Need help from Pinnacle and Skywest pilots...
06-26-2009 | 10:16 AM
#1
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Joined: Apr 2009
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From: CR7 Captain
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!
06-26-2009 | 10:45 AM
#3
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Joined: Apr 2009
Posts: 16
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From: CR7 Captain
Any limitations for the Dash would be great. I'm formatting them to work with a flash card app on the iPhone so PDFs etc of limitations or systems questions (at ASA we have an oral study guide that the training department puts out that includes 500 some questions) would be useful.
06-26-2009 | 11:02 AM
#4
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Joined: Apr 2009
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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
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
06-26-2009 | 11:13 AM
#5
Thread Starter
On Reserve
Joined: Apr 2009
Posts: 16
Likes: 0
From: CR7 Captain
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
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
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