Lifting Procedure
TTP B1-L1 ATA07 Beech 90 Series B2-L1 Lifting and Shoring JACKING The aircraft has pr o visions for a three-point jack- pad system. T w o pads are located on the center section rear spar inboard of each nacelle and one is near the aft edge of the nose w heel w ell, to the left of the fuselage center line. If all of the landing gear is to be raised off the g roun d , the fuel in the wings should be e v en l y distri b uted. It is pe r missi b le to jack the aircraft with a full fuel load. CAUTION When jacking ind i vidual w heels, use an automot i v e type jack with a lifting capacity of at least 1/2 of the g ross w eight of the aircraft. Jac k point s o n eac h mai n an d nos e landin g gear axl e ena b l e th e ind i vidua l raisin g o f eac h w hee l for changin g tire s o r w hee l bra k e repai r ...