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Loading manoeuvre sequence "sample-g550m87step"...
Sequence created with "Gulfstream G550" (12:44,Wed.Feb.15.2006)...done
Summary of segments in the sequence:
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Seg. Speed mode Thrust mode Stop condition
1. v3 at-%mto to alt 1500.
2. specify-cas at-%mcl to alt 10000.
3. same-cas at-%mcl to mach 0.82
4. same-mach at-%mcl to alt 35000.
5. specify-mach level-cruise to next stepup
6. same-mach at-%mcl to dalt ±2000.
7. same-mach level-cruise to next stepup
8. same-mach at-%mcl to dalt ±2000.
9. same-mach level-cruise to next stepup
10. same-mach at-%mcl to dalt ±2000.
11. same-mach level-cruise to next stepup
12. same-mach at-%mcl to dalt ±2000.
13. same-mach level-cruise to next stepup
14. same-mach at-%mcl to dalt ±2000.
15. same-mach level-cruise to mass 53168.
16. specify-mach at-idle to cas 300.
17. same-cas at-idle to alt 10000.
18. specify-cas at-idle to alt 1500.
19. vapp match-grad to alt 50.
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Manoeuvre segment 1 starts at:
Initial Mass 90739. lb. (CL 0.93 trapezoidal)
Initial Altitude 35. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 159. kts (V3)
Flaps 15 deg.
Undercarriage up
All eng.operative
Thrust per engine 12381. lbf. (100% MTO)
Climb/Descent rate 3128. feet/min
Flightpath angle 11.0 deg. (grad.19.43%)
True airspeed 159. kts
Fuel Flow rate 12520. lb/hr
NOx emission rate 270.4 lb/hr
HC emission rate 0.251 lb/hr
CO emission rate 14.0 lb/hr
L/D ratio 13.83
Total aircraft drag 6560. lbf.
Segment 1 ends at total time = 0.5 mins, endmass = 90642.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +1465. +28.4 +0.00 +97.3 +2.09 +0.002 +0.11
Final : 1500. 28.4 0.00 97.3 2.09 0.002 0.11
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
35. 0.0 0.000 0.0 12381. 159. 0.240 3128. 6560. 159.
198. 3.1 0.000 10.9 12338. 159. 0.241 3121. 6560. 159.
361. 6.3 0.000 21.7 12296. 159. 0.242 3113. 6559. 160.
523. 9.4 0.000 32.5 12253. 159. 0.242 3106. 6558. 160.
686. 12.5 0.000 43.3 12211. 159. 0.243 3098. 6557. 160.
849. 15.7 0.000 54.2 12168. 159. 0.244 3090. 6556. 161.
1012. 18.9 0.000 65.0 12126. 159. 0.244 3083. 6555. 161.
1174. 22.0 0.000 75.7 12084. 159. 0.245 3075. 6555. 162.
1337. 25.2 0.000 86.5 12041. 159. 0.246 3067. 6554. 162.
1500. 28.4 0.000 97.3 11999. 159. 0.247 3059. 6553. 162.
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Acceleration to 300.kts in level flight at 1500.feet =0.19g:
Time +40.4 sec, Dist +2.67 n.miles, Fuelburn +138.1 lb.
NOx +3.05 lb., HC +0.003 lb., CO +0.159 lb.
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Manoeuvre segment 2 starts at:
Initial Mass 90504. lb. (CL 0.26 trapezoidal)
Initial Altitude 1500. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 300. kts (input)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 8654. lbf. (100% MCL)
Climb/Descent rate 3504. feet/min
Flightpath angle 6.4 deg. (grad.11.30%)
True airspeed 306. kts
Fuel Flow rate 10700. lb/hr
NOx emission rate 202.5 lb/hr
HC emission rate 0.219 lb/hr
CO emission rate 11.4 lb/hr
L/D ratio 15.33
Total aircraft drag 5905. lbf.
Segment 2 ends at total time = 3.8 mins, endmass = 90070.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +8500. +158. +14.30 +433.5 +7.95 +0.009 +0.48
Final : 10000. 227. 16.97 668.9 13.08 0.014 0.75
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
1500. 68.8 2.674 235.4 8654. 300. 0.465 3504. 5905. 306.
1947. 76.5 3.330 258.2 8583. 300. 0.469 3479. 5903. 308.
2395. 84.3 3.995 280.9 8513. 300. 0.473 3453. 5901. 310.
2842. 92.1 4.669 303.6 8443. 300. 0.476 3427. 5898. 312.
3289. 99.9 5.353 326.3 8373. 300. 0.480 3401. 5896. 314.
3737. 107.8 6.046 349.0 8304. 300. 0.484 3375. 5894. 316.
4184. 115.8 6.749 371.7 8234. 300. 0.488 3348. 5892. 318.
4632. 123.9 7.462 394.5 8165. 300. 0.492 3321. 5889. 320.
5079. 132.0 8.186 417.2 8095. 300. 0.495 3294. 5887. 322.
5526. 140.2 8.921 439.9 8020. 300. 0.499 3262. 5885. 324.
5974. 148.5 9.667 462.7 7945. 300. 0.503 3230. 5882. 326.
6421. 156.8 10.43 485.4 7870. 300. 0.507 3198. 5879. 328.
6868. 165.2 11.20 508.3 7796. 300. 0.511 3166. 5877. 330.
7316. 173.8 11.98 531.1 7722. 300. 0.516 3134. 5874. 332.
7763. 182.4 12.78 554.0 7649. 300. 0.520 3102. 5871. 334.
8211. 191.1 13.59 576.9 7576. 300. 0.524 3070. 5868. 337.
8658. 199.9 14.41 599.8 7504. 300. 0.528 3038. 5865. 339.
9105. 208.7 15.25 622.8 7432. 300. 0.532 3005. 5862. 341.
9553. 217.7 16.11 645.8 7361. 300. 0.537 2973. 5858. 343.
10000. 226.8 16.97 668.9 7290. 300. 0.541 2941. 5855. 345.
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Manoeuvre segment 3 starts at:
Initial Mass 90070. lb. (CL 0.27 trapezoidal)
Initial Altitude 10000. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 300. kts (fixed)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 7290. lbf. (100% MCL)
Climb/Descent rate 2941. feet/min
Flightpath angle 4.8 deg. (grad.8.41%)
True airspeed 345. kts
Fuel Flow rate 9107. lb/hr
NOx emission rate 160.1 lb/hr
HC emission rate 0.211 lb/hr
CO emission rate 10.6 lb/hr
L/D ratio 15.38
Total aircraft drag 5855. lbf.
Segment 3 ends at total time = 15.0 mins, endmass = 88756.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +21839. +673. +78.21 +1313.7 +19.69 +0.037 +1.78
Final : 31839. 900. 95.19 1982.6 32.77 0.051 2.53
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
10000. 226.8 16.97 668.9 7290. 300. 0.541 2941. 5855. 345.
11149. 250.6 19.28 728.4 7102. 300. 0.552 2851. 5846. 351.
12299. 275.2 21.70 788.4 6916. 300. 0.564 2760. 5837. 357.
13448. 300.6 24.24 848.8 6732. 300. 0.576 2669. 5826. 363.
14598. 326.9 26.92 909.8 6551. 300. 0.589 2576. 5815. 369.
15747. 354.2 29.74 971.4 6370. 300. 0.601 2482. 5804. 376.
16897. 382.5 32.72 1033.8 6204. 300. 0.614 2394. 5791. 382.
18046. 411.8 35.86 1097.1 6039. 300. 0.628 2307. 5778. 389.
19195. 442.3 39.18 1161.3 5877. 300. 0.641 2218. 5764. 395.
20345. 474.1 42.69 1226.6 5718. 300. 0.656 2129. 5749. 402.
21494. 507.2 46.42 1293.1 5561. 300. 0.670 2040. 5733. 409.
22644. 541.7 50.39 1360.8 5407. 300. 0.685 1951. 5716. 416.
23793. 577.9 54.61 1430.0 5255. 300. 0.700 1862. 5699. 424.
24943. 615.9 59.12 1500.8 5107. 300. 0.716 1772. 5682. 431.
26092. 655.9 63.96 1573.4 4958. 300. 0.732 1680. 5666. 439.
27241. 698.1 69.15 1648.2 4813. 300. 0.749 1588. 5651. 447.
28391. 743.0 74.76 1725.5 4672. 300. 0.766 1493. 5643. 455.
29540. 790.8 80.86 1805.9 4535. 300. 0.783 1393. 5653. 463.
30690. 842.6 87.57 1890.7 4399. 300. 0.801 1277. 5696. 471.
31839. 900.2 95.19 1982.6 4265. 300. 0.820 1124. 5826. 479.
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Manoeuvre segment 4 starts at:
Initial Mass 88756. lb. (CL 0.29 trapezoidal)
Initial Altitude 31839. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 300. kts (fixed Mach 0.820)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 4265. lbf. (100% MCL)
Climb/Descent rate 1625. feet/min
Flightpath angle 1.9 deg. (grad.3.35%)
True airspeed 479. kts
Fuel Flow rate 5665. lb/hr
NOx emission rate 73.3 lb/hr
HC emission rate 0.195 lb/hr
CO emission rate 9.6 lb/hr
L/D ratio 15.24
Total aircraft drag 5826. lbf.
Segment 4 ends at total time = 17.0 mins, endmass = 88572.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +3161. +123. +16.20 +184.0 +2.29 +0.007 +0.37
Final : 35000. 1023. 111.39 2166.6 35.06 0.058 2.90
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
31839. 900.2 95.19 1982.6 4265. 300. 0.820 1625. 5826. 479.
32005. 906.4 96.01 1992.3 4249. 299. 0.820 1618. 5803. 479.
32172. 912.6 96.83 2001.9 4232. 298. 0.820 1611. 5780. 479.
32338. 918.8 97.66 2011.6 4216. 297. 0.820 1603. 5758. 478.
32505. 925.0 98.49 2021.2 4199. 296. 0.820 1596. 5735. 478.
32671. 931.3 99.32 2030.9 4182. 295. 0.820 1588. 5713. 478.
32837. 937.6 100.15 2040.6 4166. 293. 0.820 1580. 5691. 477.
33004. 943.9 100.99 2050.2 4149. 292. 0.820 1572. 5670. 477.
33170. 950.3 101.84 2059.9 4132. 291. 0.820 1564. 5649. 477.
33336. 956.7 102.68 2069.6 4116. 290. 0.820 1556. 5628. 476.
33503. 963.1 103.53 2079.2 4099. 289. 0.820 1547. 5607. 476.
33669. 969.6 104.39 2088.9 4082. 288. 0.820 1539. 5586. 476.
33835. 976.1 105.25 2098.6 4066. 287. 0.820 1530. 5566. 475.
34002. 982.7 106.11 2108.3 4049. 286. 0.820 1521. 5546. 475.
34168. 989.2 106.98 2118.0 4033. 285. 0.820 1512. 5526. 474.
34335. 995.9 107.85 2127.7 4016. 284. 0.820 1503. 5506. 474.
34501. 1003. 108.73 2137.4 3999. 283. 0.820 1494. 5487. 474.
34667. 1009. 109.61 2147.1 3983. 282. 0.820 1484. 5468. 473.
34834. 1016. 110.50 2156.9 3966. 281. 0.820 1475. 5449. 473.
35000. 1023. 111.39 2166.6 3949. 279. 0.820 1465. 5431. 473.
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Acceleration to 299.kts in level flight at 35000.feet =0.03g:
Time +51.1 sec, Dist +6.94 n.miles, Fuelburn +82.3 lb.
NOx +1.12 lb., HC +0.003 lb., CO +0.140 lb.
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Manoeuvre segment 5 starts at:
Initial Mass 88490. lb. (CL 0.29 trapezoidal)
Initial Altitude 35000. feet (1.66g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 299. kts (input Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 3457. lbf. (level cruise) =97.1%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 501. kts
Fuel Flow rate 4625. lb/hr
NOx emission rate 50.9 lb/hr
HC emission rate 0.220 lb/hr
CO emission rate 14.8 lb/hr
L/D ratio 12.80
Total aircraft drag 6913. lbf.
Segment 5 ends at total time = 43.0 mins, endmass = 86561.lb.(1.69g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +1509. +210.20 +1928.9 +21.13 +0.092 +6.28
Final : 35000. 2583. 328.53 4177.8 57.31 0.153 9.32
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
35000. 1074. 118.33 2248.9 3457. 299. 0.870 0. 6913. 501.
35000. 1153. 129.34 2350.4 3455. 299. 0.870 0. 6910. 501.
35000. 1232. 140.36 2451.9 3453. 299. 0.870 0. 6906. 501.
35000. 1311. 151.38 2553.5 3451. 299. 0.870 0. 6902. 501.
35000. 1390. 162.41 2655.0 3449. 299. 0.870 0. 6899. 501.
35000. 1470. 173.44 2756.5 3447. 299. 0.870 0. 6895. 501.
35000. 1549. 184.48 2858.0 3446. 299. 0.870 0. 6891. 501.
35000. 1628. 195.53 2959.6 3444. 299. 0.870 0. 6888. 501.
35000. 1707. 206.58 3061.1 3442. 299. 0.870 0. 6884. 501.
35000. 1787. 217.64 3162.6 3440. 299. 0.870 0. 6880. 501.
35000. 1866. 228.70 3264.1 3438. 299. 0.870 0. 6877. 501.
35000. 1946. 239.77 3365.7 3437. 299. 0.870 0. 6873. 501.
35000. 2025. 250.84 3467.2 3435. 299. 0.870 0. 6869. 501.
35000. 2105. 261.92 3568.7 3433. 299. 0.870 0. 6866. 501.
35000. 2184. 273.01 3670.2 3431. 299. 0.870 0. 6862. 501.
35000. 2264. 284.10 3771.7 3429. 299. 0.870 0. 6859. 501.
35000. 2344. 295.20 3873.3 3428. 299. 0.870 0. 6855. 501.
35000. 2423. 306.30 3974.8 3426. 299. 0.870 0. 6851. 501.
35000. 2503. 317.41 4076.3 3424. 299. 0.870 0. 6848. 501.
35000. 2583. 328.53 4177.8 3422. 299. 0.870 0. 6844. 501.
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Manoeuvre segment 6 starts at:
Initial Mass 86561. lb. (CL 0.29 trapezoidal)
Initial Altitude 35000. feet (1.69g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 299. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 3923. lbf. (100% MCL)
Climb/Descent rate 654. feet/min
Flightpath angle 0.7 deg. (grad.1.29%)
True airspeed 501. kts
Fuel Flow rate 5252. lb/hr
NOx emission rate 64.8 lb/hr
HC emission rate 0.199 lb/hr
CO emission rate 10.4 lb/hr
L/D ratio 12.65
Total aircraft drag 6844. lbf.
Segment 6 ends at total time = 46.9 mins, endmass = 86239.lb.(1.55g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +2000. +231. +32.12 +321.9 +3.82 +0.013 +0.74
Final : 37000. 2814. 360.65 4499.7 61.13 0.167 10.06
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
35000. 2583. 328.53 4177.8 3923. 299. 0.870 654. 6844. 501.
35105. 2593. 329.89 4192.0 3907. 298. 0.870 644. 6827. 501.
35211. 2602. 331.26 4206.3 3891. 297. 0.870 634. 6810. 501.
35316. 2612. 332.66 4220.8 3875. 297. 0.870 624. 6793. 501.
35421. 2623. 334.08 4235.5 3859. 296. 0.870 613. 6776. 501.
35526. 2633. 335.52 4250.3 3843. 295. 0.870 603. 6760. 500.
35632. 2644. 336.99 4265.3 3827. 294. 0.870 593. 6743. 500.
35737. 2654. 338.48 4280.5 3811. 294. 0.870 582. 6727. 500.
35842. 2665. 340.00 4295.9 3795. 293. 0.870 572. 6711. 500.
35947. 2677. 341.55 4311.6 3779. 292. 0.870 561. 6695. 499.
36053. 2688. 343.13 4327.4 3763. 292. 0.870 550. 6679. 499.
36158. 2700. 344.83 4344.4 3747. 291. 0.870 485. 6664. 499.
36263. 2713. 346.65 4362.6 3731. 290. 0.870 475. 6649. 499.
36368. 2727. 348.51 4381.1 3714. 289. 0.870 465. 6635. 499.
36474. 2740. 350.42 4399.9 3698. 289. 0.870 455. 6620. 499.
36579. 2755. 352.37 4419.1 3682. 288. 0.870 444. 6606. 499.
36684. 2769. 354.36 4438.6 3666. 287. 0.870 434. 6592. 499.
36789. 2784. 356.40 4458.6 3650. 287. 0.870 423. 6578. 499.
36895. 2799. 358.50 4478.9 3634. 286. 0.870 413. 6564. 499.
37000. 2814. 360.65 4499.7 3618. 285. 0.870 402. 6550. 499.
-----------------------------------------------------------------------------
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Manoeuvre segment 7 starts at:
Initial Mass 86239. lb. (CL 0.32 trapezoidal)
Initial Altitude 37000. feet (1.55g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 285. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 3275. lbf. (level cruise) =99.8%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 499. kts
Fuel Flow rate 4356. lb/hr
NOx emission rate 46.3 lb/hr
HC emission rate 0.221 lb/hr
CO emission rate 15.0 lb/hr
L/D ratio 13.17
Total aircraft drag 6550. lbf.
Segment 7 ends at total time = 154.3 mins, endmass = 78619.lb.(1.70g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +6443. +893.09 +7619.8 +79.58 +0.400 +27.88
Final : 37000. 9257. 1253.74 12119.5 140.71 0.567 37.94
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
37000. 2814. 360.65 4499.7 3275. 285. 0.870 0. 6550. 499.
37000. 3146. 406.64 4900.7 3267. 285. 0.870 0. 6534. 499.
37000. 3479. 452.75 5301.8 3259. 285. 0.870 0. 6518. 499.
37000. 3812. 498.98 5702.8 3251. 285. 0.870 0. 6502. 499.
37000. 4146. 545.31 6103.9 3243. 285. 0.870 0. 6486. 499.
37000. 4482. 591.76 6504.9 3235. 285. 0.870 0. 6471. 499.
37000. 4817. 638.32 6906.0 3228. 285. 0.870 0. 6455. 499.
37000. 5154. 684.99 7307.0 3220. 285. 0.870 0. 6440. 499.
37000. 5492. 731.78 7708.1 3212. 285. 0.870 0. 6424. 499.
37000. 5830. 778.68 8109.1 3205. 285. 0.870 0. 6409. 499.
37000. 6169. 825.69 8510.1 3197. 285. 0.870 0. 6394. 499.
37000. 6509. 872.81 8911.2 3190. 285. 0.870 0. 6379. 499.
37000. 6850. 920.04 9312.2 3182. 285. 0.870 0. 6364. 499.
37000. 7191. 967.38 9713.3 3175. 285. 0.870 0. 6350. 499.
37000. 7534. 1014.83 10114.3 3167. 285. 0.870 0. 6335. 499.
37000. 7877. 1062.39 10515.4 3160. 285. 0.870 0. 6320. 499.
37000. 8221. 1110.06 10916.4 3153. 285. 0.870 0. 6306. 499.
37000. 8565. 1157.85 11317.5 3146. 285. 0.870 0. 6292. 499.
37000. 8911. 1205.74 11718.5 3139. 285. 0.870 0. 6277. 499.
37000. 9257. 1253.74 12119.5 3132. 285. 0.870 0. 6263. 499.
-----------------------------------------------------------------------------
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Manoeuvre segment 8 starts at:
Initial Mass 78619. lb. (CL 0.29 trapezoidal)
Initial Altitude 37000. feet (1.70g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 285. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 3618. lbf. (100% MCL)
Climb/Descent rate 626. feet/min
Flightpath angle 0.7 deg. (grad.1.24%)
True airspeed 499. kts
Fuel Flow rate 4815. lb/hr
NOx emission rate 55.9 lb/hr
HC emission rate 0.207 lb/hr
CO emission rate 11.7 lb/hr
L/D ratio 12.55
Total aircraft drag 6263. lbf.
Segment 8 ends at total time = 158.2 mins, endmass = 78319.lb.(1.55g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +2000. +235. +32.58 +300.2 +3.41 +0.013 +0.75
Final : 39000. 9492. 1286.32 12419.7 144.13 0.580 38.69
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
37000. 9257. 1253.74 12119.5 3618. 285. 0.870 626. 6263. 499.
37105. 9267. 1255.15 12133.1 3602. 285. 0.870 615. 6248. 499.
37211. 9278. 1256.58 12146.9 3586. 284. 0.870 604. 6233. 499.
37316. 9288. 1258.05 12160.9 3570. 283. 0.870 593. 6218. 499.
37421. 9299. 1259.54 12175.0 3554. 283. 0.870 582. 6203. 499.
37526. 9310. 1261.05 12189.4 3538. 282. 0.870 571. 6188. 499.
37632. 9321. 1262.60 12203.9 3522. 281. 0.870 560. 6174. 499.
37737. 9333. 1264.18 12218.7 3506. 280. 0.870 549. 6159. 499.
37842. 9344. 1265.79 12233.8 3490. 280. 0.870 537. 6145. 499.
37947. 9356. 1267.44 12249.1 3474. 279. 0.870 526. 6131. 499.
38053. 9368. 1269.12 12264.6 3458. 278. 0.870 514. 6117. 499.
38158. 9381. 1270.85 12280.5 3442. 278. 0.870 503. 6103. 499.
38263. 9393. 1272.61 12296.6 3426. 277. 0.870 491. 6090. 499.
38368. 9406. 1274.42 12313.1 3410. 276. 0.870 479. 6076. 499.
38474. 9420. 1276.27 12329.9 3394. 276. 0.870 467. 6063. 499.
38579. 9433. 1278.17 12347.0 3378. 275. 0.870 455. 6050. 499.
38684. 9447. 1280.12 12364.5 3362. 274. 0.870 443. 6037. 499.
38789. 9462. 1282.13 12382.5 3345. 274. 0.870 430. 6024. 499.
38895. 9477. 1284.19 12400.9 3329. 273. 0.870 418. 6011. 499.
39000. 9492. 1286.32 12419.7 3313. 272. 0.870 405. 5998. 499.
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Manoeuvre segment 9 starts at:
Initial Mass 78319. lb. (CL 0.32 trapezoidal)
Initial Altitude 39000. feet (1.55g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 272. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 2999. lbf. (level cruise) =99.8%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 499. kts
Fuel Flow rate 3990. lb/hr
NOx emission rate 40.7 lb/hr
HC emission rate 0.221 lb/hr
CO emission rate 14.8 lb/hr
L/D ratio 13.06
Total aircraft drag 5998. lbf.
Segment 9 ends at total time = 274.0 mins, endmass = 70806.lb.(1.71g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +6949. +963.30 +7513.8 +75.09 +0.431 +29.82
Final : 39000. 16442. 2249.62 19933.5 219.22 1.012 68.51
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
39000. 9492. 1286.32 12419.7 2999. 272. 0.870 0. 5998. 499.
39000. 9850. 1335.85 12815.2 2991. 272. 0.870 0. 5982. 499.
39000. 10208. 1385.51 13210.6 2983. 272. 0.870 0. 5967. 499.
39000. 10567. 1435.31 13606.1 2976. 272. 0.870 0. 5951. 499.
39000. 10927. 1485.23 14001.5 2968. 272. 0.870 0. 5935. 499.
39000. 11288. 1535.29 14397.0 2960. 272. 0.870 0. 5920. 499.
39000. 11650. 1585.48 14792.5 2952. 272. 0.870 0. 5905. 499.
39000. 12013. 1635.80 15187.9 2945. 272. 0.870 0. 5890. 499.
39000. 12377. 1686.24 15583.4 2937. 272. 0.870 0. 5875. 499.
39000. 12742. 1736.82 15978.9 2930. 272. 0.870 0. 5860. 499.
39000. 13108. 1787.53 16374.3 2922. 272. 0.870 0. 5845. 499.
39000. 13475. 1838.36 16769.8 2915. 272. 0.870 0. 5830. 499.
39000. 13842. 1889.32 17165.2 2908. 272. 0.870 0. 5816. 499.
39000. 14211. 1940.41 17560.7 2901. 272. 0.870 0. 5801. 499.
39000. 14580. 1991.63 17956.2 2893. 272. 0.870 0. 5787. 499.
39000. 14951. 2042.98 18351.6 2886. 272. 0.870 0. 5773. 499.
39000. 15322. 2094.45 18747.1 2879. 272. 0.870 0. 5759. 499.
39000. 15694. 2146.04 19142.5 2872. 272. 0.870 0. 5745. 499.
39000. 16068. 2197.77 19538.0 2865. 272. 0.870 0. 5731. 499.
39000. 16442. 2249.62 19933.5 2858. 272. 0.870 0. 5717. 499.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 10 starts at:
Initial Mass 70806. lb. (CL 0.29 trapezoidal)
Initial Altitude 39000. feet (1.71g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 272. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 3313. lbf. (100% MCL)
Climb/Descent rate 649. feet/min
Flightpath angle 0.7 deg. (grad.1.28%)
True airspeed 499. kts
Fuel Flow rate 4409. lb/hr
NOx emission rate 49.1 lb/hr
HC emission rate 0.205 lb/hr
CO emission rate 11.4 lb/hr
L/D ratio 12.39
Total aircraft drag 5717. lbf.
Segment 10 ends at total time = 277.9 mins, endmass = 70536.lb.(1.56g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +2000. +231. +32.00 +269.1 +2.93 +0.013 +0.73
Final : 41000. 16672. 2281.61 20202.5 222.14 1.025 69.24
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
39000. 16442. 2249.62 19933.5 3313. 272. 0.870 649. 5717. 499.
39105. 16451. 2250.98 19945.5 3297. 272. 0.870 637. 5703. 499.
39211. 16461. 2252.37 19957.7 3281. 271. 0.870 624. 5689. 499.
39316. 16472. 2253.78 19970.0 3265. 270. 0.870 611. 5675. 499.
39421. 16482. 2255.23 19982.6 3249. 270. 0.870 598. 5661. 499.
39526. 16493. 2256.71 19995.4 3233. 269. 0.870 585. 5647. 499.
39632. 16504. 2258.23 20008.4 3217. 269. 0.870 572. 5634. 499.
39737. 16515. 2259.77 20021.7 3201. 268. 0.870 559. 5620. 499.
39842. 16526. 2261.36 20035.2 3185. 267. 0.870 545. 5607. 499.
39947. 16538. 2262.99 20048.9 3169. 267. 0.870 532. 5594. 499.
40053. 16550. 2264.65 20063.0 3154. 266. 0.870 520. 5581. 499.
40158. 16562. 2266.35 20077.3 3139. 265. 0.870 508. 5568. 499.
40263. 16575. 2268.10 20091.8 3125. 265. 0.870 496. 5555. 499.
40368. 16588. 2269.88 20106.7 3110. 264. 0.870 485. 5542. 499.
40474. 16601. 2271.71 20121.8 3095. 263. 0.870 473. 5530. 499.
40579. 16614. 2273.59 20137.2 3081. 263. 0.870 461. 5518. 499.
40684. 16628. 2275.51 20153.0 3066. 262. 0.870 449. 5506. 499.
40789. 16643. 2277.49 20169.1 3052. 261. 0.870 437. 5493. 499.
40895. 16657. 2279.52 20185.6 3037. 261. 0.870 425. 5482. 499.
41000. 16672. 2281.61 20202.5 3023. 260. 0.870 412. 5470. 499.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 11 starts at:
Initial Mass 70536. lb. (CL 0.31 trapezoidal)
Initial Altitude 41000. feet (1.56g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 260. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 2735. lbf. (level cruise) =99.8%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 499. kts
Fuel Flow rate 3638. lb/hr
NOx emission rate 35.4 lb/hr
HC emission rate 0.221 lb/hr
CO emission rate 14.7 lb/hr
L/D ratio 12.90
Total aircraft drag 5470. lbf.
Segment 11 ends at total time = 403.1 mins, endmass = 63143.lb.(1.74g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +7511. +1041.11 +7393.9 +70.48 +0.467 +32.16
Final : 41000. 24183. 3322.72 27596.5 292.63 1.491 101.40
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
41000. 16672. 2281.61 20202.5 2735. 260. 0.870 0. 5470. 499.
41000. 17058. 2335.07 20591.7 2727. 260. 0.870 0. 5454. 499.
41000. 17445. 2388.68 20980.9 2720. 260. 0.870 0. 5439. 499.
41000. 17833. 2442.44 21370.0 2712. 260. 0.870 0. 5424. 499.
41000. 18221. 2496.35 21759.2 2704. 260. 0.870 0. 5409. 499.
41000. 18611. 2550.41 22148.3 2697. 260. 0.870 0. 5394. 499.
41000. 19003. 2604.61 22537.5 2690. 260. 0.870 0. 5379. 499.
41000. 19395. 2658.97 22926.6 2682. 260. 0.870 0. 5364. 499.
41000. 19788. 2713.48 23315.8 2675. 260. 0.870 0. 5350. 499.
41000. 20182. 2768.13 23704.9 2668. 260. 0.870 0. 5336. 499.
41000. 20578. 2822.94 24094.1 2661. 260. 0.870 0. 5321. 499.
41000. 20974. 2877.89 24483.2 2654. 260. 0.870 0. 5307. 499.
41000. 21371. 2932.98 24872.4 2647. 260. 0.870 0. 5293. 499.
41000. 21770. 2988.22 25261.6 2640. 260. 0.870 0. 5279. 499.
41000. 22170. 3043.61 25650.7 2633. 260. 0.870 0. 5265. 499.
41000. 22570. 3099.15 26039.9 2626. 260. 0.870 0. 5252. 499.
41000. 22972. 3154.83 26429.0 2619. 260. 0.870 0. 5238. 499.
41000. 23375. 3210.65 26818.2 2612. 260. 0.870 0. 5225. 499.
41000. 23778. 3266.61 27207.3 2606. 260. 0.870 0. 5211. 499.
41000. 24183. 3322.72 27596.5 2599. 260. 0.870 0. 5198. 499.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 12 starts at:
Initial Mass 63143. lb. (CL 0.28 trapezoidal)
Initial Altitude 41000. feet (1.74g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 260. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 3023. lbf. (100% MCL)
Climb/Descent rate 678. feet/min
Flightpath angle 0.8 deg. (grad.1.34%)
True airspeed 499. kts
Fuel Flow rate 4022. lb/hr
NOx emission rate 42.9 lb/hr
HC emission rate 0.205 lb/hr
CO emission rate 11.2 lb/hr
L/D ratio 12.15
Total aircraft drag 5198. lbf.
Segment 12 ends at total time = 406.7 mins, endmass = 62908.lb.(1.59g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +2000. +221. +30.60 +234.5 +2.44 +0.013 +0.69
Final : 43000. 24404. 3353.32 27830.9 295.06 1.504 102.08
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
41000. 24183. 3322.72 27596.5 3023. 260. 0.870 678. 5198. 499.
41105. 24192. 3324.03 27607.0 3008. 260. 0.870 665. 5185. 499.
41211. 24202. 3325.36 27617.6 2993. 259. 0.870 653. 5172. 499.
41316. 24212. 3326.71 27628.4 2979. 258. 0.870 640. 5158. 499.
41421. 24222. 3328.09 27639.3 2964. 258. 0.870 627. 5145. 499.
41526. 24232. 3329.50 27650.4 2950. 257. 0.870 614. 5133. 499.
41632. 24242. 3330.94 27661.7 2935. 256. 0.870 601. 5120. 499.
41737. 24253. 3332.41 27673.2 2921. 256. 0.870 588. 5107. 499.
41842. 24264. 3333.92 27684.9 2906. 255. 0.870 575. 5095. 499.
41947. 24275. 3335.46 27696.8 2892. 255. 0.870 562. 5082. 499.
42053. 24286. 3337.04 27709.0 2877. 254. 0.870 548. 5070. 499.
42158. 24298. 3338.65 27721.3 2862. 253. 0.870 535. 5058. 499.
42263. 24310. 3340.31 27734.0 2848. 253. 0.870 521. 5046. 499.
42368. 24322. 3342.01 27746.9 2833. 252. 0.870 508. 5034. 499.
42474. 24335. 3343.76 27760.0 2819. 251. 0.870 494. 5022. 499.
42579. 24348. 3345.56 27773.5 2804. 251. 0.870 480. 5010. 499.
42684. 24361. 3347.41 27787.3 2790. 250. 0.870 466. 4999. 499.
42789. 24375. 3349.32 27801.5 2775. 250. 0.870 452. 4987. 499.
42895. 24389. 3351.29 27816.0 2761. 249. 0.870 438. 4976. 499.
43000. 24404. 3353.32 27830.9 2746. 248. 0.870 423. 4965. 499.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 13 starts at:
Initial Mass 62908. lb. (CL 0.31 trapezoidal)
Initial Altitude 43000. feet (1.59g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 248. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 2482. lbf. (level cruise) =99.8%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 499. kts
Fuel Flow rate 3302. lb/hr
NOx emission rate 30.6 lb/hr
HC emission rate 0.221 lb/hr
CO emission rate 14.8 lb/hr
L/D ratio 12.67
Total aircraft drag 4965. lbf.
Segment 13 ends at total time = 553.9 mins, endmass = 55043.lb.(1.81g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +8832. +1224.29 +7865.1 +71.15 +0.551 +38.14
Final : 43000. 33236. 4577.61 35696.0 366.22 2.054 140.23
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
43000. 24404. 3353.32 27830.9 2482. 248. 0.870 0. 4965. 499.
43000. 24856. 3415.98 28244.9 2474. 248. 0.870 0. 4949. 499.
43000. 25309. 3478.84 28658.8 2467. 248. 0.870 0. 4933. 499.
43000. 25764. 3541.90 29072.8 2459. 248. 0.870 0. 4918. 499.
43000. 26221. 3605.16 29486.7 2451. 248. 0.870 0. 4902. 499.
43000. 26678. 3668.62 29900.7 2443. 248. 0.870 0. 4887. 499.
43000. 27138. 3732.28 30314.7 2436. 248. 0.870 0. 4872. 499.
43000. 27598. 3796.14 30728.6 2428. 248. 0.870 0. 4857. 499.
43000. 28060. 3860.20 31142.6 2421. 248. 0.870 0. 4842. 499.
43000. 28524. 3924.45 31556.5 2414. 248. 0.870 0. 4827. 499.
43000. 28989. 3988.90 31970.5 2406. 248. 0.870 0. 4812. 499.
43000. 29455. 4053.54 32384.4 2399. 248. 0.870 0. 4798. 499.
43000. 29923. 4118.38 32798.4 2392. 248. 0.870 0. 4784. 499.
43000. 30392. 4183.41 33212.3 2385. 248. 0.870 0. 4770. 499.
43000. 30863. 4248.63 33626.3 2378. 248. 0.870 0. 4756. 499.
43000. 31334. 4314.04 34040.2 2371. 248. 0.870 0. 4742. 499.
43000. 31808. 4379.65 34454.2 2364. 248. 0.870 0. 4728. 499.
43000. 32282. 4445.45 34868.1 2357. 248. 0.870 0. 4715. 499.
43000. 32758. 4511.43 35282.1 2351. 248. 0.870 0. 4701. 499.
43000. 33236. 4577.61 35696.0 2344. 248. 0.870 0. 4688. 499.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 14 starts at:
Initial Mass 55043. lb. (CL 0.27 trapezoidal)
Initial Altitude 43000. feet (1.81g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 248. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 2746. lbf. (100% MCL)
Climb/Descent rate 738. feet/min
Flightpath angle 0.8 deg. (grad.1.46%)
True airspeed 499. kts
Fuel Flow rate 3654. lb/hr
NOx emission rate 37.1 lb/hr
HC emission rate 0.205 lb/hr
CO emission rate 11.2 lb/hr
L/D ratio 11.74
Total aircraft drag 4688. lbf.
Segment 14 ends at total time = 557.4 mins, endmass = 54844.lb.(1.65g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +2000. +208. +28.77 +199.1 +1.96 +0.012 +0.66
Final : 45000. 33443. 4606.37 35895.1 368.18 2.066 140.89
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
43000. 33236. 4577.61 35696.0 2746. 248. 0.870 738. 4688. 499.
43105. 33244. 4578.81 35704.8 2731. 248. 0.870 723. 4675. 499.
43211. 33253. 4580.03 35713.7 2717. 247. 0.870 708. 4662. 499.
43316. 33262. 4581.28 35722.7 2702. 247. 0.870 693. 4650. 499.
43421. 33271. 4582.56 35731.9 2688. 246. 0.870 678. 4637. 499.
43526. 33281. 4583.86 35741.2 2673. 245. 0.870 663. 4625. 499.
43632. 33291. 4585.20 35750.7 2659. 245. 0.870 647. 4613. 499.
43737. 33300. 4586.57 35760.4 2644. 244. 0.870 632. 4601. 499.
43842. 33311. 4587.97 35770.2 2629. 244. 0.870 616. 4588. 499.
43947. 33321. 4589.41 35780.3 2615. 243. 0.870 601. 4577. 499.
44053. 33332. 4590.89 35790.6 2600. 242. 0.870 585. 4565. 499.
44158. 33342. 4592.40 35801.1 2586. 242. 0.870 569. 4553. 499.
44263. 33354. 4593.97 35811.8 2571. 241. 0.870 553. 4541. 499.
44368. 33365. 4595.57 35822.8 2557. 241. 0.870 537. 4530. 499.
44474. 33377. 4597.23 35834.0 2542. 240. 0.870 521. 4518. 499.
44579. 33390. 4598.94 35845.6 2528. 239. 0.870 505. 4507. 499.
44684. 33402. 4600.70 35857.4 2513. 239. 0.870 488. 4496. 499.
44789. 33415. 4602.52 35869.6 2498. 238. 0.870 472. 4485. 499.
44895. 33429. 4604.41 35882.2 2484. 238. 0.870 455. 4474. 499.
45000. 33443. 4606.37 35895.1 2469. 237. 0.870 439. 4463. 499.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 15 starts at:
Initial Mass 54844. lb. (CL 0.30 trapezoidal)
Initial Altitude 45000. feet (1.65g buffet)
Delta-ISA +0. deg.C
Airspeed (CAS) 237. kts (fixed Mach 0.870)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 2231. lbf. (level cruise) =99.9%MCR
Climb/Descent rate 0. feet/min
Flightpath angle 0.0 deg. (grad.0.00%)
True airspeed 499. kts
Fuel Flow rate 2968. lb/hr
NOx emission rate 25.9 lb/hr
HC emission rate 0.223 lb/hr
CO emission rate 15.1 lb/hr
L/D ratio 12.29
Total aircraft drag 4463. lbf.
Segment 15 ends at total time = 591.5 mins, endmass = 53168.lb.(1.71g buff)
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: +0. +2046. +283.65 +1675.6 +14.57 +0.127 +8.68
Final : 45000. 35489. 4890.02 37570.7 382.74 2.193 149.57
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
45000. 33443. 4606.37 35895.1 2231. 237. 0.870 0. 4463. 499.
45000. 33550. 4621.21 35983.3 2230. 237. 0.870 0. 4460. 499.
45000. 33657. 4636.05 36071.5 2228. 237. 0.870 0. 4456. 499.
45000. 33765. 4650.90 36159.7 2227. 237. 0.870 0. 4453. 499.
45000. 33872. 4665.77 36247.9 2225. 237. 0.870 0. 4450. 499.
45000. 33979. 4680.64 36336.1 2223. 237. 0.870 0. 4447. 499.
45000. 34086. 4695.53 36424.3 2222. 237. 0.870 0. 4444. 499.
45000. 34194. 4710.43 36512.4 2220. 237. 0.870 0. 4440. 499.
45000. 34301. 4725.34 36600.6 2219. 237. 0.870 0. 4437. 499.
45000. 34409. 4740.25 36688.8 2217. 237. 0.870 0. 4434. 499.
45000. 34517. 4755.18 36777.0 2215. 237. 0.870 0. 4431. 499.
45000. 34625. 4770.12 36865.2 2214. 237. 0.870 0. 4428. 499.
45000. 34732. 4785.07 36953.4 2212. 237. 0.870 0. 4425. 499.
45000. 34840. 4800.03 37041.6 2211. 237. 0.870 0. 4422. 499.
45000. 34948. 4815.00 37129.8 2209. 237. 0.870 0. 4419. 499.
45000. 35056. 4829.99 37218.0 2208. 237. 0.870 0. 4415. 499.
45000. 35165. 4844.98 37306.2 2206. 237. 0.870 0. 4412. 499.
45000. 35273. 4859.98 37394.3 2205. 237. 0.870 0. 4409. 499.
45000. 35381. 4874.99 37482.5 2203. 237. 0.870 0. 4406. 499.
45000. 35489. 4890.02 37570.7 2202. 237. 0.870 0. 4403. 499.
-----------------------------------------------------------------------------
Deceleration to 222.kts in level flight at 45000.feet =-0.06g:
Time +27.3 sec, Dist +3.67 n.miles, Fuelburn +6.9 lb.
NOx +0.03 lb., HC +0.011 lb., CO +0.307 lb.
-----------------------------------------------------------------------------
Manoeuvre segment 16 starts at:
Initial Mass 53161. lb. (CL 0.32 trapezoidal)
Initial Altitude 45000. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 222. kts (input Mach 0.820)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine 458. lbf. (idle)
Climb/Descent rate -2292. feet/min
Flightpath angle -2.8 deg. (grad.-4.81%)
True airspeed 470. kts
Fuel Flow rate 904. lb/hr
NOx emission rate 3.8 lb/hr
HC emission rate 1.437 lb/hr
CO emission rate 41.1 lb/hr
L/D ratio 15.30
Total aircraft drag 3474. lbf.
Segment 16 ends at total time = 596.0 mins, endmass = 53103.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -13161. +245. +32.04 +58.8 +0.24 +0.109 +2.88
Final : 31839. 35762. 4925.73 37636.4 383.01 2.313 152.75
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
45000. 35517. 4893.69 37577.6 458. 222. 0.820 -2292. 3474. 470.
44307. 35535. 4896.02 37582.1 442. 225. 0.820 -2367. 3526. 470.
43615. 35552. 4898.28 37586.4 426. 229. 0.820 -2445. 3580. 470.
42922. 35569. 4900.46 37590.5 410. 233. 0.820 -2525. 3638. 470.
42229. 35585. 4902.58 37594.5 394. 236. 0.820 -2609. 3699. 470.
41537. 35600. 4904.63 37598.4 378. 240. 0.820 -2695. 3763. 470.
40844. 35616. 4906.61 37602.1 362. 244. 0.820 -2784. 3830. 470.
40151. 35630. 4908.53 37605.7 346. 248. 0.820 -2876. 3900. 470.
39459. 35645. 4910.38 37609.1 317. 252. 0.820 -2994. 3974. 470.
38766. 35658. 4912.16 37612.4 284. 256. 0.820 -3122. 4051. 470.
38073. 35671. 4913.86 37615.5 251. 260. 0.820 -3254. 4131. 470.
37381. 35684. 4915.50 37618.5 218. 265. 0.820 -3388. 4215. 470.
36688. 35696. 4917.07 37621.3 185. 269. 0.820 -3526. 4302. 470.
35995. 35707. 4918.51 37623.9 153. 273. 0.820 -4029. 4394. 471.
35302. 35717. 4919.84 37626.3 120. 278. 0.820 -4205. 4493. 472.
34610. 35727. 4921.11 37628.5 87. 282. 0.820 -4387. 4597. 474.
33917. 35736. 4922.33 37630.6 54. 286. 0.820 -4573. 4704. 475.
33224. 35745. 4923.51 37632.6 21. 291. 0.820 -4763. 4815. 476.
32532. 35753. 4924.64 37634.5 -12. 295. 0.820 -4958. 4929. 478.
31839. 35762. 4925.73 37636.4 -45. 300. 0.820 -5158. 5047. 479.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
Manoeuvre segment 17 starts at:
Initial Mass 53103. lb. (CL 0.17 trapezoidal)
Initial Altitude 31839. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 300. kts (fixed)
Flaps 0 deg. (hi-speed)
Undercarriage up
All eng.operative
Thrust per engine -45. lbf. (idle)
Climb/Descent rate -3570. feet/min
Flightpath angle -4.2 deg. (grad.-7.35%)
True airspeed 479. kts
Fuel Flow rate 798. lb/hr
NOx emission rate 3.2 lb/hr
HC emission rate 1.520 lb/hr
CO emission rate 38.6 lb/hr
L/D ratio 10.52
Total aircraft drag 5047. lbf.
Segment 17 ends at total time = 602.2 mins, endmass = 53027.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -21839. +371. +42.06 +76.0 +0.29 +0.136 +3.40
Final : 10000. 36133. 4967.79 37712.4 383.30 2.449 156.15
-----------------------------------------------------------------------------
History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
31839. 35762. 4925.73 37636.4 -45. 300. 0.820 -3570. 5047. 479.
30690. 35781. 4928.30 37640.7 -73. 300. 0.801 -3510. 4949. 471.
29540. 35801. 4930.86 37645.0 -101. 300. 0.783 -3489. 4908. 463.
28391. 35821. 4933.38 37649.3 -117. 300. 0.766 -3475. 4901. 455.
27241. 35840. 4935.87 37653.7 -139. 300. 0.749 -3479. 4911. 447.
26092. 35860. 4938.30 37658.0 -167. 300. 0.732 -3494. 4928. 439.
24943. 35880. 4940.67 37662.2 -200. 300. 0.716 -3516. 4946. 431.
23793. 35899. 4942.99 37666.3 -238. 300. 0.700 -3544. 4964. 424.
22644. 35919. 4945.26 37670.2 -262. 300. 0.685 -3551. 4984. 416.
21494. 35938. 4947.49 37674.1 -284. 300. 0.670 -3555. 5002. 409.
20345. 35958. 4949.67 37677.9 -306. 300. 0.656 -3557. 5019. 402.
19195. 35977. 4951.82 37681.7 -325. 300. 0.641 -3555. 5036. 395.
18046. 35996. 4953.93 37685.6 -349. 300. 0.628 -3556. 5051. 389.
16897. 36016. 4956.01 37689.4 -377. 300. 0.614 -3561. 5065. 382.
15747. 36035. 4958.04 37693.2 -409. 300. 0.601 -3569. 5079. 376.
14598. 36054. 4960.04 37696.9 -430. 300. 0.589 -3563. 5091. 369.
13448. 36074. 4962.02 37700.7 -447. 300. 0.576 -3551. 5103. 363.
12299. 36093. 4963.96 37704.5 -461. 300. 0.564 -3534. 5114. 357.
11149. 36113. 4965.89 37708.4 -472. 300. 0.552 -3514. 5124. 351.
10000. 36133. 4967.79 37712.4 -481. 300. 0.541 -3490. 5133. 345.
-----------------------------------------------------------------------------
Deceleration to 250.kts in level flight at 10000.feet =-0.10g:
Time +29.9 sec, Dist +2.62 n.miles, Fuelburn +6.3 lb.
NOx +0.02 lb., HC +0.010 lb., CO +0.248 lb.
-----------------------------------------------------------------------------
Manoeuvre segment 18 starts at:
Initial Mass 53020. lb. (CL 0.22 trapezoidal)
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 -298. lbf. (idle)
Climb/Descent rate -2274. feet/min
Flightpath angle -4.4 deg. (grad.-7.78%)
True airspeed 289. kts
Fuel Flow rate 774. lb/hr
NOx emission rate 3.0 lb/hr
HC emission rate 1.220 lb/hr
CO emission rate 30.3 lb/hr
L/D ratio 13.33
Total aircraft drag 3979. lbf.
Segment 18 ends at total time = 606.6 mins, endmass = 52961.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -8500. +236. +17.79 +59.5 +0.24 +0.084 +2.10
Final : 1500. 36399. 4988.20 37778.2 383.57 2.543 158.51
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
10000. 36162. 4970.42 37718.7 -298. 250. 0.452 -2274. 3979. 289.
9553. 36174. 4971.36 37721.2 -298. 250. 0.449 -2264. 3980. 287.
9105. 36186. 4972.30 37723.8 -299. 250. 0.445 -2253. 3980. 285.
8658. 36198. 4973.25 37726.5 -298. 250. 0.441 -2242. 3981. 283.
8211. 36210. 4974.19 37729.2 -298. 250. 0.438 -2231. 3982. 281.
7763. 36222. 4975.13 37732.0 -297. 250. 0.434 -2219. 3983. 279.
7316. 36234. 4976.06 37734.9 -296. 250. 0.431 -2207. 3984. 278.
6868. 36247. 4977.00 37737.8 -295. 250. 0.427 -2195. 3984. 276.
6421. 36259. 4977.94 37740.8 -294. 250. 0.424 -2183. 3985. 274.
5974. 36271. 4978.87 37743.8 -292. 250. 0.420 -2171. 3985. 272.
5526. 36284. 4979.81 37746.9 -290. 250. 0.417 -2158. 3986. 270.
5079. 36296. 4980.74 37750.1 -288. 250. 0.413 -2146. 3987. 269.
4632. 36309. 4981.68 37753.4 -286. 250. 0.410 -2133. 3987. 267.
4184. 36321. 4982.61 37756.7 -283. 250. 0.407 -2120. 3987. 265.
3737. 36334. 4983.54 37760.1 -281. 250. 0.404 -2107. 3988. 264.
3289. 36347. 4984.47 37763.5 -278. 250. 0.400 -2093. 3988. 262.
2842. 36360. 4985.41 37767.1 -275. 250. 0.397 -2081. 3988. 260.
2395. 36372. 4986.34 37770.7 -273. 250. 0.394 -2068. 3989. 259.
1947. 36385. 4987.27 37774.4 -271. 250. 0.391 -2056. 3989. 257.
1500. 36399. 4988.20 37778.2 -269. 250. 0.388 -2043. 3989. 255.
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Deceleration to 111.kts in level flight at 1500.feet =-0.23g:
Time +31.8 sec, Dist +1.47 n.miles, Fuelburn +9.8 lb.
NOx +0.04 lb., HC +0.012 lb., CO +0.310 lb.
-----------------------------------------------------------------------------
Manoeuvre segment 19 starts at:
Initial Mass 52951. lb. (CL 1.11 trapezoidal)
Initial Altitude 1500. feet
Delta-ISA +0. deg.C
Airspeed (CAS) 111. kts (Vapp)
Flaps 30 deg.
Undercarriage down
All eng.operative
Thrust per engine 2113. lbf. (match grad.) =18.9%MCL
Climb/Descent rate -602. feet/min
Flightpath angle -3.0 deg. (grad.-5.24%)
True airspeed 114. kts
Fuel Flow rate 3327. lb/hr
NOx emission rate 25.7 lb/hr
HC emission rate 0.170 lb/hr
CO emission rate 16.2 lb/hr
L/D ratio 7.52
Total aircraft drag 7046. lbf.
Segment 19 ends at total time = 609.6 mins, endmass = 52814.lb.
Altitude Time Distance Fuel Burn NOx HC CO
feet sec n.miles lb. lb. lb. lb.
Increm: -1450. +146. +0.00 +137.0 +1.06 +0.007 +0.66
Final : 50. 36576. 4989.68 37925.0 384.67 2.562 159.48
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History: Alt Time Dist Burnt FN/eng CAS Mach RoC Drag TAS
1500. 36430. 0.000 37788.0 2113. 111. 0.173 -602. 7046. 114.
1339. 36446. 0.000 37802.8 2113. 111. 0.172 -601. 7044. 113.
1178. 36463. 0.000 37817.8 2113. 111. 0.172 -599. 7042. 113.
1017. 36479. 0.000 37832.8 2112. 111. 0.171 -598. 7040. 113.
856. 36495. 0.000 37848.0 2112. 111. 0.171 -596. 7038. 112.
694. 36511. 0.000 37863.2 2111. 111. 0.170 -595. 7037. 112.
533. 36527. 0.000 37878.5 2111. 111. 0.170 -593. 7035. 112.
372. 36544. 0.000 37893.9 2111. 111. 0.169 -592. 7033. 112.
211. 36560. 0.000 37909.4 2110. 111. 0.168 -591. 7031. 111.
50. 36576. 0.000 37925.0 2110. 111. 0.168 -589. 7029. 111.
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