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Max Ramp Weight
36,000 lbs.
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Max Takeoff Weight
35,700 lbs.
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Max Landing Weight
31,800 lbs.
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Max Zero Fuel Weight
24,400 lbs.
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Max Fuel Imbalance (Normal)
400 lbs.
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Max Fuel Imbalance (Emergency)
800 lbs.
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Tailcone Baggage Compartment
700 lbs.
-
-
Vmo (below 8000 ft.)
270 KIAS
-
Vmo ( 8000 ft. to 30,650 ft.)
350 KIAS
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Mmo (above 30,650 ft.)
.92 Mach (indicated)
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Mmo (Mach Trim Inop)
.82 Mach (indicated)
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Turbulent Air Penetration Speed
300 KIAS/ .90 Mach
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Max Tire Groundspeed
182 KIAS
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Max Slat Extended Speed
250 KIAS
-
-
-
-
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Max Speed Brake Extended Speed
No Limit
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Min. Speed Brake Extended Speed
Vref + 15 KIAS
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Min. Speed in Icing
200 KIAS
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Max Operating Altitude
FL510
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Max TakeOff / Landing Altitude
14,000 ft.
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Max Altitude for Gear / Flap Extension
FL180
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Max Temp. Takeoff & Landing
ISA + 39* C
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Min. Temp. Takeoff & Landing
-54* C
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Max Tailwind Component
10 kts.
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Crosswind Component
21 kts. (demonstrated)
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Manual Reversion
10 kts. crosswind
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Slat Asymmetry
10 kts. crosswind
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Main Generator Limits (up to FL410)
400 amps
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Main Generator Limits (above FL410)
300 amps
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APU Generator Limits (ground)
300 amps
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APU Generator Limits (flight)
200 amps
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Cold Soaked Battery Temp
-20* C
Battery should be removed and placed in a warm environment for aircraft parked at these temps.
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Engine Type
Allison AE 3007C Turbofan
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Min. Start Duct Pressure
25 psi (30 psi recommended)
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Starter Limit
3 consecutive normal starts followed by 25 minutes of cooling
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Approved Oil
Mobil Jet II
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Min. Oil Temp. for Start
-40* C
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Max Reverse Thrust
70% N1
-
-
Min. Fuel Temp for Start
-37* C
-
Max Fuel Temperature
+98.9* C
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Center wing transfer must be initiated prior to.....
.....3100 lbs. per side wing fuel
-
Simultaneous use of crossfeed and center-to-wing tank transfer is prohibited when wing fuel quantity is....
....2900 lbs. or less per side. Fuel lateral imbalance will result.
-
Approved Hydraulic Fluid
Skydrol (Purple)
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APU not approved for....
....unattended ground operation
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Max altitude for APU start
31,000 ft.
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Max Altitude for APU operation
31,000 ft.
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Max Starter Duty Cycles (APU)
Maximun of 6 consecutive successful starts at 10 minute intervals
-
APU compartment inspection is required after.....
.....an automatic APU shutdown
-
Crew O2 masks are not approved for sustained operation at a cabin altitude greater than....
....40,000 ft.
-
Pax O2 masks are not approved for sustained operation at a cabin altitude greater than....
25,000 ft.
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Nose Tire Inflation
130 +/- 5 psig, unloaded.
Unloaded weight is while the a/c is on jacks. Loaded weight will be 2 - 5 psig higher.
-
Minimum Single Engine Enroute Climb Speed
190 KIAS
-
Min. Altitude for In-Flight use of Speed Brakes
500' AGL
-
Min. Wing Fuel per Tank for Takeoff
500 lbs.
-
Takeoff in High Idle is.....
Prohibited (except for touch and go)
-
Auto Pilot Minimum Use Height :
Cruise:
Precision: Cat I
Non Precision:
1000' AGL
170' AGL
400' AGL
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Auto Pilot coupled operation with single operational or displayed AHRS or IRS is.....
Prohibited
-
Auto pilot coupled ILS approached with flaps up are....
Prohibited
-
Normal Cabin Pressure Limitation
9.7 psi Maximum Differential
-
-
-
-
Horizontal Stabalizer
26.09'
-
-
-
Wing Sweep
Horizontal Stabilizer Sweep
40 *
43 *
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Each engine produces _________ pounds of thrust at sea level?
6442 lbs.
-
-
Bleed Air extracted from the ____ and ____ stage of the compressor section.
8th and the 14th
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Fuel Capacity
13,000 lbs.
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Wing Fuel Tank Capacity
3500 lbs.
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Center Tank Capacity
6000 lbs.
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Fuel Burn is approx. ______for the first hour, and then approx. ______ for each hour there after.
2500 lbs/hr
1800 - 2000 lbs/hr
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