Descriptive Data Engine; Propeller; Fuel - Beechcraft Musketeer Sport III A23-19 Pilot Operating Handbook

BEECHCRAFT Sport III
Musketeer A23-19. 19A
DESCRIPTIVE DATA
ENGINE
Section l
General
Airplane is equipped with an Avco Lycoming 0-320-E2B.
0-320-E2C or 0-320-E3D engine rated at 150
horsepower.
Take-off and maximum continuous operation (sea level):
2700 rpm, fuli throttle .
Engine cooling ha s been demonstrated for a 100°
F
day.
PROPELLER
Sensenich M74DM-0-58 or 74DM6-0-58 fixed-pitch,
twa-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
Aviation Gasoline 80/87 (red) minimum grade or 100LL
(blue) or 100 (green) .
*59.8-gallon system
(29.9 gallans each tank) . . . . . *58.8 gallans usable
Each tank has provisions for partial filling to :
20 gallans each tank
15 gallans each tank
October 1979
38.8 gallans usable
28.8 gallans usable
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