Page 200 2
nd
Edition – Rev 0
07-00
JACKING – MAINTENANCE PRACTICES
07-00 JACKING – MAINTENANCE PRACTICES
General
For the aircraft jacking , two lifting points are provided under the two outer keelsons, on both
sides od fuselage. The lifting point consists of a small aluminium cylinder fastened to the
outer keelsons. Below of it could be placed either a hydraulic jack or a lifting rod. The lifting
point is realized with a
11mm hole which could be used to fit a lifting rod safety pivot.
Figure 1: Lifting point
Jacking the aircraft
Tools
Commercial (check for suitable max load)
Commercial (fitted with suitable padded support to hold the front
of fuselage)
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