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STORM RALLY FOR SALE

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.

Storm Rally

 

 

 

 

 

STANDARD FEATURESRally cockpit


• 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

INSTRUMENTS

• Airspeed indicator • Hour meter
• Vertical Speed indicator • CHT
• Altimeter • Oil Temp
• Slip Indicator • Oil pressure
• Magnetic compass • Fuel Pressure
• Tachometer • RIL Fuel Level indicators

AVIONICS
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

Storm Rally layout

SPECIFICATIONS
  PERFORMANCE (ISA Conditions, SPECIFICATIONS Sea Level)
ENGINE
SPEED
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
PROPELLER
CRUISE
Number of blades: 3
Propeller type: Ground adjustable
Propeller : 70” WARP DRIVE
Range: 75% @ 2000 ft: 438 nm/504 sm
Duration: 4.1*hrs
RATE OF CLIMB AT SEA LEVEL: 800 fpm
SERVICE CEILING: 12,000 ft
FUEL
TAKEOFF PERFORMANCE

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
Oil
LANDING PERFORMANCE
Oil capacity: 0.8 gal

Ground roll: 450 ft
Total distance over 50 ft obstacle: 1000 ft
Maximum Aircraft Weights
Gross Take-off Weight: 1,320 lbs.
Standard Empty Weight, Basic: 760 lbs.
Maximum useful load: 560 lbs.
Baggage Allowance: 100 lbs.
Cabin and Entry Dimensions
STALL SPEED:
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
WING LOADING: 10.34 lbs/sq ft
GLIDE RATIO: 17:1
POWER LOADING: 13.2 lbs/hp

 

Airspeed Limitations
KTS/MPH
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