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Hello,
I have test flown PSS' 777-300ER and wrote down all relevant data, and inserted them in a new prf file. But everytime I build a flight plan it keeps me at FL280/290. I have included the prf file. See what you guys think of it.
Regards,
Xander
edit: for some reason it won't accept the attachment. Here it is:
[B773ER] ---------------- Boeing 777-300ER w GE90-115BL --- (Xander Koote) ---
[UNITS]
FUEL=kgs/hr
MACHCRUISE=84
[CLIMB]
; ALT TAS ROC FUEL
1000 196 3800 36600
3000 255 3600 26000
5000 262 3300 24800
7000 269 3200 23400
9000 277 3000 22200
11000 354 1200 20400
13000 365 2900 19800
15000 375 2600 18400
17000 386 2300 17200
19000 398 2000 15800
21000 410 1700 14600
23000 423 1500 13400
25000 436 1200 12600
27000 449 1000 11800
29000 463 900 11400
31000 478 800 11000
33000 487 900 10600
35000 482 900 10000
37000 481 900 9600
39000 481 900 9200
41000 481 900 8900
43000 481 900 8500
[CRUISE]
; GRWT/FF (based on.M84 cruise) (GrWt in thousands of kgs, total of both engines)
; (FF kgs/hr)
[GRWT] 180 190 200 210 220 230 240 250 260 270 280 290 300 310 320 330
; ALT TAS
43000 481 5340 5580 -- -- -- -- -- -- -- -- -- -- -- -- -- --
41000 481 5670 5760 5850 5940 -- -- -- -- -- -- -- -- -- -- -- --
39000 481 5925 6060 6195 6330 6465 6600 -- -- -- -- -- -- -- -- -- --
37000 481 6380 6480 6580 6680 6780 6880 6980 7080 -- -- -- -- -- -- -- --
35000 481 6744 6876 7008 7140 7272 7141 7273 7142 7800 7890 7980 -- -- -- -- --
33000 486 7416 7500 7584 7668 7752 7836 7920 8028 8136 8244 8352 8460 8568 -- -- --
31000 480 7416 7524 7632 7740 7848 7956 8064 8172 8280 8376 8472 8568 8664 8760 8810 --
29000 465 7296 7380 7464 7548 7632 7716 7800 7920 8040 8160 8280 8400 8520 8640 8730 8850
27000 452 7170 7275 7380 7488 7596 7704 7812 7920 8030 8140 8270 8410 8520 8580 8650 8800
[DESCENT]
; ALT TAS ROD FUEL
1000 165 800 8400
3000 200 1000 3400
5000 245 900 3200
7000 272 1000 3200
9000 280 1000 3200
11000 341 2000 3200
13000 352 2100 3200
15000 362 2200 3200
17000 373 2400 3200
19000 384 2400 3200
21000 390 2500 3200
23000 408 2700 3200
25000 420 2900 3200
27000 433 3000 3200
29000 449 3200 3200
31000 462 3500 3200
33000 480 3900 3200
35000 480 4000 3200
37000 480 4200 3200
39000 480 4400 3200
41000 480 4500 3200
43000 480 4500 3200
[Altitude]
;--- Altitude Capability - Lowered by 5000 lbs.
; Altiude Max GrossWt
30000 340000
31000 320000
32000 315000
33000 310000
34000 294000
35000 277400
36000 263000
37000 250900
38000 239000
39000 227000
40000 216000
41000 205000
42000 195000
43000 185000
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