Part 5 - Flight Planning and Operating Data Flashcards
Weight (2 PoB, Full Fuel)
7,290 lbs
Empty weight
4,560 lbs
Fuel Flow and IAS, Sea level, max power
33.5 lbs / min, 268 kts
Fuel Flow and IAS, Sea Level, Max Intermediate
30.8 lbs/min, 256 kts
Fuel Flow and IAS, Sea Level, Max Continuous
27.4 lbs/min, 241 kts
Fuel allowance for start up, taxi and take off
60 lbs
Ground run and distance to 50ft (max weight, sea level, 10 degrees)
Ground run: 1,830 ft, 560m
50 ft: 2,960 ft, 900m
Fuel consumption, distance, time, climb speed fir climb to 5,000ft, max weight from SL
Fuel: 172 lb (includes 80 lb for start up, taxi, take off and acceleration to climb speed)
Speed: 165 kts
Time: 5.1 mins
Distance: 8 nm
Range, Range Speed and Fuel Flow at Sea Level, full tanks
286 nm, 180 kts, 18 lb/min (includes descent + 400 lb minimum fuel)
Range, Range speed and Fuel Flow at 10,000 ft (full tanks)
376 nm, 160 kts, 14 lb/min includes descent and 400l lb. in fue,l
Endurance, best endurance speed and fuel flow at sea level (full tanks)
2h, 120 kts, 14.3 lb/min
Endurance from tip tanks / main tanks at 170kts sea level
750 lb - 18 lb/min = 35 min ( assuming 80 lb for start up, taxi and take off)
1400 lb - 18 lb/min = 55 min (assuming landing with 400 lb min fuel)
Landing distance (ground roll, 90kts threshold speed, sea level, 10 degrees)
1930 ft (600m)
Landing distance (50ft, sea level 90kts threshold speed, 10 degrees)
3,340 ft (1,000m)