{"product_id":"casa-c-295m-primary-source-documentation-collection","title":"CASA C-295M — Primary-Source Documentation Collection","description":"\u003ch3\u003eCASA C-295M — Primary-Source Documentation Collection\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eAirbus (EADS CASA) · Twin-Turboprop Tactical Military Transport\u003c\/strong\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — 5 Primary-Source Documents\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003e#\u003c\/th\u003e\n\u003cth\u003eDocument Title\u003c\/th\u003e\n\u003cth\u003eReference\u003c\/th\u003e\n\u003cth\u003eDate\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003e1\u003c\/td\u003e\n\u003ctd\u003eTraining Manual Performance — C-295M\u003c\/td\u003e\n\u003ctd\u003eME-50(1,2)201-1\u003c\/td\u003e\n\u003ctd\u003eOctober 2004\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e2\u003c\/td\u003e\n\u003ctd\u003eCargo Loading Manual — C-295 Aircraft\u003c\/td\u003e\n\u003ctd\u003eEADS CASA\u003c\/td\u003e\n\u003ctd\u003eOriginal Issue July 2002 \/ Rev. 1 June 2003\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e3\u003c\/td\u003e\n\u003ctd\u003eOperations Manual Vol I — Systems Description (C-295M)\u003c\/td\u003e\n\u003ctd\u003eEADS CASA\u003c\/td\u003e\n\u003ctd\u003eMay 2006\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e4\u003c\/td\u003e\n\u003ctd\u003eOperations Manual Vol II — Limitations \u0026amp; Procedures (C-295M)\u003c\/td\u003e\n\u003ctd\u003eEADS CASA\u003c\/td\u003e\n\u003ctd\u003eMay 2006\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e5\u003c\/td\u003e\n\u003ctd\u003ePerformance Data Manual — Military Operation (C-295M)\u003c\/td\u003e\n\u003ctd\u003eP.D.M. C-295M-MIL OP\u003c\/td\u003e\n\u003ctd\u003eApril 2006\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eAircraft Technical Overview\u003c\/h3\u003e\n\u003cp\u003eThe Airbus (EADS CASA) C-295M is an aerodynamically optimized stretch derivative of the CASA\/IPTN CN-235, engineered for tactical airlift, STOL operations from semi-prepared surfaces, and multi-role military transport missions.\u003c\/p\u003e\n\u003ch4\u003eAerodynamic Architecture\u003c\/h4\u003e\n\u003cp\u003eHigh-wing configuration with high-aspect-ratio straight wing optimized for high lift at low flight envelopes (110–130 knots). Modern C-295W\/MW variants integrate winglets to suppress wingtip vortices and reduce induced drag. Primary flight controls are mechanical — low weight, simplified hydraulic infrastructure, no fly-by-wire complexity.\u003c\/p\u003e\n\u003ch4\u003ePower Plant\u003c\/h4\u003e\n\u003cp\u003eTwo Pratt \u0026amp; Whitney Canada PW127G turboprop engines, each delivering 1,972 kW (2,645 shp). Hamilton Sundstrand 568F-5 six-bladed composite propellers minimize acoustics and cabin vibration while maximizing low-speed thrust. The left engine features an integrated propeller brake enabling APU-mode ground operation without external ground support equipment.\u003c\/p\u003e\n\u003ch4\u003eHandling \u0026amp; Stability\u003c\/h4\u003e\n\u003cp\u003eCertified to military airworthiness standards and EASA CS-25. Stable flight profiles from deck level to 30,000 ft service ceiling. Validated 30-knot crosswind threshold. Extended fuselage moment arm delivers strong yaw stability and directional control under asymmetric thrust (engine-out above V₁).\u003c\/p\u003e\n\u003ch4\u003ePerformance Data (ISA, Standard Conditions)\u003c\/h4\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e23,200 kg (51,146 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Payload\u003c\/td\u003e\n\u003ctd\u003e9,700 kg (21,385 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Cruise Speed\u003c\/td\u003e\n\u003ctd\u003e260 KTAS (480 km\/h)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eSTOL Takeoff Distance (SL, MTOW)\u003c\/td\u003e\n\u003ctd\u003e962 m (3,156 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eSTOL Landing Distance (SL, MLW)\u003c\/td\u003e\n\u003ctd\u003e774 m (2,541 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eFerry Range\u003c\/td\u003e\n\u003ctd\u003e5,278 km (2,850 nm)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange at Max Payload\u003c\/td\u003e\n\u003ctd\u003e1,333 km (720 nm)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003ch4\u003eRegulatory \u0026amp; Certification Notes\u003c\/h4\u003e\n\u003cp\u003eType Certification Data Sheet: EASA.A.186 (shared pilot type rating with CN-235). FAA Flight Standardization Board directives establish Master Difference Requirements for glass cockpit transitions. Structural inspection bulletins cover landing gear attachment links, wing-to-fuselage fairing junctions, and rear cargo ramp hinge locks.\u003c\/p\u003e\n\u003chr\u003e\n\u003cblockquote\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e 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. \u003cstrong\u003eThis archival document does not satisfy that requirement.\u003c\/strong\u003e\u003c\/p\u003e\n\u003c\/blockquote\u003e\n\u003chr\u003e\n\u003cp\u003e\u003cem\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\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53700990009691,"sku":null,"price":50.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/c-295m-banner-2-polish-camouflage.png?v=1785599199","url":"https:\/\/onlineaviationlibrary.com\/products\/casa-c-295m-primary-source-documentation-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}