The Watanabe Ironworks 
         Company was responsible for the design of a crew trainer to meet the 
         requirements of the Imperial Japanese Navy, but by the time that the 
         trainer was ordered into production this manufacturer had been 
         reorganised as the Kyushu Aeroplane Company, explaining the designation 
         of this aircraft as the Kyushu K11W. A mid-wing cantilever monoplane 
         with retractable tailwheel landing gear, the K11W had a deep-section 
         fuselage to provide the requisite accommodation for a complete bomber 
         crew and an instructor. This was arranged with the pilot and 
         radio-operator/gunner in a canopied cockpit above the wing, and with 
         the instructor, bomb-aimer and navigator in a cabin below the wing. 
         Power was provided by a 515 hp (384 kW) Hitachi GK2B Amakaze 21 
         (heavenly wing) 9-cylinder radial engine. 
         
           
         A Kyushu K11W Shiragiku of the Imperial Japanese Navy 
         The K11W1 prototype was 
         first flown during November 1942, its early testing and service trials 
         being completed quite quickly because only minor faults were found. 
         Ordered into production as the Navy Operations Trainer Shiragiku (white 
         chrysanthemum). Designed as an economical successor to the obsolete 
         Mitsubishi K3M series, the first examples began to enter service in the 
         summer of 1943, these carrying a rear-firing 7.7 mm (0.303 in) Type 92 
         machine-gun and two 66 lbs (30 kg) bombs for armament training. Used 
         extensively by the navy, almost 800 had been built by August 1945, this 
         total including a small number of an alternative version of all-wood 
         construction which, designated K11W2, was built to fulfil ASW and 
         transport roles. Like many Japanese aircraft, K11Ws were pressed into 
         service for kamikaze attacks during the final stages of the war 
         carrying a single 511 lbs (250 kg) bomb. The aircraft was nothing if 
         not obscure and thus never was given an Allied code name, it is only 
         superficially described even in Japanese-published references. 
         Variants 
         Kyushu K11W Shiragiku - 
         The main production type with all-metal construction and fabric-covered 
         control surfaces. 798 were built. 
         Kyushu K11W2 Shiragiku 
         - Similar to the above but of all-wood construction and built primarily 
         to fufil ASW and Transport roles. Only a small number were built.  
         (Navy Operations 
         Trainer Shiragiku "White Chrysanthemum" - Kyushi K11W) 
         Allied Codename: 
         None  
         Type: Five Seat 
         Advanced Bomber Crew Trainer  
         Accommodation/Crew: 
         Pilot and radio-operator/gunner in canopied cockpit above the wing with 
         the instructor, bomb-aimer and navigator in a cabin below the wing. 
         Design: Watanabe 
         Tekkosho KK Design Team  
         Manufacturer: 
         Watanabe Tekkosho Kabushiki Kaisha (Watanabe Iron Works Limited) in 
         Zatsushonokuma, Fukoaka, Japan. In 1942 the company was re-organised 
         and renamed Kyushu Hikoki Kabushiki Kaisha. 
         Powerplant: One 
         Hitachi GK2B Amakaze 21 9-cylinder radial piston engine rated at 515 hp 
         (384 kW) for take-off and 480 hp (358 kW) at 4,921 ft (1500 m) driving 
         a two-bladed metal propeller. 
         Performance: 
         Maximum level speed 143 mph (230 km/h) at 5,580 ft (1700 m); cruising 
         speed 109 mph (175 km/h) at 3,280 ft (1000 m); service ceiling 18,400 
         ft (5620 m); climb to 9,842 ft (3000 m) in 19 minutes 35 seconds. 
         Range: 1,094 
         miles (1760 km) on internal fuel. 
         Weight: Empty 
         3,697 lbs (1677 kg) with a normal take-off weight of 5,821 lbs (2,640 
         kg) and a maximum take-off weight of 6,173 lbs (2800 kg). Wing loading 
         of 17.85 lbs/sq ft (86.6 kg/sq m); Power loading 11.2 lbs/hp (5.1 
         kg/hp). 
         Dimensions: Span 
         49 ft 1 3/4 in (14.98 m); length 33 ft 7 1/4 in (10.24 m); height 12 ft 
         10 3/4 in (3.93 m); wing area 328.31 sq ft (30.50 sq m). 
         Armament: One 
         rear firing 7.7 mm (0.303 in) Type 92 machine-gun on a flexible mount 
         plus two 66 lbs (30 kg) bombs when required for training purposes. When 
         used in the kamikaze role a single 551 lbs (250 kg) bomb was 
         used. 
         Variants: K11W1 
         (prototype), K11W (trainer), K11W2 (ASW & transport). 
         Equipment/Avionics:
         Standard communications and navigation equipment. 
         History: First 
         flight (prototype) November 1942. 
         Operators: Japan 
         (Imperial Japanese Navy).  |