German single-engine STOL utility aircraft and first mass-produced aircraft in Germany following the end of the Second World War
https://en.wikipedia.org/wiki/Dornier_Do_27https://military-history.fandom.com/wiki/Dornier_Do_27https://backcountrypilot.org/forum/dornier-do27-20848https://plans.modelaircraft.org/product/dornier-do-27/General characteristics
Crew: 1
Capacity: 4 or 5 pax
Length: 10.08 m (33 ft 1 in)
Do 27H2 9.9 m (32 ft)
Do 27S 10.08 m (33.1 ft)
Wingspan: 12 m (39 ft 4 in)
Height: 4.18 m (13 ft 9 in)
Do 27S 4.18 m (13.7 ft)
Wing area: 19.4 m2 (209 sq ft)
Aspect ratio: 7.42:1
Airfoil: NACA 23018
Empty weight: 985 kg (2,172 lb)
Do 27Q3 1,010 kg (2,230 lb)
Do 27Q4 1,050 kg (2,310 lb)
Do 27S 1,275 kg (2,811 lb)
Gross weight: 1,570 kg (3,461 lb)
Do 27Q3 1,700 kg (3,700 lb)
Do 27Q4 1,850 kg (4,080 lb)
Do 27S 1,850 kg (4,080 lb)
Fuel capacity: 220 L (58 US gal; 48 imp gal) in two wing tanks, (Do 27Q4 provision for two 82 L (22 US gal; 18 imp gal) external tanks)
Powerplant: 1 × Lycoming GO-480-B1A6 6-cylinder air-cooled horizontally-opposed piston engines, 205 kW (275 hp)
Propellers: 2-bladed Hartzell metal constant-speed propeller, 2.48 m (8 ft 2 in) diameter
Performance
Maximum speed: 250 km/h (160 mph, 130 kn) at 1,000 m (3,300 ft)
Do 27H2 255 km/h (158 mph; 138 kn)
Do 27Q3 227 km/h (141 mph; 123 kn)
Do 27Q4 247 km/h (153 mph; 133 kn)
Do 27S 237 km/h (147 mph; 128 kn)
Cruise speed: 205 km/h (127 mph, 111 kn)
Stall speed: 58 km/h (36 mph, 31 kn)
Landing speed: 65 km/h (40 mph; 35 kn)
Range: 870 km (540 mi, 470 nmi)
Service ceiling: 5,500 m (18,000 ft)
Time to altitude:
1,000 m (3,300 ft) in 2 minute 36 seconds
2,000 m (6,600 ft) in 6 minute 30 seconds
3,000 m (9,800 ft) in 12 minute
4,500 m (14,800 ft) in 26 minute 30 seconds
Take-off run to 15 m (49 ft): 170 m (560 ft)
Landing run from 15 m (49 ft): 160 m (520 ft) in nil wind
Author
Topic: Dornier Do 27 (Read 430 times)
