Nexaer LS1

The Nexaer LS1, a 2-seat composite airplane that meets Light Sport Aircraft classifications and is being promoted and marketed by Sportplanes.com. The LS1, manufactured by Nexaer in Colorado Springs, Colorado, fetures a 54” wide cockpit, a cruise speed of 120 knots and a useful load in excess of 600 lbs. The prototype of the LS1 was unveiled at AirVenture 2005.
With a moulded carbon fiber composite structure, the Nexaer LS1 features a 4-point harness, and an all-plane parachute.

Standard features include:
No-flap
Tricycle landing gear for easy ground handling
Molded Kevlar® fuel tank (single center-mounted tank)
21-inch-wide seating with slide and tilt adjustment
Cabin heat and vent
Rear baggage compartment for standard cargo
Sporting goods cargo area for skiis, fishing poles, hunting gear, and golf clubs
Passenger-side glove compartment with flip-down tray and 12V power outlet

Standard Edition (SE)
Jabaru 2200 engine (80 hp)
Standard mechanical flight instruments (6-pack)
Standard analog engine gauges
Garmin SL-40 comm radio
Garmin GTX327 digital transponder
Single pilot-side yoke and pedals
Landing light
Navigation lights and strobes

Trainer Edition (TE)
Jabaru 2200 engine (80 hp)
Standard mechanical flight
instruments (6-pack)
Standard analog engine gauges
Garmin SL-30 nav/comm radio
Garmin GTX327 digital transponder
Dual flight controls
Landing light
Navigation lights and strobes
All-plane parachute

Luxury Edition (LE)
Jabaru 3300 engine (120 hp)
Dual electronic flight instrumentation system (EFIS)
Dual GPS
Electronic engine monitor with matching LCD display
Garmin SL-40 comm radio
Garmin GTX330 digital transponder
PSEngineering PCD7100-I stereo intercom with CD/MP3
2-axis digital autopilot
Single pilot-side flight controls
Landing light
Navigation lights and strobes
All-plane parachute
Keychain remote door unlock and open

Length: 23.25 ft.
Height: 7 ft. 10 in.
Wing span: 29.5 ft.
Wing Area: 124 sq. ft.
Cabin Width: 54 in.
Seat width: 21 in.
Max Gross Weight: 1320 lbs.
Empty Weight: 750 lbs.
Fuel Capacity: 27 USgal. (162 lbs.)
Useful Load: 570 lbs.
Design load factor: +4.5/-2.0 g
Power: 80 – 120 hp
Stall speed: 44 knots (51 mph)
Max speed in level flight: 120 knots (138 mph)
Maneuvering speed (VA): 105 knots (121 mph)
Never-exceed speed (VNE): 160 knots (184 mph)
Max rate of climb (sea level): 1500 ft./min
Max rate of climb (10,000 ft.): 700 ft./min
Service ceiling: TBD
Take-off distance (sea level): 350 ft
Take-off distance (10,000 ft): 750 ft
Endurance: 4 hours (with 30 minute reserve)
Range: 550 miles (ave.)

New Standard D-29 / NT-1

New Standard D-29A NC155M s/n 1007

The 1929 New Standard D-29 design (ATC 198) evolved from license-built Belgian Stampe-Vertongen D-29A. Probably only one machine was built, priced at $4,250.

Twenty-six of the 1929 D-29A (ATC 216) were built; NC36K, NC151N/158M, NC164M/172M, NC715Y, NC913V, NC922V/926V, and NC9195, powered by a Kinner K-5 and priced at $4,250.

New Standard D-29 Special NX172M

The D-29 Special of 1929 (2-326) was for 95hp Menasco B-4 installation as D-29 Special in NX172M c/n 1026.

New Standard D-29 Special NX172M

USN version with Kinner B-5 was NT-1.

The D-29S of 1930 (ATC 2-272) was a “Sport” version with coupe-type cockpit priced at $5,000.

One special model built for Charles H Day, NC173M c/n 1020; also appears on registers as D-25C.

D-29
Engine: 85hp Cirrus Mk III
Wingspan: 30’0″
Length: 24’11”
Useful load: 535 lb
Max speed: 88 mph
Cruise: 75 mph
Stall: 37 mph
Range: 300 mi
Seats: 2

D-29A
Engie: 100hp Kinner K-5
Wingspan: 30’0″
Length: 24’8″
Useful load: 625 lb
Max speed:: 98 mph
Cruise: 80 mph
Stall: 42 mph
Range: 250

D-29 Special
Engine: 95hp Menasco B-4 i

NT-1
Engine: Kinner B-5

D-29S
Useful load: 655
Max speed: 102 mph
Cruise: 85 mph
Stall: 45 mph
Range: 340 mi

D-25C
NC173M c/n 1020