# TCDS A4IN: Avions Jodel - Type: Type certificate data sheet - Status: Current - Holder: Avions Jodel - Revision: 0 - Revised: November 23, 1962 - Product: Aircraft, Small Airplane - Certification basis: Part 3, CAR 3, CAR 10 - Data sheet PDF: https://openairdocs.org/files/sha256/da/02/da020ef30ffa64c6dfa018d5ebe06fc77adfa88f8d5bf9e0519aef0738c323a5 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/678953C7807A09FF8525673800624A5E.0001 - Page: https://openairdocs.org/tcds/A4IN ## Models (1) As the data sheet lists them. - DR-1050 ## 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 A4IN JODEL DR-1050 November 23, 1962 TYPE CERTIFICATE DATA SHEET NO. A4IN This data sheet which is a part of type certificate No. A4IN 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 Avions Jodel Route de Seurre Beaune (Cote d'Or), France I - Model DR-1050, 3 PCLM (Normal Category), Approved April 19, 1962 Engine Continental O-200-A Fuel 80/87 minimum grade aviation gasoline Engine limits For all operations, 2750 r.p.m. (100 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 2400, not under 2300. No additional tolerance permitted. Diameter: Maximum 69 1/2 in., minimum allowable for repairs 67 1/2 in. No further reduction permitted. Airspeed limits Never exceed 162 m.p.h. (140 knots) Maximum structural cruising 131 m.p.h. (114 knots) Maneuvering 106 m.p.h. ( 92 knots) Maximum speed for drag brakes 94 m.p.h. ( 82 knots) C.G. range (+12.6) to (+20.1) Empty weight C.G. range None Datum Leading edge of wing Leveling means Upper longeron of fuselage Maximum weight 1660 lb. No. seats 3 (2 at +19, 1 at +47) (See NOTE 3 for rear seat occupancy) Maximum baggage See NOTE 3 Fuel capacity Two tanks: 14 gal. usable (-10), 13 gal. usable (+47) Oil capacity 5 qt. (-28) Control surface movements Aileron Up 12° Down 12° Elevator Up 25° Down 20° Elev. trim tab Up 40° Down 25° Rudder Right 25° Left 25° (Tolerance permitted 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. Certification basis CAR 10. Type Certificate No. A4IN issued April 19, 1962. Application for Type Certificate dated February 1, 1962. Each aircraft and any replacement parts manufactured in France must be designated as "import" and clearly labeled as such in accordance with CAR 10.30. A41N Page 2 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 3-6 and conforms to T.C. A4IN." Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: (a) 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 the time of original certification. The certificated empty weight and corresponding center of gravity location must include unusable and system fuel of 5 lb. at (+47). NOTE 2. (a) The following placard must be displayed in front and in clear view of the pilots: "THIS AIRPLANE MUST BE OPERATED IN NORMAL CATEGORY IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS AND MANUALS. NO ACROBATIC MANEUVERS, INCLUDING SPINS, APPROVED." (b) The following placard must be displayed in the rear seat: "MAX. WEIGHT ON REAR SEAT 240 LB." NOTE 3. Rear seat may be occupied by two persons provided: (a) The total weight on the rear seats (including baggage) does not exceed 240 lb. (b) The rear seat is equipped with two separate safety belts. (c) Aircraft weight and C.G. position are within approved limits. - END - ``` ## ADs None name its models. ## STCs approved under this data sheet (14) - [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 - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA308EA](https://openairdocs.org/stc/SA308EA): Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped with Marvel-Schebler MA-2, MA-3, MA-4, MA-4-5, MA-6 and HA-6 series carburetors. (Normal,Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.). Alfred R Puccinelli --- 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.