Limitations
SCHWEIZER
Model 269C Helicopter Pilot's Flight Manual
Reissued: 16 Jan 2019
2-9
Powerplant
Type Lycoming Hor i zon tally Op posed
Des ig na tion HIO-360-D1A
Cyl in ders 4
Horse power 190 hp at 3200 rpm
2-10. FUEL SYS TEM
Fuel Ca pac ity, see Ta ble 2-2.
Ta ble 2-2. Fuel Ca pac ity
Tank Quan tity Us able Quan tity
Main 30 U.S. gal lons 29.8 U.S. gal lons
Aux 19 U.S. gal lons 18.8 U.S. gal lons
To tal 49 U.S. gal lons 48.6 U.S. Gal lons
OR
Main 33 U.S. gal lons 32.5 U.S. Gal lons
See sup ple ments CSP-C-1R or CSP-C-1U for aux il iary quan ti ties
2-11. AUX IL IARY FUEL TANK CAL I BRA TION
Aux il iary Fuel Quan tity, see Ta ble 2-3.
Ta ble 2-3. Aux il iary Fuel Quan tity
10
0 15
Total
5 20 25 30Gage
0 10 18 27 34 42 49
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
FAA Approved
CSP Book 1 CSP-C-1.indd 61 8/4/19 12:45 PM
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