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SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-8 (Sheet 12)*
510FM-S4-01 S4-AA S4-69
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-8 (Sheet 13)*
S4-70 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-8 (Sheet 14)*
510FM-S4-01 S4-AA S4-71
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-8 (Sheet 15)*
S4-72 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
LANDING PERFORMANCE
PROCEDURES FOR USE OF APPROACH AND LANDING PERFORMANCE
TABLES WHICH CAN BE USED TO SHOW COMPLIANCE TO JAR
OPERATIONS
Landing distances determined from Procedures for use of Approach and Landing Performance
Tables from the basic FAA Approved Airplane Flight Manual must be corrected in accordance with
applicable operating rules (refer to Figure S4-9 for Anti-Ice OFF or Figure S4-10 for Anti-Ice ON).
510FM-S4-01 S4-AA S4-73
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-9*
NOTE
The Abnormal Overspeed (+10 knots) Wet Runway Factor presented on this figure is
restricted to landings without tailwinds.
S4-74 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-10*
510FM-S4-01 S4-AA S4-75
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
DATA FOR WATER, SLUSH, SNOW, AND ICE COVERED
RUNWAYS
INTRODUCTION
The following information is considered the most accurate and practical guidance material available
for adverse runway operations. The information is approved in accordance with JAR 25X1591 and
the airplane certification basis. This performance information does not in any way replace or amend
the Operating Limitations and Performance Information for non-contaminated runways.
PERFORMANCE
For takeoffs and landings on contaminated covered runways, use the following tables and correction
factors. The performance information assumes runway contaminant to be of uniform depth and
density over the entire runway surface. The impingement drag is based on testing performed on a
Cessna Citation Mustang. This performance does not include operational factors.
WARNING
THESE DISTANCES AND CORRECTION FACTORS FOR CONTAMINATED
RUNWAY CONDITIONS ARE APPROXIMATE AND ARE TO BE
CONSIDERED MINIMUMS, AS ACTUAL RUNWAY CONDITIONS MAY
REQUIRE DISTANCES GREATER THAN THOSE DETERMINED. WHERE
POSSIBLE, EVERY EFFORT SHOULD BE MADE TO ENSURE THAT THE
RUNWAY SURFACE IS CLEARED OF ANY SIGNIFICANT
CONTAMINATION. GROUND HANDLING CHARACTERISTICS,
PARTICULARLY FOLLOWING ENGINE FAILURE, IN CROSSWINDS MAY
BE DEGRADED.
DEFINITIONS
(Continued Next Page)
Runway Contaminated by
Compacted Snow: A runway is considered contaminated by compacted snow when
covered by snow which has been compressed into a solid mass such
that the airplane wheels at representative operating pressures and
loadings will run on the surface without causing significant rutting.
Runway Contaminated by
Wet Snow: A runway is considered contaminated by wet snow when covered by
snow, which if compacted by hand will cause water to be squeezed
out, with a specific gravity of 0.85.
Runway Contaminated by
Dry Snow: A runway is considered contaminated by dry snow when covered by
fresh snow with relatively little liquid water content, such that water
cannot be squeezed out when compacted by hand, and with a specific
gravity not greater than 0.2.
Runway Contaminated by
Standing Water: A runway is considered contaminated by standing water when
covered by water of a depth greater than 3mm.
S4-76 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
DEFINITIONS (Continued)
Runway Contaminated by
Slush: A runway is considered contaminated by slush when covered by
partly melted snow or ice with a high water content, such that it cannot
significantly resist compression by hand, and of an assumed specific
gravity of 0.85.
Runway Contaminated by
Wet or Dry Ice (untreated): A frozen surface which is presumed to be slippery whether wet or dry.
Takeoff Field Length:
(Contaminated) The takeoff field length given for each combination of gross weight,
ambient temperature, altitude, wind, and runway gradients is the
greatest of the following:
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