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Cessna C-106 Loadmaster

Posted on July 19, 2026 By

In 1943, the American aircraft manufacturer Cessna proactively developed the P-260 project, a light transport aircraft for the U.S. Army Air Forces. This project represented a modified version of the C/UC-78 transport, adapted for more powerful engines. The C-106 Loadmaster was designed with a tubular steel fuselage covered in fabric and semi-monocoque wooden wings, combining materials for a light yet sturdy structure.

For its powerplant, two air-cooled Pratt & Whitney R-1340 radial engines were chosen, each boasting 600 hp (450 kW) and fitted with two-bladed propellers. This configuration promised robust performance for the transport duties it was intended to undertake.

Table of Contents

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    • Successful Trials and Production Prospects
    • A Promising Project Thwarted
    • Technical Specifications
  • Image and diagram gallery of the Cessna C-106 Loadmaster
    • How to cite this article:

Successful Trials and Production Prospects

During 1943, two prototypes were built for evaluation tests: the C-160 (NX24176) with R-1340-S3H1 engines and the C-160A (NX44600) with R-1340-AN-2. These prototypes underwent rigorous military trials, where the aircraft received very positive reviews for its performance and reliability.

Due to its successful results, the C-106 Loadmaster was recommended for series production. Towards the end of 1943, a preliminary contract was signed for the manufacture of 500 units, indicating great confidence in Cessna’s design.

A Promising Project Thwarted

Despite the initial enthusiasm and the substantial order, a shortage of plywood, an essential material for its construction, prevented Cessna from commencing mass production. This factor, common during the war years, ultimately thwarted the widespread deployment of a highly promising light transport aircraft capable of handling up to 1100 kg of cargo.

Technical Specifications

Modification C-106
Wingspan, m 19.71
Length, m 15.57
Height, m 3.73
Empty weight 4445
Normal takeoff weight 6713
Engine type 2 Piston engines Pratt & Whitney R-1340
Power, hp 2 x 600
Maximum speed, km/h 314
Cruising speed, km/h 274
Practical range, km 1200
Crew, crew members 4
Payload: 1100 kg of cargo

Image and diagram gallery of the Cessna C-106 Loadmaster

C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster
C-106 Loadmaster

How to cite this article:

APA: Cessna C-106 Loadmaster (). Cessna C-106 Loadmaster. wp.archivoaereo.com. https://wp.archivoaereo.com/en/cessna-c-106-loadmaster-3/
VANCOUVER: Cessna C-106 Loadmaster [online]. wp.archivoaereo.com; [cited 2026-07-20]. Available at: https://wp.archivoaereo.com/en/cessna-c-106-loadmaster-3/
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WWII Military Transport Tags:American, Cessna

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