{"product_id":"potez-heinkel-cm191-twin-jet-executive-aircraft-documentation","title":"Potez-Heinkel CM.191 — Twin-Jet Executive Aircraft | Original Factory Documentation Archive","description":"\u003ch3\u003ePotez-Heinkel CM.191 — Twin-Jet Executive \u0026amp; Liaison Aircraft\u003c\/h3\u003e\n\u003ch3\u003eFranco-German Experimental Programme · 1961–1963\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003ePotez-Heinkel CM.191\u003c\/strong\u003e was a four-seat, twin-turbojet executive and liaison aircraft jointly developed in 1961 by \u003cstrong\u003eÉtablissements Henry Potez\u003c\/strong\u003e (Paris, France) and \u003cstrong\u003eErnst Heinkel Flugzeugbau GmbH\u003c\/strong\u003e (Speyer, West Germany). Derived directly from the celebrated \u003cstrong\u003eFouga CM.170 Magister\u003c\/strong\u003e military jet trainer, the CM.191 represented an ambitious attempt to translate the Magister's proven aerodynamic pedigree into a high-performance civil and military liaison platform. Only two prototypes were constructed before the programme was closed.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Archive — Manifest\u003c\/h3\u003e\n\u003cp\u003eThis archival edition brings together the surviving primary-source factory documentation for the CM.191 programme:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eVerkaufsbroschüre (Sales Brochure)\u003c\/strong\u003e — 6 pages · German language · Ernst Heinkel Flugzeugbau GmbH, Speyer · Covers general description, airframe, equipment, avionics, powerplant, and performance data\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlughandbuch (Flight Manual) — Illustrations Volume\u003c\/strong\u003e · Airframe diagrams and system schematics\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlughandbuch (Flight Manual) — Text Volume\u003c\/strong\u003e · Operational procedures and systems description\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTechnische Daten \/ Specifications Sheets\u003c\/strong\u003e — 7 pages · Detailed dimensional, structural, aerodynamic, and performance data tables\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnlage 1 — UHF-Anlage Type AN\/ARC-34\u003c\/strong\u003e · Sender-Empfänger RT-263\/ARC-34 · 225.0–399.9 MHz · 1,750 channels · 10 W output\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnlage 2 — Funkkompaß-Anlage Type ADF-102\u003c\/strong\u003e · Lear ADF-102 radio compass · Fully transistorised · 5 pre-selectable frequencies · 535–1600 kHz\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnlage 3 — Bord-Eigenverständigungs-Anlage IV T 3 Serie 01\u003c\/strong\u003e · Intercom system by TEAM, Paris · Licensed manufacture by Bauknecht-GEA, Fellbach · 4.63 kg\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eTotal documents in this archive: 15 unique primary-source pages and plates.\u003c\/strong\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eAirframe \u0026amp; Design\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e All-metal mid-wing monoplane with twin turbojets mounted aft of the wing roots, side-by-side four-seat cabin\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuselage:\u003c\/strong\u003e Conventional semi-monocoque shell construction using oval frames and four longerons; pressurised and climate-controlled cabin with full-vision Plexiglas canopy\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing:\u003c\/strong\u003e Trapezoidal single-spar structure, aspect ratio 7.67, slight leading-edge sweep (15°), NACA Series 64 profile — 19% thickness at root, 12% at tip; hydraulically actuated Fowler-type flaps, Frise ailerons, retractable spoilers\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpennage:\u003c\/strong\u003e Iconic V-tail (butterfly tail) inherited from the Fouga Magister — combined pitch\/yaw control via differential rudder deflection and servo trim tabs\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUndercarriage:\u003c\/strong\u003e Tricycle, wide-track main gear (4.41 m), hydraulic retraction — nose gear retracts forward to the nose, main gear folds into the wing roots\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePowerplant — Turbomeca Marboré VI\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eType:\u003c\/strong\u003e Single-stage centrifugal compressor \/ single-stage axial turbine \/ annular combustion chamber with centrifugal fuel injection\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eExhaust:\u003c\/strong\u003e Constant-area nozzle\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax diameter:\u003c\/strong\u003e 0.567 m · \u003cstrong\u003eLength:\u003c\/strong\u003e 1.416 m · \u003cstrong\u003eWeight:\u003c\/strong\u003e 146 kg\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eQuantity:\u003c\/strong\u003e 2 × Marboré VI, mounted on either side of the rear fuselage beneath removable fairings\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eAvionics Suite\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eUHF Transceiver:\u003c\/strong\u003e AN\/ARC-34 (RT-263\/ARC-34) — 225.0–399.9 MHz, 1,750 channels at 1\/10 MHz steps, 20 pre-selectable channels, 10 W output, 27 kg total installation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRadio Compass:\u003c\/strong\u003e Lear ADF-102 — fully transistorised, 5 pre-selectable frequencies, 535–1,600 kHz, Gonio antenna and Gonio coupler, indicator ID 91\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIntercom:\u003c\/strong\u003e Bauknecht-GEA IV T 3 Serie 01 — normal and emergency modes, UHF monitoring capability, pilot priority on transmit\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eKey Performance Data (Factory Specification)\u003c\/h3\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\u003eWingspan\u003c\/td\u003e\n\u003ctd\u003e12.02 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLength\u003c\/td\u003e\n\u003ctd\u003e9.93 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eHeight\u003c\/td\u003e\n\u003ctd\u003e3.20 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWing area\u003c\/td\u003e\n\u003ctd\u003e18.83 m²\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eAspect ratio\u003c\/td\u003e\n\u003ctd\u003e7.67\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax take-off weight\u003c\/td\u003e\n\u003ctd\u003e4,437 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax speed (Gm, no tip tanks)\u003c\/td\u003e\n\u003ctd\u003e710 km\/h at 21,500 rpm\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruise ceiling (Gm)\u003c\/td\u003e\n\u003ctd\u003e12.1 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eClimb rate at sea level (GA, 1 engine)\u003c\/td\u003e\n\u003ctd\u003e3.83 m\/s\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange at 9,000 m (no climb\/descent)\u003c\/td\u003e\n\u003ctd\u003e1,270 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange at 9,000 m (with climb\/descent)\u003c\/td\u003e\n\u003ctd\u003e1,570 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEndurance at 9,000 m\u003c\/td\u003e\n\u003ctd\u003e3.2 h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax speed (with large tip tanks)\u003c\/td\u003e\n\u003ctd\u003e660 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange (large tip tanks, no climb\/descent)\u003c\/td\u003e\n\u003ctd\u003e1,800 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax endurance (large tip tanks)\u003c\/td\u003e\n\u003ctd\u003e4.42 h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e2-seat ferry range (additional tank)\u003c\/td\u003e\n\u003ctd\u003eup to 2,630 km \/ ~5 h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eProgramme History\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eOrigin:\u003c\/strong\u003e Developed jointly by Potez-Air Fouga (Paris), Ernst Heinkel Flugzeugbau GmbH (Speyer), and Fouga — derived from the Fouga CM.170 Magister\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFirst flight:\u003c\/strong\u003e 19 March 1962, Toulouse — test pilots Jacques Grangette and Pierre Caneille\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIntended roles:\u003c\/strong\u003e Civil — business transport, fast feeder, sport aircraft; Military — jet conversion trainer, instrument\/night flying, liaison and courier, reconnaissance\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eProgramme closure:\u003c\/strong\u003e Competition from the Morane-Saulnier MS.760 Paris prevented serial production\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrototype 1 (N8015Q):\u003c\/strong\u003e Exported to the United States\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrototype 2:\u003c\/strong\u003e Preserved at Technik Museum Speyer, Germany\u003c\/li\u003e\n\u003c\/ul\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":53695075516763,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/potez-heinkel-cm-191-banner-3.png?v=1785486181","url":"https:\/\/onlineaviationlibrary.com\/products\/potez-heinkel-cm191-twin-jet-executive-aircraft-documentation","provider":"Online Aviation Library","version":"1.0","type":"link"}