Schweizer 269C-1 - Fuel Tank Configuration

Limitations
Pilot's Flight Manual
Fig ure 2-3. Air craft In stru ments (Sheet 2 of 4)
Reissued: 16 Jan 2019 2-9
CYL IN DER HEAD TEM PER A TURE:
GREEN ARC - 230° TO 450°F
YEL LOW ARC - 450° TO 500°F
RED LINE - 500°F
FUEL GAGES SHOWN REP RE SENT 32.5 OR 64.0 GALLON US ABLE FUEL CA PAC ITY IN STAL LA TIONS
STD. FUEL TANK CON FIG U RA TION
He li cop ters with carbureted en gine (HO-360-C1A)
AUX FUEL TANK CON FIG U RA TION
He li cop ters with carbureted en gine (HO-360-C1A)
CYL IN DER HEAD TEM PER A TURE:
GREEN ARC - 230°F TO 450°F
YEL LOW ARC - 450°F TO 500°F
RED RA DIAL - 500°F
STD. FUEL TANK CON FIG U RA TION
He li cop ters with fuel in jected en gine (HIO-360-G1A)
FUEL PRESS (PSI)
RED RA DIAL - 14 AND 35 PSIG
GREEN ARC - 14 TO 30 PSIG
SCHWEIZER
Model 269C-1 Helicopter
FAA Approved
CSP book 2..indd 55 8/4/19 12:53 PM