Part 5 - Flight Planning and Operating Data Flashcards

1
Q

Weight (2 PoB, Full Fuel)

A

7,290 lbs

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2
Q

Empty weight

A

4,560 lbs

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3
Q

Fuel Flow and IAS, Sea level, max power

A

33.5 lbs / min, 268 kts

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4
Q

Fuel Flow and IAS, Sea Level, Max Intermediate

A

30.8 lbs/min, 256 kts

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5
Q

Fuel Flow and IAS, Sea Level, Max Continuous

A

27.4 lbs/min, 241 kts

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6
Q

Fuel allowance for start up, taxi and take off

A

60 lbs

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7
Q

Ground run and distance to 50ft (max weight, sea level, 10 degrees)

A

Ground run: 1,830 ft, 560m
50 ft: 2,960 ft, 900m

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8
Q

Fuel consumption, distance, time, climb speed fir climb to 5,000ft, max weight from SL

A

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

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9
Q

Range, Range Speed and Fuel Flow at Sea Level, full tanks

A

286 nm, 180 kts, 18 lb/min (includes descent + 400 lb minimum fuel)

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10
Q

Range, Range speed and Fuel Flow at 10,000 ft (full tanks)

A

376 nm, 160 kts, 14 lb/min includes descent and 400l lb. in fue,l

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11
Q

Endurance, best endurance speed and fuel flow at sea level (full tanks)

A

2h, 120 kts, 14.3 lb/min

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12
Q

Endurance from tip tanks / main tanks at 170kts sea level

A

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)

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13
Q

Landing distance (ground roll, 90kts threshold speed, sea level, 10 degrees)

A

1930 ft (600m)

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14
Q

Landing distance (50ft, sea level 90kts threshold speed, 10 degrees)

A

3,340 ft (1,000m)

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