Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 739 / 923

Page 9-4 P/N 140-590032-0007
Revision A5: Feb, 2012
Pilot’s Operating Manual
Section IV - Sub-section 9
EXTENDED RANGE OPERATIONS (Non-ETOPS)
The 180 minute distance of 1027 nm was calculated as follows:
• From the Single Engine High Speed Descent data:
• From the Single Engine Maximum Continuous Thrust (MCT) Cruise data at 15,000 ft, the
following table was prepared by linear interpolation:
— Single Engine Maximum Continuous Thrust (MCT) Cruise at 15,000 ft:
• From the above table, the following Single Engine Maximum Continuous Thrust (MCT)
Cruise performance data at 15,000 ft was calculated (all numbers rounded to the nearest
unit):
• Adding the fuel, distance, and time from the Single Engine High Speed Descent to 15,000
ft and the Single Engine Maximum Continuous Thrust (MCT) Cruise at 15,000 ft, the
following results were obtained:
Top Of Descent Descent Bottom Of Descent
Altitude
(ft)
Weight
(lb)
Fuel
(lb)
Distance
(nm)
Time
(min)
Altitude
(ft)
Weight
(lb)
39000 23524 484 146 22 14000 23040
15000 23524 51 11 2 14000 23473
subtracting 2
nd
row from 1
st
row:
39000 23524 433 135 20 15000 23091
Weight
(lb)
TAS
(knot)
Fuel Flow
(lb/hr)
18000 340 1649
20000 337 1646
22000 333 1642
24000 329 1638
Weight (lb)
KTAS
Avg
Fuel
(lb)
Distance
(nm)
Time
(min)
Start End Avg
23091 21997 22544 332 1094 221 40
21997 20353 21175 335 1644 335 60
20353 18708 20308 336 1645 336 60
Cruise Total = 4383 892 160
Fuel
(lb)
Distance
(nm)
Time
(min)
4816
(433+4383)
1027
(135+892)
180
(20+160)