TCDS TC G-2-11

MODEIS_: Schweizer Army IG-3A Glider, 2 PCIM I.C. NUMBER: G-2-11 (Approved 2/27/47) Type Class I or Class II Airspeed limits Glide or dive - 90 mph True Ind. Spoilers open - 90 mph True Ind. Auto-winch tow - 63 mph True Ind. Airplane tow - 90 mph True Inc. C.G. range (+16.5) to (+21.4) Datum Wing leading edge at root Leveling means Lugs on left of fuselage frame, aft of rear cockpit Maximum weight 1100 lbs. as Class I 1200 1bs. as Class II No. seats 2 (1 at -28 and one at +30) Baggage control surface Down 29 degrees movements Elevator trim tab Up 11 degrees Down 19 degrees Aileron Up 31 degrees Down 14 degrees Spoilers (top) Up 90 degrees Down 0 degrees Up 0 degrees Dowr. 82 degrees Right 26 degrees Left 28 degrees Rudder trim tab Right 24 degrees Left 11 degrees Serial numbers eligible Required equipment Items 301, 302, 401 SPECIFICATIONS PERTINENT TO ALL MODELS: Certification basis Airworthiness Certificate only (CAR 5.031) EQUIPMENT: Landing Gear 301. Wheel (Goodyear GH/MBM) 1+27 302- Tire (Goodyear 6.00-6 4-ply) 1+27 Interior Equipment 401- Airspeed indicator (-50) A weight and balance report including a list of equipment included in the certificated empty weight must be submitted for each glider with original inspector's report and each subsequent report covering change in eguipment. Each glider must be weighed to determize its weight and prior to original certification unless satisfactory army weight and balance report is available. Prior to certification as a civil aircraft the following must re Tent, ust be state in view of the pilot? as determined by the weight and balance Solo - Use front seat only - Minimum Weight, Pilot and Parachute (2) Dual - Front Seat - Minimum Weight, Pilot and Parachute Seat - Maximum Weight, occupant and Parachute (b) Rudder and elevator trim tab controls must be marked to indicate direction of rotatior or position of tab. The manufacturer's serial number and the date of conversion to certificated status must be includej on the nameplate. A stop should be installed in the spoiler system in accordance with Figure 1. The airspeed pitot head should be located in accordance with Figure 2. Disconnect electrical system, remove dry batteries and position of light bulbs. 1/- 0.0. = .041 JO TDIM I f so an and tar LOS2Or DOLdiNE .b. . .. 130 TUA2 3/8 0.D. I.058 044-308018 U30 TAIN AC J0S-& Bvt poslar faLlerank- paller ДЕТ ПРОНІЯ STP ТО СІТІ POTLEN: 1 MAIDAN 90 DO HES TEYTICAL DI FLICHT FORITION M28980 2 - 3020r1a1 - (•:1o0d 1Ioc: sonter I.1 2. I-Pec. Chroa. Yoly Sheet S200. 1 2/2° × 1° 1 .041 1-M1 tot Tobo-Typo 8-6 7:1018 122 Arta] Clans - -1/2° (ra t b05) 52 1am Grammet, Aubber PITOT TUBE TTPE I Eolt lowor "1" 1gl0 Jmco . Itot boom to lover radio contr 1/ing trackoe. 3/4° K 22 hoe] (lempo