Do 217 was a World War II medium bomber designed from scratch as a replacement for the venerable Do 17. Dornier recognized shortcomings of its fast Do 17 well before the war. With Junker’s new Ju 88 prototype being superior to the Do 17 in every way, Dornier decided to make a new bomber better than its Do 17, and its Junkers Ju 88 competition. The new aircraft was externally similar to the Do 17, but was in fact a completely different aircraft. It first flew in October 1938. The combat version flew in winter 1940/1941.

In almost every way, the Do 217 was a success. It could carry much higher bomb loads than both the Junkers Ju 88 and the Heinkel He 111. It was also very fast, matching the speed of the Junkers Ju 88. It was Germany’s largest bomber for nearly 2 years until the Heinkel He 177 was finally safe enough to use. Do 217’s sank the Italian battleship Roma with Fritz X missiles. However, the Do 217 had some quite serious flaws. It was at the limit in terms of size that a twin engined bomber could be with the engines available. Unlike its agile cousin Do 17, this aircraft was difficult to fly. Stability issues were always a problem, and it always seemed to lack powerful engines.

Like Do 17 and Ju 88, it was used in a variety of different variants and roles, including reconnaissance aircraft and night fighter.Production stopped in late 1943 in favour of fighters.

Type

• Twin-engined heavy bomber.

• Shoulder-wing cantilever monoplane with a three-section structure.
  • Center section incorporates a portion of the fuselage.
  • Two outer sections have semi-circular wing-tips.
  • Two-spar wing structure with girder truss ribs and solid plate ribs at stress points.
  • Smooth outer stress-bearing skin riveted to spars and ribs.
  • Slotted ailerons on outer sections.
  • Electrically-operated split flaps with a maximum angle of 55°.
  • Ailerons droop when flaps are lowered.
  • Leading edge of outer wing sections is double-skinned and heated by engine hot air.

• All-metal structure in three sections:
  • Nose section accommodating the crew.
  • Section integral with the wing center-section.
  • Rear fuselage.
• Main structure built with formers and stringers, riveted stressed skin.
• Center and rear fuselage sections divided horizontally.
• Lower half forms the bomb cell, upper half contains transverse bracing frames for bomb load support.

• Cantilever monoplane type with twin fins and rudders.
  • Tailplane and fins have two spars and are covered with metal skin.
  • Fins have fixed slats with trailing edges on the inside.
  • Rudders have narrow horn balances for mass-balancing and full-length trimming tabs.
  • Tailplane incidence changes automatically with landing flaps and can be manually adjusted.

• Retractable type with two oleo legs and a single wheel per unit.
• Electrically retracted rearwards into the engine nacelle.
• Electrically-operated, retractable tail wheel.

• Two Daimler-Benz DB 603 A twelve-cylinder inverted Vee liquid-cooled engines on welded steel-tube mountings.
• Coolant radiators beneath engines.
• Oil radiators in top cowling.
• Five fuel tanks (total capacity 230 + 175 + 175 + 44 + 44 + 35 + 35 Imp. gallons) and two oil tanks in wings.
• CO2 gas release in emergency.
• VDM three-bladed fully-feathering propellers with de-icing equipment.

• Crew of four housed in cabin forward of the wing:
  • Pilot on port side with a spectacle-type control column.
  • Bomb-aimer in the nose or seated beside the pilot.
  • Radio-operator behind the pilot.
  • Rear gunner aft.
• Cabin heating by exhaust-pipe muffs and hot-air sprays for transparent panels.
• Armored pilot’s seat and gun-turret sides.
• Armored recess for dinghy stowage in rear fuselage.

• One twin MG 81 (1,000 rounds) in the nose.
• One MG 131 (500 rounds) in dorsal turret.
• One MG 131 (1,000 rounds) in lower rear position.
• Two MG 81 (750 rounds per gun) in lateral positions.

• Main bomb cell: 14 ft. 10 in. long with a 5 ft. 8 in. extension for torpedo.
• Maximum load: 5,550 lbs. of various combinations of bombs, torpedo, or mines.
• Two 550-lb. bomb racks under wings, one outboard of each engine.
• Electrical fusing system for different bombing modes.
• Heating for bomb compartment when carrying torpedo.

• Span: 62 ft. 5 in. (19 m.)
• Length: 56 ft. 6 in. (17 m.)
• Gross wing area: 610 sq. ft. (56.6 sq. m.)
• Net wing area: 522 sq. ft. (48.5 sq. m.)

• 35,000 lbs. (15,890 kg.)

• Maximum speed at sea level: 290 mph (464 km/h).
• Maximum speed at 22,000 ft.: 330 mph (528 km/h).
• Service ceiling (fully loaded): 24,000 ft. (7,320 m.)
• Service ceiling (light): 27,000 ft. (8,235 m.)
• Range with maximum fuel: 2,400 miles (3,840 km.)