Do 17 Z-2

Do 17 Z-2

Modification of
Do 17 Z
Changes
Main production model with the Bramo 323 P-1 tuned for low altitude, 1,000 kg bomb load, six MG 15; from May 1940 422 Z-2 flew with KG 2, KG 3, KG 76 and KG 77 (en).
Crew
4
Length
15,800 mm
Wingspan
18,000 mm
Wing area
53.3 m²
Empty weight
5,210 kg
Normal takeoff weight
8,600 kg
Max takeoff weight
8,837 kg
Internal fuel
1,540 L
Engine
Bramo 323 P Fafnir
Engines
2
Blades
3
Max speed
410 km/h
Max speed altitude
5,000 m
Service ceiling
8,200 m

Armament

WeaponCountPosition
MG 156Flexible

Loadouts

NameChanges
1,000 kg1,000 kg internally: 20 × 50 kg or 4 × 250 kg bombs.

Service

≈ 10 May 1940 – Oct 1940