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The Airbus A400M Atlas [nb 1] is a European four-engine turboprop military transport aircraft.It was designed by Airbus Military, now Airbus Defence and Space, as a tactical airlifter with strategic capabilities to replace older transport aircraft such as the Transall C-160 and the Lockheed C-130 Hercules. [3]
The Series 400 introduced an even longer airframe that was stretched 6.83 metres (22.4 ft) over the Series 300 (10.26 metres (33.7 ft) over the Series 100/200), had slightly more wing span due to a larger wing section inboard of the engines, a stouter T-tail and had a passenger capacity of 68–90.
Data from Extra EA-400 Standard Specification, Pilots Information Manual General characteristics Crew: 1 Capacity: 5 passengers Length: 9.57 m (31 ft 5 in) Wingspan: 11.5 m (37 ft 9 in) Height: 3.09 m (10 ft 2 in) Empty weight: 1,500 kg (3,307 lb) Max takeoff weight: 1,999 kg (4,407 lb) Powerplant: 1 × Continental TSIOL-550-C Voyager 6-cyl. horizontally opposed liquid cooled turbocharged ...
400+ [1] The Europrop International TP400-D6 is an 11,000 shp (8,200 kW) powerplant, developed and produced by Europrop International for the Airbus A400M Atlas military transport aircraft . The TP400 is the most powerful turboprop in service using a single propeller; only the Soviet-designed Kuznetsov NK-12 and Progress D-27 , using contra ...
The Turbo-Hydramatic or Turbo Hydra-Matic (THM) series was developed to replace both the original Hydra-Matic models and the Buick Dynaflow. In its original incarnation as the Turbo-Hydramatic 400, it was first used in the 1964 model year in Cadillacs. The Buick version, which followed shortly thereafter, was known as the Super-Turbine 400.
Collection of control yokes at Boeing Future of Flight Museum: 747, 707, B-29, Trimotor.The former two yokes are W-shaped, while the latter two are circular. The cockpit of Concorde, which has an M-shaped yoke mounted on a control column The cockpit of an Embraer ERJ with an M-shaped yoke "W"/"U" style yoke in a Cessna 152 light aircraft, mounted on a horizontal tube protruding from the ...
The 400 cu in (6.6 L) version was the second, tall-deck "big-block" Olds. Two distinct versions of the 400 CID engine were made: 1965-1967 "Early" 400s used a slightly oversquare 4.000 in (101.60 mm) bore and 3.975 in (100.97 mm) stroke for an overall displacement of 399.6 cu in (6,549 cc). All the pre-1968 engines used a forged steel crankshaft.
Data from Columbia 400 Pilot's Operating Handbook General characteristics Crew: 1 pilot Capacity: 3 passengers Length: 25 ft 2 in (7.67 m) Wingspan: 36 ft 1 in (11.00 m) Height: 9 ft 0 in (2.74 m) Wing area: 141 sq ft (13.1 m 2) Empty weight: 2,500 lb (1,134 kg) Max takeoff weight: 3,600 lb (1,633 kg) Powerplant: 1 × Teledyne Continental TSIO-550-C air-cooled flat-6 engine, 310 hp (230 kW ...
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