TCDS TC 711

ROY A. GOOD MODELS: Good (Pigman, feed, American Flyers, Rearwin), 8090, 9125, 8135 (Army UC-102A), 8135T I.C. NUMBER: 711 I - MODEL 909, 2 PCIM (APPrOved 10/17/39) Engine LeBlond 90 5 F (See item 209(a)) Fuel 65 minimum octane aviation gasoline Engine limits For all operations, 225) rpm (90 hp) Airspeed limits Level flight or clinh - 127 mph True Ind. Glide or dive - 152 mph True Ind. Propeller limits Static rpm at maxinum permissible throttle setting - Not more than 2150 - Not less than 2000 more than 96 inches - Not less than 76 inches C.G. range (+13.0) to (+17.5) Maximum weight No. seats Maximum baggage 50 1bs. (+44) Fuel capacity 34 gallons (+10) Oil capacity 2-1/+ gallons (-21) Control surtace Elevator - Up 30 degrees; down 33 degrees movement Rudder - Pight and left 20.5 degrees fron centerline Ailerons - Up 20.75 degrees; down 21.75 degrees Serial numbers eligible 801 and up per NOTE A (See also NOTE 2) Required equipment Items 101, 102, 103, 104, 105 (a) II - MODEL 8125, 2 PCLM (Approved 10/17/39) (Same as 3090 except engine installation) Engine Ken Royce 7F (See Item 208 (b)) Fuel 73 minimum octane aviation gasoline Engine limits For all operations, 2225 Ipm (120 hp) Airspeed limits Level flight or climb - 127 mph Irue Ind. Glide or dive - 170 mph Irue Propeller limits Static rpm at maximun permissible throttle setting - Not less than 1950 - Not more than &f inches - Not less than 76 inches C.G. range (+11.6) to (+15.9) Maximum weight No. seats 2 at (+22) Maximum bajjage 50 1bs. maximum (*44) Fuel capacity 34 gallons (*1?) 011 capacity 3 gallons (-21) Control surface Elevators - Up 30 degrees; down 33 deqrees movement Pudder - Right and left 20.5 degrees from centerline Ailerons = Up 20.75 degrees; down 21.75 degrees Serial numbers eligible and up per NOTE A (see also NOTE 2) Required equipment Items 101, 102, 103, 104, III - Model 9135 (JC-102A), 3 PCIM (Approved 2/27/40) (Same as 8125 except interior arrangement and minor structural changes) Engine Ken Royce 7F (See Item 203(b)) Fuel 73 minimum octane aviation gasoline Engine limits For all operations, 2225 rpm (120 hp) Airspeed limits Level flight or clinb - 127 mph True Ini. Glide or dive - 170 mph True Ind. Propeller limits Static rpn at naxinun permissible throttle setting - Not less than 1950 Dianeter C.G. range (- 9) to 117.9 16 inches Maxinun weight (See NOTE 3) No. seats Maximum baqgage may be increased as follows, to 190 ibs. seat is not occupied (see NOTE Serial numbers 80? and renainder on rear (b) Serial numiers 912 and up - 100 1bs. on rear compartment floor, remainder on rear seat. Fuel capacity 34 gallons (+19) Oil capacity Control surface Elevators - Up 30.5 degrees; down 31.5 degrees Elevator tab - Up 12.5 degrees; down 26.5 degrees Rudder - Right and left 18.5 degrees fron centerline Ailerons - Up 20 degrees; down 20 degrees Serial numbers eligible and up per NOT! 4 and all AAF numbers (see also Required equipment Itens 101, 102, 103 (bl, 104, 105(b) and 106 IV - MODEL 8135T, 2 PCIM (Approved 6/18/41) (Same as 8136 except for seating arrangement, control system, fuel systen and minor structural changes) Engine Ken Royce 7G (See Item 209(c)) Fuel 73 minimum octane aviation gasoline Engine limits For all operations, Airspeed limits Level flight or climb - 127 mph Irue Ind. Glide or dive - 170 nph True Propeller limits Static rpm at maxinun permissible throttle setting more than 2100 - Not less than 1950 Diameter - Not more than 31 inches - Not less than 16 inches C.G. range (+10.9) to (+17.+) Maximum weight 1900 1bs. No. seats 2 (one at _11 and one at +49) Maximum badJage None Fuel capacity 34 gallons (+19) oil capacity 3 gallons (-27) control surface Elevators - up 30.5 degrees; Aown 31.5 degrees movements Flevator tab - up 12.5 degrees; down 26.5 degrees Rudder - right and left 18.5 degrees fron centerline Ailerons - up 20 degrees; down 20 degrees Serial numbers eliqible 877 and up per NOTE Reguired equipment Items 101, 102, 103, 104, 105 (c) and (d) and 105 SPECIFICATIONS PERTINENT TO ALL MODELS: Datum Wing leading edge Leveling means is provided by a spirit level on left door frane accessible zipper on serial numbers 002 and up. Serial numbers 101 and 801 may be leveled by spirit level on propeller nub Certification basis Type Certificate No. 711 (CAR 4a) production basis None (See NOIE A) Export eligibility Eligible for export as follows, subject to provisions as follows, subject to provisions of MOP 2-4: (a) Canada - Landplane - elijible. Skiplane - not eligible. (b) All other countries except New Zealand. * plus (*) or ninus (-) sign preceding weight of an optional iten indicated the net weight change between that iten and the equivalent 8020 9125 2135 81357 Propeller and Propeller Accessories Propeller (fixed pitch) 21 1bs. (-48) (-53) (-53) Engine and Engine Accessories Engine ring Cowl (NAJA) Fuel and Oil System 20 lbs. (-39) carburetor heater (-45) (Eclipse Y-150) 19 1bs. (-25) (-30) (Eclipse Model 4, Type 635) 17 1bs. (-25) (-30) (Champion Model 100) 19 1bs. (-25) (-30) (LeBlond 90 5G) +4 1bs. (-40) (Ken Royce 7G) +3 lbs. (-40) (-45) Model 8135T (-45 (-40) - 45) 1-451 Vacuum pump installation (-21) 214. Oil purolator (does not apply to Model 8090) (=23} Logged oil tank and lines (Drawing 8125147) (Models 8125, 8135 and 8135T only) No weight change Landing Gear and Floats 103. 3-inch wheels (Goodyear 3INBM) 18x8-3 4-ply tires or H.D. tires (wheels be placarded for 4-ply 29 1bs. 8-inch streamline tail wheel and tire (Drawing 84-023) (-189) (+189) (+189) Wheel streamlines (Drawing 74-006) (- 6) (-6) (- 6) 304. 3-inch wheel (Goodyear 3LMBM) with brakes *6 1bs. 1-0 (-6) (-6) 305. Parking brake 1 1b. - 10' (-10 (-10) 306- and tire (Drawing +2 1bs. (+180) (+180) (+180) Electrical and Radio Equipment 201. Battery and box (Exide 6-TS-7-1; 12 volt) 31 1bs. (-19) (+62) (+62) 0I (-23) (b) (Exide 6-TS-13-1; 12 volt) 41 Ibs. (- 19) (-23) (c) (Exide 6-AC-7-1; (-19) (-23) (d) (Exide 3-AC-7-1; 6 volt) (-19) (-23) (e) (Willard SYR-7-6; (+62) (+57) OI (+62) 203. Extra instrument or radio on instrument panel (a) 23 1bs. (0) (0) (b) (Front panel) 36 Ibs. - - (c) (Rear panel) 60 1bs. 209- Radio variable. Weight and location of items should be shown in weight and balance report. The structure has been substantiated for equipment as follows: (a) 11 1bs. under right seat (* 16) (b) 8 1bs. in cabin under cowling (- 12) (c) 6 1bs. under instrument panel (+11) (d) 2 lbs. in roof (+19) (e) 150 lbs. on shelf (See NOTE 5) (+46.5) (£) 20 1bs. on dynamotor support (+35) 0I (+63) 301- Landing lights (a) Grumes ST-250 (s) (+12) (+12) (b) Grimes ST-250 (1) Ibs. (+12) 307- Generator - wind driven (a) (Champion W-128-12 volt) 9 1bs. (+9) (+9) - _ (b) (Lear Type 1030-A with Lear Type 913-A regulator 12 volt) 11 1bs. (-6) (- 6) (* 9) (c) (Champion W-612-6volt) 9 1bs. (+9) (+9) (Champion W-128B-12 volt) 10 1bs. (-5) (-5) (-5) 308. Antenna (a) (Aeronaut antenna reel) 5 lbs. (+21) (+21) (D) (Lear - 10 inch loop) 2 1bs. (*33) (c) (Lear fired antenna) 2 1bs. (+35) (Lear trailing antenna with Lear Junior hand reel INM-603) 3 1bs. (+51) (e) Lear Unihand reel and antenna • 1bs * 14 (f) Belly antenna 2 Ibs. (+30) (+30) (+30) Interior Eguipment 105. Seat cushions (a) 10 lbs. (+26) (b) 25 Ibs. - - (+30) - - (c) (Front) 5 1bs. (+ 11) (₫) (Rear) Ibs. (+40) 206. Parachutes (a) (TWO) 20 Ibs. (+22) (+20) each (b) (Front) 20 1bs. (+ 11) (c) (Rear) 20 ibs. (+48) 207. Flares - three 1-1/2 minutes (International) 16 1bs. (+42) 210- Instrument pane. - rear 4 1bs. - - (+31) 213- Blind flying curtain 2 1bs. - - (+ 38) 303. Cabin heater (Drawing 86-006 Or 86-014) 2 1bs. (-28) (-33) (-32) 311- Cabin ventilator (a) (Firewall type (Drawing 812B168)) 2 lbs. - - (-30) (b) (Floor type) 1 1b. (+62) (c) (30of type - Drawings 812G335 and 812G336) 1 1b. - - (+43) Miscellaneous (not listed above) 204. Fuselage and control system protective covering → Ibs. (+100) (+100) 310. Electric heater pitot NOTE (a) Each aircraft must, prior to original certification, , satisfactorily pass: inspection workmanship, materials conformity priming or final finish is applied. All woodwork maybe varnished A final inspection of the completed aircraft. Check of flight characteristics. Weight and balance report including list f equipment included in certificated weigi empty, ali leadiors instructions when necessar and loading when necessary report covering changes in equipment. ust be submitted for each aircraft wi serial numbers 302, 804 and 805 eligible with firewall moved forward 4 inches, engine mount, ltered windshield contour, seat backs moved forward 2 inches and revised baggage compartment structure. NOTE 3. Serial numbers 819 and up eligible as follows: Maximum weight C.G. range (+10.9) t0 (+17.4) Serial number 818 also eligible the above weight and C.G range, provided that a 1-1/2 .065 streamline axle strut 058 streamline axle strut. NOTE 4. "Full Oil" capacity (model 8135) may be reduced to 1-3/4 gallons to provide for increase in disposable load provided oil tank cap and stock gauge is marked accordingly. NOTE 5. hot exceed 190 let far 20 not is in colleed hen of bitems installe equipment must not exceed 190 Ibs.