Canterbury (NZ) Aviation Co Biplane

The first NZ designed and built land-biplane, strongly reminiscent of a Sopwith Tabloid, was designed and built at the Canterbury (NZ) Aviation Co Ltd workshops at Sockburn, near Christchurch, the two persons most concerned with the construction being Mr C M Hill, the company’s chief flying instructor, and Mr J G Mackie, the engineer.

The working drawings for this unnamed biplane were chalked out on the black-painted wall of one of the early Sockburn hangars, which full size drawings was apparently quite satisfactory as the biplane performed well in the air. The drawings were so “permanent” that they could still be seen, according to Mr W S Dini, as late as 1938 when he left the RNZAF after 14 years’ service. Cupboards had been built along the rear wall of the hangar in later years, and these helped in no small measure to preserve the drawings.

The aeroplane was rolled out of its hangar on 17th January 1919, and was a two-seater fitted with a 30 h.p. Anzani radial motor which was originally used to power one of the School’s Caudron biplane trainers. Main spars were of ash and the wing struts were of cedar, with bracing wires encased in cedar streamlines. Ailerons were fitted (instead of the Caudrons’ wing-warping and the wings had a slight dihedral. The aircraft, according to the Lyttelton Times of 18th January’ was “produced with little or no effort”. Wings and fuselage were fabric-covered.

Mr Hill made the first solo flight in the biplane on 17th January and found that it had a good rate of climb and was light on the controls. It also had a shallow gliding angle for its type, and Mr Hill predicted that it would be suitable for aerobatics. He said on landing that he had never before tested an aeroplane in which everything was so satisfactory, and he praised Mr Mackie’s work in high terms. The only alteration he recommended after the first flight was a small one to the control circuits to enable the aeroplane to be flown hands-off in level flight. He found that, trimmed hands-off, it tended to climb slightly. A very short landing was made after that first flight, another good feature.

Plans were then made for a flying tour to Invercargill, the aeroplane to be flown by Mr Hill and demonstrations and passenger flights to be given at selected centres. Passengers would also be booked between several of the towns to be visited, and it was thought that with a full tankage of 27 gallons of petrol, two people could be carried about 200 miles in still air.

The longest passenger flight in NZ on record, according to the Lyttelton Times, was made on 18th January 1919 when Mr Hill took off from Sockburn for a 28 minute flight over Christchurch and New Brighton, with Mr E S Fleming as passenger. This presumably would be the longest passenger flight made by an aircraft of the Canterbury (NZ) Aviation Co.Ltd. Mr Fleming, of the Riccarton Flour Mills, was a brother of Mr W H P (Herby) Fleming of Gore, who had also booked a flight between Gore and Invercargill during the forthcoming tour. Mr E S Fleming’s flight was made at between 2 and 3,000 feet, and there were “no engine troubles”. Later flights the same day were made with passengers Mr A V Smith and Mr Notman.

The southern flight was never made as the biplane was completely wrecked and Mr Hill killed on 1st February. It had been the custom for an aeroplane of the Canterbury (NZ) Aviation Co. Ltd to make a flight over the Racecourses at Addington and Riccarton on Race days, and Mr Hill had been requested to fly over the Riccarton meeting on the 1st. The Hon. H F Wigram, chairman of the Company, asked the Chairman of the Jockey Club if he would like to have an exhibition flight over the Racecourse that Saturday afternoon as an added attraction, and so it was arranged with Mr Hill. Mr Hill took off from Sockburn at 3.11 pm and set course for the Racecourse’ where he appeared just as the Lyttelton Plate was being run. He circled twice, and finally flew low over the course, where he was cheered by the crowd as he went past.

Mr Hill waved to the crowd, and then circled again to get more height. Another wide sweep over the course was made at a height of 2000 feet, and then the aeroplane disappeared into cloud. On his reappearance, he dived the aeroplane and came over in a loop. It would appear that the aircraft had some difficulty in going over the top, and soon went into another dive. This final dive was made towards the crowd, and as the aircraft climbed into its second loop, a distinct crack was heard and the port wings collapsed. Mr Hill tried to hold the aircraft straight but this was impossible and the aeroplane then disappeared from sight behind a belt of trees.

When members of the public arrived at the scene of the crash Mr Hill was dead and the aeroplane completely wrecked. At the subsequent inquest and investigation it was found that a flying wire had broken and this in turn had caused the other flying wire to break. The main spars had then cracked and the whole port wing assembly folded up. It was said that ordinary piano wire had been used for the flying wires, instead of cable.

Mr Hill had not previously attempted any aerobatics with the aeroplane and indeed had not permitted anyone else to fly it until he had completely tested it to his satisfaction. It had only made a very few flights at the time of the accident and it was fortunate that no passenger was being carried at the time.

The Coroner, Mr T A B Bailey SM, found “That on 1st February, while the deceased was making an exhibition flight over the Riccarton Racecourse, and attempting to loop the loop, one wing of the machine collapsed and the machine fell to the ground, the deceased being killed as a result of the fall, The collapse of the wing appears to have been due to the breaking of one of the flying wires. The machine was built under the personal supervision of the deceased, who was a competent mechanic and he expressed himself satisfied with the machine”.

Engine: 30 h.p. Anzani
Wingspan: 23 ft 6 in
Length: 20 ft
Wing area: 220 sq.ft
All-up-weight: 500 lbs
Fuel capacity: 200 lbs
Seats: 2

Canterbury (NZ) Aviation Co. Ltd

The Flying Training School at Sockburn, operated by the Canterbury Aviation Company, was formed in 1917. The company had applied to the New Zealand Government for assistance and had been refused, and it had entered into an agreement with the British Government. Training started in June with one aircraft, a Caudron II with a sixty-horsepower Anzani engine.

The Canterbury (NZ) Aviation Co imported six Caudron GIII one and two-seat trainers, built up three locally made copies – #3 #5 and #9, aand built an own design biplane in 1919.

Cant Z.1018 Leone

Concurrently with development of the production models of the Alcione, Zappata was engaged on the development of the twin- engined Z.1018, the first of several prototypes of which flew in 1939.

The Z.1018 broke away from previous C.R.D.A. practice in featuring metal construction, although one of two Piaggio P.VII- powered prototypes tested an alternative wooden fuselage. Several types of engines were installed in the prototypes, one having Piaggio P.XV radials, another having Alfa Romeo 135 R.C.32 radials, and yet another having Daimler-Benz DB 605 engines. Some prototypes had twin fin and rudder assemblies, but a single unit was adopted far the production model which, powered by 1,400-h.p. Atfa Romeo 135 R.C.32 radials, began to appear in service in 1943 but was too late to participate extensively in the air war prior to ltaly’s collapse.

Cant Z.1011

A twin-engined medium bomber/transport powered by 840-h.p.Isotta-Fraschini Asso Xl R.C.15 engines. Five prototypes of the Z.1011 were built, but the bomber was under-powered and inadequate performance led to the abandonment of further development in favor of the Z.1007.

Cant Z.1007 Alcione

The Alcione (Kingfisher) was an Italian bomber of the Second World War, designed by the CRDA Cant, it was the company’s first landplane, and stemmed directly from the Z.506 Airone. The pro¬totype, flown in late 1937, had three Asso liquid cooled engines in annular cowls, but all production machines had radials, usually the 1000 hp Piaggio P.XIbis RC40.

Cant Z.1007 Alcione Article

First prototype of the Z.1007

Of all wooden construction, the Alcione had a long bomb bay under the wing able to carry up to 2000 (4410 lb). There were manual gun positions at front and rear of this bay (often the front position was used solely for bomb aiming) and most Alciones had a dorsal turret and two beam guns. The guns were at first all 7.7 mm, but by 1940 the dorsal and ventral guns were 12.7 mm. When Italy entered the war in 1940 there were 87 in service, and the type was being built by Cant, Piaggio and IMAM Meridionali. In 1941 the Z.1007bis appeared, with the fuselage 244 cm (96 in) longer, span 83 cm (33 in) greater and stronger landing gear. Many of these had twin fins.

Z.1007bis

The Alcione operated from Tunisia to the Soviet Union, often carrying two 450 mm (1000 lb) torpedoes or in the strategic recon¬naissance role. A few Z.1007ter, with 1175 hp Piaggio P.XIX engines, entered service in 1942. Cant tried to improve performance by fitting the 1500 hp Piaggio P.XIX engine, and at the very end of Italian participation in the war produced the Z.1018 Leone (Lion).

Gallery

CANT Z.1007bis Alcione (Kingfisher)
Engines: 3 x Piaggio P.XI RC.40 radial piston, 1,000 horsepower
Length: 60.20ft (18.35m)
Wing span: 81.36ft (24.80m)
Wing area: 807.300 sqft / 75.0 sqm
Wing load: 37.31 lb/sq.ft / 182.00 kg/sq.m
Height: 17.13ft (5.22m)
Maximum Speed: 301mph (485kmh; 262kts)
Maximum Range: 1,115miles (1,795km)
Range (max. weight): 945 nm / 1750 km
Service Ceiling: 24,606ft (7,500m; 4.7miles)
Armament: 3 x 12.7mm Scotti OR SAFAT heavy machine gun, 2 x 7.7mm SAFAT machine guns
Up to 2,645lbs of internal stores and up to 2,200lbs of external stores OR 2 x 1,800lb torpedoes.
Accommodation: 5
Hardpoints: 2
Empty Weight: 20,715lbs (9,396kg)
Maximum Take-Off Weight: 30,029lbs (13,621kg)

Cant Z.511

Z.511A

During the war years the C.R.D.A. completed two prototypes of the Z.511 commercial transport floatplane designed by Zappata before the war and intended far use on Alitalia’s South Atlantic route as the world’s largest floatplane. Construction of the Z.511 commenced in 1941 and the first prototype flew on 8th September 1943. The first prototype was destroyed when it struck a mine, and the second, commandeered by the Luftwaffe, was destroyed in Germany. The Z.511 was powered by four 1,500-h.p. Piaggio P.XII R.C.35 radials and had a loaded weight of 74,957 lb.