Usorterede DASH-ONE spørgsmål Flashcards

1
Q

ELECTRICAL SYSTEM?

A

The electrical system is powered by an engine driven 28 V generator with built-in rectifier

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2
Q

GENERATOR CAUTION?

A

In case the voltage of the bus drops below 25 ± 0.5 V, the control box will close the circuit and turn on the GEN light. The cause for low voltage is normally a malfunction of the charging system.

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3
Q

ENGINE FIRE WARNING?

A

In case the temperature in the engine compartment rises to 275° C the bi-metallic switch will close a circuit, thus turning on the FIRE ENG warning light.

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4
Q

OIL PRESSURE WARNING?

A

The pressure switch is located at the fitting behind the oil pressure indicator. When the oil pressure is below 6.5 ± 2.0 PSI, the circuit is closed and the warning light illuminates.

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5
Q

UNUSABLE FUEL?

A

The tanks can be completely emptied in level flight, but a normal amount of unusable fuel is 2.5 US gallons (10 litres) per tank. Thus, the total usable fuel is 42 US gallons (158 litres).

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6
Q

Hvad sker der når ALT STATIC AIR åbnes?

A

Airspeed kan vise 5-10 IAS for meget, og altitude ændringer kan være over normalt

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7
Q

Hvad indikerer at altitude encoder er i stykker?

A

CODE OFF

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8
Q

Hvad kan resultere i pause-and-accelerate effekt på altimeteret? Og hvornår skal man være særlig opmærksom på denne effekt?

A

The internal vibrator is inoperative. Be especially watchful when the minimum approach altitude lies between 8 and 2 (eg 1800-2200)

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9
Q

Voltage operating range for attitude indicator

A

18-31 V DC

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10
Q

Attitude indicator will operate satisfactorily under following conditions:

A

Operation range: -20C - 55C Exposure range: -55C - 85C Pressure -1000’ - 50.000’ Humidity: up to 95% at 50C

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11
Q

When starting up the attitude indicator note that:

A

Erect within 30 sec after power has been applied (regardless of reason for power on) Under standard conditions normal performance is achieved within 3 min. In temp range from -20C - 55C within 5 min.

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12
Q

Fire extinguisher specifications

A

Contains 700g HALON 1211 under nitrogen pressure of 7 bar at 20C Length of throw: 0.5-1.0 m in 20-30 sec (this time is reduced as temperature rises)

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13
Q

Hvilken fuel og olie bruger T-17

A

Fuel: AVGAS 100LL (NATO F-18) Olie: - Tilkørt motor: Aero Shell oil 15W50 - Ny motor 1/12-31/3: Straight mineral aviation oil 65 - Ny motor 1/4-30/11: Straight mineral aviation oil 80

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14
Q

Frequency range of VHF2 and UHF

A

VHF2: 118.000 MHz - 136.975 MHz UHF: 225.000 MHz - 399.975 MHz

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15
Q

Frequency for guard channel

A

243.000 MHz

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16
Q

Final and base speed corrections:

A

No flaps: +5kts to base and final >1050 kg: +5kts to base and final Alt stat air on: +10kts to base and final Gust +10kts: +1/2 gustfactor to final Short field landing: -10 kts to final

17
Q

Entry speed for: Roll Top Roll Half Roll Loop Lazy Eight Chandelle Clover Leaf Cuban 8 Barrel Roll Inverted Flight

A

Roll - 130 Top Roll - 150 Half Roll - 70 Loop - 140 Lazy Eight - 130 Chandelle - 130 Clover Leaf - 140 Cuban 8 - 140 Barrel Roll - 130 Inverted Flight - 130

18
Q

Hvad sker der når Emergency vælges på intercon

A

PPT fra VHF1 og VHF2 transmitterer

19
Q

AUX FUEL PUMP should be ON during entire TAKE-OFF climb when

A

+40C High density altitude

20
Q

AUX FUEL PUMP should be ON when airborn

A

Below 500’ AGL Utilizing fuel selector Fluctuating fuel flow

21
Q

AUX FUEL PUMP should be ON during TAXI when

A

+40C

22
Q

RUN UP CHECK 1-4 ikke bestået:

A

Varm motoren op ved 1200 RPM, til olietemperaturen er over 50C. Start derefter RUN UP CHECK forfra

23
Q

RUN UP CHECK viser drop på magnetos, udenfor limits:

A

Magnetos BOTH ON 2500 RPM Lean to peak EGT og kør motoren i 30-40 sek Reducer throttle til 1200 RPM og sæt mixture i rich (i denne rækkefølge) Start RUN UP CHECK forfra Er drops stadig udenfor limits, ground abort aircraft