TCDS 5A4

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Rev. No. 65 58 59 59 59 58 58 59 59 59 58 59 59 58 Page No. 15 16 17 18 19 20 21 22 23 24 25 26 27 28 Rev. No. 58 59 58 58 63 58 58 58 58 58 59 59 62 64 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 5A4 Revision 65 Textron Aviation 50 (L-23A) D50E-5990 B50 (L-23B) E50 (L-23D, C50 RL-23D) D50 (L-23E) F50 D50A G50 D50B H50 D50C J50 D50E November 27, 2017 TYPE CERTIFICATION DATA SHEET NO. 5A4 This data sheet which is a part of Type Certificate No. 5A4 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard Wichita, KS 67215 Type Certificate Holder Record: Beech Aircraft Corporation transferred to Raytheon Aircraft Company on April 15, 1996 Raytheon Aircraft Company transferred to Hawker Beechcraft Corporation on March 26, 2007 Hawker Beechcraft Corporation transferred to Beechcraft Corporation on April 12, 2013 Beechcraft Corporation transferred to Textron Aviation Inc. on October 12, 2016 I. Model 50, Twin Bonanza, (Military L-23A), 6 PCLM (Normal Category), Approved May 25, 1951 Engines Two (2) Lycoming GO-435-C2 or GO-435-C2E Fuel 80/87 minimum grade aviation gasoline Engine limits (See also Takeoff (one minute), 3400 rpm. (260 hp.) limits under Items For all other operations, 3000 rpm. (240 hp.) 2(d) and 2(e)) Airspeed limits Maneuvering 165 mph. (144 knots) (TIAS) Maximum structural cruising 180 mph. (157 knots) Never exceed 227 mph. (197 knots) Design dive 270 mph. (234 knots) Flaps extended 125 mph. (109 knots) Landing gear extended 125 mph. (109 knots) 5A4 2 Rev. 65 I. Model 50 (cont’d) C.G. range (landing (+116.5) to (+124.6) at 5500 lb. gear extended) (+114.0) to (+124.6) at 4550 lb. or less Straight line variation between points given. 112 114 116 118 120 122 124 126 4500 4700 4900 5100 5300 5500 LB. INCHES Empty wt. C.G. range Forward compartment 100 lb. (using baggage Rear compartment 200 lb. placard) (+116.0) to (+116.7) at 4100 lb. (+114.3) to (+115.6) at 3625 lb. (+114.3) to (+115.3) at 3500 lb. Straight line variation between points given. 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 non-standard arrangements. For empty weight C.G. outside, both forward and rearward of the limits given, and for applicable range and pertinent baggage compartment placards, refer to weight and balance section of the operating limitations (loading schedule), or contact the manufacturer. 113 114 115 116 117 3500 3700 3900 4100 LB. INCHES Maximum weight 5500 lb. No. of seats 6 (3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 260 lb. (+193) (For loading instructions, see weight and balance report.) Fuel capacity 134 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 23 gal. tanks at +117) See NOTE 1 for data on system fuel. Oil capacity 24 qt. (12 qt. in each engine at +72) See NOTE 1 for data on system oil. Rev. 65 3 5A4 I. Model 50 (cont’d) Control surface Wing flaps Down 30° movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 30° Rudder Right 30° Left 30° Serial Nos. eligible H-1 through H-11, LH-1 through LH-55 Required equipment Items 1, 101(a) and (b), 102(a) or (b), 103(a), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(a), (b) or (c), 401(a) and 601 II. Model B50, Twin Bonanza, (Military L-23B), 8 PCLM (Normal Category), Approved July 31, 1953 Engines 2 Lycoming GO-435-C2 or GO-435-C2B or GO-435-C2D6 or GO-435-C2E Fuel 80/87 minimum grade aviation gasoline Engine limits Takeoff (one minute), 3400 rpm. (260 hp.) For all other operations, 3100 rpm. (245 hp.) Airspeed limits Maneuvering 165 mph. (144 knots) (TIAS) Maximum structural cruising 180 mph. (157 knots) Never exceed 227 mph. (197 knots) Design dive 270 mph. (234 knots) Flaps extended 125 mph. (109 knots) Landing gear extended 125 mph. (109 knots) C.G. range (landing (+116.8) to (+124.6) at 6000 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given 112 114 116 118 120 122 124 126 5700 5900 6100 5500 LB. INCHES 5300 5A4 4 Rev. 65 II. Model B50 (cont’d) Empty wt. C.G. range Forward compartment 100 lb. (using baggage placards) Rear compartment 200 lb. (+115.7) to (+117.4) at 4500 lb. (+114.3) to (+116.95) at 4253 lb. (+114.3) to (+116.3) at 3900 lb. Straight line variation between points given 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 non-standard arrangements. For empty weight C.G. outside, both forward and rearward of the limits given, and for applicable range and pertinent baggage compartment placards, refer to weight and balance section of the operating limitations (loading schedule), or contact the manufacturer. 113 114 115 116 117 3900 4100 4300 4100 LB. INCHES 118 Maximum weight 6000 lb. No. of seats Maximum 8, Normal 6 (3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 260 lb. (+193) (For loading instructions, see weight and balance report) Fuel capacity 134 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 23 gal. tanks at +117) See NOTE 1 for data on system fuel. Oil capacity 24 qt. (12 qt. in each engine at +72) See NOTE 1 for data on system oil. Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Serial Nos. eligible CH-12 through CH-110, LH-56 through LH-95 Required equipment Items 2(d) or (e) and (b) with GO-435-C2 or -C2E engines, or 4 with -C2D6 engines, or 6 with -C2B engines, 101(a) or (b), 102(b), 103(a), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(b) or (c), 302(a) or (b), 401(d) and 601 III. Model C50, Twin Bonanza, 8 PCLM (Normal Category), Approved October 13, 1954 Engines 2 Lycoming GO-480-F6 ot GO-480-F1A6 Fuel 80/87 minimum grade aviation gasoline Rev. 65 5 5A4 III. Model C50 (cont’d) Engine limits Takeoff (one minute), 3400 rpm. (275 hp.) For all other operations, 3100 rpm. (265 hp.) Airspeed limits Maneuvering 165 mph. (144 knots) (TIAS) Maximum structural cruising 180 mph. (157 knots) Never exceed 230 mph. (200 knots) Design dive 270 mph. (234 knots) Flaps extended 125 mph. (109 knots) Landing gear extended 125 mph. (109 knots) C.G. range (landing (+116.8) to (+124.6) at 6000 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given (Refer to Section II for figure.) Empty wt. C.G. range For standard arrangement, refer to empty weight C.G. range under Section II for Model B50. For range with 46 gal. auxiliary fuel tanks, refer to Item 106. Maximum weight 6000 lb. No. of seats Maximum 8, Normal 6 (3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 300 lb. (+193) (For loading instructions, see weight and balance report.) Fuel capacity 134 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 23 gal. tanks at +117) See NOTE 1 for data on system fuel Oil capacity 24 qt. (12 qt. in each engine at +72) See NOTE 1 for data on system oil. Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Serial Nos. eligible CH-111 through CH-360 Required equipment Items 3, 101(a) and (b), 102(b), 103(a), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(b) or (c), 302(a) or (b), 401 (e) or (i) and 601 IV. Model D50, Twin Bonanza, (Military L-23E), 8 PCLM (Normal Category), Approved December 6, 1955 Engines Two (2) Lycoming GO-480-C2C6 or GO-480-C2D6 (See Item 108 for optional engine.) Fuel 100/130 minimum grade aviation gasoline Engine limits Takeoff (one minute), 3400 rpm. (295 hp.) For all other operations, 3100 rpm. (285 hp.) 5A4 6 Rev. 65 IV. Model D50 (cont’d) Airspeed limits Maneuvering 175 mph. (152 knots) (TIAS) Maximum structural cruising 200 mph. (174 knots) Never exceed 252 mph. (219 knots) Design dive 280 mph. (243 knots) Flaps extended 135 mph. (117 knots) Landing gear extended 150 mph. (130 knots) C.G. range (landing (+116.8) to (+124.6) at 6300 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given 112 114 116 118 120 122 124 126 5300 5500 5700 5900 6100 6300 LB. INCHES Empty wt. C.G. range None Maximum weight 6300 lb. No. of seats Maximum 8, Normal 6 (2 or 3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 300 lb. (+193) (For loading instructions, see weight and balance report.) Fuel capacity 134 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 23 gal. tanks at +117) See NOTE 1 for data on system fuel. Oil capacity 24 qt. (12 qt. in each engine at +72) See NOTE 1 for data on system oil. Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (S/N DH-1 through DH-143, except DH-18) (main surfaces in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Tabs (S/N DH-18, DH-144 and up) (main surfaces in neutral) Aileron Up 7-1/2° Down 7-1/2° Tab, Anti-Servo (S/N DH-18, DH-144 and up) (main surface in extreme position) Aileron Up 14° Down 8° Serial Nos. eligible DH-1 through DH-154 Rev. 65 7 5A4 IV. Model D50 (cont’d) Required equipment Items 5, 101(a) and (b), 102(b), 103(a), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(b) or (c), 302(a) or (b), 401(h) and 601 or 602 V. Model E50, Twin Bonanza, (Military L-23D, RL-23D), 8 PCLM (Normal Category), Approved December 1, 1956 Engines Two (2) Lycoming GSO-480-A1A6 (Military O-480-1) or GSO-480-B1B6 Fuel 100/130 minimum grade aviation gasoline Engine limits Straight line manifold pressure variation with altitudes shown HP RPM MP ALT Takeoff 340 3400 48.0 S.L. Takeoff 340 3400 44.5 8000 Maximum continuous 320 3200 45.0 S.L. Maximum continuous 320 3200 43.0 7500 Airspeed limits Maneuvering 185 mph. (161 knots) (TIAS) Maximum structural cruising 205 mph. (178 knots) Never exceed 270 mph. (235 knots) Design dive 300 mph. (261 knots) Flaps extended 150 mph. (130 knots) Landing gear extended 150 mph. (130 knots) C.G. range (landing (+118.0) to (+124.6) at 7000 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given 112 114 116 118 120 122 124 126 5000 5400 5800 6200 6600 7000 LB. INCHES Empty wt. C.G. range None Maximum weight 7000 lb. No. of seats Maximum 8, Normal 6 (2 or 3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 300 lb. (+193) (For loading instructions, see weight and balance report.) Fuel capacity 180 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 46 gal. tanks at +127) See NOTE 1 for data on system fuel. Oil capacity 32 qt. (16 qt. in each nacelle at +103) See NOTE 1 for data on system oil. 5A4 8 Rev. 65 V. Model E50 (cont’d) Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tab, Anti-Servo (main surface in extreme position) Aileron Up 14° Down 8° Tabs (main surface in neutral) Aileron Up 7-1/2° Down 7-1/2° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Serial Nos. eligible EH-1 through EH-70 (LH-96 and on, L-23D), (RLH-1 and on, L-23D remanufactured), (LHC-1 and on, LHD-1 and on, RLHE-1, RLHE-2, LHE-3 and on - different radar versions of RL-23D). Prior to civil certification, L-23D and RL-23D airplanes that have been operated by the military services must be modified by Beech Dwg. 50-001016 and 50-001062, respectively. Required equipment Items 7, 101(c) and (d), 102(c), 103(b), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(d) or (e), 302(a) or (b), 401(j) and 602 VI. Model D50A, Twin Bonanza, 8 PCLM (Normal Category), Approved October 29, 1957 Engines Two (2) Lycoming GO-480-G2D6 Fuel 100/130 minimum grade aviation gasoline Engine limits Takeoff (one minute), 3400 rpm. (295 hp.) For all other operations, 3100 rpm. (285 hp.) Airspeed limits Maneuvering 185 mph. (161 knots) (TIAS) Maximum structural cruising 205 mph. (178 knots) Never exceed 270 mph. (235 knots) Design dive 300 mph. (261 knots) Flaps extended 150 mph. (130 knots) Landing gear extended 150 mph. (130 knots) C.G. range (landing (+116.8) to (+124.6) at 6300 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given (Refer to Section IV for figure.) Empty wt. C.G. range None Maximum weight 6300 lb. No. of seats Maximum 8, Normal 6 (2 or 3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 300 lb. (+193) (For loading instructions, see weight and balance report.) Fuel capacity 134 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 23 gal. tanks at +117) See NOTE 1 for data on system fuel. Oil capacity 24 qt. (12 qt. in each engine at +72) See NOTE 1 for data on system oil. Rev. 65 9 5A4 VI. Model D50A (cont’d) Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 7-1/2° Down 7-1/2° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Tabs, Anti-Servo (main surface in extreme position) Aileron Up 14° Down 8° Serial Nos. eligible DH-155 through DH-198 Required equipment Items 5, 101(a) and (b), 102(d), 103(a), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(b) or (c), 302(a) or (b), 401(l) and 602 VII. Model F50, Twin Bonanza, 8 PCLM (Normal Category), Approved October 29, 1957 Engines Two (2) Lycoming GSO-480-B1B6 Fuel 100/130 minimum grade aviation gasoline Engine limits Straight line manifold pressure variation with altitudes shown HP RPM MP ALT Takeoff 340 3400 48.0 S.L. Takeoff 340 3400 44.5 8000 Maximum continuous 320 3200 45.0 S.L. Maximum continuous 320 3200 43.0 7500 Airspeed limits Maneuvering 185 mph. (161 knots) (TIAS) Maximum structural cruising 205 mph. (178 knots) Never exceed 270 mph. (235 knots) Design dive 300 mph. (261 knots) Flaps extended 150 mph. (130 knots) Landing gear extended 150 mph. (130 knots) C.G. range (landing (+118.0) to (+124.6) at 7000 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given (Refer to Section V for figure) Empty wt. C.G. range None Maximum weight 7000 lb. No. of seats Maximum 8, Normal 6 (2 or 3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 300 lb. (+193) (For loading instructions, see weight and balance report.) Fuel capacity 180 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 46 gal. tanks at +127) See NOTE 1 for data on system fuel. 5A4 10 Rev. 65 VII. Model F50 (cont’d) Oil capacity 32 qt. (16 qt. in each nacelle at +103) See NOTE 1 for data on system oil. Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs, Anti-Servo (main surfaces in extreme position) Aileron Up 14° Down 8° Tabs (main surfaces in neutral) Aileron Up 7-1/2° Down 7-1/2° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Serial Nos. eligible FH-71 through FH-96 (except FH-94) Required equipment Items 7, 101(c) and (d), 102(c), 103(b), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(d) or (e), 302(a) or (b), 401(m) and 602 VIII. Model D50B, Twin Bonanza, 8 PCLM (Normal Category), Approved November 10, 1958 Engines Two (2) Lycoming GO-480-G2D6 Fuel 100/130 minimum grade aviation gasoline Engine limits Takeoff (one minute), 3400 rpm. (295 hp.) For all other operations, 3100 rpm. (285 hp.) Airspeed limits Maneuvering 185 mph. (161 knots) (TIAS) Maximum structural cruising 205 mph. (178 knots) Never exceed 270 mph. (235 knots) Design dive 300 mph. (261 knots) Flaps extended 150 mph. (130 knots) Landing gear extended 150 mph. (130 knots) C.G. range (landing (+116.8) to (+124.6) at 6300 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given (Refer to Section IV for figure.) Empty wt. C.G. range None Maximum weight 6300 lb. No. of seats Maximum 8, Normal 6 (2 or 3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 300 lb. (+193) Rear compartment 125 lb. (+193) with Item 411 (Item 411) Optional baggage compartment 115 lb. (+223) (For loading instructions, see weight and balance report.) Fuel capacity 134 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 23 gal. tanks at +117) See NOTE 1 for data on system fuel. Rev. 65 11 5A4 VIII. Model D50B (cont’d) Oil capacity 24 qt. (12 qt. in each engine at +72) See NOTE 1 for data on system oil. Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surfaces in neutral) Aileron Up 7-1/2° Down 7-1/2° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Tabs, Anti-Servo (main surfaces in extreme position) Aileron Up 14° Down 8° Serial Nos. eligible DH-199 through DH-236 Required equipment Items 5, 101(a) and (b), 102(d), 103(a), 201(a), 202(a) or (b), 205(a), 206(a) or (b), 301(b) or (c), 302(a) or (b), 401(n) and 602 IX. Model G50, Twin Bonanza, 8 PCLM (Normal Category), Approved November 10, 1958 Engines Two (2) Lycoming IGSO-480-A1A6 Fuel 100/130 minimum grade aviation gasoline Engine limits Straight line manifold pressure variation with altitudes shown HP RPM MP ALT Takeoff 340 3400 48.0 S.L. Takeoff 340 3400 44.5 11,000 Maximum continuous 320 3200 45.0 S.L. Maximum continuous 320 3200 41.3 11,000 Airspeed limits Maneuvering 185 mph. (161 knots) (TIAS) Maximum structural cruising 205 mph. (178 knots) Never exceed 270 mph. (235 knots) Design dive 300 mph. (261 knots) Flaps extended 150 mph. (130 knots) Landing gear extended 150 mph. (130 knots) C.G. range (landing (+118.4) to (+124.6) at 7150 lb. gear extended) (+114.0) to (+124.6) at 5350 lb. or less Straight line variation between points given 112 114 116 118 120 122 124 126 5200 5600 6000 6400 6800 7200 LB. INCHES 5A4 12 Rev. 65 IX. Model G50 (cont’d) Empty wt. C.G. range None Maximum weight Landing 7000 lb. Takeoff 7150 lb. No. of seats Maximum 8, Normal 6 (2 or 3 at +116, 3 at +154) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 300 lb. (+193) Item 411 Optional baggage compartment 115 lb. (+223) Rear compartment 200 lb. (+193) (with Item 411) (For loading instructions, see weight and balance report.) Fuel capacity 180 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 46 gal. tanks at +127) See NOTE 1 for data on system fuel Oil capacity 32 qt. (16 qt. in each nacelle at +103) See NOTE 1 for data on system oil Control surface Wing flaps Down 30° movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tab, Anti-Servo (main surface in extreme position) Aileron Up 14° Down 8° Tabs (main surfaces in neutral) Aileron Up 7-1/2° Down 7-1/2° Elevator Up 10° Down 21° Rudder Right 30° Left 30° Serial Nos. eligible GH-94, GH-97 through GH-119 Required equipment Items 7, 101(c) or (e) and (d), 102(c), 103(b), 201( a), 202(a) or (b), 205(a), 206(a) or (b), 301(d) or (e), 302(a) or (b), 401(o) or (p) and 602 X. Model H50, Twin Bonanza, 7 PCLM (Normal Category), Approved November 13, 1959 Engines Two (2) Lycoming IGSO-480-A1A6 Fuel 100/130 minimum grade aviation gasoline Engine limits Straight line manifold pressure variation with altitudes shown HP RPM MP ALT Takeoff 340 3400 48.0 S.L. Takeoff 340 3400 44.0 11,000 Maximum continuous 320 3200 45.0 S.L. Maximum continuous 320 3200 41.3 11,000 Airspeed limits Maneuvering 185 mph. (161 knots) (TIAS) Maximum structural cruising 205 mph. (178 knots) Never exceed 270 mph. (235 knots) Design dive 300 mph. (261 knots) Flaps extended 150 mph. (130 knots) Landing gear extended 150 mph. (130 knots) Rev. 65 13 5A4 X. Model H50 (cont’d) C.G. range (landing (+118.4) to (+125.6) at 7300 lb. gear extended) (+114.0) to (+125.6) at 5350 lb. or less Straight line variation between points given 112 114 116 118 120 122 124 126 5400 5800 6200 6600 7000 7400 LB. INCHES Empty wt. C.G. range None Maximum weight Landing 7000 lb. Takeoff 7300 lb. No. of seats Maximum 7, Normal 6 (crew at +116) (See loading instructions for passenger loading) Maximum baggage Forward compartment 395 lb. (+ 60) (structural limits) Rear compartment 200 lb. (+223) (For loading instructions, see weight and balance report.) Fuel capacity 180 gal. (4 tanks in wings - two 44 gal. tanks at +139, two 46 gal. tanks at +127) See NOTE 1 for data on system fuel Oil capacity 32 qt. (16 qt. in each nacelle at +103) See NOTE 1 for data on system oil Control surface movements Wing flaps Down 30° Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs, Anti-Servo (main surfaces in extreme position) Aileron Up 14° Down 8° Tabs (main surfaces in neutral) Aileron Up 7-1/2° Down 7-1/2° Elevator Up 10° Down 22° Rudder Right 30° Left 30° Serial Nos. eligible HH-120 through HH-149 Required equipment Items 7, 101(c) or (e) and (d), 102(c), 103(b), 201(a), 202(a) or (b), 205 (a), 206(a) or (b), 301(d) or (e), 302(a) or (b), 401(v) and 602 XI. Model D50C, Twin Bonanza, 7 PCLM (Normal Category), Approved November 13, 1959 Engines Two (2) Lycoming GO-480-G2D6 Fuel 100/130 minimum grade aviation gasoline 5A4 14 Rev. 65 XI. Model D50C (cont’d) Engine limits Takeoff (one minute), 3400 rpm. (295 hp.) For all other operations, 3100 rpm. (285 hp.) Airspeed limits Maneuvering 185 mph. (161 knots) (TIAS) Maximum structural cruising 205 mph. (178 knots) Never exceed 270 mph. (235 knots) Design dive 300 mph. (261 knots) Flaps extended 150 mph. (130 knots) Landing gear extended 150 mph. (130 knots) C.G. range (landing (+116.8) to (+125.6) at 6300 lb. gear extended) (+114.0) to (+125.6) at 5350 lb. Straight line variation between points given 112 114 116 118 120 122 124 126 5000 5400 5800 6200 6600 7000 LB. INCHES Empty wt. C.G. range None Maximum weight 6300 lb. No. of seats Maximum 7, Normal 6 (crew 2 at +116) (See loading instructions for passenger loading) Maximum baggage Forward compartment 395 lb. (+ 60)