# TCDS G1EA: K & L Soaring LLC - Type: Type certificate data sheet - Status: Current - Holder: K & L Soaring LLC - Revision: 5 - Revised: November 29, 2010 - Product: Aircraft, Glider - Certification basis: Part 5, CAR 5 - Registered aircraft: 47, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/bd/2c/bd2cab41470957fda3e6e7c53d7738d7719b487922ecc61cc15762a018dd6bd8 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3097E822380E4A468625780E005D43EF.0001 - Page: https://openairdocs.org/tcds/G1EA ## Models (1) As the data sheet lists them. - SGS 2-32 ## 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. 5 5 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION G1EA Revision 5 K & L Soaring, LLC SGS 2-32 November 29, 2010 GLIDER DATA SHEET NO. G1EA This data sheet which is a part of type certificate No. G1EA 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 K & L Soaring, LLC 5996 State Route 224 Cayuta, New York 14824 Type Certificate Holder Record Schweizer Aircraft Corporation County Airport, P.O. Box 147 Elmira, New York 14902 I - Model SGS 2-32, 2 PCLM, Approved June 19, 1964 Type Class I, High Performance Class II, Utility Airspeed limits Class I Class II (CAS) High Performance Utility Vne-Glide or dive, dive br akes open 158 m.p.h. 139 m.p.h. Vne-Glide or dive, dive brak es closed 150 m.p.h. 139 m.p.h. Vta-Airplane tow 120 m.p.h. 110 m.p.h. Vtaw-Auto-winch to w 86 m.p.h. 86 m.p.h. C.G. range Class I, High Performance (+15.2) to (+20.5) at 1130 lb. or less (+15.2) to (+19.3) at 1340 lb. Class II, Utility (+15.2) to ( 20.5) at 1340 lb. or less (+15.2) to (+19.3) at 1430 lb. Straight-line variation between points given. 1000 1130 1340 1430 15.2 19.3 20.5 Class I High Performance Class II Utility LB. INCHES AFT DATUM Maximum weight Class I, High Performance: 1340 lb. Class II, Utility: 1430 lb. G1EA 2 ______________________________________________________________________________________________________ No. seats Class I, High Performance: 2 (1 at -24) (1 at +3) Class II, Utility: 3 (1 at -24) (2 at +3) Baggage None Control surface movements Limits Stabilator (trailing edge) Up 19 1/2° Down 9 1/2° +0°, -3° Stabilator tab Anti-servo Up 36° Down 22° Trim Up 6° Down 7° + 2° Rudder Left 39° Right 29° + 1° Aileron Up 29° Down 13° +0°, -3° Dive Brakes Top Up 85° Bottom + 5° Down 85° Serial nos. eligible 2 and up Specifications Pertinent to All Models Datum Wing leading edge at root M.A.C. 41.17 in. (L.E. of M.A.C. 4.87 in. aft of wing leading edge at root) Leveling means Two brackets on right side under aft deck Certification basis CAR 5 effective February 15, 1956, Amendment 5-1 effective May 3, 1962, and Basic Glider Criteria Handbook, 1962. Date of App lication for Type Certificate June 5, 1962. Type Certificate No. G1EA issued June 19, 1964. Production basis None Equipment: The basic equipment as prescribed in the applicable airworthiness regulations (See certification basis) must be installed in the aircraft for certification. NOTE 1. Suitable placards to cover the various pilot and passenge r weights must be installed in full view of the pilot as determined from the manufactur er's weight and balance report. NOTE 2. The following placards must be installed in full view of the pilot: (a) "Solo front seat only." (b) "Class I, High Performance Max. glide or dive, dive brakes open 158 m.p.h. Max. glide or dive, dive brakes closed 150 m.p.h. Max. aero tow 120 m.p.h. Max. auto-winch tow 86 m.p.h. (c) "Class II, Utility Max. glide or dive 139 m.p.h. Max. aero tow 110 m.p.h. Max. auto-winch tow 86 m.p.h. Instrument flight prohibited." NOTE 3. Glider characteristics are suitable for instrument flight, and the glider may be so approved for Class I, High Performance, provided that minimu m equipment required by Civil Air Regulations for IFR flight is installed and operable. Flight in clouds permi ssible when altimeter and turn-and-bank indicator are installed. NOTE 4. Auto-winch towing permitted provided recomme ndations in SGS 2-32 Pilot's Handbook are observed. NOTE 5. Approved safety belt and shoulde r harness required for each occupant. ...END... ``` ## ADs (2, in force first) - [AD 87-17-01](https://openairdocs.org/ad/87-17-01): Tow Release Installation · K & L Soaring SGS 1-23, SGS 1-23D, SGS 1-23F and 25 more. Effective Aug 19, 1988 - [AD 87-02-01](https://openairdocs.org/ad/87-02-01): Tow-Release Installation Inspection · K & L Soaring SGM 2-37, SGS 1-23, SGS 1-23D and 32 more. Effective Jan 21, 1987 ## Registered aircraft by registry model (OpenAirDocs) - [Schweizer SGS 2-32](https://openairdocs.org/model/schweizer-sgs-2-32): 47 aircraft (registry code 8050206) ## STCs approved under this data sheet (4) - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey - [STC SG01164CH](https://openairdocs.org/stc/SG01164CH): Install Cooper superflite 102 fabric.. Aviation Products Systems Inc. - [STC SG1244GL](https://openairdocs.org/stc/SG1244GL): Surrendered and incorporated into STC SG01164CH.. Cooper Aviation Supply Company, 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.