Extra 300S - Weight Limitations; Acrobatic Maneuver Limitations

Page Date: 20. April 2002 2 - 5
Pilot´s Operating Handbook
EXTRA 300S
Section 2
Limitations
f) Cylinder head temperature
-Max 500°F
2.5 PROPELLER
MT-Propeller Entwicklung GmbH, Federal Republic of Germany
a) Type MTV-9-B-C-/C 200-15
b) Type MTV-14-B-C-/C 190-17
-Max. Take-Off (max 5 min) 2700 RPM
-Max. Continuous 2400 RPM *
NOTE:
If not stated otherwise (refer to section: 4.12 Acrobatic Maneuvers) the aircraft may be
operated in acrobatic maneuvers up to 2700 RPM.
2.6 WEIGHT LIMITS
Max. allowed empty weight:
-Normal category 711 kg (1567 lbs)
-Acrobatic category 697 kg (1536 lbs)
Max. allowed T/O weight:
-Normal category 920 kg (2028 lbs)
-Acrobatic category 820 kg (1808 lbs)
Max allowed landing weight: 920 kg (2028 lbs)
2.7 WEIGHT AND C.G. ENVELOPE
Vertical reference = fire-wall.
Horizontal reference = upper longerons in cockpit.
2.7.1 NORMAL FLIGHT
Max T/O Weight: forward C.G. rear C.G.
920 kg (2028 lbs) 48.9 cm (19,3") 71,4 cm (28,1")
(and below)
2.7.2 ACROBATIC FLIGHT
Max T/O weight: forward C.G. rear C.G.
820 kg (1808 lbs) 48.9 cm (19,3") 71,4 cm (28,1")
(and below)
2.8 ACROBATIC MANEUVERS
2.8.1 NORMAL FLIGHT
All acrobatic maneuvers are prohibited except stall, chandelle, lazy eight and turns up to 60
degrees bank angle.
NOTE *
Page Date: 31. January 2006