Shark UL - 2.7. Center of Gravity (CG); 2.8. Approved Maneuvers; 2.9. Maneuvering Load Factor G

Page 2-6
Flight manual UL aircraft
2.7. CENTER OF GRAVITY (CG)
The values for ready to fly airplane (including fuel, crew, baggage).
Front center of gravity limit
16 % MAC
Rear center of gravity limit
34 % MAC
See Section 6 for center of gravity calculation.
Retraction of landing gear moves CG 0,5-1% backwards.
2.8. APPROVED MANEUVERS
The Shark Airplane may perform:
- turns required for normal flying
- practicing falls
- steep turn (max. bank 60°)
WARNING:
All maneuvers must be performed with a positive overload
because the fuel and lubrication system is designed for positive
overloads. All maneuvers must be performed in a maneuver
envelope with maximum positive + 4g and negative -2g overload.
WARNING: Aerobatics, intentional stalls and spins are prohibited.
Maximum angle of bank: 60°
2.9. MANEUVERING LOAD FACTOR G
Flap up 0°
Maximum positive center of gravity load factor
+ 4
Maximum negative center of gravity load factor
- 2
Flaps down
Maximum positive center of gravity load factor
+ 2
Maximum negative center of gravity load factor
0
2.10. FLIGHT CREW
Minimum crew on board 1 pilot
Maximum crew on board 2 persons