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Challenger 300 Limitations > Rob Forst > Flashcards

Flashcards in Rob Forst Deck (33)
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1
Q

Vmo (up to 8000 ft)

A

300 KIAS

2
Q

Vmo (8001 ft to 29,475 ft)

A

320 KIAS

3
Q

Mmo (above 29,475 ft)

A

.83 Mach Indicated

4
Q

Vra (rough air penetration speed)

A

265 KIAS/.75 MI

5
Q

Vlo (retract)

A

200 KIAS

6
Q

Vlo (extend)

A

250 KIAS

7
Q

Vle (extended)

A

250 KIAS

8
Q

Vfe (flaps 10)

A

210 KIAS

9
Q

Vfe (flaps 20)

A

210 KIAS

10
Q

Vfe (flaps 30)

A

175 KIAS

11
Q

Maximum tire speed (ground speed)

A

182 Kts

12
Q

Minimum operating speed

A

Intentional speed reduction below the onset of the stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for flight test or training ops.

13
Q

Maximum takeoff and landing pressure altitude

A

10,000 ft

14
Q

Maximum tailwind component

A

10 kts

15
Q

Takeoff and landing are limited to _________ runways

A

paved

16
Q

The maximum runway slopes approved for takeoff and landing are ___ % uphill and ___ % downhill

A

+2, -2%

17
Q

The maximum crosswind component for takeoff is ___ knots

A

28

18
Q

The maximum crosswind component for landing is ___ knots

A

24

19
Q

The maximum crosswind component for takeoff and landing on contaminated runway is ___ knots

A

10

20
Q

Operations on runways with a coefficient of less than __ is prohibited

A

0.3

21
Q

Maximum pressure altitude (enroute)

A

45,000 feet

22
Q

Takeoff (is/is not) permitted with frost adhering to the underside of the wing that is caused by cold soaked fuel

A

is (refer to FCM, Supplement 1 - Cold WX Ops)

23
Q

Maneuvering load factor, flaps up (+, - g)

A

+2.6 g to -1.0 g

24
Q

Maneuvering load factor, flaps extended (+, - g)

A

+2.0 g to 0.0 g

25
Q

If type III, III & IV anti-icing fluids have been applied

A

The wing anti-ice system must only be selected on, if required, just prior to thrust increase for takeoff

26
Q

Maximum operating temerature

A

50 deg C

27
Q

Minimum operating temperature

A

-45 deg C airframe limit, (see fuel temp limit)

28
Q

APU - maximum altitude for operation

A

37,000 feet

29
Q

APU - maximum altitude for generator operation

A

30,000 feet

30
Q

APU - maximum altitude for APU bleed air for engine start operation

A

20,000 feet

31
Q

APU - maximum altitide for ECS bleed air

A

20,000 feet for aircraft with SB 100-21-05 compliance

32
Q

APU - do not use the APU to start the ___ engine above ___ feet

A

left, 9000 feet

33
Q

APU - do not start the APU above ___ knots

A

300