| 摘要 |
1. A transport plane with 2 (or 4) primary jet engines-under-the-wing is supplemented by a smaller proficient "Auxiliary" jet engine installed on eac h side of the rear fuselage that has the mechanical and technological capability to rotate 180 degrees for Horizontal Short Take Off and Landing (H/STOL) capability. The exhaust thrust of the "Auxiliary" jet engines rotated to the front on landing serves as a direct and efficient braking mechanism for the jet plane to stop on a short runway and also to effectively "backup" the plane to its setting and there, expeditiously load or unload its cargo of either peace keeping military troo ps and equipment or humanitarian aid. The two "Auxiliary" jet engines are independent and have separate controls f or rotatability, have their own fuel supply and electrical system with the pilo t able to shift essential flight controls and thrust of the plane to the "Auxiliary" j et engines on "standard mode" either during high altitude flying to conserve fuel or in the event of an emergency, have sufficient power for the pilot to land the plane and its cargo safely. The invention is applicable to private and commercial jet planes.</SDOAB >
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