TCDS A-758

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 Rev No. 23 22 22 22 22 22 22 23 23 22 23 23 Reformatted 2/94. FEDERAL AVIATION ADMINISTRATION A-758 Revision 23 APDC (AAMSA) (AERO COMMANDER) (INTERMOUNTAIN) (CALLAIR) A, A-2, A-3, A-4, A-5, A-5T, A-6, A-7, A- 7T, A-9, A-9B January 1, 1982 AIRCRAFT SPECIFICATION NO. A-758 Type Certificate Holder: Aircraft Parts & Development Corp. P. O. Box 1849 Laredo, Texas 78041 I - Model A, 2 PCLM, Approved July 26, 1944 Engine Lycoming O-235 Fuel 73 min. grade aviation gasoline Engine limits For all operations, 2550 rpm (100 hp) Airspeed limits Level flight or climb 125 mph (109 knots) True Ind. Glide or dive 150 mph (131 knots) True Ind. C.G. range (+12.7) to (+18.0) (See NOTE 2 for serials 2, 3, 4, & 5) Maximum weight 1550 lbs. No. seats 2 (+25.5) Maximum baggage 50 lbs. (+55) Fuel capacity 25 gals. (-6) Oil capacity 2 gals. (-40) Control surface movements Elevator Up 16 degrees Down 25 degrees (See Note 2 for serials Elevator trim tab Up 15 degrees Down 25 degrees 2, 3, 4, 5) Ailerons Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Fixed Serial Nos. eligible 2 to 5 incl. (Also see NOTE 3) Required equipment In addition to the pertinent required basic equipment s pecified in CAR 4a, the following items of equipment must be installed: 1, 101, 201, 202, and 205. II - Model A-2, 2 PCLM, Approved July 31, 1946 (Same as Model A except for revised powerplant installation, elevator tab control installation, and smaller rudder.) Engine Lycoming O-290-A, O-290-B, or 0290-C Fuel 73 minimum aviation gasoline Engine limits For all operations, 2600 rpm (125 hp) Airspeed limits Level flight or climb 125 mph (109 knots) True Ind. Glide or dive 150 mph (131 knots) True Ind. C.G. range (+12.7) to (+18.0) A-758, Rev 22 Page 2 Empty weight C.G. (+14.2) to (+15.6) When the empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for nonstandard arrangements. Maximum weight 1550 lbs. No. seats 2 (+25.5) Maximum baggage 50 lbs. (+55) (See Item 401 for additional baggage) Fuel capacity 25 gals. (-6) Oil capacity 2 gals. (-40) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Ailerons Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Ground adjustable Stabilizer Fixed Serial Nos. eligible 6, 7, 8, 110, 111, 123, 126, 128, 129 (Also see NOTE 3) In addition Required equipment to the pertinent required basic equipment specified in CAR 4a, the following items of equipment must be installed: Items 2, 101, 202, and 205 III - Model A-3, 2 PCLM, Approved June 11, 1947 (Same as Model A-2 except for different powerplant installation, and minor changes.) Engine Continental C125-2 Fuel 73 min. grade aviation gasoline Engine limits For all operations, 2550 rpm (125 hp) Airspeed limits Level flight or climb 125 mph (109 knots) True Ind. Glide or dive 150 mph (131 knots) True Ind. C.G. range (+12.7) to (+18.0) Empty weight C.G. (+14.2) to (+15.6) When the empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for nonstandard arrangements Maximum weight 1550 lbs. No. seats 2 (+25.5) Maximum baggage 50 lbs. (+55) (See Item 401 for additional baggage). Fuel capacity 25 gals. (-6) Oil capacity 2 gals. (-40) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Ailerons Up 21 degrees Down 21 degrees Rudder Right 1 degrees Left 21 degrees Rudder trim tab Ground adjustable Stabilizer Fixed Serial Nos. eligible 109, 112 through 122, 124, 125, 127, (Also See NOTE 3) Required equipment In addition to the pertinent required basic equipment specified in CAR 4a, the following items of equipment must be installed: Items 2, 101, 105, 201, 202, and 205. IV - Model A-4, 2 PCLM, Approved November 15, 1954 (Same as Model A-2 and A-3 except for engine, engine mount, propeller, and associated minor changes.) Engine Lycoming O-290-D2 (See Item 109 for optional engine) Fuel Min. grade 80/87 aviation gasoline Engine limits For all operations, 2600 rpm (135 hp) Airspeed limits Level flight or climb 125 mph (109 knots) True Ind. Glide or dive 150 mph (131 knots) True Ind. C.G. range (+12.7) to (+18.0) Page 3 A-758, Rev 22 Empty weight C.G. (+15.4) to (+17.25) When empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for nonstandard arrangements Maximum weight 1550 lbs. No. seats 2 (+25.5) Maximum baggage 50 lbs. (+55) (See Item 401 for additional baggage). Fuel capacity 25 gals. (-6) (See Item 107 for auxiliary tank) (Optional) Oil capacity 2 gals. (-40) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Ailerons Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Ground adjustable Stabilizer Fixed Serial Nos. eligible 137, 141 through 201, and 203 through 207 (also See NOTE 3) Required equipment In addition to the pertinent required basic equipment specified in CAR 4a, the following items of equipment must be installed: 4, 101, 105(b), 105(c), 108, 201(d), 202(d), and 205(d). V - Model A-5, 1 PO-CLM, (Restricted Category Only), Approved May 19, 1958 (See NOTE 4 for additional limitations) Engine Lycoming O-320-A2A Fuel 80/87 min. grade aviation gasoline Engine limits For all operations, 2700 rpm (150 hp) Airspeed limits Never exceed 135 mph True Ind. C.G. range (+12.7) to (+18.0) Maximum weight 1550 lbs. No. seats 1 (+25.5) Fuel capacity 25 gals. (-6.0) Oil capacity 2 gals. (-38.0) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Aileron Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Ground adjustable Serial Nos. eligible 208 through 243, 245 through 247, 249 through 251, 253 through 261, 266, 267, 272, 274, 275, 277, 278, 280, 283, 286, 290, 291, 292, 301, 302, 304, 305, 309, 310, 312. Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 5, 101, 108, 201(e) or (f), 202(e) or (f), 205(d) or (e), 307(d), 305(b) VI - Model A-5T, 1 PO-CLM, (Restricted Category Only), Approved January 31, 1961 (See NOTE 7 for additional limitations) Engine Lycoming O-320-A2A Fuel 80/87 min. grade aviation gasoline Engine limits For all operations, 2700 rpm (150 hp) Airspeed limits Never exceed 135 mph True Ind. C.G. range (+16.4) to (+18.0) Maximum weight 1550 lbs. No. seats 1 (+25.5) Fuel capacity 25 gals. (-6.0) Oil capacity 2 gals. (-38.0) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Aileron Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Ground adjustable A-758, Rev 22 Page 4 Serial Nos. eligible 303, 315 through 318, 320, 5T-321 and up (U.S. mfg. acft. only) Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 5, 101, 108, 201(e) or (f), 202(e) or (f), 205(d) or (e) VII - Model A-6, 1 PO-CLM, (Restricted Category Only), Approved September 2, 1958 (See NOTE 5 for additional limitations) Engine Lycoming O-360-A1A or -C1A Fuel 91/96 min. grade aviation gasoline Engine limits For all operations, 2700 rpm (180 hp) Airspeed limits Never exceed 135 mph True Ind. C.G. range (+12.7) to (+18.0) Maximum weight 1550 lbs. No. seats 1 (+25.5) Fuel capacity 40 gals. (+26.0) Oil capacity 2 gals. (-39.0) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Aileron trim tab Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Ground adjustable Serial Nos. eligible 202, 244, 248, 252, 262 through 265, 268 through 271, 273, 279, 281, 282, 276, 284, 285, 287 through 289, 29 3 through 295, 297, 298, 300, 307 through 308, 313 Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 6 or 7, 101, 105(d), 105(e) or (f), 108, 201(e) or (f), 202(e) or (f), 205(d) or (e), 305, 307 VIII - Model A-7, 1 POLM, (Restricted Category Only), Approved July 20, 1961 (See NOTE 8 for additional limitations) Engine Gulf Coast Dusting Company W670-240 NOTE: Aircraft is not eligible for waiver to permit operation over congested areas because of uncertificated powerplant components. Fuel 80/87 min. grade aviation gasoline Engine limits Takeoff (2 min.) 2200 rpm (240 hp) Maximum continuous, 1925 rpm (218 hp) Airspeed limits Never exceed 135 mph True Ind. C.G. range (+12.7) to (+18.0) Maximum weight 1550 lbs. No. seats 1 (+25.5) Fuel capacity 20 gals. (+26.0) Oil capacity 4.4 gals. (-4.0) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Aileron Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Ground adjustable Serial Nos. eligible 299, 7-001 and up (U.S. manufactured aircraft only) Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 8 or 9, 101, 105(g) and (h), 201(e) or (f), 202(f), 205(d) or (e) Page 5 A-758, Rev 22 IX - Model A-7T, 1 PO-CLM, (Restricted Category Only), Approved September 21, 1961 (See NOTE 9 for additional limitations) Engine Gulf Coast Dusting Company W670-240 NOTE: Aircraft is not eligible for waiver to permit operation over congested areas because of uncertificated powerplant components. Fuel 80/87 Min. grade aviation gasoline Engine limits Takeoff (2 min.) 2200 rpm (240 hp) Maximum continuous, 1925 rpm (218 hp) Airspeed limits Never exceed 135 mph True Ind. C.G. range (+12.7) to (+18.0) Maximum weight 1900 lbs. No. seats 1 (+25.5) Fuel capacity 40 gals. (+26.0) Oil capacity 4.4 gals. (-4.0) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 15 degrees Down 25 degrees Aileron Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Rudder trim tab Ground adjustable Serial Nos. eligible 311, 7T-001 and up (U.S. manufactured aircraft only) Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 8 or 9, 101, 105(g) and (h), 201(e) or (f), 202(f), 205(d) or (e) X - Model A-9, 1 PL-CLM, (Restricted Category Only), Approved November 9, 1962 Engine Lycoming O-540-B2B5 with carburetor setting No. 10-4404 Fuel 80/87 min. grade aviation gasoline Engine limits 2575 rpm (235 hp) for all operations Airspeed limits Never exceed 135 mph True Ind. C.G. range (+18.0) to (+21.0) Maximum weight 1900 lbs. No. seats 1 (+64.0) Fuel capacity 40 gals. - 2 tanks, 20 gals. each (+26) (See NOTE 1 for unusable fuel) Oil capacity 3 gals. (-35.0) Control surface movements Elevator Up 16 degrees Down 25 degrees Elevator trim tab Up 25 degrees Down 25 degrees Aileron Up 21 degrees Down 21 degrees Rudder Right 21 degrees Left 21 degrees Serial Nos. eligible 1000 through 1125, Nos. 1061 through 1125 are eligible for 3,000 lbs. gross weight. These aircraft may also be certificated as Models A-9A under CAR 3, (Data Sheet A4WE) by complying with FAA approved Aero Commander Report No. 550 dated 6/14/68. Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 10 (or 11, 12, or 14), 105(i), 105(j), or 105(k), 108(c), 201(f), 202(f), 205(e), 305(c) or 306(a) or 306(b), and 307(e) or 307(f) or 307(g) or 307(h) or 307(i). XI - Model A-9, 1 PO-CLM, (Restricted Category Only), with flaps, droop ailerons and wing leading edge change, Approved January 5, 1965 Engine Lycoming O-540-B2B5 with carburetor setting No. 10-4404 Fuel 80/87 min. grade aviation gasoline Engine limits 2575 rpm (235 hp) for all operations A-758, Rev 22 Page 6 Airspeed limits Never exceed 135 mph True Ind. C.G. range (+18.0) to (+21.0) Max. weight 3000 lbs. No. seats 1 (+64.0) Fuel capacity 40 gals. - 2 tanks, 20 gals. each (+ 26) (See NOTE 1 for unusable fuel) Oil capacity 3 gals. (-35.0) Control surface movements Elevator Up 22 degrees Down 25 degrees Elevator trim tab Up 25 degrees Down 25 degrees Aileron (zero flap) Up 20 degrees Down 15 degrees Aileron Droop Down 10½ degrees Flaps Down 24 degrees Rudder Right 21 degrees Left 21 degrees Serial Nos. eligible 1048, 1126 through 1263, 1265 through 1615. These same serial numbered airplanes may also be certificated as Models A-9A, under CAR 3. See Data Sheet A4WE, when modified in accordance with FAA approved Aero Commander Report No. 550 dated 6/14/68. Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 10 (or 11, 12, or 14), 105(i), 105(j), or 105(k), 108(c), 201(f), 202(f), 205(e), 305(c) or 306(a) or 306(b), and 307(e) or 307(f) or 307(g) or 307(h) or 307(i). XII - Model A-9B, 1 PCLM, (Restricted Category Only), Approved December 16, 1966 Engine Lycoming IO-540-G1C5 Engine Limits 2575 RPM (290 hp) for all operations Optional Engine Lycoming IO-540-K1A5 Engine Limits 2700 RPM (300 hp) for all operations (+56 lb.) Fuel 100/130 min. grade aviation gasoline Airspeed limits Never exceed 135 mph True Ind. C.G. range (+18.0) to (+21.0) Maximum weight 3000 lbs. No. seats 1 (+64.0) Fuel capacity 40 gals. - 2 tanks, 20 gals. each (+26) (See NOTE 1 for unusable fuel) Oil capacity 3 gals. (-35.0) Control surface movements Elevator Up 22 degrees Down 25 degrees Elevator trim tab Up 25 degrees Down 25 degrees Aileron (Zero flap)Up 20 degrees Down 15 degrees Aileron droop Down 10½ degrees Flaps Down 24 degrees Rudder Right 21 degrees Left 1 degrees Serial Nos. eligible 1306 thru 1615 and 5001 and on Required equipment In addition to the pertinent required basic equipment specified in CAR 8, the following items of equipment must be installed: Items 13, 105(l), 105(m), 108(d), 20 1(f), 202(f), 202(f), 205(e) 306(c), and 307(h) or 307(i) SPECIFICATIONS PERTINENT TO ALL MODELS Datum Leading edge of wing at fuselage Leveling means Models A, A-2, A-3, A-4, A-5, A-5T, A-6, A-7 and A-7T - Vertical lugs on fuselage aft left door on bulkhead, Model A-9, A-9B, bottom of first rib outboard of fuselage. Certification basis Type Certificate No. 758 (Models A, A-2, A-3, and A-4 - CAR 4a; Models A-5, A-5T, A-6, A-7, A-7T, A-9, and A-9B - CAR 8 Production basis None. Page 7 A-758, Rev 22 Equipment: A Plus (+) or minus (-) sign preceding the weight of an item indicates the net weight change when that item is installed. PROPELLERS AND PROPELLER ACCESSORIES 1. Propeller (Model A) (incl. hub) 14 lbs. (-59) Any fixed wood which is eligible for the engine power and speed which meets the following limits: Static rpm at maximum permissible throttle setting: Not over 2380, nor under 2080. No additional tolerance permitted. Diameter: Not over 74 in., not under 72 in. 2. Propeller (Model A-2) - Sensenich 76JB or 15 lbs. (-59) (Model A-3) - Sensenich 76JR, meeting the following static 15 lbs. (-59) rpm and diameter limits: or any other fixed wood propeller eligible for the engine power and speed which meets the following limits: Static rpm at maximum permissible throttle setting No additional tolerance permitted. Model A-2 - Not over 2350, nut under 2050. Model A-3 - Note over 2310, not under 2050. Diameter: Not over 76 in., not under 74.5 in. 3. Propeller (Model A-2 only) - McCauley 1A170-LL with the following limits: 33 lbs. (-59) Static rpm at maximum permissible throttle setting: Not over 2350, not under 2100. No additional tolerance permitted. Diameter: Not over 76 in., not under 74.5 in. 4. Propeller (Model A-4 with Lycoming O-290-D2 engine only). 24 lbs. (-58.5) Sensenich M76AM-2, fixed pitch metal Static rpm at maximum permissible throttle setting: Not over 2325, not under 2225. No additional tolerance permitted. Diameter: Not over 76 in., not under 74.5 in. 5. Propeller (Models A-4, A-5, and A-5T with Lycoming O-320-A2A engine only) 30 lbs. (-58.50) Sensenich M74DM, fixed pitch, metal Static rpm at maximum permissible throttle setting: Not over 2480, , not under 2250. Diameter: Not over 74 in., not under 72 in. 6. (a) Propeller (Model A-6 with Lycoming O-360-A1A or -C1A engine only) 58 lbs. (-62) McCauley 2D36C14/78KM-4, constant speed Pitch at 36 in. sta.: Low 13.5°, high 27° Diameter: Not over 74 in., not under 72 in. (b) Propeller governor, Woodward G210105 3 lbs. (-27.5) 7. Propeller (Model A-6 with Lycoming O-360-A1A or C1A engine only) 43 lbs. (-60.5) McCauley 1A200-FA, fixed pitch metal Static rpm at maximum permissible throttle setting: Not over 2310, not under 2210. Diameter: Not over 82 in., not under 80 in. A-758, Rev 23 Page 8 8. Propeller (Model A-7 or A-7T with Gulf Coast Dusting Co. W670-240 57 lbs. (-43.5) engine only). Universal 220/0-93 Aeromatic Static rpm at full throttle: Not over 1975, not under 1875 Pitch at 30 in. sta.: Low 15½°, high 27° Diameter: 90 in. Installation in accordance with propeller manufacturer's instructions. 9. Propeller (Model A-7 OR A-7T with Gulf Coast Dusting Co. 59 Lbs. (-43.5) W670-240 engine only). Universal 220/0-93 Aeromatic Static rpm at full throttle: Not over 1985, not under 1885 Pitch at 30 in. sta.: Low 15°, high 27° Diameter: 93 in. Installation in accordance with propeller manufacturer's instructions. 10. Propeller (Model A-9 with Lycoming O-540-B2B5 engine only) 42 lbs. (-60) McCauley 1A200-FA fixed pitch metal (S/N 1000 through 1035) Static rpm at maximum permissible throttle setting: Not over 2350, not under 2250 Diameter: Not over 84 in., not under 82 in. 11. Propeller (Model A-9 with Lycoming O-540-B2B5 engine only) 38 lbs. (-60) McCauley 1P235-PFA fixed pitch metal Static rpm at maximum permissible throttle setting: Not over 2400, not under 2250 Diameter: Not over 84 in., not under 82 in. (a) Propeller spinner, McCauley P/N C-3245, and 3 lbs. (-64) (b) Nose cowl installation per IMCO Dwg. No. 12500 9 lbs. (-58) are required with this propeller installation 12. Propeller (Model A-9 with Lycoming O-540-B2B5 engine only) 54 lbs. (-60) McCauley 2D34CT69/84HF two positions Pitch at 30 in. station: Low 14°, high 17° Diameter: Not over 84 in., not under 82 in. (a) Propeller spinner, McCauley P/N D-28093 lbs. (-64) (b) Nose cowl installation per IMCO Dwg. 12500 are required with this 9 lbs. (-58) installation (c) Woodward governor 2104273.5 lbs. (-54) 13. Propeller Model A-9B (with Lycoming IO-540-G1C5 or IO-540-K1A5 engines) 44 lbs. (-60) McCauley 1A200 DFA Static rpm at maximum permissible throttle setting: Not over 2400, not under 2250 Diameter: Not over 90 in., not under 88 in. (a) Propeller Spinner, McCauley P/N D-3328 when modified in accordance with McCauley Service Bulletin NO. 61 14. Propeller (Model A-9 with Lycoming O-540-B2B5 engine only) 44 lbs. (-60) McCauley 1A200 DFA Static rpm at maximum permissible throttle setting: Not over 2400, not under 2325 Diameter: Not over 90 in., not under 84 in. (a) Propeller spinner, McCauley P/N D-3328 Page 9 A-758, Rev 23 ENGINE AND ENGINE ACCESSORIES - Fuel and Oil System 101. Exhaust manifolds with carburetor air heater Use actual wt. and arm 102. Deleted October 31, 1950 103. Deleted October 31, 1950 104. Starter (a) Continental Part No. 50309 (Model A-3 only) 15 lb. (-26) (b) 12 Volt E-80 Eclipse Model 50 or 54 (Model A-2 only) 19 lb. (-28) (c) Delco Model 1109657-12UA12V (Model A-4 only) 10.5 lb. (-51) (d) Delco Model 1109673 (Model A-6 only) 18 lb. (-49) (e) Delco Model 1109688 (Model A-9 only 18.0 lb. (-46) 119511 or equivalent (f) Prestolite Model MHB 4001 or 4016 (A-9B only) (-46) 105. Fuel pumps (a) Engine-driven (Continental Part No. 40585) (Model A-3 only) 2 lb. (-53) (b) Hand emergency (Aero Supply Part No. 54609-1) 3 lb. (-25) (Models A-3 and A-4 only) (c) Engine-drive AC Type AH (Model A-4 only) 3 lb. (-30.5) (d) Engine-drive AC Type AH (Model A-6 only) 3.5 lb. (-30) (e) Electric emergency (Bendix Model 478360) (Model A-6 only) 2 lb. (-26) (f) Hand emergency (AC Model 4460) (Model A-6 only) 3.5 lb. (-25.5) (g) Engine-drive (Titan Model 4170) (Models A-7 and A-7T) Use actual wt. and arm (h) Hand emergency (AN 2009 Type D-2) Use actual wt. and arm (i) Engine-driven AC diaphragm type (Lycoming P/N 74082) 1.5 lb. (-22) (Model A-9 only) (j) Electric emergency (Bendix Model 478360, 12 volt (2 req.) 4 lb. (-3) (Lycoming P/N 74082) (Model A-9 only) (k) Electric emergency (Bendix Model 476-088 or 480-500) (24 volt) 4 lb. (-3) (2 required) (Model A-9 only) (l) Electric boost pump (Weldon 1003F) (24 volt) (1 required) 2 lb. (-15) (Model A-9B only) (m) Engine-driven pump (Lear Siegler RG17980) (Model A-9B only) 1 lb. (-22) 106. Deleted August 2, 1955. (See Item 104) 107. 13-1/2 gal. auxiliary fuel tank (Model A-4) 13 lb. (+28) Arm of fuel(+28) (To be used for level flight cruise operation only) 108. Oil radiator (a) Harrison AP-13-CJ03-1 (Model A-4 only) 6 lb. (-26) (b) Harrison AP-12-CU03-01 (Models A-5, A-5T, A-6 only) 7 lb. (-60) (c) Harrison 8526250 (Model A-9 only) 2.0 lb. (-54) (d) Harrison P/N 8534108 (Model A-9B only) 6 lb. (-54) 109. Lycoming O-320-A2A (Eligible on Model A-4 when installed in accordance 282 lb. (-42.5) with Callair Dwg. No. 335) Engine Limits: For all operations, 2700 rpm (150 hp) Fuel: 80/87 min. grade aviation gasoline Propeller - Item 5 required. 110. Deleted March 15, 1962. 111. Deleted March 15, 1962. LANDING GEAR AND FLOATS 201. Two main wheel-brake assemblies, Type III (a) Hayes Model 840, 8.00-4 6 lb. (+4.5) (b) Hayes Model 841, 8.00-4 10 lb. (+4.5) (c) Firestone Model 6C5YFB, 6.00-6 16 lb. (+4.5) (d) Goodyear Model LF6HBD, 6.00-6 12 lb. (+4.5) Wheel Assembly 511960-M, brake assembly 9520517 (e) Goodyear Model LF6HBD, 6.00-6 14.5 lb. (+2) Wheel Assembly 511960-M, brake assembly 9520517 A-758, Rev 22 Page 10 (f) Cleveland Use actual wt. (+2) Wheel Assembly 40-99, or 40-24; brake assembly 30-41 or 30-6 Use actual wt. (+2) (see Note 12) (g) Cleveland Wheel Assembly 40-47; Brake Assembly 30-32 (see note 13) Use actual wt. (+2) 202. Two main gear 4 ply rating tires (a) Type III, 8.00-4 with tubes 18 lb. (+4.5) (b) Type III, 6.00-6 with tubes 18 lb. (+4.5) (c) Type III, 7.00-6 with tubes 21 lb. (+4.5) (d) Goodyear Nylon cord, 7.00-6 helicopter tires and tubes 14 lb. (+4.5) (e) Goodyear Nylon cord, 7.00-6 helicopter tires and tubes 14 lb. (+2) (f) Type III, 8.50-6 with tubes Use actual wt. (+2) 205. Tail Wheel Assembly (a) Scott G5A with 6X2 solid tire 5 lb. (+208.5) (b) Scott 3-24B with Heath 42-T-1 rudder arm and 6X2 solid tire 6 lb. (+208.5) (c) Maule Model SFS-1-2 steerable with Heath 42-T-1 rudder arm and 7 lb. (+208.5) 6X2 solid tire (d) Maule Model SFS-1-2P8 steerable with 42-T-1 rudder arm and 8" 7 lb. (+208.5) pneumatic tire and tube (e) Scott Model 3200 8 lb. (+207.5) 208. Skis-Call S1, S2, S5, or S7 (Dwgs. 37, 1003, 1014) Use actual wt. change 210. Wheel fenders (Call Dwg. 211) 6 lb. (+4) ELECTRICAL EQUIPMENT 305. Battery and box (12 volt 24 amp. hr.) (a) Models A-2, A-3, A-4 27 lb. (+98) (b) Model A-5, A-6 26 lb. (+56) (c) Model A-9 21 lb. (-5.0) 306. Battery and box (12 volt 35 amp. hr.) (a) Model A-9 27 lb. (-5.0) (b) Model A-9 (optional) (24 volts) (2 required) 54 lb. (-5.0) (c) Model A-9B (2 required) 54 lb. (-5.0) 307. Generators/Alternators (a) 12 volt Leece-Neville 15 amp. Type E7A (Model A-2 only) 24 lb. (-27) (b) 14.5 volt Pierson Electric Type E128 8 amp. (Model A-2 only) 8 lb. (-27) (c) Delco-Remy Model 110189.12UA12V (Model A-4 only) 17 lb. (-48.5) (d) Delco-Remy Model 1101899 (12 volt 20 amp.) 11 lb. (-50.5) (Models A-5 and A-6 only) (e) Delco-Remy Model 1101899 (12 volt 20 amp.) (Model A-9 only) 11 lb. (-48) (f) Delco-Remy Model 1101915 (12 volt 50 amp.) (Model A-9 only) 17 lb. (-48) (g) Delco-Remy Model 1105055 (24 volt 50 amp.) (Optional A-9) 25 lb. (-48) (h) Delcotron 24 volt 50 amp. Alternator 1100718 15 lb. (-48) (i) Prestolite 24 volt 50 amp. Alternator ALT-8404 or ALU 8421 12 lb. (-48) (j) Prestolite 24 volt 70 AMP Alternator ALU 8403 (see note 14) 308. Narco VHT-4 radio(+48) INTERIOR EQUIPMENT 401. Optional front baggage compartment and enlarged rear baggage compartment, Call dwgs. Nos. 300, 301, 126, and 127 (Models A-2, A-3, and A-4)