FIELD: aeronautical engineering. SUBSTANCE: engine front mount point and engine rear mount point are secured in succession on side pylon. Then cross-piece is mounted on front mount and load-bearing members of rear mount are coupled; to this end, cross-piece of front mount is secured on side pylon, after which engine is secured on lower mount and is turned in transverse vertical plane relative to its longitudinal axis; then upper mount is secured and pin of bracket of rear mount fitted on the engine is inserted in hole of movable rear mount of pylon, after which bracket is secured on the pylon. EFFECT: enhanced reliability. 6 dwg
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Authors
Dates
1995-02-20—Published
1992-08-24—Filed