THRUSH S2R-H80 Flight Manual page 27

b.
Locate in the center of rear instrument panel:
"STABILIZED GROUND OPERATION IS PROHIBITED BETWEEN 400
AND 1100 RPM. THE PROPELLER MAY BE OPERATED WHEN
FEATHERED AT OR BELOW 400 RPM."
c.
Locate below MVP-50T screen on rear instrument panel:
d.
e.
f.
Locate at the forward side of lower rear door window.
g.
Locate at the forward side of lower rear door window.
h.
Locate at the aft side of lower rear door window.
"DO NOT OPEN DOOR ON THE GROUND WITH THE ENGINE
RUNNING UNLESS HEADED OUT OF THE WIND WITH PROPELLER
FEATHERED."
i.
Locate at each door handle:
j.
Located (inverted) at each door hinge pin:
k.
OCCUPIED BY A CREWMEMBER."
l.
Locate on rear instrument panel
"FORWARD BALLAST BOX MUST BE INSTALLED ANYTIME THE
REAR SEAT IS OCCUPIED."
AFM H8001 SINGLE & DUAL COCKPIT Revision B
FAA APPROVAL DATE: 3/19/2015
"USEABLE FUEL 114 U.S. GAL.PER TANK.
FUEL ABOVE 82 GAL. IS UNGAGEABLE"
Locate on lower right on rear instrument panel:
"SOLO
FRONT SEAT ONLY"
Locate on rear instrument panel:
"OCCUPANT MUST ATTACH SEAT BELT AND
SHOULDER HARNESS, AND WEAR A D.O.T.
APPROVED OR MIL-SPEC HELMET"
"PUSH OUT AND LIFT HINGE PIN FOR EMERGENCY EXIT."
"DO NOT OPEN IN FLIGHT"
Open
"PULL HINGE PIN ⇩ FOR EMERGENCY EXIT."
Locate on rear instrument panel.
"HOPPER RINSE TANK MUST BE FULL WHEN REAR COCKPIT IS
S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
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