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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
Max N2% RPM
99.3%
26
Max oil temp
163c
27
Oil press normal range
26 to 115 psi
28
When must continuous ignition be used?
- 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
29
When is the ATS system not permited
- 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
Starter cranking limits
-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
Dry Motoring limits
First start- 90sec ON/5 min OFF | Subsequent- 30sec ON/5 min OFF
32
Max altitude for engine relight?
21,000ft
33
Airspeed for windmilling engine relight?
8,000 to 21,000ft=300kts-348kts sea level to 8,000ft=300kts
34
Airspeed for starter-assisted cross bleed?
15,000-21,000ft=200kts-300kts sea level to 15,000fts=140kts-300kts
35
Max fuel imbalance between main tanks for takeoff, taxi, and landing?
400lbs
36
Max fuel imbalance between main tanks during flight?
800lbs
37
Max usable fuel in main tanks
4,860lbs each
38
Max usable fuel in AUX tank
7,168lbs
39
Max usable fuel in TAIL tank
3,112lbs
40
APU max RPM
110%
41
APU max EGT
731c
42
Min temp for APU start
-40c
43
APU starting cycles
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
APU max EGT during start
974c
45
Max altitude for APU start
20,000ft
46
APU restriction for in-flight engine restart
Only permissible with dual engine failure
47
Max altitude for APU bleed air
15,000ft
48
Max APU generator load
30kVA
49
Max airspeed/Mmo
348kts/.85 mach
50
Max flap extension speeds
20deg - 231kts 30deg - 197kts 45deg - 189kts
51
Max gear extension and retraction speed
197kts
52
Max gear extended speed
250kts
53
Max flap altitude
15,500ft
54
Max altitude for gear extension
20,000ft
55
Max tire speed
182kts
56
Turbulent air penetration speed
280kts
57
Flaps 0 min maneuvering speed
170kts
58
Flaps 20 min maneuvering speed
160kts
59
Flaps 30 min maneuvering speed
150kts
60
Flaps 45 min maneuvering speed
145kts
61
Min fuel required for go-around
1,000lbs
62
Min engine fuel temp
6c
63
Max fuel imbalance when overwinging
2,500lbs
64
What is the N2 yellow arc with anti-ice on?
0-77.9%
65
Max cabin pressure differential while flying
9.0psi
66
Max structural diff pressurization
9.2psi
67
Leading edge temp limit during de-ice operations
31c
68
Max speed/mmo when hand flying
250kts or Mach .70
69
Flaps min maneuvering speed
0 - 170kts 20 - 160kts 30 - 150kts 45 - 145kts
70
Tiller max turning angle
55 degrees
71
Rudder turning angle
7 degrees

Challenger 605 (9 decks)

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