{"product_id":"socata-tb-10-tobago-primary-source-technical-documentation-collection","title":"Socata TB-10 Tobago — Primary-Source Technical Documentation Collection","description":"\u003ch2\u003eSOCATA TB-10 Tobago — Primary-Source Technical Documentation Collection\u003c\/h2\u003e\u003cp\u003eThe SOCATA TB-10 Tobago is a French all-metal, low-wing, four-seat light aircraft developed by Socata (Groupe Aérospatiale \/ EADS) as a touring and instrument flight trainer. Powered by the Lycoming O-360-A1AD (180 HP) with a Hartzell constant-speed propeller, the TB-10 offered a significant performance step over its sibling the TB-9 Tampico, with greater range, higher cruise speed, and a wider cabin. It became a staple of European flight training and private touring fleets through the 1980s and 2000s.\u003c\/p\u003e\u003cp\u003eThis Living Collection brings together \u003cstrong\u003e16 original factory documents\u003c\/strong\u003e spanning the complete technical lifecycle of the TB-10 airframe — from airframe maintenance and structural inspection to parts identification, flight operations, and pilot information.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest — 16 Original Factory Documents\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003eMaintenance Manual Series (EADS-Socata, P\/N Z00.18010310E0R13):\u003c\/strong\u003e\u003c\/p\u003e\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\u003c\/ul\u003e\u003cp\u003e\u003cstrong\u003eElectrical Maintenance Manual Series (TB 9–10–200 Family Document, P\/N Z00.18320310E0R6):\u003c\/strong\u003e\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 1\u003c\/li\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 2\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003e\u003cstrong\u003eIllustrated Parts Catalog Series (EADS-Socata, P\/N Z00.18082010E0R15):\u003c\/strong\u003e\u003c\/p\u003e\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\u003cp\u003e\u003cstrong\u003ePilot Documentation:\u003c\/strong\u003e\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003ePilot's Information Manual — TB 10 (EADS-Socata)\u003c\/li\u003e\n\u003cli\u003ePilot's Information Manual — TB 10 (Socata \/ Aérospatiale Matra, from S\/N 848, P\/N T00.DVDPIPYE, September 1989) — 9 sections + 7 supplements including KAP 100 Autopilot, KAP\/KFC 150 Autopilot, Ground Power Receptacle, Auxiliary Air Pump, Low Noise Exhaust, Garmin 150 GPS\u003c\/li\u003e\n\u003cli\u003eSocata TB-10 User Manual — Tome 1\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAirframe \u0026amp; Engine Technical Reference\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirframe:\u003c\/strong\u003e All-metal, low-wing monoplane — semi-tapered wing planform, fixed tricycle gear with fairings\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCabin Width:\u003c\/strong\u003e 4 ft 3 in — widest in class for a four-seat GA trainer\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Lycoming O-360-A1AD — 4-cylinder, horizontally opposed, air-cooled, direct-drive\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower Output:\u003c\/strong\u003e 180 HP (134 kW) at 2,700 RPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Hartzell constant-speed, two-blade metal (HC-C2YK-1BF\/F7666A-2)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel System:\u003c\/strong\u003e Carburetor induction — 54 US gallons total capacity\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMTOW:\u003c\/strong\u003e 1,150 kg (2,530 lbs) · Standard Empty Weight: 1,477 lbs\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Cruise Speed:\u003c\/strong\u003e 127–133 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRate of Climb (Vy):\u003c\/strong\u003e 790 FPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 13,000 ft\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Range:\u003c\/strong\u003e 653 NM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTakeoff Ground Roll (10° Flaps):\u003c\/strong\u003e 286 m (938 ft)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStall Speed — VS0 (landing config):\u003c\/strong\u003e 53 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStall Speed — VS (clean):\u003c\/strong\u003e 60 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Demonstrated Crosswind:\u003c\/strong\u003e 25 knots\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eType Certificate:\u003c\/strong\u003e EASA.A.378 \/ FAA A51EU\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAirworthiness \u0026amp; Engineering Bulletin Reference\u003c\/h3\u003e\u003cp\u003eKey mandatory actions tracked in this documentation set:\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-085-57\u003c\/strong\u003e — Wing internal rib structural inspections and reinforcement kit installation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAerospatiale SB 15 \u0026amp; SB 29\u003c\/strong\u003e — Elevator trim tab linkage and control rod end-fitting checks to prevent attachment play\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003eActive fleet documentation is managed via the Veryon Publications Service Catalog or Daher's official MySocata Portal.\u003c\/p\u003e\u003chr\u003e\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\u003chr\u003e\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\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":53656554635611,"sku":null,"price":59.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-d-over-the-clouds.png?v=1785038456","url":"https:\/\/onlineaviationlibrary.com\/products\/socata-tb-10-tobago-primary-source-technical-documentation-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}