119:, the mains connect to the engine mount. The wing tanks feed a 5.75 imperial gallons (26.1 L; 6.91 US gal) header tank through automotive electric fuel pumps. The header tank feeds the engine by gravity.
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The prototype first flew in 1976. The
Hirondelle is built primarily of wood and cloth. It is a low-wing cantilever monoplane with a fixed tail-wheel landing gear and seats two side-by-side. It was designed for the
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The prototype weight includes an upholstered interior, a full electrical system and venturi driven gyros. With its 108 hp (81 kW) engine it can cruise at 135 mph (217 km/h) at 2500 rpm.
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The primary wing structure is a wood box spar connected to an aileron spar by ribs cut on a band saw. To the front of the main spar are strapped D-shaped fiberglass fuel tanks which can carry up to 12
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with a 55 in (140 cm) chord; the wing is rectangular, being straight and untapered. No flaps were fitted to the prototype, but they were being considered.
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The fuselage is built up from spruce and covered in 3 mm (0.12 in) plywood. Cabin width on the prototype was 38 in (97 cm). The main gear uses
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per wing. Over the tanks is the framing and plywood skin of the wing's nose. Behind the main spar, the wings are covered in cloth. The wing section is the
76:) is a Canadian two-seat aircraft for cross country and recreational flying, designed by Western Aircraft Supplies to be
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tapered rods and was designed to take standard Cessna wheel pants. As with the
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Western
Aircraft Supplies PGK-1 Hirondelle specifications, image and video
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but accommodates engines from 100 to 160 hp (75 to 119 kW).
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Aircraft of comparable role, configuration, and era
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317:Movie from a group of French PGK-1 builders
203:145 mph (232 km/h, 126 kn)
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80:from plans. The name is French for the
215:12.3 lb/sq ft (60 kg/m)
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272:Cox, Jack, "The PGK-1 Hirondelle,"
154:26 ft 0 in (7.93 m)
148:20 ft 6 in (6.25 m)
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160:7 ft 6 in (2.29 m)
266:Jane's Encyclopedia of Aviation
166:120 sq ft (11 m)
264:Taylor, Michael J. H. (1989).
209:800 ft/min (4.1 m/s)
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251:McLeod Cavalier SA102 series
178:1,475 lb (669 kg)
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268:. London: Studio Editions.
188:, 108 hp (81 kW)
172:933 lb (423 kg)
54:Western Aircraft Supplies
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236:SAN Jodel D.150 Mascaret
74:Western PGK-1 Hirondelle
276:1978-01, pp. 23–25
231:Jodel DR1050 Excellence
133:General characteristics
332:Homebuilt aircraft
72:(specifically the
70:Western Hirondelle
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117:Wittman Tailwind
102:imperial gallons
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32:Type of aircraft
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194:Performance
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88:Description
19:Hirondelle
258:References
164:Wing area:
106:NACA 23012
152:Wingspan:
78:homebuilt
30:monoplane
28:Homebuilt
326:Category
220:See also
158:Height:
146:Length:
113:Wittman
82:Swallow
44:Canada
281:Notes
140:Crew:
63:1976
24:Role
184:1 ×
298:Cox
328::
289:^
248:A
142:2
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