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Challenger 605 > Limitations > Flashcards

Limitations Flashcards

1
Q

CL605 is approved for what operations?

A
  • Day and Night
  • VFR and IFR
  • Flight in icing conditions
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2
Q

Is the Challenger 605 approved for ditching?

A

Yes so long as the appropriate safety equipment is installed.

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3
Q

Max ramp/taxi weight

A

48,300lbs

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4
Q

Max take-off weight

A

48,200lbs

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5
Q

Max landing weight

A

38,000lbs

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6
Q

Max airport pressure altitude for take-off and landing

A

10,000 ft

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7
Q

Max operating altitude

A

41,000 ft

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8
Q

Max temp for take-off and landing

A

ISA+35C

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9
Q

Min temp for take-off

A

-40C

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10
Q

Above ________ft a safety harness must be worn by one pilot

A

25,000ft

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11
Q

In cold weather ops when is take-off prohibited

A

with frost, ice, snow or slush adhering to any critical surface (wings, horizontal stabilizer, vertical stabilizer, control surfaces, engine inlets and upper surface of the fuselage).

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12
Q

Icing conditions exist when

A
  • TAT of 10C or below and
  • Visible moisture is present or
  • Visibility is less than 1 mile
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13
Q

Engine cowl anti-ice system must be on

A
  • when ice is indicated by ice detection system
  • when in icing conditions, if an ice detector has failed

*If below 22,000ft ice detector fail does not require use

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14
Q

Wing anti-ice must be on for take-off when

A

OAT is 5C or below and

  • visible moisture or
  • runway surface contamination
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15
Q

Max/min runway slopes

A

+/- 2 degrees

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16
Q

Max tailwind component

A

10kts

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17
Q

Max crosswind component for take-off and landing

A

24kts

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18
Q

Max crosswind component for take-off and landing on a contaminated surface

A

10kts

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19
Q

Min Go-Around altitude

A

Two Engines-50ft

One Engine-100ft

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20
Q

Ground ops with winds in excess of ______ mph require inspection and functional check of the aileron, elevator, and rudder PCUs.

A

60mph

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21
Q

Maximum N1?

A

98.6% rpm

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22
Q

Maximum ITT with APR not operating

A
  • 900c for 2min

- 884c for next 3min

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23
Q

Maximum ITT with APR operating

A
  • 928c for 2min

- 900c for next 3min

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24
Q

Max continual thrust ITT

A

900c

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25
Q

Max N2% RPM

A

99.3%

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26
Q

Max oil temp

A

163c

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27
Q

Oil press normal range

A

26 to 115 psi

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28
Q

When must continuous ignition be used?

A
  • Take-offs and landings on contaminated runways
  • Take-offs with high crosswind components
  • Flight through moderate or heavier intensity rain
  • Flight through moderate or heavier intensity turbulence
  • Flight in the vicinity of thunderstorsm
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29
Q

When is the ATS system not permited

A
  • single engine
  • cat II approaches
  • any indication of stall
  • with APR selected on FMS performance page
  • during go-around
  • if flaps are selected to less than 45 for landing must be disconnected prior to 100ft AGL
30
Q

Starter cranking limits

A

-Three consecutive engine start cycles with 5 minutes cooling between additional cycles

  • ITT must be 120c or less for all ground starts
  • ITT must be 90c or less for all air starts
31
Q

Dry Motoring limits

A

First start- 90sec ON/5 min OFF

Subsequent- 30sec ON/5 min OFF

32
Q

Max altitude for engine relight?

A

21,000ft

33
Q

Airspeed for windmilling engine relight?

A

8,000 to 21,000ft=300kts-348kts

sea level to 8,000ft=300kts

34
Q

Airspeed for starter-assisted cross bleed?

A

15,000-21,000ft=200kts-300kts

sea level to 15,000fts=140kts-300kts

35
Q

Max fuel imbalance between main tanks for takeoff, taxi, and landing?

A

400lbs

36
Q

Max fuel imbalance between main tanks during flight?

A

800lbs

37
Q

Max usable fuel in main tanks

A

4,860lbs each

38
Q

Max usable fuel in AUX tank

A

7,168lbs

39
Q

Max usable fuel in TAIL tank

A

3,112lbs

40
Q

APU max RPM

A

110%

41
Q

APU max EGT

A

731c

42
Q

Min temp for APU start

A

-40c

43
Q

APU starting cycles

A

Starting with aircraft batteries:

  • 3 start attempts of 30 seconds cont cranking
  • 20 minute off time
  • 2 further attempts of 30 seconds cont cranking

Starting with ground power:

  • 2 start attempts of 15 seconds cont cranking
  • 20 minute off time
  • 2 further attempts of 15 seconds cont cranking

If either method is unsuccessful a further start must ot be attempted for a period of at least 35 minutes

44
Q

APU max EGT during start

A

974c

45
Q

Max altitude for APU start

A

20,000ft

46
Q

APU restriction for in-flight engine restart

A

Only permissible with dual engine failure

47
Q

Max altitude for APU bleed air

A

15,000ft

48
Q

Max APU generator load

A

30kVA

49
Q

Max airspeed/Mmo

A

348kts/.85 mach

50
Q

Max flap extension speeds

A

20deg - 231kts
30deg - 197kts
45deg - 189kts

51
Q

Max gear extension and retraction speed

A

197kts

52
Q

Max gear extended speed

A

250kts

53
Q

Max flap altitude

A

15,500ft

54
Q

Max altitude for gear extension

A

20,000ft

55
Q

Max tire speed

A

182kts

56
Q

Turbulent air penetration speed

A

280kts

57
Q

Flaps 0 min maneuvering speed

A

170kts

58
Q

Flaps 20 min maneuvering speed

A

160kts

59
Q

Flaps 30 min maneuvering speed

A

150kts

60
Q

Flaps 45 min maneuvering speed

A

145kts

61
Q

Min fuel required for go-around

A

1,000lbs

62
Q

Min engine fuel temp

A

6c

63
Q

Max fuel imbalance when overwinging

A

2,500lbs

64
Q

What is the N2 yellow arc with anti-ice on?

A

0-77.9%

65
Q

Max cabin pressure differential while flying

A

9.0psi

66
Q

Max structural diff pressurization

A

9.2psi

67
Q

Leading edge temp limit during de-ice operations

A

31c

68
Q

Max speed/mmo when hand flying

A

250kts or Mach .70

69
Q

Flaps min maneuvering speed

A

0 - 170kts
20 - 160kts
30 - 150kts
45 - 145kts

70
Q

Tiller max turning angle

A

55 degrees

71
Q

Rudder turning angle

A

7 degrees

Challenger 605 (9 decks)

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