| POSITION | DELIVERY | DEPOSIT | KIT PRICE | SELF-BUILD COST | BUILD ASSIST COST |
|---|---|---|---|---|---|
| Position No. 16 | 34 months | $50k | $247k | $450k | $750k |
| Position No. 26 | 36 months | $25k | $247k | $450k | $750k |
| POSITION | DELIVERY | DEPOSIT | KIT PRICE | SELF-BUILD COST | BUILD ASSIST COST |
|---|---|---|---|---|---|
| Position No. 16 | 34 months | $50k | $247k | $450k | $750k |
| Position No. 26 | 36 months | $25k | $247k | $450k | $750k |
Build options range from $450k for self-build to $750k for build assist. Fully built planes will be available for $850k-$1M after the flying prototype is completed.
Max Speed (KTAS)
IFR Range (NM)
Useful Load (lbs)
First two columns are Aerovolare engine – 2nd two columns are TIO-520
Or any engine of your choosing for price difference
| Cruise speed | 25,000 ft | 300 knots |
| Stall Speed | 72 knots w/flaps | 79 knots w/o flaps |
| Climb Rate | 2825 ft/min | 1 engine 1020 ft/min |
| Range | 1950 NM IFR w/R | 1980 NM VFR |
| VNE | 195 KIAS | |
| Take Off | over 50 foot | 1130 ft |
| Landing | over 50 foot | 1120 ft |
| Fuel Load | 120 gal | (can put 50+ more under luggage) |
| Empty Weight | 2400 lbs | |
| Useful Load | 1800 lbs | |
| Wingspan | 35.2' | |
| Wing Loading | 27lb/sq ft | |
| Tail Span | 94 inches | |
| Interior Cockpit | 52 inches | |
| Middle row | 56 inches wide | |
| Back seat | 55 inches wide | |
| Head Room Pilots | 36 inches | |
| Middle seats | 39 inches | |
| Back seats | 36 inches | |
| Baggage compartments | 2 | |
| Nose – outside entry | 12x18x18 | |
| Rear - behind seats | 36 inches deep and wide high | |
| Length | 29' | |
| High | 9.2' | |
| Kit Cost | $247,000 | $750k build assist |
| Cruise speed | 25,000 ft | 300 knots | 25,000 ft | 274 knots |
|---|---|---|---|---|
| Stall Speed | 72 knots w/flaps | 79 knots w/o flaps | 72 knots w/flaps | 79 knots w/o flaps |
| Climb Rate | 2825 ft/min | 1 engine 1020 ft/min | 2600 ft/min | 1 engine 700 ft/min |
| Range | 1950 NM IFR w/R | 1980 NM VFR | 1700 NM IFR w/R | 1760 NM VFR |
| VNE | 195 KIAS | 195 KIAS | ||
| Take Off | over 50 foot | 1130 ft | over 50 foot | 1280 ft |
| Landing | over 50 foot | 1120 ft | over 50 foot | 1360 ft |
| Fuel Load | 120 gal | (can put 50+ more under luggage) | 120 gal | |
| Empty Weight | 2400 lbs | 2800 lbs | ||
| Useful Load | 1800 lbs | 1400 lbs | ||
| Wingspan | 35.2' | 35.2' | ||
| Wing Loading | 27lb/sq ft | 27lb/sq ft | ||
| Tail Span | 94 inches | 94 inches | ||
| Interior Cockpit | 52 inches | 52 inches | ||
| Middle row | 56 inches wide | 56 inches wide | ||
| Back seat | 55 inches wide | 55 inches wide | ||
| Head Room Pilots | 36 inches | 36 inches | ||
| Middle seats | 39 inches | 39 inches | ||
| Back seats | 36 inches | 36 inches | ||
| Baggage compartments | 2 | 2 | ||
| Nose – outside entry | 12x18x18 | 12x18x18 | ||
| Rear - behind seats | 36 inches deep and wide high | 36 inches deep and wide high | ||
| Length | 29' | 29' | ||
| High | 9.2' | 9.2' | ||
| Kit Cost | $247,000 | $750k build assist |
| @6,000 @75% power | 230 knots burning 32 gph |
| @18,000 @75% power | 250 knots burning 26 gph |
| @25,000 @75% power | 300 knots burning 22 gph |
| Stall Speed | Climb Rate |
| 72 knots w/flaps | 2825 ft/min |
| 79 knots w/o flaps | 1 engine 1020 ft/min |
| @6,000 @75% power | 230 knots burning 32 gph |
| @18,000 @75% power | 250 knots burning 26 gph |
| @25,000 @75% power | 300 knots burning 22 gph |
| Stall Speed | Climb Rate |
|---|---|
| 72 knots w/flaps | 2825 ft/min |
| 79 knots w/o flaps | 1 engine 1020 ft/min |
| @18,000 @65% power | 248 knots burning 22 gph | 1233 nm |
| @18,000 @55% power | 235 knots burning 18.6 gph | 1400 nm |
| @18,000 @45% power | 220 knots burning 15.2 gph | 1625 nm |
| @18,000 @35% power | 202 knots burning 12 gph | 1950 nm |
| @18,000 @65% power | 248 knots burning 22 gph | 1233 nm |
| @18,000 @55% power | 235 knots burning 18.6 gph | 1400 nm |
| @18,000 @45% power | 220 knots burning 15.2 gph | 1625 nm |
| @18,000 @35% power | 202 knots burning 12 gph | 1950 nm |
| @25,000 @65% power | 270 knots burning 22 gph | 1110 nm |
| @25,000 @55% power | 258 knots burning 18.6 gph | 1315 nm |
| @25,000 @45% power | 239 knots burning 15.2 gph | 1590 nm |
| @25,000 @35% power | 218 knots burning 12 gph | 1989 nm |
| @25,000 @65% power | 270 knots burning 22 gph | 1110 nm |
| @25,000 @55% power | 258 knots burning 18.6 gph | 1315 nm |
| @25,000 @45% power | 239 knots burning 15.2 gph | 1590 nm |
| @25,000 @35% power | 218 knots burning 12 gph | 1989 nm |
| Take Off | Landing |
|---|---|
| over 50 foot, 1130 ft | over 50 foot, 1020 ft |
| Empty Weight | Useful Load |
| 2400 lbs | 1800 lbs (1900 lbs an added option) |
| Kits is $247k for composite and unique parts only | 12 - 36 months delivery depending on position |
| Flying planes will be $850k to 1M - when we have the flying prototype, we will be auctioning off the first two planes for first quarter 2026 delivery |
| Company | Veloce 600 Pressurized Twin | Van's Aircraft | Velocity Inc | Evolution Aircraft | Cirrus Aircraft | Cirrus Jet | Diamond Aircraft | Beechcraft |
|---|---|---|---|---|---|---|---|---|
| Website | www.VelocePlanes.com | www.vansaircraft.com | www.velocityaircraft.com/v-twin | evolutionaircraft.com | cirrusaircraft.com | cirrusaircraft.com | diamondaircraft.com/en/private-pilots/aircraft/da62/overview/ | beechcraft.txtav.com/en/baron-g8.com |
| Price | $247,000 | $54,000 | $127,000 | 1M | 1M | 2.5M | 1.5M | 1.5M |
| Price Complete | $750,000 | $175,000 | $250,000 | 1M | 1M | 2.5M | 1.5M | 1.5M |
| Engine | AV 350 HP | Lycoming IO-540 235 - 260 HP | Lycoming IO 320 (160hp) Lycoming IO 360 (180hp) Titan IO 370 (190hp) | YTEO-540-iE2 350 hp | TSIO-550-K Turbocharged 315hp | FJ33-5A Thrust ~1,846 lbs | 2 × Austro Engine AE 330 turbocharged 2.0 180 HP | CONTINENTAL IO-550-C 300 hp |
| Cruise | 300 ktas at FL250 @32 gph 270 ktas at FL250 @24 gph | 194mph 75% @ 8000ft 235HP | 205 ktas | 230 ktas @ 24,000 Economy Cruise 215 KTAS | 213 ktas | 311ktas | 75 % (12,000 ft) 171 kts TAS - 317 km/h TAS; Cruise Speed at 85 % (12,000 ft) 185 kts TAS - 342 km/h TAS; | 202 ktas |
| Range | VFR Range 1233 nm @18,000 @65% power, 248 knots burning 22 gph, 1950nm @18,000 @35% power, 202knots burning 12 gph IFR Range 1989 nm @25,000 @35% power, 218 knots burning 12 gph | 1000 NM | 1400 NM | 1380 NM | 1,021nm | 1,275nm/td> | 1,283 nm | 1,480 nm |
| Take Off | 1130 ft | 360 ft | 1500 ft | 1450 ft | 1,517 ft | 2,036 ft | 1,574 ft | 1,373 ft |
| Landing | 1020 ft | 525 ft | 1500 ft | 1650 ft | 1,178 ft | 1,628 ft | 1,447 ft | |
| Stall speed | 72 knots w/flaps, 79 knots w/o flaps | 57 mph | - | Vs 76 KTS; Vso 61 KTS | Stall Speed with Flaps 60 kcas | Stall Speed with Flaps 67 knots | 64 KIAS | 74 KIAS |
| Empty weight | 2400 lbs | 1630 Ibs | 2000 Ibs | 2650 lbs | 2,354 lbs | 3,550 lbs | 3,505 lbs | 3965 lbs |
| Max weight | 4200 lbs | 2700 | 3200 | 4550 lbs | 3600 lbs | 6,000 lbs | 4,100 lbs | 5,500 lbs |
| Useful load | 1800 lbs | 1100 lbs | 1380 Ibs | 1,400 lbs | 1,246 lbs | 2450 lbs | 1,565 lbs | 1,559 lbs |
| Company | Veloce 600 Pressurized Twin |
Van's Aircraft | Velocity Inc | Evolution Aircraft |
Cirrus Aircraft | Cirrus Jet | Diamond Aircraft | Beechcraft |
|---|---|---|---|---|---|---|---|---|
| Website | www.VelocePlanes.com | www.vansaircraft.com | www.velocityaircraft.com/v-twin | evolutionaircraft.com | cirrusaircraft.com | cirrusaircraft.com | diamondaircraft.com/en/private-pilots/aircraft/da62/overview/ | beechcraft.txtav.com/en/baron-g8.com |
| Price | $247,000 | $54,000 | $127,000 | 1M | 1M | 2.5M | 1.5M | 1.5M |
| Price Complete |
$750,000 | $175,000 | $250,000 | 1M | 1M | 2.5M | 1.5M | 1.5M |
| Engine | AV 350 HP | Lycoming IO-540 235 - 260 HP | Lycoming IO 320 (160hp) Lycoming IO 360 (180hp) Titan IO 370 (190hp) |
YTEO-540-iE2 350 hp | TSIO-550-K Turbocharged 315hp | FJ33-5A Thrust ~1,846 lbs | 2 × Austro Engine AE 330 turbocharged 2.0 180 HP | CONTINENTAL IO-550-C 300 hp |
| Cruise | 300 ktas at FL250 @32 gph 270 ktas at FL250 @24 gph | 194mph 75% @ 8000ft 235HP | 205 ktas | 230 ktas @ 24,000 Economy Cruise 215 KTAS | 213 ktas | 311ktas | 75 % (12,000 ft) 171 kts TAS - 317 km/h TAS; Cruise Speed at 85 % (12,000 ft) 185 kts TAS - 342 km/h TAS; | 202 ktas |
| Range | VFR Range 1233 nm @18,000 @65% power, 248 knots burning 22 gph, 1950nm @18,000 @35% power, 202knots burning 12 gph IFR Range 1989 nm @25,000 @35% power, 218 knots burning 12 gph |
1000 NM | 1400 NM | 1380 NM | 1,021nm | 1,275nm/td> | 1,283 nm | 1,480 nm |
| Take Off | 1130 ft | 360 ft | 1500 ft | 1450 ft | 1,517 ft | 2,036 ft | 1,574 ft | 1,373 ft |
| Landing | 1020 ft | 525 ft | 1500 ft | 1650 ft | 1,178 ft | 1,628 ft | 1,447 ft | |
| Stall speed | 72 knots w/flaps, 79 knots w/o flaps |
57 mph | - | Vs 76 KTS; Vso 61 KTS |
Stall Speed with Flaps 60 kcas | Stall Speed with Flaps 67 knots | 64 KIAS | 74 KIAS |
| Empty weight | 2400 lbs | 1630 Ibs | 2000 Ibs | 2650 lbs | 2,354 lbs | 3,550 lbs | 3,505 lbs | 3965 lbs |
| Max weight | 4200 lbs | 2700 | 3200 | 4550 lbs | 3600 lbs | 6,000 lbs | 4,100 lbs | 5,500 lbs |
| Useful load | 1800 lbs | 1100 lbs | 1380 Ibs | 1,400 lbs | 1,246 lbs | 2450 lbs | 1,565 lbs | 1,559 lbs |
Currently, all pieces are completed and controls installed. engine nacelles are the only pieces left to make. otherwise, it’s mostly just fuel, door, and interior.
The prototype is expected to be flying in August 2025