Performance
Pilot's Flight Manual
Reissued: 16 Jan 2019
5-1
Sec tion V
PER FOR MANCE DATA
5-1. PERFORMANCE DATA
Note
: The fol low ing per for mance fig ures are based
on nor mal gross weight (2050 pounds) and stan dard
day con di tions:
Best rate of climb speed: 41 knots (47 mph) IAS
Hovering ceil ing: 5900 feet al ti tude
(2-foot skid height)
Con trol la bil ity has been shown to be ad e quate in 17 knot
(20 mph) winds from any di rec tion.
In di cated air speed (IAS) cor rected for po si tion and
in stru ment er ror equals Cal i brated Air speed (CAS).
(See Fig ure 5-1, Air speed Cal i bra tion Curve.)
5-2. NOISE LEVEL
The Model 269C He li cop ter equipped as fol lows meets FAR 36
Ap pen dix J, Ad den dum 20. At max i mum gross weight, the he li -
cop ter pro duces the fol low ing noise lev els.
Ex haust Con fig u ra tion
Noise Level
269A8257-3/-9 Exhaust Pipe Installation 78.8
269A8801-5 Exhaust Muffler 81.1
269A8245-BSC Exhaust Muffler and
Resonator
79.2
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
SCHWEIZER
Model 269C Helicopter
FAA Approved
CSP Book 1 CSP-C-1.indd 117 8/4/19 12:46 PM
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