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 (1750 pounds) and stan dard
day con di tions:
Best rate of climb speed 41 KIAS
Hovering ceil ing 4600 feet den sity al ti tude
(2-foot skid height, mix ture leaned)
Con trol la bil ity has been shown to be ad e quate in
17 kt (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
The Model 269C-1 He li cop ter meets FAR36 Ap pen dix J.
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
269A8257-9 Ex haust Pipe In stal la tion 78.8 dBA SEL
269A8263-1 Ex haust Dif fuser In stal la tion 81.8 dBA SEL
SCHWEIZER
Model 269C-1 Helicopter
FAA Approved
CSP book 2..indd 109 8/4/19 12:53 PM
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