Blackshape Prime - 2.9. Centre of Gravity; 2.10. Approved Maneuvers; 2.11. Maneuvering Load Factors

CF 300 – Flight Manual sect. 2 – Operating limitations
BY BLACKSHAPE
Document
n° BPU/FM003 Rev 3 dtd 03/06/2014 Page 22
-66
2.9. CENTER OF GR AVITY
The center of gravity (CG) is described in section 6, section 6.4.4. and calculated using the maximum
take-off weight from the table of weights centering. It is the responsibility of the pilot to ensure,
depending on the loading of the airplane, the correct weight and balance in flight line.
· FWD limit 16.6% MAC
· AFT limit 36.6% MAC
· Reference Plane Engine firewall
2.10. APPROVED MANEUVERS
This airplane is for non-aerobatic use only. The aerobatic us
e does not includes:
· All the maneuvers related to “normal” flights;
· Stalls (except whip stalls)
· Lazy eight;
· Turns with angle of inclination not exceeding 60°
WARNING
ANY TYPE OF ACROBATIC OPERATION IS FORBIDDEN
2.11. MANEUVERING LOAD FACTORS
Table of structural maximum permissible load factors.
at V
A
at V
NE
With Flaps in
T/O or LDG
position
Positive
+ 4 + 4 + 2
Negative
- 2 - 2 + 0
UNCONTROLLED