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TTA&E: 257 hrs. Fresh Annual. Rotax 912 ULS, GRT Sport 2000 PDF, GRT Eninge Monitor (EIS), Garmin 496 w/XM Wx, ICOM 760-Ch VHF Comm, Garmin 320 Transponder, PS Engineering Stereo Intercom, Electric Flaps, Trim, Toe Brakes, Stick mounted trim and PTT, Standby Altimeter & Airspeed, Wheel pants, Cruise 120 mph @ 4.7 gph. Hangared. $108,500.00 Will deliver.


• Rotax 912 ULS2 100HP engine
• 70”, 3-bladed ground adjustable prop
• Electric Elevator trim
• Steer-able nose gear
• Differential Toe Brakes (both sides)
• Cabin Heat System
• “Leather Touch” in-flight adjustable seats
• 4 point lap and shoulder seat belts
• 5” main landing gear wheels with disc brakes
• Center Console Parking brake
• Electric, 4-position flaps
• Wingtip Strobes, Tail Position & Landing Light
• Stick mounted elevator trim and comm.
Pilot Report on the Storm Rally
| • Airspeed indicator |
• Hour meter |
| • Vertical Speed indicator |
• CHT |
| • Altimeter |
• Oil Temp |
| • Slip Indicator |
• Oil pressure |
| • Magnetic compass |
• Fuel Pressure |
| • Tachometer |
• RIL Fuel Level indicators |
Choose from a wide variety of optional avionics including:
• Garmin or Icom VHF Comm
• Stereo Intercom
• Garmin GTX320A/GTX327 TSO transponder
• Ameri-King AK350 encoder
• Ameri-King AK450 ELT
• Dynon or Grand Rapids Technology EFIS & Engine Monitor
• GPS/Moving Map w/weather
• Optional 2-axis autopilot

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(ISA Conditions, SPECIFICATIONS Sea Level) |
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Engine: ROTAX 912 UL S2
Engine type: Normally aspirated, 4-cyl, 4-stroke, liquid/aircooled
engine with opposed cylinders, dry sump, forced lubrication
with separate 0.8 gal oil tank, 2 carburetors, mechanical and
electric fuel pumps, Ducati electronic dual ignition, electric
starter, integrated reduction gear 1:2.43.
HP rating: 100 BHP @ 5800 RPM, 95 BHP @ 5500 (continuous). |
Maximum at sea level: 120 kts/138 mph
Cruise (75% power @ 2000 ft): 107 kts/123 mph |
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Number of blades: 3
Propeller type: Ground adjustable
Propeller : 70” WARP DRIVE |
Range: 75% @ 2000 ft: 438 nm/504 sm
Duration: 4.1*hrs
800 fpm
12,000 ft |
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Fuel capacity
(both tanks):
Total usable: |
Std Tanks
24 US gal
21 US gal |
Long Range
35 US gal
31 US gal |
Ground roll: 360 ft
Total distance over 50 ft obstacle: 600 ft |
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Oil capacity: 0.8 gal
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Ground roll: 450 ft
Total distance over 50 ft obstacle: 1000 ft |
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Gross Take-off Weight: 1,320 lbs.
Standard Empty Weight, Basic: 760 lbs.
Maximum useful load: 560 lbs.
Baggage Allowance: 100 lbs. |
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Cabin Height: Top of seats to roof = 40”
Entrance Doors: 34” wide x 39” high
Length: Instrument panel to rear bulkhead—70”
Cabin width: 43.7”(Door to Door)
Baggage Area: 26” (L) x 28-42” (W) x 27- 32” (H)
Volume = + 16 cu. ft. |
Flaps up, power off: 44 knots
Flaps down, power off: 35 knots
10.34 lbs/sq ft
17:1
13.2 lbs/hp |
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| VNE (Do not exceed this speed—design limit) |
140/161 |
| VNE (L.S.A. limit) |
120/138 |
| VNO (Maximum structural cruising speed.) |
120/138 |
| VA (Maneuvering speed) |
88/101 |
| VFE/VLE (Maximum speed, flap extended) |
60/69 |
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