Need To Know

Question 0

Max airspeed with take off power?

Answer 0

90 KIAS

Question 1

Minimum voltage required for a start?

Answer 1

23volts

Question 2

Q line is ?

Answer 2

500kg / 1102lbs

Question 3

Low fuel light illuminates at…?

Answer 3

92kg / 202lbs

Question 4

If a boost pump is inoperative and cross feed is open, you will have ……… Of unusable fuel?

Answer 4

228kg / 502lbs

Question 5

AEO
Max continuous power?

Max T/O…5min?

Max transient…5sec?

Answer 5

100%

110%

121%

Question 6

VLE/VLO?

Answer 6

150 KIAS

Question 7

Pitot heat must be on between ….

Answer 7

4c and 10c

Question 8

OEI
Max continuous…..

Max 2.5min ……….

Max transient 5sec…

Answer 8

140 KIAS

160 KIAS

176 KIAS

Question 9

Min Auto Speed?

Answer 9

40KIAS

Question 10

IFR approach, MIN and MAX speeds?

Answer 10

Max 150KIAS, Min 50KIAS.

Question 11

Starting ITT 2sec limit?

Answer 11

1000c.

Question 12

Max speed for wheel brake application?

Answer 12

40kts.

Question 13

Paved and grass taxi speed limits?

Answer 13

Paved, 40kts above 20 nose wheel must be locked.

Grass, 20kts above 10 nose wheel must be locked.

Emergency landing, 60kts on paved, 40kts on grass.

Question 14

Starter limits?

Answer 14

45sec on 60sec off, 45sec on 60sec off, 45sec on 30min off.

Question 15

With torque limiter set what is the max AEO tq available?

Answer 15

114% 114% (228%)

Question 16

If MAU 1 or 2 fail, electrical and HYD synoptic pages are…..?

Answer 16

Unreliable.

Question 17

Critical relative wind sector?

Answer 17

090-135

Question 18

Abort engine start if……?

Answer 18

Light off is not achieved within 10sec.
Abnormal noise heard.
ITT increases beyond limits (hot start caution illuminates).
Engine hangs (NG stagnation below 54%).
The main rotor has not begun to rotate by 40% NG.
Engine starter fails to disengage by 49%.

Question 19

Aborted start procedure?

Answer 19

ENG Mode Switch - OFF
If engine does not SHUT OFF then:
ECL - OFF
FUEL PUMP - OFF
ENG FUEL Switch - OFF
Wait 30sec then follow dry motor procedure found on page 36QRH

Question 20

Define PC2

Answer 20

Performance Class 2 profiles mimic Cat A profiles with the emphasis for takeoff using 18- 23% PI over hover power, not to exceed MTOP to decrease exposure time to achieve Vtoss and Vy.
Should an engine fail, the helicopter may safely continue the flight except when….Engine failure prior to TDP or after LDP a forced landing may be required.

Question 21

With one AP failed, what limitations are imposed?

Answer 21

100kts Max Climb.

140kts Max Cruise.

Max ROC 1000fpm.

Question 22

CAT A Clear Area VTOSS = ?

CAT A Offshore Helideck VTOSS = ?

Answer 22

Clear Area = 50kts.

Offshore = 40kts.

Question 23

If servo light illuminates…..?

Answer 23

DO NOT use SOV…….this could render the whole servo stack inoperative.

Question 24

VY = ?

Answer 24

VY = 80kts.

Question 25

Land Immediately = ?

Answer 25

1. Fire, that cannot be extinguished.
2. Multiple transmission failures.
3. Tail rotor; control fail, binding, drive fail in hover.