{"product_id":"rockwell-dasa-ranger-2000-fr-06-technical-documentation-archive","title":"Rockwell\/DASA Ranger 2000 (FR-06) — Technical Documentation Archive","description":"\u003ch3\u003eRockwell\/DASA Ranger 2000 (FR-06) — Primary-Source Technical Documentation Archive\u003c\/h3\u003e\n\u003cp\u003eOne of the rarest military jet trainer documentation sets in existence. The Rockwell\/DASA Ranger 2000 was a high-performance primary trainer developed jointly by \u003cstrong\u003eRockwell International (North American Aircraft Division)\u003c\/strong\u003e and \u003cstrong\u003eDaimler-Benz Aerospace (DASA)\u003c\/strong\u003e for the U.S. military's \u003cstrong\u003eJoint Primary Aircraft Training System (JPATS)\u003c\/strong\u003e competition in the early 1990s. With only three prototypes ever built before the contract was awarded to the Beechcraft T-6 Texan II, original factory documentation for this aircraft is extraordinarily scarce.\u003c\/p\u003e\n\u003cp\u003eThis archive brings together the core manufacturer-issued technical publications for the FR-06 prototype series — preserved in high-resolution archival format.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocuments Included in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePilot's Operating Handbook (POH) \/ Aircraft Flight Manual — Prototypes RP01 \u0026amp; RP03\u003c\/strong\u003e\u003cbr\u003ePublication No. POH-R-150-M-0001 · Deutsche Aerospace AG, Military Aircraft Division, Munich · LBA Approved · Original Issue: 15 June 1994 · Dasa FR-06 designation · FAR Part 23 compliant handbook\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRanger 2000 Indoctrination Briefing\u003c\/strong\u003e\u003cbr\u003eRef. TMB0794-20-01 · Authored by Fred Knox, Senior Engineering Test Pilot, North American Aircraft · Rockwell Aerospace · Covers aircraft systems familiarization, handling characteristics, and test pilot operational notes\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCFR \/ Safety Procedures Manual\u003c\/strong\u003e\u003cbr\u003eRef. MISC-JPTS-TOC · Covers: Aircraft Diagram, Crash Rescue Information (Entry, Restraints, Canopy Fracturization, Ejection Seats, Engine Shutdown, Battery), Aircraft Rescue Procedures, Ramp \u0026amp; Standby Operations, Ejection Seat Familiarization, Standard Practice (Communications, Pre-Accident Plan, Tow\/Control, Work Restrictions, Fueling\/Defueling, Electrical Equipment, Pyrotechnics, Severe Weather, Pressure Test Safety)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePowerplant:\u003c\/strong\u003e Pratt \u0026amp; Whitney Canada JT15D-5C turbofan — 3,190 lbf (14.19 kN) thrust\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Speed:\u003c\/strong\u003e Mach 0.62 · 410 knots \/ 760 km\/h\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 35,000 ft (10,668 m)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eG-Limits:\u003c\/strong\u003e +6.0 g \/ −3.0 g structural threshold\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDesign Lineage:\u003c\/strong\u003e Aerodynamic evolution of the Rhein-Flugzeugbau (RFB) Fantrainer — transitioning from ducted-fan to pure turbojet configuration\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eJPATS Evaluation:\u003c\/strong\u003e Flight testing conducted at Wright-Patterson Air Force Base, July–October 1994\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFR-06 Redesign:\u003c\/strong\u003e Following the fatal loss of the second prototype (July 1993), the surviving aircraft underwent significant aerodynamic modifications to tail geometry and control surfaces before rebranding as FR-06\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic \u0026amp; Engineering Significance\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eExtensive wind tunnel matrices refined boundary layer airflow to the high-mounted aft engines, ensuring clean flow at high angles of attack\u003c\/li\u003e\n\u003cli\u003eEngineering briefs document the transition from prototype stability defects to an upgraded rigid-body design balancing static aeroelasticity with robust manual flight control loops\u003c\/li\u003e\n\u003cli\u003eThe Ranger 2000 design has been used as a baseline in modern conceptual modeling frameworks (CEASIOM) for predicting advanced flying qualities and aeroelastic wing-load derivatives\u003c\/li\u003e\n\u003cli\u003eTechnical notes focus on dual lateral fuselage air intakes, engine bypass efficiency metrics, and internal flow ducts optimized to prevent compressor stalls during aggressive student-pilot maneuvering\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePermitted Uses\u003c\/h3\u003e\n\u003cp\u003eThis archive is intended for: historical research, flight simulation, museum restoration, aeronautical education, and serious collector reference.\u003c\/p\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. 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.\u003cbr\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":53732661199195,"sku":null,"price":14.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/ranger-2000-formation-banner-with-footer.png?v=1786118088","url":"https:\/\/onlineaviationlibrary.com\/products\/rockwell-dasa-ranger-2000-fr-06-technical-documentation-archive","provider":"Online Aviation Library","version":"1.0","type":"link"}