SECTION 8 CESSNA
,-~
HANDLING, SERVICE, AND MAINTENANCEMODEL 2088
(675
SHP)
GROUND HANDLING
(Continued)
JACKING
(Continued)
f-
,-
Anytime the cargo pod is installed, if the main gear-to-fuselage fairings
are removed, jacks can be positioned adjacent to the sides of the cargo
,.
pod and raised to engage the receptacle on the end of the jacks over
the head of the outboard bolt which secures the main gear attach
,
~
trunnion bearing cap (aft) on the left and right gear. These jacking
locations serve essentially the same purpose as the fuselage jack
,
-
points at the main gear supports. An additional jack point on each main
gear axle fitting is used primarily when the cargo pod is installed and it
is desired to jack a single main gear for tire replacement, etc. If desired,
jack stands with wing jack pads may be fabricated so that the front wing
spar at stations 141.2 or 155.9 on each wing may be used as jacking
locations. A tail jack must be used in conjunction with wing jacking.
CAUTION
.
A TAlL JACK STAND MUST BE USED WHEN
CONDUCTING MAINTENANCE
INSIDE THE TAlL
SECTION, AND SHOULD BE INSTALLED IN MOST
JACKING OPERATIONS. BE SURE THE STAND IS
SUITABLY HEAVY TO KEEP THE TAIL STABLE
UNDER ALL CONDITIONS AND IS STRONG
ENOUGH TO SUPPORT THE AIRPLANE. PLACING A
JACK
STAND
UNDER
THE
NOSE
JACK
POINT
(IF
NOT USED FOR
JACKING) WILL PROVIDE
ADDITIONAL STABILITY.
DO NOT USE CARGO POD STRUCTURE FOR
JACKING OR AS A BLOCKING SURFACE.
RAISE THE AIRPLANE NO MORE THAN REQUIRED
FOR THE MAINTENANCE BEING PERFORMED.
In some instances, it may be necessary to use a sling or hoisting rings
for the initial lift, to be followed with jacking at the jack points. Refer to
the Maintenance Manual for procedures on jacking and hoisting, and
information concerning jacking equipment.
(Continued Next Page)
1
8-14 U.S.
Revision 23
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