TCDS GTC 7

CORCORAN, STANLEY R. MODELS: Concoran (Pormerly Frankfort) Glider B (Army XIG-1, IG-1A, TG-1C, 2 PCLM I-C. NUMBER: GTC 7 (Approved 4/23/42) Type Class I (See NOTE 2 (C) airplane tow - 80 mph: Airspeed limits Glide or dive - 80 mph; (T.I.A.S.) auto-winch tow - 55 mph; spoilers open - 60 mph C. G. range (+1501) to (+2209) (See NOTE 2(b) and (d) Datum Wing leading edge of root Leveling means Level top longeron in forward cockpit for weighing Maximum weight 830 1bs. (See NOTE 2) No. seats 2 (1 at (+26.6) and pilot at (-19.4) Baggage Control Surface Left 32 degrees 90 degrees 0 degrees available Serial Nos. eligible B-2-3 and up per NOTE A and all AAP Nos. (See also Required equipment Items 101, 102 and 103 Specifications Pertinent to All Models: Certification basis Type Certificate No. 7 (CAR 5) Production basis None (See NOTE A) EQUIPMENT: Landing Gear Wheel (General C-1569) with 14h 6-ply 11.0 1bs. (+19) Interior Equipment 101. Airspeed indicator Airspeed pitot • 105 1bs. 202. Extra instruments Front cockpit 1.0 1bs. -31 Rear cockpit 2.5 1bs. (+19 Miscell. neous (maristed above) Mud guard 1.5 1bs. (+19) Prior to original certification, each glider manufactured for civil use must satisfactorily pass: covering, metal priming or finish is applied. All woodwork may be varnished. inspection of the completed glider. Check of flight characteristics. and balance report including list of equipment included in the certificated weight empty must be submitted for each aircraft with original inspector's report and each subsequent report covering change in equipment. The following placard, as determined by the weight report, must be installed in full view of the pilot: Solo - Use Front Seat Only - Minimum Weight, Dual - Front Seat - Minimum Weight, Occupant and Parachute - Rear Seat - Maximum Weight, Occupant and Parachute Serial Nos. B-2-1 is eligible for certification for a maximum Serial Nos. B-1-1, B-1-4 to B-1-8, inclusive, and B-1-10 to B-1-12, inclusive, are eligible for certification with small fin and stabilizer, large rudder and elevator, elevator control system bungee and no spoilers with the folloving restrictions: Maximum weight C.G. range Serial Nos. B-1-2, B-1-3 and B-2-2 are eligible for certification as Class II gliders in accordance with the provisions set forth in with the following placard: Airplane tow Auto-wing tow 55 mph True Ind. Inverted flying prohibited. The above gliders may be certificated as Class I gliders when revised (revisions necessary to D-nose section and to accommodate balanced alleron), balanced type aileron, and balance weights in the elevators, are installed. Serial Nos. B-2-23 and up are eligible for certification vith the following restrictions: Maximum weight (+16-2) to (+21-6)