S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
AFM H8001 SINGLE & DUAL COCKPIT Revision B
Page 13
FAA APPROVAL DATE: 3/19/2015
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:
“USEABLE FUEL 114 U.S. GAL.PER TANK.
FUEL ABOVE 82 GAL. IS UNGAGEABLE
”
d.
Locate on lower right on rear instrument panel:
“SOLO
FRONT SEAT ONLY”
e.
Locate on rear instrument panel:
“OCCUPANT MUST ATTACH SEAT BELT AND
SHOULDER HARNESS, AND WEAR A D.O.T.
APPROVED OR MIL-
SPEC HELMET”
f.
Locate at the forward side of lower rear door window.
“PUSH OUT AND LIFT HINGE PIN FOR EMERGENCY EXIT.”
g.
Locate at the forward side of lower rear door window.
“DO NOT OPEN IN FLIGHT”
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:
Open
j.
Located (inverted) at each door hinge pin:
“PULL HINGE PIN
⇩
FOR EMERGENCY EXIT.”
k.
Locate on rear instrument panel.
“HOPPER RINSE TANK MUST BE FULL WHEN REAR COCKPIT IS
OCCUPIED
BY A CREWMEMBER.”
l.
Locate on rear instrument panel
“FORWARD BALLAST BOX MUST BE INSTALLED ANYTIME THE
REAR SEAT IS OCCUPIED.”
