Max Taxi and Ramp Weight
39,000 lb
Max Takeoff Weight
38,850 lb
Max Landing Weight
33,750 lb
(5,100 lb less than Max Takeoff)
How much fuel must you burn before landing if you took off at Max Takeoff Weight?
5,100 lb
Max Zero Fuel Weight
27,200 lb
Maxumum Usable Fuel (lb) - Pressure Refuel
14,150 lb Total
(7,075 lb / Side)
Maxumum Usable Fuel (lb) - Gravity Refuel
13,000 lb Total
(6,500 lb / Side)
Maximum Fuel imbalance
Varies from 250 - 600 lb
250 lbs with Total fuel more than 13,700 lbs
600 lbs with Total fuel less than 4,700 lbs
Minumum Fuel for Go-Around
500 lb per side
Maximum Bulk Fuel Temp for TakeOff
50 C
Minimum Bulk Fuel Temps for Takeoff
-30 (Jet A)
- 35 (Jet 1)
- 40 (Jet B)
Fuel X-Flow Position For TakeOff
Power and Gravity X-Flow Must be OFF
Maximum Operating Altitude
45,000 ft
Maximum Takeoff and Landing Altitude
10,000 ft
Minimum Altitude for Autopilot Useage
(Climb, Enroute or Descent)
700 ft AGL
Minimum Altitude for Autopilot Useage
(Visual or Non Precision)
200 ft AGL
Minimum Altitude for Autopilot Useage
(Precision Approach with Glidepath of 3.5 or less)
80 ft AGL
Minimum Altitude for Autopilot Useage
(Precision Approach with Glidepath 4.5 or less)
160 ft AGL
Maximum Altitude with Yaw Damper OFF
31,000 ft
Maximum Gear Extension Altitude
18,000 ft
Maximum Flaps Extension Altitude
18,000 ft
Minimum Altitude for Spoilers
500 ft AGL
Maximum Altitude With the APU Running
37,000 ft
Maximum Altitude with APU GEN
30,000 ft
Maximum Altitude with ECS Bleed
20,000 ft
Maximum Altitude for Engine (APU) Start
20,000 ft
Maximum Altitude for Crew/PAX O2 Masks
40,000 ft
Maximum Tailwind Component
10 knots
Maximum Demonstrated Crosswind (Takeoff)
28 knots for Takeoff
Maximum Demonstrated Crosswind (Landing)
24 knots for landing
Maximum Demonstrated Crosswind (NWS Inop)
15 knots
Maximum Demonstrated Crosswind (On AHRS Channel Inop)
15 kntos
Vmo (Up to 8,000 ft)
300 KIAS
Vmo (8,001 - 29,475 ft)
320 KIAS
Mmo (Above 29,475 ft)
0.83 Mach
Vra (Rough Air Penetration Speed)
265 KIAS / 0.75 Mach
VLO ret
200 KIAS
VLO ext
250 KIAS
VLE (Operations with the Gear Extended)
250 KIAS
VFE (10/20)
210 KIAS
VFE (30)
175 KIAS
Tire Speed Limit
182 KIAS
Minimum Spoiler Speed
VAPP + 8 KIAS
Thrust Reverse IDLE Only
Below 40 KIAS
Use of Engine Anti-Ice In Flight
SAT (Static Air Temperature) is 10 to -40 C with visible moisture, or when ICE DETECTED CAS message is displayed.
Minimum Temp for Takeoff
-40 C
Minimum Oil Temperature for Starting
-40 C
After three start attempts, how long must the starter be allowed to cool?
15 min cooling period
How long should an starter be allowed to cool after a 5 minutes (cranking) attempt?
15 min
How long must an engine be motored after an aborted start?
30 sec
Minimum Oil Pressure At IDLE
28 psi
Minimum Idle N2
46.0%
Max Ground Start ITT
650 C
Maximum ITT to Begin a Start
350 C
Maximum Generator Electrical Load (2 or 3 Gens Operating)
400 amps
Maximum Generator Electrical Load (1 Gen on the ground)
400 amps
Maximum Generator Electrical Load (1 Gen in Flight)
500 amps
Maximum Generator Electrical Load (Transient 5 min)
600 amps
Maximum APU RPM
108%
Maximum APU EGT (Start)
973 C
Maximum APU EGT (Normal)
718 C
How many start attempts do you get to start the APU?
3, followed by a 1 minute cooling period.
How much of a cooling period do you need after each of your 3 APU start attempts?
1 min
How long of a cooling period do you need after the 3rd APU start attempt?
20 min
How long should you wait to make another APU start, after a successful start.
10 min
How many successful start attemps can you make with 10 minute cooling intervals before you need to wait an hour?
6 attempts
How long do you need to wait after 6 successful starting attempts?
1 hour
Can you use the APU during de/anti-ice operations?
No - Use is Prohibited.
Is TakeOff with a APU SHUTDOWN CAS Message allowed?
No - Takeoff without inspection is prohibited.
Five Limitations for use of Thrust Reverse
- Use on paved surfaces only. 2. Do not deploy in flight. 3. Do not back up the airplane. 4. No use for touch and go landings. 5. Below 40 KIAS - IDLE Only.
TRIM AIR ONLY
Prohibited on ground.
Max Pressurization Differential On Ground
0.1 psi
Max Pressurization Differential - Landing
1.0 psi
Max Pressurization Differential (Positive)
9.4 psi
Max Pressurization Differential (Negative)
-0.5 psi
Minimum flight weight?
23,100 lbs
To be used for navigation, the FMS must be recieving:
- One VOR/DME or 2. Two DMEs or 3. GPS (RAIM must be available)
Minimum battery temp for takeoff?
-20 C
Use of Takeoff Power (time)?
5 min
Use of APR power (auto)?
10 min
Use of APR power (manual)?
5 min
When should you remove the battery?
When the temp is expected to be less than -30 C for more than 10 hours.
What is the limitation for use of battery or GPU on the ground?
If temp is above 40 C, no more than 30 min.
Minimum Oil temp for above Idle?
5 C
Minimum Oil temp for Takeoff?
15 C
Maximum pressure for pressure refueling?
55 psi
Maximum pressure for pressure defueling?
-8.0 psi
Types of operation
Day, Night, VMC, IMC Icing
What equippment is required for RVSM?
Autopilot Altitude Alerting System One Altitude Reporting Transponder Two Air Data Computers
Restriction on Holding in Ice
No Flaps
Side window building ice
Assume flight in super cooled large droplets. Wing and Engine anti-ice ON Leave icing conditions as soon as possible.
Engine Anti-Ice System On For Takeoff (Ground)
OAT 10 C or colder with visible moister (such as fog with vis. of 1 mile or less).
Engine Anti-Ice System On For Taxi (Ground)
OAT 10 C or colder with surface contaminants