{"product_id":"socata-tb-9-tampico-primary-source-technical-documentation-collection","title":"Socata TB-9 Tampico — Primary-Source Technical Documentation Collection","description":"\u003ch3\u003eSOCATA TB-9 Tampico — Primary-Source Technical Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe SOCATA TB-9 Tampico is a French all-metal, low-wing, four-seat light aircraft developed by Socata (Groupe Aérospatiale \/ EADS) as a primary and instrument flight trainer. Powered by the Lycoming O-320-D2A (160 HP), the TB-9 became a cornerstone of European flight training fleets from the late 1980s through the 2000s, prized for its structural robustness, positive stability characteristics, and high demonstrated crosswind capability (25 knots).\u003c\/p\u003e\n\u003cp\u003eThis Living Collection brings together \u003cstrong\u003e15 original factory documents\u003c\/strong\u003e spanning the complete technical lifecycle of the TB-9 airframe — from airframe maintenance and structural inspection to parts identification, flight operations, and pilot information.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — 15 Original Factory Documents\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eMaintenance Manual Series (Socata \/ EADS-Socata):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMaintenance Manual — Tome 1\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 2\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 3\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 4\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 5\u003c\/li\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 1 (Référence: Z00.18320310E0R6)\u003c\/li\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 2 (Référence: Z00.18320310E0R6)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eIllustrated Parts Catalog Series (EADS-Socata, P\/N Z00.18082009E0R15):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 1\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 2\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 3\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 4\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 5\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eFlight Operations \u0026amp; Pilot Documentation:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eManuel de Vol \/ Flight Manual — TB 9 (French, Socata \/ Groupe Aérospatiale)\u003c\/li\u003e\n\u003cli\u003ePilot's Operating Handbook (POH) — TB-9\u003c\/li\u003e\n\u003cli\u003ePilot's Information Manual — TB-9 (from S\/N 948, Socata \/ Aérospatiale Matra, P\/N T00.DUOPHPYE, September 1989)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAirframe \u0026amp; Engine Technical Reference\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirframe:\u003c\/strong\u003e All-metal, low-wing monoplane — continuous heavy single milled spar construction\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Lycoming O-320-D2A — 4-cylinder, horizontally opposed, air-cooled, direct-drive\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower Output:\u003c\/strong\u003e 160 HP (120 kW) at 2,700 RPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel System:\u003c\/strong\u003e Carburetor induction — 40-gallon total capacity\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical System:\u003c\/strong\u003e 28V DC — 70-amp engine-mounted alternator + backup battery\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMTOW:\u003c\/strong\u003e 1,060 kg (2,332 lbs)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Cruise Speed:\u003c\/strong\u003e 109–115 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eVNE:\u003c\/strong\u003e 144 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRate of Climb (ISA, SL):\u003c\/strong\u003e 665–738 FPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 11,000 ft\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Range:\u003c\/strong\u003e 505–532 NM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Demonstrated Crosswind:\u003c\/strong\u003e 25 knots\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIntentional Spins:\u003c\/strong\u003e Prohibited\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAirworthiness \u0026amp; Engineering Bulletin Reference\u003c\/h3\u003e\n\u003cp\u003eKey mandatory actions tracked in this documentation set:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-152\u003c\/strong\u003e — Horizontal stabilizer spar inspection and corrosion repair (airframes \u0026gt;4 years or \u0026gt;2,000 flight hours)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEASA AD F-1994-264R1\u003c\/strong\u003e — Front wing attachment fitting NDT inspection (every 3,000 landings or 2,000 flight hours)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-064\u003c\/strong\u003e — Fuel tank venting line retrofit and replacement intervals\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eActive fleet documentation is managed via the Veryon Publications Service Catalog or Daher's official MySocata Portal.\u003c\/p\u003e\n\u003chr\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\u003chr\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.\u003c\/p\u003e\n\u003cp\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":53656551326043,"sku":null,"price":59.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-c-white-factory-livery.png?v=1785036867","url":"https:\/\/onlineaviationlibrary.com\/products\/socata-tb-9-tampico-primary-source-technical-documentation-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}