Limitations Flashcards
Max Operating Altitude
25,000
Maneuvering Limit Load Factors
Flaps Retracted = 2.5g to -1g
Flaps extended = 2g to 0g
Gear Down = 2g to 0 G
Cargo Door Crosswind Operation
no more than 45kts
Max Passenger Seats
60
Max Ramp Weight
41,380 lbs
18,770 Kg
Max Take Off Weight
41,005 lbs
18,600 Kg
Max Landing Weight
40,344 lbs
18,300 Kg
Max Zero Fuel Weight
36,817 lbs
16,700 Kg
Vmo
250 kts IAS
Mmo
0.55
Va
160 kts IAS
VFE
Flaps 15 = 180 kts
Flaps 25 = 160 kts
Flaps 35 = 150 kts
Vle
180 kts
Vlo ret
160 kts
Vlo low
170 kts
Vra (max rough air)
180 kts
Vwo (wiper operating)
160 kts
Max Tire Speed
165 kts (ground speed)
Tail Wind Limit
15 kts
Max Rnwy Slope
+- 2%
X-Wind
45 kts
Fuel Quantity
4960 lbs
Max Fuel Unbalance
1212lbs
Max Dif Pressure
6.35 PSI
Max Negative Dif Pressure
-0.5 PSI
Max Dif Pressure for Landing
0.35 PSI
Max Dif Pressure for OVBD Valve Full Open
1 PSI
Max Alt for ONE BLEED OFF
20,000 Ft
Fuel Density and Temp Limitations
Density: 6.3 to 7.1 pounds per US gallon
Max Temp: 54C
Min Temp: -40 Jet A
-47 JetA1
Fuel and Hydraulic Circuit Breaker Reset?
Not allowed
Reduced Thrust
Not permitted on Contaminated Runways
Not Permitted with significant workload items (ie inop Auto skid, engine gauges etc)
Evacuation System
Slide Girt Bars must be installed and emergency operating handle on rear bulkhead door must be exposed prior to leaving loading until arriving at loading ramp
Emergency Light System must be armed for:
all flight operations
Windshield Heat/Cracked Windshield
Windshield anti-ice must be on and checked for flight ops except as follows:
1) no operate on cracked window
2) Do not exceed 315 KIAS below 10000 when heat inop
Cracked wind shield below 10000 -
315 outer
235 inner
Air FLOW switch
Must be NORM for takeoff
Autoland
Tailwind 10kts Crosswind 15kts Headwind 25kts Do not use if: 1) Align not annunciated by 100ft RAD 2) "RUDDER PWR OFF alert displayed 3) Airport elevation exceeds 8000MSL 4) runway slope +/- 0.8% 5) Flight Control adnormals 6) Runway width less than 145ft
AutoPilot
no engagement below 200ftAGL
Disengage prior than Mins minus 50 feet
no use if STAB OUT OF TRIM alert longer than 3 sec. after glideslope
Max Airspeed for malfunc or inop Mach Trim Compen
.78 Mach