de Havilland DH.18

DH.18
DH.18
	DH.18B
General information
Type	Airliner
Manufacturer	Airco
Designer	Geoffrey de Havilland
Primary users	Aircraft Transport and Travel Daimler Hire Ltd; Instone Air Line
Number built	6
History
Manufactured	1919–1921
Introduction date	1920
First flight	8 April 1920
Retired	1923

The de Havilland DH.18 was a single-engined British biplane transport aircraft of the 1920s built by de Havilland.

Design and development

The DH.18 was designed and built in 1919 by Airco as their first aircraft specifically for commercial work, earlier aircraft such as the DH.16 being modified military types. The DH.18 was a single-engined biplane, powered by a Napier Lion engine with wooden two-bay, wire-braced wings, and a forward fuselage clad in plywood. It accommodated eight passengers in an enclosed cabin with the pilot in an open cockpit behind the cabin. The first prototype flew early in 1920.^[1]

DH.18A G-EARO of Instone Air Lines

Operational history

The first DH.18 was delivered to Aircraft Transport and Travel for use on the Croydon-Paris service, but was wrecked in a forced landing shortly after takeoff from Croydon on 16 August 1920.^[2] Two more aircraft were under construction by Airco for Aircraft Transport and Travel when the bankrupt Airco was purchased by BSA, who did not wish to continue aircraft development or production. Geoffrey de Havilland, the chief designer of Airco then set up the de Havilland Aircraft Company, completing the two partly completed aircraft as DH.18As, with improved engine mountings and undercarriages.

Aircraft Transport and Travel closed down in early 1921, due to competition from subsidised French airlines. In March 1921, the British government granted temporary subsidies for airline services,^[3] with the Air Council purchasing a number of modern commercial aircraft for leasing to approved firms.^[2] The three ex-A.T.&T. DH.18s were purchased in this way and leased to Instone Air Line. A further DH.18A was built to Air Council order, as were two modified DH.18B, which had fuselages that were entirely plywood-clad and had built-in emergency exits.^[2]

The DH.18s were kept busy flying on continental air services for Instone, building up high flying hours. One aircraft, G-EAWO, was transferred to Daimler Airway for operation on the Croydon-Paris route until the de Havilland DH.34s which it had on order could be delivered. However, on 4 April 1922, two days after Daimler commenced operations with the aircraft, it collided with a Farman Goliath over Northern France,^[2] 62 mi (100 km) north of Paris, killing seven people, the first midair collision between airliners.^[4]

The DH.18 was retired from commercial service in 1923, with one aircraft, G-EARO, having flown 90,000 mi (144,834 km) without accident.^[2] Two aircraft were used for test purposes, with one the subject of an Air Ministry experiment on how long an aircraft could stay afloat after being ditched, being deliberately landed on water off Felixstowe on 2 May 1924, floating for 25 minutes.^[2] The other remaining aircraft was used for test purposes at RAE Farnborough until 1927, when it was scrapped.^[1]

Variants

DH.18: Prototype – registered G-EARI.
DH.18A: Initial production version – modified undercarriages and engine mountings. Three built – (G-EARO, G-EAUF, G-EAWO).
DH.18B: Plywood-covered fuselage and increased weights. Two built – (G-EAWW and G-EAWX).

Operators

United Kingdom

Netherlands

KLM (Leased)

Specifications (DH.18A)

De Havilland DH.18 3-view drawing from Flight, 24 March 1921

Data from British Civil Aircraft since 1919, Volume 2^[2]

General characteristics

Crew: One
Capacity: 8 passengers
Length: 39 ft 0 in (11.89 m)
Wingspan: 51 ft 3 in (15.62 m)
Height: 13 ft (4.0 m)
Wing area: 621 sq ft (57.7 m²)
Empty weight: 4,040 lb (1,833 kg)
Gross weight: 6,516 lb (2,956 kg)
Powerplant: 1 × Napier Lion 12-cylinder water-cooled W-block aircraft piston engine, 450 hp (340 kW)
Propellers: 2-bladed wood fixed pitch propeller

Performance

Maximum speed: 125 mph (201 km/h, 109 kn)
Cruise speed: 100 mph (160 km/h, 87 kn)
Range: 400 mi (640 km, 350 nmi)
Service ceiling: 16,000 ft (4,900 m)
Rate of climb: 660 ft/min (3.4 m/s)

References

^ ^a ^b Donald, David, ed. The Encyclopedia of World Aircraft (London: Aerospace Publishing, 1997), p.311-312.
^ ^a ^b ^c ^d ^e ^f ^g Jackson, A.J. British Civil Aircraft since 1919 Volume 2. London: Putnam, 1973. ISBN 0-370-10010-7 pp. 64–66.
^ "British Airways Museum Collection 1920–30". Archived from the original on 27 December 2008. Retrieved 17 June 2007.
^ "Review of ACAS RA Downlink, An assessment of the technical feasibility and operational usefulness of providing ACAS RA awareness on CWP" (PDF). p. 20. Archived from the original on 27 September 2007. Retrieved 17 June 2007.{{cite web}}: CS1 maint: unfit URL (link)

External links

"The D.H. 18 Limousine". Flight. XIII (12): 203–206. 24 March 1921. No. 639. Contemporary technical description with drawings and photographs.

[world_aircraft-1] Donald, David, ed. The Encyclopedia of World Aircraft (London: Aerospace Publishing, 1997), p.311-312.

[jacksonv2-2] ^ ^a ^b ^c ^d ^e ^f ^g Jackson, A.J. British Civil Aircraft since 1919 Volume 2. London: Putnam, 1973. ISBN 0-370-10010-7 pp. 64–66.

[3] "British Airways Museum Collection 1920–30". Archived from the original on 27 December 2008. Retrieved 17 June 2007.

[4] "Review of ACAS RA Downlink, An assessment of the technical feasibility and operational usefulness of providing ACAS RA awareness on CWP" (PDF). p. 20. Archived from the original on 27 September 2007. Retrieved 17 June 2007.{{cite web}}: CS1 maint: unfit URL (link)

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