Zenith Aircraft Corp American Albatross B-1

Zenith B-1 NX6772

Designed by Charles Rocheville, the sole 1928 American Albatross B-1 NX6772 was sold in 1929 to (Alva Roy) Ebrite Aero Corp of Long Beach CA, for charter work and is sometimes seen as Ebrite New Albatross, reportedly repowered with 400hp P&W Wasp. It was used for 1929 endurance record attempts by John Gugliemetti and Lee Schoenhair, but without success.

Engine: 260hp Menasco-Salmson
Wingspan: 56’0″
Length: 39’0″
Useful load: 2350 lb
Max speed: 128 mph
Cruise speed: 92 mph
Stall: 40 mph
Range: 1000 mi
Seats: 8

Zenith Aircraft Corp Albatross Z-12 / Schofield Albatross

Zenith Z-12 NX3622

The sole 1927 Albatross Z-12, or Schofield Albatross, NX3622, succeeded, after four attempts, in taking off with 9898 lbs, 2.47 times its empty weight, in a 1928 demonstration flight.

Engine: 3 x 125hp Siemens-Halske
Wingspan: 90’0″
Length: 47’6″
Useful load: 9650 lb
Max speed: 110 mph
Cruise speed: 95 mph
Stall: 48 mph
Range: 6700 mi
Fuel capacity: 1300 USgallon
Seats: 12

Zenith Aircraft Corp Albatross Z 6

The 1927 Albatross Z-6 six place biplane was designed by Charles Rocheville, Albin Peterson. Three were built: NX578K, N7076, and NX707E, and one conversion: NX7580.

The two Albatross Z-6-A (ATC 2-269) of 1928 seated four in the cabin. For $20,000, one was for Bennett Air Lines in Idaho (NC392V), and one with ATC 2-212 for 450hp Wasp SC conversion (NC134W).

Zenith Z-6-A NC392V

NC392V was restored in 2006 at PAR, Maryland Heights MO.

Three Albatross Z-6-B were built in 1929 (ATC 2-315). At $20,000, they were NC835Y, NC935Y, and NC977Y.

Zenith Z-6-B NC935Y

Gallery

Albatross Z-6
Engine; 220hp Wright J-5
Wingspan: 38’5″
Length: 30’0″
Useful load: 1667 lb
Max speed: 110 mph
Cruise speed: 95 mph
Range: 54 mph
Range: 500 mi
Seats: 6

Albatross Z-6-A
Engine: 420hp P&W Wasp C
Wingspan: 47’6″
Length: 29’9″
Useful load: 2100 lb
Max speed: 155 mph
Cruise speed: 130 mph
Stall: 58 mph
Range: 650 mi

Albatross Z-6-B
Engine: 420hp P&W Wasp C
Wing span: 41’6″
Length: 30’0″
Useful load: 1918 lb
Max speed: 150 mph
Cruise speed: 125 mph
Stall: 58 mi
Range: 650 mi
Seats: 7

Zenair Zipper

Single seat single engined high wing mono¬plane with conventional three axis control. Wing has unswept leading edge, swept for¬ward trailing edge and tapering chord; con¬ventional tail. Pitch control by fully flying tail; yaw control by fully flying rudder; roll control by half span ailerons; control inputs through stick for pitch/roll and pedals for yaw. Wing braced from below by struts; wing profile double surface. Undercarriage has three wheels in tricycle formation; glass fibre sus¬pension. Push right go right nosewheel steer¬ing connected to yaw control. Aluminium tube and sheet framework, with optional total enclosure pod. Engine mounted at wing height driving tractor propeller. All aluminium and hardware is of aircraft quality.
The Zipper is a conventional three axis machine with rudder pedals and centre stick, and it appears to be quite conventional in its choice of materials, being basically a tube and Dacron machine. There are some interesting features though, such as the tail boom, which is not tubular but is constructed of sheet aluminium alloy formed into a rectangular cross section.
Most of the innovation, however, is centred on the wing design, which has an unusual shape plan, with ailerons attached to the trailing edges. The design allows the wing to be folded in two minutes, the maker claims, after which the aircraft can be towed on its own wheels, avoiding the expense of a trailer.
Engine is the direct drive JPX PUL425, which is available in two states of tune 22 hp standard or 26hp with tuned exhaust. The aircraft is sold in kit form, but Zenair says the kit takes only an afternoon to complete, having already been test assembled in the factory before shipping. Other options include floats and wheel spats, while an enclosed cockpit, skis and propeller spinner are also offered.

Length overall 14.5 ft, 4.42 m
Height overall 5.5ft, 1.68m
Wing span 28.0ft, 8.53m
Mean chord 5.0ft, 1.52m
Sweepback 0 deg
Total wing area 140 sq.ft, 13.0 sq.m
Wing aspect ratio 5.6/1
Engine: JPX PUL425, 22hp at 4600rpm
Propeller diameter 42 inch, 1.07 m
No reduction
Max static thrust 180 lb, 82 kg
Power per unit area 0.16hp/sq.ft, 1.7hp/sq.m
Fuel capacity 6.0 US gal, 5.0 Imp gal, 22.7 litre
Empty weight 180lb, 82kg
Max take off weight 420 lb, 191 kg
Payload 240 lb, 109 kg
Max wing loading 3.00 lb/sq.ft, 14.7 kg/sq.m
Max power loading 19.1lb/hp, 8.7kg/hp
Load factors +6.0, 3.0 design
Max level speed 50 mph, 80 kph
Never exceed speed 80 mph, 129 kph
Cruising speed 40mph, 64 kph
Stalling speed 20 mph, 32 kph
Max climb rate at sea level 700 ft/min, 3.6 m/s
Take off distance 120 ft, 35 m
Landing distance 80 ft, 25 m
Range at average cruising speed 100 mile, 161 km
Seats: 1

Zenair CH801 Super STOL

The STOL CH 801 was developed to provide maximum short-field performance while being easy to build and maintain. The STOL CH 801 is a four-seat sport utility kit aircraft based on the two-seat STOL CH 701.

Zenith CH-801 C-GCUI

The larger STOL CH 801 has been developed to expand the utility of the STOL CH 701 model by increasing the useful load from 500 lbs. (225 kg) to 1,000 lbs. (450 kg.) while retaining the original design’s short and rough field capability. While the two designs share many similarities in appearance, they actually do not share any airframe parts due to the significantly larger size of the STOL CH 801.

Built of all-metal construction, the STOL CH 801 is designed to provide the durability and ruggedness required of an “off-airport” bushplane with high-lift wing with slats and flaps, the kit (basic airframe) was $18,490, and $20,950 in 2002.

Engine: Subaru, 180 hp
Wing span: 9.4 m / 30 ft 10 in
Wing area: 15 sq.m
Length: 23 ft 2 in
MAUW: 920 kg
Empty weight: 460 kg
Fuel capacity: 150 lt
Max speed: 200 kph / 125 mph
Cruise speed: 175 kph / 110 mph
Minimum speed: 62 kph / 39 mph
Climb rate: 5.3 m/s
Take-off roll: 200 ft
Landing roll: 150 ft
Seats: 4
Fuel consumption: 30 lt/hr

Engine: Lycoming O-360-A, 180 hp
Prop: Sensenich 76-EM8-0-54 fixed
Engine range: 150 – 240 hp, 440lb
Length: 24 ft.6 in./ 7.5 m.
Height: 10 ft.0 in./ 3.0 m
Ultimate load: + 5.7, – 2.8g
Wing Span: 31 ft.4 in./ 9.55 m
Wing Area: 167 sq.ft./ 15.5 m.sq.
Wing Chord: 5 ft.3 in./ 1.6 m
Empty Weight: 1,150 lb./ 522 kg
Horizontal Tail Span: 10 ft.1 in./ 3.1 m
Gross Weight: 2,200 lb./ 1,000 kg
Horizontal Tail Area: 30 sq.ft./ 2.8 m.sq
Useful Load: 1,050 lb./ 478 kg
Fuel Cap (Std): 30 USG. (2 x 15)/ 112 lt (2 x 56)
Design Payload: 800 lb./ 360 kg.
Fuel Cap (Opt): 60 USG. (4 x 15)/ 224 lt (4 x 56)
Wing Loading: 13.2 lb /sq.ft /64.4 kg/m sq.ft.
Power Loading: 11.95 lb /hp / 5.44 kg/hp
Cabin Width: 44 in/112 cm.
Cabin Length: 78 in/198 cm
Max. Flap Speed: 80 mph/129 km/h
Max. Cruise: 120 mph/193 km/h
Vne: 150 mph/240 km/h
Take-Off Roll: 290-390 ft./ 88-119 m
Max Level Speed: 110 -112 mph/178-181 km/h
Cruise (75%, 7,000 ft.): 105 -106 mph/169-170 km/h
Stall (Flaps Dn): 35-39 mph/56-64 km/h
Stall (Flaps Up): 43-48 mph/69-77 km/h
Rate Of Climb: 720 -1,200 fpm/3.7 -6.1 m/s
Endurance (Std): 3.0 Hrs
Endurance (Opt): 6.0 Hrs.
Range (Std): 315 -320 sm/507 -515 km
Range (Opt): 630-640 sm/1015-1030 km.
Service Ceiling: 14,000 -16,000+ ft/4,267-4,875+ m.
Cockpit width: 44 in
Undercarriage: trigear