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The aircraft's pitch and yaw axes Y and Z are not shown, and its fixed reference frame xyz has been shifted backwards from its center of gravity (preserving angles) for clarity. Axes named according to the air norm DIN 9300
In February 1976, work commenced to automate the methods contained in the USAF Stability and Control DATCOM, specifically those contained in sections 4, 5, 6 and 7.The work was performed by the McDonnell Douglas Corporation under contract with the United States Air Force in conjunction with engineers at the Air Force Flight Dynamics Laboratory in Wright-Patterson Air Force Base.
It was initially developed by the AeroSpace and Defence Industries Association of Europe (ASD) for use with military aircraft. Since Issue 2 the scope has been extended to include land, sea and even non-equipment products. [1] It is widely used in civil as well as military products. S1000D is part of the S-Series of ILS specifications.
The -150 involves the conversion of Group 1 and Group 2 L-1011-1 aircraft to an MTOW of 470,000 pounds (210,000 kg), an increase of 40,000 pounds (18,000 kg), about 10%, from the L-1011-1, giving the aircraft a slightly better range than the -50, but without the additional center-section fuel tank, less than the L-1011-100 aircraft.
The largest aircraft by dimensions and volume (as of 2016) is the 302 ft (92 m) long British Airlander 10, a hybrid blimp, with helicopter and fixed-wing features, and reportedly capable of speeds up to 90 mph (140 km/h; 78 kn), and an airborne endurance of two weeks with a payload of up to 22,050 lb (10,000 kg).
Data from Embraer Phenom 2020 300E brochure, Aircraft Performance Database General characteristics Crew: 1 or 2 pilots Capacity: 6–8 passengers (standard configurations); 10 passengers maximum (with passenger in cockpit, optional side-facing divan, and optional belted lavatory) Length: 15.64 m (51 ft 4 in) Wingspan: 15.91 m (52 ft 2 in) Height: 5.1 m (16 ft 9 in) Max takeoff weight: 8,414.59 ...
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The RAAF now operates 16 aircraft from both No. 32 Squadron and No. 38 Squadron. The Japan Ground Self-Defense Force operates nine B300s, designated LR-2, in the reconnaissance and communications roles. The aircraft were delivered between 1998 and 2004 and include the last B300 built without the Pro Line 21 avionics package (c/no. FL-382). [54 ...