{"product_id":"fokker-f28-fellowship-manuals-collection","title":"Fokker F28 Fellowship — Manuals Collection","description":"\u003ch2\u003eFokker F28 Fellowship — Manuals Collection\u003c\/h2\u003e\n\n\u003cp\u003eThe \u003cstrong\u003eFokker F28 Fellowship\u003c\/strong\u003e was the Netherlands' first purpose-designed jet airliner — a twin rear-fuselage turbofan regional transport that entered service in 1969 and remained in production through 1987, with 241 aircraft delivered across four principal marks. Designed and manufactured by Fokker B.V. at Schiphol-Oost, the F28 established Dutch aerospace engineering on the world stage and served with over 50 operators across six continents.\u003c\/p\u003e\n\n\u003cp\u003eThis living collection assembles the primary-source technical documentation issued by \u003cstrong\u003eFokker B.V.\u003c\/strong\u003e and \u003cstrong\u003eFokker-VFW International B.V.\u003c\/strong\u003e across the operational life of the Fellowship series — from initial certification through the extended Mk 3000 and Mk 4000 variants. Every document is an archival, static-copy edition fixed at its original publication date, presented without alteration or editorial interpolation.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\n\u003cp\u003e\u003cstrong\u003e1. F28 Engineers Guide\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Comprehensive engineering reference covering airframe systems, structural philosophy, powerplant integration, and ground support interface data for maintenance engineers and technical representatives.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e2. F28 Flight Handbook — Including R.L.D. Approved Flight Manual\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker B.V., Schiphol, The Netherlands\u003cbr\u003e\nScope: Pilot operating procedures, performance data, systems descriptions, and the R.L.D. (Rijksluchtvaartdienst) approved flight manual supplement. Covers normal, abnormal, and emergency procedures for the Fellowship series.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e3. F28 MK 3000 and 4000 — Ground Handling and Servicing Data\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Ground servicing procedures, fuelling, towing, jacking, mooring, and ramp handling specifications specific to the stretched Mk 3000 and Mk 4000 variants.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e4. Fokker F28 Structural Repair Manual (SRM)\u003c\/strong\u003e\u003cbr\u003e\nDocument Reference: 6670E | ATA Chapter Structure: 51–57\u003cbr\u003e\nRevision: August 1988\u003cbr\u003e\nScope: Full structural repair data organized by ATA chapter — Fuselage (Ch. 53), Doors (Ch. 52), Windows (Ch. 56), Stabilizers (Ch. 55), Nacelle-Stubwing (Ch. 54), Wings (Ch. 57). Includes the F28 Chapter Arrangement index illustration (Fig. 1, Ref. 28-51-4129).\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e5. Super F28 — Design Features\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker, Schiphol-Oost, Netherlands | Date: January 1979\u003cbr\u003e\nScope: Engineering design features document for the Super F28 development programme — covering aerodynamic refinements, structural upgrades, and performance improvements proposed for the extended-range and higher-capacity variants.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e6. Fokker F28 Fellowship Training Manual\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker B.V.\u003cbr\u003e\nScope: Systems training manual for flight crew and technical personnel. Covers aircraft systems in depth for type rating and recurrent training purposes across the Fellowship series.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e7. Fokker F28 Brochure (1979)\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Original manufacturer's commercial brochure documenting the F28 Fellowship programme as of 1979 — performance summaries, variant overview, and operational characteristics.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e8. Fokker F28 Brochure (General Edition)\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker B.V., Schiphol, The Netherlands\u003cbr\u003e\nScope: General commercial and technical overview brochure for the F28 Fellowship series.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e9. Fokker F28 Brochure (1980)\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Updated manufacturer's brochure reflecting the 1980 production status, including Mk 3000 and Mk 4000 variant data.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eTechnical Reference Data — Fokker F28 Fellowship Series\u003c\/h3\u003e\n\n\u003ch4\u003eAerodynamic Design \u0026amp; Lift Profile\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Sweep:\u003c\/strong\u003e 16° quarter-chord sweep\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAspect Ratio:\u003c\/strong\u003e 7.3:1\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDesign Cruise Altitude:\u003c\/strong\u003e 25,000 ft (initial variants)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDesign Lift Coefficient:\u003c\/strong\u003e C\u003csub\u003eL\u003c\/sub\u003e = 0.20 at Mach 0.73 (Mk 1000\/2000); C\u003csub\u003eL\u003c\/sub\u003e ≈ 0.45 at Mach 0.73 (Mk 4000 with wing modifications)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Ceiling:\u003c\/strong\u003e 35,000 ft (Mk 4000)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSpeed Brake System:\u003c\/strong\u003e Split-tail cone speed brake assembly\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003ePowerplant\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine Type:\u003c\/strong\u003e Rolls-Royce RB.183 Spey — twin-shaft bypass turbofan, rear-fuselage mounted\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTakeoff Thrust:\u003c\/strong\u003e 9,850 lbf (43.9 kN) per engine — Spey Mk 555-15\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUpgraded Configuration:\u003c\/strong\u003e Spey Mk 555-15N per Fokker Service Bulletin No. 71-9\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel Compliance:\u003c\/strong\u003e Rolls-Royce Operating Instructions Document No. F-Sp2-F\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eHandling \u0026amp; Stability\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eTail Configuration:\u003c\/strong\u003e T-tail — single vertical stabilizer with high-mounted horizontal stabilizer\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCruise Pitch Attitude (FL110):\u003c\/strong\u003e 1° – 1.5° nose-up\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNominal Pitch Trim:\u003c\/strong\u003e 0.1°\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Controls:\u003c\/strong\u003e Mechanical push-pull linkages (secondary surfaces); hydraulic boost (primary axes)\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003ePerformance Data by Variant\u003c\/h4\u003e\n\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eMk 1000\u003c\/th\u003e\n\u003cth\u003eMk 2000\u003c\/th\u003e\n\u003cth\u003eMk 4000\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e29,485 kg (65,000 lb)\u003c\/td\u003e\n\u003ctd\u003e29,480 kg (65,000 lb)\u003c\/td\u003e\n\u003ctd\u003e33,110 kg (73,000 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOperating Empty Weight (OEW)\u003c\/td\u003e\n\u003ctd\u003e16,144 kg (35,517 lb)\u003c\/td\u003e\n\u003ctd\u003e16,707 kg (36,953 lb)\u003c\/td\u003e\n\u003ctd\u003e17,645 kg (38,900 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Cruise Speed\u003c\/td\u003e\n\u003ctd\u003e848 km\/h (458 kn)\u003c\/td\u003e\n\u003ctd\u003e848 km\/h (458 kn)\u003c\/td\u003e\n\u003ctd\u003e844 km\/h (455 kn)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff Field Length (ISA, SL)\u003c\/td\u003e\n\u003ctd\u003e1,676 m (5,500 ft)\u003c\/td\u003e\n\u003ctd\u003e1,676 m (5,500 ft)\u003c\/td\u003e\n\u003ctd\u003e1,680 m (5,510 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Passenger Seating\u003c\/td\u003e\n\u003ctd\u003e65\u003c\/td\u003e\n\u003ctd\u003e79\u003c\/td\u003e\n\u003ctd\u003e85\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003ch4\u003eEngineering \u0026amp; Service Bulletin Notes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eRegulatory Authority:\u003c\/strong\u003e Fokker Services B.V. — EASA Type Certificate Data Sheet A.037\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Compliance:\u003c\/strong\u003e Fatigue damage tracking per flight via FOQA metrics; validated against full-scale NASA crash modelling data\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDe-icing:\u003c\/strong\u003e C\/FIMS fluid monitoring systems modifying baseline wing leading-edge bleed heating assemblies\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eNature of the Collection\u003c\/h3\u003e\n\u003cp\u003eAll documents in this collection are archival, static-copy editions fixed at their original publication dates. They are presented as issued by Fokker B.V. and Fokker-VFW International B.V. without editorial modification. This collection is a living archive — additional documents will be added as they are processed and verified, at no additional cost to existing purchasers.\u003c\/p\u003e\n\n\u003ch3\u003eOur Editorial Philosophy\u003c\/h3\u003e\n\u003cp\u003eOnline Aviation Library publishes primary-source aviation documentation for researchers, historians, restorers, flight simulation developers, and serious collectors. We do not simplify, summarize, or repackage. Every document is presented as the manufacturer issued it — with full provenance, original pagination, and unaltered technical content.\u003c\/p\u003e\n\n\u003chr\u003e\n\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\u003e\n\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":53617228906843,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fokker-f28-banner-braathens-safe.png?v=1784385293","url":"https:\/\/onlineaviationlibrary.com\/products\/fokker-f28-fellowship-manuals-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}