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 |