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Zenith STOL CH 750
2.7 WEIGHT LIMITS
Maximum Take-off Weight ............................................................. 600 Kg
Maximum Landing Weight .............................................................. 600 Kg
Maximum Weight in Baggage Compartment ................................... 18 Kg
2.8 CENTER OF GRAVITY
Datum Reference
Mean Aerodynamic Cord (MAC)
Maximum Forward Station
Maximum Aft Station
See Section 6 "Weight & Balance" for further information.
2.9 APPROVED MANEUVERS
This airplane is accepted for flights as per the Normal Category. Intentional
spins and aerobatics maneuvers are prohibited.
2.10 MANEUVERING LOAD FACTORS
Flight load limits
2.11 FLIGHT CREW
1 Pilot
2.12 KIND OF OPERATION
VFR day operation only
Issued: 01.02.2020
Airplane Flight Manual
Flaps up
Flaps extended
Revision 0, Dat. 01.02.2020
Wing leading edge
1480 mm (+/- 15) mm
MAC 19 % / 280 mm
MAC 34 % / 500 mm
Positive
Negative
Positive
Negative
HB-YRC
+ 4.0 G
- 2.0 G
+ 2.0 G
- 0.0 G
Page 17-93
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