{"product_id":"curtiss-wright-snc-1-falcon-model-22b-flight-technical-documentation-collection","title":"Curtiss-Wright SNC-1 Falcon (Model 22B) — Flight \u0026 Technical Documentation Collection","description":"\u003ch3\u003eCurtiss-Wright SNC-1 Falcon (Model 22B) — Flight \u0026amp; Technical Documentation Collection\u003c\/h3\u003e\n\u003ch3\u003eCW-22B-NEI · SNC-1 · Wright R-975 Whirlwind\u003c\/h3\u003e\n\u003cp\u003eOnline Aviation Library presents a structured archival collection of surviving original flight and technical documentation for the Curtiss-Wright Model 22B and its U.S. Navy designation, the SNC-1 Falcon. These are primary-source documents: the actual publications issued to aircrew and ground engineers during active service — released by the Curtiss-Wright Corporation Airplane Division, St. Louis Plant, and the Bureau of Aeronautics, Navy Department.\u003c\/p\u003e\n\u003cp\u003eThe SNC-1 was an all-metal, cantilever low-wing monoplane derived from the CW-19 light fighter, engineered at the Curtiss-Wright St. Louis Airplane Division as an advanced transition trainer. Its wide-vision tandem canopy, fighter-like control response, and retractable undercarriage made it a demanding and effective bridge between primary trainers and frontline combat aircraft.\u003c\/p\u003e\n\u003ch3\u003e📋 Document Manifest\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eReport CW22-Z18 — Pilot's Handbook, Curtiss Model 22B-NEI\u003c\/strong\u003e — Factory publication released by the Curtiss-Wright Corporation, Airplane Division, St. Louis Plant; covers structural operating speeds, limitations, and systems descriptions for the export variant\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003ePilot's Handbook, Model SNC-1 Airplane\u003c\/strong\u003e — U.S. Navy Bureau of Aeronautics publication; RESTRICTED; covers emergency checklists, fuel plumbing system schematics, weight-and-balance parameters, and operational limitations for the Navy trainer variant\u003c\/p\u003e\n\u003ch3\u003e⚙️ Wright R-975 Whirlwind Engine Technical Documentation\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eT.O. No. 02-35A-1 — Handbook of Operating Instructions, R-975-7 and R-975-11 Aircraft Engines\u003c\/strong\u003e — Published by authority of the Commanding General, Army Air Forces, by the Headquarters, Air Service Command, Patterson Field, Fairfield, Ohio; April 25, 1941, Revised 3-10-43\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eT.O. No. 02-35A-2 — Service Instructions, R-975-7 and R-975-11 Aircraft Engines\u003c\/strong\u003e — Published by authority of the Commanding General, Army Air Forces; 5 April 1943, Revised 20 September 1944\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eAN 02-35A-3 — Overhaul Instructions, R-975-7 and R-975-11 Aircraft Engines\u003c\/strong\u003e — Published under joint authority of the Commanding General, Army Air Forces, the Chief of the Bureau of Aeronautics, and the Air Council of the United Kingdom; 15 October 1943, Revised 25 August 1944\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003e(USAF) T.O. 2R-R975-4 \/ (Navy) AN 02A-40DA-4 — Technical Manual: Illustrated Parts Breakdown, Aircraft Engine, USAF Model R-975-46\u003c\/strong\u003e — Published under authority of the Secretary of the Air Force and the Chief of the Bureau of Aeronautics; 15 January 1955, Changed 31 January 1959\u003c\/p\u003e\n\u003ch3\u003e➡️ Aerodynamic Design \u0026amp; Engineering Notes\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eLow-Wing Monoplane Profile:\u003c\/strong\u003e All-metal, cantilever low-wing monoplane derived from the CW-19 light fighter, engineered by the Curtiss-Wright St. Louis Airplane Division.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eRetractable Undercarriage:\u003c\/strong\u003e Backward-retracting main landing gear identical in concept to the CW-21 Demon fighter design — wheels partially exposed in under-wing fairings, reducing drag while providing aerodynamic backup for belly-landings.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eWing Loading:\u003c\/strong\u003e Total wing area of 173.70 sq ft (16.14 m²), balancing high-speed advanced transition training with stable, low-speed runway approaches.\u003c\/p\u003e\n\u003ch3\u003e💡 Engine Technical Notes — Wright R-975 Whirlwind\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003ePower Plant:\u003c\/strong\u003e One Wright Whirlwind R-975-28, 9-cylinder air-cooled radial piston engine rated at 420–450 hp (313–336 kW), driving a two-blade variable-pitch metal propeller. Positioned as a lower-power, more fuel-efficient option for intermediate aviator transition compared to the heavier SNJ (North American T-6 Texan) with its Pratt \u0026amp; Whitney R-1340.\u003c\/p\u003e\n\u003ch3\u003e🔎 Handling \u0026amp; Stability\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eTandem Configuration:\u003c\/strong\u003e Evaluated under U.S. Navy criteria for transitional training. The wide glass canopy offered excellent visibility for both instructor and student, addressing limitations common in older biplane trainers.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eControl Response:\u003c\/strong\u003e Built to mirror the rapid control surfaces of a frontline fighter — intentionally teaching stall recovery, rudder control against engine torque, and complex instrument flight conditions.\u003c\/p\u003e\n\u003ch3\u003e📊 Performance Reference Data\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eSpecification\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e198 mph (319 km\/h)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruise Speed\u003c\/td\u003e\n\u003ctd\u003e172 kt \/ 193 mph\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e21,800 ft (6,645 m)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRate of Climb\u003c\/td\u003e\n\u003ctd\u003e1,650 ft\/min (8.4 m\/s)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange\u003c\/td\u003e\n\u003ctd\u003e780 miles (1,255 km)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e2,736 lbs (1,241 kg)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e3,788 lbs (1,718 kg)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\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\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 Legal Notice and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53782896804187,"sku":null,"price":49.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/snc-1-banner-3.png?v=1786702356","url":"https:\/\/onlineaviationlibrary.com\/products\/curtiss-wright-snc-1-falcon-model-22b-flight-technical-documentation-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}