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If ACCULOAD is unavailable the crew may utilize the Runway Analysis
section of the flight papers and V Speed charts found in this section of the Flight
Manual or the QRH for manual calculation of takeoff weight limitations and V
Speeds for a specific runway. Adjustments can be made for the following nonnormal
conditions with reference to appropriate charts found in this section of
the Flight Manual:
· Engine Anti-Ice ON
· Anti Skid Inoperative
· PMC Inoperative (>>@)
· EEC Normal Mode Inoperative (BCD)
Note: Because of the precision of ACCULOAD (computerized) data, manual
calculations using generic Flight Manual data (especially with nonnormal
conditions), may not exactly match those computed by
ACCULOAD. ACCULOAD data is tailored for more specific
conditions, and should be used when available.
Note: Manual calculation of takeoff data CANNOT be made for Improved
Climb, Wet Runway conditions and Contaminated Runway conditions.
Runway Analysis (Takeoff Weight Charts)
The Runway Analysis is a computer generated takeoff performance section of
the flight papers, derived from the FAA approved Airplane Flight Manual, for
use in manual calculations of specific runway takeoff weight limitations.
Weight and assumed temperature data is provided for up to seven (7) runways.
Data is separated by flap setting. The runway and climb limit weights are
provided for a range of temperatures either side of the planned takeoff
temperature.
All data presented in the Runway Analysis is based on DRY (Normal Braking)
Conditions, BLEEDS OFF, ANTI-ICE OFF, ANTI-SKID OPERATIVE, and
PMC/EEC OPERATIVE/NORMAL. For any conditions that differ, corrections
must be made using data found in this section of the Flight Manual.
Assumed (Flex) temperatures in the Runway Analysis section are limited to
54°C; however, ACCULOAD may select higher assumed temperatures up to a
70°C (or a maximum of 25% thrust reduction). ACCULOAD will adjust the
takeoff V Speeds for the selected assumed temperature.
737 Sec. 5 Page 7
Flight Manual Continental Rev. 11/15/02 #41
Example Of Runway Analysis Data:
QP MIAOCEA
.MIAXUEA 05/1956
TGW
CO 362/05 A/C 323
**** TAKEOFF GROSS WEIGHTS B737-3-B1 - BLEEDS OFF ****
DEN ELEV 5333 TEMP 36F WIND 2009 PLANNED GW 116921
PWR: -B1 FLAP: 05
RUNWAYS:35L* 17R 17L 08R 08L 26L 35R
FLEX TEMP GW
124000 N/A N/A N/A N/A N/A N/A N/A
120000 80 80 80 80 80 80 80
116000 85 85 85 85 85 85 85
112000 95 95 95 95 95 95 95
TEMP-F CLIMB
25 1326 1259 1303 1265 1315 1240 1282 1214
35 1323 1259 1301 1260 1303 1235 1279 1212
45 1320 1257 1299 1256 1292 1231 1275 1211
55 1314 1254 1297 1251 1282 1227 1272 1210
LB/KT
HW 0 0050 0 0090 0210 0100 0080 +
TW 0320 0380 0370 0540 0930 0530 0440 -
FLEX TEMP GW PWR: -B1 FLAP: 01
124000 N/A N/A N/A N/A N/A N/A N/A
120000 85 85 85 85 85 85 85
116000 90 90 90 90 90 90 90
112000 100 100 100 100 100 100 100
TEMP-F CLIMB
25 1353 1279 1328 1262 1259 1238 1293 1242
35 1350 1276 1326 1256 1249 1233 1289 1240
45 1348 1273 1324 1250 1239 1228 1295 1239
55 1342 1270 1322 1245 1229 1223 1283 1237
LB/KT
HW 0 0080 0 0120 0220 0120 0080
TW 0500 0430 0390 0620 0670 0570 0460
LENGTH 11000 11500 12000 10004 8599 10004 12000
SLOPE -0.43 0.43 0.30 0.21 0.09 -0.21 -0.30
*35L LAST 500 FT CLSD FOR CONSTRUCTION
PART 1 ** END - TGW **
Sec. 5 Page 8 737
Rev. 11/15/02 #41 Continental Flight Manual
Legend and Description
Computer message information
Destination address
Computer message information origin address
Airline Code - Flight number / Flight departure origin date
(local time)
Aircraft fleet number
Aircraft fleet type and series
Bleed Condition - Always provided BLEEDS OFF.
Note: Anti-ice corrected takeoff data will not be provided in the Runway
Analysis. Apply the appropriate decrement from charts found in
this section of the Flight Manual should engine anti-ice be
required.
Three letter departure airport code
ELEV - Field elevation - MSL
TEMP - Departure airport ambient temperature in degrees Celsius
WIND - Departure airport surface wind direction and velocity in knots
(True). (Presented for informational purpose only. Do not use for data
computations.)
PLANNED GW - Planned takeoff gross weight in pounds
PWR - Engine rating
FLAP - Flap setting for which the performance data applies
RUNWAYS: Up to seven (7) primary takeoff runways are presented per
page. An asterisk (*) following the runway number indicates one or more
special conditions may exist for the indicated runway (i.e. intersection data
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