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Max Ramp Weight
53,250 lbs
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Max Takeoff Weight
53,000 lbs
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Max Landing Weight
47,000 lbs
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Max Zero Fuel Weight
44,000 lbs
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Minimum Flight Weight
25,480 lbs
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Max Aft Cargo Weight
3,500 lbs
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Flight Time to suitable airport
45 minutes
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Max Ops Altitude
41,000 feet
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Max Takeoff and Landing Distance
10,000 feet
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Max Temperature Takeoff and Landing
ISA +35 degrees C
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Minimum Temperature for Takeoff and Landing
-40 degrees C
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Runway Slope
+/- 2 degrees
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Maximum Tailwind
10 knots
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Vmax ADG Deploy
250 knots
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VWiper Operations Max
220 knots
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Hydraulics Normal PSI
2950 - 3050 (Green)
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Hydraulics Low PSI
<1800 (Amber)
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Hydraulic High PSI
>3200 (White)
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Hydraulic Pressure Relief
>3750 (White)
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Hydraulic Accumulator PSI
1500 PSI
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Normal Hydraulic Level
45-85% (Green)
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Hydraulic High Temp Caution
93-96 Degrees C
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Brake Normal PSI
1000-3200 PSI (Green)
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Brake Anti-Skid
> 35 knots WOW +5 sec
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Anti-Skid INOP below
10 knots
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Slats/Flaps Max Altitude
15,000 feet
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Slats/Flaps Enroute Operations
prohibited
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Min Spoiler Speed
Vref + 17
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Min Altitude Spoilers
300 feet.
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Flight spoilers must not be deployed in flight with flap settings greater than:
30 degrees
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Max Takeoff Thrust
8729 lbs
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ITT Maximum Continuous Thrus
- 3A1: 860 degrees
- 3B1: 874 degrees
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ITT Max. Start
900 degrees
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Oil Temp Minimum Start
-40 Degrees C
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Oil Temp Max Continuous
155 Degrees C (Amber)
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Max. (15 min)
163 Degrees C (Red)
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Oil Min. Start/Idle Pressure
25 PSI (red)
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Min Takeoff Thrust Oil Pressure
25 psi (green)
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Max Continuous Oil Pressure
115 psi (amber)
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Max Continuous N1
98.6% (red)
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Normal Takeoff N1
96.2% (green)
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Minimum Reduced Thrust N1
83.5%
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N2 Idle
56.5 - 68% (green)
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N2 Max Takeoff (APR) op / APR Max. Power
99.4% (red)
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N2 Minimum Reduced Thrust
83.5%
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N2 Normal takeoff
98.3% (green)
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Engine Start (Ground)
- 60 sec on, 10 sec off
- 60 sec on, 10 sec off
- 60 sec on, 5 min off
- 60 sec on, 5 min off
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At Initiation of thrust lever movement from SHUT OFF to IDLE, ITT must be ______ or less for all ground start.
120 degrees
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Dry Motoring (Ground)
- 90 sec on, 5 min off
- 30 sec on, 5 min off
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Fuel Right Main
4,760 lbs
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Fuel Center Tank
4,998 lbs
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Fuel Max. Imbalance
800 lbs
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Fuel Min. for GA per wing tank
450 lbs (amber)
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Fuel Min. Temp for Takeoff
+5 degrees C
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Electric Main Gen:
- to 35,000 ft: 30 KVA
- Above 35,000 ft: 25 KVA
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APU Gen
to 37000 ft: 30 KVA
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Ground Ops DC Only time in use
5 minutes
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Automatic Flight Control System (AFCS) IAS Mode
Prohibited during approach
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Automatic Flight Control System (AFCS) APPR Mode
Prohibited for VOR approaches
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Automatic Flight Control System (AFCS) ADC Source
ADC source coupled to the active autopilot must be the same as taht coupled to the ATC transponder during flight in RVSM airspace
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Nose Steering Tiller max angle
70 Degrees Left/Right
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Nose Steering Rudder max angle
5 Degrees
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APU Max Continuous EGT
743 Degrees C (Red)
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APU Max EGT Start
974 Degrees C
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APU Min Temp Start
-40 Degrees C
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APU Max Ops Altitude
37,000 feet
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APU Max Start Altitude
30,000 feet
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APU Max Altitude Bleed Use
15,000 feet
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APU Max Alt Engine Start
13,000 feet
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APU Max Generator Load
30 KVA
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APU Max Door Open with APU not operating airspeed
300 knots
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APU Start (Aircraft Battery) 2x30 sec On
- 20 min off
- 20 min off
- 40 min off
- 40 min off
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APU Start (Generator) 2x15 sec ON
- 20 min. off
- 20 min. off
- 40 min. off
- 40 min. off
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AC and Pressurization Max Diff.
8.7 PSI
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AC and Pressurization Max Negative Differential
-0.5 PSI
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AC and Pressurization Taxi, Takeoff, and Landing Max.
0.1 PSI
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AC and Pressurization No Manual Operations to:
1,500 feet
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AC and Pressurization Single Pack Operations
25,000 feet
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AC and Pressurization Pack Overheat
88 Degrees C
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AC and Pressurization Pack Overpressure
>53 PSI
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AC and Pressurization Cabin Altitude Caution
>8,500 feet > 10,000 feet
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AC and Pressurization Cabin Altitude Warning
>10,000 feet
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AC and Pressurization CPAM Pax O2
14,000 +/- 500 feet
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AC and Pressurization CPAM NoSmFaSB
10,000 feet
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AC and Pressurization Em Depr
14,250 feet +/- 750 feet
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Engine N2 at ground idle power should not be greater than ___ split.
2%
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If N2 is ___ or less with an OAT of ____ or warmer, do not:
57%, -20 degrees C, do not accelerate above idle.
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Engine Warm Up:
Engine must remainat idle until oil pressure reaches normal operating range
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After all engine starts:
do not exceed 75% N1 for 2 mins. or until operating indications are in normal range.
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Before FFOD, when the aircraft is cold soaked at a temp of -30 degrees C or below for more than 8 hours:
the engine must be motored for 60 seconds and fan rotation verified before engine start is initiated.
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During preflight checks of the thrust reversers after being cold soaked for more than 8 hours:
the thrust reversers must be actuated until the deploy and stow cycles are less than 5 seconds.
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Continuous Ignition must be used during the following:
- Takeoffs and landings on contaminated runways
- Takeoffs with high crosswind components > 10 knots
- Flight through moderate or heavier intensity rain.
- Flight through moderate or heavier intensity turbulence
- Flight in the vicinity of thunderstorms.
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Thrust Reversers are approved for
ground use only
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After the deployment of thrust reversers
do not attempt a go-around maneuver
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During landing, application of maximum reverse thrust is not permitted at airspeeds below:
75 knots.
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Below ____ knots reverse thrust must be to idle (not abouve 30%N1)
60 KIAS
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If both engines are to be started using the APU bleed air, then the operating engines thrust must not exceed:
70% N2
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EICAS display cooling is not available when:
- the battery bus is powered and normal AC power is off
- or
- when the battery bus is powered and APU is in proper service configuration
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Between each APU start:
The APU, PWR FUEL switch/light must be selected off.
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APU at or below 50% rpm max time:
60 seconds
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Takeoff with a fiel load in excess of _____ lbs in the center tank is not permitted unless each main tank is above ______ lbs.
500 lbs, 4,400 lbs
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Takeoff with engine fuel temp indications below ___ degrees C is prohibited.
5 Degrees C
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Powered crossflow and gravity cross flow must be _____ for takeoff.
Off
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Minimum climb speed above 10,000 MSL:
250 knots to .70 M.
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Maximum climb speed above 10,000 MSL:
290 knots to .70 M.
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___ Mach will be the minimum climb speed once the transition to Mach is made from IAS to Mach.
.70
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maximum Authorized Altitude
FL 370
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Reduced thrust takeoffs are prohibited when:
- Cowl and/or wing anti-ice is selected ON
- The takeoff runway is contaminated with standing water, slush, ice or snow.
- tailwind components are in excess of 5 knots
- Warning of windshear or downdrafts have been forecast or reported.
- anti-skid is inop.
- takeoff behind a heavy aircraft
- flaps 8 takeoff
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Takeoff is _______ with frost, ice, snow or slush adhering to any critical surface.
prohibited
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Cowl anti-ice system must be ON when:
- OAT is below 10 degrees C and visible moisture in any form is present
- or
- when it is below 10 degrees C when operating on ramps, taxiways or runways where snow, ice, standing water or slush is present.
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The wing anti-ice system must be on for takeoff when:
- visible moisture is presented below 400 feet agl, or
- runway is wet or contaminated, or
- any precipitation exist.
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Anytime the wing anti-ice is selected ON, the cowl anti-ice:
must also be selected ON.
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The engine cowl anti-ice system must be ON:
- When in icing conditions, or
- when ICE is annunciated by the ice detection system.
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The wing anti-ice system must be ON:
- When ICE is annunciated by the ice detection system, or
- When in icing conditions and the airspeed is less than 230 knots
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