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Wep 5.
m o r e proceed
as
i n Step 2 t o
for
t h e baggage t o be
and e n t e r the f i g u r e s
in
t h e p r o p e r columns.
Step
T o t a l the weight columns. T h i s total must be
pounds o r l e s s . Total the
column.
not forget t o s u b t r a c t negative
n u m b e r s ,
Refer t o the Center- of- Gravity Moment Enve-
lope (page 6-8). Locate t h e
weight of
your a i r p l a n e on t h e
s c a l e of the graph and
t r a c e a line horizontally t o t h e right. Locate
t h e total
value for
a i r p l a n e
on t h e bottom s c a l e of t h e g r a p h and t r a c e a
line vertically above t h i s point until t h e horizon-
line for weight
i n t e r s e c t e d . If
point
of intersection
is
within t h e
a r e a , your
a i r c r a f t loading
i s
acceptable.
t h e point of
i n t e r s e c t i o n
outside t h e shaded a r e a , you
must r e a r r a n g e
load before takeoff.
The
Equipment
is
a
listing of all
approved
the
of
for the
having a n
X
i n
"Mark
column and dated w e r e installed a t
additional equipment is
t o
be installed
it
must be done
i n a c c o r d a n c e
the r e f e r e n c e drawing o r a s e p a r a t e
F A A
Positive a r m s a r e d i s t a n c e s aft of
a i r p l a n e
datum. Negative a r m s a r e d i s t a n c e s forward
of t h e a i r p l a n e datum.
a f t e r t h e i t e m weight and a r m indi-
c a t e
a s s e m b l y installations. Some
m a j o r components of t h e a s s e m b l y a r e listed and
indented
the
following. The summation
of t h e major components will not n e c e s s a r i l y
equal t h e complete a s s e m b l y installation.
'SUED
11- 15- 77
Содержание M20J 1978
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Страница 12: ...F I G m E 1 1 THREE m E W ISSUED f 1 15 77...
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Страница 64: ...ALTITUDE CONVERSION TAS ASx 1 m...
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Страница 66: ...E XIBMPEE Given 168 MPH Find 146 BCRS...
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Страница 71: ...ISSUED 11 15 77...
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Страница 78: ...TIME FUEL AND OlSTANCE TO CLIMB...
Страница 80: ...CRUISE MNGE AT ECONOMY CRUlSE swLWEL IS C RpMp y PI NB I FUEL iW HO BPH OAB B W bU lsR...
Страница 81: ...CRUISE L RANGE AT ECONOMY CRUlSE 2000 FT 1 9 1 ISSUED 11 15 77 5 21...
Страница 82: ...CRUlSE L RANGE AT ECONOMY CRUISE 4000 FT 7 C 5 22 ISSUED 11 15 77...
Страница 83: ...CRUISE 8 RANGE AT ECONOMY CRUISE 6000 F t 3 C ISSUED 18 15 77 5 23...
Страница 84: ...CRUISE L RANGE AT ECONOMY CRUISE 8000 FT 1 C...
Страница 85: ...CRUISE 8 RANGE AT ECONOMY CRUlSE...
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Страница 87: ...CRUISE L RANGE AT ECONOMY CRUISE 14 060 FT9 13 C...
Страница 89: ...CRUISE L RANGE AT BEST POWER MIXTURE SETTING 2000 FT ill C 1 Use FUEL RICH mixture above ISSUED 11 15 77 5 29...
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Страница 92: ...CRUlSE RANGE AT BEST POWER MIXTURE SETTING 8000 FT 1 C 1 Use F U L L RICH mixture above 5 33 ISSUED 11 15 77...
Страница 93: ...CRUlSE 4 RANGE AT BEST POWER 10 000 PT SO c MIXTURE SETTING I Use FULL RICH mixture above...
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Страница 95: ...CRUISE L RANGE AT BEST POWER...
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Страница 103: ...REVISION A 22 P J 6 5...
Страница 106: ...AIRCRAFT CG LBCATION Lyg lMCMES AFT OF DATUM SM 0 0 ISSUED 11 15 77...
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Страница 113: ...ISSUED 11 15 77 6 15...
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Страница 115: ...ISSUED 11 15 77 g d iJ i i 6 1 s...
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Страница 117: ...DAY ITEM D E S C R I P T I O N...
Страница 118: ...REV D 3 7 8 4 ISSUED 11 15 77...
Страница 128: ...d 0 4 ig m a Q Q k 8 h c car Sa O W w U k k 0 0...
Страница 145: ...FIGURE 7 3 ELECTRICAL SYSTEM SCHEMATIC REVISION A...
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