8/7/2019 Benadict

http://slidepdf.com/reader/full/benadict 1/5

Embraer ERJ-170

Power plant

ERJ-170 - Two 62.3kN (14,000lb) General Electric CF34-8E turbofans.

Performance

ERJ-170 - Max cruising speed Mach 0.82 or 890km/h (481kt). Standard range with max

 passengers at long range cruising speed 3334km (1800nm), LR range at same conditions 3889km

(2100nm).

Weights

ERJ-170 - Basic operating 20,150kg (44,422lb), standard max takeoff 35,450kg (78,153lb), LR 

max takeoff 48,500kg (106,922lb).

Dimensions

ERJ-170 - Wing span over winglets 26,00m (85ft 4in), length 29,90m (98ft 1in), height 9.67m(31ft 9in).

Capacity

Flightcrew of two.

ERJ-170 - Standard seating for 70 at four abreast.

Type

70 seat regional airliner 

8/7/2019 Benadict

http://slidepdf.com/reader/full/benadict 2/5

Douglas DC-7

Power plant

DC-7F & DC-7C - Four 2535kW (3400hp) Wright R3350EA1 or EA4 Turbo Compound radial

 piston engines driving four blade constant speed propellers.

Performance

DC-7F - Typical cruising speed 555km/h (300kt). Range with max fuel and no reserves 7130km

(3850nm). DC-7C - Typical cruising speed 555km/h (330kt). Range with max payload 5810km(3135nm), range with max fuel and no reserves 9077km (4900nm).

Weights

DC-7F - Basic operating 30,030kg (66,200lb), max takeoff 57,153kg (126,000lb). DC-7C - Basic

operating 36,287kg (80,000lb), max takeoff 64,865kg (143,000lb).

Dimensions

DC-7F - Wing span 35.81m (117ft 6in), length 33.24m (108ft 11in), height 8.90m (29ft 3in).

Wing area 136.0m2 (1463sq ft). DC-7C - Wing span 38.80m (127ft 6in), length 34.23m (112ft

3in), height 9.65m (31ft 8in). Wing area 152.0m2 (1637sq ft).

Capacity

Flightcrew of three. In passenger configurations most standard length DC-7s seated 99 in a highdensity single class layout, stretched DC-7Cs seated up to 105 passengers. Capacity of DC-7F

conversion of the DC-7B is 15,700kg (34,600lb).

Type

Piston engine airliner and freighter 

8/7/2019 Benadict

http://slidepdf.com/reader/full/benadict 3/5

Antonov An-140

Power plant

An-140 - Two 1839kW (2466shp) Motor-Sich AI-30 Series 1 turboprops (licence built KlimovTV3-117s) driving six blade propellers, or two 1864kW (2500shp) Pratt & Whitney Canada

PW127A Turboprops.

Performance

An-140 with AI-30s - Max cruising speed 575km/h (310kt), economical cruising speed 520km/h

(280kt). Range with 52 passengers 2100km (1133nm), range with a 6000kg (13,227lb) payload

at 520km/h (280kt) 900km (486nm).An-140 with PW127s - Range with 52 passengers 2500km (1349nm).

Weights

An-140 - Max takeoff 19,150kg (42,218lb).

An-140-100 - Empty 12,810kg (28,240lb), max takeoff 21,500kg (47,400lb).

DimensionsAn-140 - Wing span 24.51m (80ft 5in), length 22.61m (74ft 2in), height 8.23m (26ft 11in).

An-140-100 - Wing span 25.51m (83ft 8in).

Capacity

An-140 - Flightcrew of two. Typical passenger seating for 52 at four abreast and 75cm (30in)

 pitch or 48 at 81cm (32in) pitch. Forward starboard freight door allows 1900 to 3650kg (4188 to8046lb) of palletised freight and 36 or 20 passengers to be carried in a combi configuration.

8/7/2019 Benadict

http://slidepdf.com/reader/full/benadict 4/5

Ilyushin Il-86

Power plant

Four 127.5kN (28,660lb) KKBM (Kuznetsov) NK86 turbofans.

Performance

Max cruising speed 950km/h (513kt), typical cruising speed between 900km/h (485kt) and

950km/h (513kt). Design range with 40 tonne (88,185lb) payload 3600km (1945nm), with maxfuel 4600km (2480nm).

Weights

Max takeoff 208,000kg (458,560lb).

Dimensions

Wing span 48.06m (157ft 8in), length 59.94m (195ft 4in), height 15.81m (51ft 10in). Wing area

320m2 (3444sq ft).

Capacity

Flightcrew of three comprising two pilots and flight engineer, with provision for a navigator.Max seating for 350 at nine abreast. Mixed two class seating for 234 comprising 28 six abreast in

forward cabin and 206 eight abreast in other two cabins. Lower deck freight holds can

accommodate up to 16 standard LD3 containers if some lower deck carry on baggage racks are

omitted.

Type

Medium range widebody airliner 

8/7/2019 Benadict

http://slidepdf.com/reader/full/benadict 5/5

The Gulfstream Aerospace G-IV Gulfstream IV

Power Plant

Two 61.6kN (13,850lb) Rolls-Royce Tay Mk.6118 turbofans.

Performance

G-IV - Normal cruising speed 850km/h (460kt). Initial rate of climb 4000ft/min. Range with max

 payload and reserves 6732km (3633nm), range with eight passengers and reserves 7815km(4220nm).

G-IV-SP - Max cruising speed 936km/h (505kt), normal cruising speed 850km/h (460kt). Initialrate of climb 4122ft/min. Range with max payload and reserves 6182km (3338nm), range witheight passengers and reserves 7815km (4220nm).

Weights

G-IV - Empty 16,102kg (35,500lb), max takeoff 33,203kg (73,200lb).

G-IV-SP - Empty same, max takeoff 33,838kg (74,600lb).

Dimensions

Wing span 23.72m (77ft 10in), length 26.92m (88ft 4in), height 7.45m (24ft 5in). Wing area

88.3m2 (950.39sq ft).

Capacity

Flightcrew of two. Main cabin seating for between 14 and 19, plus flight attendant.

SRA-4 special missions version can also be configured for freight work.