TYPE OF AIRCRAFT

 Range: 1,750 mi (2,820 km, 1,520 nmi)
 Rate of climb: 2,700 ft/min (14 m/s)
 Wing loading: 25.8 lb/sq ft (126 kg/m2)

GULFSTREAM IV

Specifications[edit] GIV-SP[26] G350[27] G450[28]

GIV[26]

Cockpit crew Two

Seating 14-19 19 maximum, 12-16 typical
capacity

Length 88ft 4in / 26.92m 89ft 4in / 27.23m

Wingspan 77ft 10 / 23.72m

Wing area 950.39sqft / 88.3m²

Overall height 24ft 5in / 7.45m 25ft 2in / 7.67m

MTOW 73,200 lb 74,600 lb 70,900 lb 74,600 lb
(33,203 kg) (33,838 kg) (32,160 kg) (33,838 kg)

Empty weight 35,500 lb (16,103 kg) 42,700 lb 43,000 lb
(19,368 kg) (19,504 kg)

Cruising Mach 0.80–Mach 0.85 (459–488 kn; 850–903 km/h)
speed

Maximum Mach 0.88 (505 kn; 935 km/h)
speed

Range 4,220 nmi (7,815 km) 3,800 nmi 4,350 nmi
(7,038 km) (8,056 km)

Service ceiling 45,000 ft (13,716 m)

Engines (×2) Rolls-Royce Tay 611-8 Rolls-Royce Tay 611-8C

Thrust 13,850lbf / 61.6kN

HAAWKER 800

General characteristics

 Crew: 2 + jump seat
 Capacity: 8 / 2,000 lb (907 kg) maximum payload
 Length: 51 ft 2 in (15.60 m)
 Wingspan: 51 ft 4.5 in (15.659 m)
 Height: 17 ft 7 in (5.36 m)
 Wing area: 374 sq ft (34.7 m2)
 Empty weight: 15,600 lb (7,076 kg) basic
 Operating weight empty: 16,000 lb (7,257 kg)
 Maximum ramp weight: 27,520 lb (12,483 kg)
 Maximum zero-fuel weight: 18,000 lb (8,165 kg)
 Max takeoff weight: 27,400 lb (12,428 kg)
 Maximum landing weight: 23,350 lb (10,591 kg)
 Fuel capacity: 1,248 imp gal (1,499 US gal; 5,674 l) total ; 1,060 imp gal (1,273 US gal;

4,819 l) in wing integral tanks + 188 imp gal (226 US gal; 855 l) in rear under-fuselage
tank
 Powerplant: 2 × Honeywell TFE731-5BR turbofan engines, 4,300 lbf (19 kN) thrust
each

Performance

 Maximum speed: 456 kn (525 mph, 845 km/h) max level speed and max cruising speed
at 29,000 ft (8,839 m) / M0.87

 Cruise speed: 400 kn (460 mph, 740 km/h) economical cruise at 39,000–43,000 ft
(11,887–13,106 m)

 Stall speed: 92 kn (106 mph, 170 km/h) in landing configuration at typical landing weight
 Range: 2,580 nmi (2,970 mi, 4,780 km) with max payload
2,825 nmi (3,251 mi; 5,232 km) with max fuel and NBAA VFR reserves

 Service ceiling: 43,000 ft (13,000 m)
 Rate of climb: 3,100 ft/min (16 m/s)
 Wing loading: 73.26 lb/sq ft (357.7 kg/m2)
 Thrust/weight: 0.313
 Take-off balanced field length: 5,620 ft (1,713 m) at MTOW
 Landing distance from 50 ft (15 m): 4,500 ft (1,372 m) at typical landing weight

and 6 pax

BEECHCRAFT SUPER KING AIR

Variant 250[96] 350i[97] 350ER[98]
Crew 10
Capacity 1–2

11

Length 43 ft 10 in / 13.36 m 46 ft 8 in / 14.22 m

Span 57 ft 11 in / 17.65 m

Height 14 ft 10 in / 4.52 m 14 ft 4 in / 4.37 m

Cabin L × W × H 16'8" × 4'6" × 4'9" 19'6" × 4'6" × 4'9"
5.08 × 1.37 × 1.45 m 5.94 × 1.37 × 1.45 m

MTOW 12,500 lb / 5,670 kg 15,000 lb / 6,804 kg 16,500 lb / 7,484 kg

OEW[a] 8,830 lb / 4,005 kg 9,955 lb / 4,516 kg 9,455 lb / 4,289 kg[b]

Useful load 3,760 lb / 1,706 kg 5,145 lb / 2,334 kg 7,145 lb / 3,241 kg

Engine type (2×) PWC PT6A-52 PWC PT6A-60A

Power or Thrust 850 shp / 625 kW 1,050 shp / 783 kW

Maximum Cruise 310 kt / 574 km/h 312 kt / 578 km/h 303 kt / 561 km/h

Ferry Range 1,720 nm / 3,185 km 1,806 nm / 3,345 km 2,670 nm / 4,945 km

Takeoff 2,111 ft / 643 m[c] 350i: 3,300 ft / 1,006 m 4,057 ft / 1,237 m[8]

Ceiling 35,000 ft / 10,668 m

QUEST KODIAK

Brosur [23]

Karakteristik umum

 Kru: 1
 Kapasitas: 9 penumpang
 Panjang: 34 kaki 2 in (10,41 m)
 Rentang Sayap: 45 kaki 0 inci (13,72 m)
 Tinggi: 15 kaki 3 inci (4,65 m)
 Area sayap: 240 kaki persegi (22 m 2 )
 Berat kosong: 3.770 lb (1.710 kg)
 Berat lepas landas maks: 7.255 lb (3.291 kg)
 Pembangkit listrik: 1 × Pratt & Whitney Canada PT6 A-34 turboprop , daya lepas

landas 750 shp (560 kW) (700 shp (520 kW) kontinu)
 Baling -baling: Kecepatan konstan 4 bilah, berbulu, dapat dibalik, diameter 8 ft 0 in (2,44

m)

Performa

 Kecepatan jelajah: 211 mph (339 km / h, 183 kn)
 Kecepatan stall: 69 mph (110 km / h, 60 kn) (flaps down)
 Jangkauan: 1.303 mi (2.096 km, 1.132 nmi)
 Layanan langit-langit: 25.000 kaki (7.600 m)
 Tingkat panjat: 1.371 kaki / mnt (6,96 m / s)
 Jarak lepas landas: 934 kaki (285 m)
 Landing roll: 705 kaki (215 m)

LEARJET 31

Karakteristik umum

 Kru: 2
 Kapasitas: 8 penumpang
 Panjang: 48 kaki 8 inci (14,83 m)
 Rentang Sayap: 43 kaki 10 inci (13,36 m)
 Tinggi: 12 kaki 3 inci (3,73 m)
 Area sayap: 264,5 kaki persegi (24,57 m 2 )
 Berat kosong: 9.857 lb (4.471 kg)
 Berat kotor: 15.500 lb (7.031 kg)
 Pembangkit listrik: 2 × Garrett TFE731 -2 turbofan , masing-masing daya dorong 3,500

lbf (15,6 kN)

Performa

 Kecepatan maksimum: Mach 0.81
 Kecepatan jelajah: 515 mph (829 km / jam, 448 kn)
 Kecepatan berhenti: 97 mph (156 km / jam, 84 kn)
 Jarak tempuh : 1.877 mi (3.021 km, 1.631 nmi) (bahan bakar standar, empat

penumpang,)
 Layanan langit-langit: 51.000 kaki (16.000 m)
 Tingkat panjat: 5,480 kaki / menit (27,8 m / s)

LIBERTY XL2

General characteristics

 Crew: one
 Capacity: one passenger
 Length: 20 ft 3.8 in (6.193 m)
 Wingspan: 28 ft 7.26 in (8.7188 m)
 Height: 7 ft 4.96 in (2.2596 m)
 Wing area: 112.0 sq ft (10.41 m2)
 Airfoil: Dykins 12%
 Empty weight: 1,160 lb (526 kg)
 Gross weight: 1,750 lb (794 kg)
 Powerplant: 1 × Continental IOF-240-B four cylinder horizontally opposed four-stroke

aircraft engine with FADEC control, 125 hp (93 kW)

Performance

 Cruise speed: 125 kn (144 mph, 232 km/h)
 Stall speed: 44 kn (51 mph, 81 km/h) flaps down
 Never exceed speed: 162 kn (186 mph, 300 km/h)
 Range: 500 nmi (580 mi, 930 km)
 Service ceiling: 12,500 ft (3,800 m)
 Rate of climb: 682 ft/min (3.46 m/s)
 Wing loading: 14.76 lb/sq ft (72.1 kg/m2)

MCDONNELL DOUGLAS MD-80

Airplane Characteristics[91]

Variant MD-81/82/83/88 MD-87

Cockpitcrew Two

1-classseats[92] 155Y @32-33" (max 172) 130Y @31-33" (max 139)

2-class seats[92] 143: 12J @ 36" + 131Y@ 31-34" 117: 12J+105Y

Length 147 ft 10 in (45.06 m) 130 ft 5 in (39.75 m)

Wing 107 ft 8 in (32.82 m) span, 1,209 sq ft (112.3 m2) area, aspect ratio: 9.6

Tail height 29 ft 7 in (9.02 m) 30 ft 4 in (9.25 m)

Width 131.6 in / 334.3 cm fuselage, 122.5 in / 311.2 cm cabin

Cargo 1,253 cu ft (35.5 m3) 938 cu ft (26.6 m3)
-83/88: 1,013 cu ft (28.7 m3) 73,300 lb (33,200 kg)

Empty weight 77,900–79,700 lb(35,300–36,200 kg)

MTOW -81: 140,000 lb (63,500 kg) 140,000–149,500 lb (63,500–
-82: 149,500 lb (67,800 kg) 67,800 kg)
-83/88: 160,000 lb (72,600 kg)

Fuel capacity 5,850 US gal (22,100 L) -83/88: 7,000 US gal (26,000 L)

Engines(×2) Pratt & Whitney JT8D-200 series
Thrust (×2) 18,500–21,000 lbf (82–93 kN)

Long- Mach 0.76 (448 kn; 830 km/h)[93]
range Cruise

High-speed Mach 0.8 (472 kn; 873 km/h)[92]
cruise

Range[a] -81: 1,800 nmi(3,300 km) @ 137 pax 2,400–2,900 nmi (4,400–5,400 km)
Takeoff[b] -82: 2,050 nmi (3,800 km) @ 155 pax
-83/88: 2,550 nmi (4,720 km) @ 155

pax

7,200–8,000 ft (2,200–2,400 m) 7,500 ft (2,300 m)

PIAGGIO P.180 AVANTI

Karakteristik umum

 Kru: 1
 Kapasitas: 7–9
 Panjang: 14,4 m (47,3 kaki)
 Rentang Sayap: 14.0 m (46.0 kaki)
 Tinggi: 4,0 m (13,0 kaki)
 Area sayap: 16,0 m 2 (172 kaki persegi)
 Rasio aspek: 12.3
 Berat kosong: 3.799 kg (8.375 lb)
 Berat lepas landas maks: 5.488 kg (12.100 lb)
 Kapasitas bahan bakar: 1.271 kg (2.802 lb)
 Berat pendaratan maks: 5.216 kg (11.500 lb)
 Berat bahan bakar nol maks: 4.445 kg (9.800 lb)
 Kabin: panjang 17,5 kaki, tinggi 5,8 kaki, lebar 6,1 kaki (lantai 3,5 kaki)
 Area pesawat depan: 2,19 m² (23,59 kaki²) [37]
 Area stabilizer horizontal: 3,83 m² (41,27 kaki²) [37]
 Pembangkit listrik: 2 × Pratt & Whitney Canada PT6 A-66B turboprop , 630 kW (850

shp) masing-masing ISA + 28C Flat Rated

Performa

 Kecepatan maksimum: 740 km / jam (460 mph, 400 kn) jelajah kecepatan tinggi FL310
 Kecepatan jelajah: 589 km / jam (366 mph, 318 kn) pelayaran jarak jauh FL410
 Kecepatan kontrol minimum : 190 km / jam (120 mph, 100 kn) Vmca
 Jangkauan: 2.800 km (1.740 mi, 1.510 nmi) 4 penumpang, NBAA IFR, 100-nm

bergantian
 Kisaran feri: 2.830 km (1.760 mi, 1.530 nmi)
 Layanan langit-langit: 12.000 m (41.000 kaki)
 Waktu menuju ketinggian: 10 menit hingga FL 250
 Beban sayap: 343 kg / m 2 (70,3 lb / kaki persegi)
 Konsumsi bahan bakar: 0,220 kg / km (0,779 lb / mi)
 Tenaga / massa : 230 W / kg (0,14 hp / lb)

 Lepas landas (SL, ISA): 994 m (3.262 kaki)

PIPER PA-28 CHEROKEE

General characteristics

 Crew: one
 Capacity: three passengers
 Length: 23 ft 3.6 in (7.102 m)
 Wingspan: 30 ft 0 in (9.14 m)
 Height: 7 ft 3.6 in (2.225 m)
 Wing area: 160 sq ft (15 m2)
 Airfoil: NACA 652-415[55]
 Empty weight: 1,201 lb (545 kg)
 Gross weight: 2,150 lb (975 kg)
 Max takeoff weight: 2,150 lb (975 kg)
 Powerplant: 1 × Lycoming O-320-E2A 4-cylinder air-cooled horizontally-opposed piston

engine, 150 hp (110 kW)
 Propellers: Sensenich M74DM

Performance

 Maximum speed: 123 kn (142 mph, 228 km/h)
 Cruise speed: 108 kn (124 mph, 200 km/h)
 Stall speed: 47 kn (54 mph, 87 km/h)
 Range: 465 nmi (535 mi, 861 km)
 Service ceiling: 14,300 ft (4,400 m)
 Rate of climb: 660 ft/min (3.4 m/s)
 Wing loading: 13.4 lb/sq ft (65 kg/m2)
 Power/mass: 0.0699 hp/lb (0.1149 kW/kg)

PIPER PA-32

General characteristics

 Crew: One
 Capacity: five passengers (or six with optional seat)
 Length: 27 ft 8 in (8.4 m)
 Wingspan: 32 ft 10 in (10.0 m)
 Height: 7 ft 11 in (2.4 m)
 Wing area: 174.5 sq ft (16.5 m2)
 Airfoil: NACA 65-415
 Empty weight: 1,788 lb (811 kg)
 Gross weight: 3,400 lb (1,542 kg)
 Powerplant: 1 × Lycoming IO-540-K1A5 piston, flat six, 300 hp (225 kW)

Performance

 Maximum speed: 174 mph (280 km/h, 151 kn)
 Cruise speed: 168 mph (272 km/h, 146 kn)
 Range: 840 mi (1,361 km, 730 nmi)
 Service ceiling: 16,250 ft (4,950 m)
 Rate of climb: 1,050 ft/min (5.3 m/s)

PIPER PA-44 SEMINOLE

General characteristics

 Crew: 1
 Capacity: 3 passengers
 Length: 27 ft 7 1⁄4 in (8.414 m)
 Wingspan: 38 ft 7 1⁄4 in (11.767 m)
 Height: 8 ft 6 in (2.59 m)
 Wing area: 183.8 sq ft (17.08 m2)
 Airfoil: NACA 652-415[11]
 Empty weight: 2,354 lb (1,068 kg)
 Max takeoff weight: 3,800 lb (1,724 kg)
 Fuel capacity: 110 US gal (92 imp gal; 420 L), of which 2 US gal (1.7 imp gal; 7.6 L) are

unusable
 Powerplant: 2 × Lycoming O-360-E1A6 air-cooled flat four(counter rotating), 180 hp

(130 kW) each
 Propellers: 2-bladed Hartzell fully-feathering metal constant-speed propellers, 6 ft 2 in

(1.88 m) diameter

Performance

 Maximum speed: 193 mph (311 km/h, 168 kn)
 Cruise speed: 187 mph (301 km/h, 162 kn) (75% power)

 Stall speed: 68 mph (109 km/h, 59 kn) (flaps down) CAS
 Range: 1,053 mi (1,695 km, 915 nmi) (55% power)
 Service ceiling: 17,100 ft (5,200 m)
 Rate of climb: 1,340 ft/min (6.8 m/s)
 Single Engine Service Ceiling: 4,100 ft (1,200 m)
 Take-off to 50 ft (15 m): 1,400 ft (430 m)
 Landing from 50 ft (15 m): 1,190 ft (360 m)

PIPER PA-34 SENECA

Karakteristik umum

 Kru: Satu
 Kapasitas: Lima atau enam penumpang
 Panjang: 28 kaki 7,44 inci (8,72 m)
 Rentang Sayap: 38 kaki 10,87 inci (11,86 m)
 Tinggi: 9 kaki 10,8 inci (3,02 m)
 Area sayap: 208,7 kaki persegi (19,39 m 2 )
 Airfoil : aliran laminar NACA 652-415
 Berat kosong: 3,212 lb (1,457 kg)
 Berat kotor: 4.773 lb (2.165 kg)
 Berat lepas landas maks: 4.750 lb (2.155 kg)
 Mesin: 2 × Continental TSIO-360RB dan LTSIO-360RB 6 silinder, berpendingin

udara, mesin piston horizontal, masing-masing 220 hp (164 kW)

Performa

 Kecepatan maksimum: 204 kn (235 mph, 378 km / h) pada 23.000 kaki (7.000 m)
 Kecepatan jelajah: pelayaran econ 188 kn (216 mph, 348 km / jam) pada 25.000 kaki

(7.600 m)
 Kecepatan berhenti: Roda 61 kn (70 mph, 113 km / h) dan flaps ke bawah
 Jangan pernah melebihi kecepatan : 204 kn (235 mph, 378 km / h)

 Jangkauan: bahan bakar maks 870 nmi (1.000 mi, 1.611 km), pelayaran econ pada
ketinggian 18.000 kaki (5.500 m), tanpa cadangan

 Layanan langit-langit: 25.000 kaki (7.620 m)
 Tingkat pendakian: 1.550 kaki / menit (7,87 m / s)
 Wing memuat: 21,2 lb / sq ft (104 kg / m 2 )
 Tenaga / massa : 0,1 hp / lb (164 W / kg)

PAC P-750 XSTOL

General characteristics

 Crew: one (pilot)
 Capacity: Pilot + nine passengers or 17 parachutists [4]
 Length: 11.11 m (36 ft 5 in)
 Wingspan: 12.8 m (42 ft 0 in)
 Height: 3.88 m (12 ft 9 in)
 Wing area: 24.88 m2 (267.8 sq ft)
 Aspect ratio: 6.59
 Empty weight: 1,633 kg (3,600 lb)
 Gross weight: 3,402 kg (7,500 lb)
 Powerplant: 1 × Pratt & Whitney PT6A-34 turboprop, 560 kW (750 hp)

Performance

 Maximum speed: 315 km/h (196 mph, 170 kn)
 Cruise speed: 259 km/h (161 mph, 140 kn)
 Stall speed: 107 km/h (66 mph, 58 kn) Idle Power, Flaps Down
 Range: 2,183 km (1,356 mi, 1,179 nmi)
 Endurance: 8h
 Service ceiling: 6,096 m (20,000 ft)
 Rate of climb: 5.42 m/s (1,067 ft/min)
 Take-Off Ground Roll: 721 ft / 220 m (ISA, SL)

 Landing Ground Roll: 543 ft / 166 m (SL)

PILATUS PC-6 PORTER

General characteristics

 Crew: 1
 Capacity: up to 10 pax / 1,130 kg (2,491 lb)
 Length: 11 m (36 ft 1 in)
 Wingspan: 15.87 m (52 ft 1 in)
 Height: 3.2 m (10 ft 6 in)
 Wing area: 30.15 m2 (324.5 sq ft)
 Airfoil: NACA 64-514[55]
 Empty weight: 1,270 kg (2,800 lb)
 Max takeoff weight: 2,800 kg (6,173 lb)
 Powerplant: 1 × Pratt & Whitney Canada PT6A-27 turboprop engine, 410 kW (550 hp)

(de-rated from 507 kW (680 hp))
 Propellers: 3-bladed constant-speed reversible propeller

Performance

 Maximum speed: 232 km/h (144 mph, 125 kn) [56]
 Cruise speed: 213 km/h (132 mph, 115 kn)
 Stall speed: 96 km/h (60 mph, 52 kn)
 Never exceed speed: 280 km/h (170 mph, 150 kn)
 Range: 730 km (450 mi, 390 nmi) with maximum payload
 Ferry range: 1,612 km (1,002 mi, 870 nmi) with maximum internal and underwing fuel
 Service ceiling: 8,197 m (26,893 ft)
 Wing loading: 93 kg/m2 (19 lb/sq ft)

AMERICAN CHAMPION DECATHLON

General characteristics

 Crew: one
 Capacity: one passenger
 Length: 22.9 ft (7.0 m)
 Wingspan: 32 ft (9.8 m)
 Height: 7.7 ft (2.3 m)
 Wing area: 169.1 sq ft (15.71 m2)
 Empty weight: 1,340 lb (608 kg)
 Gross weight: 1,950 lb (885 kg) (normal category)
 Fuel capacity: 40 U.S. gallons (150 L; 33 imp gal)
 Powerplant: 1 × Lycoming AEIO-360-H1B four cylinder horizontally-opposed aircraft

engine, 180 hp (130 kW)
 Propellers: Hartzell Propeller HC-C2YR-4CF/FC7666A-2
 Propellers: 6 ft 2 in (1.88 m) diameter

Performance

 Maximum speed: 155 mph (249 km/h, 135 kn) at sea level
 Cruise speed: 141 mph (227 km/h, 123 kn)
 Stall speed: 53 mph (85 km/h, 46 kn) (clean)
 Never exceed speed: 200 mph (320 km/h, 170 kn)
 Endurance: 3.4 hours at 75% power
 Service ceiling: 15,800 ft (4,800 m)
 g limits: +6/-5
 Rate of climb: 1,280 ft/min (6.5 m/s)

 Wing loading: 10.64 lb/sq ft (51.9 kg/m2)
 Power/mass: 10 lb/hp

SOCATA TB FAMILY

General characteristics

 Crew: 1
 Capacity: 3-4
 Length: 7.63 m (25 ft 0 in)
 Wingspan: 9.76 m (32 ft 0 in)
 Height: 3.2 m (10 ft 6 in)
 Wing area: 11.9 m2 (128 sq ft)
 Airfoil: RA 16.3C3[26]-->
 Empty weight: 670 kg (1,477 lb)
 Max takeoff weight: 1,150 kg (2,535 lb)
 Fuel capacity: 210 l (55 US gal; 46 imp gal) in two wing leading edge tanks ; 7.5 l

(2.0 US gal; 1.6 imp gal) Oil
 Powerplant: 1 × Lycoming O-360-A1AD 4-cylinder air-cooled horizontally-opposed

piston engine, 134 kW (180 hp)
 Propellers: 2-bladed Hartzell constant-speed propeller, 1.88 m (6 ft 2 in) diameter

Performance

 Maximum speed: 247 km/h (153 mph, 133 kn)
 Cruise speed: 235 km/h (146 mph, 127 kn) max
217 km/h (135 mph; 117 kn) econ.

 Stall speed: 112 km/h (70 mph, 60 kn) flaps up
97 km/h (60 mph; 52 kn) flaps down

 Range: 1,210 km (750 mi, 650 nmi) max standard fuel t/o, climb, descent, 45
minutes reserve

 Service ceiling: 3,960 m (12,990 ft)
 Rate of climb: 4 m/s (790 ft/min) at sea level

TECNAM P2006T

General characteristics

 Crew: 1 (pilot)
 Capacity: 3 passengers or 618 pounds (280 kg) payload with full fuel
 Length: 8.69 m (28 ft 6 in)
 Wingspan: 11.40 m (37 ft 5 in)
 Height: 2.84 m (9 ft 4 in)
 Wing area: 14.75 m2 (158.8 sq ft)
 Aspect ratio: 8.80
 Empty weight: 760 kg (1,675 lb)
 Max takeoff weight: 1,230 kg (2,712 lb)
 Fuel capacity: 200 litres (44 imp gal; 53 US gal)
 Powerplant: 2 × Rotax 912S3 horizontally opposed four-cylindergeared piston engines,

75 kW (100 hp) each
 Propellers: 2-bladed MT Propeller MTV-21, 1.78 m (5 ft 10 in) diameter constant-speed,

fully feathering

Performance

 Maximum speed: 287 km/h (178 mph, 155 kn)
 Cruise speed: 250 km/h (155 mph, 135 kn)
 Stall speed: 87 km/h (54 mph, 47 kn)

 Never exceed speed: 309 km/h (192 mph, 167 kn)
 Minimum control speed: 115 km/h (71 mph, 62 kn)
 Range: 1,374 km (853 mi, 742 nmi)
 Endurance: 4.25 hours
 Service ceiling: 4,300 m (14,000 ft)
 Rate of climb: 6.4 m/s (1,260 ft/min) 250 ft/min (single engine)
 Wing loading: 78 kg/m2 (16 lb/sq ft) at MTOW
 Power/mass: 0,162 hp/kg (0,07 hp/lb)

EUROCOPTER AS332 SUPER PUMA

Karakteristik umum

 Kru: 2
 Kapasitas: 24 penumpang ditambah petugas / 4.490 kg (9.899 lb)
 Panjang: badan pesawat 16,79 m (55 ft 1 in)

Putaran rotor 18,7 m (61 kaki)
 Tinggi: 4,97 m (16 kaki 4 inci)
 Berat kosong: 4.660 kg (10.274 lb)
 Berat lepas landas maks: 9.150 kg (20.172 lb)
 Pembangkit listrik: 2 × Turbomeca Makila 1A1 turboshaft , masing-masing 1.376 kW

(1.845 hp)
 Diameter rotor utama: 16,2 m (53 kaki 2 in)
 Area rotor utama: 206,12 m 2 (2,218,7 kaki persegi)
 Bagian bilah: root: NACA 13112 ; tip: NACA 13106 [93]

Performa

 Kecepatan jelajah: 277 km / jam (172 mph, 150 kn) maks,
247 km / jam (153 mph; 133 kn) econ.

 Jangan pernah melebihi kecepatan : 327 km / jam (203 mph, 177 kn)
 Jarak tempuh : 851 km (529 mi, 460 nmi)
 Layanan langit-langit: 5.180 m (16.990 kaki)
 Tingkat panjat: 7,4 m / s (1.460 kaki / menit)

EUROCOPTER AS350 ÉCUREUIL

General characteristics

 Crew: 1
 Capacity: 5 pax

 4, 5, & 6 passengers options available.[100] The 6 passenger configuration
replaces the single passenger forward seat with a two-person bench seat[101]

 Length: 10.93 m (35 ft 10 in) (fuselage)
 Height: 3.145 m (10 ft 4 in)
 Empty weight: 1,174 kg (2,588 lb)
 Max takeoff weight: 2,250 kg (4,960 lb)
 Powerplant: 1 × Turbomeca Arriel 2Bturboshaft engine, 632 kW (848 hp)
 Main rotor diameter: 10.7 m (35 ft 1 in)
 Main rotor area: 89.75 m2 (966.1 sq ft)

Performance

 Cruise speed: 245 km/h (152 mph, 132 kn)
 Never exceed speed: 287 km/h (178 mph, 155 kn)
 Range: 662 km (411 mi, 357 nmi)
 Endurance: 4 hours 6 minutes
 Service ceiling: 4,600 m (15,100 ft)
 Rate of climb: 8.5 m/s (1,670 ft/min)

AGUSTA WESTLAND AW109

Karakteristik umum

 Kru: 1 atau 2
 Kapasitas: 6 atau 7 penumpang
 Panjang: badan pesawat 11.448 m (37 kaki 7 inci)
 Tinggi: 3,50 m (11 kaki 6 inci)
 Berat kosong: 1.590 kg (3.505 lb)
 Berat lepas landas maks: 2.850 kg (6.283 lb)
 Pembangkit listrik: Mesin 2 × Pratt & Whitney Canada PW206C Turboshaft, masing-

masing 418 kW (560 hp)
 Diameter rotor utama: 11,00 m (36 kaki 1 inci)

Performa

 Kecepatan maksimum: 311 km / jam (193 mph, 168 kn)
 Kecepatan jelajah: 285 km / jam (177 mph, 154 kn)
 Jangan pernah melebihi kecepatan : 311 km / jam (193 mph, 168 kn)
 Kisaran feri: 932 km (579 mi, 503 nmi)
 Tingkat panjat: 9,8 m / s (1.930 kaki / menit)

AGUSTA WESTLAND AW109S GRAND

Karakteristik umum

 Kru: 1 atau 2
 Kapasitas: 6 atau 7 penumpang
 Panjang: badan pesawat 12,96 m (42 kaki 6 inci)
 Tinggi: 3,4 m (11 kaki 2 inci)
 Berat lepas landas maks: 3.175 kg (7.000 lb) MTOW internal
 Pembangkit listrik: Mesin 2 × Pratt & Whitney Canada PW207C Turboshaft, masing-

masing 548 kW (735 hp)
 Diameter rotor utama: 10,83 m (35 kaki 6 in)

Performa

 Kecepatan maksimum: 311 km / jam (193 mph, 168 kn)
 Kecepatan jelajah: 289 km / jam (180 mph, 156 kn)
 Jangan pernah melebihi kecepatan : 311 km / jam (193 mph, 168 kn)
 Kisaran feri: 859 km (534 mi, 464 nmi)
 Layanan langit-langit: 4.900 m (16.200 kaki)
 Tingkat panjat: 9,3 m / s (1.830 kaki / menit)

AGUSTA WESTLAND AW119 KOALA

Karakteristik umum

 Kru: 1-2
 Kapasitas: 6-7 penumpang atau beban selempang 1.400 kg (3.086 lb)
 Panjang: 12,92 m (42 kaki 5 inci)
 Tinggi: 3,60 m (11 kaki 10 inci)
 Berat kosong: 1.483 kg (3.269 lb)
 Berat lepas landas maks: 2.850 kg (6.283 lb)
 Kapasitas bahan bakar:

Sistem bahan bakar 3-sel 605 l (160 US gal)
Sistem bahan bakar 4-sel 711 l (188 US gal)
Sistem bahan bakar 5-sel 870 l (230 US gal)
 Pembangkit listrik: 1 × Pratt & Whitney Canada PT6 B-37A mesin turboshaft, 747 kW
(1.002 hp)
 Diameter rotor utama: 10,83 m (35 kaki 6 in)
 Area rotor utama: 92,1 m 2 (991 kaki persegi)

Performa

 Kecepatan jelajah: 244 km / jam (152 mph, 132 kn)
 Jangan pernah melebihi kecepatan : 282 km / jam (175 mph, 152 kn)
 Jarak tempuh : 954 km (593 mi, 515 nmi)
 Daya Tahan: 5 jam 20 menit
 Layanan langit-langit: 4.572 m (15.000 kaki)
 Tingkat panjat: 9,1 m / s (1.790 kaki / menit)

AGUSTA WESTLAND AW139

Karakteristik umum

 Kru: satu atau dua
 Kapasitas: hingga 15 penumpang, tergantung konfigurasi
 Panjang: 16,66 m (54 kaki 8 inci)
 Lebar: 2,26 m (10 kaki 0 inci)
 Tinggi: 4,98 m (16 kaki 4 inci)
 Berat kotor: 6.400 kg (14.110 lb); 7.000 kg (15.000 lb) untuk versi 7 ton
 Kapasitas bahan bakar: 1568 liter (414 USgal)
 Pembangkit listrik: mesin turboshaft 2 × Pratt & Whitney Canada PT6C-67C , masing-

masing 1.142 kW (1.531 hp)
 Diameter rotor utama: 13,80 m (45 kaki 3 in)

Performa

 Kecepatan maksimum: 310 km / jam (193 mph, 167 kn)
 Kecepatan jelajah: 306 km / jam (191 mph, 165 kn)
 Jangkauan: 1.061 km (659 mil, 573 nmi)
 Daya tahan: 5 jam 13 menit
 Layanan langit-langit: 6.096 m (20.000 kaki)
 Tingkat panjat: 10,9 m / s (2.140 kaki / menit)

AGUSTA WESTLAND AW189

General characteristics

 Crew: 1 or 2
 Capacity: Up to 19 passengers
 Length: 17.60 m (57 ft 9 in) [50]
 Height: 5.06 m (16 ft 7 in)
 Wing area: 53.3 m2 (574 sq ft)
 Gross weight: 8,300 kg (18,300 lb)
 Fuel capacity: 2,063 litres (2,569 l with belly tank)
 Powerplant: 2 × General Electric CT7-2E1 turboshaft engine , 1,492 kW (2,000 hp)

each
 Main rotor diameter: 14.60 m (47 ft 11 in)

Performance

 Maximum speed: 313 km/h (194 mph, 169 kn)
 Cruise speed: 267–278 km/h (166–173 mph, 144–150 kn)
 Range: 370–907 km (230–490 mi, 200–430 nmi) [51][23]
 Service ceiling: 3,000 m (10,000 ft)

BELL206

General characteristics

 Crew: 1
 Capacity: 4 passengers
 Length: 39 ft 8 in (12.09 m)
 Height: 9 ft 4 in (2.84 m)
 Empty weight: 2,331 lb (1,057 kg)
 Max takeoff weight: 3,350 lb (1,520 kg)
 Powerplant: 1 × Allison 250-C20J turboshaft engine, 317 shp (236 kW)
(de-rated from 420 shp (313 kW) due to drivetrain limitations)

 Main rotor diameter: 33 ft 4 in (10.16 m)
 Main rotor area: 872 sq ft (81.0 m2)
 Blade section: - NACA 0012 mod (11.3%)[62]

Performance

 Maximum speed: 120 kn (140 mph, 220 km/h)
 Never exceed speed: 130 kn (150 mph, 240 km/h)
 Range: 374 nmi (430 mi, 693 km)
 Service ceiling: 13,500 ft (4,100 m)
 Rate of climb: 1,350 ft/min (6.9 m/s)
 Disk loading: 4 lb/sq ft (20 kg/m2)

 Power/mass: 0.26 hp/lb (0.43 kW/kg)

BELL 212

Karakteristik umum

 Kru: 1 (dua untuk operasi IFR )
 Kapasitas: 14 penumpang
 Panjang: 57 kaki 1,68 inci (17,4163 m)
 Tinggi: 12 kaki 6,83 inci (3,8311 m)
 Berat kosong: 6.529 lb (2.962 kg)
 Berat lepas landas maks: 11.200 lb (5.080 kg)
 Pembangkit listrik: 1 × Pratt & Whitney Canada PT6T-3 atau -3B mesin turboshaft ,

1.800 shp (1.300 kW) (TwinPac)
 Diameter rotor utama: 48 ft 0 in (14,63 m)
 Area rotor utama: 168,11 m 2 (1,809,5 kaki persegi )
 Bagian Pisau: root: NACA 0010.8 ; tip: NACA 0005.4 mod [18]

Performa

 Kecepatan jelajah: 100 kn (120 mph, 190 km / h)
 Jangan pernah melebihi kecepatan : 120 kn (140 mph, 220 km / h)
 Jarak tempuh : 237 nmi (273 mi, 439 km)
 Layanan langit-langit: 17.400 kaki (5.300 m)
 Tingkat panjat: 1.745 kaki / mnt (8,86 m / s)
 Pemuatan disk: 6,19 lb / kaki persegi (30,2 kg / m 2 )

BELL 407

General characteristics

 Crew: one pilot
 Capacity: Typical seating configuration for seven comprising pilot and passengers, with

five passengers in main cabin / 2,347 lb (1,065 kg) internal payload / Max hook capacity
1,200 kg (2,646 lb).[4]
 Length: 41 ft 8 in (12.70 m)
 Height: 11 ft 8 in (3.56 m)
 Max takeoff weight: 6,000 lb (2,722 kg)
 Powerplant: 1 × Allison 250-C47B turboshaft engine, 813 shp (606 kW)
 Main rotor diameter: 35 ft 0 in (10.67 m)
 Main rotor area: 962 sq ft (89.4 m2)
 Blade section: - root: Boeing VR-7 ; tip: Narramore 8%[37]

Performance

 Maximum speed: 140 kn (160 mph, 260 km/h)
 Cruise speed: 133 kn (153 mph, 246 km/h)
 Range: 324 nmi (373 mi, 600 km)
 Service ceiling: 18,690 ft (5,700 m)

BELL 412

General characteristics

 Crew: one-two pilots
 Capacity: up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[3]
 Length: 56 ft 1 in (17.09 m) including rotors
 Fuselage length: 43 ft (13 m)
 Height: 15 ft 0 in (4.57 m)
 Empty weight: 6,789 lb (3,079 kg)
 Max takeoff weight: 11,900 lb (5,398 kg)
 Powerplant: 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac

coupled turboshaft engine, 1,250 shp (930 kW)

900 shp (671 kW) single power section emergency power
 Main rotor diameter: 46 ft 0 in (14.02 m)
 Main rotor area: 1,662 sq ft (154.4 m2) *Blade sections: - root Boeing VR-

7 ; tip Wortmann FX 71-H-080[54]

Performance

 Maximum speed: 140 kn (160 mph, 260 km/h)
 Cruise speed: 122 kn (140 mph, 226 km/h)
 Range: 529 nmi (609 mi, 980 km)
 Service ceiling: 20,000 ft (6,100 m)
 Rate of climb: 1,350 ft/min (6.9 m/s)
 Power/mass: 0.2663 hp/lb (0.4378 kW/kg

BELL 427

General characteristics

 Crew: 2
 Capacity: 7 passengers / 2,960 lb (1,343 kg) internal load
 Length: 37 ft 6 in (11.43 m)
 Height: 10 ft 6 in (3.20 m) with standard skids[13]
 Empty weight: 3,881 lb (1,760 kg)
 Max takeoff weight: 6,550 lb (2,971 kg)
 Powerplant: 2 × Pratt & Whitney Canada PW207D turboshaftengines, 710 shp

(530 kW) each
 Main rotor diameter: 37 ft 0 in (11.28 m)
 Main rotor area: 1,075 sq ft (99.9 m2)
 Blade section: - root: Boeing VR-7 ; tip: Narramore 8%[15]

Performance

 Maximum speed: 140 kn (160 mph, 260 km/h)
 Cruise speed: 138 kn (159 mph, 256 km/h)
 Range: 394 nmi (453 mi, 730 km)
 Service ceiling: 10,000 ft (3,000 m)
 Rate of climb: 2,000 ft/min (10 m/s)

BELL 429 GLOBALRANGER

General characteristics

 Crew: 1 pilot
 Capacity: 7 passengers (six in passenger compartment; one beside pilot)[9] / 2,755 lb

(1,250 kg) payload
 Length: 41 ft 8 in (12.70 m)
 Height: 13 ft 3 in (4.04 m)
 Cabin volume: 204 cu ft (5.78 m3)
 Empty weight: 4,245 lb (1,925 kg)
 Max takeoff weight: 7,000 lb (3,175 kg)
 Fuel capacity: 215 US gal (179 imp gal; 814 l) usable with 40 US gal (33 imp gal; 151 l)

auxiliary fuel
 Powerplant: 2 × Pratt & Whitney Canada PW207D1 (or PW207D2 with fuel heater

installed) turboshaft, 625 shp (466 kW) each maximum continuous
730 shp (544 kW) for take-off[9]

 Main rotor diameter: 36 ft (11 m)
 Main rotor area: 1,018 sq ft (94.6 m2)
 Blade section: - Narramore[58]

Performance

 Cruise speed: 150 kn (170 mph, 280 km/h)
 Never exceed speed: 155 kn (178 mph, 287 km/h) [9]
 Range: 390 nmi (450 mi, 720 km)

 Service ceiling: 20,000 ft (6,100 m)
 Hover ceiling IGE: 14,130 ft (4,307 m)
 Hover ceiling IGE: 11,280 ft (3,438 m)

BELL 430

Bell 230 and Bell 430 comparison

Model 230 430
Announced
First Flight 1990 1991

Certified August 12, 1991 October 25, 1994
Delivered
March 1992 February 23, 1996

November 1992 1996

Seats 2 (pilot & copilot) + 5–6 passengers 2 + 6–8

Height 11 ft 8 in (3.56 m) 12 ft 3 in (3.73 m)

Fuselage length 42 ft 3 in (12.88 m) 44 ft 1 in (13.44 m)

Rotor diameter 42 ft (12.80 m)

Length overall 50 ft 3 in (15.32 m)

Engine (2×) Allison 250C30G2 Rolls-Royce 250-C40B

Power (2×) 700 hp (520 kW) 783 hp (584 kW)

Max. speed 140 knots (161 mph, 260 km/h) 140 knots (161 mph, 260 km/h)

Climb rate 1,600 ft/min (8.13 m/s) 1,350 ft/min (6.86 m/s)

Service ceiling 15,500 ft (4,724 m) 14,600 ft (4,450 m)

Hover ceiling 12,400 ft (3,780 m) 11,350 ft (3,459 m)

Fuel capacity 188+ US gal (710+ L) 188+ US gal (710+ L)

Range 378 nmi (434 mi, 700 km) 324 nmi (372 mi, 600 km)

Empty Weight 5,097 lb (2,312 kg) 5,305 lb (2,406 kg)

Maximum Takeoff Weight 8,400 lb (3,810 kg) 9,300 lb (4,218 kg)

Serial Numbers 23001–23038 49001–49123+

BELL 505 JET RANGER X

General characteristics

 Crew: one pilot[10]
 Capacity: four passengers[10]
 Length: 42 ft 5 in (12.93 m)
 Height: 10 ft 8 in (3.25 m)
 Empty weight: 2,180 lb (989 kg)
 Max takeoff weight: 3,680 lb (1,669 kg) (Internal load), 4,475 lb (2,030 kg) (external

load)
 Useful load: 1,500 lb (680 kg)
 Powerplant: 1 × Safron Arrius 2R turboshaft, 505 shp (377 kW)
 Main rotor diameter: 37 ft 0 in (11.28 m)
 Main rotor area: 1,075 sq ft (99.9 m2)

Performance

 Maximum speed: 144 mph (232 km/h, 125 kn) (max cruise)

 Range: 383 mi (617 km, 333 nmi) at 4,000 ft (1,200 m)
 Service ceiling: 18,610 ft (5,670 m) at 3,680 lb (1,670 kg)

MBB BO 105

Karakteristik umum

 Kru: 1 atau 2 pilot
 Kapasitas: 3 atau 4 penumpang
 Panjang: 11,86 m (38 kaki 11 in) (panjang total - termasuk rotor)
 Tinggi: 3,00 m (9 kaki 10 inci)
 Airfoil : NACA 23012
 Berat kosong: 1.276 kg (2.813 lb)
 Berat lepas landas maks: 2.500 kg (5.512 lb)
 Kapasitas bahan bakar: 570 L (150 US gal; 130 imp gal)
 Pembangkit listrik: Mesin turboshaft 2 × Allison 250 -C20B , masing-masing 310 kW

(420 shp)
 Diameter rotor utama: 9,84 m (32 kaki 3 in)
 Area rotor utama: 76,05 m 2 (818,6 kaki persegi)

Performa

 Kecepatan maksimum: 242 km / jam (150 mph, 131 kn)
 Kecepatan jelajah: 204 km / jam (127 mph, 110 kn) (pelayaran jangkauan terbaik)
 Jangan pernah melebihi kecepatan : 270 km / jam (170 mph, 150 kn)
 Jangkauan: 657 km (408 mi, 355 nmi) pada 1.525 m (5.000 kaki) (bahan bakar standar,

muatan maksimum)
 Kisaran feri: 1.112 km (691 mi, 600 nmi) pada 1.525 m (5.000 kaki) (dengan tangki

tambahan)
 Daya tahan: 3 jam 30 menit (bahan bakar standar, muatan maksimum)
 Layanan langit-langit: 5.200 m (17.000 kaki)

 Tingkat panjat: 8,00 m / s (1,575 kaki / menit)

Persenjataan

 Rudal: 6x Euromissile HOT (Bo 105 P) atau 8x BGM-71 TOW

EUROCOPTER EC130

General characteristics

 Crew: 1
 Capacity: 6 passengers (2 at front and four in the rear) can be modified to take 7

passengers (3 at front and four in the rear)
 Length: 10.68 m (35 ft 0 in)
 Height: 3.34 m (10 ft 11 in)
 Empty weight: 1,377 kg (3,036 lb)
 Max takeoff weight: 2,427 kg (5,351 lb)
 Fuel capacity: 540 l (140 US gal; 120 imp gal)
 Usable fuel: 538.7 l (142.3 US gal; 118.5 imp gal)1
 Powerplant: × Turbomeca Arriel 2B1turboshaft engine, 632 kW (848 hp)
 Main rotor diameter: 10.69 m (35 ft 1 in)
 Main rotor area: 89.75 m2 (966.1 sq ft) three blades

Performance

 Cruise speed: 240 km/h (150 mph, 130 kn)
 Never exceed speed: 287 km/h (178 mph, 155 kn) power on (less 3 kt/1 000 ft)
231.5 km/h (143.8 mph; 125.0 kn) power off (less 3 kt/1 000 ft)

 Range: 610 km (380 mi, 330 nmi)
 Service ceiling: 7,010 m (23,000 ft) max permitted in cruise
 Rate of climb: 9 m/s (1,800 ft/min)

EUROCOPTER EC135

General characteristics

 Crew: 1 pilot
 Capacity: up to seven passengers or two crew and two patients (Air Ambulance variant)

or 1,455 kg (3,208 lb) payload
 Length: 10.2 m (33 ft 6 in)
 Height: 3.51 m (11 ft 6 in)
 Empty weight: 1,455 kg (3,208 lb)
 Max takeoff weight: 2,910 kg (6,415 lb)
 Powerplant: 2 × Turbomeca Arrius 2B2turboshaft engines, 472 kW (633 hp) each

or 2 x Pratt & Whitney Canada PW206Bturboshaft engines rated at 463 kW (621 hp)
(take-off power)
 Main rotor diameter: 10.2 m (33 ft 6 in)
 Main rotor area: 81.7 m2 (879 sq ft)

Performance

 Cruise speed: 254 km/h (158 mph, 137 kn)
 Never exceed speed: 287 km/h (178 mph, 155 kn)
 Range: 635 km (395 mi, 343 nmi)
 Service ceiling: 6,096 m (20,000 ft)
 Rate of climb: 7.62 m/s (1,500 ft/min)

EUROCOPTER EC155

General characteristics

 Crew: 1 or 2 (pilots)
 Capacity: 13 passengers or 2,301 kg (5,073 lb) payload
 Length: 14.3 m (46 ft 11 in)
 Height: 4.35 m (14 ft 3 in)
 Empty weight: 2,618 kg (5,772 lb)
 Gross weight: 4,950 kg (10,913 lb)
 Max takeoff weight: 4,920 kg (10,847 lb)
 Powerplant: 2 × Turbomeca Arriel 2C2 turboshaft engines, Take-off Power, 697 kW

(935 hp) each
 Main rotor diameter: 12.6 m (41 ft 4 in)
 Main rotor area: 124.7 m2 (1,342 sq ft)

Performance

 Never exceed speed: 324 km/h (201 mph, 175 kn)
 Range: 857 km (533 mi, 463 nmi)
 Ferry range: 985 km (612 mi, 532 nmi)
 Service ceiling: 4,572 m (15,000 ft)
 Rate of climb: 8.9 m/s (1,750 ft/min)

KAMOV Ka-32

Karakteristik umum

 Kru: satu-tiga
 Kapasitas: 4.000 kg (8.818 lb) muatan (Ka-32), atau hingga 16 pasukan (Ka-29).
 Panjang: 11,3 m (37 kaki 1 in)
 Tinggi: 5,5 m (18 kaki 1 inci)
 Berat kosong: 6.500 kg (14.330 lb)
 Berat kotor: 11.000 kg (24.251 lb)
 Berat lepas landas maks: 12.000 kg (26.455 lb)
 Pembangkit listrik: mesin turboshaft 2 × Isotov TV3-117V , masing-masing 1.660 kW

(2.230 hp)
 Diameter rotor utama: 2 × 15,8 m (51 kaki 10 in)
 Area rotor utama: 392,2 m 2 (4,222 kaki persegi) rotor berputar-berlawanan dengan 3

bilah

Performa

 Kecepatan maksimum: 270 km / jam (170 mph, 150 kn)
 Kecepatan jelajah: 205 km / jam (127 mph, 111 kn)
 Jarak tempuh : 980 km (610 mi, 530 nmi)
 Layanan langit-langit: 5.000 m (16.000 kaki)

MBB/KAWASAKI BK 117

General characteristics

 Crew: 1
 Capacity: up to 10 passengers
 Length: 9.91 m (32 ft 6 in) (fuselage length)
 Height: 3.85 m (12 ft 8 in) (rotors turning)
 Empty weight: 1,727 kg (3,807 lb)
 Max takeoff weight: 3,350 kg (7,385 lb)
 Fuel capacity: 697 L (183 US Gallons, 153 Imp Gallons) internal fuel
 Powerplant: 2 × Textron Lycoming LTS 101-750B-1 turboshaft, 442 kW (593 hp) each
 Main rotor diameter: 11.00 m (36 ft 1 in)
 Main rotor area: 95.03 m2 (1,022.9 sq ft)

Performance

 Maximum speed: 250 km/h (160 mph, 130 kn) at sea level
 Never exceed speed: 278 km/h (173 mph, 150 kn)
 Range: 541 km (336 mi, 292 nmi)
 Service ceiling: 4,575 m (15,010 ft) (max certified altitude)
 Hover Ceiling: 3,565 m (11,700 ft) (in ground effect)
 Rate of climb: 11.00 m/s (2,165 ft/min)

MIL MI-17

General characteristics

 Crew: 3 (two pilots and one engineer)
 Capacity: 24 troops / 12 stretchers / 4,000 kg (8,818 lb) cargo internally / 5,000 kg

(11,023 lb) externally slung.
 Length: 18.465 m (60 ft 7 in)
 Height: 5.65 m (18 ft 6 in)
 Empty weight: 7,489 kg (16,510 lb)
 Gross weight: 11,100 kg (24,471 lb)
 Max takeoff weight: 13,000 kg (28,660 lb) normal

13,500 kg (29,762 lb) with under-slung load

 Powerplant: 2 × Klimov VK-2500PS-03 turboshaft engines, 1,800 kW (2,400 hp) each
for take-off

2,000 kW (2,700 hp) emergency rating
 Main rotor diameter: 21.25 m (69 ft 9 in)
 Main rotor area: 354.7 m2 (3,818 sq ft)
 Blade section:NACA 23012[198]

Performance

 Maximum speed: 280 km/h (170 mph, 150 kn)
 Cruise speed: 260 km/h (160 mph, 140 kn)
 Range: 800 km (500 mi, 430 nmi)
 Service ceiling: 6,000 m (20,000 ft)
 Hover ceiling OGE: 4,000 m (13,123 ft)
 Rate of climb: 8 m/s (1,600 ft/min)

ROBINSON R44

General characteristics

 Crew: 1/2
 Capacity: 3/2 / 748 lb (339 kg)
 Length: 38 ft 3 in (11.66 m)
 Height: 10 ft 9 in (3.28 m)
 Empty weight: 1,450 lb (658 kg)
 Gross weight: 2,500 lb (1,134 kg)
 Fuel capacity: Fuel: 100 Octane low lead (100LL) fuel or 100/130 Octane.

 Main tank capacity: 31.6 US gal (26 imp gal; 120 l)
 Main tank usable fuel: 30.6 US gal (25 imp gal; 116 l)
 Auxiliary tank capacity: 18.5 US gal (15 imp gal; 70 l)
 Auxiliary tank usable fuel: 18.3 US gal (15 imp gal; 69 l)

 Powerplant: 1 × Lycoming IO-540-AE1A5 6-cylinder air-cooled horizontally-opposed
piston engine, 245 hp (183 kW)

 Main rotor diameter: 33 ft (10 m)
 Main rotor area: 855.4 sq ft (79.47 m2)

Performance

 Maximum speed: 130 kn (150 mph, 240 km/h)
 Cruise speed: 110 kn (130 mph, 200 km/h)
 Range: 300 nmi (350 mi, 560 km)
 Fuel consumption: 15 gallons per hour (12 imp gal/h; 57 l/h)[26][5]
 Altitude restrictions: 14,000 ft (4,300 m) density altitude or 9,000 ft (2,700 m) above

ground level in order to be able to reach ground within 5 minutes in case of fire.

ROBINSON R66

General characteristics

 Crew: 1
 Capacity: 4 passengers or 1,200 lb (540 kg) external load[25]
 Length: 29 ft 6 in (8.99 m)
 Width: 4 ft 10 in (1.47 m)
 Height: 11 ft 5 in (3.48 m)
 Empty weight: 1,290 lb (585 kg)
 Gross weight: 2,700 lb (1,225 kg)
 Fuel capacity: 73.6 US gallons (279 l)
 Powerplant: 1 × Rolls-Royce RR300 turboshaft, 224 shp (167 kW) continuous, 270 shp

(200 kW) takeoff (5 minutes)
 Main rotor diameter: 33 ft (10 m)
 Tail rotor Diameter: 5 ft (1.52 m)

Performance

 Cruise speed: 110 kn (130 mph, 200 km/h)
 Never exceed speed: 140 kn (160 mph, 260 km/h)
 Range: 350 nmi (400 mi, 650 km)
 Service ceiling: 14,000 ft (4,300 m)
 Rate of climb: 1,000 ft/min (5.1 m/s)
 Fuel Consumption: 23 US gallons (87 l) per hour[23]

AÉROSPATIALE SA 315B LAMA

General characteristics

 Crew: 1
 Capacity: 4 passengers or 1,135 kg (2,500 lb) slung payload
 Length: 10.24 m (33 ft 7.25 in)
 Height: 3.09 m (10 ft 1.75 in)
 Empty weight: 1,021 kg (2,251 lb)
 Gross weight: 2,300 kg (5,070 lb)
 Powerplant: 1 × Turbomeca Artouste IIIB turboshaft , 649 kW (870 hp) derated to 410

kW (550 hp)
 Main rotor diameter: 11.02 m (36 ft 1.75 in)
 Main rotor area: 95.38 m2 (1,026 sq ft)

Performance

 Maximum speed: 192 km/h (119 mph, 103 kn)
 Range: 515 km (320 mi, 280 nmi)
 Service ceiling: 5,400 m (17,715 ft)
 Rate of climb: 5.5 m/s (1,080 ft/min)

SIKORSKY S-76

Karakteristik umum

 Kru: dua [a]
 Kapasitas: 13 penumpang
 Panjang: 52 ft 6 in (16 m) dari ujung rotor utama ke ujung rotor ekor
 Lebar: 10 ft 0 in (3,05 m) pada stabilizer horizontal
 Tinggi: 14 ft 6 in (4,42 m) ke ujung rotor ekor
 Berat kosong: 7.005 lb (3.177 kg) dalam konfigurasi utilitas
 Berat kotor: 11.700 lb (5.306 kg)
 Kapasitas bahan bakar: 281 US galon (1.064 liter), dengan 50 atau 102 US galon (189

atau 386 liter) tersedia dalam tangki tambahan ekstra
 Pembangkit listrik: 2 × Turbomeca Arriel 2S2 turboshaft, masing-masing 922 shp (688

kW)
 Diameter rotor utama: 44 kaki 0 in (13,41 m)

Performa

 Kecepatan maksimum: 155 kn (178 mph, 287 km / jam) pada berat lepas landas
maksimum di permukaan laut dalam kondisi atmosfer standar

 Kecepatan jelajah: 155 kn (178 mph, 287 km / h) kecepatan jelajah maksimum sama
dengan kecepatan maksimum

 Rentang: 411 nmi (473 mi, 761 km) tanpa cadangan, pada kecepatan jelajah jarak jauh di
ketinggian 4.000 kaki

 Layanan langit-langit: 13.800 kaki (4.200 m)