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 / ModelA1/B1/A2/B2A3/B3/Q1A4, Q4, Q5, Q6H2
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
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