MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
TAKEOFF PERFORMANCE
SIMPLIFIED CRITERIA
A simplified criteria is provided which is intended to cover the majority of situations where runway
length is appreciably longer than required for this airplane. The other tabulated data gives more
exact performance criteria through a range of conditions which include all but the most extreme
cases.
The majority of takeoff situations result in field length margins that permit using a single set of values
for speeds and power settings for takeoff. If the following conditions are met, the simplified
procedures may be used.
1. No obstacle in flight path.
2. Throttles - TAKEOFF detent (Thrust Mode Indicator - green T/O).
3. Takeoff and approach flaps (15°).
4. Anti-Ice OFF or ON.
5. Takeoff field length available = 5,000 feet or longer.
6. No Tailwind.
7. Runway Gradient-Takeoff = Zero to -2.0% (downhill).
8. Dry paved runway.
The values to be used are as follow:
When conditions are other than those specified in the simplified criteria, the appropriate
tabulated data must be referred to.
510FM-05 AA 4-39
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
PROCEDURES FOR USE OF TAKEOFF PERFORMANCE
TABLES
1. Determine gross weight of airplane for type of loading desired.
2. Obtain airport information; i.e., active runway, available runway length, ambient temperature
(TEMP), altitude, wind, icing conditions and runway gradient (if applicable) and obstacles in
the takeoff flight path. Determine that the temperature is within the ambient temperature
limits found in Section II, Limitations.
3. Determine wind component parallel to active runway from the crosswind component chart
(Figure 4-20).
4. Check the maximum takeoff weight permitted by climb requirements (Figure 4-21 or 4-23). If
takeoff is to be made with anti-ice on, refer to Figure 4-22 or 4-24. If this limitation restricts
the gross weight, weight must be reduced until the requirement is met.
5. Using the takeoff weight determined in step 4, determine takeoff field length, V1, VR, V2,
VENR from Figure 4-26 (Flaps UP, Anti-Ice OFF), Figure 4-28 (Flaps UP, Anti-Ice ON), Figure
4-30 (Flaps 15°, Anti-Ice OFF), or Figure 4-32 (Flaps 15°, Anti-Ice ON).
NOTE
For inoperative antiskid system, multiply the Flaps UP takeoff field length obtained
from Figures 4-26 or 4-28 by 1.39 or multiply the Flaps 15° takeoff field length
obtained from Figures 4-30 or 4-32 by 1.44.
6. For runway gradients, V1 and takeoff field length must be corrected using the correction
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