# TCDS G6EU: Aer-Pegaso S.p.A. - Type: Type certificate data sheet - Status: Current - Holder: Aer-Pegaso S.p.A. - Revision: 2 - Revised: April 14, 2022 - Product: Aircraft, Glider - Certification basis: CAR 5, CAR 10 - Registered aircraft: 4, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/9d/5d/9d5de58191647dbfce083b7de913e81af21844755a80838d5ca50aaa32b9f33f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7A0AF44E178FDFCB8625882900594C33.0001 - Page: https://openairdocs.org/tcds/G6EU ## Models (1) As the data sheet lists them. - M-100 S ## 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. 2 2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION G6EU Revision 2 AER-PEGASO M-100 S April 14, 2022 TYPE CERTIFICATE DATA SHEET NO. G6EU This data sheet which is a part of Type Certificate No. G6EU 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 Aer-Pegaso S.p.A. Torino, Italy Model "M-100 S" Glider approved February 18, 1965 Airspeed Limits (IAS) Glide or dive 119 kts. (still air) " " 70 " (rough air) Airbrakes extended 108 " (still air) " " 70 " (rough air) Airplane tow 81 " Auto-winch tow 55 " C.G. Range From (+11.3) to (+16.5) Datum Wing leading edge Leveling Means Fuselage upper contour just in front of the dorsal fin at 4° down with respect to horizontal reference. Maximum Weight 693 lbs. No. of Seats 1 at (-19.7) Baggage (+7.88) Max. permissible baggage: 100 lbs. Control Surfaces Elevator Up 28° + 2° Down 20° + 2° Rudder Right 28° + 2° Left 28° + 2° Ailerons Up 28° + 2° Down 28° + 2° Serial Nos. Eligible An Italian Export Certificate of Airworthiness (Export C of A) endorsed as noted under "Import Requirements" must be submitted for each individual glider for which application for certification is made. Certification Basis CAR 10 Type Certificate G6EU. CAR 5 dated February 5, 1956 (Basic Glider Criteria, revised 1962) Date of Application for Type Certificate May 7, 1963. Import Requirements An U.S. Airworthiness Certificate may be issued on the basis of a n Export C of A signed by a representative for the R.A.I., containing the following statement: "The glider covered by this Certificate has been examined and found to comply with CAR 5 dated February 15, 1956 (Basic Glider Criteria, revised 1962), Type Certificate G6EU and is airworthy.” Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the agreement, to identify any required statements by the exporting authority on the export certificate of airworthiness (or G6EU 2 equivalent document), and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, Airworthiness Certification of Aircraft , for requirements for issuance of an airworthiness certificate for imported aircraft. Equipment Non cloud flying and Acrobatic: safety harness, airspeed indicator, altimeter. Cloud flying: above items plus: turn and bank indicator, compass, variometer. NOTES NOTE 1. Current weight and balance report, including list of equipment included in certified empty weight, and loading instructions when necessary, must be in the glider at the time of original certification and at all times thereafter. NOTE 2. The following placards must be installed in full view of the pilot: "Max. speed (Vne) still air 119 kts. " " with airbrakes extended, still air 108 " " " rough air (airbrakes extended or closed) 70 " " " aero tow 81 " " " auto-winch tow 55 " Permitted aerobatics: Looping: entry speed 78 kts. chandelle: " " 70 " spin: " " 32 " tight turns till 3.5g. All other acrobatics are prohibited." "Night flying is prohibited" "Auto-Winch tow is permitted for towing mechanism located near the C.G." The following placard must be installed in the baggage compartment: "Max. permissible baggage: 100 lbs." ...END... ``` ## ADs (3, in force first) - [AD 76-05-09](https://openairdocs.org/ad/76-05-09): Rudder Hinge Bracket · Aer-Pegaso M-100 S. Effective Mar 25, 1976 - [AD 75-23-02](https://openairdocs.org/ad/75-23-02): Aileron Spars · Aer-Pegaso M-100 S and M-200. Effective Nov 14, 1975 - [AD 69-24-01](https://openairdocs.org/ad/69-24-01): Horizontal Stabilizer · Aer-Pegaso M-100 S and M-200. Effective Nov 23, 1969 ## Registered aircraft by registry model (OpenAirDocs) - [Aer-Pegaso M-100S](https://openairdocs.org/model/aer-pegaso-m-100s): 3 aircraft (registry code 0200506) - [Avionautica Rio M-100S](https://openairdocs.org/model/avionautica-rio-m-100s): 1 aircraft (registry code 0910102) --- 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.