Type G-0 G-3 G-5
Engine 1 BMW VI 6.0 ZU 1 BMW 132H 1 DB 601Aa
Dimensions Length 17,30 m , height 4,20 m ,  span 22,50 m , wing area 87,60 m2 , Length 17,20 m , height 4,10 m ,  span 22,60 m , wing area 87,60 m2 Length 17,10 m , height 4,10 m ,  span 22,60 m , wing area 87,60 m2
Weights Empty , loaded  8020 kg, max. take off weight   Empty , loaded  8460 kg, max. take off weight   Empty , loaded  8820 kg, max. take off weight  
Performance Max.. speed 315 km/h , cruising speed  270 km/h, range 1000 km, endurance  , service ceiling 4200 m  , climb Max.. speed 345 km/h , cruising speed  300 km/h, range 1500 km, endurance  , service ceiling 8390 m  , climb Max.. speed 415 km/h , cruising speed  275 km/h, range 1500 km, endurance  , service ceiling 6000 m  , climb
Type Werk.Nr Registration History
G-01 2534 D-AEQA "Halle" Lufthansa
G-02 2535 D-AYKI ".Magdeburg" Lufthansa
G-3 Also known as He 111L
G-3 Also known as He 111L
G-4
G-4
G-4
G-4
G-4
G-5 Delivered to Turkey
G-5 Delivered to Turkey
G-5 Delivered to Turkey
G-5 Delivered to Turkey
The He 111G represented a final attempt to sell the He 111 as a commercial airliner. It used a straight edged wing, similar to that adopted on later military He 111s, making it easier to produce that the curved wing of the He 111C. Two prototype aircraft, powered by the 660hp BMW VI 6.0 engine were produced during 1937 (G-01 and G-02), and were used by Lufthansa, as were two He 111G-3s produced using more powerful BMW engines.

Five He 111G-4s were built using 900hp Daimler-Benz DB 600G engines, with one being used by the deputy commander of the Luftwaffe, Field Marshal Erhard Milch. Finally four He 111G-5s powered by DB 700Ga engines were produced and sold to Turkey in 1938. Those He 111Gs remaining in private hands in Germany at the start of the Second World War were impressed into the Luftwaffe.