Technical Data Dornier Do27

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 Dornier Do27-

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
128,0
128,0
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 29,0) (2 x 29,0) (2 x 29,0) (2 x 29,0)
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 19,0) (2 x 19,0) (2 x 19,0) (2 x 19,0)
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)