landing run sentence in Hindi
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- Landing Grounds were often L-shaped, usually arrived at by removing a hedge boundary between two fields, and thereby allowing landing runs in two directions of.
- Flight trials proved that the aircraft had a very short landing run and the aircraft was displayed at the September 1955 Society of British Aircraft Constructors Show at Farnborough.
- The A320's spoilers did not deploy during the landing run, as the right thrust lever was above the " idle " setting required for automatic spoiler deployment.
- Towards the end of its landing run it veered off the runway embankment at the southern Moa Point Road end, none of the 37 passengers and four crew suffered injury.
- This gave the Ju 87 considerable advantage on take-off; even at a shallow angle, large lift forces were created through the aerofoil, reducing take-off and landing runs.
- The mist was threatening to deny a clear landing run for the Hudson, so it was recalled one hour early, just as the German ships were approaching " Habo s " zone.
- The smaller span raised the maximum speed from 110 km / h ( 68 mph ) to 130 km / h ( 81 mph ), but also increased stalling speed and landing run.
- The competition proper, starting the next day awarded points on performance in four different tests : high speed, low speed, distance required to take off and clear an obstacle and length of landing run.
- All test pilots reported that the plane was extremely stable in flight, to the point where it was difficult to change course; test pilots were also astounded by the very low landing speed and the consequently very short landing run.
- After casting-off from the tow plane, the rocket fighter's landing skid fails to function, the airframe decelerates over a patch of rough and rutted ground at the end of the landing run following an otherwise normal approach.
- As in any tail-less aircraft, take-off and landing runs were longer than for a conventional aircraft ( at similar wing loadings ) because at high angles of attack, downward elevon forces were much greater than those of elevators with their large moment.
- Production examples of the Pioneer CC . 1 were fitted with full-span controlled leading-edge wing slats and large-area Fowler-type trailing edge flaps, giving a take-off run of 225 feet and a landing run of only 200 feet.
- Most important of these was the addition of spoilerons ( spoilers or wing-mounted air brakes which act as ailerons by differential deployment in cruising flight ) and the ability to use idle reverse thrust in flight during the final approach so as to shorten the landing run.
- Behind the wing the upper and lower members converged to the rear; the drag on the lower members reduced the landing run to There were three vertical cross braces on each girder but the only lateral inter-girder cross-members were near the tail, though there was wire bracing.
- The aircraft is fitted with a retractable tricycle undercarriage with steerable nosewheels, The reverse pitch control that the aircraft is fitted with allows the constant-speed mechanism to be manually overridden to reverse the blade pitch angle, thus providing excellent ground handling characteristics, helping to slow down the plane to shorten the landing run.
- Erich Sommer himself once noted for late 20th-century television that the landing skid-equipped prototypes, when touching down on a wet-turf airstrip, had a landing run characteristic that " was like greased lightning " and " like [ landing on ] soap ", from the complete lack of braking capability of the landing skid system.
- A general rule agreed upon the Article 3 of the Tokyo Convention is that " the State of registration of the aircraft is competent to exercise jurisdiction over offences and acts committed on board which is in flight ( from the moment when power is applied for the purpose of take-off until the moment when the landing run ends ) ".
- However, as with the operational Messerschmitt Me 163B rocket fighter which used a landing skid, it was discovered that such a skid-format landing gear for the Ar 234A design's prototypes did not allow mobility after the end of the landing run, which would have left aircraft scattered widely over an airfield's acreage, unable to taxi off the runway without remounting each and every aircraft on a trolley for towing off the landing area.
- Using this powerplant, CANT engineers calculated a top speed for the Z . 1018 of 524 km / h ( 326 mph ) at 4, 500 m ( 14, 764 ft ), with a takeoff run of 354 m ( 1, 160 ft ), landing run of 462 m ( 1, 518 ft ), and a climb to 4, 000 m ( 13, 120 ft ) in 7 minutes 32 seconds ( 14 minutes 4 seconds to 6, 000 m / 19, 685 ft ).
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