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The Verner VM 133 is a family of Czech two cylinder, horizontally opposed, four stroke aircraft engines, designed and built by Verner Motor of Šumperk. [ 1 ] [ 2 ] [ 3 ] Design and development
Formats for license plate numbers are consistent within the state. For example, Delaware is able to use six-digit all-numeric serials because of its low population. Several states, particularly those with higher populations, use seven-character formats of three letters and four digits, including 1ABC234 in California, 1234ABC in Kansas and ABC-1234 (with or without a space or dash) in Georgia ...
Deflected slipstream is an approach to creating an aircraft that can take off and land vertically (), or at least with a very short runway ().The basic principle is to deflect the slipstream from one or more propellers approximately 90 degrees, to create an upward thrust for vertical takeoff and a downward air cushion for landing.
D-CAAA to D-CZZZ for aircraft with 5.7–14 t MTOW; D-EAAA to D-EZZZ for single-engine aircraft up to 2 t MTOW; D-FAAA to D-FZZZ for single-engine aircraft with 2–5.7 t MTOW; D-GAAA to D-GZZZ for multi-engine aircraft up to 2 t MTOW; D-HAAA to D-HZZZ for rotorcraft; D-IAAA to D-IZZZ for multi-engine aircraft with 2–5.7 t MTOW
a paper, cardboard, or lightweight plastic license plate, to be removed at the end of the temporary registration period (typically a set number of days, e.g., 15, 30, or 45 days); a standard metal license plate with temporary validation, in which case the government agency needs to issue only a validation sticker rather than a license plate; or
With the JT8D reliably powering the three-engine Boeing 727, the 60-minute rule was waived in 1964 for three-engine aircraft, which in turn opened the way for the development of wide-body, intercontinental trijets such as the Lockheed L-1011 TriStar and McDonnell Douglas DC-10. By then, only twin-engine jets were restricted by the 60-minute rule.
Some light twin-engine airplane pilots place yaw strings on their aircraft to help maintain control in the event of an engine failure, because the slip-skid indicator ball is not accurate in this case. [16] In a multiengine airplane with an inoperative engine, the centered ball is no longer the indicator of zero sideslip due to asymmetrical ...
The idea is to fly aircraft in the upward part of the wingtip vortex of a leading aircraft. [16] In 2003, NASA said one of its F/A-18 test aircraft had a 29% fuel savings by flying in the wingtip vortex of a DC-8. The DC-8/F-18 flight was an exploratory investigation of large aircraft vortex-induced performance benefits on a fighter-type aircraft.