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

DEFINITIONS
PROCEDURES FOR USE OF TAKEOFF PERFORMANCE TABLES
Determine the dry runway takeoff field length as described in Procedures for Use of Takeoff
Performance Tables in Section IV of the basic FAA Approved Airplane Flight Manual. Using the same
procedures, determine the wet takeoff field length, V1, VR, V2, and VENR from the following figures. If
the runway has a gradient, the takeoff field length and V1 must be adjusted in accordance with the
following figures:
The takeoff field length is the longer of the wet or dry takeoff field lengths. Use the takeoff speeds
determined from wet runway performance.
EXAMPLE FOR TAKEOFF WITH FLAPS UP:
From Takeoff Field Length - Feet, Flaps UP (Anti-Ice ON) in Section IV, PERFORMANCE, TAKEOFF
of the basic FAA Approved Airplane Flight Manual, the Takeoff Field Length is 3320 FEET (dry
runway, anti-ice ON).
From Figure S4-4, the Takeoff Field Length is 3450 FEET (wet runway, anti-ice ON).
V1 = 86 KNOTS, VR = 99 KNOTS, V2 = 108 KNOTS, VENR = 118 KNOTS.
Takeoff Field Length for above conditions = 3450 FEET and V1 = 86 KNOTS, VR = 99 KNOTS,
V2 = 108 KNOTS, VENR = 118 KNOTS.
(Continued Next Page)
Wet Runway: A runway is considered wet when there is sufficient moisture on the
surface to appear reflective, but without significant areas of standing
water.
Takeoff Field Length:
(Wet)
The takeoff field length given for each combination of gross weight,
ambient temperature, altitude, wind, and runway gradients is the
greatest of the following:
a. 115 percent of the two-engine horizontal takeoff distance from
start to a height of 35 feet above runway surface.
b. Accelerate-stop distance.
c. The engine-out accelerate-go distance to 15 feet.
d. The Dry Takeoff Field Length.
No specific identification is made on the charts as to which of these
distances governs a specific case.
LEVEL RUNWAY
RUNWAY GRADIENT
ADJUSTMENT
Flaps UP, anti-ice OFF Figure S4-2 Figure S4-1
Flaps UP, anti-ice ON Figure S4-4 Figure S4-3
Flaps 15°, anti-ice OFF Figure S4-6 Figure S4-5
Flaps 15°, anti-ice ON Figure S4-8 Figure S4-7
Pressure Altitude = 2000 FEET Runway Gradient = ZERO (level)
Gross Weight = 8000 POUNDS Anti-Ice = ON
Ambient Temperature = +10°C Runway Condition = WET
Wind = 10 KNOTS (HEADWIND)
510FM-S4-01 S4-AA S4-7
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
WET RUNWAY TAKEOFF PERFORMANCE (Continued)
EXAMPLE FOR TAKEOFF WITH FLAPS 15°:
From Takeoff Field Length - Feet, Flaps 15° (Anti-Ice OFF) in Section IV, PERFORMANCE,
TAKEOFF of the basic FAA Approved Airplane Flight Manual, the Takeoff Field Length is 3980 FEET
(dry runway, anti-ice off).
From Figure S4-6, the Takeoff Field Length is 4000 FEET (wet runway, anti-ice off).
V1 = 82 KNOTS, VR = 90 KNOTS, V2 = 97 KNOTS, VENR = 118 KNOTS.
Takeoff Field Length for above conditions = 4000 FEET and V1 = 82 KNOTS, VR = 90 KNOTS,
V2 = 97 KNOTS, VENR = 118 KNOTS.
Pressure Altitude = 7000 FEET Runway Gradient = ZERO (level)
Gross Weight = 8645 POUNDS Anti-Ice = OFF
Ambient Temperature = +5°C Runway Condition = WET
Wind = 10 KNOTS (HEADWIND)
S4-8 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, WITH FLAPS UP
WET RUNWAY OVER 15 FOOT SCREEN HEIGHT, ANTI-ICE OFF
Determine takeoff field length, V1, VR, V2, and VENR from Figure S4-2. If the runway has a
gradient, adjust V1 and Takeoff Field Length using Figure S4-1. If the required distance is greater
than the available distance, the airplane weight must be reduced until distance required is less
than or equal to distance available.
Figure S4-1*
510FM-S4-02 S4-AH S4-9
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 1 of 15)*
S4-10 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 2)*
510FM-S4-02 S4-AH S4-11
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 3)*
S4-12 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 4)*
510FM-S4-02 S4-AH S4-13
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 5)*
S4-14 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 2(23)