Mooney Aircraft MARK 21 - Part I: Description and Operation of Components

NOTE: Information in the 1965 MARK 21 owner's manual
also applies to the 1962 through 1964 models with the ex-
1852, 1940 thru 2207, 2209 thru
2255, 2257 thru 2296
2208,2256, 2297
thru 2622
ment to the 1965 MARK 21
owrrers manual
PAR"1" DESCRIPTION AND OPERATION
OF COMPONENTS
FUEL SYSTEM (Reference page 3)
The fuel tank capacity of the 1962 and 1963 Mark 21 is 24
gallons per wing tank or 48 gallons total fuel. The '62 and
'63 models do not have a pull ring to drain the fuel selector
sump
from the cabin. In these models the selector sump is
drained from outside using the same procedure recommended
for draining the wing tanks. 1962 and 1963 models have a
gascolator in the nose wheel well which can be inspected and
drained from outside the aircraft.
LANDING GEAR: (Reference page 6)
The thumb operated safety latch for the landing gear retrac-
tion lever has not been factory installed on serial numbers
1852, 1940 through 2050.