Abstract: The present invention discloses an apparatus for emergency landing comprising: an extraction vehicle (10), a first adjustable tower and a second adjustable tower (11), a first gearbox (4) wherein said gearbox is mounted on top of said first adjustable tower, a second gearbox wherein said second gearbox is mounted on the top of said second adjustable tower, a third gearbox wherein said third gearbox is mounted on lower right side of said chassis, a fourth gearbox unit wherein said unit is mounted on the lower left side of chassis, a first rubber restrainer (8) wrapped around said first gearbox unit and extended to said third gearbox unit wherein said rubber restrainer is wrapped around said third gearbox unit, a second rubber restrainer wrapped around said second gearbox unit and extended to said fourth gearbox unit, wherein said rubber restrainer is wrapped around said fourth gearbox unit, wherein said first and said second rubber restrainer stabilize said aircraft and reduce initial impact by said aircraft.