CASA C-207 Azor

CASA 207

The Azor is basically a scaled-up version of the CASA 202 Halcon, intended as a 30-38 seat commercial transport.

CASA C-207 Azor Article

The prototype, completed in August 1955, was powered by two 2040 hp Bristol Hercules 730 engines.

Following the production of ten of the basic C-207-A 30-passenger transport aircraft for the Spanish Air Force (designated T.7A), CASA completed ten C-207-C (T.7B) Azors equipped for cargo carrying.

C.207C Azor

C-207
Engines: 2 x Bristol Hercules 730, 1522kW
Max Take-off weight: 16500 kg / 36376 lb
Empty weight: 10600 kg / 23369 lb
Payload: 3000kg / 6614 lb
Wingspan: 27.8 m / 91 ft 2 in
Length: 20.85 m / 68 ft 5 in
Height: 7.75 m / 25 ft 5 in
Wing area: 85.8 sq.m / 923.54 sq ft
Max. speed: 420 km/h / 261 mph
Cruise speed: 400 km/h / 249 mph
Ceiling: 8000 m / 26250 ft
Range w/max.payload: 2350 km / 1460 miles
Crew: 4
Passengers: 40

CASA C-202 Halcon

CASA 202

The second aircraft of original design to be produced in Spain, the CASA 202 Halcon flew for the first time on 21 May 1953. Twenty were being produced for Iberia’s internal routes.

CASA 202 Halcon
Engines: 2 x ENMA Beta B-4, 775 hp
Wingspan: 70 ft 9 in
Wing area: 617.6 sq.ft
Length: 52 ft 6 in
Height: 12 ft 6 in
Empty weight: 11,615 lb
Loaded weight: 17,900 lb
Max speed: 192.5 mph at SL / 230 mph at 23,950 ft
Cruise 70%: 205 mph
Service ceiling: 23,950 ft
Passenger capacity: 14-18
Crew: 3

CASA C 202 B Halcon
Engine: 2 x Wright Cyclone R 1850 56, 1282 hp
Length: 53.576 ft / 16.33 m
Height: 20.899 ft / 6.37 m
Wing span: 67.52 ft / 20.58 m
Wing area: 602.784 sq.ft / 56.0 sq.m
Max take off weight: 21278.3 lb / 9650.0 kg
Weight empty: 13825.4 lb / 6270.0 kg
Max. speed: 233 kts / 432 kph
Cruising speed: 215 kts / 398 kph
Service ceiling: 24934 ft / 7600 m
Wing load: 35.26 lb/sq.ft / 172.0 kg/sq.m
Range: 1485 nm / 2750 km
Crew: 2
Payload: 8pax

Carter 1911 biplane

In the UK in 1911 Mr. Carter was out on the new machine and with the engine running fairly well, the machine made a few hops. The machine is of the biplane type of very short span, with the upper planes of slightly greater span than the lower ones. There is no elevator in front, but that position is occupied by the engine and propeller. The engine is an 8-cyl. made by the Nonpareil Motor Fitting Co. at Birmingham. At present it gives about 60-hp, but when properly tuned up it is expected to reach about 80-hp Mr.Carter succeeded in getting the biplane off the ground for short distances.

Mr. Carter was also out with his biplane after having made a few alterations to the tail. The machine rises very rapidly, in one case getting off the ground in 15 ft. but no extended flights were made owing to the fact that the engine was not running up to form.

Carpenterie M 81 Butterfly

The M 81 uses mixed wood and steel construction, all covered in heat-shrunk Dacron.

Engine: Rotax 912, 80 hp
Wing span: 9.6 m
Wing area: 15.5 sq.m
MAUW: 450 kg
Empty weight: 255 kg
Fuel capacity: 40 lt
Fuel consumption: 15 lt/hr
Max speed: 150 kph
Cruise speed: 120 kph
Minimum speed: 65 kph
Climb rate: 3 m/s
Seats: 2
Price (1998): 30,000 DM
Kit price (1998): 20,000 DM

Carlson Sparrow

Sparrow II

The Carlson Aircraft Sparrow Ultralight is a three axis aircraft conforming to FAA 103 regulations.
The Sparrow II is a two seat version of the Sparrow ultralight with optional folding wings.

Gallery

Sparrow II
Engine: Rotax 582, 66 hp.
Speed max: 130 mph.
Cruise: 110 mph.
Range: 300 sm.
Stall: 36 mph.
ROC: 1750 fpm.
Take-off dist: 75 ft.
Landing dist: 150 ft.
Fuel cap: 10 USG.
Weight empty: 510 lbs.
Gross: 1050 lbs.
Height: 7.75 ft.
Length: 18 ft.
Wing span: 31.5 ft.
Wing area: 140 sq.ft.
Seats: 2.
Landing gear: nose wheel.

Sparrow II XTC
Engine: Subaru, 82 hp.
HP range: 66-85.
Speed max: 130 mph.
Cruise: 110 mph.
Range: 400 sm.
ROC: 1100 fpm.
Take-off dist: 150 ft.
Landing dist: 250 ft.
Service ceiling: 13,000 ft.
Fuel cap: 22 USG.
Weight empty: 600 lbs.
Gross: 1250 lbs.
Height: 7.75 ft.
Length: 18 ft.
Wing span: 31.17 ft.
Wing area: 140 sq.ft.
Seats: 2.
Landing gear: nose wheel.
Optional Continental C-85 or Rotax 912 engine.

Sparrow Sport Special
Engine: Rotax 503, 52 hp.
Speed max: 120 mph.
Cruise: 85 mph.
Range: 300 sm.
Stall: 31 mph.
ROC: 1750 fpm.
Take-off dist: 85 ft.
Landing dist: 175 ft.
Service ceiling: 12,000 ft.
Fuel cap: 10 USG.
Weight empty: 360 lbs.
Gross: 710 lbs.
Height: 5.3 ft.
Length: 16.8 ft.
Wing span: 26.8 ft.
Wing area: 117 sq.ft.
Seats: 1.
Landing gear: tail wheel.

Sparrow Ultralight
Engine: Rotax 277, 28 hp.
Wing span: 30.2 ft.
Wing area: 120 sq.ft.
Length: 16.75 ft.
Height: 6.75 ft.
Weight empty: 115 kg / 254 lbs.
MTOW Weight: 229 kg / 504 lbs
Fuel cap: 5 USG.
Cruise: 50 kt / 58 mph / 93 kmh.
Range: 200 sm.
Stall: 26 mph / 23 kt / 42 kmh
VNE: 55 kt / 63 mph / 101 kmh
ROC: 750 fpm.
Take-off dist: 140 ft.
Landing dist: 195 ft.
Service ceiling: 10,000 ft.
Seats: 1.
Landing gear: nose wheel.