曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.2-4 FAA APPROVED
GIV-SP 31 May 2000
Solution:
A. Enter the Flaps 20° REFERENCE ACCELERATE-STOP DISTANCE Chart with:
Accelerate-Stop Distance available = 5800 ft. (5400 + 400) (1768 m)
Determine reference Accelerate-Stop Distance = 6300 ft. (1920 m)
B. Enter the Flaps 20° REFERENCE ACCELERATE-GO DISTANCE Chart with:
Actual runway length = 5400 ft. (1646 m)
Determine reference Accelerate-Go Distance = 5700 ft. (1737 m)
CAUTION: CLEARWAY USED MUST NOT EXCEED MAXIMUM
ALLOWABLE CLEARWAY SHOWN ON CHART.
C. Enter the Flaps 20° RUNWAY LENGTH AND V1 ADJUSTMENTS Chart with:
Reference Accelerate-Stop Distance = 6300 ft. (1920 m)
Reference Accelerate-Go Distance = 5700 ft. (1737 m)
Determine:
Effective Runway Length =6050 ft. (1844 m)
Takeoff Decision Speed Ratio V1 / VR = 0.99
NOTE: If Takeoff Decision Speed Ratio is greater than V1 / VR = 1.00, read
horizontally to left, maintaining constant Accelerate-Go Distance, until
intersecting V1 / VR = 1.00 and read effective runway length at this point.
D. Enter the Flaps 20° MAXIMUM ALLOWABLE TAKEOFF GROSS WEIGHT Chart
with:
Airport Ambient Temperature..........................................................................20° C
Airport Pressure Altitude ..............................................................................4000 ft.
Effective Runway Length.............................................................. 6050 ft. (1844 m)
Determine:
Maximum Allowable Takeoff Gross Weight = 68,000 pounds (30,844 kg)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.2-5
31 May 2000 GIV-SP
EXAMPLE 3:
(Not shown on chart)
Determine actual Accelerate-Go and Accelerate-Stop Distances for a given gross
weight and V1 / VR ratio.
Given: Airport Ambient Temperature............................................................................-5°C
Airport Pressure Altitude ..............................................................................6000 ft.
Flaps ....................................................................................................................20°
Takeoff Gross Weight .................................................... 63,000 pounds (28,580 kg)
Runway Length .......................................................................... 7000 feet (2134 m)
Runway Slope .......................................................................................+1% (uphill)
Stopway .............................................................................................. 200 ft. (61 m)
Clearway........................................................................................... 500 ft. (152 m)
Headwind .....................................................................................................10 knots
Anti-Skid and Ground Spoilers ..........................................................OPERATIVE
Cowl and Wing Anti-Ice .................................................................................... ON
V1 / VR ................................................................................................................ 1.0
Solution:
A. From example 1, effective runway length was found to be 5300 ft. (1615 m).
B. Enter the Flaps 20° RUNWAY LENGTH AND V1 ADJUSTMENTS chart with
effective runway length = 5300 ft. (1615 m) and V1 / VR = 1.00. Determine
reference accelerate-go distance to be 4900 ft. (1494 m) and reference acceleratestop
distance to be 5700 ft. (1737 m).
C. Enter the top of Flaps 20° REFERENCE ACCELERATE-GO DISTANCE chart
with 4900 ft. (1493 m) from Step B. Proceed down, making corrections as
necessary. DO NOT MAKE CLEARWAY CORRECTIONS. This result is
accelerate-go distance of 5600 ft. (1707 m). This distance is used for obstacle
clearance in Section 5.6.
D. Enter the top of Flaps 20° REFERENCE ACCELERATE-STOP DISTANCE chart
with 5700 ft. (1737 m) from Step B. Proceed down, making corrections as
necessary. Determine the accelerate-stop distance to be 5600 ft. (1707 m).
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.2-6 FAA APPROVED
GIV-SP 31 May 2000
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.2-7
31 May 2000 GIV-SP
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.2-8 FAA APPROVED
GIV-SP 31 May 2000
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：灣4飛機(jī)飛行手冊(cè)AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(122)