{"product_id":"fokker-100-f28-mk-0100-primary-source-documentation-collection","title":"Fokker 100 (F28 Mk 0100) — Primary-Source Documentation Collection","description":"\u003ch3\u003eFokker 100 (F28 Mk 0100) — Primary-Source Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThis collection assembles the core primary-source documentation for the \u003cstrong\u003eFokker 100 (F28 Mk 0100)\u003c\/strong\u003e, the advanced short-to-medium range twin-turbofan regional jet developed by Fokker Aircraft B.V., Schiphol, The Netherlands. Engineering data, certification details, and operational procedures originate directly from official flight test programs, manufacturer archives, and continuing airworthiness records.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocuments Included in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker 100 Aircraft Operating Manual (AOM)\u003c\/strong\u003e — Fokker Aircraft B.V., Schiphol. The definitive operational reference covering normal, abnormal, and emergency procedures for flight crew.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker 100 Aircraft Overview (1989)\u003c\/strong\u003e — Fokker Aircraft B.V. Illustrated overview of the aircraft's systems, configuration, and airline service entry, including USAir fleet photography.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker 100 Technical Description (1985)\u003c\/strong\u003e — Fokker Aircraft B.V. Pre-certification engineering document covering airframe structure, systems architecture, and powerplant integration.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMDF 100 Detail Type Specification DTS 9200\u003c\/strong\u003e — McDonnell Douglas \/ Fokker joint venture document. Formal type specification for the MDF 100 variant, co-branded McDonnell Douglas and Fokker.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMDF 100 Aircraft Systems\u003c\/strong\u003e — McDonnell Douglas \/ Fokker. Systems-level description of the MDF 100 configuration, covering hydraulics, avionics, environmental control, and propulsion.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMDF 100 Technical Proposal Summary for Delta Air Lines\u003c\/strong\u003e — McDonnell Douglas \/ Fokker. Rare airline-specific technical proposal document prepared for Delta Air Lines fleet evaluation.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAir Europe Fokker 100 Flight Crew Operating Manual — Volume 1\u003c\/strong\u003e — Airline-customized FCOM for Air Europe operations, reflecting operator-specific procedures and limitations.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAir Europe Fokker 100 Flight Crew Operating Manual — Volume 2\u003c\/strong\u003e — Continuation of the Air Europe FCOM, covering systems descriptions and performance data.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Engineering Notes\u003c\/h3\u003e\n\u003cp\u003eThe Fokker 100 aerodynamic profile derives from an extensively modified evolution of the original F28 Fellowship wing. Key engineering advances include:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Redesign:\u003c\/strong\u003e Compound chord extension at the root and increased wingspan (28.08 m), dramatically improving aerodynamic efficiency and lift coefficient at high altitudes.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMach Drag Optimization:\u003c\/strong\u003e Root section modifications to delay Mach drag rise during cruise phases.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWind Tunnel Verification:\u003c\/strong\u003e 25 distinct test campaigns totalling 1,928 test hours, validating stalling characteristics and nacelle-to-pylon airflow interactions.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePowerplant — Rolls-Royce Tay\u003c\/h3\u003e\n\u003cp\u003eThe aircraft utilizes rear-mounted, high-bypass twin turbofans designed for high-cycle regional operations:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eRolls-Royce Tay 620-15:\u003c\/strong\u003e Baseline powerplant — 13,850 lbf static takeoff thrust.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRolls-Royce Tay 650-15:\u003c\/strong\u003e Upgrade variant — 15,100 lbf takeoff thrust, expanded fan diameter (45 in), enhanced high-pressure turbine blades.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAcoustic Shielding:\u003c\/strong\u003e Rear fuselage installation exploiting wing noise shielding — more than 16 EPNdB below ICAO Stage 3 requirements.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eHandling and Stability\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl Surfaces:\u003c\/strong\u003e Dual-acting hydraulic systems controlling elevators, ailerons, and primary\/standby rudder actuators.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLift Dumpers:\u003c\/strong\u003e Automatic multi-mode ground spoilers with RTO auto-extension above 50 knots on thrust lever retard.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStability Loading:\u003c\/strong\u003e Longitudinal static stability dictates cargo-first loading, followed by passengers using the window-to-aisle rule, to maintain CG ahead of the aerodynamic center.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePerformance 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 Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e43,000 kg — 45,810 kg (Extended Range)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Operating Speed (V\u003csub\u003eMO\u003c\/sub\u003e \/ M\u003csub\u003eMO\u003c\/sub\u003e)\u003c\/td\u003e\n\u003ctd\u003e320 KIAS \/ Mach 0.77\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e37,000 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff \/ Landing Field Length\u003c\/td\u003e\n\u003ctd\u003e6,000 ft \/ 4,500 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOperational Range\u003c\/td\u003e\n\u003ctd\u003e1,320 nm — 1,710 nm (full payload)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eEngineering Bulletins \u0026amp; Continuing Airworthiness\u003c\/h3\u003e\n\u003cp\u003ePost-production support is managed by Fokker Services Group under \u003cstrong\u003eEASA Type Certificate EASA.A.037\u003c\/strong\u003e:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAvionics \u0026amp; RNP:\u003c\/strong\u003e Service Bulletins permit structural and electronic upgrades including RNP 0.3 and ADS-B Out V2 integration.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Durability:\u003c\/strong\u003e Certified design life of 90,000 landings, supported by fatigue analyses on 2024-T3 aluminum wing\/fuselage joints.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eNature of This Collection\u003c\/h3\u003e\n\u003cp\u003eThese documents represent the primary engineering and operational record of the Fokker 100 program — from pre-certification technical descriptions through airline-customized flight crew manuals and the McDonnell Douglas \/ Fokker MDF 100 joint venture documentation. Together they form an unparalleled archival reference for researchers, historians, restorers, and serious collectors of Dutch aviation heritage.\u003c\/p\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":53617466474843,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fokker-100-promotional-banner-blue-sky.png?v=1784382569","url":"https:\/\/onlineaviationlibrary.com\/products\/fokker-100-f28-mk-0100-primary-source-documentation-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}