ETA Logistics

Aircraft Specifications

MD-11

MD-11 General Specifications

Manufacturer
Boeing Corporation

First flight
January 10, 1990

Wingspan
169ft 6in/51.66m

Length
200ft 10 in/61.21m

Height
57ft 9in/17.6m

Ceiling
41,000ft

Range
6,500nm/12,038 km

Weight
Passenger: 295,600 lbs/134,082 kg

Power Plant
Three Pratt & Whitney PW4460/62
-or- General Electric CF6-80C2

Speed
550 knots/1,017 km/h/ 0.83mach

Crew
2

Accommodation
285-323-410 in three, two or one class configuration

MD-11F (Freighter)

Maximum Takeoff Weight
272,070 kg (502,000 lb)

Maximum Landing Weight
213,870 kg (471,500 lb)

Structural Payload
93,170 kg (205,400 lb)

Usable Volume
433m 3 (15,653ft)

Maximum Stack Height
98.25in (249.5 cm)

Forward Cargo Door
140in wide by 103.5in high (356 cm x 263 cm)

Lower Deck Capacity
5,566ft 3 (158m 3 ) of containerized or bulk cargo

ULD Accomodation
All standard industry containers.

Airbus A300-600F

Airbus A300-600F General Specifications

Manufacturer
Airbus Industries

First flight
2001

Wingspan
147ft 1in/44.84m

Length
177ft 5in/54.10m

Height
54ft 3in/16.54m

Ceiling
41,000ft

Range
1,950-2,650nm/3,650-4,850 km

Weight
300,900 lbs /136,363 kg

Power Plant
Two 262.4kN (59,000 lbs) General Electric CF6-80C2A1s

Speed
549knots /1,017 km/h/0.82mach

Crew
2

Payload
120,200 lbs/54,636 kg

Airbus A300-600 Freighter + Payload Mode

Maximum Takeoff Weight
168,000 kg (370,400 lb)

Maximum Landing Weight
143,300 kg (315,500 lb)

Bulk Hold Volume
11.27m3 (398ft3)

A300 and A310 Freighter Conversions

Typical conversion includes: installation of a 141in x 101in (3.58m x 2.57 m) main deck cargo door, floor reinforcement, a main deck cargo loading system, safety barrier net, smoke curtain, and additional fire-suppression equipment.

Cargo Loads for Converted Aircraft

Typical cargo loads for converted aircraft are:

A300 — 48 tonnes on up to 25 88in x 125in pallets, 21 carried on the main deck and four in the forward underfloor hold, or alternatively, up to 21 pallets on the main deck plus up to 23 LD3 containers in the underfloor holds.

A310 — 40 tonnes on up to 19 pallets, 16 on the main deck and three in the forward underfloor hold, or alternatively, up to 16 pallets on the main deck plus up to 15 LD3 containers in the underfloor holds.

Boeing 727-100

Manufacturer

Boeing Corporation

First flight

February 9, 1963

Wingspan

108ft/ 32.91m

Length

133ft 2in/40.59m

Height

34ft/10.36m

Ceiling

40,000ft

Range

3,000nm /5,556 km

Weight

80,600 lbs /36,560 kg

Power Plant

Three Pratt & Whitney JT8D7

Speed

529 knots /980 km/h /mach 0.80

Crew

3

Accommodation

94-131 in two or one class configuration

Boeing 727-100 Freighter

Maximum Takeoff Weight

72,580 kg (160,000 lb)

Maximum Landing Weight

62,510 kg (137,800 lb)

Structural Payload

15,650 kg (34,500 lb)

Usable Volume

99m3 (3,496ft3)

Boeing 727-200 Freighter

Maximum Takeoff Weight

78,020 kg (172,000 lb)

Maximum Landing Weight

66,0400 kg (150,000 lb)

Structural Payload

na

Usable Volume

137m3 (4,838ft3)

Boeing 747 Freighter

Boeing 747 General Specifications

Manufacturer

Boeing Corporation

Cargo Volume, Main Deck

21,347ft3 (605m3)

30 pallets, 96x125in (244 x 318 cm)

Cargo Volume, Lower Deck

5,600ft3 (159m3)

32 LD-1 containers

Cargo Volume, Bulk Cargo

520ft3 (15m3)

Maximum Payload

248,300 lbs (112,630 kg)
Optional 273,300 lbs (123,970 kg) available with maximum take-off-weight limitation

Engines Maximum Thrust

Pratt & Whitney PW4062 -63,300 lb (281.57 kN)

Rolls-Royce RB211-524H2-T – 59,500 lb (264.67 kN)

General Electric CF6-80C2B5F – 62,100 lb (276.23 kN)

Maximum Fuel Capacity

53,765 U.S. gal (203,515 L)

Maximum Takeoff Weight

875,000 lb (396,900 kg)

Maximum Range

4,445 nautical miles (8,232 km)
Typical city range:

Paris-New York

New York-Frankfurt

London-Beijing

Toyky-Sydney

Typical Cruise Speed at 35,000 feet

0.845mach, 560mph (901 km/h)

Wing Span

211ft 5in (64.4 m)

Overall Length

231ft 10in (70.7 m)

Tail Height

63ft 8in (19.4 m)

Interior Cabin Width

20 ft (6.1 m)

Boeing 757-200

Boeing 757 General Specifications

Manufacturer

Boeing Corporation

First flight

February 19, 1982

Wingspan

124ft 10in/38.05m

Length

155ft 3in/47.32m

Height

44 ft. 6in/13.56m

Ceiling

41,000ft

Range

3,928nm /7,275 km

Weight

128,730 lbs /58,391 kg

Power plant

Two RollsRoyce RB211535C / RB211535E4 -or-

Pratt & Whitney PW2037 / PW2040

Speed

530knots /982 km/h/0.80mach

Crew

2

Accommodation

192-239 in two or one class configuration

Boeing 757-200 Freighter

Maximum Takeoff Weight

115,670 kg (255,000 lb)

Maximum Landing Weight

95,260 kg (210,000 lb)

Structural Payload

31,750 kg (70,000 lb)

Usable Volume

187m3 (6,603ft3)

Boeing 767-300

Boeing 767 General Specifications

Manufacturer

Boeing Corporation

First flight:

January 30, 1986

Wingspan:

156 ft 1in/47.6m

Length:

180 ft 3in/54.9m

Height:

52 ft/15.8m

Ceiling:

41,000ft

Range:

6,115nm /11,325 km

Weight:

196,000 lbs /88,904 kg

(199,600 lbs /90,537 kg -extended range)

Power plant:

Two Pratt & Whitney PW4062 -or- General Electric CF6-80C2B7F -or- Rolls Royce RB211-514H

Speed:

530knots/982 km/h /0.80mach

Crew:

2

Accommodation:

218-269-351 in three, two or one class passenger
configuration / 60.5 tons as freighter

Boeing 767-300 Freighter

Maximum Takeoff Weight

188,880 kg (412,000 lb)

Maximum Landing Weight

147,870 kg (326,000 lb)

Structural Payload

54,840 kg (120,900 lb)

Usable Volume

336m3 (11,865ft3)

This information has been provided from AtoZWorldTrade.

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