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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 |
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Normal APU airspeed limits |
No more than 250 knots |
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Emergency APU ops limits |
Fl300 and below 285 knots |
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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 |
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CL300 max zero fuel weight |
27,200 lbs |
|
Cl300 max landing weight |
33,750 lbs |
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CL300 min flight weight |
23,100 lbs |
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Cl350 max ramp weight |
40,750 lbs |
|
CL350 max t/o weight |
40,600 lbs |
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cl350 max zero fuel weight |
28,200 lbs |
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CL 350 max landing weight |
34,150 lbs |
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Cl 350 min flight weight |
24,800 lbs |
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Max operating speed (VMO) below 8000 |
300 kts |
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max operating speed (VMO) 8001-29,475 |
320 kts |
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MM0 above 29,475 |
.83M |
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Rough Air penetration speed VRA |
265 kts / .75 M |
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VLo retraction |
200 kts |
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Vlo extension |
250 kts |
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Vle |
250 kts |
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Vfe 10 and 20 degrees |
210 kts |
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Vfe flaps 30 degrees |
175 kts |
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maximum tire speed |
182 kts |
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Max takeoff and landing altitude |
10,000 ft |
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Max tailwind |
10 kts |
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max runway slope |
+/- 2 percent |
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max tailwind on contaminated runway |
5 kts |
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max tailwind Level 2 and 3 airports |
0 kts |
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Maneuvering load factors flaps up |
+2.6 to -1 G |
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Maneuvering Load factors flaps down |
2 to 0g |
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Max xwind t/o |
28kts |
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max xwing landing |
24 kts |
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max pressure altitude CL300 and Cl350 |
45,000 ft |
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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 |
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Dimen Cl350 |
wingspan 69ft length 68ft 8 in height 20ft wingtip clearance 101ft |
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max diff psi on ground |
no more than .1 psi |
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Max diff psi during landing |
no more than 1 psi |
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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 |
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prolonged use of passenger masks above ______is not recommended |
25,000 ft cabin altitude |
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Auto pilot minimum engage height: climb, enroute, or descent |
700 ft AGL |
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Auto pilot during precision approach used for a? |
Min descent angle of 3.5 degrees or less to 80ft |
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Auto Pilot during precision approach used for a |
min descent angle of 3.5 and 4.5 degrees to 160ft |
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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 |
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Ground Anti ice operations when? |
visible moisture in any form, fog with visibility of 1 mile or less, rain, snow, sleet or ice crystals |
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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 |
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Wing anti-ice systems ON when? |
Takeoff when OAT is 5 degrees C or below |
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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 |
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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 |
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RNP Ops to LPV mins is prohibited unless what equipment is working? |
Dual PFD Dual GNSS with SBAS Dual FMC |
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Required equipment for RVSM |
Operational Auto Pilot Operational Altitude alerting System One operating Altitude reporting transponder Two ADCs |
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Do not extend flaps above? |
18,000 ft |
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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 |