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Tank
a r e near each wing root forward of the
wheel wells.
s m a l l plastic cup
is
supplied in the loose
obtaining fuel samples. T o
a
fuel sample, i n s e r t the cup actuator prong i n t h e sump
r e c e p t a c l e and push
t o opera the valve mo-
mentarily and d r a i n fuel
the cup.
water is in the
fuel, a distinct line separating the water f r o m between
the gasoline will be
through the transparent cup
wall. Water, being
will settle t o the bottom
of the cup, while the colored fuel will r e m a i n on top.
Continue taking fuel samples until
water is purged
f r o m the tank.
The fuel tank gascolator control
is
on the cabin floor
forward of the pilot's seat, To flush the gascolator
sump and the
leading from the wing tanks t o
the s e l e c t o r
t u r n the selector handle t o the
and pull t h e fuel drain control
about five
seconds. Repeat t h e procedure for the
being s u r e
the fuel drain
ring is returned
to the closed position and that the drain
is
not
The
new
been
and
tested
a t
t h e factory. Operate
new
engine
at
power
limitations given
Section
Before
every
engine
level and replenish a s
Check engine
level after engine has been stopped
enough f o r oil t o d r a i n back
sump. The oil filler cap
a c c e s s door is located in the top cowling. Any lubricating
either straight mineral or
must conform
with
Specification No.
t o be acceptable for
u s e in
New or newly
should be operated on aviation grade straight mineral
during t h e f i r s t 25
of operation or until oil consump-
tion has stabilized. The a i r c r a f t
is
delivered from
with straight mineral
of the correct viscosity,
The engine
is
equipped with an external oil filter and the
engine
may
extended t o
filter element
is
A T
INTERVALS. If a n engine
been
on
mineral
Summary of Contents for M20J 1978
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Page 12: ...F I G m E 1 1 THREE m E W ISSUED f 1 15 77...
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Page 64: ...ALTITUDE CONVERSION TAS ASx 1 m...
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Page 66: ...E XIBMPEE Given 168 MPH Find 146 BCRS...
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Page 71: ...ISSUED 11 15 77...
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Page 75: ...ISSUED 11 15 77...
Page 78: ...TIME FUEL AND OlSTANCE TO CLIMB...
Page 80: ...CRUISE MNGE AT ECONOMY CRUlSE swLWEL IS C RpMp y PI NB I FUEL iW HO BPH OAB B W bU lsR...
Page 81: ...CRUISE L RANGE AT ECONOMY CRUlSE 2000 FT 1 9 1 ISSUED 11 15 77 5 21...
Page 82: ...CRUlSE L RANGE AT ECONOMY CRUISE 4000 FT 7 C 5 22 ISSUED 11 15 77...
Page 83: ...CRUISE 8 RANGE AT ECONOMY CRUISE 6000 F t 3 C ISSUED 18 15 77 5 23...
Page 84: ...CRUISE L RANGE AT ECONOMY CRUISE 8000 FT 1 C...
Page 85: ...CRUISE 8 RANGE AT ECONOMY CRUlSE...
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Page 87: ...CRUISE L RANGE AT ECONOMY CRUISE 14 060 FT9 13 C...
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Page 93: ...CRUlSE 4 RANGE AT BEST POWER 10 000 PT SO c MIXTURE SETTING I Use FULL RICH mixture above...
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Page 95: ...CRUISE L RANGE AT BEST POWER...
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Page 103: ...REVISION A 22 P J 6 5...
Page 106: ...AIRCRAFT CG LBCATION Lyg lMCMES AFT OF DATUM SM 0 0 ISSUED 11 15 77...
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Page 113: ...ISSUED 11 15 77 6 15...
Page 114: ...6 16 ISSUED 11 15 8...
Page 115: ...ISSUED 11 15 77 g d iJ i i 6 1 s...
Page 116: ...ISSUED 11 15 77...
Page 117: ...DAY ITEM D E S C R I P T I O N...
Page 118: ...REV D 3 7 8 4 ISSUED 11 15 77...
Page 128: ...d 0 4 ig m a Q Q k 8 h c car Sa O W w U k k 0 0...
Page 145: ...FIGURE 7 3 ELECTRICAL SYSTEM SCHEMATIC REVISION A...
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