TM 55-1500-342-23
NOTE
Before attempting to raise an
aircraft, relative heights of main
and nose or tail landing wheels in
both
three-point
and
level
attitudes should be considered in
order to determine the proper
blocking, lifting, and/or jacking
equipment required. Raising a tail
wheel to level an aircraft may be
quite a problem unless adequate
lifting, hoisting, and supporting
equipment is available. Jacks
should never be employed at any
place on the aircraft other than
specified jacking points.
CAUTION
Excessive side loads may cause
cell
breakage
and
incorrect
readings. If wing and fuselage
jacks are used to level the aircraft,
shock struts must be restrained to
prevent
them
from
extending
when aircraft is raised.
CAUTION
During
leveling
procedure,
extreme care should be exercised
to avoid side loads which may
cause the aircraft to slip off jacks.
For example, when wing jacks are
in place while tail is lifted to the
level position, it is likely that side
loads caused by rotation of the
fuselage will cause jacks to slip
off the jack points causing severe
damage to the wing. Correct
procedure requires that the tail be
lifted
while
the
aircraft
is
supported on main gear with
brakes unlocked. When raising
the aircraft with two wing or two
main landing gear jacks be sure
that the two jacks are actuated
simultaneously
in
order
to
maintain the aircraft in a lateral
level attitude.
e. Level aircraft in accordance with aircraft
maintenance manuals.
f. Measure and record dimensions once aircraft is
in a level position. Three horizontal dimensions must be
either measured or otherwise known to determine the
horizontal location of the center of gravity of the aircraft
as weighed. When landing gear are used as reaction
points, dimensions to be determined are as follows:
(1)
The
horizontal
distance
from
the
reference datum to some known jig point. It is not
necessary to measure this distance as it is given in
Chart E data and will remain fixed.
(2)
The distance from the jig point to a lateral
line passing through the main reaction points. This
measurement must be made along a line which is
parallel to the longitudinal axis of the aircraft.
(3)
The wheel base or distance between the
main and forward or aft reaction points.
g. Measure dimension in steps f(2) and (3) above
by projecting required points to hangar floor. Project jig
point to hangar floor by suspending a plumb bob from
center of jig point so that plumb bob is approximately
1/2 inch above floor. Wait until swing of plumb bob
stops, and make a cross mark on floor directly under tip
of plumb bob. Print words JIG POINT near cross on
floor to distinguish it from other projected points. Main
reaction points are projected in the same manner as
described above for the jig point. After marking crosses
for the two main reaction points, stretch a chalked string
between them and draw taut. Snap string against floor,
leaving a clear straight chalk line between main reaction
points. Nose or tail reaction point is projected in a
similar manner to plumb bob method.
h. Move plumb bob line a short distance fore or aft
(in a direction parallel to longitudinal axis of aircraft)
when jacks or other obstructions interfere with free fall
of plumb bob. Plumb bob will then swing free of
obstructions. Drop plumb bob and mark floor contact
point. Measure distance necessary to move plumb line;
be sure to correct for this transferred distance when
recording measurements on DD Form 365-2.
i.
Measure required dimensions after these points
are projected to floor. Dimensions to be measured are
listed as B and D on DD Form 365-2. Distance B is the
same dimension as discussed in step f(2) above. It is
the perpendicular distance from the projected jig point to
the chalk line between the main reaction points.
Distance D is the same dimension as referred to in step
f(3) above. It is the wheel base, or distance from the
centerline of the main reaction points to the nose or tail
Change 1 3-4
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