DASH 1 Sec 3: Emergency Procedures

Question 1

Air minimum control speed, Vmca is ______ and Ground minimum control speed, Vmcg is ___.

Answer 1

8988

Question 2

The pilot’s responsibilities during emergency ground egress are:

Answer 2

throttles- cutoff; parking brake - as required; battery - off

Question 3

There are ____ hand held fire extinguishers on the T-1.

Answer 3

2

Question 4

Securing a failed or on-fire engine should not be accomplished prior to ____ feet, or clear of obstructions.

Answer 4

400

Question 5

If, during an engine fire during flight, the fire switchlight goes out you should.

Answer 5

test the fire warning system

Question 6

normal oil pressure is _____.

Answer 6

60 to 83 psi at speeds above 60% N2

Question 7

A popped fuel system circuit breaker can be reset _____.

Answer 7

0

Question 8

You should not reset popped BUS FDR circuit breakers.

Answer 8

TRUE

Question 9

For the trim interrupt and autopilot disengage switch to work, both pilots must push the red button.

Answer 9

FALSE

Question 10

You can use up to ____ degrees of bank during an emergency descent.

Answer 10

45

Question 11

In a crew environmental emergency with all occupants breathing oxygen, attempt to keep the cabin at or below ______ft, but in no case allow it to exceed ______ft.

Answer 11

18000; 25000

Question 12

During loss of airspeed indication the Dash-1 wants you to maintain an AOA of .2. This equates to about what airspeed.

Answer 12

210

Question 13

During a single engine go-around, rotate to approximately ____ degrees nose high.

Answer 13

10

Question 14

Do not attempt an actual single engine go-around after _______.

Answer 14

selecting 30- degree flaps

Question 15

Ideally, you should arrive at high key during a forced landing with no power at _____KIAS and ____ feet AGL.

Answer 15

160; 4000

Question 16

During ditching you should unstrap before you hit the water.

Answer 16

FALSE

Question 17

An illuminated HYD LEVEL LO annunciator indicates there is less than _____ gallons of hydraulic fluid in the reservoir.

Answer 17

0.6

Question 18

The glide ratio for the T-1 is about _____miles for every 1000 feet AGL.

Answer 18

2

Question 19

If you are flying over Vance at 11,000 feet when both engines flame out the maximum glide distance is _____.

Answer 19

about 22 miles

Question 20

Primary egress after a ditching is through the .

Answer 20

emergency escape hatch

Question 21

A no flap landing will increase your 30-flap landing distance by _____ %

Answer 21

35

Question 22

If you have zero hydraulic pressure, your computed 30 degree flap landing distance will increase by ____%.

Answer 22

90

Question 23

Consider recycling the gear handle during a gear malfunction only with.

Answer 23

A and C

Question 24

The maximum airspeed for emergency gear extension is ______.

Answer 24

150

Question 25

When emergency extending the landing gear, they should down lock in approximately ____ seconds.

Answer 25

30

Question 26

Anti-skid protection is not available during emergency braking.

Answer 26

TRUE

Question 27

If ice accumulation is visible on the wing leading edge, use ____ flaps for landing.

Answer 27

10 degree

Question 28

An approach speed of Vapp+ _______ KIAS is required for ice accumulations of approximately 1.5 inches.

Answer 28

35

Question 29

If the rudder boost is off during single engine operations, you will experience

Answer 29

higher than normal rudder pedal forces.

Question 30

If the yaw damper fails, flight may be continued below.

Answer 30

FL280

Question 31

With a dual RTU failure, _______ is the only comm/nav frequency that can be retuned

Answer 31

Nav 1

Question 32

When you have a failure of a stall warning system you should avoid.

Answer 32

low indicated airspeeds at high altitudes

Question 33

If the DOOR UNLOCK annunciator illuminates send the Jump or Copilot to check for "8 whites"

Answer 33

FALSE

Question 34

Momentarily holding the horizontal stab de-ice back up switch to manual energizes the system for \_\_\_\_\_\_. Repeat this procedure every \_\_\_\_\_\_.

Answer 34

30 seconds; 2 minutes

Question 35

After prolonged flight in cold temperatures, followed by rapid descent, one or both ______ annunciators may illuminate momentarily when gear down is selected.

Answer 35

H PMP Press LO

Question 36

If you inadvertently encounter icing, wait ____ between turning on engine anti-ice for the second engine.

Answer 36

1 minute

Question 37

Anti-skid protection is available during emergency braking.

Answer 37

FALSE

Question 38

You can still use the parking brake even though you have lost hydraulic power.(not talking about setting parking break during ground ops.)

Answer 38

FALSE

Question 39

Air minimum control speed, Vmca is ______ and Ground minimum control speed, Vmcg is \_\_\_.

Answer 39

8988

Question 40

The pilot's responsibilities during emergency ground egress are:

Answer 40

throttles- cutoff; parking brake - as required; battery - off

Question 41

There are ____ hand held fire extinguishers on the T-1.

Answer 41

2

Question 42

Securing a failed or on-fire engine should not be accomplished prior to ____ feet, or clear of obstructions.

Answer 42

400

Question 43

If, during an engine fire during flight, the fire switchlight goes out you should.

Answer 43

test the fire warning system

Question 44

normal oil pressure is \_\_\_\_\_.

Answer 44

60 to 83 psi at speeds above 60% N2

Question 45

A popped fuel system circuit breaker can be reset \_\_\_\_\_.

Answer 45

0

Question 46

You should not reset popped BUS FDR circuit breakers.

Answer 46

TRUE

Question 47

For the trim interrupt and autopilot disengage switch to work, both pilots must push the red button.

Answer 47

FALSE

Question 48

You can use up to ____ degrees of bank during an emergency descent.

Answer 48

45

Question 49

In a crew environmental emergency with all occupants breathing oxygen, attempt to keep the cabin at or below \_\_\_\_\_\_ft, but in no case allow it to exceed \_\_\_\_\_\_ft.

Answer 49

18000; 25000

Question 50

During loss of airspeed indication the Dash-1 wants you to maintain an AOA of .2. This equates to about what airspeed.

Answer 50

210

Question 51

For a single engine landing, normal landing distance will increase by ______ percent.

Answer 51

20

Question 52

Set flaps to 30-degree for a single engine landing only if \_\_\_\_\_\_\_.

Answer 52

10-deg landing distance is greater than the runway available.

Question 53

If selecting flaps to 30-degrees for a single engine landing, do so no later than \_\_\_\_\_\_\_.

Answer 53

300 feet AGL

Question 54

During a single engine go-around, rotate to approximately ____ degrees now high.

Answer 54

10

Question 55

Do not attempt an actual single engine go-around after \_\_\_\_\_\_\_.

Answer 55

selecting 30- degree flaps

Question 56

Ideally, you should arrive at high key during a forced landing with no power at \_\_\_\_\_KIAS and ____ feet AGL.

Answer 56

160; 4000

Question 57

During ditching you should unstrap before you hit the water.

Answer 57

FALSE

Question 58

An illuminated HYD LEVEL LO annunciator indicates there is less than _____ gallons of hydraulic fluid in the reservoir.

Answer 58

0.6

Question 59

The glide ratio for the T-1 is about \_\_\_\_\_miles for every 1000 feet AGL.

Answer 59

2

Question 60

If you are flying over Vance at 11,000 feet when both engines flame out the maximum glide distance is \_\_\_\_\_.

Answer 60

about 22 miles

Question 61

Primary egress after a ditching is through the .

Answer 61

emergency escape hatch

Question 62

A no flap landing will increase your 30-flap landing distance by _____ %

Answer 62

35

Question 63

If you have zero hydraulic pressure, your computed 30 degree flap landing distance will increase by \_\_\_\_%.

Answer 63

90

Question 64

Consider recycling the gear handle during a gear malfunction only with.

Answer 64

A and C

Question 65

The maximum airspeed for emergency gear extension is \_\_\_\_\_\_.

Answer 65

150

Question 66

When emergency extending the landing gear, they should down lock in approximately ____ seconds.

Answer 66

30

Question 67

Anti-skid protection is not available during emergency braking.

Answer 67

TRUE

Question 68

If ice accumulation is visible on the wing leading edge, use ____ flaps for landing.

Answer 68

10 degree

Question 69

An approach speed of Vapp+ _______ KIAS is required for ice accumulations of approximately 1.5 inches.

Answer 69

35

Question 70

If the rudder boost is off during single engine operations, you will experience

Answer 70

higher than normal rudder pedal forces.

Question 71

If the yaw damper fails, flight may be continued below.

Answer 71

FL280

Question 72

With a dual RTU failure, _______ is the only comm/nav frequency that can be retuned

Answer 72

Nav 1

Question 73

When you have a failure of a stall warning system you should avoid.

Answer 73

low indicated airspeeds at high altitudes

Question 74

If the DOOR UNLOCK annunciator illuminates send the Jump or Copilot to check for "8 whites"

Answer 74

FALSE

Question 75

Momentarily holding the horizontal stab de-ice back up switch to manual energizes the system for \_\_\_\_\_\_. Repeat this procedure every \_\_\_\_\_\_.

Answer 75

30 seconds; 2 minutes

Question 76

After prolonged flight in cold temperatures, followed by rapid descent, one or both ______ annunciators may illuminate momentarily when gear down is selected.

Answer 76

H PMP Press LO

Question 77

If you inadvertently encounter icing, wait ____ between turning on engine anti-ice for the second engine.

Answer 77

1 minute

Question 78

Anti-skid protection is available during emergency braking.

Answer 78

FALSE

Question 79

You can still use the parking brake even though you have lost hydraulic power.(not talking about setting parking break during ground ops.)

Answer 79

FALSE