Forberedelse Dash-1 delmålsprøve

Question 1

The shoulder safety harness is stressed for ?

Answer 1

20 G

Question 2

Fine pitch (high RPM) is maintained by means of?

Answer 2

Oil pressure

Question 3

Flying with full tanks and the fuel selector in position BOTH ON may cause siphoning of fuel
from either tank. To correct the situation, place the fuel selector in position LEFT or RIGHT
ON and the siphoning will stop within _____ sec.

Answer 3

10-15 seconds

Question 4

Correcting a fuel imbalance by skidding the aircraft under ____ may cause _______.

Answer 4

IMC, spatial
disorientation

Question 5

TO INCREASE POWER – first, ______ , then follow with _______.

Answer 5

enrich mixture, then follow with throttle

Question 6

TO DECREASE POWER – first, reduce _______, and then adjust _____

Answer 6

reduce throttle, then adjust mixture

Question 7

If using a high power setting, reduce _____ before selecting ______

Answer 7

Power, before …… high RPM

Question 8

If ALT STATIC AIR is selected, increase ____ and ____ speeds by ____.

Answer 8

base and final speeds by 10 kts

Question 9

For a no-flap landing increase base and final speeds by ____.
If the aircraft gross weight is above _____ kg, increase base and final speeds by ____.
When winds are gusty, add one-half the gust factor to final airspeed.

Answer 9

5 kts.
1050 kg
5 kts.

Question 10

Too rapid movement of the throttle may cause engine over speed.

True/false?

Answer 10

True

Question 11

Before ’’Engine Shut Down’’ engine RPM should be set at ____ RPM until oil temperature
has stabilized.
Unless inconvenient due to environmental conditions, RPM should be increased to _____
RPM before ’’Mixture – CUT OFF for a period of _____ sec’’.

Answer 11

1200, 1800, 15-20 sec

Question 12

Pulling _________ disconnects the Generator from the electrical system. The
aircraft main battery will thereafter supply electrical power to the primary and secondary
electrical buses if the generator switch is on, for a period of approximately ________.

Answer 12

Generator Field C/B
30 minutes

Question 13

CAUTION FORCED LANDING
The engine must smoothly be cleared by opening the throttle to ___’’ MP for _________ for
every _______’ of gliding at IDLE power to remove lead from spark plugs.

Answer 13

26
3 seconds
1000’

Question 14

In case of malfunction or unwanted noise from the ANR system, the _______
should be pulled. This will not affect the normal operation of the intercom system.

Answer 14

ANR circuit breaker

Question 15

The GARMIN GNS 430 SYSTEM contains:

Answer 15

GPS
VHF-1 radio
VOR/ILS reciever

Question 16

In an in-flight emergency, depressing and holding the Comm Transfer Button for will select the emergency frequency of ______ into the ’’Active frequency
window’’.

Answer 16

2 seconds
121.500 Mhz

Question 17

The GUARD Frequency is not monitored in position MAIN.

True/False

Answer 17

True

Question 18

Due to interference between the ___ zones of the ILS and the propeller blades at the ______
RPM, the localizer and glide slope needles may oscillate if more than _____ RPM is used on
ILS final approach.

Answer 18

90 Hz
2700
2500

Question 19

The amount of unusable fuel supply is________per tank. Each tank, however,
can be completely emptied in level flight.

Answer 19

10 liters/ 2.5 gallons

Question 20

Before starting any aerobatics the …. list 3 things

Answer 20

Auxiliary fuel pump must be switched ON
Fuel selector turned to BOTH ON position
RPM set to 2500 RPM.

Question 21

At temperature below _____, engine oil should be preheated before starting engine.

Answer 21

-15 C

Question 22

______ in each tank, _____ total
Unusable fuel is ___________
The total usable fuel is therefore _____
With partly filled tanks the indicator may show as much as _____ more
With completely empty tanks indicator may show as much as ____ in each tank
The tanks can only be completely emptied in straight and level flight

Answer 22

23.5 G, 47 G
2.5 G/ 10 L
42 G
3.5 G
2 G

Question 23

Map reading lights are powered from the emergency bus and the EPU switch must be in on
positions to supply electrical power to the map lights.

True/false

Answer 23

True

Question 24

Generator ____ Volt
Main battery _____ Volt
EPU (emergency power supply unit) ____ Volt

Answer 24

28 V
24 V
24 V

Question 25

The EPU switch shall be in OFF position whenever external power is connected to the aircraft. True/False

Answer 25

True

Question 26

BAT switch shall be in ____ position when external power is used, otherwise the external power is shut ____.

Answer 26

OFF, off

Question 27

When will canopy warning light illuminate?

Answer 27

CANOPY warning light (red) when canopy unlocked and BAT is ON.

Question 28

When will canopy audio signal sound?

Answer 28

In addition also an audio signal when any of the IGN switches is ON and the canopy is unlocked.

Question 29

GEN caution light (amber) in case the voltage of the bus drops below ______

Answer 29

25 +- 0,5V

Question 30

FIRE ENG warning light (red) in case the temperature in the engine compartment rises to _____

Answer 30

275 C

Question 31

OIL PRESS warning light (red) illuminates when the oil pressure is below ______

Answer 31

6,5 +- 2,0 PSI

Question 32

FUEL PUMP ON light (amber) to indicate that the fuel pump is ON and delivering a minimum fuel pressure of _____

Answer 32

20 +- 1 PSI

Question 33

If minimum oil pressure _____ is not indicated within ______ after engine start, stop engine.

Answer 33

25 psi, 30 seconds

Question 34

Do not exceed ____ RPM on ground except during take-off.

Answer 34

2500

Question 35

NEVER ATTEMPT TAXIING IN WIND VELOCITIES OF MORE THAN _____. USE EXTREME CAUTION IN WIND VELOCITIES OF MORE THAN _______.

Answer 35

50 kts 25 kts

Question 36

Taxiing in slush may cause the static ports to get blocked by ice due to splash from the main wheels. Therefore taxi speed should be as ____ as possible.

Answer 36

low

Question 37

An RPM increase of _____ or more indicates an excessively ____ Mixture. An Immediate decrease in RPM, if not preceded by an increase, indicates the Idle Mixtures is too Lean.

Answer 37

50 RPM, Rich Idle

Question 38

If the RPM drop exceeds _____, slowly lean the mixture until the RPM peaks. Then retard the throttle to the specified _______ for the magneto check and repeat the check. If the drop-off does not exceed ______, the difference between the magnetos does not exceed______, and the engine is running smoothly, then the ignition system is operating properly. Return the mixture to full rich.

Answer 38

175 RPM 2000 RPM 175 RPM 50 RPM

Question 39

If ’’Engine Run-Up’’ shows magneto drop out of limit and/or uneven engine run, then, with both magnetos ’’____’’, set RPM to _____ RPM, lean to peak EGT, and run the engine for ______ seconds at peak EGT, then reduce RPM to _____ RPM and select mixture rich. Perform a new engine run-up check. If magneto drop is still out of limits, ground abort aircraft.

Answer 39

ON, 2500, 30-40 seconds, 1200

Question 40

When airborne the auxiliary fuel pump should be ON during the following conditions?

Answer 40

-When flying below 500 ft AGL -During any airborne utilization of the fuel selector, until the operator is assured that there will be no interruption of the fuel flow (5 seconds). -Any time the fuel flow is fluctuating or the engine is affected by the fluctuation.