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Schweizer S300C 269C - Section V - PERFORMANCE DATA (FAA APPROVED)

Schweizer S300C 269C
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Performance
Pilot's Flight Manual
Reissued:
5-i
Sec tion V
PER FOR MANCE DATA
IN DEX
Paragraph
Title Page
5-1
5-2
Per for mance Data .................
Noise Level ....................
evruC noit arb i laC deeps riA 1-5 eru giF ....
Figure5-1A Air speed Cal i bra tion Curve-Heated
Pitot Tube ....................
ta marg a iD yti col eV thgieH 2-5 eru giF
Sea Level ....................
ytis neD sus reV thgieW ssorG 3-5 eru giF
Al ti tude at Take off ...............
gni lieC revoH tcef fE dnuorG nI 4-5 eru giF
,thgieH dikS tooF-2( thgieW ssorG sus reV
3200 rpm)....................
gni lieC revoH tcef fE dnuorG nI 5-5 eru giF
,thgieH dikS tooF-2( thgieW ssor
G sus reV
)yti dim uH evit a leR %08 ,mpr 0023 .....
gni lieC revoH tcef fE dnuorG nI 6-5 eru giF
,thgieH dikS tooF-2( thgieW ssorG sus reV
3200 rpm)....................
5-1
5-1
5-2
5-2.1
5-3
5-4
5-5
5-6
5-7
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
Model 269C Helicopter
FAA Approved
CSP Book 1 CSP-C-1.indd 115 8/4/19 12:45 PM

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