TCDS GTC 13

MODELS: Sailplane (Formerly Briegleb) BG-8 Glider (Army XTG-13), 2 PCIM I.C. NUMBER: GTC 13 (Approved 12/31/42) Airspeed limits Glide or dive - 90 mph True Ind. Airplane tow - 90 mph True Ind. Spoilers extended - 90 mph True Ind. Auto-winch tow - 60 mph True Ind. C.G. range (+20.5) to (+22.7) (See NOTE 1) Datum Leveling means longeron of rear cockpit left side 78 and 105) Maximum weight No. seats 2 (one at (-16) and one at (+31)) Baggage Control surface Up 90 degrees Down 0 degrees movements Up 15 degrees Down 23 degrees Elevator tab Up 23 degrees Dowr. 7 degrees Stabilizer 24 degrees right 13 degrees Down 7 degrees Rudder tab 19 degrees right 19 degrees left Serial numbers eligible 801 and up (See NOIE A) Required equipment Items 200 MODELS: Certification basis Glider Type Certificate No. 13 (CAR 5) Production basis None (See NOTE A) EQUIPMENT: Landing Gear and Floats 200. 6-inch wheel (General C-1569) with 14 inch by 4-ply tire 10 1bs. (+15) 201. Brake - Briegleb Drawing 8-3301 5 1bs. (+15) Interior Equipment Airspeed indicator and pitot 1 1b. (-47) Miscellaneous extra instruments not to exceed Front panel 6 1ks. (-45) Rear panel 6 1bs. (+5) covering Metal prising or final fish je age. i wooots; An inspection for covering, metal priming or final finish is applied. may be varnished. A final inspection of the completed glider. flight characteristics including spin ard stability tests at rear C.G. and trim at forward c.s. Weight ard balance report including list of equipment inciuded ir the certificated weight empty must be submittej for each glider with origiral inspector's report and each subsequent report covering change in equipment. The following placard, as determined by the weight and balance report, must te installed in full view of the pilot: Solo - Use Front Seat Only - 60 1bs. ballast in rear seat Minimum Weight, Pilot and Parachute --- 1hs. Dual - Front Seat - Minimum Weight occupant and Parachute Rear Seat - Maximum Weight Occupant and Parachute Maximum weight