Need help from Pinnacle and Skywest pilots...
I'm trying to create some flashcards for an iPhone app, I've got info on ASA, Shuttle, Chautauqua, Expressjet, but I need limitations for Pinnacle (CRJ and CR9) and Skywest (CR2/7/9). Other airlines welcome too, PSA, Piedmont, Eagle, etc. Anyone able to help me out? PM me if you're able to help, thanks!
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What kind of info do you need about Piedmont?
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Originally Posted by dashtrash300
(Post 635545)
What kind of info do you need about Piedmont?
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Dash 8 100 Limitations
Max Take off Weight 34,500 Max Landing Weight 33,900 Max Ramp Weight 34,700 Max Zero Fuel Weight 31,400 Max Fuel Imbalance in flight 600 lbs Max Operating Altitude 25,000 Max Operating Altitude for take off and landing 10,000 Max Runway Slops +/- 2% Vmo 0-14,000 ft 242kts Vmo 15,000 ft 239kts Vmo 20,000 ft 223kts Vmo 25,000 ft 207kts Vfe flaps 5 148kts Vfe flaps 15 148kts Vfe flaps 35 130kts Max ITT for takeoff is 816 degrees C Max Normal ITT for takeoff is 785 degrees C Max Continuous ITT is 800 degrees C Max Transient ITT is 850 degrees C for 20 seconds Max ITT in reverse is 785 degrees C Max Take-off NH% is 100% Normal takeoff Np RPM should not exceed 1212 Normal Oil Pressure 55-65 PSI Normal Oil Temp is 45-115 degrees C Max speed for unfeathering prop is 165kts Max Torque with a prop feathered is 50% Max altitude with the landing gear/flaps extended is 15000 feet Max tire groundspeed is 139kts Max cabin altitude for pressurized flight is 8000 Minimum NH is 60% Va 163kts Vlo 158kts Vle 172kts Rough Air 180kts Alt gear extension speed is 140kts Max take off torque is 105% Normal take off torque is 90% Max transient torque is 125% for 20 seconds Max reserve torque is 90% Dash 8 300 Limitations Max Take off Weight 43,000 Max Landing Weight 42,000 Max Ramp Weight 43,200 Max Zero Fuel Weight 39,500 Max Fuel Imbalance in flight 600 lbs Max Operating Altitude 25,000 Max Operating Altitude for take off and landing 10,000 Max Runway Slops +/- 2% Vmo 0-17,000 ft 243kts Vmo 20,000 ft 232kts Vmo 25,000 ft 214kts Vfe flaps 5 163kts Vfe flaps 15 150kts Vfe flaps 35 138kts Max ITT for takeoff is 800 degrees C Max Normal ITT for takeoff is 765 degrees C Max Continuous ITT is 800 degrees C Max Transient ITT is 840 degrees C for 20 seconds Max ITT in reverse is 765 degrees C Max Take-off NH% is 102.7% Normal takeoff Np RPM should not exceed 1212 Normal Oil Pressure 55-65 PSI Normal Oil Temp is 45-115 degrees C Max speed for unfeathering prop is 165kts Max Torque with a prop feathered is 48% Max altitude with the landing gear/flaps extended is 15000 feet Max tire groundspeed is 165kts Max cabin altitude for pressurized flight is 8000 Minimum NH is 66% Va 177kts Vlo 163kts Vle 173kts Rough Air 190kts Alt gear extension speed is 140kts Max take off torque is 105.6% Normal take off torque is 90% Max transient torque is 115% for 20 seconds Max reserve torque is 90% Let me know if there is anything else you need |
Originally Posted by dashtrash300
(Post 635553)
Dash 8 100 Limitations
Max Take off Weight 34,500 Max Landing Weight 33,900 Max Ramp Weight 34,700 Max Zero Fuel Weight 31,400 Max Fuel Imbalance in flight 600 lbs Max Operating Altitude 25,000 Max Operating Altitude for take off and landing 10,000 Max Runway Slops +/- 2% Vmo 0-14,000 ft 242kts Vmo 15,000 ft 239kts Vmo 20,000 ft 223kts Vmo 25,000 ft 207kts Vfe flaps 5 148kts Vfe flaps 15 148kts Vfe flaps 35 130kts Max ITT for takeoff is 816 degrees C Max Normal ITT for takeoff is 785 degrees C Max Continuous ITT is 800 degrees C Max Transient ITT is 850 degrees C for 20 seconds Max ITT in reverse is 785 degrees C Max Take-off NH% is 100% Normal takeoff Np RPM should not exceed 1212 Normal Oil Pressure 55-65 PSI Normal Oil Temp is 45-115 degrees C Max speed for unfeathering prop is 165kts Max Torque with a prop feathered is 50% Max altitude with the landing gear/flaps extended is 15000 feet Max tire groundspeed is 139kts Max cabin altitude for pressurized flight is 8000 Minimum NH is 60% Va 163kts Vlo 158kts Vle 172kts Rough Air 180kts Alt gear extension speed is 140kts Max take off torque is 105% Normal take off torque is 90% Max transient torque is 125% for 20 seconds Max reserve torque is 90% Dash 8 300 Limitations Max Take off Weight 43,000 Max Landing Weight 42,000 Max Ramp Weight 43,200 Max Zero Fuel Weight 39,500 Max Fuel Imbalance in flight 600 lbs Max Operating Altitude 25,000 Max Operating Altitude for take off and landing 10,000 Max Runway Slops +/- 2% Vmo 0-17,000 ft 243kts Vmo 20,000 ft 232kts Vmo 25,000 ft 214kts Vfe flaps 5 163kts Vfe flaps 15 150kts Vfe flaps 35 138kts Max ITT for takeoff is 800 degrees C Max Normal ITT for takeoff is 765 degrees C Max Continuous ITT is 800 degrees C Max Transient ITT is 840 degrees C for 20 seconds Max ITT in reverse is 765 degrees C Max Take-off NH% is 102.7% Normal takeoff Np RPM should not exceed 1212 Normal Oil Pressure 55-65 PSI Normal Oil Temp is 45-115 degrees C Max speed for unfeathering prop is 165kts Max Torque with a prop feathered is 48% Max altitude with the landing gear/flaps extended is 15000 feet Max tire groundspeed is 165kts Max cabin altitude for pressurized flight is 8000 Minimum NH is 66% Va 177kts Vlo 163kts Vle 173kts Rough Air 190kts Alt gear extension speed is 140kts Max take off torque is 105.6% Normal take off torque is 90% Max transient torque is 115% for 20 seconds Max reserve torque is 90% Let me know if there is anything else you need |
have you got skywest yet?
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Originally Posted by nigelcobalt
(Post 635584)
have you got skywest yet?
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Essw,
PM me |
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