Mooney M20J 1978, Руководство по эксплуатации для пилотов

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maximum g r o s s weight. The aircraft must be operated
strictly within the of the Center-of -Gravity
Moment Envelope shown on page
PROCEDURE
(A) Place a spirit %eve% on the skin line
above the a c c e s s door when leveling the
a i r c r a f t longitudinally. %eve% the a i r c r a f t by i n c r e a s -
ing or decreasing a i r p r e s s u r e in the nose wheel t i r e .
(B) WEIGHING: T o weigh the a i r c r a f t , select a level work
a r e a and:
Check f o r installation of a l l equipment a s listed in
t h e Weight Equipment
F i l l both fuel tanks t o full capacity. Subtract
able fuel gal
@
6
=
total
weight
as
weighed,
-
Ground and
follows:
a.
Kine
at
boost
fitting,
t o output fitting
a
receptacle,
f u e l selector salve t o tank
remove cap fuel
25 gal, fuel each
Replace caps,
3 . F i l l oil capacity
-
8
Position front s e a t s in full forward position,
in position,
Position a 2000-pound capacity under each
of the t h r e e
a s previously described making
certain nose wheel
is
centered,
t h e a i r c r a f t and deduct any t a r e each
.
Find reference point by dropping
a
plumb f r o m
center of nose g e a r trunnion (retracting pivot
point of intersection,
Locate center line main axles in s a m e
.
REVISION A