Schweizer S300C 269C - Section VIII - ADDITIONAL OPERATIONS AND PERFORMANCE DATA

Operations & Performance
Pilot's Flight Manual
Reissued: 16 Jan 2019
8-i
Sec tion VIII
AD DI TIONAL OP ER A TIONS AND
PER FOR MANCE DATA
IN DEX
Paragraph Title Page
Fig ure 8-1. Hover Ceil ing Out of Ground Ef fect
Ver sus Gross Weight (3200 rpm).........
Fig ure 8-2. Rate of Climb Chart (Stan dard Day,
No Muf fler, 3200 rpm, Max i mum Rate of Climb
Speed: 47 mph IAS.................
Fig ure 8-3. Fuel Flow (Stan dard Day, No
Muffler, Lycoming HIO-360-D1A, 3200 rpm) .
Fig ure 8-4. Max i mum Cruise Speed (3200 rpm,
No Muf fler) ....................
Fig ure 8-5. Cruise Chart (Sea Level, Stan dard
Day, 3200 rpm, No Muf fler) ...........
Fig ure 8-6. Cruise Chart (4000 ft, Stan dard Day,
3200 En gine rpm, No Muf fler) ..........
Fig ure 8-7. Range and En dur ance (Sea Level,
Stan dard Day, 3200 En gine rpm, No Muf fler) .
Fig ure 8-8. Range and En dur ance (4000 ft,
Stan dard Day, 3200 En gine rpm, No Muf fler) .
Fig ure 8-9. Pay load - Range (Sea Level to 4000
ft, Stan dard Day, 3200 En gine rpm, No Muf fler)
Fig ure 8-10. Rate of De scent (Auto ro ta tion,
471 Ro tor rpm)...................
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8-3
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8-5
8-6
8-7
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8-9
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8-11
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
SCHWEIZER
Model 269C Helicopter
CSP Book 1 CSP-C-1.indd 177 8/4/19 12:46 PM