{"product_id":"cant-z-1007-alcione-manuals-collection","title":"CANT Z.1007 Alcione Manuals Collection","description":"\u003ch2\u003eCANT Z.1007 Alcione: Technical Manual Collection\u003c\/h2\u003e\u003cp\u003eA historical technical library for the CANT Z.1007 Alcione (Kingfisher), the prominent all-wood three-engine medium bomber designed by Filippo Zappata for CRDA \/ CANT and operated by Italy’s Regia Aeronautica during the Second World War.\u003c\/p\u003e\u003cp\u003eThis collection brings together airframe, engine and propeller documentation for the Z.1007 Bis, plus an Isotta Fraschini Asso XI engine manual for the earlier Z.1007 configuration.\u003c\/p\u003e\u003ch3\u003eCollection contents\u003c\/h3\u003e\u003ch4\u003eZ.1007 Bis variant, 8 manuals\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eZ.1007 Bis Operating and Maintenance\u003c\/li\u003e\n\u003cli\u003eZ.1007 Bis Series I Instructions and Regulations for Aircraft Assembly and Adjustment, 1940, Italian language\u003c\/li\u003e\n\u003cli\u003eZ.1007 Bis Series IV Instructions and Regulations for Aircraft Assembly and Adjustment, 1941, Italian language\u003c\/li\u003e\n\u003cli\u003eZ.1007 Bis Series VII Instructions and Regulations for Aircraft Assembly and Adjustment, 1941, Italian language\u003c\/li\u003e\n\u003cli\u003ePiaggio P.XI Aircraft Engine, Operating Instructions, 1938, Italian language\u003c\/li\u003e\n\u003cli\u003ePiaggio P.XI Bis RC40D Aircraft Engine, Illustrated Parts Catalogue, 1941, Volume 3, Italian language\u003c\/li\u003e\n\u003cli\u003ePiaggio P.1001 Variable-Pitch Propeller, Instructions for Use, 1940, Italian language\u003c\/li\u003e\n\u003cli\u003ePiaggio P.1001 Variable-Pitch Propeller, Illustrated Parts Catalogue, Italian language\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eEarlier Z.1007 engine, 1 manual\u003c\/h4\u003e\u003cul\u003e\u003cli\u003eIsotta Fraschini Asso XI R.2 C.15 D Aircraft Engine, Operating Instructions, 1937, Italian language\u003c\/li\u003e\u003c\/ul\u003e\u003ch3\u003eTechnical overview\u003c\/h3\u003e\u003cp\u003eThis document compiles historical engineering reports, technical notes and flight data sheets detailing the Alcione’s development and operational profile.\u003c\/p\u003e\u003ch4\u003eAerodynamic reports and fuselage geometry\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eElliptical profile:\u003c\/strong\u003e Zappata designed an exceptionally clean, elliptical fuselage cross-section intended to minimize parasitic drag and support efficient cruise performance.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAerodynamic cleanliness and environmental degradation:\u003c\/strong\u003e The smooth plywood skinning originally provided a low coefficient of drag. In harsh climates such as North Africa and the Eastern Front, cracks, separations and surface delamination could severely deform the lifting surfaces and increase drag.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTandem seating:\u003c\/strong\u003e To preserve the narrow aerodynamic fuselage line, the two pilots sat in tandem rather than side by side.\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eEngine technical notes and powerplant evolution\u003c\/h4\u003e\u003cp\u003eThe aircraft’s powerplants changed in response to power-to-weight requirements, moving from inline engines to more powerful radials:\u003c\/p\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003ePrototype and early series\u003c\/th\u003e\n\u003cth\u003eDefinitive Z.1007bis\u003c\/th\u003e\n\u003cth\u003eFinal Z.1007ter\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eEngine model\u003c\/td\u003e\n\u003ctd\u003e3 × Isotta Fraschini Asso XI R.C.40\u003c\/td\u003e\n\u003ctd\u003e3 × Piaggio P.XI R.C.40, 14-cylinder radials\u003c\/td\u003e\n\u003ctd\u003e3 × Piaggio P.XIX Turbine\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOutput per engine\u003c\/td\u003e\n\u003ctd\u003eApproximately 830–840 hp\u003c\/td\u003e\n\u003ctd\u003e1,000 hp\u003c\/td\u003e\n\u003ctd\u003e1,180 hp\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePowerplant notes\u003c\/td\u003e\n\u003ctd\u003eInline engines, judged significantly underpowered for military payload demands\u003c\/td\u003e\n\u003ctd\u003eRadial switch improved reliability, although the weight of the third engine partially offset the gains\u003c\/td\u003e\n\u003ctd\u003eLate-war stopgap reported to have achieved 500 km\/h in testing\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch4\u003eHandling, stability and control studies\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eLongitudinal instability:\u003c\/strong\u003e Initial testing of the single-fin configuration identified significant longitudinal stability deficiencies. A major aerodynamic redesign resulted in a twin-tail, or dual-fin, arrangement for later production blocks to stabilize pitch and yaw coupling.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePilot consensus:\u003c\/strong\u003e When well maintained, the Alcione was regarded as having forgiving, light control response and high lateral stability, making it suitable for long-range over-water sorties.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAsymmetric thrust control:\u003c\/strong\u003e The trimotor configuration offered survivability if one engine was neutralized, allowing the aircraft to maintain altitude and return on the remaining two engines.\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePerformance data, Z.1007bis\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eMaximum speed: 465 km\/h (289 mph) at altitude\u003c\/li\u003e\n\u003cli\u003eCruising speed: 380 km\/h (236 mph)\u003c\/li\u003e\n\u003cli\u003eService ceiling: 8,200 m (26,900 ft)\u003c\/li\u003e\n\u003cli\u003eMaximum range: 1,750 km to 2,800 km, depending heavily on external bomb load\u003c\/li\u003e\n\u003cli\u003eEmpty weight: 9,396 kg\u003c\/li\u003e\n\u003cli\u003eMaximum loaded weight: 13,620 kg\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eEngineering and maintenance bulletins\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eClimatic structural vulnerability:\u003c\/strong\u003e Technical updates highlighted degradation of organic glues and wooden structures under extreme heat or moisture. Regular inspection of spar joints for delamination was mandatory.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eArmor modification:\u003c\/strong\u003e Later modifications integrated defensive armor, including a 0.76 m × 1.1 m plate for the dorsal gunner and 5 mm to 6 mm plates around the side and ventral gunner stations to offset the vulnerability of the wooden skin.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBuoyancy advantage:\u003c\/strong\u003e Emergency handling bulletins noted that the hollow, all-wooden structure could act as a natural flotation device, allowing the airframe to float for extended periods during maritime ditching maneuvers.\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003e\u003cstrong\u003eImportant:\u003c\/strong\u003e This is historical and reference material, not current approved airworthiness data, maintenance approval or operational guidance. Verify provenance, document-level rights and intended use before relying on or distributing the material.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53969632002395,"sku":null,"price":100.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/cant-z-1007-alcione-banner-using-the-online-aviation-library-logo.png?v=1788515309","url":"https:\/\/onlineaviationlibrary.com\/products\/cant-z-1007-alcione-manuals-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}