{"product_id":"nord-nc-701-martinet-sncac-aircraft-technical-descriptive-manual","title":"Nord NC-701 Martinet — S.N.C.A.C. Aircraft Technical Descriptive Manual","description":"\u003ch2\u003eNord NC-701 Martinet — S.N.C.A.C. Aircraft Technical Descriptive Manual\u003c\/h2\u003e\n\n\u003cp\u003eThe \u003cstrong\u003eNord NC-701 Martinet\u003c\/strong\u003e is a French post-WWII twin-engine light transport, aerial photogrammetry, and advanced trainer aircraft developed by \u003cstrong\u003eSNCAC (Société Nationale de Constructions Aéronautiques du Centre)\u003c\/strong\u003e. A direct engineering evolution of the German Siebel Si 204D, the Martinet was adopted across multiple French military and civil roles and exported to allied operators including LOT Polish Airlines and the Swedish government.\u003c\/p\u003e\n\n\u003cp\u003eThis archival edition reproduces the original factory documentation compiled under reference \u003cstrong\u003eS.N.C.A.C. Notice Technique No. 701.01 — Notice Descriptive\u003c\/strong\u003e, covering the Type de Base No. 701 and its operational variants (Types II through V: Marine, D.T.A., État-Major, École de Navigation, and Mission Photographique).\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e1. Airframe \u0026amp; Aerodynamic Configuration\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e Low-wing cantilever monoplane — all-metal duralumin semi-monocoque fuselage\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Structure:\u003c\/strong\u003e Single-spar wing with trailing-edge split (crocodile) flaps for high-drag steep approaches\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl Surfaces:\u003c\/strong\u003e Fabric-covered ailerons and elevators — minimised weight and flutter tendency\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNose Section:\u003c\/strong\u003e Fully glazed, unstepped ogival nose — optimised for student navigator and bomb-aimer visibility\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpennage:\u003c\/strong\u003e Twin vertical stabiliser and rudder layout — positive directional control and asymmetric yaw management on single-engine operations\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLongitudinal Trim:\u003c\/strong\u003e Adjustable horizontal stabiliser to counteract pitch moments from CG shifts and flap deployment\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e2. Powerplant — Renault 12S-00\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine Type:\u003c\/strong\u003e Twin Renault 12S-00 — air-cooled, inverted V-12 inline; French derivative of the wartime Argus As 411A1\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTakeoff Power:\u003c\/strong\u003e 580 hp (427 kW) at sea level\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eContinuous Power:\u003c\/strong\u003e 390 hp (287 kW)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSupercharger:\u003c\/strong\u003e Single-stage mechanically driven centrifugal supercharger with elastic drive coupling — rated to critical altitude of 2,400 m\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Variable-pitch three-bladed propellers (upgrade over original German two-bladed design)\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e3. Performance Data\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Speed:\u003c\/strong\u003e 350 km\/h (220 mph) at 3,000 m\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCruising Speed:\u003c\/strong\u003e 325 km\/h (202 mph) at 3,000 m\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanding \/ Stall Speed:\u003c\/strong\u003e 115 km\/h (71 mph) — flaps fully extended\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRate of Climb:\u003c\/strong\u003e 5.3 m\/s (1,043 ft\/min) at maximum continuous power\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 6,400 m (21,000 ft)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOperational Range:\u003c\/strong\u003e 810 km (500 mi) standard; up to 1,400 km with auxiliary ferry tanks\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpty Weight:\u003c\/strong\u003e 3,860 kg (passenger layout) \/ 3,920 kg (aerial photography configuration)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMTOW:\u003c\/strong\u003e 5,600 kg\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e4. Handling, Stability \u0026amp; Systems\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eIce Mitigation:\u003c\/strong\u003e Hot-air de-icing ducts integrated into windscreen and flight deck viewing panels\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Controls:\u003c\/strong\u003e Dual control posts with disconnect capability; electro-hydraulic flap command system\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUndercarriage:\u003c\/strong\u003e Retractable tricycle gear — mechanical, hydraulic, and electrical actuation with manual emergency backup and braking\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e5. Operational Variants \u0026amp; Engineering Bulletins\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérophotogrammétrie Conversion:\u003c\/strong\u003e Heavy KF radio station, dual automated floor cameras, rear darkroom compartment — operated by LOT Polish Airlines and the Swedish government for mapping missions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSanitary Evacuation Variant:\u003c\/strong\u003e Cabin conversion for medical evacuation litters — seat removal procedure documented in technical bulletins\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMagnetic Mine Sweeping (NC-701 No. 8):\u003c\/strong\u003e Structural retrofit of Airframe No. 8 for French Navy magnetic mine detonation trigger array testing — unique engineering bulletin\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDocument Manifest — Notice Technique No. 701.01\u003c\/h3\u003e\n\u003cp\u003e\u003cem\u003eNotice Descriptive — S.N.C.A.C., Numéro 701.01\u003c\/em\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003ePlaneur — Voilure (Wing Assembly): Caissons AV\/AR internes et externes, longeron principal, extrémités d'aile, raccord voilure-fuselage\u003c\/li\u003e\n\u003cli\u003eAileron, Volets d'Intrados, Bâti Moteur Intermédiaire et Capotage\u003c\/li\u003e\n\u003cli\u003eFuselage — Partie AV (Cabine Pilote), Partie Médiane, Partie AR, Pointe AR\u003c\/li\u003e\n\u003cli\u003eCommandes de Vol — Gauchissement, Profondeur, Direction, Flettners, Volets d'Intrados\u003c\/li\u003e\n\u003cli\u003eEmpennages Horizontaux et Verticaux (Dérives, Gouvernails)\u003c\/li\u003e\n\u003cli\u003eAtterrisseurs AV et AR — Commande de Train Rentrant (mécanique, hydraulique, électrique), Freinage, Carénage\u003c\/li\u003e\n\u003cli\u003eAccessibilité et Démontabilité\u003c\/li\u003e\n\u003cli\u003eGroupe Moto-Propulseur — Moteurs, Commandes Moteurs, Démarrage, Alimentation (Essence, Amorçage, Transvasement), Graissage, Refroidissement, Hélices\u003c\/li\u003e\n\u003cli\u003eMatériel d'Équipement — Instruments de Pilotage et Navigation, Contrôle Moteurs, Changement de Pas d'Hélice, Escamotage de Train, Volets d'Intrados, Flettners\u003c\/li\u003e\n\u003cli\u003eMatériel Électrique, Radio Électrique, Radio Goniométrie, Photographique, Téléphonique\u003c\/li\u003e\n\u003cli\u003eInstallation d'Oxygène, Matériels Divers\u003c\/li\u003e\n\u003cli\u003eInstallation de l'Équipage et des Passagers\u003c\/li\u003e\n\u003cli\u003eTable des Figures — 23 numbered figures (pp. 14–45) covering wing, fuselage, flight controls, and electro-hydraulic schematics\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\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 authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/strong\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659345453403,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/nc-701-martinet-wide-hero-banner.png?v=1785080450","url":"https:\/\/onlineaviationlibrary.com\/products\/nord-nc-701-martinet-sncac-aircraft-technical-descriptive-manual","provider":"Online Aviation Library","version":"1.0","type":"link"}