Closed Book

Question 1

PUSHING IN THE FEATHER BUTTON TO THE FEATHER POSITION

Answer 1

ALL OF THE ABOVE

Question 2

DURING A RESTART, THE FEATHER BUTTON LIGHT REMAINS ON FOLLOWING PCO. YOU SHOULD

Answer 2

PULL THE E-HANDLE. IF THE LIGHT GOES OUT, PUSH THE E-HANDLE IN AND CONTINUE THE RESTART PROCEDURE.

Question 3

THE NEGATIVE TORQUE SENSING SYSTEM

Answer 3

LIMITS NEGATIVE TORQUE TO APPROX -150 TO -500 SHP FOR THE OUTBOARD PROPELLERS

Question 4

FAILURE OF AN ENGINE NTS LIGHT TO ILLUMINATE FOLLOWING ENGINE SHUTDOWN FROM LOW RPM WITH THE FUEL AND IGNITION SWITCH REQUIRES MAINTENANCE ACTION.

Answer 4

TRUE

Question 5

DURING AN INFLIGHT RESTART, BLADE/ANGLE ROTATIONIS OBSERVED AFTER PUSHING PCO YOU SHOULD

Answer 5

EXECUTE THE EMERGENCY SHUTDOWN PROCEDURE

Question 6

DURING A LOITER SHUTDOWN, RPM STABILIZES AT 8% AFTER THE E-HANDLE IS PULLED. YOU SHOULD

Answer 6

PERFORM THE PROP FAIL TO FEATHER PROCEDURES

Question 7

UNDER EXTREMELY COLD CONDITIONS YOU MAY OPERATE AN ENGINE WITH OIL TEMPERATURE BETWEEN 50-60 DEGREES C PROVIDED

Answer 7

ALL OIL PX LIMITATIONS ARE MAINTAINED

Question 8

WITH AN ENGINE OIL TEMPERATURE BETWEEN 0 AND 40 DEGREES C, THE MAXIMUM ALLOWABLE SHP IS

Answer 8

1000

Question 9

THE MINIMUM RECOMMENDED AIRSPEED FOR A NORMAL INFLIGHT RESTART IS

Answer 9

170 KIAS

Question 10

PITCHLOCK IS MECHANICALLY CAMMED OUT

Answer 10

BELOW 17 DEGREES BLADE ANGLE AND ABOVE 57 DEGREES BLADE ANGLE

Question 11

IF FORCED TO OPERATE A PITCHLOCKED PROPELLER WITH AN INOPERATIVE ELECTRONIC SYNC SYSTEM, ATTEMPT TO

Answer 11

MAINTAIN RPM IN THE UNDERSPREED RANGE OF 96-98 PERCENT TO REINFORCE PITCHLOCK

Question 12

PITCHLOCK PROVIDES PROTECTIONS AGAINST AN UNCOTROLLABLE OVERSPEED BY PREVENTING AN INCREASE OR DECREASE IN BLADE ANGLE

Answer 12

FALSE

Question 13

PRIOR TO TURNING OFF THE FUEL/IGNITION SWITCH DURING PITCHLOCK PROP PROCEDURES, WHAT CAN BE DONE TO INCREASE SHP

Answer 13

DECREASE TAS

Question 14

AFTER FUEL CHOPPING A PITVHLOCKED PROP, THE INSTRUMENTS INDICATIONS ARE: RPM 35%, SHP -300 TO -400, AND A FLASHING FEATHER VALVE LIGHT. YOU MAY ASSUME YOU HAVE STABILIZED NTS AND THE EMERGENCY SHUT DOWN HANDLE SHOULD BE PULLED

Answer 14

TRUE

Question 15

THE PROPER PROCEDURE FOR HANDLING A PITCHLOCKED PROP WITHOUT OVERSPEED IS TO FUEL CHOPPED THE ENGINE IN THE TERMINAL AREA. WITH STABILIZED NTS, PULL THE EHANDLE.

Answer 15

FALSE

Question 16

TEMPERATURE BELOW 0 DEGREES CELSIUS CAN RESULT IN ERRONEOUS ALTIMETER READINGS. TO ENSURE OBSTACLE CLEARANCE DURING APPROACH PHASE OF FLIGHT WHEN TEMPERATURES ARE BELOW 0, REFER TO FIH SECTION D FOR CORRECTIONS TO_ , _ AND _ IN THE FINAL APPROACH FIX

Answer 16

DECISION HEIGHT, MDA AND STEP DOWN FIXES

Question 17

THE INDICATIONS OF A SPIN ARE

Answer 17

STALLED AOA, PEGGED TURN NEEDLE, AND STABILIZED AIRSPEED

Question 18

OVERSPEEDING OF THE GEAR OR FLAPS, IF EXTENDED, IS LIKELY TO OCCUR DURING OUT OF CONTROL FLIGHT RECOVERY PROCEDURES. IF OVERSPEED OCCURS, FURTHER MOVEMENT OF THE FLAPS OR LANDING GEAR MAY RESULT IN ADDITIONAL

Answer 18

DAMAGE

Question 19

THE MAX SYMMETRICAL G LIMIT FOR GROSS WEIGHTS ABOVE 125000 IS

Answer 19

2.0

Question 20

AFTER POWER TO THE DAS, WAIT APPROX _ SECONDS BEFORE ENGAGING THE AUTOPILOT TO ENSURE THE STARTUP BIT IS COMPLETE

Answer 20

20

Question 21

THE DAS REQUIRES REMOVAL OF STATIC PLUGS, PITOT COVERS, AND INERTIAL ALIGNMENT TO PASS A SUCCESSFUL IBIT

Answer 21

TRUE

Question 22

THE COPILOT SHALL CALL “APPROACH ACTIVE” DURING FMS APPROACHES WHEN RNP VALUES SEQUENCES TO _ AND APPROACH IS DISPLAYED ON THE CDU-7000

Answer 22

RNP 0.3

Question 23

THE RINU-G _ ARE/IS CERTIFIED FOR UTILIZING THE GPS AS THE PRIMARY MEANS OF NAVIGATION FOR OCEANIC, ENROUTE, TERMINAL, APPROACH OPERATIONS AND AS AN EXTERNAL FIXING SOURCE b

Answer 23

BOTH A AND B

Question 24

HE ADDU IS POWERED BY

Answer 24

MON DC AND FLIGHT DC

Question 25

THE ADDU ALERT LIGHT WILL ILLUMINATE WHEN THE AIRCRAFT ALTITUDE IS WITHIN A CAPTURE WINDOW OF _ FT OF THE SELECTED ALTITUDE, THE ALERT LIGHT GOES OUT WITH _ OF SELECTED ALTITUDE. AFTER ALTITUDE IS CAPTURED, IF THE AIRCRAFT DEVIATES MORE THAN _ FT THE ALERT LIGHT WILL ILLUMINATE.

Answer 25

1000/200/200

Question 26

THE MLR 2020A-1 MULTIMODE RECEIVERS ARE LOCATED IN RACK J-2. THESE MULTIMODE RECIVERS

Answer 26

PROVIDE FM-IMMUNE VHF RECEPTION IN THE 108.0 TO 117.95 MHZ FREQUENCY RANGE