Spartan SP-21M/IMPA SI-21S
A floatplane equipped Sp-21 variant initially for the Commando de Aviacion Naval for the reconnaissance role with a secondary attack role.
Dimensions: span 20.42m; length 12.19; height 3.84m; wing area 600sq ft; wing loading 31.33 lb/sq ft; power loading 0.234kg/hp 0.10 lb/hp
Structure: all-metal monocoque fuselage in four sections with Z section fames and L section stringers with light alloy covering, light alloy used for tail construction and cantilever tailplane covering. Cantilever all-metal wing with two steel spars, all-metal split flaps and aluminium framed ailerons with fabric covering. Rudder and elevators aluminium framed with fabric covering. Two amphibious watertight floats fixed underwing with optional beaching wheels.
Weights: empty 11,670lbs, maximum take-off 18,800lbs Powerplant: two 1000hp Spartan 1000 supercharged radial engines
Performance: max speed 248mph; service ceiling 25,500ft; rate of climb 1,025ft per minute at 1,500ft; range 957 miles with 3,000lbs bomb load
Capacity: pilot in enclosed cockpit, navigator in rear fuselage cabin with one window and one access door ahead of radio operator/gunner in a hydraulic-powered dorsal turret
Armament: one dorsal turret with two 7.92mm FMG/M32 MG (drum feed), four fixed 13mm Browning HMG in the lower nose under the cockpit, bombload 3000lbs in one lower fuselage bomb bay or one semi-recessed 18-21in torpedo
Equipment: full controls and navigation equipment including receiver/transmitter, HF/DF set, naval co-operation beacon, Sperry autopilot, reflector gun sight with torpedo aiming bar, two cameras fitted in navigators cabin floor, three flare chutes and two rescue dinghies.