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62 Cards in this Set

  • Front
  • Back

APU on the ground only for?

- A proposed departure


- Updating FMS databases


- Cleaning and securing of the aircraft following a trip


- AR for maintenance

Normal APU airspeed limits

No more than 250 knots

Emergency APU ops limits

Fl300 and below


285 knots

APU during ground ops

- If time between arrival and departure does not exceed 1Hr 30 min APU remains on




- if time between arrival and departure does exceed 1HR 30min APU shutdown




- After last flight of the day if no longer needed for securing and cleaning ops

CL300 max ramp weight

39,000lbs

CL300 max t/o weight

38,850 lbs

CL300 max zero fuel weight

27,200 lbs

Cl300 max landing weight

33,750 lbs

CL300 min flight weight

23,100 lbs

Cl350 max ramp weight

40,750 lbs

CL350 max t/o weight

40,600 lbs

cl350 max zero fuel weight

28,200 lbs



CL 350 max landing weight

34,150 lbs

Cl 350 min flight weight

24,800 lbs



Max operating speed (VMO) below 8000

300 kts

max operating speed (VMO) 8001-29,475

320 kts

MM0 above 29,475

.83M

Rough Air penetration speed VRA

265 kts / .75 M

VLo retraction

200 kts

Vlo extension

250 kts



Vle

250 kts

Vfe 10 and 20 degrees

210 kts

Vfe flaps 30 degrees

175 kts

maximum tire speed

182 kts

Max takeoff and landing altitude

10,000 ft

Max tailwind

10 kts

max runway slope

+/- 2 percent

max tailwind on contaminated runway

5 kts

max tailwind Level 2 and 3 airports

0 kts

Maneuvering load factors flaps up

+2.6 to -1 G

Maneuvering Load factors flaps down

2 to 0g

Max xwind t/o

28kts

max xwing landing

24 kts

max pressure altitude CL300 and Cl350

45,000 ft

ops with glide path greater than______ is prohibited and category 2 apps are prohibited

4.5 degrees or greater

Dimen CL300

wingspan 63 ft 10 in


length 68ft 8 in


height 20ft


wingtip clearance 95ft 5in

Dimen Cl350

wingspan 69ft


length 68ft 8 in


height 20ft


wingtip clearance 101ft



max diff psi on ground

no more than .1 psi

Max diff psi during landing

no more than 1 psi



max diff psi aircraft S/N 20001-20886

positive 9.4psi


negative .5 psi


7800ft cabin altitude at FL450

Max Diff psi aircraft S/N 20887-to present

positive 10.1psi


negative .5 psi


5800 ft cabin altitude at FL450

crew and passenger oxygen masks are not approved for use above _______

40,000ft cabin altitude

prolonged use of passenger masks above ______is not recommended

25,000 ft cabin altitude

Auto pilot minimum engage height: climb, enroute, or descent

700 ft AGL

Auto pilot during precision approach used for a?

Min descent angle of 3.5 degrees or less to 80ft

Auto Pilot during precision approach used for a

min descent angle of 3.5 and 4.5 degrees to 160ft

Auto pilot disconnect for visual and non precision apps

200 ft

Max alt with yaw dampener off

31,000ft

Holding in icing conditions with flaps extended is ______

prohibited

Ground Anti ice operations when?

visible moisture in any form, fog with visibility of 1 mile or less, rain, snow, sleet or ice crystals

Engine anti-ice ON when?

-OAT on ground or for T/O is 10 degrees C or below.


-OAT is 10 degrees C or less on ramps taxiways or runways where snow, ice, standing water, or slush is present

Wing anti-ice systems ON when?

Takeoff when OAT is 5 degrees C or below

Flight Anti Ice ON when

-(TAT CL350) 10 degrees C or below


(SAT CL300) 10 degrees C or below and visible moisture in and form except when SAT is -40degrees or below.

operation with type 2, 3, or 4 A/I fluids

wing anti ice must only be selected on just prior to thrust increase for takeoff

Navigation equipment required to be operative for FMS use (with SB350) and without (SB350)

Two GNSS or,


Two DMEs or,


One VOR/DME or,


One IRS

FMS range and Fuel management is____

Advisory only

RNP Ops to LPV mins is prohibited unless what equipment is working?

Dual PFD


Dual GNSS with SBAS


Dual FMC

Required equipment for RVSM

Operational Auto Pilot


Operational Altitude alerting System


One operating Altitude reporting transponder


Two ADCs



Do not extend flaps above?

18,000 ft

Flight spoilers must not be extended in flight below

500 ft AGL and at airspeeds below approach speed

two or three generator load ?

Max 400 amps

Engine type CL300

HTF7000