Starter; Propeller; Fuel System; Fuel Tanks - Beechcraft Musketeer Sport III A23-19 Pilot Operating Handbook

SectionVII
Systems Description
STARTER
BEECHCRAFT Sport III
Musketeer A23-19. 19A
The starter is relay-controlled and is actuated by a rotary
type, momentary-on switch incorporated in the
MagnetcyStart switch. The magnetof.>tart switch, located
on the subpanel to the left of the pilot ' s eontroi column , in-
corporates R (right), L (left). and 80TH magneto positions
in addition to the normai OFF and START positions. After
activation of the starter, the spring loaded switch returns
to the 80TH position when released .
PROPELLER
Sensen ich M74DM-0-58 or 74DM6-0-58 fixed -pitch,
tvvo-blade propeller. Static rpm at maximum permissible
throttle settings: Not over 2400 rpm and not under 2300
rpm. No additional tolerance permitted. Diameter 74
inches, no cutoff permitted.
FUEL SYSTEM
The airplane is designed for operation on 80/ 87 (Red)
grade aviation gasoline. In the event this gradeis not avail -
able. 1
OOLL (Biue) or
100
(Green) grade aviation gasolines
may be used.
CAUTION
See Avco Lycoming Service Letter No. L 1 85A
or later revision for operation on alternate
fuels .
FUEL TANKS
Fuel tanks located in each wing leading edge have a nomi -
nal capacity of 29.9 gallons. In the filier neck of each tank
is a visual measuring tab which permits partial filling of
7-16 October 1979