TCDS H-1

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION H-1 Revision 42 Scotts – Bell 47 47 47B 47B3 47D 47D1 47E 47G 47G-2 47H-1 June 3, 2010 HELICOPTER SPECIFICATION NO. H-1 This data sheet which is part of Type Certificate No. H-1 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder Scotts-Bell 47 Inc. 780 S Elmwood Ave Le Sueur, Minnesota 56058-2169 Type Certificate Holder Record Bell Helicopter Textron Inc. transferred TC H-1 to Scotts-Bell 47 Inc. on June 3, 2010. I. Model 47 Approved May 8, 1946 Serial Nos. eligible 1 through 9 II. Model 47B, 2 PCL-SH, Approved November 4, 1947; Models 47B2, Deleted June 15, 1950; (See NOTE 8 for Float Information) Engine Aircooled Motors Franklin 6V4- 178-B3 (Becomes 6V4-178-B32 with Item 119) Fuel 80 minimum octane aviation gasoline Engine limits Maximu m r.p.m. 3000 (178 hp.) Carburetor Marvel MA4-5 Rotor limits & operational Power On (Engine Tach.) Power Off (Rotor Tach.) engine speeds Maximum 3000 Maximum 350 Minimum 2800 (S.L.) Minimum 285 Airspeed limits Never exceeds speed 92 m.p.h. (80 knots) True Ind. C.G. range (-2.0) to (+2.9) Empty weight C.G. range See Figure H-1 Page 2 of 24 II – Model 47B (cont’d) 1514 1518 1522 1526 1530 1534 1538 5.38 .42 .46 .50 .54 .58 .62 .66 FWD LIMIT AFT LIMIT Inches Aft of Datum Empty Weight Pounds (In order to maintain empty weight C.G. l i m i t s ,u pt o2 5l b s .o f fixed ballast can be added in forward baggage compartment (Sta. -68) in addition to the maximum capacity 30 lb.) MODEL 47B (without floats) Maximum weight 2200 lb. No. of seats 2 (Pilot and passenger) (-32) Maximum baggage Aft compartment 40 lb. (+43); Fwd. compartment 30 lb. (-68) Fuel capacity 33 gal. (24 gal. at +25), (9 gal. at -24) Oil capacity 3 gal. (+12), (including 1 gal. unusable) Control movements (Tolerances +1/2°) Swashplate travels for Stick Position Swashplate Angle from Level cyclic pitch for basic Full forward 9° Down and forward configuration (for other Full aft 9° Down and aft configs., see appl. Bell Full left 8° Down and aft Dwg. & Serv. instr.) Full right 6° Down and right Collective pitch Blade average pitch settings; High 10°, low 1/2° Anti-torque rotor pitch - Measured at tip; Hi gh +10-1/2° to +12-1/2°, low -8-1/2° to -9° Serial Nos. eligible 2 and up Required equipment In addition to the pertinent require d basic equipment specified in CAR 6, the following items of equipment must be installed (see section titled “DATA PERTINENT TO ALL MODELS” following section VIII): 2, 3(b), 5, 6, 110, 112, 113(a), 114, 117, 130, 135, 202(1), 203, 204, 205, 213, 305, 306(a), 402. III. Model 47B3, 2 POLH, Approved July 2, 1948; Model 47D, 2 PO-CLH, Approved February 25, 1948 2 PO-CLH, Approved November 18, 1948 ; (See NOTE 8 for Float Information) Model 47B3 is similar to the Model 47B except for revised cockpit enclosure and furnishings, engine compartment fairings and cowling, and other miscellaneous items. Model 47D is similar to the Model 47B3 except for revised cockpit enclosure, revised wheel installation incorporating brakes, 24 volt electrical system, and minor changes to the fuel system and cowling. Engine Aircooled Motors Franklin 6V4- 178-B32 (See Item 137 for optional engines) Fuel 80 minimum octane aviation gasoline Engine limits Maximu m r.p.m. 3000 (178 hp.) Carburetor Marvel MA4-5 Rotor limits & operational Power On (E ngine Tach.) Power Off (Rotor Tach.) engine speeds Maximum 3000 Maximum 350 Minimum 2800 (S.L.) Minimum 285 Airspeed limits Never exceed speed 92 m.p.h. (80 knots) True Ind. C.G. range (-2.0) to (+2.9) Empty weight C.G. range None Maximum weight 2200 lb. No. of seats 2 (Pilot and passenger) (-32) Maximum baggage 40 lb. (+43), Models 47D, 47D (Floats) None, Models 47B3 (all c onfigurations), 47D (Litters) Fuel capacity 33 gal. (24 at +25), (9 at -24) Oil capacity 3 gal. (+5) (including 1 gal. unusable) H-1 Page 3 of 24 III – Model 47B3 & Model 47D (cont’d) Control movements (Tolerance +1/2°) Swashplate travels for Stick Position Swashplate Angle from Level cyclic pitch for basic Full forward 9° Down and forward configuration (for other Full aft 9° Down and aft configs., see appl. Bell Full left 8° Down and aft Dwg. & Serv. instr.) Full right 6° Down and right Collective pitch Blade average pitch settings: High 11°, low 1/2° Anti-torque rotor pitch - Measured at tip: Hi gh +10-1/2° to +12-1/2°, low -8-1/2° to -9° Serial Nos. eligible Model 47B3: 29 and up. Model 47D: 1 and up. Required equipment In addition to the pertinent require d basic equipment specified in CAR 6, the following items of equipment must be installed (see section titled “DATA PERTINENT TO ALL MODELS” following section VIII): Model 47B3: 2, 3(b), 5, 6, 112, 113, 114, 118, 119, 130, 135, 202(a), 203, 204, 205, 213, 305, 306(b), 404. Model 47D: 2, 3(b), 5, 6, 112, 118, 119, 121, 122, 130, 135, 202(b), 203, 208, 209, 213, 313, 314, 407. IV - Model 47D1, 3 PCLH, Approved March 29, 1949; (See NOTE 8 for Float Information) Model 47D1 is similar to Model 47D, except for three-place seating arrangement, revised cockpit enclosure, gravity type fuel system, addition of ventral fin-fixed tab combination, main rotor counterweights, roller-bearing type transmission, movable battery, and elimination of cowling and tail boom covering. Engine Aircooled Motors Franklin 6V4- 178-B32 (See Item 137 for optional engines) Fuel 80 minimum octane aviation gasoline Engine limits Maximu m r.p.m. 3000 (178 hp.) Carburetor Marvel MA4-5 Rotor limits & operational Power On (Engine Tach.) Power Off (Rotor Tach.) engine speeds Maximum 3000 Maximum 350 Minimum 2800 (S.L.) Minimum 285 Airspeed limits Never exceed speed 95 m.p.h. (80 knots) True Ind. C.G. range (-2.0) to (+2.9) Empty weight C.G. range See Figure 3.4 .6 .8 4.0 .2 .4 .6 1320 1360 1400 1440 1480 FWD LIMIT AFT LIMIT Empty Weight Pounds Inches Aft of Datum (In order to maintain empty weight C.G. limits, fixed ballast may be added at Sta. -62 and +210 as required.) Maximum weight 2200 lbs. No. of seats 3 (Pilot and 2 passengers) (-30) Maximum baggage none Fuel capacity 29 gal. (+24) Oil capacity 3 gal. (+5), (including 1 gal. unusable) Control movements (Tolerance +1/2°) Swashplate travels for Stick Position Swashplate Angle from Level H-1 Page 4 of 24 IV – Model 47D1 (cont’d) cyclic pitch for basic Full forward 9° Down and forward configuration (for other Full aft 9° Down and aft configs., see appl. Bell Full left 7 1/2° Down and aft Dwg. & Serv. instr.) Full right 6 1/2° Down and right Collective pitch Blade average pitch settings; High 11°, low 1/2° Anti-torque rotor pitch - Measured at tip: Hi gh +10-1/2° to +12-1/2°, low -8-1/2° to 9° Serial Nos. eligible 47; 82; 145 and up. Copter s Unlimited Bell 47D, S/N CS-1; Big State Industries, S/N 1001, 1002; Rep-Air S/N 001; Utility C opters, S/N 200; World Wide Helicopters S/N 15 and 57; Agrotors, Inc. S/N 895; Rebel Rotors S/N B-101-R and B-109-R; Kitz Kopters, S/N T-121, T-122, T-123, and B-110-R; Cavalier Helicopter Corp., S/N CH-2004; Nat'l Helicopter Serv. & E ngr., S/N NH963; Shelby Aero., S/N SA-2; Gulf Coast Helicopters, S/N 1; World Helicopters, Inc., S/N WH5001, WH5003 thru WH5011, and WH5016. Louis Wm. Cottriel 5501, Kitz Kopter, Inc., S/N T558 and T610, and Florida Helicopters, S/N 001, K Copters S/N K732, K853 S/N K6112, Timothy Moriarty, S/N M-1; Houston Helicopter, S/N 101. Action Bell S/N N211 Required equipment In addition to the pertinent require d basic equipment specified in CAR 6, the following items of equipment must be installed (see section titled “DATA PERTINENT TO ALL MODELS” following section VIII): 2, 3(c), 5, 6, 112, 118, 119, 122, 132, 135, 202(b), 203, 208, 209, 213, 313, 314, 410. See Note 13. V - Model 47E, 2 PO-CLH, Approved April 19, 1950. Engine Aircooled Motors Franklin 6V4-200-C32 Fuel 91 minimum octane aviation gasoline Engine limits Maximu m r.p.m. 3100 (200 hp.) Carburetor Marvel MA4-5 Rotor limits & operational Power On (Engi ne Tach.) Power Off (Rotor Tach.) engine speeds Maximum 3100 Maximum 360 Minimum 2900 (S.L.) Minimum 294 Airspeed limits Never exceed 98 m.p.h. (85 knots) True Ind. C.G. range (-2.0) to (+2.9) Empty weight C.G. range None Maximum weight 2350 lbs. No. of seats 2 (Pilot and passenger) (-32) Maximum baggage 40 lbs. (+43) Fuel capacity 33 gal. (24 at +25), (9 at -24) Oil capacity 3 gal. (+5) (including 1 gal. unusable) Control movements (Tolerance +1/2°) Swashplate travels for Stick Position Swashplate Angle from Level cyclic pitch for basic Full forward 9° Down and forward configuration (for other Full aft 9° Down and aft configs., see appl. Bell Full left 7 1/2° Down and aft Dwg. & Serv. instr.) Full right 6 1/2° Down and right Collective pitch Blade average pitch settings: High 11°, low 1/2° Anti-torque rotor pitch - Measured at tip: Hi gh +10-1/2° to +12-1/2°, low -8-1/2° to -9° Serial Nos. eligible 165 thru 173 Required equipment In addition to the pertinent require d basic equipment specified in CAR 6, the following items of equipment must be installed (see section titled “DATA PERTINENT TO ALL MODELS” following section VIII): 2(a), 3(c), 5, 6, 112, 118, 119, 122, 132, 134, 135, 202(b), 203, 208, 209, 213, 323, 328, 413. VI - Model 47G, 3 PCLH, Approved June 19, 1953. Model 47G is similar to the Model 47D1, except for saddle type fuel tanks, new and relocated battery, synchronized elevator, electrical system, ventral fin, tail rotor gear box and other minor items. Engine Aircooled Motors Franklin 6V4-200-C32 Fuel 91 minimum octane aviation gasoline H-1 Page 5 of 24 VI – Model 47G (cont’d) Engine limits Maximu m r.p.m. 3100 (200 hp.) Carburetor Marvel MA4-5 Rotor limits & operational Power On (Engine Tach.) Power Off (Rotor Tach .) engine speeds Maximum 3100 Maximum 360 Minimum 2900 (S.L.) Minimum 294 Airspeed limits Never exceed 100 m.p.h. (87 knots) True Ind. (Large Area Synchronized Elevator) 90 m.p.h. (78 knots) True Ind. (Small Area Synchronized Elevator) C.G. range (-3.0) to (+4.0) Empty weight C.G. range See Figure 1400 1420 1440 1460 1480 1500 6.8 7.0 7.2 7.4 7.6 Empty Weight Pounds Inches Aft of Datum FWD LIMIT AFT LIMIT Maximum weight 2350 lb. No. of seats 3 (Pilot and 2 passengers) (-30) Maximum baggage none Fuel capacity 43 gal. (+5) Oil capacity 3 gal. (+5), (including 1 gal. unusable) Control movements (Tolerance +1/2°) Swashplate travels for Stick Position Swashplate Angle from Level cyclic pitch for basic Full forward 9° Down and forward configuration (for other Full aft 9° Down and aft configs., see appl. Bell Full left 7 1/2° Down and aft Dwg. & Serv. instr.) Full right 6 1/2° Down and right Synchronous elevator Stick Position Synchr onous Elevator Angle of Chord from Level travels for cyclic pitch Full forward Leading edge up 14° +1/2° (Cable tension 25 lb.+5 lb.) Full aft Leading edge down 27° +3° with min. travel of 37 1/2° Collective pitch Blade average pitch settings: High 11°, low 1/2° Anti-torque rotor pitch - Measured at tip: Metal blades - High +12-1/2° to +13-1/2°, low -10-1/2° to 11-1/2° (See S.I. 438) Wood blades - High +8-1/2° to +10-1/2° to -11° Serial Nos. eligible 7; 295; 604; 666 and up; Continen tal Copters El Tomcat Mark II, S/N 1 thru 4 and 9, See Note 11; Continental Copters, S/N CCI-163, CCI-263, CCI-463, CCI-563, CCI-69-1; World Wide Helicopters, S/N 1209; Carson, S/N C5001 thru C5012, C5015; A.L. Hicks, CD-1, S/N 1; Shelby Aero , S/N SA3; Wiggins Airways, S/N 665-1; Agrotors, Inc., S/N 19; Gulf Coast Helic opters, S/N 2GC; Monahan, S/N 208; Carson Helicopters, Inc. C5016, C5018 and K C opters, S/N K651; Versatile, S/N 27; March Associates, S/N 5503; Versatile, S/N VH-2. Required equipment In addition to the pertinent require d basic equipment specified in CAR 6, the following items of equipment must be installed (see section titled “DATA PERTINENT TO ALL MODELS” following section VIII): 2, 3(c), 5, 6(b), 118, 129, 120(a), 132, 135, 215(a), 323, 328(a) or (b), 417. H-1 Page 6 of 24 VII - Model 47G-2, 3 PCLH, Approved January 20, 1955. Model 47G-2 is similar to the 47G except for the installation of the Lycoming Model VO-435-A1A engine and the relocation of the fore, aft, and lateral cyclic hydraulic boost controls and installation of Lock and Load valves. Engine Lycoming VO-435-A1A, VO- 435-A1B, VO-435-A1D, VO-435-A1E or VO-435-A1F Fuel 80 minimum octane aviation gasoline Engine limits Maximu m r.p.m. 3100 (200 hp.) Carburetor & carb. settings Marvel MA4-5 (setting #10-3856) Rotor limits & operational Power On (Engi ne Tach.) Power Off (Rotor Tach.) engine speeds Maximum 3100 Maximum 360 Minimum 2900 (S.L.) Minimum 294 Airspeed limits Never exceed 100 m.p.h. (87 knots) True Ind. C.G. range (-3.0) to (+4.0) Empty weight C.G. range See Figure 1550 1570 1590 1610 1630 1650 5.9 6.1 6.3 6.5 6.7 Empty Weight Pounds Inches Aft of Datum FWD LIMIT AFT LIMIT 6.9 Maximum weight 2450 lb. No. of seats 3 (Pilot and 2 passengers) (-30) Maximum baggage none Fuel capacity 43 gal. (+5) Oil capacity 3.5 gal. (+26.5) ( 1.5 gal. unusable) Control movements (Tolerance +1/2°) Swashplate travels for Stick Position Swashplate Angle from Level cyclic pitch for basic Full forward 9° Down and forward configuration (for other Full aft 9° Down and aft configs., see appl. Bell Full left 7 1/2° Down and left Dwg. & Serv. instr.) Full right 6 1/2° Down and right Synchronous elevator Stick Position Synchr onous Elevator Angle of Chord from Level travels for cyclic pitch Full forward Leading edge up 14° +1/2° (Cable tension 25 lb. Full aft Leadi ng edge down 27° +3° with min. travel +5 lb.) of 37 1/2° Collective pitch Blade average pitch settings: High 11°, low 1/2° Anti-torque rotor pitch - Measured at tip: Hi gh +12 1/2° to +13-1/2°, low - 10 1/2° to 11 1/2° (See S.I. 438) Serial Nos. eligible 1342 and up, Scarbor ough G-21, S/N 1. Campbell CH-G2 S/N 1, Petroleum Helicopters, Inc. S/ N 52, 491, 1282, Ronald Rogers, S/N RR-100, and Durkee Skeetercopter, Model DGH, S/N V-1. Continental Copters, S/N CCI-165 and CCI-101. K Copters, S/N K821, Ballew and Briggs S/N BB 2383, Action Bell, S/N M210. Required equipment In addition to the pertinent required basic equipment specified in CAR 6, the following items of equipment must be installed (see section titled “DATA PERTINENT TO ALL MOD ELS” following section VIII): 2(b), 3(c), 5, 6(b), 120(a), 132, 139, 140, 215(a), 323, 328(b), 418. H-1 Page 7 of 24 VIII - Model 47H-1, 3 PCLH, Approved March 21, 1955. Model 47H-1 is similar to the 47G, except for semi-monocoupe tail boom, increased cabin width, contour fuel tanks, revised skid type landing gear, addition of baggage compartment. Engine Aircooled Motors Franklin 6V 4-200-C32 (See Item 137(b) for opt. eng.) Fuel 91 minimum octane aviation gasoline Engine limits Maximu m r.p.m. 3100 (200 hp.) Carburetor Marvel MA4-5 Rotor limits & operational Power On (Engine Tach.) Power Off (Rotor Tach.) engine speeds Maximum 3100 Maximum 360 Minimum 2900 (S.L.) Minimum 294 Airspeed limits Never exceed 100 m.p.h. (87 knots) True Ind. C.G. range (+81.5) to (+88.0) Empty weight C.G. range See Figure FWD LIMIT AFT LIMIT Empty Weight Pounds Inches Aft of Datum 8 9 . 5 . 6. 7. 8. 99 0 . 1. 2 1470 1480 1490 1500 1510 1520 1530 1540 1550 1560 1570 MODEL 47H-1 In order to maintain empty weight C.G. limits fixed ballast may be added at Sta. +6 and +282 as required. Maximum weight 2350 lbs. No. of seats 3 (Pilot and 2 passengers) (+56.5) Maximum baggage 200 lbs. Fuel capacity 35 gals. (+95) Oil capacity 2.7 gals. (+90) (including 0.7 gal. unusable) Control movements (Tolerance +1/2°) Swashplate travels for Stick Position Swashplate Angle from Level cyclic pitch for basic Full forward 9° Down and forward configuration (for other Full aft 9° Down and aft configs., see appl. Bell Full left 7° Down and left Dwg. & Serv. instr.) Full right 7° Down and right Synchronous elevator Stick Position Synchr onous Elevator Angle of Chord from Level travels for cyclic pitch Full forward Leading edge down 0° + 2° (Cable tension 30 lb. Full aft Leading edge down 26° + 28° +35 lb.) Collective pitch Blade average pitch settings: High 11°, low 1/2° Anti-torque rotor pitch - Measured at tip: High +12-1/2° to +13-1/2°, low -10-1/2° to 11-1/2° Serial Nos. eligible 1347 and up. (See NOTE 12 on S/N's 1368 and 1370.) H-1 Page 8 of 24 VIII - Model 47H-1 (cont’d) Required equipment In addition to the pertinent required basic equipment specified in CAR 6, the following items of equipment must be installed (see section titled “DATA PERTINENT TO ALL MOD ELS” following section VIII): 2(b), 3(c), 5, 6(b), 118, 120(b), 129, 132, 140, 215(b), 323, 328(a) or (b), 419. DATA PERTINENT TO ALL MODELS Datum All models except Model 47H-1: Station 0; Centerline of weld cluster just forward of leveling lugs (weld cluster approximate ly 2 in. forward of centerline mast) Model 47H-1: Station 0; 82 in. forward of centerline of weld cluster just forward of leveling lugs (weld cluster approximately 5 in. forward of centerline mast) Leveling means Leveling lugs lower left-hand longeron aft of mast and adjacent cross tube Certification basis Type Certificate No. H-1 (CAR 6, effective May 24, 1946) (structural loading cond. skid) Landing Gear dated 11-12-74) Production basis None. See Note 15 for serial numbers produced under Bell Helicopter Textron Inc. Production Certificate No. 100 Equipment: A plus (+) or minus (-) sign preceding th e weight of an item indicates the net weight change when that item is installed. "- -" indicates "same as preceding model." "—" indicates "does not apply." An E. indicates eligible. An N.E. indicates not eligible. The first number under a mode l indicates weight in pounds. The second number indicates location. Rotors & Rotor Equipment 47B 47B3 47D 47D1 47E 47G 47G-2 47H-1 1. (a) Wood main blades Bell 47-110-120 E. - - - - - - - - - - - - - - (b) Metal main blades — — — — — — E. — Bell 47-110-250 2. (a) Tail rotor wood Bell 47-642-020 N.E. - - - - - - - - - - — — (b) Tail rotor metal E. - - - - - - - - - - - - - - Bell 47-642-102 Eligible as indicated in Bell Serv. Instr. 185SI 3. 2 Stabilizer Bar Dampners (a) Deleted (b) Houde Mfg. Co. A12141 4 (+2) - - - - — — — — (c) Houde Mfg. Co. A13965 4 (+2) - - - - - - - - - - - - 4 (+87) 4. Deleted 5. 2 Main rotor counter- Use act. - - - - - - - - - - - - - - weights wt. ch. (a) Bell Dw. 47-110- 120 installed in accordance with Bell Serv. Instr. 117SI 6. Main rotor hub (a) Bell 47-120-164 N.E. - - - - - - - - — — — (Alum. alloy yoke) (b) Bell 47-120-184 75 (+2) - - - - - - - - - - - - 75 (+87) (Steel yoke) 7. Deleted 8. Metal Main Rotor Blades Bell 47-706- 590 Serv. Inst. 320SI — — — — — — 3 (0) — H-1 Page 9 of 24 Rotors & Rotor Equipment (cont’d) 47B 47B3 47D 47D1 47E 47G 47G-2 47H-1 9. Tail Rotor Blade 47-642-117 S.I. 438 Use act Use act wt. chg. wt. chg. Engine and Engine Accessories - Fuel and Oil Systems Starter 110. Delco-Remy 1109659 16 (-4) — — — — — — — 111. Deleted, included in Item 119 119. Delco-Remy 1109661 +2 (-4) - - - - - - - - __ __ __ 129. Delco-Remy 1109662 __ __ __ 17 (-4) - - - - __ 17 (+80) 139. Eclipse-Pioneer 756-22C __ __ __ __ __ __ 19 (+4) __ Oil Cooler 112. Clifford E-36778 12 (+8.5) 12 (-12) 12 (-9) - - - - — — — 120. (a) Harrison 8520470 — — — 9 (-8) — 9 (-8) - - — (oil cooler valve in- cluded with this cooler) (b) Bell 47-671-025 — — — — — — — 5 (+81) Oil Cooler Valve 114. United Aircraft 3 (+7) 3 (-12) __ __ __ __ __ __ UA32257V 122. Clifford U3225V DUB __ __ 2 (-12) 2 (-9) 2 (-12) __ __ __ 131. Deleted Auxiliary Fuel Pump 113. (a) Auto pulse 6V521 6 (-12) - - __ __ __ __ __ __ (b) Auto pulse 12V511 No wt. ch. - - __ __ __ __ __ __ 121. Weldon 4013A __ __ 3 (-12.5) __ __ __ __ __ 134. Weldon 4013C __ __ __ __ 3 (-16) __ __ __ 2 Fan Belts 115. Deleted, included in Item 130 123. Deleted, included in Item 130 130. Bell 47-661-026 1 (-9) - - - - __ __ __ __ __ 132. Bell 47-661-041 __ __ __ No wt. ch. - - - - - - - - Fuel Filter and Drain - Deleted Oil Filter 117. Air Maze B15358 1 (0) __ __ __ __ __ __ __ 118. Air Maze 02S07 __ 1 (+7) - - - - - - - - __ 1 (+93) 125. Deleted, included in Item 118 128. Fram PB-5 (Fram 3 (+24) __ __ __ __ __ __ __ Inst. Dwg. 61974) Muffler 126. Bell 47-706-023 in- 5 (+14) - - - - __ __ __ __ __ stalled in accordance with Serv. Bull. 47011 Carburetor Air Filter 127. Deleted 140. Purolator 51845 __ __ __ __ __ __ 1 (+100) - - Bell Kit No. 47-2883-2, installed in accordance with Bell Service Instruction 235SI. H-1 Page 10 of 24 Carburetor Air Filter (cont’d) 47B 47B3 47D 47D1 47E 47G 47G-2 47H-1 135. Air Maze 13218 1 (-10) - - - - - - - - - - __ __ 136. Deleted Engine 137. (a) Aircooled Motors __ __ Use act ual weight Ch. Std. Std. __ Std. Franklin 6V4-200-C32 (62SI) (150SI) inst. in accordance with Bell Dwg. 47- 706-061 and Serv. Instr. indicated. The same limitations on fuel, eng. limits, rotor limits & operational engine speeds, & max. wt. listed under Model 47E are applicable when this engine installed. (b) Aircooled Motors __ __ __ __ __ __ __ Use Franklin 6V-335-A per actual Bell Dwg. 47-600-025. weight Engine Limits - 3100 r.p.m. (200 hp.) 28.0" Hg. for all operations. Cooling Fan Assy., P/N 47-661-037-13, & Flight Manual Supplement dated July 15, 1957 required. When floats (Item 207(3)) are installed Flight Manual Supplement dated Oct. 6, 1959, required. Winterization Cowlings 138. (a) Bell 47-340-172 __ __ __ 37 (+3) __ __ __ __ Inst. in accordance with Serv. Instr. 83SI. Sup- plemental pages are re- quired in Flight Manual. (b) Bell 47-340-175 __ __ __ __ __ 37 (+9) __ __ Inst. in accordance with or 40 (+10) Serv. Instr. 189SI. Sup- plemental pages are re- quired in Flight Manual. Landing Gear 2 Main Wheels & Brakes 204. 12.50, Type I, Wheel 4 (+47) - - __ __ __ __ __ __ Assy. Goodrich (For- merly Hayes) No. D-3-46M 208. 5.00-6, Type III, Wheel- brake Assy. Goodyear Model L5HBM (Total assy. wt. shown opposite resp. brake) H-1 Page 11 of 24 2 Main Wheels & Brakes (cont’d) 47B 47B3 47D 47D1 47E 47G 47G-2 47H-1 208. (cont’d) Wheel Assy. No. 9520265 Brake Assy. No.: 9520264 7 (+47) - - - - - - - - __ __ __ 9520425 __ __ __ __ -3 (+47) __ __ __ 9520908 __ __ No wt. ch. - - __ __ __ __ For Models 47B & 47B3 install in accordance with Bell 47-726-023 & Serv. Instr. 40SI. 211. Deleted, included in Item 208. 214. Deleted, included in Item 208. 2 Main Wheel Tires 202. (a) 12.50, Type I. 10 (+47) - - __ __ __ __ __ __ 4-ply rating, with regular tubes (b) 5.00-5, Type III, 3 (+47) - - - - - - - - __ __ __ 4-ply rating, with regular tubes 2 Front Wheels, 12.50, Type I 205. Goodrich (Formerly 4 (-42 1/2) - - - - - - - - __ __ __ Hayes) Wheel Assy. D-3-79-M) 209. (a) General Wheel __ __ No wt. ch. - - - - __ __ __ Assy. VG-1250-1 (b) Deleted, identical to Item 205. (c) General Wheel __ __ No wt. ch. - - - - __ __ __ Assy. 204A42 (d) Firestone Wheel __ __ No wt. ch. - - - - __ __ __ Assy. C0200FM 2 Front Wheel Tires 203. 12.50, Type I, 4-ply 10 (-42 1/2) - - - - - - - - __ __ __ rating, with reg. tubes 2 Shimmy Dampeners 206. (Deleted, included 210. (in Item 213. 213. Bell 47-518-001 4 (-47) - - - - - - - - __ __ __ Use actual weight for all float k its except those listed under Item 207(4) 2 Floats 207. (a) Air Cruiser Model 2199 (b) Air Cruiser Model 2383 (c) Goodyear Model SK106-409