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HIGH) and landing gear extended. For Emergency and Abnormal
Procedures, the airspeed equal to the 50-foot point speed with flaps in
landing position as defined and landing gear extended.
VSO: The stalling speed or the minimum steady flight speed in the landing
configuration.
VSSE: Safe, intentional, one-engine inoperative speed.
• Flaps UP and Flaps 15° VSSE = V2
• Flaps LAND VSSE = VREF
VS1: The stalling speed or the minimum steady flight speed obtained in a
specified configuration.
VX: Best angle of climb speed (Multi-engine, flaps 0°) 114 KIAS.
VY: Best rate of climb speed (Multi-engine, flaps 0°) 150 KIAS.
Visible Moisture: Visible moisture includes, but is not limited to, the following
conditions: fog with visibility less than one mile, wet snow and rain.
Wind: The wind velocities recorded as variables on the charts of this section
are to be understood as the headwind or tailwind components of the
actual winds at 32.8 feet (10 meters) above the runway surface (tower
winds).
510FM-07 AA 4-11
SECTION IV - PERFORMANCE MODEL 510
GENERAL
FAA APPROVED
U.S. Configuration
CONFIGURATIONS
Figure 4-1
NOISE CHARACTERISTICS
CERTIFICATED NOISE LEVELS
The following noise levels were established using test data obtained and analyzed under procedures
of 14 CFR 36, Amendment 26 and the equivalent procedures of International Civil Aviation
Organization (ICAO) Annex 16, Volume I, Aircraft Noise, Third Edition, July 1993, Amendment 7,
effective March 21, 2002. This aircraft complies with the Stage 4 noise limits of 14 CFR 36 and the
Chapter 4 noise limits of ICAO Annex 16.
Flyover and lateral noise levels were obtained at a takeoff weight of 8,645 pounds with 15 degrees
flaps and climb speed of 107 KIAS. For flyover, thrust was cut back from takeoff N1 to 78.3% N1 at
2799 feet AGL. Approach data was obtained at 8000 pounds, landing gear down, flaps 30° and 104
KIAS.
No determination has been made by the Federal Aviation Administration that the noise levels of this
airplane are or should be acceptable or unacceptable for operation at, into, or out of, any airport.
(Continued Next Page)
NUMBER OF
OPERATING
ENGINES
THRUST FLAP SETTING GEAR
1st SEGMENT TAKEOFF CLIMB 1 TAKEOFF UP and 15° DOWN
2nd SEGMENT TAKEOFF CLIMB 1 TAKEOFF UP and 15° UP
3rd SEGMENT HORIZONTAL
ACCELERATION
1 TAKEOFF
(10 MINUTES MAXIMUM)
THEN MAXIMUM CONTINUOUS
SINGLE ENGINE THRUST
UP and 15° UP
ENROUTE CLIMB 1 MAXIMUM CONTINUOUS
SINGLE ENGINE THRUST
UP UP
APPROACH CLIMB 1 TAKEOFF 15° UP
LANDING CLIMB (Stall Warning-NORMAL) 2 TAKEOFF 30° / LAND DOWN
LANDING CLIMB (Stall Warning-HIGH) 2 TAKEOFF 15° DOWN
NOISE REFERENCE EPNdB
FLYOVER 73.9
LATERAL 85.0
APPROACH 86.0
STAGE 4/CHAPTER 4 MARGIN 26.1
4-12 AA 510FM-07
MODEL 510 SECTION IV - PERFORMANCE
GENERAL
FAA APPROVED
Configuration U.S.
NOISE CHARACTERISTICS (Continued)
SUPPLEMENTAL A-WEIGHTED NOISE LEVELS
The following A-weighted noise levels were established for 14 CFR Part 36 reference conditions
used in CERTIFICATED NOISE LEVELS.
Flyover and lateral noise levels were obtained at a takeoff weight of 8645 pounds with 15 degrees
flaps and climb speed of 107 KIAS. For flyover, thrust was cut back from takeoff N1 to 78.3% N1 at
2799 feet AGL. Approach data was obtained at 8000 pounds, landing gear down, flaps 30° and 104
KIAS.
NOISE REFERENCE dBA
FLYOVER 62.2
LATERAL 74.8
APPROACH 75.7
510FM-07 AA 4-13/4-14
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
STANDARD CHARTS
TABLE OF CONTENTS
PAGE
ISA Temperature Deviation Correction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-17
Ambient Temperature - °C . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-17
Temperature Conversion - Celsius to Fahrenheit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-18
Pressure Conversion - Inches of Mercury to Millibars . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-18
Fuel Quantity Conversion - U.S. Gallons to Liters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-19
Weight Conversion - Pounds to Kilograms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-19
Horizontal Length Conversion - Feet to Meters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-20
Airspeed and Machmeter Calibration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-21
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