Dornier Do 27
Country of Origin
Four to six seat STOL utility light aircraft
The Dornier Do 27 was the first military aircraft to be manufactured in quantity in what was West Germany since World War 2, and it was also built in limited numbers for civil customers. <p>The Do 27 traces back to the Do 25, which Professor Claude Dornier (Dornier was responsible for the Do 17 medium bomber in WW2) designed in Spain for a Spanish military requirement for a light general purpose utility aircraft. Two prototype Do 25s were built, the first was powered by a 110kW (150hp) ENMA Tigre GIVB engine and flew for the first time on June 25 1954. Subsequently CASA built 50 production aircraft as Do 27As for the Spanish air force (Spain designated the type C127). <p>Following this success the German military ordered the Do 27 in large numbers. Some 428 were delivered to Germany's armed forces from the mid 1950s to 1960, although these aircraft have since been retired. Small numbers were built for other military customers, and others for commercial use. <p>Features of the Do 27 design include a flat six Lycoming engine, a wide and relatively roomy cabin, wide track undercarriage and excellent STOL performance. The STOL performance in particular suited the Do 27 for use in undeveloped countries, and several have seen service in Africa and Papua New Guinea. <p>Do 27 models include the initial Do 27A and dual control Do 27B for Germany; the Do 27H series that was based on the A4 but with a more powerful engine and three blade prop; and the Do 27Q series, equivalent to the Do 27A. <p>
Do 27H2 - One 255kW (340hp) Lycoming GSO480B1B6 flat six piston engine driving a three blade Hartzell propeller. Do 27Q5 - One 200kW (270hp) GSO480B1A6 driving a two blade prop.
Do 27H2 - Max speed 245km/h (132kt), high speed cruise 212km/h (115kt), economical cruising speed 180km/h (97kt). Initial rate of climb 965ft/min. Service ceiling 22,000ft. Range with max fuel and no reserves 1360km (735nm). Do 27Q5 - Max speed 232km/h (125kt), 75% power cruising speed 211km/h (114kt), 60% power cruising speed 190km/h (103kt), economical cruising speed 175km/h (95kt). Initial rate of climb 650ft/min. Service ceiling 10,800ft. Range with max fuel and no reserves 1102km (595nm).
Do 27H2 - Empty equipped 1170kg (2580lb), max takeoff 1848kg (4070lb). Do 27Q5 - Empty equipped 1130kg (2490lb), max takeoff 1848kg (4070lb).
Do 27H2 & Q5 - Wing span 12.00m (39ft 5in), length 9.60m (31ft 6in), height 2.80m (9ft 2in). Wing area 19.4m2 (208.8sq ft).
Pilot and passenger side by side with between four and six passengers behind them. Can carry freight with rear seats removed.
Total Do 27 production of 577, including 195 Do 27A1s, 75 Do 27A3s, 54 A4s, 88 D1s, 18 B3s, one H1, 12 H2s, one Q3, 34 Q4s and one Q5.
Dornier Do 27
The backbone of this section is from the The International Directory of Civil Aircraft by Gerard Frawley and used with permission. To get your own copy of the book click here.