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DASH-ONE > DASH-1 TEST > Flashcards

DASH-1 TEST Flashcards

1
Q

What is the ICAO code of T-17?

A

MFI-17

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2
Q

What is the wing dehidral?

A

1,5 degrees

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3
Q

What is the wing sweep forward?

A

5 degress

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4
Q

What construction i T-17?

A

The fuselage is a light semi-monocoque construction.

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5
Q

What is the fire wall made off? Which loads does it carry?

A

Stainless steel. It carries the loads from the engine mount and the nose gear.

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6
Q

Which loads does the lower beam absorb?

A

The lower beam absorbs the loads from the wing struts, main landing gear and safety harness.

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7
Q

Where is the main spar located? What profile is it?

A

The main spar is located at 30 % of the mean aerodynamic chord. It is an extruded I-profile.

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8
Q

Where is the rear spar located? What profile is it?

A

The rear spar is located at 75 % of the mean aerodynamic chord. Is a bent-up C-section.

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9
Q

What is done with the fuselage to avoid “oil canning”?

A

The fuselage panels are slightly curved to avoid “oil canning”

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10
Q

Which positions can the pilot seats be adjusted into”?

A

From Full aft/Full down to Full forward/Full up

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11
Q

What is the shoulder harness stressed for? Where is it attached?

A

20 g attached to the primary structure

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12
Q

Is the rear door lockable from the inside? Can it be opened during flight?

A

Yes and yes ( max 70 knots opening and max 100 knots when open)

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13
Q

What fuel is the engine powered by?

A

Avgas 100LL aviation grade fuel (F18)

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14
Q

Where is the fire detector located?

A

In the engine compartment through the right hand rear baffle plate

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15
Q

State propeller used by T-17?

A

Hartzell two-blade constant speed propeller

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16
Q

How is coarse pitch maintained?

A

By a mechanical device comprising counterweights which are acted upon by centrifugal force

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17
Q

How is fine pitch maintained?

A

By means of oil pressure

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18
Q

What happens is case of total oil pressure loss?

A

The propeller blades move into coarse pitch (thus preventing engine over speed)

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19
Q

Which fuel pumps are incorporated in the fuel system?

A

An engine driven diaphragm fuel pump and an electrically driven auxiliary fuel pump

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20
Q

What happens to the manifold pressure and RPM when opening the throttle?

A

Manifold pressure increases, RPM may increase

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21
Q

What is the range of the propeller control detent?

A

2500 RPM - 2700 RPM

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22
Q

What does clockwise movement of the friction lock do?

A

Increase friction

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23
Q

What happens if something is blocking the air intake?

A

The air is automatically drawn from the engine compartment (the alternate air intake is used)

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24
Q

What does the starting system consist of?

A

A 24V electric motor

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25
Q

What is unique for the left hand magneto compared to the right hand magneto?

A

It employs an impulse coupling to obtain the retarted spark necessary for starting

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26
Q

How is pressure distributed to the MP indicator and from where?

A

Via a hose from the engine

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27
Q

From where does the fuel flow indicator receive fuel pressure and reference pressure?

A

From the fuel divider bracket

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28
Q

How is the RPM indicator driven?

A

Mechanically through a drive shaft driven by the engine

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29
Q

How is oil pressure distributed to the oil pressure indicator?

A

Via a restrictor and a hose from the engine

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30
Q

Where is the cylinder head temperature picked up?

A

No. 3 cylinder head

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31
Q

From where does the EGT indicator receive information? What happens to the indication during VHF-AM transmissions?

A

The exhaust stack of cylinder no. 3. The indicator will show a false value caused by radiation

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32
Q

Describe the oil system?

A

The system is a full pressure, wet sump lubrication system, operated by a pump

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33
Q

Where is the oil cooler mounted?

A

On the RH side of the fire wall

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34
Q

Where is the oil separator tank installed? what is it’s function?

A

On the fire wall. Used to recover oil drained during negative g-loads

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35
Q

Where is the oil temperature transmitter located?

A

In the full flow oil filter adapter

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36
Q

Where is the fuel filter located?

A

On the fire wall between the fuel selector and the fuel pump

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37
Q

Describe the alternator? How many volts? Output?

A

Engine driven 28 V. MAX 28,7 volts at 70 amp

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38
Q

Describe the battery? Where is it located?

A

24V, 11AH. Mounted in the avionic compartment

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39
Q

What does volt/ammeter indicate?

A

The actual generator load

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40
Q

Where is the EGT fuse located?

A

Next to the EGT instrument

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41
Q

Which fuses are located in the avionic compartment?

A

Three fuses for the attitude indicator and one for the VHF/COM #2

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42
Q

State warning/caution light in the order of the instrument panel?

A

Canopy, Generator, Fire engine, Oil pressure

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43
Q

When will the canopy warning light illuminate?

A

When the canopy is unlocked and the BAT switch is on

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44
Q

When will the generator light illuminate?

A

Below 25 V +/- 0,5 V

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45
Q

When will the fire engine warning light illuminate?

A

At 275 degrees

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46
Q

When will the oil pressure warning light illuminate?

A

Below 6,5 PSI +/- 2,0 PSI

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47
Q

When will the stall warning horn sound?

A

5-10 knots above stalling speed

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48
Q

What type of landing gear is the T-17 equipped with? Where is it attaché to?

A

Fixed tricycle. Attached to the main bulkhead and the floor structure

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49
Q

Where is the nose gear attached to?

A

The engine mount and the fire wall

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50
Q

What kind of brakes are on T-17? Where is the hydraulic fluid container located?

A

Disc brakes. On the left hand side of the fire wall

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51
Q

Mention the pressure instruments?

A

Airspeed indicator, VVI, Altimeter

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52
Q

Mention the electrical instruments?

A

Radio magnetic indicator (RMI), Main Attitude indicator, Stand-by Attitude indicator, Turn/lip indicator

53
Q

In which direction does the ALT static air handle point when closed?

A

To the right (3 o’clock)

54
Q

What is the increase in indicated airspeed when ALT static air is used?

A

5-10 knots

55
Q

When will CODE OFF flag appear on the pneumatic altimeter?

A

When the encoder is inoperative

56
Q

How long does it take before the speed of the rotor on the attitude indicator is sufficient?

A

Within 3 minutes after normal power is applied

57
Q

What is the range of the accelerometer?

A

-5g to +10g

58
Q

Never engage starter for more than _____ sec. in one attempt

A

30

59
Q

For how long should the starter system cool off if it has been engaged for longer than 30 sec?

A

2 minutes

60
Q

What can happen if the RH magneto is switched on before the engine fires?

A

The engine will probably backfire

61
Q

If minimum oil pressure is not indicated within ____ sec. After engine start, stop engine?

A

30

62
Q

What is the max. Wind velocity for taxiing?

A

50 knots

63
Q

When should you use extreme caution when taxiing?

A

Above 25 knots

64
Q

What are the limits in the magnetos?

A

Drop not exceeding 175 RPM and max. differential drop between magnetos 50 RPM

65
Q

What happens to the RPM when take-off is performed with engine oil temperature below normal operating range?

A

A higher than normal engine RPM may be expected

66
Q

At what temperature should the aux. Fuel pump be turned on during the entire climb?

A

Above + 40 degrees

67
Q

Below what altitude should the aux. fuel pump be on?

A

500 ft AGL

68
Q

What can be done to avoid siphoning?

A

Place the fuel selector in position LEFT or RIGHT ON

69
Q

Base and final speeds should be increased by _____ when alt static air is selected.

A

10 knots

70
Q

For a no-flap landing increase base+final airspeed by_____.

A

5 knots

71
Q

At ______ kg ______ knots should be added to base and final speed.

A

1050, 5

72
Q

What should be added to final airspeed when winds are gusty?

A

1/2 the gust factor

73
Q

State RPM limits

A

2200 RPM - 2700 RPM, Never above 2730 RPM

74
Q

State oil pressure limits.

A

Caution 25 - 60 PSI and 85 - 100 PSI, Normal 60 - 85 PSI, MAX 100 PSI

75
Q

State oil temperature limits

A

Normal 50 - 120 degrees, MAX 120 degrees

76
Q

State cylinder head temperature limits.

A

Normal 105 - 225 degrees, Caution 225 - 245 degrees, MAX 245 degrees

77
Q

State fuel flow.

A

55% 8-9 GPH, 65% 9-11 GPH, 75% 10-12 GPH

78
Q

State AUW, G factor and maneuvers in normal category.

A

1200 kg, + 4,4 g - 2,2 g,

  1. Any maneuver used in normal flight
  2. Stalls (except whip stall, hammer stall)
  3. Lazy eights, chandelles and steep turns with angle of bank NOT exceeding 60 degrees
79
Q

State AUW, G factor and maneuvers in Utility I.

A

1125 kg, + 4,8 g - 2,4 g

  1. Any maneuvers in normal category
  2. Erect stall
  3. Spins
  4. Lazy eights, chandelles and steep turns with angle of bank exceeding 60 degrees
80
Q

State AUW, G factor and maneuvers in Utility II.

A

1000 kg + 5,4 g - 2,7 g

  1. Any maneuvers in utility category I
  2. Rolling
  3. Looping
  4. Half roll (Split-S)
  5. Top roll (Immelmann)
81
Q

State AUW, G factor and maneuvers in aerobatic.

A

900 kg + 6,0 g - 3,0 g

Same maneuvers as in utility categories I and II

82
Q

What is inverted flight limited to?

A

10 sec

83
Q

What is the maximum permissible load in the rear compartment?

A

100 kg if the load is placed on a special cargo floorboard, the maximum load can be raised to 150 kg.

84
Q

What is maximum landing weight?

A

1140 kg

85
Q

What can happen during and/or immediately after inverted flight?

A

A momentary loss of power due to air locks in the fuel system

86
Q

How many persons are allowed on board during aerobatic flight?

A

Two people

87
Q

State Vne and explain the meaning of Vne.

A 
196 knots (Never exceed)
Air speed never to be exceeded
88
Q

State Vno and explain the meaning of Vno.

A 
154 knots (Max. structural cruising)
Air speed at which turbulent airspeed can damage aircraft
89
Q

State Va and explain the meaning of Va.

A 
143 knots (Max manuevering)
Airspeed at which abrupt control can damage aircraft
90
Q

State Vf and explain the meaning of Vf.

A

130 knots

Max airspeed with flaps extended 1-10 degrees

91
Q

State Vfe and explain the meaning of Vfe.

A

100 knots

Max airspeed with flaps extended 11-38 degrees

92
Q

State spin entry.

A

?

93
Q

State spin recovery.

A

?

94
Q

State entry speed of roll.

A

130 knots

95
Q

State entry speed of top roll (Immelmann).

A

150 knots

96
Q

State entry speed of half roll (Split-S).

A

70 knots

97
Q

State entry speed of loop.

A

140 knots

98
Q

State entry speed of lazy eights.

A

130 knots

99
Q

State entry speed of chandelle.

A

130 knots

100
Q

What should you do before starting any aerobatic maneuvers?

A

Aux fuel pump ON, Fuel selector BOTH ON, RPM set 2500

101
Q

What is the aircraft basic weight?

A

761 kg

102
Q

State engine limits on ground?

A

Avoid RPM lower than 1200. Never exceed 2500 RPM

103
Q

Define a warning.

A

Operation procedures, techniques, etc., which will result in personal injury or loss of life if not carefully followed.

104
Q

Define a caution.

A

Operaion procedures, techniques, etc., which will result in damage to equipment if not carefully followed.

105
Q

Define a note.

A

An operatting procedurem technique, etc., which it is considered essential to emphasize.

106
Q

State limits on altimeter.

A

-1.000 to + 50.000 feet

107
Q

Total fuel on board for each tank?

A

23,5 USG

108
Q

When will the warning horn sound due to canopy unlocked?

A

When any of the IGN switches is on and the canopy is unlocked.

109
Q

With completely empty tanks the fuel indicators may show as much as ____ USG in each tank.

A

2 USG

110
Q

Is the wing flap system mechanically operated?

A

NO it’s electrically operated.

111
Q

When external power is used the battery should be in _____ position and the generator should be in _____ position.

A

OFF, OFF

112
Q

Total useable fuel per wing tank?

A

21 USG

113
Q

A total of _____ feet altitude loss is average for entry, ____ turns of spin and recovery.

A

2500, 6

114
Q

What is the guard frequency on UHF and VHF?

A

243,000 MHz 121,500 kHz

115
Q

State spin rate of rotation and altitude loss per turn.

A

2,5 sec/turn, approx. 300-400 ft/turn

116
Q

With partly filled tanks each fuel indicator may show as much as _____ USG more

A

3,5

117
Q

State leaning procedure.

A

With both magnetos “ON”, set RPM to 2500 RPM, lean to peak EGT, and run the engine for 30 - 40 seconds at peak EGT.

118
Q

At what temperature should the oil be preheated before starting the engine?

A
  • 15 degrees C
119
Q

What is the guideline for battery capacity, with the generator switched off?

A

30 min

120
Q

Where is the landing light installed?

A

The landing light is installed in the front of the lower engine cowling

121
Q

Name the exterior lights

A

Landing light, taxi light, navigation lights, strobe lights and anti-collision lights

122
Q

Where is the taxi light installed?

A

The taxi light is installed on the nose wheel landing gear

123
Q

Where are the navigation lights installed?

A

On the LH wing tip (Red light) and on the RH wing tip (Green light) and one white light in the tail cone

124
Q

Where are the strobe lights installed?

A

On the wing tips

125
Q

Where are the anti-collision lights installed?

A

One in the tip fairing of the rudder and the other one in the ventral fin underneath the tail section

126
Q

Name the two flight instrument groups

A

Pressure instruments and electrical instruments

127
Q

Name the electrical flight instruments

A

Main and ST-BY attitude indicator, RMI (Radio Magnetic indicator) and Turn/Slip indicator

128
Q

What happens if the altimeter’s internal vibrator is inoperative?

A

The pause-and-accelerate effect may be exaggerated

129
Q

What are the maximum parralax error of pitch and bank indication, within a cone angle of 30 degrees?

A

Less than 2 degrees

DASH-ONE (6 decks)

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