Sonex is excited to announce the approval of a higher maximum gross weight for all Sonex and Waiex aircraft powered by engines of 100hp or greater. Following a series of engineering studies and flight tests, Sonex and Waiex owners may designate a max. gross weight of 1220 lbs. for aircraft with 100hp or more. This represents a 70 lb. increase vs. the previous 1150 lb. limit and is applicable to both A-Model (Legacy) and B-Model aircraft.
"We expect these changes to be very popular and greatly expand the appeal of the Sonex and Waiex to today’s homebuilder," said Sonex owner and president Mark Schaible. "Due to the aerobatic load limit capability of the two aircraft models and the impending MOSAIC changes to the Light Sport Aircraft rules, we took the opportunity to study this change to our specifications. We are pleased to report that stall speed testing has proven the aircraft still qualify for Sport Pilots to fly under the existing rules."
Stall Speed: Still Sport Pilot Compliant!
While this additional gross weight allowance was originally intended for adoption after the FAA MOSAIC NPRM takes effect as a final rule with an increase in allowable stall speeds for Sport Pilots, the Sonex team is pleased to report that stall speeds observed between the two test aircraft are still within current Light Sport Aircraft limits.
Stall Speed at 1220 lbs. Gross Weight:
- Clean Stall Speed: 50 mph
- Full Flaps Stall Speed: 43 mph
Rate of Climb at 1220 lbs.
In addition to structural capability, the most important aspect of increasing gross weight is assuring safe climb performance. The numbers collected by the flight test aircraft are as-follows:
- AeroVee Turbo: 700 fpm @ 95 mph (with cruise prop)
- Rotax 912 100hp: 800 fpm @ 80 mph
Owners of complete and flying Sonex and Waiex aircraft wishing to make this change can do so in-accordance with their individual aircraft’s operating limitations. Changing the gross weight constitutes a "major change," and would be handled in the same manner as any other major change to an Experimental Amateur Built aircraft (installing a different prop or engine, floats, etc.). The operating limitations issued to the aircraft will include a process for incorporating a major change. For most operating limitations issued in the past 20 years or more, this will involve contacting the FAA FSDO to get a flight test area approved, then moving the aircraft back into Phase 1 flight testing via an aircraft logbook entry. The owner/operator would then test the aircraft up to the new gross weight, document the new performance characteristics (stall speeds, climb and glide rates, CG compatibility, etc.) for a minimum of 5 hours. Once the flight testing is completed, the owner/operator would then make another logbook entry, per the guidance found in the operating limitations, to move the aircraft back into phase 2 normal operations.
It is very important to follow the guidance found in each specific aircraft’s operating limitations with regard to incorporating a major change. Operating limitations have changed somewhat over the years, so what works for one aircraft may not work for another. Each individual will have to follow the procedure outlined in their particular operating limitations.
Updated Sonex-B and Waiex-B Specifications & Performance
Seats: | 2 |
Length: | 18′ 1″ |
Wing Span: | 22′ |
Wing Area: | 98.0 sq. ft. |
Tail Configuration: | Conventional (Sonex), Y-Tail (Waiex) |
Tail Height (Std Gear): | 56″ (Sonex), 51″ (Waiex) |
Tail Height (Tri-Gear): | 74″ (Sonex), 69″ (Waiex) |
Tail Width–with tail tips: | 92″ (Sonex), 88″ (Waiex) |
Main Gear Width: | 71″ (with wheel pants) |
Air Foil: | 64-415 |
Primary Structure: | 6061-T6 aluminum |
Cockpit Width (entire cockpit): | 40″ |
Fuel Capacity: | 20 US Gal. |
Stall Speed (full flaps): | 40-43 mph [64-69 km/h] |
Stall Speed (clean): | 46-50 mph [74-80 km/h] |
Max Flap Extended Speed (Vfe): | 100 mph [161 km/h] |
Maneuvering Speed: | 125 mph [201 km/h] |
Never Exceed Speed (Vne): | 197 mph [317 km/h] |
Performance | AeroVee 80hp | AeroVee Turbo 100hp | Jabiru 120hp |
---|---|---|---|
Basic Empty Weight | 680 lbs. | 700 lbs. | 700 lbs. |
Range (1) | 515-634 miles | 450-525 miles | 445-540 miles |
Cruise Speed @ Sea Level* | 130 mph | 135 mph | 135 mph |
Cruise Speed @ 8000 ft (TAS) | 150 mph | 165 mph | 170 mph |
T.O. Distance | 400 ft | 300 ft | 250 ft |
Landing Distance | 500 ft | 500 ft | 500 ft |
Service Ceiling (calculated) | 16,000 ft | 23,000 ft | 23,000 ft |
Utility Category | AeroVee 80hp | AeroVee Turbo 100hp | Jabiru 120hp |
Max. Gross Weight | 1100 lbs | 1220 lbs | 1220 lbs |
Baggage (Max) | 40 lbs | 40 lbs | 40 lbs |
Useful Load | 480 lbs | 530 lbs | 530 lbs |
Power Loading (GW/HP) | 13.75 lbs/hp | 12.2 lbs/hp | 10.16 lbs/hp |
Rate of Climb | 500-900 fpm | 700-1000 fpm | 1000-1400 fpm |
Stall Speed (full flaps) | 40 mph | 43 mph | 43 mph |
Stall Speed (clean) | 46 mph | 50 mph | 50 mph |
Positive Load Factor | +4.4 Gs | +4.4 Gs | +4.4 Gs |
Negative Load Factor | -2.2 Gs | -2.2 Gs | -2.2 Gs |
L/D | 11:1 | 11:1 | 11:1 |
CG Limits | 20-32% Wing Chord | 20-32% Wing Chord | 20-32% Wing Chord |
Aerobatic Category | AeroVee 80hp | AeroVee Turbo 100hp | Jabiru 120hp |
Gross Weight – Aerobatic | 950 lbs | 950 lbs | 950 lbs |
Baggage (Max) | 10 lbs | 10 lbs | 10 lbs |
Power Loading (GW/HP) | 11.875 lbs/hp | 9.5 lbs/hp | 7.9 lbs/hp |
Rate of Climb | 800-1100 fpm | 1000-1500 fpm | 1500-2000 fpm |
Positive Load Factor | +6.0 Gs | +6.0 Gs | +6.0 Gs |
Negative Load Factor | -3.0 Gs | -3.0 Gs | -3.0 Gs |
CG Limits | 23-29% Wing Chord | 23-29% Wing Chord | 23-29% Wing Chord |
*Note: All Models meet FAA Sport Pilot Regulations at maximum continuous power at Sea Level, as required. Read More…
(1) Range of various power settings and altitudes based on 15 gallons used for cruise flight and 5 gallons used for takeoff, climb, and 30 minutes reserve. At 8,000′ AeroVee powered Sonex/Waiex can acheive 150 mph TAS @ 3.5gph. Jabiru 3300 powered Sonex/Waiex can achieve 170 mph TAS @ 4.9gph at 8,000′.
Specifications subject to change without notice. |