Technical Info Flashcards

1
Q

Airframe construction?

A

Aluminium alloy with steel engine mounts / landing gear and fibreglass / thermo plastic fairings.

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2
Q

Fuselage construction?

A

Semi-monocoque.

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3
Q

Wing design?

A

Semi-tapered.

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4
Q

Main spar (%MAC)?

A

40%

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5
Q

How many spars per wing?

A

3 Spars

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6
Q

What type of tab does the stabilator have and what does it do?

A

Anti servo tab providing longitudinal stability and longitudinal trim.

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7
Q

What type of tab does the rudder have and what does it do?

A

Servo tab which lags behind the control inputs of the rudder and moves in the opposite direction which eases control inputs.

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8
Q

Engine Specs (9)

A

Continental Motors L/TSIO-360-RB Direct drive Horizontally opposed Fuel Injected Air Cooled Turbo Charged (After cooled) Variable waste gate 220 BHP

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9
Q

what does the variable waste gate controller restrict the MAP to?

A

38”

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10
Q

In the event of the waste gate malfunctioning what pressure will the pressure relief valve release the pressure at?

A

42”

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11
Q

Propellor specs (4)

A

McCauley 3 Blade Constant speed Counter rotating

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12
Q

What generates the force to fine / coarse propellor pitch?

A

Fine = Oil px Coarse = Counter weights

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13
Q

How long does it take to feather?

A

6 seconds

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14
Q

How much fuel and where from does the combustion heater take fuel?

A

Right wing, 1/2 USG per hour

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15
Q

After turning off the combustion heater how long must the air intake be left open for?

A

15 Seconds

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16
Q

After use of combustion heater on the ground how long must the fan be on for?

A

2 minutes

17
Q

When is the heater fan automatically switched off?

A

When the gear is retracted

18
Q

What prevents the heater from working if the intake is not fully open or it partially blocked?

A

Safety switch

19
Q

What voltage is the electrical system?

A

24V

20
Q

Primary battery specs (3)

A

19 ampere hour 24V Lead Acid

21
Q

How long should the emergency battery last?

A

30 mins

22
Q

Where are the primary and the emergency batteries located?

A

Under the floor of the aft baggage area

23
Q

Alternator specs (3)

A

85 Amps 28 V Regulated not to exceed 32 V

24
Q

How many fuel tanks per wing?

A

3: Inboard Outboard Bladder

25
Q

Fuel Capacity

A

64 Each side (including 3 unusable) Total 122 USG (Usable)

26
Q

Which fuel tank is fuel drawn from?

A

Inboard

27
Q

Type of fuel system sensors?

A

Float type (2 per wing)

28
Q

After pressing the pneumatics boots when is the air released into the boots?

A

After reaching 6 seconds or 17 psi

29
Q

When is the SURF DEICE ON CAS message displayed?

A

Above 8 psi

30
Q

Describe the cycle for the propellor de-ice?

A

90 seconds on all 3 blades on one side and then alternates to the other side.

31
Q

Tyre Specs

A

6.00 x 6 Nose = 6 ply Mains = 8 ply

32
Q

How many degrees is the nose wheel steerable either side the centre line?

A

27 degrees

33
Q

When is the gear unsafe caution displayed? (3)

A

When below 14” MAP Flaps selected 25 - 40 Gear selector up on the ground

34
Q

When does the check gear CAS caution displayed as a check gear CAS warning?

A

Below 400 feet.

35
Q

What is the speed restriction when using the emergency gear to deploy them?

A

85 KIAS

36
Q

What is the definition of non threat traffic on TAS

A

Beyond 6 nm +/- 1200’

37
Q

What are the symbols used on the TAS?

A
38
Q

When is the diamond shape replaced by a triangle on the TAS?

A

When the traffic is equiped with ADS-B.