Design parameters^*

The comprehensive and revolutionary design of the Brevity™ is based on thorough aerodynamic and technical studies and the latest technologies in epoxy reinforeced production methods. This combination enabled us to eliminate the major design flaws inherent with most of the current models of seaplanes.

The results of these studies have accumulate in a preliminary design that addresses a thriving and expanding General Aviation market. As the concept of the Brevity™ is an evolution of an existing JAR 23 certified aircraft design, certification risks are rather limited.

Below a brief overview reveal some of the Brevity's capabilities and advantages. Also engine, cockpit and some interior features are accessible via this list.

Principal dimensions:		Metric	English
	Length:	10,80 m	35,43 ft
	Width:	1,65 m	5.41 ft	(at max. cabin width)
	Height:	2,70 m	8,85 ft
	Wingspan:	11,85 m	36,08 ft	(excl. winglets)
	Wingsurface:	15,50 m²	161.45 ft2
Performance:
	Max. cruising speed:	261 kmh.	141 KIAS	SL/100%MCP
	Cruise speed:	250 kmh.	135 KIAS	8000ft/75%MCP
	Max. Climb speed:	289 mtr/min	950 ft/min.	at Slant MTOW
	Runway dist. at take-off:	TBD (STOL)	TBD (STOL)	(Compared with similar powered and wing loaded propeller aircraft).
	Max. range:	1595 kmh.	861 Nm.	at 60%MCP/8000ft (at best perform.)
Endurance:
		8 Hrs.		at full fuel and 75% MCP*)
		6.1 Hrs.		at full load and 75%MCP
		TBD		at 45% MCP
Weights:
	Max. take-off weight:	1500 / 1800 kg.	3306 / 3968 lbs
	Max. Landing weight:	1500 / 1800 kg.	3306 / 3968 lbs
	Empty weight:	950 / 1250kg.	2094 / 2756 lbs
	Useful load:	300 / 550 kg.	661 / 1212 lbs
Powerplant:
		549-595 kw.	420-450 SHP		Fact sheet
		746- 796 kw.	571-609 SHP		Fact sheet
Fuel tank capacity:		300-550 ltr.	79 - 145 galls	Depending on model and utility.
Seating capacity:		1 - 4		6 seat capacity in design.
	Configuration options:	2+2 (+2)
		1 or 2 + cargo		Rear seats removed.
		2 + stretcher		Right hand seats removed.
Storage capacity	Main cargo aerea	3,5 M2	123,60 ft2	(Depending on configuration)
	Front storage bay	0,11 M2	4 ft2	(Estimated)
Equipement				(VFR - IFR)
Certification				EASA CS-23
Click on the pictures for additional (design) information. MCP = Maximum Continues Power assumed to 450 or 609 SHP. TBD= To Be Determined