# TCDS A10IN: Avions Jodel - Type: Type certificate data sheet - Status: Current - Holder: Avions Jodel - Revision: 0 - Revised: August 1, 1963 - Product: Aircraft, Small Airplane - Certification basis: Part 3, CAR 3, CAR 10 - Data sheet PDF: https://openairdocs.org/files/sha256/a3/9a/a39a7d5aa1fa3532ea232c7e984bfee2c2091dd4591b373dc2ec8338af924be0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/73819584BC64E8E78525673800628AF3.0001 - Page: https://openairdocs.org/tcds/A10IN ## Models (1) As the data sheet lists them. - D-1190 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev. No. - - FEDERAL AVIATION AGENCY A10IN JODEL D-1190 August 1, 1963 TYPE CERTIFICATE DATA SHEET NO. A10IN This data sheet which is a part of type certificate No. A10IN prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder Avion Jodel Route de Seurre Beaune (Cote d'Or), France Model D-1190, 2 PCLM (Normal and Utility Category), Approved June 20, 1963 Engine Continental C-90-14F Fuel 80/87 minimum grade aviation gasoline Engine limits Takeoff, 2625 r.p.m. (95 hp.); Maximum continuous, 2475 r.p.m. (90 hp.) Propeller and propeller limits Any approved fixed pitch wood propeller which is eligible for the engine power and speed and which meets the following limits: Static r.p.m. at maximum permissible throttle setting, not over 2350, not under 2150, no additional tolerance permitted. Diameter: Maximum 70 in., minimum allowable for repairs 68 in. (No further reduction permitted). Airspeed limits Never exceed 157 m.p.h. (136 knots) Maximum structural cruising 124 m.p.h. (107 knots) Maneuvering 100 m.p.h. ( 87 knots) C.G. range (+12) to (+21) Empty weight C.G. range None Datum Leading edge of wing Leveling means Upper longeron of fuselage Maximum weight 1360 lb. (normal category), 1190 lb. (utility category) No. of seats 2 at 23 Maximum baggage See NOTE 2(b) Fuel capacity One tank: 29 gal. (+43) (See NOTE 1) Oil capacity 5 qt. (-27) (See NOTE 1) Control surface movements Aileron Up 14° Down 14° Elevator Up 25° Down 20° Elev. trim tab Up 40° Down 25° Rudder Right 25° Left 25° (Tolerance on all surface travels +3° -0°) Serial Nos. eligible The S.G.A.C. Certificate of Airworthiness for Export endorsed as noted below under "Certification basis" must be submitted for each individual airplane for which application for certification is made. A10IN Page 2 Certification basis CAR 10. Type Certificate No. A10IN issued June 20, 1963. Date of Application for Type Certificate dated February 17, 1961. Each aircraft and any replacement parts manufactured in France must be clearly identified as imported. A U. S. Airworthiness Certificate may be issued on the basis of a Certificate of Airworthiness for Export signed by a representative of the French Secretariat General a l'Aviation Civile (SGAC) containing the following statement: "The airplane covered by this certificate has been examined and found to comply with U.S. Civil Air Regulations Part 3 dated May 15, 1956, including amendments 3 -1 through 3-5 and conforms to T.C. A10IN." Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. The following additional item must be installed: Pre-stall warning indicator, Safe Flight Instrument Corporation 164. NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at time of original certification. The certificated empty weight and corresponding center of gravity location must include unusable and system fuel of 2 lb. at +43 and unusable oil of 4 lb. at -27. NOTE 2. (a) The following placard must be displayed in front and in clear view of pilots: (1) "This airplane must be operated as a Normal or Utility Category in compliance with the approved airplane flight manual. All markings and placards, on this airplane apply to its operation as a Normal Category airplane. For Utility Category operations, refer to the airplane flight manual. No acrobatic maneuvers (including spins) are approved for Normal Category operations.." (2) "Do not place anything on the floor." (3) "Day VFR flight only." (b) The following placard must be displayed on the baggage area behind the seat: "Maximum weight 60 lb." For additional loading instructions see weight and balance data. NOTE 3. This airplane is limited to day VFR operations until compliance with applicable portions of CAR 3 and 4B is shown for night and/or IFR approval. - END - ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Jodel Avion D-1190](https://openairdocs.org/model/jodel-avion-d-1190): 0 aircraft (registry code 47004RA) ## STCs approved under this data sheet (12) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd - [STC SA10077SC](https://openairdocs.org/stc/SA10077SC): Installation of push-button starter system.. Hartzell Engine Technologies, LLC - [STC SA10921SC](https://openairdocs.org/stc/SA10921SC): Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators. Hartzell Engine Technologies, LLC - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc. - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA2683NM](https://openairdocs.org/stc/SA2683NM): Installation of Precise Flight, Inc. stand-by vacuum system (SVS). Precise Flight Inc - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc. - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.