Zenith STOL CH 750
Airplane Flight Manual
HB-YRC
Issued: 01.02.2020
Revision 0, Dat. 01.02.2020
Page 17-93
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
Wing leading edge
Mean Aerodynamic Cord (MAC)
1480 mm (+/- 15) mm
Maximum Forward Station
MAC 19 % / 280 mm
Maximum Aft Station
MAC 34 % / 500 mm
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
Flaps up
Positive
+ 4.0 G
Negative
- 2.0 G
Flaps extended
Positive
+ 2.0 G
Negative
- 0.0 G
2.11 FLIGHT CREW
1 Pilot
2.12 KIND OF OPERATION
VFR day operation only
