{"product_id":"fiat-as1-light-trainer-technical-manuals-collection","title":"Fiat AS.1 — Light Trainer Technical Manuals Collection","description":"\u003cp\u003eThis Living Collection brings together primary-source technical documentation for the \u003cstrong\u003eFiat AS.1\u003c\/strong\u003e — the light trainer and touring monoplane designed by Celestino Rosatelli for Fiat Aviazione. A direct evolutionary lineage from the CR series, the AS.1 established foundational structural and aerodynamic templates for Italy's interwar light aviation. The collection covers the baseline AS.1 and the \u003cstrong\u003eTR.1\u003c\/strong\u003e variant, with documents spanning construction, maintenance, spare parts, a photographic archive, and a rare NACA technical circular in English.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch2\u003eCollection Contents — 4 Documents\u003c\/h2\u003e\n\n\u003ch3\u003eAS.1 TR.1 Technical Publications (1 Document)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eA.S.1 Series TR.1 Aircraft — NACA Circular No. 130 — 1930\u003c\/strong\u003e: \u003cem\u003eThe Fiat \"T.R.1\" Training and Touring Airplane — A Two-Place High-Wing Monoplane\u003c\/em\u003e (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003eAS.1 Operating and Maintenance (1 Manual)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAS.1 Aircraft Construction Description\u003c\/strong\u003e, \u003cem\u003eIstruzioni per l'Uso e la Manutenzione\u003c\/em\u003e (Italian Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003eAS.1 Spare Parts List (1 Manual)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAS.1 Aircraft, Illustrated Parts Catalog Manual\u003c\/strong\u003e, \u003cem\u003eCatalogo Nomenclatore\u003c\/em\u003e (Italian Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003eAS.1 Slides, Photos and Brochures (1 Document)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAS.1 Aircraft Photo Collection\u003c\/strong\u003e (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch2\u003eAircraft \u0026amp; Technical Overview\u003c\/h2\u003e\n\n\u003ch3\u003eAerodynamic Architecture\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSesquiplane Configuration:\u003c\/strong\u003e Significantly smaller lower wing surface area minimises drag while maximising structural rigidity.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWarren-Truss Strut System:\u003c\/strong\u003e Distinctive Warren-truss arrangement between wings eliminates traditional wire bracing and reduces parasite drag.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAerodynamic Balance:\u003c\/strong\u003e Horn-balanced ailerons exclusively on the top wing for optimised high-rate roll control.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOpen Cockpit Profile:\u003c\/strong\u003e Fixed un-spatted main landing gear and open-cockpit configuration factored into drag calculations.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003ePowerplant — Isotta Fraschini Asso V-8\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Liquid-cooled Isotta Fraschini Asso V-8 — 240 kW (320 hp).\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropulsion:\u003c\/strong\u003e Two-bladed fixed-pitch wooden propeller optimised for mid-altitude cruising efficiency.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eThermal Management:\u003c\/strong\u003e Frontal nose radiator with manually adjustable shutter slats for in-flight temperature control.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel System:\u003c\/strong\u003e Gravity-assist fuel tank inside the upper wing centre section, minimising mechanical pump dependencies.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003eHandling \u0026amp; Stability\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eLateral Control:\u003c\/strong\u003e Highly sensitive aileron response due to concentrated wing layout — rapid roll initialisation.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePitch Stability:\u003c\/strong\u003e Neutral-to-positive static longitudinal stability margin, minimal stick force for pitch corrections.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eYaw Tendency:\u003c\/strong\u003e Minor directional slip during high-power climbs, managed by permanent offset rigging on the vertical stabiliser.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStall Characteristics:\u003c\/strong\u003e Gentle, predictable nose-drop stall with instant recovery on elevator pressure release.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003ePerformance Data\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eSpecification (320 hp Asso V-8)\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e225 km\/h (140 mph)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e7,450 m (24,440 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange\u003c\/td\u003e\n\u003ctd\u003e650 km (404 miles)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e839 kg (1,850 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e1,155 kg (2,546 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003ch3\u003eEngineering Bulletins\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Construction:\u003c\/strong\u003e Early variants featured full-wooden main spars, later reinforced with duralumin sleeves to address stress fractures from aerobatic manoeuvres.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFabric Maintenance:\u003c\/strong\u003e Mandated inspection intervals for doped fabric covering the rear fuselage to prevent humidity-induced sagging.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine Conversions:\u003c\/strong\u003e Later engineering sheets authorised retrofitting alternative powerplants including the Fiat A.20 inline engine to extend airframe operational lifespan.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003cp\u003e⚠️ Regulatory Notice: Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\n\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53609297248603,"sku":"OAL-IT-FIAT-AS1","price":30.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fiat-as-1-square-impact.png?v=1784221845","url":"https:\/\/onlineaviationlibrary.com\/products\/fiat-as1-light-trainer-technical-manuals-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}