
Seats
Up to 204
Cruise
Mach 0.95
Range
4,000+ nm
Span
124 ft
Length
150 ft
MTOW
190,000 lb
Overview
The SM-920 is a revolutionary twin engine single aisle commercial airliner that will set a new standard for efficiency, performance, eloquence and style. Up to 204 passengers at near sonic speeds.

The SM-920 is a revolutionary twin engine single aisle commercial airliner that will set a new standard for efficiency, performance, eloquence and style. It is the first airliner to benefit from an all new configuration in the last 50 years and is more aerodynamically refined and optimized than any other aircraft in the industry. With its distinguished style, the SM-920 will carry up to 204 passengers at near sonic speeds with unmatched economy, comfort and low environmental impact.
The SM-920 configuration combines a high aspect ratio M wing optimized for transonic flight with twin engines encased in novel nacelles that incorporate variable geometry air intakes and exhaust nozzles and serve as an end junction to the horizontal stabilizer. With a single vertical stabilizer, the SM-920 has a highly swept wing and a high fineness ratio, speed optimized fuselage. A modular airplane, the SM-920 will be constructed primarily from aluminum lithium foam metal sandwich structures that combine aluminum lithium and titanium skins with a laser welded aluminum foam metal core. Featuring aluminum lithium, scandium aluminum and titanium construction, the SM-920 exploits the advantages of proven advanced aluminums and superalloys.
The SM-920 is a transformational aircraft that will define the future. An extremely efficient twin engine 204 passenger airliner, the SM-920 will cruise at up to 0.95 Mach with a range in excess of 4,000 nm. Employing advanced foam metal sandwich construction, innovative air inlets and exhaust nozzles and a unique, highly efficient transonic cruise optimized wing, the SM-920 will compete with the Boeing 737 MAX and Airbus A320neo.
Designed to serve as a successor to the Boeing 737, Airbus A320 and Airbus A321 families of aircraft, the SM-920 is an original design conceived by Stavatti founder Christopher R. Beskar and is protected by USPTO Design Patent Number US D1,116,977 S. The SM-920 will be Type Certified as a Transport Category aircraft under FAA FAR Part 25.
Gallery
Authentic Stavatti imagery.















Variants
One airframe. Multiple missions.
SM-920
Baseline
PW1133G, LEAP-1A32, or NeoThrust E750 aft-fan options.
SM-920H
Hydrogen
Zero emission hydrogen fuel cell derivative.
SM-920F
Freighter
Narrowbody freighter. 58,000 lb payload, 12 AAA/AAY containers on the upper deck.
Data
Specifications and performance.
SM-920 Airliner
Aircraft
- Aircraft
- SM-920 narrowbody commercial airliner
- Manufacturer
- Stavatti Aerospace Ltd
- Unit flyaway cost
- $100,000,000
- First flight
- 2028-2029
- Availability
- Pre-Order Today to Secure Delivery Slot
- Crew / seating
- 2 / up to 204
Dimensions
- Wingspan
- 124 ft 0 in
- Length
- 150 ft 0 in
- Height
- 43 ft 4 in
- Wing area
- 1,500 sq ft
- Wing aspect ratio
- 10.25
- Wing LE sweep
- 36.0°
- Cabin length / max width / height
- 118 ft 5 in / 13 ft 8 in / 7 ft 6 in
- Cabin floor area
- 1,519 sq ft
Powerplant
- Number
- 2
- Type
- Geared turbofan
- Model
- PW1133G-JM
- Manufacturer
- Pratt & Whitney
- Max thrust (each / total)
- 33,110 / 66,220 lbs
- Inlet / nozzle
- Pitot shock / variable geometry
Weights
- Empty
- 100,000 lbs
- Max internal fuel
- 45,000 lbs
- Max fuel payload
- 43,000 lbs
- Max useful load
- 88,000 lbs
- Typical landing weight
- 147,874 lbs
- Max takeoff weight
- 190,000 lbs
Loadings
- Wing loading (MTOW / TLW)
- 127 / 99 lbs/sq ft
- Thrust to weight (MTOW / TLW)
- 0.35 / 0.45
- Design load factor (MTOW)
- +2.50
Passenger configurations
- First / economy two class
- 180
- Business / economy two class
- 182
- All business class
- 135
- Premium economy class
- 162
- All economy class
- 204
Performance
- Max level speed
- 0.95 Mach
- Max cruise
- 0.90 Mach
- Typical cruise
- 0.85 Mach
- Takeoff / approach / stall
- 157 / 122 / 106 KTAS
- Max climb at SL
- 10,110 ft/min
- Service ceiling
- 45,000 ft
- Range at 0.95 Mach / FL430
- 3,000 nm
- Range at 0.90 Mach / FL400
- 3,448 nm
- Range at 0.85 Mach / FL400
- 3,546 nm
- Range at 0.85 Mach / FL350
- 3,588 nm
- Takeoff ground roll / over 50 ft
- 4,765 / 5,853 ft
- Landing ground roll / over 50 ft
- 1,324 / 2,208 ft
Avionics & Displays
- Architecture
- Stavatti Avionics System Architecture (SASA)
- Displays
- Full panel active displays
- HUD
- Canopy Embedded Display (CED) / holographic MFD
- Flight controls
- Digital Power-By-Wire
- Navigation
- GPS/INS
- Surveillance
- ADS-B Out and In

