Pubs Review 2 Flashcards

1
Q

THE C146 CABIN IS ____ FEET LONG

A

42.5

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2
Q

THE C146 FLOOR WIDTH IS _____ FEET

A

6

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3
Q

THE C146 MAX WIDTH OF THE CABIN IS ____ FEET

A

6.725

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4
Q

THE C146 MAX HEIGHT OF THE CABIN IS ____ FEET

A

6.725

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5
Q

DISTANCE FROM THE NLG TO MLG

A

24’ 4”

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6
Q

DISTANCE FROM NOSE TO APU CONE

A

68’ 7”

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7
Q

DISTANCE FROM NOSE TO TOP OF VERT STAB

A

69’ 10”

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8
Q

DISTANCE FROM GROUND TO TOP OF VERT STAB

A

23’ 9”

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9
Q

REFERENCE DATUM LINE TO NOSE

A

4’ 9.2”

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10
Q

THE TIP OF THE NOSE CONE IS STATION

A

59.06

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11
Q

THE OVERHEAD ESCAPE HATCH IS

A

19 X 20”

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12
Q

THE ANTENNA UNDERNEATH THE SERVICE DOOR IS THE ______.

A

VHF/UHF (LOS) ANTENNA

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13
Q

THE TWO SATCOM ANTENNAS ARE THE ______

A

TWO BATWING ANTENNAS ON TOP OF THE PLANE, FWD & AFT OF THE WING

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14
Q

THERE ARE ____ TCAS ANTENNAS, LOCATED _____.

A

TWO TCAS ANTENNAS, LOCATED ABOVE AND BELOW THE CREW ENTRANCE DOOR

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15
Q

THERE IS ONE VHF ANTENNA ON TOP OF THE PLANE _______

A

AFT OF THE WING AND SAT 1 ANTENNA

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16
Q

THERE IS ONE VHF ANTENNA BELOW THE PLANE ______

A

FWD OF THE LANDING LIGHTS

17
Q

THE ANTENNA ON THE VERT STAB HALF WAY UP IS THE _________

A

VOR/LOC 1, 2

18
Q

THE ANTENNA IMMEDIATELY BEHIND THE NLG IS THE ______

A

ATC 1, 2

19
Q

AT WHAT SPEED IS THE SERVO SPRING TAB DISABLED?

A

160 KIAS

20
Q

THE GUST LOCK SYSTEM PREVENTS INADVERTENT OPERATION OF THE _______

A

POWER LVR’S FWD OF THE FLIGHT IDLE RANGE (MAKING A TAKEOFF WITH LOCKED CONTROL SURFACES IMPOSSIBLE)

21
Q

MAX CAPACITY OF FUEL IN GALLONS

A

1133.6 US GAL

22
Q

TO MAKE A FULL 180 DEGREE TURN YOU NEED ________ FEET, MEASURED FROM THE CENTER OF THE LEFT MLG TO OUTSIDE THE RIGHT WING OR RIGHT MLG TO OUTSIDE OF THE LEFT WING. (THIS ALLOWS THE NLG TO STAY ON THE PAVEMENT AND IS THE MIN RUNWAY WIDTH)

A

47’ 6”

23
Q

TURNING RADII DISTANCE FROM WING TIP TO WEAR IT WILL END UP AFTER A 180 DEGREE TURN

A

97 FEET

24
Q

DO NOT TOW THE AIRCRAFT AT SPEEDS GREATER THAN ________ ON ASPHALT OR CONCRETE SURFACES

A

6 MPH

25
Q

AOH 2.1 PAGE 52 DO NOT MOVE THE AIRCRAFT _________.

A

BY PUSHING ON CONTROL SURFACES OR LANDING GEAR DOORS

26
Q

MAX CABIN ALTITUDE

A

14,500 +/- 500 FT

27
Q

AT 31,000 FT MSL THE CABIN ALTITUDE WILL BE _____

A

8,000 FT MSL

28
Q

AT 25,000 FT MSL THE CABIN ALTITUDE WILL BE _____

A

5,325 FT MSL

29
Q

TO DUMP THERE IS A _______ INSTALLED ON THE FRONT PRESSURE BULKHEAD WHICH EXHAUSTS INTO THE NOSE LANDING GEAR BAY.

A

PNEUMATIC OUTFLOW VALVE

30
Q

THERE IS ALSO A ______ INSTALLED IN THE AFT PRESSURE BULKHEAD AND EXHAUSTS INTO THE TAIL CONE

A

ELECTRO-PNEUMATIC OUTFLOW VALVE

31
Q

YOU WILL RECIEVE AN EXCESSIVE CABIN ALTITUDE WARNING AT ______ CABIN ALTITUDE

A

9500 FT

32
Q

WHEN AIRCRAFT SPEED IS LESS THAN ____ KIAS, THE HEAT EXCHANGERS ARE SUPPLIED WITH COOLING AIR FROM AUTOMATICALLY CONTROLLED COOLING FANS

A

120

33
Q

THE NACA VENT RIGHT BEFORE THE WING IS A ______

A

RAM AIR INTAKE WICH LEADS TO THE DUAL HEAT EXCHANGER

34
Q

THE SCREEN COVERED CIRCULAR HOLE BENEATH THE WING IS AN INTAKE FOR THE _____

A

HEAT EXCHANGER FAN (HX FAN)

35
Q

THE ______ ARE AUTOMATICALLY SWITCHED ON BY AIR DATA COMPUTERS WHEN AIRSPEED IS BELOW ____ KIAS TO SUPPLEMENT THE RAM AIR COOLING FOR THE DUAL HEAT EXCHANGERS

A

HEAT EXCHANGER FAN (HX FAN) & 120

36
Q

THE ______ PACK SUPPLIES ALL THE AIR FOR THE FLIGHT DECK WITH ITS EXCESS FLOW ADDED TO THE AIR FROM THE ____ PACK FOR THE MAIN CABIN COMPARTMENT

A

RIGHT, LEFT

37
Q

THE LOADMASTER CAN OVERRIDE THE TEMPERATURE WITH THE CONTROL KNOB BY THE FA SEAT BY HOW MANY DEGREES?

A

+-/- 9 F OR +/- 5 C

38
Q

THE STATIC DISCHARGERS HELP WITH WHAT?

A

THEY HELP TO REDUCE RADIO FREQUENCY ELECTROMAGNETIC INTERFENCE ASSOCIATED WITH THE DISCHARGE OF AIRCRAFT ELECTROSTATIC CHARGES ACCUMULATED DURING FLIGHT.