Generating manoeuvre sequence from 'range' calculations...
Summary of segments in the sequence:
-----------------------------------------------
Seg. Speed mode Thrust mode Stop condition
1. v3 at-%mto to alt 1500.
2. specify-cas at-%mcl to alt 10000.
3. specify-cas at-%mcl to mach 0.83
4. same-mach at-%mcl to alt 37000.
5. specify-mach level-cruise to next stepup
6. same-mach at-%mcl to dalt ±4000.
7. same-mach level-cruise to mass 304318.
8. specify-mach at-idle to cas 277.
9. specify-cas at-idle to alt 10000.
10. specify-cas at-idle to alt 1500.
11. vapp match-grad to alt 50.
-----------------------------------------------
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Manoeuvre segment 1 starts at:
Initial Mass 476000. lb. (CL 1.18 wimpress)
Initial Altitude 35. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 175. kts (V3)
Flaps 10 deg.
Undercarriage up
All eng.operative
Thrust per engine 50066. lbf. (100% MTO)
Climb/Descent rate 2566. feet/min
Flightpath angle 8.2 deg. (grad.14.44%)
True airspeed 175. kts
Fuel Flow rate 37128. lb/hr
NOx emission rate 809.4 lb/hr
HC emission rate 1.109 lb/hr
CO emission rate 2.4 lb/hr
L/D ratio 16.58
Total aircraft drag 28710. lbf.
Segment 1 ends at total time = 0.6 mins, endmass = 475647.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +1465. +34.7 +0.00 +352.7 +7.62 +0.011 +0.02
Final : 1500. 34.7 0.00 352.7 7.62 0.011 0.02
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
35. 0.0 0.000 0.0 50066. 175. 0.265 2566. 28710. 175.
198. 3.8 0.000 39.2 49880. 175. 0.266 2559. 28709. 176.
361. 7.6 0.000 78.5 49695. 175. 0.267 2551. 28707. 176.
523. 11.5 0.000 117.7 49509. 175. 0.268 2543. 28706. 177.
686. 15.3 0.000 156.9 49323. 175. 0.268 2535. 28705. 177.
849. 19.2 0.000 196.1 49138. 175. 0.269 2527. 28703. 178.
1012. 23.0 0.000 235.2 48953. 175. 0.270 2519. 28702. 178.
1174. 26.9 0.000 274.4 48768. 175. 0.271 2511. 28701. 178.
1337. 30.8 0.000 313.6 48583. 175. 0.271 2503. 28700. 179.
1500. 34.7 0.000 352.7 48398. 175. 0.272 2495. 28698. 179.
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Acceleration to 250.kts in level flight at 1500.feet =0.14g:
Time +28.1 sec, Dist +1.70 n.miles, Fuelburn +282.1 lb.
NOx +6.15 lb., HC +0.009 lb., CO +0.018 lb.
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Manoeuvre segment 2 starts at:
Initial Mass 475365. lb. (CL 0.58 wimpress)
Initial Altitude 1500. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 250. kts (input)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 38146. lbf. (100% MCL)
Climb/Descent rate 2726. feet/min
Flightpath angle 6.0 deg. (grad.10.54%)
True airspeed 255. kts
Fuel Flow rate 32246. lb/hr
NOx emission rate 606.6 lb/hr
HC emission rate 1.135 lb/hr
CO emission rate 1.7 lb/hr
L/D ratio 21.52
Total aircraft drag 22088. lbf.
Segment 2 ends at total time = 4.5 mins, endmass = 473674.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +8500. +207. +15.63 +1690.8 +30.56 +0.067 +0.27
Final : 10000. 270. 17.33 2325.6 44.33 0.086 0.31
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
1500. 62.8 1.699 634.8 38146. 250. 0.388 2726. 22088. 255.
1947. 72.7 2.403 723.0 37751. 250. 0.391 2701. 22088. 257.
2395. 82.7 3.118 811.3 37357. 250. 0.394 2675. 22087. 259.
2842. 92.8 3.844 899.6 36966. 250. 0.397 2650. 22087. 260.
3289. 102.9 4.583 987.9 36575. 250. 0.400 2624. 22087. 262.
3737. 113.2 5.333 1076.3 36187. 250. 0.404 2598. 22087. 264.
4184. 123.6 6.096 1164.7 35800. 250. 0.407 2572. 22087. 265.
4632. 134.1 6.872 1253.3 35415. 250. 0.410 2545. 22087. 267.
5079. 144.7 7.660 1341.9 35032. 250. 0.413 2519. 22087. 269.
5526. 155.4 8.463 1430.6 34651. 250. 0.417 2492. 22086. 270.
5974. 166.3 9.279 1519.4 34271. 250. 0.420 2465. 22086. 272.
6421. 177.2 10.11 1608.4 33893. 250. 0.424 2438. 22086. 274.
6868. 188.3 10.96 1697.5 33518. 250. 0.427 2411. 22086. 276.
7316. 199.5 11.82 1786.7 33144. 250. 0.431 2383. 22085. 278.
7763. 210.8 12.69 1876.1 32772. 250. 0.434 2355. 22085. 279.
8211. 222.3 13.58 1965.6 32402. 250. 0.438 2328. 22085. 281.
8658. 233.9 14.49 2055.3 32034. 250. 0.441 2300. 22084. 283.
9105. 245.6 15.42 2145.2 31669. 250. 0.445 2272. 22084. 285.
9553. 257.5 16.36 2235.3 31305. 250. 0.449 2244. 22083. 287.
10000. 269.5 17.33 2325.6 30965. 250. 0.452 2218. 22082. 289.
-----------------------------------------------------------------------------
Acceleration to 277.kts in level flight at 10000.feet =0.09g:
Time +16.9 sec, Dist +1.43 n.miles, Fuelburn +139.3 lb.
NOx +2.68 lb., HC +0.005 lb., CO +0.009 lb.
-----------------------------------------------------------------------------
Manoeuvre segment 3 starts at:
Initial Mass 473535. lb. (CL 0.48 wimpress)
Initial Altitude 10000. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 277. kts (input)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 29819. lbf. (100% MCL)
Climb/Descent rate 2249. feet/min
Flightpath angle 4.0 deg. (grad.6.96%)
True airspeed 319. kts
Fuel Flow rate 27212. lb/hr
NOx emission rate 479.0 lb/hr
HC emission rate 1.180 lb/hr
CO emission rate 6.6 lb/hr
L/D ratio 21.19
Total aircraft drag 22348. lbf.
Segment 3 ends at total time = 26.1 mins, endmass = 466643.lb.(1.37g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +25738. +1280. +145.24 +6892.4 +103.13 +0.441 +5.96
Final : 35738. 1567. 164.00 9357.3 150.14 0.533 6.28
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
10000. 286.5 18.76 2464.9 29819. 277. 0.500 2249. 22348. 319.
11355. 323.3 22.06 2739.5 28823. 277. 0.512 2162. 22334. 326.
12709. 361.7 25.56 3017.2 27845. 277. 0.525 2074. 22318. 332.
14064. 401.8 29.30 3298.6 26888. 277. 0.539 1985. 22301. 339.
15418. 443.7 33.28 3584.2 25952. 277. 0.553 1895. 22282. 346.
16773. 487.7 37.55 3874.8 25037. 277. 0.567 1805. 22262. 353.
18128. 533.9 42.13 4171.3 24138. 277. 0.582 1714. 22240. 360.
19482. 582.6 47.06 4474.9 23256. 277. 0.597 1622. 22217. 368.
20837. 634.2 52.38 4786.6 22392. 277. 0.613 1530. 22192. 375.
22192. 689.1 58.16 5108.0 21547. 277. 0.629 1437. 22165. 383.
23546. 747.6 64.45 5440.6 20722. 277. 0.646 1344. 22136. 391.
24901. 810.1 71.32 5785.5 19980. 277. 0.663 1259. 22105. 400.
26255. 876.9 78.82 6143.9 19266. 277. 0.681 1177. 22072. 408.
27610. 948.6 87.04 6517.6 18562. 277. 0.700 1093. 22037. 417.
28965. 1026. 96.11 6909.2 17869. 277. 0.719 1008. 21999. 426.
30319. 1111. 106.22 7322.8 17158. 277. 0.739 919. 21949. 435.
31674. 1205. 117.70 7765.8 16389. 277. 0.760 818. 21897. 444.
33028. 1310. 130.89 8246.6 15683. 277. 0.781 725. 21844. 454.
34383. 1430. 146.15 8772.7 15045. 277. 0.803 639. 21793. 464.
35738. 1567. 164.00 9357.3 14476. 277. 0.825 555. 21843. 474.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 4 starts at:
Initial Mass 466643. lb. (CL 0.53 wimpress)
Initial Altitude 35738. feet (1.37g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 277. kts (fixed Mach 0.825)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 14476. lbf. (100% MCL)
Climb/Descent rate 805. feet/min
Flightpath angle 1.0 deg. (grad.1.68%)
True airspeed 474. kts
Fuel Flow rate 15189. lb/hr
NOx emission rate 199.2 lb/hr
HC emission rate 1.255 lb/hr
CO emission rate 21.1 lb/hr
L/D ratio 21.37
Total aircraft drag 21835. lbf.
Segment 4 ends at total time = 28.0 mins, endmass = 466184.lb.(1.29g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +1262. +112. +14.68 +458.6 +5.93 +0.039 +0.66
Final : 37000. 1678. 178.67 9816.0 156.07 0.572 6.94
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
35738. 1567. 164.00 9357.3 14476. 277. 0.825 805. 21835. 474.
35804. 1572. 164.65 9378.3 14451. 276. 0.825 800. 21831. 474.
35871. 1577. 165.31 9399.3 14426. 276. 0.825 794. 21827. 474.
35937. 1582. 165.97 9420.4 14400. 276. 0.825 789. 21823. 474.
36003. 1587. 166.64 9441.7 14375. 275. 0.825 783. 21819. 474.
36070. 1592. 167.31 9463.0 14350. 275. 0.825 778. 21816. 473.
36136. 1597. 168.02 9485.6 14311. 274. 0.825 700. 21813. 473.
36203. 1603. 168.78 9509.4 14267. 274. 0.825 691. 21811. 473.
36269. 1609. 169.54 9533.5 14222. 273. 0.825 682. 21810. 473.
36336. 1615. 170.31 9557.8 14178. 273. 0.825 673. 21808. 473.
36402. 1621. 171.10 9582.4 14134. 273. 0.825 664. 21807. 473.
36469. 1627. 171.89 9607.2 14090. 272. 0.825 655. 21805. 473.
36535. 1633. 172.70 9632.3 14045. 272. 0.825 646. 21804. 473.
36601. 1639. 173.51 9657.7 14001. 271. 0.825 637. 21804. 473.
36668. 1645. 174.34 9683.3 13957. 271. 0.825 628. 21803. 473.
36734. 1652. 175.18 9709.2 13912. 270. 0.825 619. 21802. 473.
36801. 1658. 176.04 9735.4 13868. 270. 0.825 610. 21802. 473.
36867. 1665. 176.90 9762.0 13824. 270. 0.825 601. 21802. 473.
36934. 1672. 177.78 9788.8 13780. 269. 0.825 592. 21802. 473.
37000. 1678. 178.67 9816.0 13735. 269. 0.825 583. 21802. 473.
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Acceleration to 278.kts in level flight at 37000.feet =0.01g:
Time +68.5 sec, Dist +9.27 n.miles, Fuelburn +279.3 lb.
NOx +3.60 lb., HC +0.024 lb., CO +0.376 lb.
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Manoeuvre segment 5 starts at:
Initial Mass 465905. lb. (CL 0.53 wimpress)
Initial Altitude 37000. feet (1.19g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 278. kts (input Mach 0.850)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 11183. lbf. (level cruise) =87.6%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 488. kts
Fuel Flow rate 11803. lb/hr
NOx emission rate 141.6 lb/hr
HC emission rate 1.191 lb/hr
CO emission rate 28.0 lb/hr
L/D ratio 20.83
Total aircraft drag 22366. lbf.
Segment 5 ends at total time = 364.1 mins, endmass = 404133.lb.(1.37g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +20099. +2721.98 +61771.9 +727.84 +6.479 +162.44
Final : 37000. 21846. 2909.93 71867.2 887.52 7.075 169.76
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
37000. 1747. 187.95 10095.2 11183. 278. 0.850 0. 22366. 488.
37000. 2742. 322.71 13346.4 11105. 278. 0.850 0. 22209. 488.
37000. 3744. 458.42 16597.6 11027. 278. 0.850 0. 22054. 488.
37000. 4753. 595.08 19848.7 10950. 278. 0.850 0. 21900. 488.
37000. 5769. 732.69 23099.9 10874. 278. 0.850 0. 21748. 488.
37000. 6792. 871.23 26351.0 10799. 278. 0.850 0. 21597. 488.
37000. 7822. 1010.72 29602.2 10724. 278. 0.850 0. 21449. 488.
37000. 8859. 1151.15 32853.3 10651. 278. 0.850 0. 21301. 488.
37000. 9903. 1292.52 36104.5 10578. 278. 0.850 0. 21156. 488.
37000. 10954. 1434.84 39355.6 10506. 278. 0.850 0. 21012. 488.
37000. 12012. 1578.10 42606.8 10435. 278. 0.850 0. 20869. 488.
37000. 13076. 1722.30 45857.9 10364. 278. 0.850 0. 20729. 488.
37000. 14148. 1867.44 49109.1 10295. 278. 0.850 0. 20589. 488.
37000. 15227. 2013.53 52360.3 10226. 278. 0.850 0. 20451. 488.
37000. 16312. 2160.56 55611.4 10157. 278. 0.850 0. 20315. 488.
37000. 17405. 2308.54 58862.6 10090. 278. 0.850 0. 20180. 488.
37000. 18505. 2457.47 62113.7 10023. 278. 0.850 0. 20046. 488.
37000. 19611. 2607.34 65364.9 9957. 278. 0.850 0. 19914. 488.
37000. 20725. 2758.16 68616.0 9892. 278. 0.850 0. 19783. 488.
37000. 21846. 2909.93 71867.2 9827. 278. 0.850 0. 19654. 488.
-----------------------------------------------------------------------------
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Manoeuvre segment 6 starts at:
Initial Mass 404133. lb. (CL 0.46 wimpress)
Initial Altitude 37000. feet (1.37g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 278. kts (fixed Mach 0.850)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 13724. lbf. (100% MCL)
Climb/Descent rate 952. feet/min
Flightpath angle 1.1 deg. (grad.1.93%)
True airspeed 488. kts
Fuel Flow rate 14680. lb/hr
NOx emission rate 189.5 lb/hr
HC emission rate 1.250 lb/hr
CO emission rate 19.8 lb/hr
L/D ratio 20.56
Total aircraft drag 19654. lbf.
Segment 6 ends at total time = 371.0 mins, endmass = 402646.lb.(1.13g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +4000. +411. +55.73 +1486.7 +18.08 +0.143 +2.33
Final : 41000. 22257. 2965.65 73353.9 905.59 7.218 172.09
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
37000. 21846. 2909.93 71867.2 13724. 278. 0.850 952. 19654. 488.
37211. 21859. 2911.75 71921.9 13583. 277. 0.850 921. 19632. 488.
37421. 21873. 2913.65 71978.0 13442. 275. 0.850 889. 19612. 488.
37632. 21888. 2915.61 72035.5 13300. 274. 0.850 856. 19594. 488.
37842. 21903. 2917.64 72094.6 13159. 273. 0.850 824. 19579. 488.
38053. 21918. 2919.76 72155.5 13018. 271. 0.850 791. 19566. 488.
38263. 21935. 2921.97 72218.2 12876. 270. 0.850 758. 19555. 488.
38474. 21952. 2924.28 72283.1 12735. 269. 0.850 724. 19546. 488.
38684. 21970. 2926.70 72350.3 12594. 267. 0.850 691. 19540. 488.
38895. 21988. 2929.24 72420.0 12452. 266. 0.850 657. 19536. 488.
39105. 22008. 2931.92 72492.7 12311. 265. 0.850 622. 19535. 488.
39316. 22029. 2934.75 72568.6 12170. 263. 0.850 588. 19535. 488.
39526. 22051. 2937.75 72648.2 12028. 262. 0.850 553. 19539. 488.
39737. 22075. 2940.95 72732.0 11887. 261. 0.850 518. 19545. 488.
39947. 22100. 2944.37 72820.7 11746. 260. 0.850 482. 19553. 488.
40158. 22127. 2948.04 72914.6 11625. 258. 0.850 451. 19564. 488.
40368. 22156. 2951.96 73014.0 11511. 257. 0.850 422. 19578. 488.
40579. 22187. 2956.17 73119.5 11397. 256. 0.850 392. 19594. 488.
40789. 22221. 2960.71 73232.4 11284. 255. 0.850 362. 19612. 488.
41000. 22257. 2965.65 73353.9 11170. 253. 0.850 332. 19634. 488.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 7 starts at:
Initial Mass 402646. lb. (CL 0.55 wimpress)
Initial Altitude 41000. feet (1.13g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 253. kts (fixed Mach 0.850)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 9816. lbf. (level cruise) =94.7%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 488. kts
Fuel Flow rate 10379. lb/hr
NOx emission rate 115.0 lb/hr
HC emission rate 1.221 lb/hr
CO emission rate 26.5 lb/hr
L/D ratio 20.51
Total aircraft drag 19632. lbf.
Segment 7 ends at total time = 1016.4 mins, endmass = 304318.lb.(1.50g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +38726. +5244.65 +98328.5 +1050.88 +12.513 +312.37
Final : 41000. 60983. 8210.30 171682.4 1956.48 19.731 484.45
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
41000. 22257. 2965.65 73353.9 9816. 253. 0.850 0. 19632. 488.
41000. 24065. 3210.52 78529.1 9682. 253. 0.850 0. 19363. 488.
41000. 25899. 3458.92 83704.3 9550. 253. 0.850 0. 19100. 488.
41000. 27760. 3710.84 88879.4 9422. 253. 0.850 0. 18843. 488.
41000. 29646. 3966.26 94054.6 9296. 253. 0.850 0. 18591. 488.
41000. 31557. 4225.15 99229.8 9172. 253. 0.850 0. 18345. 488.
41000. 33494. 4487.49 104405.0 9052. 253. 0.850 0. 18104. 488.
41000. 35457. 4753.27 109580.2 8934. 253. 0.850 0. 17867. 488.
41000. 37445. 5022.48 114755.4 8818. 253. 0.850 0. 17636. 488.
41000. 39458. 5295.12 119930.5 8705. 253. 0.850 0. 17410. 488.
41000. 41496. 5571.18 125105.7 8594. 253. 0.850 0. 17188. 488.
41000. 43560. 5850.67 130280.9 8485. 253. 0.850 0. 16971. 488.
41000. 45649. 6133.59 135456.1 8379. 253. 0.850 0. 16758. 488.
41000. 47763. 6419.95 140631.3 8275. 253. 0.850 0. 16549. 488.
41000. 49903. 6709.74 145806.5 8172. 253. 0.850 0. 16345. 488.
41000. 52068. 7002.98 150981.7 8072. 253. 0.850 0. 16144. 488.
41000. 54259. 7299.65 156156.8 7974. 253. 0.850 0. 15948. 488.
41000. 56475. 7599.76 161332.0 7878. 253. 0.850 0. 15756. 488.
41000. 58716. 7903.31 166507.2 7783. 253. 0.850 0. 15567. 488.
41000. 60983. 8210.30 171682.4 7691. 253. 0.850 0. 15382. 488.
-----------------------------------------------------------------------------
Deceleration to 245.kts in level flight at 41000.feet =-0.05g:
Time +14.1 sec, Dist +1.86 n.miles, Fuelburn +3.1 lb.
NOx +0.01 lb., HC +0.008 lb., CO +0.199 lb.
-----------------------------------------------------------------------------
Manoeuvre segment 8 starts at:
Initial Mass 304314. lb. (CL 0.44 wimpress)
Initial Altitude 41000. feet (1.64g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 245. kts (input Mach 0.825)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine -502. lbf. (idle)
Climb/Descent rate -2525. feet/min
Flightpath angle -3.0 deg. (grad.-5.27%)
True airspeed 473. kts
Fuel Flow rate 793. lb/hr
NOx emission rate 1.5 lb/hr
HC emission rate 2.072 lb/hr
CO emission rate 50.7 lb/hr
L/D ratio 20.26
Total aircraft drag 15024. lbf.
Segment 8 ends at total time = 1018.6 mins, endmass = 304287.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -5262. +120. +15.71 +27.8 +0.05 +0.065 +1.59
Final : 35738. 61117. 8227.88 171713.3 1956.54 19.804 486.24
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
41000. 60997. 8212.16 171685.5 -502. 245. 0.825 -2525. 15024. 473.
40723. 61004. 8213.02 171687.0 -509. 247. 0.825 -2533. 15063. 473.
40446. 61010. 8213.89 171688.4 -516. 248. 0.825 -2542. 15105. 473.
40169. 61017. 8214.74 171689.9 -522. 250. 0.825 -2551. 15149. 473.
39892. 61023. 8215.60 171691.3 -529. 251. 0.825 -2560. 15195. 473.
39615. 61030. 8216.45 171692.8 -537. 253. 0.825 -2570. 15243. 473.
39338. 61036. 8217.30 171694.2 -545. 255. 0.825 -2581. 15293. 473.
39061. 61043. 8218.14 171695.7 -553. 256. 0.825 -2592. 15345. 473.
38784. 61049. 8218.99 171697.2 -561. 258. 0.825 -2603. 15400. 473.
38507. 61055. 8219.82 171698.7 -570. 260. 0.825 -2614. 15456. 473.
38230. 61062. 8220.66 171700.1 -578. 261. 0.825 -2626. 15515. 473.
37953. 61068. 8221.49 171701.6 -586. 263. 0.825 -2638. 15575. 473.
37676. 61074. 8222.31 171703.1 -594. 265. 0.825 -2650. 15638. 473.
37399. 61081. 8223.14 171704.6 -602. 266. 0.825 -2663. 15703. 473.
37123. 61087. 8223.95 171706.1 -610. 268. 0.825 -2676. 15770. 473.
36846. 61093. 8224.77 171707.5 -618. 270. 0.825 -2690. 15839. 473.
36569. 61099. 8225.58 171709.0 -626. 272. 0.825 -2703. 15910. 473.
36292. 61105. 8226.39 171710.5 -634. 273. 0.825 -2718. 15984. 473.
36015. 61111. 8227.15 171711.9 -642. 275. 0.825 -3006. 16062. 474.
35738. 61117. 8227.88 171713.3 -653. 277. 0.825 -3029. 16147. 474.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 9 starts at:
Initial Mass 304287. lb. (CL 0.34 wimpress)
Initial Altitude 35738. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 277. kts (input)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine -653. lbf. (idle)
Climb/Descent rate -2088. feet/min
Flightpath angle -2.5 deg. (grad.-4.35%)
True airspeed 474. kts
Fuel Flow rate 888. lb/hr
NOx emission rate 1.7 lb/hr
HC emission rate 1.851 lb/hr
CO emission rate 45.3 lb/hr
L/D ratio 18.84
Total aircraft drag 16147. lbf.
Segment 9 ends at total time = 1031.9 mins, endmass = 304030.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -25738. +795. +85.68 +256.4 +0.58 +0.417 +10.21
Final : 10000. 61912. 8313.56 171969.6 1957.12 20.222 496.45
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
35738. 61117. 8227.88 171713.3 -653. 277. 0.825 -2088. 16147. 474.
34383. 61156. 8232.96 171723.0 -673. 277. 0.803 -2079. 16215. 464.
33028. 61195. 8237.96 171733.1 -690. 277. 0.781 -2068. 16281. 454.
31674. 61234. 8242.87 171743.6 -704. 277. 0.760 -2056. 16349. 444.
30319. 61274. 8247.72 171754.4 -716. 277. 0.739 -2043. 16414. 435.
28965. 61314. 8252.49 171765.5 -736. 277. 0.719 -2030. 16477. 426.
27610. 61354. 8257.19 171777.1 -756. 277. 0.700 -2017. 16530. 417.
26255. 61395. 8261.82 171789.1 -774. 277. 0.681 -2002. 16580. 408.
24901. 61435. 8266.40 171801.4 -790. 277. 0.663 -1985. 16626. 400.
23546. 61476. 8270.91 171814.2 -815. 277. 0.646 -1970. 16669. 391.
22192. 61518. 8275.36 171827.5 -833. 277. 0.629 -1953. 16709. 383.
20837. 61560. 8279.77 171841.2 -847. 277. 0.613 -1935. 16746. 375.
19482. 61602. 8284.12 171855.4 -857. 277. 0.597 -1915. 16780. 368.
18128. 61645. 8288.44 171870.1 -864. 277. 0.582 -1894. 16811. 360.
16773. 61688. 8292.71 171885.3 -868. 277. 0.567 -1872. 16840. 353.
15418. 61731. 8296.95 171901.1 -869. 277. 0.553 -1849. 16866. 346.
14064. 61776. 8301.15 171917.4 -878. 277. 0.539 -1828. 16890. 339.
12709. 61820. 8305.32 171934.3 -888. 277. 0.525 -1806. 16912. 332.
11355. 61866. 8309.45 171951.7 -894. 277. 0.512 -1784. 16931. 326.
10000. 61912. 8313.56 171969.6 -897. 277. 0.500 -1761. 16949. 319.
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Deceleration to 250.kts in level flight at 10000.feet =-0.06g:
Time +27.2 sec, Dist +2.29 n.miles, Fuelburn +10.7 lb.
NOx +0.03 lb., HC +0.014 lb., CO +0.350 lb.
-----------------------------------------------------------------------------
Manoeuvre segment 10 starts at:
Initial Mass 304020. lb. (CL 0.38 wimpress)
Initial Altitude 10000. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 250. kts (input)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine -700. lbf. (idle)
Climb/Descent rate -1475. feet/min
Flightpath angle -2.9 deg. (grad.-5.04%)
True airspeed 289. kts
Fuel Flow rate 1408. lb/hr
NOx emission rate 3.4 lb/hr
HC emission rate 1.883 lb/hr
CO emission rate 46.1 lb/hr
L/D ratio 19.48
Total aircraft drag 15610. lbf.
Segment 10 ends at total time = 1038.4 mins, endmass = 303868.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -8500. +362. +27.30 +152.1 +0.38 +0.190 +4.65
Final : 1500. 62301. 8343.16 172132.4 1957.53 20.426 501.45
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
10000. 61939. 8315.85 171980.3 -700. 250. 0.452 -1475. 15610. 289.
9553. 61957. 8317.31 171987.5 -702. 250. 0.449 -1468. 15611. 287.
9105. 61975. 8318.77 171994.7 -705. 250. 0.445 -1461. 15612. 285.
8658. 61994. 8320.22 172002.1 -708. 250. 0.441 -1454. 15613. 283.
8211. 62012. 8321.67 172009.5 -710. 250. 0.438 -1447. 15613. 281.
7763. 62031. 8323.12 172017.0 -713. 250. 0.434 -1440. 15614. 279.
7316. 62049. 8324.56 172024.6 -715. 250. 0.431 -1433. 15614. 278.
6868. 62068. 8326.01 172032.3 -716. 250. 0.427 -1427. 15615. 276.
6421. 62087. 8327.45 172040.1 -718. 250. 0.424 -1420. 15615. 274.
5974. 62106. 8328.88 172048.0 -719. 250. 0.420 -1413. 15615. 272.
5526. 62125. 8330.32 172056.0 -720. 250. 0.417 -1405. 15615. 270.
5079. 62144. 8331.75 172064.1 -721. 250. 0.413 -1398. 15615. 269.
4632. 62164. 8333.18 172072.3 -722. 250. 0.410 -1391. 15615. 267.
4184. 62183. 8334.61 172080.6 -723. 250. 0.407 -1384. 15615. 265.
3737. 62202. 8336.04 172089.0 -723. 250. 0.404 -1377. 15614. 264.
3289. 62222. 8337.47 172097.4 -723. 250. 0.400 -1370. 15614. 262.
2842. 62241. 8338.89 172106.0 -723. 250. 0.397 -1363. 15613. 260.
2395. 62261. 8340.32 172114.7 -723. 250. 0.394 -1356. 15613. 259.
1947. 62281. 8341.74 172123.5 -723. 250. 0.391 -1349. 15612. 257.
1500. 62301. 8343.16 172132.4 -722. 250. 0.388 -1342. 15611. 255.
-----------------------------------------------------------------------------
Deceleration to 123.kts in level flight at 1500.feet =-0.19g:
Time +36.5 sec, Dist +1.82 n.miles, Fuelburn +16.2 lb.
NOx +0.04 lb., HC +0.019 lb., CO +0.467 lb.
-----------------------------------------------------------------------------
Manoeuvre segment 11 starts at:
Initial Mass 303851. lb. (CL 1.54 wimpress)
Initial Altitude 1500. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 123. kts (Vapp)
Flaps 35 deg.
Undercarriage down
All eng.operative
Thrust per engine 11055. lbf. (match grad.) =23.1%MCL
Climb/Descent rate -666. feet/min
Flightpath angle -3.0 deg. (grad.-5.24%)
True airspeed 126. kts
Fuel Flow rate 8864. lb/hr
NOx emission rate 84.2 lb/hr
HC emission rate 2.383 lb/hr
CO emission rate 63.2 lb/hr
L/D ratio 7.92
Total aircraft drag 38345. lbf.
Segment 11 ends at total time = 1041.2 mins, endmass = 303524.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -1450. +132. +0.00 +327.8 +3.11 +0.087 +2.31
Final : 50. 62470. 8344.97 172476.4 1960.67 20.532 504.23
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
1500. 62338. 0.000 172148.6 11055. 123. 0.191 -666. 38345. 126.
1339. 62352. 0.000 172184.5 11055. 123. 0.190 -664. 38341. 125.
1178. 62367. 0.000 172220.4 11055. 123. 0.190 -663. 38337. 125.
1017. 62381. 0.000 172256.5 11055. 123. 0.189 -661. 38332. 125.
856. 62396. 0.000 172292.8 11054. 123. 0.189 -660. 38328. 124.
694. 62411. 0.000 172329.2 11054. 123. 0.188 -658. 38324. 124.
533. 62425. 0.000 172365.8 11054. 123. 0.187 -656. 38319. 124.
372. 62440. 0.000 172402.5 11054. 123. 0.187 -655. 38315. 124.
211. 62455. 0.000 172439.4 11053. 123. 0.186 -653. 38311. 123.
50. 62470. 0.000 172476.4 11053. 123. 0.186 -652. 38306. 123.
-----------------------------------------------------------------------------
Summary of segments in the sequence:
-----------------------------------------------
Seg. Speed mode Thrust mode Stop condition
1. v3 at-%mto to alt 1500.
2. specify-cas at-%mcl to alt 10000.
3. specify-cas at-%mcl to mach 0.83
4. same-mach at-%mcl to alt 37000.
5. specify-mach level-cruise to next stepup
6. same-mach at-%mcl to dalt ±4000.
7. same-mach level-cruise to mass 304318.
8. specify-mach at-idle to cas 277.
9. specify-cas at-idle to alt 10000.
10. specify-cas at-idle to alt 1500.
11. vapp match-grad to alt 50.
-----------------------------------------------