Сводная таблица основных параметров. Эта таблица двухлетней давности. Уже думаю можно будет дополнить данные по XLR и MAX10. А220-500 не существет на данный момент. я поигрался с простым удлинением салона. Для МС-21 максимальное количество пассажиров указал в соотвествии с цифрой в сертификате типа.
Для удобства скопируйте и перетаищите ее в Excel
Ревизия Rev NC.
Для удобства скопируйте и перетаищите ее в Excel
Ревизия Rev NC.
A220-300 | A220-500 | A319NEO | A320NEO | A321NEO | A321XLR | 737-7 | 737-8-200 | 737-9 | 737-10 | MC21-200 | MC21-300 | |
WEIGHT | ||||||||||||
MRW, Maximum Ramp Weight, t | 71.3 | 75.9 | 75.9 | 79.4 | 97.4 | 80.512 | 82.417 | 88.541 | 89.992 | |||
MTOW (t) | 70.9 | 75.5 | 75.5 | 79 | 97 | 101 | 80.285 | 82.644 | 88.314 | 89.765 | 72.56 | 79.25 |
MLW (t) | 58.74 | 62 | 63.9 | 67.4 | 77.3 | 66.043 | 69.308 | 74.343 | 75.931 | 63.1 | 71.3 | |
MZFW (t) | 57.6 | 59.18 | 60.3 | 64.3 | 73.3 | 62.913 | 65.952 | 70.987 | 72.574 | 59.6 | 68.1 | |
FUEL, Left Main Tank, l | 3770 | 3770 | 7979.5 | 7738.35 | 7738.35 | |||||||
FUEL, Right Main Tank, l | 3770 | 3770 | 7979.5 | 7738.35 | 7738.35 | |||||||
FUEL, Center Tank, l | 13968 | 13968 | 8250 | 8248 | 8248 | |||||||
FUEL, standard, l | 21,508 | 21,508 | 24,209 | 23,859 | 23,490 | 25,816 | 25,816 | 25,816 | 25,816 | 26,154 | 26,154 | |
FUEL AUX, MAX(unusable), l | 10,614 | 8,484 | 9,363 | 13,529 | 15,524 | |||||||
MAX FUEL, kg, 0.8 | 17.21 | 17.21 | 19.43 | 19.09 | 18.79 | 0.00 | 20.65 | 20.65 | 20.65 | 20.6528 | 20.92 | 20.92 |
OEW (t) | 37.08 | 39.68 | 42.6 | 44.3 | 50.1 | 51.7 | 43 | 45.07 | 48.1 | 49.9 | 40.7 | 46.80 |
Minimum Weight, t | 37.2 | 39.6 | 46.3 | 47.1 | ||||||||
MPLD, Maximum Payload, t | 18.70 | 19.50 | 17.70 | 20.00 | 25.50 | 19.91 | 20.88 | 22.89 | 22.67 | 18.90 | 21.10 | |
FUEL @ MPLD | 15.12 | 16.32 | 15.20 | 14.70 | 21.40 | 101.00 | 17.37 | 16.69 | 17.33 | 17.19 | 12.96 | 11.35 |
PLD @ MAXFUEL | 53.69 | 58.29 | 56.07 | 59.91 | 78.21 | 59.63 | 61.99 | 67.66 | 69.11 | 51.64 | 58.33 | |
WEIGHT RATIOS | ||||||||||||
OEW/MTOW | 0.52 | 0.53 | 0.56 | 0.56 | 0.52 | 0.51 | 0.54 | 0.55 | 0.54 | 0.56 | 0.56 | 0.59 |
MPLD/MTOW | 0.26 | 0.26 | 0.23 | 0.25 | 0.26 | 0.00 | 0.25 | 0.25 | 0.26 | 0.25 | 0.26 | 0.27 |
MPLD/OEW | 0.50 | 0.49 | 0.42 | 0.45 | 0.51 | 0.00 | 0.46 | 0.46 | 0.48 | 0.45 | 0.46 | 0.45 |
PAX/OEW | 4.31 | 4.79 | 3.76 | 4.40 | 4.87 | 4.72 | 4.00 | 4.66 | 4.57 | 4.61 | 4.05 | 3.74 |
FuelMAX/MTOW | 0.24 | 0.23 | 0.26 | 0.24 | 0.19 | 0.00 | 0.26 | 0.25 | 0.23 | 0.23 | 0.29 | 0.26 |
MLW/MTOW | 0.83 | 0.82 | 0.85 | 0.85 | 0.80 | 0.00 | 0.82 | 0.84 | 0.84 | 0.85 | 0.87 | 0.90 |
OEW/Seat (t) | 0.23 | 0.21 | 0.27 | 0.23 | 0.21 | 0.21 | 0.25 | 0.21 | 0.22 | 0.22 | 0.25 | 0.27 |
FUSELAGE | ||||||||||||
Fuselage diameter, m | ||||||||||||
Fuselage width, m | 3.7 | 3.7 | 3.95 | 3.95 | 3.95 | 3.95 | 3.76 | 3.76 | 3.76 | 3.76 | 4.06 | 4.06 |
Fuselage height, m | 3.7 | 3.7 | 4.14 | 4.14 | 4.14 | 4.14 | 4.025 | 4.025 | 4.025 | 4.025 | 4.06 | 4.06 |
Finess ratio | 8.57 | 9.51 | 11.27 | 11.27 | 8.63 | 10.21 | 10.9 | TBA | ||||
Seats, single class (high density) | 160 | 190 | 160 | 195 | 244 | 244 | 172 | 210 | 220 | 230 | 165 | 175 |
Seats abreast | 5 | 5 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 | 6 |
Cabin Length (m) | 27.5 | 32.32 | 23.78 | 27.51 | 34.44 | 34.4 | 26.1 | 30 | 32.7 | 34.3 | 26.5 | 31.9 |
Cabin width, m | 3.28 | 3.28 | 3.7 | 3.7 | 3.7 | 3.7 | 3.53 | 3.53 | 3.53 | 3.53 | 3.81 | 3.81 |
Cabin Hight, m | 2.13 | 2.13 | 2.18 | 2.18 | 2.18 | 2.18 | 2.12 | 2.12 | 2.12 | |||
Aisle width, m/in | 0.51/20 | 0.51/20 | 0.48/19 | 0.48/19 | 0.48/19 | 0.48/19 | 0.51/20 | 0.51/20 | 0.51/20 | 0.51/20 | 0.61/24 | 0.61/24 |
Cabin floor area m² | 84 | 99.43 | 82.7 | |||||||||
Passenger Cabin volume, m³ | 120 | 139 | 155 | 155 | ||||||||
Cockpit volume, m³ | 9 | 9 | 9 | 9 | ||||||||
Pressurized Fuselage Volume, m³ | 285 | 330 | 418 | |||||||||
Seat/area | ||||||||||||
Seat/volume | ||||||||||||
Seat/meter cabin | 5.82 | 5.88 | 6.73 | 7.09 | 7.08 | 7.09 | 6.59 | 7.00 | 6.73 | 6.71 | 6.23 | 5.49 |
Passenger deplane pax/min | 18 | 18 | 20 | 20 | 20 | 20 | 18 | 18 | 18 | 18 | ||
Passenger enplane pax/min | 12 | 12 | 12 | 12 | 12 | 12 | 12 | 12 | 12 | 12 | ||
Aircraft Length (m) | 38.7 | 43.52 | 33.84 | 37.57 | 44.51 | 44.51 | 35.56 | 39.52 | 42.16 | 43.8 | 36.8 | 42.2 |
Aircraft Height, m | 11.5 | 11.5 | 11.76 | 11.76 | 11.76 | 11.76 | 12.3 | 12.3 | 12.3 | 12.3 | 11.5 | 11.5 |
WING | ||||||||||||
Wing span, m | 35.1 | 35.9 | 35.8 | 35.8 | 35.8 | 35.8 | 35.9 | 35.9 | 35.9 | 35.9 | 35.9 | 35.9 |
Wing area, m² | 112.3 | 113.5 | 122.6 | 122.6 | 122.4 | 122.4 | 127 | 127 | 127 | 127 | 138 | 138 |
Aspect Ratio | 10.14811 | 10.15 | 10.15 | 10.15 | ||||||||
1/4 chord sweep | 25 | 25 | 25.03 | 25.03 | 25.03 | 25.03 | ||||||
MAC | ||||||||||||
Flap Span/Wing Span | 0.599 | 0.599 | 0.599 | 0.599 | ||||||||
VERTICAL TAIL | ||||||||||||
Area, m² | 28.2 | 26.44 | 26.44 | 26.44 | 26.44 | |||||||
Height, m | 7.16 | 7.16 | 7.16 | 7.16 | ||||||||
Rudder Area, m² | 5.22 | 5.22 | 5.22 | 5.22 | ||||||||
Aspect Ratio | 1.94 | 1.94 | 1.94 | 1.94 | ||||||||
Taper Ratio | 0.271 | 0.271 | 0.271 | 0.271 | ||||||||
1/4 chord sweep | 35 | 35 | 35 | 35 | ||||||||
HORIZONTAL TAIL | ||||||||||||
Tailplane Area, m² | 36.6 | 36.6 | 32.78 | 32.78 | 32.78 | 32.78 | ||||||
Elevators Area, m² | 6.55 | 6.55 | 6.55 | 6.55 | ||||||||
Span, m | 12.263 | 12.263 | 12.45 | 12.45 | 12.45 | 14.35 | 14.35 | 14.35 | 14.35 | |||
Aspect Ratio | 6.16 | 6.16 | 6.16 | 6.16 | ||||||||
Taper Ratio | 0.203 | 0.203 | 0.203 | 0.203 | ||||||||
1/4 chord sweep | 30 | 30 | 30 | 30 | ||||||||
UNDERCARRIAGE | ||||||||||||
Track, m | 6.73 | 6.73 | 7.59 | 7.59 | 7.59 | 7.59 | 5.72 | 5.72 | 5.72 | 5.72 | ||
Wheelbase, m | 14.63 | 18.7 | 12.64 | 16.9 | 16.9 | 12.6 | 15.6 | 17.17 | 18.34 | |||
Turning radius, m | 21.76 | 22.5 | 24.7 | 24.7 | 21.6 | 22.3 | 22.6 | 22.6 | ||||
Tail skid angular clearance, (TO/landing), deg | 13/11 | 10.5/9 | 15.5/13.9 | 13.5/11.7 | 11.2/9.7 | 11/9.2 | 10/8.3 | |||||
BAGGAGE/CARGO | ||||||||||||
Hold capacity, m³ | 31.6 | 42.6 | 44.3 | 50.1 | 32.3 | 43.6 | 51.3 | 55.5 | 34 | 49 | ||
Water volume, FWD CC, m³ | 12.65 | 8.52 | 13.28 | 22.81 | 12.3 | 19 | 23.2 | 25.8 | ||||
Water volume, AFT CC, m³ | 14.81 | 13.91 | 18.26 | 23.03 | 20 | 24.6 | 28.2 | 29.7 | ||||
Water volume, Bulk CC, m³ | n/a | n/a | 7.51 | 5.88 | 5.88 | n/a | n/a | n/a | n/a | |||
Max loading, FWD Cargo Comp,kg | 2446 | 2.268 | 3.4 | 5.67 | ||||||||
Max loading, AFT Cargo Comp, kg | 2606 | 3.021 | 4.536 | 5.67 | ||||||||
Rear (bulk), t | n/a | n/a | 1.497 | 1.497 | 0.8 | n/a | n/a | n/a | n/a | n/a | ||
Container/pallet options | no | no | LD3-45 | LD3-45 | LD3-45 | LD3-45 | no | no | no | no | no | |
Volume per passenger | ||||||||||||
Range, no ACT (NM) | 3350 | 3300 | 3750 | 3500 | 4000 | 4700 | 3850 | 3550 | 2875 | 2700 | 3500 | 3200 |
Speed, M | 0.78 | 0.78 | 0.82 | 0.82 | 0.82 | 0.82 | 0.79 | 0.79 | 0.79 | 0.79 | 0.79 | 0.79 |
LOADINGS | ||||||||||||
MAX wing Load kg/m² | 631.34 | 665.20 | 615.82 | 644.37 | 792.48 | 825.16 | 632.17 | 650.74 | 695.39 | 706.81 | 525.80 | 574.28 |
POWER PLANT | ||||||||||||
Installed thrust, MAX (k lb) | 46.6 | 49.5 | 48.8 | 54 | 66.22 | 66 | 53.58 | 56.06 | 58.64 | 58.64 | 56 | 62 |
Thrust/Weight Ratio | 0.30 | 0.30 | 0.29 | 0.31 | 0.31 | 0.30 | 0.31 | 0.30 | 0.30 | 0.35 | 0.35 | |
Fan Diameter, m/in | 1.854/73 | 2.22/87.57 | 2.22/87.57 | 2.22/87.57 | 2.22/87.57 | 2.22/87.57 | ||||||
BPR | 12 | 12.5 | 12.5 | 12.5 | 12.5 | 11 | 11 | 11 | 11 | 12 | 12 | |
OPR | 50 | 50 | 50 | 50 | 50 | 40 | 40 | 40 | 40 | 50 | 50 | |
Engine type | PW1524G-3 | PW1100G | PW1100G | PW1100G | LEAP-1B | PW1431G | PW1431G | |||||
Engine weight, each, t | 2.177 | 2.177 | 2.86 | 2.86 | 2.86 | 2.78 | 2.86 | 2.86 |