MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
TAKEOFF / GO-AROUND THRUST SETTINGS
ANTI-ICE OFF (TO DETENT)
Figure 4-13
510FM-00 AA 4-27
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
TAKEOFF / GO-AROUND THRUST SETTINGS
ANTI-ICE ON (TO DETENT)
Figure 4-14
4-28 AA 510FM-00
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
MAXIMUM CONTINUOUS THRUST SETTING EXAMPLES
EXAMPLE 1: (SINGLE-ENGINE CLIMB)
Anti-Ice = OFF
a. Indicated RAT = -15°C
b. Pressure Altitude = 30,000 FEET
c. N1 = 90.4% RPM (Refer to Figure 4-15)
EXAMPLE 2: (SINGLE-ENGINE CLIMB)
Anti-Ice = ON
a. Indicated RAT = -40°C
b. Pressure Altitude = SEA LEVEL
c. N1 = 81.4% RPM (Refer to Figure 4-16)
EXAMPLE 3: (MULTI-ENGINE)
Anti-Ice = OFF
a. Indicated RAT = -10°C
b. Pressure Altitude = 30,000 FEET
c. N1 = 88.8% RPM (Refer to Figure 4-17)
EXAMPLE 4: (MULTI-ENGINE)
Anti-Ice = ON
a. Indicated RAT = -30°C
b. Pressure Altitude = 10,000 FEET
c. N1 = 90.4% RPM (Refer to Figure 4-18)
510FM-00 AA 4-29
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
MAXIMUM CONTINUOUS THRUST SETTINGS
SINGLE-ENGINE (CLB DETENT) ANTI-ICE OFF
Figure 4-15
4-30 AA 510FM-00
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
MAXIMUM CONTINUOUS THRUST SETTINGS
SINGLE-ENGINE (CLB DETENT) ANTI-ICE ON
Figure 4-16
510FM-00 AA 4-31
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
MAXIMUM CONTINUOUS THRUST SETTINGS
MULTI-ENGINE (CLB DETENT) ANTI-ICE OFF
Figure 4-17
4-32 AA 510FM-00
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
MAXIMUM CONTINUOUS THRUST SETTINGS
MULTI-ENGINE (CLB DETENT) ANTI-ICE ON
Figure 4-18
510FM-00 AA 4-33
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
BUFFET ONSET / AIRSPEED - KIAS
Figure 4-19
LOW HIGH
EXAMPLE: EXAMPLE:
Indicated Mach = 0.25 Indicated Mach = 0.40
Pressure Altitude = 20,000 FEET Pressure Altitude = 30,000 FEET
Weight = 8,000 POUNDS Weight = 8,000 POUNDS
Buffet Onset Buffet Onset
Load Factor = 1.35 G’S Load Factor = 2.07 G’S
Bank Angle = GREATER THAN 42° Bank Angle = 61°
4-34 AA 510FM-00
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
CROSSWIND COMPONENT
Figure 4-20
EXAMPLE:
WIND VELOCITY = 30 KNOTS
ANGLE BETWEEN WIND DIRECTION AND RUNWAY = 30°
CROSSWIND COMPONENT = 15 KNOTS
WIND COMPONENT PARALLEL TO RUNWAY = 26 KNOTS
510FM-00 AA 4-35/4-36
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
TAKEOFF
TABLE OF CONTENTS
PAGE
Takeoff Performance Simplified Criteria . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-39
Procedures for Use of Takeoff Performance Tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-40
Maximum Takeoff Weight - Pounds Permitted by Climb Requirements,
Flaps UP (Anti-Ice OFF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-41
Maximum Takeoff Weight - Pounds Permitted by Climb Requirements,
Flaps UP (Anti-Ice ON) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-42
Maximum Takeoff Weight - Pounds Permitted by Climb Requirements,
Flaps 15° (Anti-Ice OFF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-43
Maximum Takeoff Weight - Pounds Permitted by Climb Requirements,
Flaps 15° (Anti-Ice ON). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-44
Takeoff Field Length - Feet, Flaps UP (Anti-Ice OFF). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-45
Takeoff Field Length - Feet, Flaps UP (Anti-Ice ON). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-61
Takeoff Field Length - Feet, Flaps 15° (Anti-Ice OFF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-77
Takeoff Field Length - Feet, Flaps 15° (Anti-Ice ON) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-93
Single-Engine Takeoff Flight Path - Flaps UP (First and Second Segments) . . . . . . . . . . . . . . . 4-109
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