLIMB AND MISSED APPROACH_____ ```

Answer 48

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) AUTOPILOT MINIMUM USE HEIGHT: 1 ENROUTE AND DESCENT-1000 FEET AGL 2 PRECISION APPROACH (ILS/LPV)-160 FEET AGL 3 NON-PRECISION APPROACH-200 FEET AGL 4 TAKEOFF,CLIMB AND MISSED APPROACH-400 FEET AGL

Question 49

AUTOMATIC FLIGHT CONTROL SYSTEM (ACFS) AUTO-THROTTLE MUST NOT BE ARMED OR USED DURING_____; ARM ONLY WHEN CLEARED FOR TAKEOFF AUTO-THROTTLE OPERATION IS_____WHEN ANY COMPARISON MONIOTR MESSAGE IS DISPLAYED AND APPROPRIATE SENSOR REVERSION HAS NOT BEEN SELECTED. AUTO-THROTTLE HOLD MODE MUST BE DISPLAYED PRIOR TO_____KIAS DURING TAKEOFF.

Answer 49

AUTOMATIC FLIGHT CONTROL SYSTEM (ACFS) AUTO-THROTTLE MUST NOT BE ARMED OR USED DURING- TAXI OPERATIONS ARM ONLY WHEN CLEARED FOR TAKEOFF AUTO-THROTTLE OPERATION IS-PROHIBITED WHEN ANY COMPARISON MONIOTR MESSAGE IS DISPLAYED AND APPROPRIATE SENSOR REVERSION HAS NOT BEEN SELECTED. AUTO-THROTTLE HOLD MODE MUST BE DISPLAYED PRIOR TO-65KIAS DURING TAKEOFF.

Question 50

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) AUTO-THROTTLE ENGAGEMENT ABOVE_____KIAS ON GROUND OR BELOW_____FEET AGL IS PROHIBITED. AUTO-THROTTLE MUST BE DISENGAGED PRIOR TO_____FEET AGL FOR TOUCH AND GO LANDINGS. AUTO-THROTTLE MUST BE DISENGAGED PRIOR TO LANDING WITH FLAPS NOT IN THE _____ POSITION. WHEN USING AUTO-THROTTLE ON APPROACH THE SELECTED AIRSPEED MUST BE SET TO Vref +_____KNOTS OR GREATER.

Answer 50

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) AUTO-THROTTLE ENGAGEMENT ABOVE-65 KIAS ON GROUND OR BELOW-400 FEET AGL IS PROHIBITED. AUTO-THROTTLE MUST BE DISENGAGED PRIOR TO-50 FEET AGL FOR TOUCH AND GO LANDINGS. AUTO-THROTTLE MUST BE DISENGAGED PRIOR TO LANDING WITH FLAPS NOT IN THE-FULL POSITION. WHEN USING AUTO-THROTTLE ON APPROACH THE SELECTED AIRSPEED MUST BE SET TO Vref +3 KNOTS OR GREATER.

Question 51

G5000 FLIGHT MANAGMENT SYSTEM IFR ENROUTE AND TERMINAL NAVIGATION IS_____UNLESS THE PILOT VERIFIES THE CURRENCY OF THE DATABASE OR VERIFIES EACH SELECTED WAYPOINT FOR ACCURACY BY REFERENCE TO CURRENT DATA. THE USE OF MANUALLY INSERTED RUNWAY COORDINTAES IS LIMITED TO_____OPERATIONS.

Answer 51

G5000 FLIGHT MANAGMENT SYSTEM IFR ENROUTE AND TERMINAL NAVIGATION IS-PROHIBITED UNLESS THE PILOT VERIFIES THE CURRENCY OF THE DATABASE OR VERIFIES EACH SELECTED WAYPOINT FOR ACCURACY BY REFERENCE TO CURRENT DATA. THE USE OF MANUALLY INSERTED RUNWAY COORDINTAES IS LIMITED TO-VFR OPERATIONS.

Question 52

FMS NAVIGATIONAL OPERATIONAL CAPABILITIES (SOFTWARE 2009.22 OR SOFTWARE 2009.24, CONFIG AG) RNP AR PROCEDURES WITH A MISSED APPROACH RNP LESS THAN 1.0, OR PROCEDURES WITH RF LEGS ARE_____AUTHORIZED.

Answer 52

FMS NAVIGATIONAL OPERATIONAL CAPABILITIES (SOFTWARE 2009.22 OR SOFTWARE 2009.24, CONFIG AG) RNP AR PROCEDURES WITH A MISSED APPROACH RNP LESS THAN 1.0, OR PROCEDURES WITH RF LEGS ARE-NOT AUTHORIZED.

Question 53

``` FMS NAVIGATION OPERATIONAL CAPABILITIES VERTICAL NAVIGATION (VNAV) ``` FOR APPROACH PROCEDURES USING BARO VNAV TO DA, THE CURRENT_____FROM THE LANDING AIRPORT IS REQUIRED.

Answer 53

``` FMS NAVIGATION OPERATIONAL CAPABILITIES VERTICAL NAVIGATION (VNAV) ``` FOR APPROACH PROCEDURES USING BARO VNAV TO DA, THE CURRENT-ALTIMETER SETTING FROM THE LANDING AIRPORT IS REQUIRED.

Question 54

FMS NAVIGATIONAL OPERATIONAL CAPABILITIES APPROACH WHEN CONDUCTING FMS BASED APPROACHES,THE APPROPRIATE APPROACH_____MUST BE INDICATED IN MAGENTA ON THE HSI,AND RAIM NOT AVAILABLE FROM FAF TO MAP SYSTEM MESSAGE MUST NOT BE POSTED PRIOR TO CROSSING THE FAF FOR RVAV (GPS), RNAV (GNSS) AND RNAV (RNP)(SOFTWARE 2009.40 ONLY) APPROACH PROCEDURES, THE MAXIMUM PREDICTED RAIM OUTAGE DURATION IS____MINUTES.

Answer 54

FMS NAVIGATIONAL OPERATIONAL CAPABILITIES APPROACH WHEN CONDUCTING FMS BASED APPROACHES,THE APPROPRIATE APPROACH- SERVICE LEVEL MUST BE INDICATED IN MAGENTA ON THE HSI,AND RAIM NOT AVAILABLE FROM FAF TO MAP SYSTEM MESSAGE MUST NOT BE POSTED PRIOR TO CROSSING THE FAF FOR RVAV (GPS), RNAV (GNSS) AND RNAV (RNP)(SOFTWARE 2009.40 ONLY) APPROACH PROCEDURES, THE MAXIMUM PREDICTED RAIM OUTAGE DURATION IS-5 MINUTES.

Question 55

FMS NAVIGATION OPERATIONAL CAPABILITIES APPROACH THE FLIGHT CREW MUST VERIFY THE ACTIVE NAVIGATION SOURCE IS_____OR_____(GREEN NEEDLES) PRIOR TO CROSSING THE FINAL APPROACH FOX FOR ILS,LOC,LOC-BC,LDA, AND SDF APPROACH PROCEDURES.

Answer 55

FMS NAVIGATION OPERATIONAL CAPABILITIES APPROACH THE FLIGHT CREW MUST VERIFY THE ACTIVE NAVIGATION SOURCE IS-LOC OR-BC (GREEN NEEDLES) PRIOR TO CROSSING THE FINAL APPROACH FOX FOR ILS,LOC,LOC-BC,LDA, AND SDF APPROACH PROCEDURES.

Question 56

FMS NAVIGATION OPERATIONAL CAPABILITIES APPROACH WHNE CONDUCTING MISSED APPROACH PROCEDURES,AUTOPILOT COUPLED OPERATION IS_____UNTIL THE FLIGHT CREW HAS ESTABLISHED A RATE OF CLIMB THAT ENSURES ALL ALTITUDE REQUIREMENTS OF THE PROCEDURE WILL BE MET AND AUTOPILOT MINIMUM USE HEIGHT IS REACHED. WHEN FLYING AN FMS APPROACH TO AN MDA, THE ALTITUDE PRESELECTOR MUST BE SET TO THE_____AND A VERTICAL MODE OTHER THAN_____MUST BE USED TO LEVEL AT THE MDA.

Answer 56

FMS NAVIGATION OPERATIONAL CAPABILITIES APPROACH WHNE CONDUCTING MISSED APPROACH PROCEDURES,AUTOPILOT COUPLED OPERATION IS-PROHIBITED UNTIL THE FLIGHT CREW HAS ESTABLISHED A RATE OF CLIMB THAT ENSURES ALL ALTITUDE REQUIREMENTS OF THE PROCEDURE WILL BE MET AND AUTOPILOT MINIMUM USE HEIGHT IS REACHED. WHEN FLYING AN FMS APPROACH TO AN MDA, THE ALTITUDE PRESELECTOR MUST BE SET TO THE-MDA AND A VERTICAL MODE OTHER THAN-GP MUST BE USED TO LEVEL AT THE MDA.

Question 57

FMS NAVIGATION OPERATIONAL CAPABILITIES APPROACH (SOFTWARE 2009.40, CONGIG AF) AUTOPILOT OR FLIGHT DIRECTOR MUST BE USED FOR RNAV (RNP) PROCEDURES WITH _____LEGS. FOR RNAV (RNP) APPROACH PROCEDURES USING BARO VNAV, BOTH ADC’S MUST BE OPERATIONAL ANF THE FLIGHT CREW MUST VERIFY THAT THE PILOT’S AND CO PILOT’S ALTIMETERS ARE SET TO THE CURRENT ALTIMETER SETTING FOR THE LANDING AIRPORT AND AGREE WITHIN_____FEET PRIOR TO FAF BUT NOT EARLIER THAN THE INITIAL APPROACH FIX (IAF)

Answer 57

FMS NAVIGATION OPERATIONAL CAPABILITIES APPROACH (SOFTWARE 2009.40, CONGIG AF) AUTOPILOT OR FLIGHT DIRECTOR MUST BE USED FOR RNAV (RNP) PROCEDURES WITH -RF LEGS. FOR RNAV (RNP) APPROACH PROCEDURES USING BARO VNAV, BOTH ADC’S MUST BE OPERATIONAL ANF THE FLIGHT CREW MUST VERIFY THAT THE PILOT’S AND CO PILOT’S ALTIMETERS ARE SET TO THE CURRENT ALTIMETER SETTING FOR THE LANDING AIRPORT AND AGREE WITHIN +/- 75 FEET PRIOR TO FAF BUT NOT EARLIER THAN THE INITIAL APPROACH FIX (IAF)

Question 58

FMS NAVIGATIONAL OPERATIONAL CAPABILITIES TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS II) EVASIVE MANEUVERS BASED SOLEY ON TCAS TRAFFIC ADVISORIES (TAs) WITHOUT______OF THE INTRUDER AIRPLANE ARE PROHIBITED.

Answer 58

FMS NAVIGATIONAL OPERATIONAL CAPABILITIES TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS II) EVASIVE MANEUVERS BASED SOLEY ON TCAS TRAFFIC ADVISORIES (TAs) WITHOUT-VISUAL ACQUISITION OF THE INTRUDER AIRPLANE ARE PROHIBITED.

Question 59

TERRAIN AWARENESS AND WARNING SYSTEM (TAWS-A) THE USE OF THIS SYSTEM IS LIMITED TO PERFORMING A CAUTION/WARNING FUNCTION ONLY. THE GARMIN TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) IS-NOT INTENDED AS A PRIMARY FLIGHT INSTRUMENT. PILOT ARE-AUTHORIZED TO DEVIATE FROM THEIR CURRENT AIR TRAFFIC CONTROL (ATC) CLEARANCE TO THE EXTENT NECESSARY TO COMPLY WITH A TAWS WARNING. THE TERRAIN DISPLAY IS INTENDED TO SERVE AS A_____TOOL ONLY. THE TERRAIN/OBSTACLE DATABASE DOES NOT INCLUDE 100% OF ALL TERRAIN, NOR UPON USE OF THE TERRAIN DATABASE DISPLAY.

Answer 59

TERRAIN AWARENESS AND WARNING SYSTEM (TAWS-A) THE USE OF THIS SYSTEM IS LIMITED TO PERFORMING A CAUTION/WARNING FUNCTION ONLY. THE GARMIN TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) IS_____INTENDED AS A PRIMARY FLIGHT INSTRUMENT. PILOT ARE_____TO DEVIATE FROM THEIR CURRENT AIR TRAFFIC CONTROL (ATC) CLEARANCE TO THE EXTENT NECESSARY TO COMPLY WITH A TAWS WARNING. THE TERRAIN DISPLAY IS INTENDED TO SERVE AS A-SITUATIONAL AWARENESS TOOL ONLY. THE TERRAIN/OBSTACLE DATABASE DOES NOT INCLUDE 100% OF ALL TERRAIN, NOR UPON USE OF THE TERRAIN DATABASE DISPLAY.

Question 60

SAFE TAXI DEPICTED DATA_____INCLUDE KNOWLEDGE OF CURRENT NOTICE TO AIRMEN (NOTAM) AND THEREFORE FACTORS SUCH AS CLOSURE OF RUNWAYS OR TAXIWAYS MAN NOT BE REFLECTED. CREWS MUST BE COGNIZANT OF PREVAILING NOTAM AND AUTOMATIC TERMINAL INFORMATION SERVICE (ATIS) DATA. SIMILARLY, DATA ON NEWLY CONSTRUCTED OR ALTERED AIRFIELD GEOGRAPHY MAY NOT NECESSARILY BE INCLUDED IN THE DATABASE. PAINTED HOLD LINES MAY NOT AGREE WITH DEPICTED DATA. CREWS MUST REMAIN BEHIND HOLD LINES WHEN REQUIRED AND_____DEPEND ON DEPICTED DATA FOR POSITIONING RELATIVE TO HOLD LINES.

Answer 60

SAFE TAXI DEPICTED DATA-DO NOT INCLUDE KNOWLEDGE OF CURRENT NOTICE TO AIRMEN (NOTAM) AND THEREFORE FACTORS SUCH AS CLOSURE OF RUNWAYS OR TAXIWAYS MAN NOT BE REFLECTED. CREWS MUST BE COGNIZANT OF PREVAILING NOTAM AND AUTOMATIC TERMINAL INFORMATION SERVICE (ATIS) DATA. SIMILARLY, DATA ON NEWLY CONSTRUCTED OR ALTERED AIRFIELD GEOGRAPHY MAY NOT NECESSARILY BE INCLUDED IN THE DATABASE. PAINTED HOLD LINES MAY NOT AGREE WITH DEPICTED DATA. CREWS MUST REMAIN BEHIND HOLD LINES WHEN REQUIRED AND-MUST NOT DEPEND ON DEPICTED DATA FOR POSITIONING RELATIVE TO HOLD LINES.

Question 61

TAKEOFF AND LANDING DATA (TOLD) (SOFTWARE 2009.40, CONFIGURATION AF) THE V SPEEDS, REQUIRED FIELD LENGTH, AND OTHER PERFORMANCE INFORMATION FOR A SPECIFIC OPERATION MUST BE OBTAINED FROM A_____;I.E EITHER THE AFM, CPCalc, OR FMS TAKEOFF AND LANDING PERFORMANCE DATA. IT IS THE RESPONSIBILITY OF THE _____TO VERIFY ALL INPUTS REGARDING AIRPLANE CONFIGURATION, RUNWAY INFORMATION, AND AMBIENT CONDITIONS.

Answer 61

TAKEOFF AND LANDING DATA (TOLD) (SOFTWARE 2009.40, CONFIGURATION AF) THE V SPEEDS, REQUIRED FIELD LENGTH, AND OTHER PERFORMANCE INFORMATION FOR A SPECIFIC OPERATION MUST BE OBTAINED FROM A-SINGLE SOURCE;I.E EITHER THE AFM, CPCalc, OR FMS TAKEOFF AND LANDING PERFORMANCE DATA. IT IS THE RESPONSIBILITY OF THE -CREW TO VERIFY ALL INPUTS REGARDING AIRPLANE CONFIGURATION, RUNWAY INFORMATION, AND AMBIENT CONDITIONS.

Question 62

SURFACEWATCH (SOFTWARE 2009.40, CONFIGURE AF) SURFACE WATCH IS A SITUATIONAL AWARENESS TOOL AND_____BE USED AS A PRIMARY MEANS OF NAVIGATION. CURRENT NOTAM AND ATIS INFORMATION IS NOT INCLUDED IN SURFACE WATCH ALERTS. SURFACE WATCH DOES NOT DEPICT THE ACTUAL LOCATION OF PAINTED HOLD LINES AT AIRPORTS. CREWS MUST REMAIN BEHIND HOLD LINES WHEN REQUIRED AND _____DEPEND ON SURFACEWATCH FOR POSITIONING RELATIVE TO HOLD LINES.

Answer 62

SURFACEWATCH (SOFTWARE 2009.40, CONFIGURE AF) SURFACE WATCH IS A SITUATIONAL AWARENESS TOOL AND-MUST NOT BE USED AS A PRIMARY MEANS OF NAVIGATION. CURRENT NOTAM AND ATIS INFORMATION IS NOT INCLUDED IN SURFACE WATCH ALERTS. SURFACE WATCH DOES NOT DEPICT THE ACTUAL LOCATION OF PAINTED HOLD LINES AT AIRPORTS. CREWS MUST REMAIN BEHIND HOLD LINES WHEN REQUIRED AND-MUST NOT DEPEND ON SURFACEWATCH FOR POSITIONING RELATIVE TO HOLD LINES.

Question 63

HF RADIO HF RADIO TRANSMISSIONS ARE PROHIBITED WHEN NAVIGATION IS PREDICTED ON THE USE OF THE_____ HF RADIO TRANSMISSION DURING REFUELING OPERATION, DURING EXTERIOR PREFLIGHT OR WHEN_____IS PROHIBITED. HF TRANSMITTERS USE A LARGE PORTION OF THE AIRPLANE FOR A GROUND PLANE AND ELECTRICAL SHOCK CAN RESULT FROM TOUCHING THE AIRPLANE EXTERIOR DURING TRANSMISSION.

Answer 63

HF RADIO HF RADIO TRANSMISSIONS ARE PROHIBITED WHEN NAVIGATION IS PREDICTED ON THE USE OF THE-AUTOMATIC DIRECTION FINDER (ADF) HF RADIO TRANSMISSION DURING REFUELING OPERATION, DURING EXTERIOR PREFLIGHT OR WHEN- BOARDING PASSENGERS IS PROHIBITED. HF TRANSMITTERS USE A LARGE PORTION OF THE AIRPLANE FOR A GROUND PLANE AND ELECTRICAL SHOCK CAN RESULT FROM TOUCHING THE AIRPLANE EXTERIOR DURING TRANSMISSION.

Question 64

ELECTRONIC NAVIGATION CHARTS WHEN DISPLAYED, THE GEOGRAPHIC-REFERENCED AIRPLANE SYBOL PN THE OPTIONAL ELECTRONIC CHARTS_____BE USED FOR NAVIGATION. BACK-UP CHARTS_____BE AVAILABLE TO THE FLIGHT CREW ELECTRONIC CHART DATABASE CHART CURRENCY MUST BE VERIFIED_____TO USE.

Answer 64

ELECTRONIC NAVIGATION CHARTS WHEN DISPLAYED, THE GEOGRAPHIC-REFERENCED AIRPLANE SYBOL PN THE OPTIONAL ELECTRONIC CHARTS-MUST NOT BE USED FOR NAVIGATION. BACK-UP CHARTS-MUST BE AVAILABLE TO THE FLIGHT CREW ELECTRONIC CHART DATABASE CHART CURRENCY MUST BE VERIFIED-PRIOR TO USE.

Question 65

RADAR SYSTEM DO NOT OPERAT THE RADAR SYSTEM WITHIN_____FEET OF PERSONNEL OR FLAMMABLE/EXPLOSIVE MATERIAL. DO NOT POSITION THE AIRPLANE FACING BUILDINGS OR LARGE METAL STRUCTURES THAT ARE LIKELY TO REFLECT THE RADAR ENERGY BACK TO THE AIRPLANE. THE AREA WITHIN THE SCAN AAREA (+/-90* OF THE NOSE)AND WITHIN_____FEET OF THE RADAR SYSTEM DURING OPERATION CONSTITUTES A HAZARDOUS AREA.

Answer 65

RADAR SYSTEM DO NOT OPERAT THE RADAR SYSTEM WITHIN-11 FEET OF PERSONNEL OR FLAMMABLE/EXPLOSIVE MATERIAL. DO NOT POSITION THE AIRPLANE FACING BUILDINGS OR LARGE METAL STRUCTURES THAT ARE LIKELY TO REFLECT THE RADAR ENERGY BACK TO THE AIRPLANE. THE AREA WITHIN THE SCAN AAREA (+/-90* OF THE NOSE)AND WITHIN-11 FEET OF THE RADAR SYSTEM DURING OPERATION CONSTITUTES A HAZARDOUS AREA.

Question 66

DATALINK WEATHER OPTIONAL WEATHER SERVICES SUCH AS SIRIUS XM AND GARMIN CONNEXT ARE FOR_____ONLY AND MUST NOT BE USED FOR_____EVALUATION OF DEVELOPING WEATHER. USE OF NEXRAD_____IS PROHIBITED. (SOFTWARE 2009.22, CONFIGURATION CODE AC ONLY).

Answer 66

DATALINK WEATHER OPTIONAL WEATHER SERVICES SUCH AS SIRIUS XM AND GARMIN CONNEXT ARE FOR-SITUATIONAL AWARENESS ONLY AND MUST NOT BE USED FOR-REAL TIME EVALUATION OF DEVELOPING WEATHER. USE OF NEXRAD-ANIMATION IS PROHIBITED. (SOFTWARE 2009.22, CONFIGURATION CODE AC ONLY).

Question 67

CONTROLLER/PILOT DATALINK COMMUNICATION (CPDLC) THE CPDLC INSTALLATION IS LIMITED TO PROVIDING A SUPPLEMENTARY MEANS OF COMMUNICATION._____IS THE PRIMARY MEANS OF ATC COMMUNICATION. CPDLC MUST NOT BE USED FOR_____COMMUNICATION.

Answer 67

CONTROLLER/PILOT DATALINK COMMUNICATION (CPDLC) THE CPDLC INSTALLATION IS LIMITED TO PROVIDING A SUPPLEMENTARY MEANS OF COMMUNICATION.-VOICE IS THE PRIMARY MEANS OF ATC COMMUNICATION. CPDLC MUST NOT BE USED FOR-TIME CRITICAL COMMUNICATION.