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Dash-1 > Forberedelse Dash-1 delmålsprøve > Flashcards

Forberedelse Dash-1 delmålsprøve Flashcards

1
Q

The shoulder safety harness is stressed for ?

A

20 G

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2
Q

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

A

Oil pressure

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3
Q

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.

A

10-15 seconds

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4
Q

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

A

IMC, spatial
disorientation

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5
Q

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

A

enrich mixture, then follow with throttle

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6
Q

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

A

reduce throttle, then adjust mixture

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7
Q

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

A

Power, before …… high RPM

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8
Q

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

A

base and final speeds by 10 kts

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9
Q

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.

A

5 kts.
1050 kg
5 kts.

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10
Q

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

True/false?

A

True

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11
Q

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’’.

A

1200, 1800, 15-20 sec

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12
Q

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 ________.

A

Generator Field C/B
30 minutes

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13
Q

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.

A

26
3 seconds
1000’

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14
Q

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.

A

ANR circuit breaker

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15
Q

The GARMIN GNS 430 SYSTEM contains:

A

GPS
VHF-1 radio
VOR/ILS reciever

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16
Q

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

A

2 seconds
121.500 Mhz

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17
Q

The GUARD Frequency is not monitored in position MAIN.

True/False

A

True

18
Q

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.

A

90 Hz
2700
2500

19
Q

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

A

10 liters/ 2.5 gallons

20
Q

Before starting any aerobatics the …. list 3 things

A

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

21
Q

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

A

-15 C

22
Q

______ 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

A

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

23
Q

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

A

True

24
Q

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

A

28 V
24 V
24 V

25
Q

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

True/False

A

True

26
Q

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

A

OFF, off

27
Q

When will canopy warning light illuminate?

A

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

28
Q

When will canopy audio signal sound?

A

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

29
Q

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

A

25 +- 0,5V

30
Q

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

A

275 C

31
Q

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

A

6,5 +- 2,0 PSI

32
Q

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

A

20 +- 1 PSI

33
Q

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

A

25 psi, 30 seconds

34
Q

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

A

2500

35
Q

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

A

50 kts
25 kts

36
Q

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.

A

low

37
Q

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.

A

50 RPM, Rich Idle

38
Q

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.

A

175 RPM
2000 RPM
175 RPM
50 RPM

39
Q

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.

A

ON, 2500, 30-40 seconds, 1200

40
Q

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

A

-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.

Dash-1 (5 decks)

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