CAMS 32R

The CAMS 32R flying boat was developed by Rafaele Conflenti, a designer from Chantiers Aeromaritimes de la Seine (CAMS). It was built to a Navy specification for a two-seat reconnaissance flying boat, featuring folding wings for shipboard deployment.

Development and First Flight

Construction of the sole prototype was completed during the winter of 1923-1924. Its inaugural flight took place on March 28, 1924, originating from the River Seine.

Naval Competition and Outcome

Following factory trials, the CAMS 32R was delivered to the Saint-Raphael research center to compete against two other contenders for a Navy contract. The competition was ultimately unsuccessful for all participants, leading the military to abandon this specific requirement.

Technical Specifications

Modification	CAMS 32R
Wingspan, m	12.40
Length, m	9.38
Height, m	3.06
Wing area, m2	43.00
Empty weight	999
Maximum takeoff weight	1500
Engine type	1 Piston engine Hispano-Suiza 8 Ac
Power, hp	1 x 180
Maximum speed, km/h	160
Cruising speed, km/h	140
Practical range, km	300
Crew	2

Image and diagram gallery of the CAMS 32R

CAMS 32	CAMS 32
CAMS 32