Engine | Polini THOR 303 DS |
Propeller | E-Prop 2 blade Plug N Fly |
Reduction ratio | 2.88:1 |
Horsepower | 39 |
Gross Weight | 550 lbs |
Empty Weight | 254 lbs (rescue chute not incl) |
Useful Load | 296 lbs |
Wing Span | 26' .25" |
Wing Loading | 3.17-4.98 lb/sq ft |
Chord Length | 40.25" |
Chord Length with Flaperons | 52" |
Length (Nose cone to rudder tip) | 15' 8" |
Wings Folded Length (Nose cone to wing end rib) | 18' 6" |
Width (wings folded) | 19" |
Height (Standard landing gear) | 5'4" |
Track Width (main gear) | 5' 1" |
Tire Size | 15 x 6.00 – 6 |
Fuel Capacity | 5 Gallons |
Cabin Width | 24" |
Kit options may vary.[/vc_column_text]
Airspeed Limitations (IAS mph)
Vne Never exceed
---80 mph
Vno Maximum cruise
---63 mph
Va Maneuvering Speed
---59 mph
Vx Best Angle
---38 mph
Vy Best Rate
---47 mph
Vref Landing Reference
---40 mph
VsO Stall speed
---26 mph (full flaps)
Vr Rotate speed
---35 mph
Maximum at Sea Level ......................... 80 MPH
Cruise, 75% Power………….. ................. 54 MPH
5 Gallons Usable Fuel. .................... Time – 1.75 HRS
Range ……………………………............. Range - 100 NM
RATE-OF-CLIMB AT SEA LEVEL ...................... 750 FPM
Ground Roll .................................... *150 FEET
Total Distance Over 50 Foot Obstacle ............... *400 FEET
Ground Roll .................................... *100 FEET
Total Distance Over 50 Foot Obstacle ............... *400 FEET
**Normal operations.
Flaps Up, Power Off .............................. 32 MPH
Flaps Down, Power Off ........................... .26 MPH
Takeoff .................................... 550 POUNDS
Landing ................................... 550 POUNDS
STANDARD EMPTY WEIGHT .................... 254 POUNDS
MAXIMUM USEFUL LOAD ....................... 296 POUNDS
BAGGAGE ALLOWANCE ........................ 25 POUNDS
WING LOADING: Lbs/Sq. Ft. ............................. 4.981
POWER LOADING: Lbs/HP .............................. 14.102
FUEL CAPACITY ............................... 5 GALLONS
OIL CAPACITY .................................. 100cc (Gear box)
ENGINE: Polini THOR ......................... 303 DS 39 BHP at 8000 RPM
PROPELLER: Fixed Pitch, Diameter .................. 59 INCHES (150CM)
NORMAL CATEGORY / PART 103
MODEL F1-F5 *Exclds Light Sport/Experimental
Flight Load Factors (Maximum Takeoff Weight - 550 lbs.):
*Flaps Up . . . . . . . . . . . . . . . . . . . . . . . +3.8g, -1.52g
*Flaps Down . . . . . . . . . . . . . . . . . . . . . +3.0g
Gross Weight 550lbs
Takeoff: Minimum Field Length required to clear 50’ object -400’ (Engine dependent) Be safe.
Landing: Minimum Field Length required to clear 50’ object -400’ (Engine dependent) Act safe.
*The design load factors are 125% of the above, and in all cases, the structure meets or exceeds design loads.