# TCDS G-17: K & L Soaring LLC - Type: Type certificate data sheet - Status: Current - Holder: K & L Soaring LLC - Revision: 2 - Revised: November 29, 2010 - Product: Aircraft, Glider - Certification basis: CAR 5 - Registered aircraft: 17, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/cc/00/cc008fb9a9fb5724c19033eb74284f8dc590a6ae38b5bb13cb3c7dc3a3fb6c9f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DD6BF6B16D984E048625780E006571BD.0001 - Page: https://openairdocs.org/tcds/G-17 ## Models (2) As the data sheet lists them. - SGU-1-19 - SGU-1-19A ## 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 - DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION G-17 Revision 2 K & L Soaring, LLC SGU-1-19 SGU-1-19A November 29, 2010 GLIDER SPECIFICATION NO. G-17 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 - Models SGU-1-19 or SGU-1-19A 1 PCLM, Approved June 19, 1946 and August 19, 1946 respect. (Gliders assembled from kit designated SGU-1-19A) Type Class II Airspeed limits Glide or dive 75 mph True Ind. Airplane tow 75 mph True Ind. Auto-winch tow 60 mph True Ind. Spoilers extended 75 mph True Ind. C.G. range (+14) to (+19) Maximum weight 550 lbs. No. seats 1 (at -8 or -11.5 or -15 adjustable) Baggage None Control surface Movements Elevator Up 20° Down 22° Rudder Right 30° Left 30° Aileron Right 38° Down 18° Spoilers Up 75° Down 0° Serial Nos. eligible 2 and up Required equipment Items 201, 401 Specifications Pertinent to All Models Datum Wing leading edge at root Leveling means Top of upper longeron aft of wing Certification basis Glider Type Certificate No. 17 (CAR 5) Production basis None G-17 2 ______________________________________________________________________________________________________ Equipment: A plus (+) or minus (-) sign preceding the we ight of an item indicates net weight change when that item is installed. Landing Gear 201. 6.00-6 wheel (Goodyear L6MBD) with 6.00-6 4 ply tire 13 lbs. (+21) 202. Goodyear disc brake 4 lbs. (+21) 203. Schweizer circumferential brake 1 lb. (+12) Interior Equipment 401. Airspeed indicator Neglect weight. 402. Cockpit visor Neglect weight. NOTE 1. Each glider assembled from a kit is designated M odel SGU-1-19A and will be eligible for an airworthiness certificate when accompanied by an affidavit to th e effect that the glider is constructed in exact accordance with the approved drawings and that the parts and materials furnished in the kit have been used, and further, wh en the following inspections have been satisfactorily passed: (a) An inspection for workmanship, materials, and conformity before any covering, metal priming or final finish is applied. All woodwork may be sealed. (b) A final inspection of the completed glider. (c) Check of flight characteristics. Two types of kits are covere d by the above note as follows: Kit No. 1: Includes all materials, all metal fittings, complete fuselage and tail surfaces, complete plans and instructions. Wing ribs and ailerons are to be fabricated from material supplied with the kit. Kit No. 2: Same as Kit No. 1 except that wood mate rial for wing ribs and ailerons and finishing material (fabric, primer, done) not included with kit. NOTE 2. Suitable placards to cover the various pilot weights a nd seats positions must be installed in full view of the pilot as determined from the manufact urer's weight and balance report. NOTE 3. The following placard must be installed in full view of the pilot: "Instrument flight prohibited." ...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 SGU-1-19](https://openairdocs.org/model/schweizer-sgu-1-19): 16 aircraft (registry code 8050502) - [Schweizer SGU-1-19A](https://openairdocs.org/model/schweizer-sgu-1-19a): 1 aircraft (registry code 8050504) ## STCs approved under this data sheet (6) - [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 SA1351WE](https://openairdocs.org/stc/SA1351WE): Replace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12). Ceconite Inc - [STC SG10WE](https://openairdocs.org/stc/SG10WE): Replace existing fabric on wings, fuselage, empennage, and/or control surfaces with Ceconite103 material.. Ceconite Inc - [STC SG4-1240](https://openairdocs.org/stc/SG4-1240): Installation of Eonnex cover on aircraft surfaces.. Ceconite, Inc - [STC SG7WE](https://openairdocs.org/stc/SG7WE): Ceconite 101 covering of complete airframe.. Cooper Engineering Corporation --- 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.