Limitations
Pilot's Flight Manual
SCHWEIZER
Model 269C Helicopter
2-6
Reissued:
16 Jan 2019
2-7. WEIGHT AND CG LIM I TA TIONS
Max i mum Gross Weight
Late he li cop ters (Se rial No. 210 and subs.) 2050 pounds
Early he li cop ters (Se rial No. 004 through 209) 1900 pounds
For ward CG limit sta tion = 95.0
Aft CG limit sta tion = 101.0
Note: Da tum line is 100.0 inches for ward of ro tor cen -
ter line.
Lat eral CG lim its
At Sta tion 95
+ 3.0 to -1.0
At Sta tion 99.5
+ 4.0 to -2.12
At Sta tion 101
+ 2.0 to -2.5
Lin ear vari a tions be tween cor ners: plus (“+”) is right of cen ter line,
mi nus (“-”) is left of cen ter line of he li cop ter when view ing for ward
(see Fig ure 2-2).
Note: Lat eral da tum line is the cen ter line of the he li -
cop ter through the main ro tor.
2-8. CENTER OF GRAV ITY (CG EN VELOPE)
The per mis si ble range of lon gi tu di nal and lat eral cen ter-of-grav ity
travel is il lus trated in Fig ure 2-2.
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
FAA Approved
CSP Book 1 CSP-C-1.indd 58
8/4/19 12:45 PM
Содержание S300C 269C
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