Limitations Flashcards
Max Ramp Weight
115,100
Max Takeoff Weight ***
114,850
Max Landing Weight ***
87,600
Max Zero Fuel Weight
67,500
Minimum Flight Weight
60,000
45 minute IFR Reserve Fuel
2500 lb
Hot Spare fuel
8500 lb
Emergency fuel
1500 lb Wings
or 750 lb per wing
Parking Inclement weather fuel
20000 lb
Runway Requirements
4500 ft long
98 ft or 30 m wide
Max slope 2%
Opp review required
Dry less than 5000 ft
Wet/Contaminated less than 5800 ft
Max Crosswind ***
27
Contaminated/Runway
Fair/Medium 20
Poor. 10
Max Tailwind ***
10
Buoyancy Limitations when above max landing weight ***
Taking off or landing over water you must have
Outflow valve 2 closed
R Pack off
Baggage compartment weight limit
2500 lb
Maximum operating altitude***
51,000 ft
Maximum take off and landing altitude
10,000 ft. Pres. Alt
Maximum slat/flap extended altitude
18,000 ft
Maximum landing gear extended altitude
20,000 ft
Minimum flight spoiler altitude ***
300 ft
Minimum take off temperature
-40 c
Maximum take off and landing temperature
ISA +40 c
Vmo below 8000 ft
300
Vmo 8000 -10,000 ft
300 increasing linear to 335
Vmo 10,000-16,000 ft
335
Vmo 16,000-20,000 ft
335 decreasing linear to 320
Vmo 20,000-35,000 ft
320
Vmo 35,000-51,000
.925
Vfe Flaps 1 ***
225
Vfe Flaps 2 ***
210
Vfe Flaps 3 ***
210
Vfe Flaps 4 ***
185
Minimum speed with flight spoilers extended
Vref+10
Vlo ***
200
Vle
250
Maximum tire speed
195
Turbulent air penetration speed MSL to 8,000ft
265 linear to 285
Turbulent air penetration speed 10,000 ft and above ***
Lesser of 285 or .85
Max differential preservation
10.73
Max negative relief pressurization
-0.5
Max differential taxi and take off pressurization
0.1
Max differential landing
1.0
Air conditioning and pressurization Aux Press On Max altitude ***
41,000 ft
Max passengers
14 pax + 1 FA + 3 pilots =18
Lap children are approved for seat
4 and Crew rest seat. May not occupy the divan during Taxi Takeoff and Landing
APU start attempts limit ***
3 attempts in 1 hour
APU max altitude for start ***
45,000 ft
APU min temp for starting on ground
-40 c
APU max temp during start EGT
Red max limit AOM
1032° C. CAE sheet
APU max operating altitude ***
51,000 ft
APU max air extraction altitude
25,000 ft
APU max air extraction temp on the ground
+48 c or 118.4 f
Autopilot after Takeoff ***
400 ft AGL
Autopilot non steep Approach ***
80 ft AGL
Autopilot steep Approach ***
200 AGL
Engine Generator Load Limit
60 kVA continuous
67.5 kVA for 5 min
75 kVA for 2 min
APU generator load limits
40 kVA at 51,000 ft
60 kVA at 45,000 ft
Fuel capacity pressure fueling
Wings. 35,100 Both 17,550 Each
Center 14,200
Aft. 2550
Total. 51850
Fuel imbalance
Ground. 600
In-flight. 1100
Fuel crossfeed/xfer usage limits
•Do not select AFT XFER ON if either wing tank exceeds 15,000 lb
•Fuel crossfeed must be closed for Takeoff and landing
•Do not use fuel crossfeed below 10,000 ft for dual engine operations
•Minimum fuel quantity is 2500 lb per wing tank for wing to wing fuel transfer
Fuel Temp. Limitations
• Do not takeoff if engine fuel temp below 5°c
• Min. bulk fuel temp. for Takeoff -30°c
• In flight bulk fuel temp must remain above the applicable bulk fuel freezing point Jet A is -40°c
Engine anti ice ***
•Must be on for Takeoff when OAT is 10°c or below in visible moisture or when operating on contaminated runway use in accordance with anti-ice System operations
Wing Anti-ice ***
• Must be on for Takeoff when OAT is 5°c or below in visible moisture or when operating on contaminated runway.
Use in accordance with Anti-Ice system operation
• Do not hold in icing conditions with slats out
• When TAT is above 10°c do not use wing Anti-Ice in flight
Brakes min turn time ***
15 min if Temp is white 35 min & decreasing through 15 indication
EFIS ***
Do not use MAP PLAN display for navigation while operating north of 70°N or south or 70°S
FLC mode ***
When descending on any segment of any instrument or visual approach, use of FLC mode is prohibited
Approach Category ***
C with speeds faster than 140 kt use category D
Max tailwind for engine start ***
20 kt
When crosswind component exceeds 18 kt ***
Do not exceed 60% N1 below 30 kt
Min oil temp for taxi ***
20°c
Min oil temp for takeoff ***
43°c
Min oil for the oil replenishment system ***
2.5 qt minimum
Starter limitations ***
Start 1 & 2 max time 5 min followed by a cool down of 5 min and starts 3 through 10 max time 5 min followed by a cool down of 15 min
Thrust Reversers Limitations
• Use TRs in flight
• Touch & Go after deployment or TRs
• Use TRs to back the aircraft
Display Units
No operations with cabin temp in excess of 40°C for more than 30 min
Usable Fuel with Gravity Refueling
L/R wing tank 14,850 lb each
29,700 lb total
Wide cut fuels and mixing of fuels
JP4, Jet B wide cut fuels prohibited
Fuel mixing is permitted
T.O thrust time 2 & 1 engines
5 min. Both
10 min. Single
Minimum Oil start temp.
-40° c
Max oil consumption rate
.31 qt/hr
Oil replenishment min. temp.
-12°c
APU max temp for operations
ISA + 40°c
OMS Onboard Maintenance System
Prohibited for use in flight
Super Cooled Large Droplet Icing
WAI & CAI required ON
Leave ice if ice builds on side window
Max Starter Engagement
56% N2
Towing With torque link connected
Is prohibited except for straight push back
QFE ops landing
Manually set landing elevation to 0.
Engine inoperative: What’s your limitation, when it come to type of speed
Man speed only
Max Spoiler
Prohibited unless directed by procedure.
Speakers muted
Crew must wear headsets.
Wing Span
104 ft
Height
27 ft
Wheelbase distance
14 ft 5 in
