Limitations And Numbers Flashcards
Max Baggage
AFT & Forward
Aft-2534 LBS
Forward-3306 LBS
Max ramp weight
Max takeoff weight
Max landing weight
Max zero fuel weight
MRW- 85,870
MTOW-85,517
MLDW-74,957
MZFW-69,886
G Loading limits
Flaps up & Flaps full (1-Full….)
Flaps Up -1.0 + 2.5
Flaps Down -0.0 + 2.0
Altitudes
Max operation
Max take-off and Landing
Minimum Take-off and Landing
41,000
8,000
-1,000
Max speed in Turbulence
Below 10,000 = 250 KIAS
At or Above 10,000 = 270 KIAS or .76 M
Max Cross Wind (dry,wet,compacted snow, slush, Ice)
Dry = 38 kts Wet =31 Compact Snow = 20 Standing Water / slushy snow= 18 Ice = 12 kts
Total Usable fuel and fuel Per Tank in pounds
Total = 20,786
Per Tank = 10,393
Differential Pressure -
Max
Over pressure
Takeoff and Landing
Negative
37,000 and below = 7.8 PSI 37,000 and Above = 8.34 Over pressure = 8.77 Negative = -0.5 Take-off Landing = 0.2
Max Altitude for Single PACK
31,000 feet
Max ITT?
Start, continuous, TOGA
Start - 815C
Continuous - 960C
TOGA Two engine - 990C for ten minutes
Single engine - 990C for ten minutes with up to 1006*C for the first two minutes.
Max Oil Temperatures and minimum/maximum Pressure?
Temperature:
Continuos - 155C
Transient - 163C
Pressure:
Minimum - 25psi
Maximum - 95 psi
Engine starter duty cycles ?
Attempt one and two : 90 seconds on, 10 seconds off
Attempt three - five : 90 seconds on, 5 minutes off
Tail Height
32’ 3”
Wingspan ?
94’
Total length?
103’ 11”
Turning Radius ?
59’ 2” (for a 180 degree turn)
APU Max Altitudes:
Start
Electrical power
Bleed
Engine start assist
Start: 30,000’
Electric: 33,000’
Bleed: 15,000’
Engine Start: 21,000’
Maximum Speeds:
Tire-
Windshield Wiper-
Direct Vision Window-
Tire - 195
Wiper operation - 253
Direct Vision Window - 160
Max operation speeds
Below 8,000’
Above 10,000’
Mmo (FL 290-410)
Below 8,000’ = 300 KIAS
Above 10,000’ = 320 KIAS
Max Mach = .82
Max static takeoff crosswind
25 knots
Static Takeoff
Pilot lines up the airplane on the runway, applies brakes, adjusts thrust to 40% N1, when engines stabilize at 40% N1, advances thrust levers to TOGA detent. Release the brakes when N1 reaches 60%.
NOTE Due to the possibility of compressor stall, a static takeoff is not recommended with a crosswind greater than 25 kt.
How many cabin hand held fire extinguishers?
Five
Two front halon
Two aft halon
One aft water
What differential pressure will open the over pressure outflow valve?
8.6 PSI
The airplane will explode at 8.77