# TCDS G36EU: Alexander Schleicher GmbH & Co. Segelflugzeugbau - Type: Type certificate data sheet - Status: Current - Holder: Alexander Schleicher GmbH & Co. Segelflugzeugbau - Revision: 2 - Revised: February 8, 2022 - Product: Aircraft, Glider - Certification basis: Part 21 - Registered aircraft: 43, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/b1/bd/b1bd3cc6591242e2fa4b79e7ddf52835f412b2b6e76b9efcb12513c411410508 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F2B479C6201603F98625886100681A7F.0001 - Page: https://openairdocs.org/tcds/G36EU ## Models (2) As the data sheet lists them. - ASW-19B - ASW-19 ## 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 3 4 Rev. No. 2 2 2 2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION G36EU Revision 2 Alexander Schleicher GmbH ASW-19 ASW-19B February 8, 2022 TYPE CERTIFICATE DATA SHEET NO. G36EU This data sheet which is a part of Type Certificate No. G36EU prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder. Alexander Schleicher GmbH & Co. Segelflugzeugbau Alexander-Schleicher-Str. 1 36163 Poppenhausen Germany Type Certificate Holder Record. Alexander Schleicher, Segelflugzeugbau transferred TC G36EU to Alexander Schleicher GmbH & Co. Segelflugzeugbau in 1984. I - Model ASW-19 Glider, approved January 12, 1977 Airspeed Limits. (I.A.S.) Max. speed 135 knots (155 mph) Airplane tow 92 knots (106 mph) Auto-winch tow 65 knots (75 mph) Dive brakes extended 135 knots (155 mph) Maneuvering speed 92 knots (106 mph) C.G. Range. (+9.45 inches) to (+15.12 inches) Datum. Wing leading edge at wing root rib Leveling Means. Slope of rear top edge of fuselage 1000 to 45. Maximum Weight. 900 lbs (with water ballast) 805 lbs (without water ballast) (See NOTE 2) No. of Seats. 1 (-22 in) Baggage. 33 lbs (+6.0 in) Control Surface Movements. Elevator Up 22° + 3.5° Down 18° + 2.0° Rudder Right 30° + 3° Left 30° + 3° Aileron Up 22° + 3.5° Down 14° + 2.0° Wink Links for Towing. Winch launching 1100 lbs (500 kg) max. Airplane tow 1100 lbs (500 kg) max. G36EU 2 II - Model ASW-19B Glider, approved July 12, 1978 Same data as Model ASW-19 except the following: Airspeed Limits. (I.A.S.) Max. speed to 10,000' MSL 138 knots (158 mph) 10,000 to 23,000' MSL 110 knots (126 mph) 23,000 to 29,500' MSL 95 knots (109 mph) Va Maneuvering speed 92 knots (106 mph) Vt Aerotow (max.) 92 knots (106 mph) Autowinch (max.) 67 knots (78 mph) Dive brakes extended 138 knots (158 mph) Maximum Weight. 1000 lbs (with water ballast) 805 lbs (without water ballast) (See NOTE 2) Weak Link for Towing. 1323 lbs (600 kg max.) Serial Numbers Eligible. (See Import Requirements and NOTE 5) Data Pertinent To All Models Serial Nos. Eligible. The NAA Export Certificate of Airworthiness (Export C of A) endorsed as noted below under "Import Requirements" must be submitted for each individual glider for which application for standard airworthiness certification is made. (See NOTE 5) Import Requirements. A U.S. airworthiness certificate may be issued on the basis of an NAA Export C of A signed by a representative of the German Airworthiness Authority, the Luftfahrt-Bundesamt (LBA), containing the following statement: "The glider covered by this certificate has been examined and found to comply with the Federal Republic of Germany glider airworthiness requirements dated February 1966 and conforms to Type Certificate No. G36EU and is in condition for safe operation". 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 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. Certification Basis. FAR 21.29, effective February 1, 1965. Federal Republic of Germany Airworthiness Requirements, dated February 1966 were found to provide a level of safety equivalent to provisions of FAR 21.23 to enable certification under the provision of FAR 21.29. Type Certificate No. G36EU issued January 12, 1977. Date of Application for Type Certificate: May 5, 1976. The LBA, originally type certificated these gliders under its Type Certificate (TC) No. 308, initial issue May 7, 1976. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of these models and the LBA TC was deemed to be issued by EASA and remains valid. Equipment. The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the glider for standard G36EU 3 airworthiness certification. In addition the following equipment must be installed: 1) Instruments (Non-Cloud flying): (i) Airspeed indicator, Winter 6FMS/W 19, or PZL PR-250S/W 19 with extended range to 270 km/h., or an FAA-approved equivalent. (ii) Altimeter. (iii) Lap and shoulder straps. 2) Additional Instruments for Cloud flying: (i) Magnetic compass. (ii) Turn and bank. (iii) Variometer. 3) For Model ASW-19: LBA-approved Flight and Operations Manual dated May 1976 or later LBA-approved issue. For Model ASW-19B: LBA-approved Flight and Operations Manual dated June 1978 or later LBA-approved issue. Service Information. Each of the documents listed below must state that it is approved by the EASA or – for approvals made before September 28, 2003 – by the LBA: • Service bulletins • Structural repair manuals • Vendor manuals • Aircraft flight manuals • Overhaul and maintenance manuals The FAA accepts such documents and considers them FAA-approved for type design data only unless one of the following conditions exists: • The documents change the limitations, performance, or procedures of the FAA approved manuals. The FAA uses post type validation procedures to approve these documents. The FAA may delegate on a case-by-case basis to EASA to approve these on behalf of the FAA for the U.S. type certificate. If this is the case, it will be noted on the document. NOTES. NOTE 1. Current weight and balance report including list of equipment in certificated empty weight, and loading instructions, when necessary, must be provided for each glider at the time of original certification. NOTE 2. The following placards must be installed in full view of the pilot: 1) "This glider must be operated in compliance with the operating limitations stated in the form of placards, markings and manuals." 2) "Cloud flying: Permitted only when the following instruments are installed: (1) Airspeed indicator (2) Altimeter (3) Turn and bank Indicator (4) Variometer (5) Compass." 3) "Acrobatic maneuvers including spins must be accomplished in accordance with the LBA- approved Model ASW-19 Flight and Operations Manual. Aerobatics prohibited with water ballast aboard." 4) "Night flying is prohibited." G36EU 4 Applicable to ASW-19: 5) Maneuvering speed 92 knots (106 mph) Airplane tow speed 92 knots (106 mph) Auto-winch tow speed 65 knots (75 mph) Stall speed - Dive brakes extended 42 knots (48 mph) 6) For gliders without water ballast system installed: "Maximum Weight 805 lb." 7) For gliders with water ballast system installed: "Maximum Weight excluding water ballast 805 lb. Maximum Weight with water ballast 900 lb." 8) "Weak Link - Airplane/Auto/Winch Tow 1100 lb.” Applicable to ASW-19B: 9) Vne to 10,000' MSL 138 knots (158 m.p.h.) 10,000 to 23,000' MSL 110 knots (126 m.p.h.) 23,000 to 29,500' MSL 95 knots (109 m.p.h.) Maneuvering speed 92 knots (106 m.p.h.) Airplane tow speed 92 knots (106 m.p.h.) Autowinch tow speed 67 knots (78 m.p.h.) Stall speed - Dive brakes extended 42 knots (48 m.p.h.) 10) For gliders without water ballast system installed: "Maximum weight 805 lb." 11) For gliders with water ballast system installed: "Maximum weight excluding water ballast 805 lb. Maximum weight with water ballast 1000 lb." 12) “Weak link - Airplane/auto/winch tow 1323 lb.” NOTE 3. All external portions of the glider exposed to sunlight must be painted white. Registration and Competition numbers must be painted blue-gray or in any other light colors. NOTE 4. Information essential to the proper operation, maintenance, inspection and repair is contained in the Schleicher "Flight and Operations Manual," applicable to the model concerned. Major repairs must be performed in accordance with repair methods approved by Alexander Schleicher or by the FAA. NOTE 5. ASW-19 Serial Numbers 19001 through 19225 are eligible for a Standard Airworthiness Certificate as a Model ASW-19B when modified in accordance with the manufacturer's Technical NOTE ASW 19 No. 6a and placard installed per NOTE 2(9) of this TCDS. ...END... ``` ## ADs (5, in force first) - [AD 98-17-02](https://openairdocs.org/ad/98-17-02): Tow Release Cable Guide Fittings Inspection · Alexander Schleicher ASW-19 and ASW-19B. Effective Sep 26, 1998 - [AD 98-12-03](https://openairdocs.org/ad/98-12-03): Rudder Panel, Airbrake Bellcrank, Rear Canopy Hinge · Alexander Schleicher ASK 21, ASW-19 and ASW-19B. Effective Jul 14, 1998 - [AD 98-04-46](https://openairdocs.org/ad/98-04-46): Inspection Hole Cover Entering Fuselage · Alexander Schleicher ASW-19 and ASW-19B. Effective Apr 3, 1998 - [AD 97-08-06 R1](https://openairdocs.org/ad/97-08-06-R1): Quick Connectors · Alexander Schleicher AS-K 13, AS 12, ASK 21 and 39 more. Effective Aug 1, 1997 - [AD 84-13-04](https://openairdocs.org/ad/84-13-04): Horizontal Tailplane Flutter · Alexander Schleicher ASW-19 and ASW-19B. Effective Sep 13, 1984 ## Registered aircraft by registry model (OpenAirDocs) - [Schleicher ASW-19](https://openairdocs.org/model/schleicher-asw-19): 26 aircraft (registry code 3801508) - [Schleicher ASW-19B](https://openairdocs.org/model/schleicher-asw-19b): 17 aircraft (registry code 3801505) --- 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.