TCDS TC 611

MODELS: Rankin, Porterfield 35W and 75-C, 2 PCIM I.C. NUMBER: 611 I - SPECIFICATIONS PERTINENT TO ALL MODELS: No. passengers 1 (+11) Or (+41) (See NOTE 3) Standard weight 1326 1bs. Specification basis Type Certificate No. 611 (Aero. Bulletin 7A requirements) EQUIPMENT: (Datum is wing leading edge) (* Means net increase) Class I: 35W 75-C 101- Engine speed ring (See NOTE 2) 9 1bs. 102. Wheels (a) 18x8-3 (Goodyear 3LMBM) with brakes and tires 33 1bs. (-8) (k) 6.00-6 (Shinn 6C5HB) with brakes and 4-ply tires (wheels must be placarded 103. Tail skid for these tires) 3 1bs. 32 1bs. (-7) 104. Propeller - fixed pitch wood (with hub) 20 1ts. 15 1bs. (-55) 105. Two exhaust manifolds and carburetor heater 11 1bs. (-42) 106. 6x2.00 steerable tail wheel with special spring 10 IDS. (+1/0) 107. Oil radiator (Continental) 6 Ibs. (-46) Class II: 200- Miscellaneous items as noted in approved weight and balance report. 201. Combined exhaust collector and speed ring (See NOTE 2) 202. Propeller, fixed or adjustable metal (See NOTE 2) 29 lbs. 203. Wheel streamlines (a) For 18x8-3 wheels 14 1bs. (-7) (b) For 6.00-6 wheels 12 1bs.(-7) 204. 6.00-6 wheels (Shinn 6C5HB) with brakes and 6.00-6 4-ply tires (wheels must be placarded for these tires) Net decrease 3 1bs. (-8) 205. Battery installation in engine compartment 31 1bs. (-30) 206. Generator, wind-driven under fuselage (Air Assoc. GE-20) 7 1bs. (-8) Class III: 301- Emergency exit No weight change 2 1bs. (+19) 302- Outside baggage door No weight change 303. Miscellaneous extra instruments 7 1bs. (+1) 304. Tail wheels (a) 4 inch diameter solid rubber No weight change (b) 3-1/2 inch diameter solid rubber, castoring No weight change (c) 6×2.00 wheel assembly, castoring 1 1b.*(+189) 305. carpet 2 1bs. (+7) 306. Engine primer 1 1b. (-8) 307- Cabin heater 2 1bs. (-39) 308. Wheel streamlines 10 1bs. (-5) 309. Landing light (left wing) 4 1bs. (+17) 310- Dash light 1 1D. (+ 1) 311. Parking brake 11b. (0) 312. Propeller - Adj. pitch wood - Freedman Burnham PC-203 hub, P-216A blades 14 1bs. (-55) NOTE 1. Eligible for export as follows, subject to inspection for equipment specified in Chapter XII of Inspection Handbook: (a) Canada - Landplane - skiplane - not eligible. (b) All other countries except New Zealand. Model 35W eligible without engine speed ring provided c.G. check is made. Item 202 cannot be installed with engine speed ring (item 101 or part of item 201). NOTE 3. On serials 650, 1651 and up, Model 75-C, the following placard is required unless otherwise substantiated by weight and balance report: "Solo from front seat only." II - MODEL 35W: Engine Warner Scarab Jr. Engine limits For all operations - 2025 rpm (90 hp) Propeller Maximum permissible diameter 80 inches Airspeed limits Level flight or climb - 105 mph True Ind. Glide or dive - 160 mph True Ind. Fuel capacity 18 gallons (one tank in fuselage) (-10) oil capacity 3 gallons (-23) Baggage 30 lbs. (aft of rear seat) (+73) C.G. limits (+6.3) and (+13.9) Serial Numbers 301 and up manufactured prior to 1/8/46 eligible. Approval expired as of that date. III - Model 75-C: Engine Continental A-75-8 Engine limits For all operations - 2600 rpm (75 hp) Propeller Static rpm at maximum permissible throttle setting - Not more than 2350 - Not less than 2350. - Not more than 83 inches - Not less than 68 inches. Airspeed limits Level flight or climb - 105 mph True Ind. Glide or dive - 150 mph True Ind. Fuel capacity 18 gallons (-15) cil capacity Baggage 40 1bs. (+73) C.G. limits (+8.1) and (+16.8) leveling means Use lower side of center section cross tube at rear spar and special 1/4 inch tube at left front Serial Numbers (5gligible. Approval expired as of that date. 1651 and up manufactured prior to 1/8/46