{"product_id":"socata-tb-20-trinidad-master-documentation-collection","title":"SOCATA TB-20 Trinidad — Master Documentation Collection","description":"\u003ch3\u003eSOCATA TB-20 Trinidad — Master Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe most comprehensive archival documentation package available for the \u003cstrong\u003eSOCATA TB-20 Trinidad\u003c\/strong\u003e — 15 official EADS\/SOCATA documents in a single Living Collection. From the cockpit to the last structural fastener, from the wiring bus to the parts catalog: this is the definitive factory library for one of France's finest high-performance touring aircraft.\u003c\/p\u003e\n\u003ch3\u003eCollection Manifest — 15 Documents\u003c\/h3\u003e\n\u003ch4\u003ePilot's Information Manual (PIM) — 1 Document\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eTB-20 Pilot's Information Manual\u003c\/strong\u003e — EADS\/SOCATA. Primary flight operations reference: normal and emergency procedures, performance data, systems descriptions, weight \u0026amp; balance. Issued under EADS\/SOCATA authority.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eStandard Illustrated Parts Catalog (IPC) — 5 Tomes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 1\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Airframe structural components, fuselage assemblies, primary structural hardware. © SOCATA 1993–2001.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 2\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Flight control surfaces, landing gear assemblies, actuation hardware.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 3\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Engine installation, cowling, exhaust, firewall-forward components.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 4\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Fuel system, hydraulic system, environmental control components.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 5\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Avionics, instruments, interior furnishings, miscellaneous equipment.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eMaintenance Manual (MM) — 4 Tomes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 1\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Airframe structure, fuselage, primary structural maintenance, inspection intervals, corrosion control. © SOCATA 1991–2001.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 2\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Flight controls, landing gear, hydraulic actuation, rigging data, overhaul limits.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 3\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Powerplant installation, engine mount, cowling, exhaust, firewall-forward systems, troubleshooting.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 4\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Fuel system, electrical system, avionics installation, environmental control, wiring references.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eElectrical Maintenance Manual — 4 Tomes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 1\u003c\/strong\u003e — Réf. Z00.18320E0R5. Power generation, battery, external power, bus distribution, master circuit protection. © SOCATA\/Aerospatiale Matra 1988–2000.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 2\u003c\/strong\u003e — Réf. Z00.18320E0R5. Engine electrical systems, ignition, starter circuits, fuel system electrical controls.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 3\u003c\/strong\u003e — Réf. Z00.18320E0R5. Avionics and instrument electrical installations, lighting systems, pitot-static heating, autopilot wiring.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 4\u003c\/strong\u003e — Réf. Z00.18320E0R5. Landing gear and flap electrical actuation, warning systems, stall warning, gear position indication.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirframe:\u003c\/strong\u003e Low-wing, all-metal semi-monocoque. Advanced airfoil — positive controllability at low speeds, gentle predictable stall.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Loading:\u003c\/strong\u003e 19.4 lb\/ft² (95 kg\/m²) at MTOW — highest in class, exceptional turbulence tracking stability.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Avco Lycoming IO-540-C4D5D — naturally aspirated, fuel-injected, six-cylinder horizontally opposed. 250 BHP at 2,575 RPM.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Hartzell two-blade constant-speed (hydraulically actuated). Optional three-blade for improved ground clearance and reduced cabin noise.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel:\u003c\/strong\u003e 100LL. Total 88.8 USG (336 L); 86.2 USG usable. Unusable: 2.2 USG (7.2 kg).\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eGT Variants:\u003c\/strong\u003e Swept vertical stabilizer, aerodynamically optimized rounded wingtips.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePerformance Data (ISA, Sea Level)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eMTOW: 3,080 lb (1,400 kg)\u003c\/li\u003e\n\u003cli\u003eMax Cruise Speed (Vc): 163 KIAS\u003c\/li\u003e\n\u003cli\u003eStall Speed (Vso): 59 KIAS — flaps fully extended, gear down\u003c\/li\u003e\n\u003cli\u003eMax Rate of Climb: 1,200 fpm\u003c\/li\u003e\n\u003cli\u003eService Ceiling: 20,000 ft\u003c\/li\u003e\n\u003cli\u003eTakeoff Roll (ISA, SL): 761 ft (232 m)\u003c\/li\u003e\n\u003cli\u003eDemonstrated Crosswind Component: 25 knots\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eKey Service Bulletins Referenced\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-148 (Wing Spar Lower Boom):\u003c\/strong\u003e Periodic NDI for fatigue cracks or corrosion; Type 1 or Type 2 metallic repairs if tolerances exceeded.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-058 (Cabin Door Latches):\u003c\/strong\u003e Replacement of AU4G aluminum catches with steel hardware P\/N TB10 250 72 101.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHartzell HC-ASB-61-251:\u003c\/strong\u003e Propeller attachment, dynamic balancing, hub torque standardization.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTextron Lycoming SB No. 480:\u003c\/strong\u003e Multi-viscosity mineral or ashless dispersant engine oil compliance.\u003c\/li\u003e\n\u003c\/ul\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":53655014736219,"sku":null,"price":89.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/tb-20-banner-golden-sunset.png?v=1784993756","url":"https:\/\/onlineaviationlibrary.com\/products\/socata-tb-20-trinidad-master-documentation-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}