EKQ

Question 1

Height and speed limitations DI0

Answer 1

Sea Level - 5000ft = 550Kts
5000 - 13500 = 0.9M
13500 - 30000 = 475Kts
30000 - 48000 = 1.2M

Question 2

Landing Gear limits

Answer 2

200 Kts

Question 3

Flaps limits

Answer 3

200 Kts 0 - 2.5g

Question 4

Airbrake limits

Answer 4

Above 0.9 - 1g

Below 0.9 - 7.2g

Question 5

Landing Gear Emergency Lowering limits

Answer 5

200kts

Question 6

Landing Gear Emergency Lowering limits

Answer 6

200kts

Question 7

Flap emergency lowering

Answer 7

200kts

Question 8

Hawks G limits

Answer 8

DI0 - minus 3.5 - 8
DI5 - minus 3.5 - 7.2*
DI15 - minus 3.5 - 7.2*

Question 9

Hawks G limits

Answer 9

DI0 - minus 3.5 - 8
DI5 - minus 3.5 - 7.2*
DI15 - minus 3.5 - 7.2*

Question 10

How do you calculate threshold speed for:

Answer 10

Normal - 115 + 1kt / 100kg
Flapless - 135 + 1kt / 100kg
PFL/AFL - 150 min 170 max
HYD1 and HYD2 - 125kt

Question 11

Approach Category Hawk

Answer 11

C

Question 12

The DH/MDH allowance for Standby Instruments?

Answer 12

50

Question 13

The DH/MDH allowance for Standby Instruments?

Answer 13

100

Question 14

Minimum power setting on normal approach

Answer 14

70%

Question 15

What is the minimum runway distance to go that power must be applied during a PFL touch and go?

Answer 15

3000ft

Question 16

What are the standard stall recovery actions?

Answer 16

a. Simultaneously:
(1) Unload - Move control column forward to reduce AOA and eliminate the buffet.
(2) Full Power.
(3) Wings Level. Use aileron but avoid re-stalling the wing.

b. Climb. As power bites, smoothly select a climbing attitude. Do not re-enter buffet.
c. Clean up. With a positive ROC on both the main altimeter and VSI selected gear and flap up. Check: “GearUp, Flap Up and Captions Clear by 200kts”.

Question 17

What are the standard spin recovery actions?

Answer 17

Simultaneously
1 -check height,
2 - select idle,
3 - centralise controls, and check TPI zero.

When the spin stops, roll to the nearest horizon and ease out of the dive on the light buffet.

(A common error is to call the height out first, before centralising the controls. This in effect delays the recovery and increases the height lost. The actions should be carried out simultaneously;it is the centralisation of the controls that will stop the spin.)

Question 18

At what height would you eject if the aircraft is still spinning?

Answer 18

5000ft AGL

Question 19

What are the crosswind limits for (Hawk T1 Formation SOPs)

Answer 19

Singleton - 30kts
Vic T/O - ***
Pairs T/O - 15
Formation Landing - 15

Question 20

Max TGT during start

Answer 20

570 (Transient exceeded 20 degrees for 10 seconds)

Question 21

Max TGT during relight

Answer 21

585 (Transient exceeded 20 degrees for 10 seconds)

Question 22

Idle RPM Nominal (Bleed Valve Closed)

Answer 22

55.0 at ISA

Question 23

Idle TGT Nominal (Bleed Valve Closed)

Answer 23

450

Question 24

Max Continuous RPM and TGT

Answer 24

99.3% - 615

Question 25

Max Power RPM TGT

Answer 25

104.0% - 665 (TGT limiter is set to 660 +- 5 ) limited to 30 min per flight

Question 26

Transient TGT

Answer 26

685 limited to 20 seconds

Question 27

If on Start the Rotation MI failed to show Green within 10 seconds of selecting the Start switch to START?

Answer 27

Throttle - Confirm HP OFF
Engine Start Switch - OFF
Report Defect

Question 28

If on Start the engine failed to light within 15 seconds from selecting idle?

Answer 28

Throttle - HP OFF

Carry out dry crank

Question 29

If on Start The TGT appears likely to exceed 570 degrees C?

Answer 29

Throttle - HP OFF (Transient can be exceeded by 20 degrees for 10 seconds)