PC24 Limitations Flashcards

(54 cards)

1
Q

What documents must be aboard the aircraft in paper format?

A

The PC-24 Airplane Flight Manual (AFM)

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2
Q

What documents must be aboard the aircraft in either electronic (digital) or paper format?

A
  • Quick Reference Handbook (QRH)
  • The Advanced Cockpit Environment Pilot’s Guide
  • Flight Crew Operating Manual
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3
Q

What is the minimum pressure altitude?

A

1,000 ft MSL

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4
Q

What is the maximum pressure altitude for landing field elevation?

A

10,000 ft MSL

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5
Q

What is the maximum runway slope?

A

±2%

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6
Q

What is the maximum tailwind component for takeoff and landing?

A

10 kt

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7
Q

Flight operation above ______ ft (MSL) with the yaw damper disengaged is prohibited.

A

30,000 ft (MSL)

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8
Q

The minimum engagement height of the autopilot after take-off is _____

A

400 feet AGL

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9
Q

The minimum engagement height of the yaw damper after take-off is _____

A

50 feet AGL

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10
Q

The autopilot, yaw damper and autothrottle must be disengaged below:

A

3D Approach (ILS OR VGP) = 200 ft AGL (<4.5 degree glide slope)
2D Approach (Non-Precision) = 400 ft AGL

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11
Q

Maximum Operating Speed

A

VMO 290 KIAS
MMO 0.74 M

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12
Q

Do not make full or abrupt control movements above this speed

A

8300 kg - 170 KIAS
5190 kg - 120 KIAS

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13
Q

Maximum Operating Maneuvering Speed (Rudder)

A

Full or abrupt control movements - 125 KIAS (130 KIAS Below FL200)

1/3 of pedal travel - 185 KIAS

1/10 of pedal travel - 290 KIAS

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14
Q

Maximum Flap Extended Speed (VFE)

A

8° & 15° - 200 KIAS
33° - 175 KIAS

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15
Q

Maximum Landing Gear Extended Speed

A

250 KIAS

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16
Q

Maximum Landing Gear Operating Speed:
Extend _____ KIAS
Retract _____ KIAS
Extend EGES _____ KIAS QRH

A

Extend 250 KIAS
Retract 200 KIAS
Extend EGES 160 KIAS QRH

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17
Q

Cargo Limititations:
Maximum Freight Loads _____ kg

A

1,134 kg

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18
Q

Maximum Baggage Weight:
Large Net _____ kg
Small Net _____ kg

A

Large Net 240 kg
Small Net 180 kg

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19
Q

Maximum Floor Loading:
Seat Rails _____ kg/m
Floor Panel _____ kg/m (Sq)

A

Seat Rails 500 kg/m
Floor Panel 1000 kg/m (Sq)

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20
Q

Cooling time of the wheels and brakes for Rejected takeoff with brake on speed greater than VR -20 kt and heavy brake usage and 0° flap full stop landing and heavy brake usage?

A

120 minutes

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21
Q

Maximum permissible tire speed

A

165 kt groundspeed

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22
Q

Maximum cabin positive pressure differential

23
Q

Maximum cabin negative pressure differential

24
Q

Generator Limitations:
Quiet Power Mode _____ A
Ground idle and above Flight _____ A Maximum Maximum Voltage _____ V

A

Quiet Power Mode 250 A
Ground idle and above Flight 400 A Maximum Maximum Voltage 29.5 V

25
Minimum battery temperature (Li-Ion): Engine Start _____°C For flight _____°C
Engine Start = -5°C For flight = 0°C
26
Minimum battery volts for start
State Of Charge (SOC) indicators of both batteries are green
27
Permissible fuel temperature range
-40 °C to 80°C
28
Maximum permissible imbalance
330 lb
29
The maximum refueling pressure
60 psi
30
Temperature by which inflation of the deiceer pneumatic boots is not recommended
<-40 °C
31
The WAI is inhibited in these conditions
TAT > 15 °C Aircraft on ground.
32
Do not operate the WAI system with a TAT of more than _____°C
10 °C
33
Do not extend the flaps beyond _____° if in icing conditions
15°
34
The minimum airspeed with flaps retracted in icing conditions
150 KIAS
35
Maximum Takeoff Weight
8,300 kg
36
Maximum Ramp Weight
8,345 kg
37
Maximum Landing Weight
7,665 kg
38
Maximum Zero Fuel Weight
6,450 kg
39
Flight Maneuver Load Factor Limits
Flap Up = +3.0 g, -1.2 g Flap Down = +2.0 g, -0.0 g
40
Sea Level Outside Air Temperature Limitations Range
-54 °C, +50 °C
41
Minimum oxygen quantity for dispatch
680 liters
42
Do not use the oxygen saver function below an altitude of _____ ft
25,000 ft
43
For pressurized flight above 25,000 ft MSL, a minimum oxygen supply of _____ min duration for flight crew and passengers is required.
10 minutes
44
Engine Operating Limitations - ITT (°C)
TO / ATR = 855 °C (5mins), MCT = 835°C
45
Engine Operating Limitations - ATR
Maximum 10 min (with OEI, otherwise 5 min)
46
Engine Start ITT (°C) Limit
1000 °C for 15 seconds then 900 °C
47
Maximum tailwind component for engine start
20 kt
48
Maximum crosswind component for engine start
25 kt tower wind
49
Maximum time to Light-Off for engine start
12 sec
50
NAI must be switched on for all ground operations and for takeoff and landing when any of the following conditions are present:
- Visible moisture - Indicated SAT or reported OAT <10 °C
51
Airbrake is permitted when during an approach, provided that the aircraft is on a stable approach and the airbrake is stowed no later than _____ ft AGL.
50 ft AGL
52
Do not operate the flaps in flight if the aircraft altitude is >_____ ft.
>20,000 ft
53
Landing with Flaps __° or ___° is prohibited unless flaps have failed
0° or 8°
54
Do not use secondary stab trim unless the _____ stab trim has failed
primary stab