Operations & Performance
Pilot's Flight Manual
8-3
0
2000
4000
6000
8000
10000
12000
14000
16000
0 200 400 600 800 1000 1200 1400
RATE OF CLIMB ~ FT/MIN
PRESSURE ALTITUDE ~ FT
GROSS WEIGHT ~ LBS
1700
1900
2050
ENGINE CRITICAL ALTITUDE
Figure 8-2. Rate of Climb Chart
Reissued:
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Rate of Climb Speed: 47 mph (41 knots) IAS
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 181 8/4/19 12:46 PM
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