Бурундук de Havilland Canada DHC-1 - Фото и видео

de Havilland Canada DHC-1 Chipmunk
Страны	Великобритания + Канада
Роль	Тренерский самолет
Первый полет	22 мая 1946 г.
Построен	1284

Teh де Хэвилленд Канада DHC-1 Бурундук — тандемный двухместный одномоторный учебно-тренировочный самолёт, спроектированный и разработанный канадской авиастроительной компанией de Havilland Canada. Он был разработан вскоре после Второй мировой войны и продавался в больших количествах в течение первых послевоенных лет, обычно использовался в качестве замены биплана de Havilland Tiger Moth.

Источник: де Хэвилленд Канада DHC-1 Бурундук в Википедии

DHC-1 Chipmunk Walk Around
Photographer	Josef Mezera
Localisation	Unkonw
Photos	45

de Havilland DHC-1 Chipmunk 1

de Havilland DHC-1 Chipmunk 2

de Havilland DHC-1 Chipmunk 3

de Havilland DHC-1 Chipmunk 4

de Havilland DHC-1 Chipmunk 5

de Havilland DHC-1 Chipmunk 6

de Havilland DHC-1 Chipmunk 7

de Havilland DHC-1 Chipmunk 8

de Havilland DHC-1 Chipmunk 9

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De Havilland Canada DHC-1 ‘Chipmunk’ T.10 Walk Around
Photographer	Ondrej Skarka
Localisation	Unkonw
Photos	12

General Characteristics

The de Havilland Canada DHC-1 Chipmunk (often nicknamed “Chippie”) is a tandem two-seat, single-engine primary trainer aircraft. It was the first aircraft designed and built by de Havilland Canada and was intended to replace the venerable **de Havilland Tiger Moth** biplane. The Chipmunk served as the standard basic trainer for the Royal Air Force (RAF), Royal Canadian Air Force (RCAF), and many other air forces from the late 1940s well into the 1990s.

Property	Typical Value (T.Mk 10 Variant)
Роль	Primary Trainer / Aerobatic / Liaison
Производителя	de Havilland Canada (DHC), de Havilland UK, OGMA (Portugal)
First Flight	May 22, 1946
No. Built	1,284 (Total production)
Экипажа	2 (Student and Instructor in tandem)
Длина	7.75 m (25 ft 5 in)
Размах крыла	10.47 m (34 ft 4 in)
Max Takeoff Weight	953 kg (2,100 lb)

Design and Powerplant

Engine: One de Havilland Gipsy Major 8 or 10-2 4-cylinder, air-cooled, inverted in-line piston engine.
Power Output: 108 kW (145 hp).
Construction: Predominantly all-metal fuselage and wings (stress-skinned alloy) with the control surfaces and the rear portion of the wings being fabric-covered.
Configuration: Low-wing cantilever monoplane with a fixed conventional tailwheel landing gear. The cockpit features a clear perspex canopy providing excellent all-round visibility.
Handling: Known for its delightful and responsive handling, making it an excellent platform for learning basic flight, instrument flying, and aerobatics.

Performance and Service

Maximum Speed: Up to 222 km/h (138 mph, 120 knots) at sea level.
Cruise Speed: Approximately 166 km/h (103 mph, 90 knots).
Service Ceiling: 4,800 m (15,800 ft).
Range: Approximately 417 km (259 mi, 225 nmi).
Rate of Climb: 4.6 m/s (900 ft/min).
Major Variants:
- Chipmunk T.Mk 10 (British-built for RAF, standard enclosed canopy).
- DHC-1B-2 (Canadian-built, often featuring a larger “bubble” canopy).
- Chipmunk Mk 23 (Agricultural/crop-spraying variant).
Civilian Use: Hundreds of ex-military Chipmunks remain popular today with private owners for sport flying and aerobatics.