Technical Data Dornier Do 27

All Data shown are for information only. There is no guarantee for entity and correctness. In doubts the data of the current flightmanuals are valid.

Type / Model A1/B1/A2/B2 A3/B3/Q1 A4, Q4, Q5, Q6 H2 Empty weight (lbs) ~ 2200 ~ 2200 ~ 2500 ~ 2500 Max. Takeoff-Weight (lbs) 3460 3750 / 3860 4080 4080 Length (meters) 9,60 9,60 9,60 9,90 Wingspan (meters) 12,00 12,00 12,00 12,00 Height (meters) 3,50 3,50 3,50 3,50 Wingarea (sqm) 19,40 19,40 19,40 19,40 Horizontal Fin Area (sqm) 4,00 4,00 4,00 4,00 Vertical Fin Area (sqm) 2,56 2,56 2,56 3,06 Cabinheight (meters) 1,40 1,40 1,40 1,40 Cabinwidth (meters) 1,30 1,30 1,30 1,30 Cabinlength (meters) 3,50 3,50 3,50 3,50 Seats 6 6 6 6 Landinggeartrack (width) 2,28 2,28 2,74 (2,31) 2,74 (2,31) Shockstrutpressure (psi) 99,6 99,6 128 128 Wheelsize (inches) 8,50 x 6 8,50 x 6 8,50 x 10 8,50 x 10 Wheelweight (kg) 12,3 12,3 15,0 15,0 Speeds (kts IAS)
Vne (never exceed) 180 180 180 180 Vno (normal operating) 130 130 130 130 Va (manoeuvering speed) 90 90 90 90 Vfe (flaps ext. 15 deg.) 75 75 75 75 Vs (idle,flaps 15) < 40 < 40 < 40 < 40 Engine Lycoming GO480 B1A6 GO480 B1A6 GO480 B1A6 GSO480 B1B6 hp 270 270 270 340 Max. RPM 3400 3400 3400 3400 Climb RPM 3000 3000 3000 3200 Cruise 2750 2750 2750 2850 Econ. Cruise 2600 2600 2600 2650 Propeller: Hartzell HC-82-V-20 or HC-A2-V-20 HC-93-Z20 Blades 2 2 2 3 Diameter 2,49 2,49 2,49 2,36 Fuelquantity Standard
Total fuelcapacity (US gal) 2 x 29 2 x 29 2 x 29 2 x 29 Total useable fuel 2 x 27,2 2 x 27,2 2 x 27,2 2 x 27,2 Unusable 2 x 1,8 2 x 1,8 2 x 1,8 2 x 1,8 Auxiliarytanks option option standard Q4, Q5 option Total fuelcapacity (US gal) 2 x 19 2 x 19 2 x 19 2 x 19 Total useable fuel 2 x 17,2 2 x 17,2 2 x 17,2 2 x 17,2 Unusable 2 x 1,8 2 x 1,8 2 x 1,8 2 x 1,8