Turbine DC-3s

[rigpiggy]

Look at the Penturbo.com -67 DHC-4 re-engine.

WEIGHTS
Design Take-off Weight

28,500 lbs.

Design Landing Weight

28,500 lbs.

Maximum Zero Fuel Weight

27,000 lbs.

Maximum Payload

10,000 lbs.

Maximum Fuel
(Internal Tanks)

5540 lbs

PERFORMANCE SUMMARY

The following is a summary of the performance data that applies under ISA conditions at the design gross weight of 28,500 lbs. Takeoff and landing distances are given at sea level, zero wind, and from a dry level surface.

TAKE-OFF AND LANDING: SHORT FIELD TECHNIQUE (STOL)
Aircraft Operating Data – PART 8 Charts



Take-off (flaps 25º, both engines at T.O. power)


Ground Run

800 ft

Total distance to clear 50-ft. obstacle

1300 ft

Landing (Flaps 40º)

Ground Run

425 ft

Total distance from 50-ft. obstacle

945 ft

TAKE-OFF AND LANDING: AIRLINE TECHNIQUE (FAR 25)
Take-off (flaps 7º engines at T.O. power)
Ground Run

1630 ft

Total distance to 35-ft obstacle

2550 ft

Take-off (Flaps 7º)
One engine inop. at V1 to 35-ft obstacle

3955 ft

Landing (Flaps 30º)
Ground Run

1100 ft

Total Distance from 35-ft. obstacle

2250 ft