RKA Flashcards

1
Q

WHITE CIRCLE AROUND CONTROL SWITCH

A

Equipment operable during dual gen failure

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2
Q

RECOG LIGHTS

A

Wingtips

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3
Q

WING ICE LIGHTS

A

OUTBOARD NACELLE

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4
Q

To turn Threshold lights ON

A

SWITCH - ON

AIRSTAIR DOOR OPEN

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5
Q

GREEN ANNUNCIATOR

A

ADVISORY

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6
Q

AMBER ANNUNCIATOR

A

CAUTION

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7
Q

AUTOIGNITION ARMED

A

ICING, PRECIP,TURBULENCE (TIP)

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8
Q

MIN N1 FOR START

A

12%

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9
Q

PRIMARY ENGINE POWER CONTROLS

A

POWER LEVERS

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10
Q

WHEN ENGINES NOT RUNNING DO NOT MOVE

A

POWER LEVERS TO GROUND FINE OR REVERSE

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11
Q

MIN PROP RPM ON THE GROUND

A

1050

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12
Q

FIRST GATE AFT OF IDLE

A

GROUND FINE

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13
Q

SECOND GATE AFT OF IDLE

A

REVERSE

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14
Q

AUTOFEATHER WILL FX

A

TQ BELOW 10% AND BOTH POWER LEVERS ARE ABOVE THE MICROSWITCH (APPROX 88%N1)

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15
Q

AUTOFEATHER WILL DISARM OPPOSITE ENGINE

A

AT 17% TQ AND BOTH POWER LEVERS ABOVE MICROSWITCH

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16
Q

PROPER OPERATION OF AUTO PROP DEICE

A

OBSERVED ON PROPS AMMETER

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17
Q

PROPER OPERATION OF MAN PROP DEICE

A

RISE IN BOTH DC LOAD METERS

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18
Q

MIN ICE ACCUM SPEED

A

140

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19
Q

ENGINE ANTI-ICE SHALL BE ON

A

+5 C and VISIBLE MOISTURE

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20
Q

LANDING GEAR WARNING

A

POWER LEVERS BELOW 85% N1

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21
Q

RED GEAR HANDLE LIGHTS

A

UNSAFE, IN-TRANSIT, UNLOCKED, HORN ACTIVATED

22
Q

RUDDER BOOST

A

DELTA TQ

MUST B OPERATIONAL PRIOR TO ALL FLIGHTS

23
Q

DUAL AFT BODY STRAKES

A

YAW DAMP MUST B OPERATIVE ABOVE FL190

24
Q

MIN AUTOPILOT HEIGHT ON APPROACH

A

79’ AGL

25
Q

MIN AUTOPILOT HEIGHT AFTER TAKEOFF

A

400’ AGL

26
Q

AIRSPEED TREND

A

EXPECTED IN 10 SECONDS

27
Q

ACTIVE LATERAL AND VERTICAL MODE

A

GREEN

28
Q

ARMED LATERAL AND VERTICAL MODE

A

WHITE

29
Q

the TO waypoint on the LEGS page

A

GREEN

30
Q

MAX ZERO FUEL WEIGHT

A

12,500#

31
Q

RED ANNUNCIATOR

A

WARNING

REQUIRES IMMEDIATE ACTION

32
Q

WARNING or CAUTION

A

WILL EXTINGUISH WHEN FAULT IS NO LONGER SENSED

33
Q

BATT BUS SWITCH IN “NORM”

A

BATTERY POWER TO BATT BUS AND DUAL-FED BUS

34
Q

ENGINE ANTI-ICE SYSTEM

A

ON FOR ALL GROUND OPS (FOD)

35
Q

VACUUM AIR IS FOR

A

SAFETY VALVE AND PRESSURIZATION CONTROLLER OPERATION

36
Q

ENGINE ANTI-ICE

A

OFF WHEN OAT>10C

37
Q

DUMP

A

FROM FL350 TO 13,500 WILL TAKE THE CABIN TO 13,500

38
Q

CABIN DIFF HI

A

DIFF > 6.9PSI

39
Q

RED CABIN ALT HI

A

CABIN PA > 12,500

PAX O2 MASKS WILL AUTO-DEPLOY

40
Q

WHITE CABIN ALTITUDE

A

CABIN PA > 10,000

41
Q

Vyse

A

125

42
Q

MAX ALTITUDE

A

FL350

43
Q

MAX OAT FOR TAKEOFF

A

ISA + 37C/ISA + 98F

44
Q

AUTOFX ARMED

A

TAKEOFF/CLIMB/APPROACH/LANDING

45
Q

LANDING GEAR

A

6 CYCLES/

1 EVERY 5 MIN/15 MIN COOL DOWN

46
Q

RUDDER BOOST

A

OPERATIONAL PRIOR TO ALL FLIGHTS

47
Q

BLEED AIR FAIL

A

PNEU&ENVIR OFF

48
Q

CABIN DIFF HI

A

ENVIR OFF

49
Q

FROM waypoint on LEGS page 1 on CDU

A

CYAN (BLUE)

50
Q

TO waypoint on LEGS page on CDU

A

GREEN

51
Q

EXTERNAL POWER RECEPTACLE

A

R/ WING OUTBOARD OF NACELLE

52
Q

L/R FUEL QTY

A

LESS THAN 30 MINUTES FUEL AT CONTINUOUS PWR