CL-30 Limitations Flashcards
Cabin Differential Pressure Limits
Air………………………… -.5 to 9.4 psi
Landing………………… -.5 to 1.0 psi
Taxi………………………… -.5 to .1 psi
Generator Load Limits
2 or 3 generators operating………………….400 amps
1 generator operating (on ground)…………400 amps
1 generator (in flight)…………………………….500 amps
Transient limit (5 minutes)………………………600 amps
V mo
M mo
Up to 8000 ft ………………………. 300 kts
8000 ft to 29475 ft ………………..320 kts
Above 29475 ft ……………………… .83m
V mcg
111 kts
Maneuvering Load Factors
Flaps up …………………… 2.6g to -1.0g
Flaps down …………………. 2.0g to -0g
APU Maximum Altitudes
- Operation
- Generator
- Bleed Air
Operation …………………….. 37,000 ft
Generator …………………….. 30,000 ft
Bleed Air ………………………. 20,000 ft
APU Starter Cooling Times
Start Attempts Cooling Time
1 ............................................... 1 min 2 ............................................... 1 min 3 ............................................. 20 min 4 ............................................... 1 min 5 ............................................. 40 min
V’LE
V’LO
- Retraction - Extension
V’LE …………………………. 250 kts
V’LO Ret…………………… 200 kts
Ext……………………. 250 kts
V’RA
V’FE
V’RA …………………………. 265 kts or .75 m
V’FE
Flaps 10 or 20 …………………… 210 kts
Flaps 30 …………………………… 175 kts
Spoilers
Do not extend spoilers below:
Approach + 8 kts
500 ft AGL
Do not select flight spoilers to EMER except during an
emergency or as required by procedure.
Maximum useable fuel
- Single Point - Over Wing
Per Tank Total
Single Point ………………. 7075 lbs 14,150 lbs
Over Wing ………………… 6500 lbs 13,000 lbs
Approved Fuels
Jet A Jet A1 Jet B JP 4 JP 5 JP 8
Maximum depth of Water or Slush
Takeoff / Landing
Takeoff ………………….. .25”
Landing ………………… .5”
Autopilot Minimum Use Height
Climb, Enroute, Descent ……………………………. 700 ft AGL
Visual and Non Precision Approaches ………… 200 ft AGL
Precision Approaches (GS 3.5d or less) ............. 80 ft AGL
(GS 3.6d - 4.4d) ............ 160 ft AGL
Required Equipment for RVSM
Autopilot
Altitude Alerting System
Altitude Encoding Transponder
2 Air Data Computers
Maximum Ramp Weight
39,000 lbs
Maximum Landing Weight
33,750 lbs
Thrust Reversers
- Use only on paved surfaces
- Do not use in flight
- Do not use to backup aircraft
- Do not use on touch & go’s
- Reverse thrust above idle is prohibited below 40 kts
Runways
- Paved runways only
- Maximum slope +/- 2%
- 4000 ft long (company limitation)
- 70 ft wide (company limitation)
Maximum Gear Extension Altitude
18,000 ft
V’1mcg
116 kts
Auto flight
- Do not intentionally overpower the autopilot
- Maximum altitude with the yaw damper off is 31,000 ft
Maximum depth of wet snow
Takeoff / Landing
Takeoff ………………… .5”
Landing ……………….. 1”
V’mca
Flaps 10 …………….106 kts
Flaps 20 …………… 102 kts
Maximum Takeoff Weight
38,850 lbs
Maximum Fuel Imbalance
Fuel onboard Max imbalance
< 4700 lbs ………………………………. 600 lbs
4700 lbs - 10,000 lbs ………………. 450 lbs
10,000 lbs - 13,700 lbs ……………. 315 lbs
> 13,700 lbs …………………………….. 250 lbs
V’MCL
Flaps 10 ………… 108 kts
Flaps 20 ………… 106 kts
Flaps 30 ………… 102 kts
Maximum depth of dry snow
Takeoff / Landing
Takeoff ………………. 2”
Landing ……………… 3”
Maximum Zero Fuel Weight
27,200 lbs
Jet A temperature limits
-30c thru 50c
For temps > or = 45c
- Minimum fuel for takeoff is 2800 lbs
- < 2000 lbs of fuel (1000 lbs per side), do not
operate engines for more than 30 minutes
Minimum fuel for a “Go Around”
500 lbs per side
Maximum Takeoff / Landing Pressure Altitude
10,000 ft
Maximum Tailwind Component
10 kts
Maximum Tire Speed
182 kts
Maximum altitude for flap deployment
18,000 ft
Maximum operating altitude
45,000 ft
Minimum Flight Weight
23,100 lbs
Minimum battery temperature for takeoff
-20c
Air Source Selector
Do not select the Air Source switch to “TRIM AIR ONLY” while aircraft is on the ground.
Engine Starts
- 3 consecutive starts followed by 15 minutes of cooling
- Engine must be motored for 30 seconds after aborted start
Crew and passenger oxygen masks
- Not approved for use above 40,000 ft cabin altitude.
- Prolonged use of passenger masks above 25,000 ft cabin altitude not recommended.
Wing Anti Ice (ground)
On for takeoff when temperature is 5c or below and visible moisture is present, or when surface snow, ice, water or slush is present.
Standby Instrument / Standby Compass
- Standby instrument can not be used for localizer back course approaches
- Left and right windshield heat must be selected OFF while the standby compass is being read
Wing Anti Ice (flight)
Selected ON when temperature is 10c thru -40c and visible moisture is present.
Selected ON if “ICE DETECTED” CAS illuminates
For N530FX and newer; airspeed below 210 kts
APU Anti ice / De-ice procedures
Do not operate APU during de-icing
Wing Anti Ice with Type II and Type IV Anti Ice fluids
If required the wing anti ice must be selected “ON” just prior to throttle advance for takeoff.
Engine Anti Ice (flight)
Selected “ON” when temperature is 10c thru -40c and visible moisture is present.
Selected “ON” when “ICE DETECTED” CAS illuminates.
Engine Anti Ice (ground)
Selected “ON” when temperature is 10c or below and visible moisture is present, or when surface snow, ice, water or slush is present
Minimum bulk fuel temperature for takeoff.
-30c
Maximum bulk fuel temperature for takeoff.
50c
Maximum altitude when using Jet B or JP 4 fuels.
16,000 ft
Maximum speed and altitude APU can be started.
30,000 ft and 285 kts
Maximum demonstrated crosswind.
Takeoff / Landing
Takeoff ………………….. 28 kts
Landing …………………. 24 kts
Wingspan
63’ 10”
Aircraft length
68’ 8”
Aircraft height
20 ft
Minimum pavement width for 180 degree turn
58 ft
Engine type
HTF-7000
Maximum altitude for Left engine start on ground
9000 ft
Maximum altitude for APU start on ground
14,000 ft
Maximum single point refueling / de-fueling pressure
Refueling …………………. 55 psi
De-fueling ……………….. -8 psi
