TCDS 2A13

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Revision No. 66 48 48 48 48 48 64 48 48 48 48 48 48 48 48 48 48 48 Page No. 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 Revision No. 65 50 65 65 63 48 57 50 63 63 59 48 48 48 48 48 59 65 Page No. 37 38 39 40 41 42 43 44 45 46 47 Revision No. 61 64 66 59 65 65 65 65 59 62 65 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 2A13 Revision 66 Piper Aircraft, Inc PA-28-140 PA-28-151 PA-28-150 PA-28-161 PA-28-160 PA-28-181 PA-28-180 PA-28R-201 PA-28-235 PA-28R-201T PA-28S-160 PA-28-236 PA-28S-180 PA-28RT-201 PA-28R-180 PA-28RT-201T PA-28R-200 PA-28-201T October 10, 2025 TYPE CERTIFICATE DATA SHEET NO. 2A13 This data sheet, which is a part of Type Certificate 2A13, 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 Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 Type Certificate Holder Record The New Piper Aircraft, Inc transferred TC 2A13 to Piper Aircraft, Inc on August 7, 2006. I - Model PA-28-160 (Cherokee), 4 PCLM (Normal Category), Approved October 31, 1960, for S/N 28-03; 28-1 through 28-4377; and 28-1760A. Engine Lycoming O-320-B2B or O-320-D2A with carburetor setting 10-3678-32 Fuel 91/96 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (160 hp) Propeller and Propeller Limits Sensenich M74DM or 74DM6 on S/N 28-1 through 28-1760, and 28-1760A. Sensenich M74DMS or 74D6S5 on S/N 28-1761 through 28-4377. Static r.p.m. at maximum permission throttle setting not over 2425 r.p.m., not under 2325 r.p.m. No additional tolerance permitted. Diameter: Not over 74", not under 72.5". Propeller Spinner Piper P/N 14422-00 on S/N 28-1 through 28-1760, and 28-1760A. Piper P/N 63760-04 or P/N 65805-00 on S/N 28-1761 through 28-4377. See NOTE 11. Airspeed Limits Never exceed 171 mph (148 knots) CAS Maximum structural cruising 140 mph (121 knots) CAS Maneuvering 129 mph (112 knots) CAS Flaps Extended 115 mph (100 knots) CAS 2A13 Page 2 of 47 Center of Gravity Range (+84.0) to (+95.9) at 1650 lb. or less (+85.9) to (+95.9) at 1975 lb. (+89.2) to (+95.9) at 2200 lb. Straight line variation between points given. Empty Weight C. G. Range None Maximum Weight 2200 lb. No. of Seats 4 (2 at +85.5, 2 at +118.1) Maximum Baggage 125 lb. at (+142.8) on S/N 28-1 through 28-1760, and 28-1760A. See NOTE 8. 200 lb. at (+142.8) on S/N 28-1761 through 28-4377. Fuel Capacity 50 gallons at (+95) ( 2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 quarts at (+32.5), 6 quarts usable See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (± 2°) Up 0° Down 40° Ailerons (± 2°) Up 30° Down 15° Rudder (± 2°) Left 27° Right 27° Stabilator (± 2°) Up 18° Down 2° Stabilator Tab (± 1°) Up 3° Down 12° Nose Wheel Travel (±1°) Left 30° Right 30° (Effective on S/N 28-1 through 28-3377, and 28-1760A) (1) Left 22° Right 22° (Effective S/N 28-3378 through 28-4377) Manufacturer's Serial Nos. 28-03; 28-1 through 28-4377; and 28-1760A. II - Model PA-28-150 (Cherokee), 4 PCLM (Normal Category), Approved June 2, 1961, for S/N 28-03; 28-1 through 28-4377; and 28-1760A. Engine Lycoming O-320-A2B or O-320-E2A with carburetor setting 10-3678-32 Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (150 hp) Propeller and Propeller Limits Sensenich M74DM or 74DM6 on S/N 28-1 through 28-1760, and 28-1760A. Sensenich M74DMS or 74DM6S5 on S/N 28-1761 through 28-4377. Static r.p.m. at maximum permissible throttle setting not over 2375 r.p.m., not under 2275 r.p.m. No additional tolerance permitted. Diameter: Not over 74", not under 72.5". Propeller Spinner Piper P/N 14422-00 on S/N 28-1 through 28-1760, and 28-1760A. Piper P/N 63760-04 or 65805-00 on S/N 28-1761 through 28-4377. See NOTE 11. Airspeed Limits Never exceed 171 mph (148 knots) CAS Maximum structural cruising 140 mph (121 knots) CAS Maneuvering 129 mph (112 knots) CAS Flaps Extended 115 mph (100 knots) CAS Page 3 of 47 2A13 Center of Gravity Range (+84.0) to (+95.9) at 1650 lb. or less (+85.9) to (+95.9) at 1975 lb. (+88.4) to (+95.9) at 2150 lb. Straight line variation between points given. Empty Wt. C. G. Range None Maximum Weight 2150 lb. No. of Seats 4 (2 at +85.5, 2 at +118.1) Maximum Baggage 125 lb. at (+142.8) on S/N 28-1 through 28-1760, and 28-1760A. See NOTE 8. 200 lb. at (+142.8) on S/N 28-1761 through 28-4377. Fuel Capacity 50 gallons at (+95) ( 2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 quarts at (+32.5) (6 quarts usable) See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (± 2°) Up 0° Down 40° Ailerons (± 2°) Up 30° Down 15° Rudder (± 2°) Left 27° Right 27° Stabilator (± 1°) Up 18° Down 2° Stabilator Tab (± 1°) Up 3° Down 12° Nose Wheel Travel (± 2) Left 30° Right 30° (Effective on S/N 28-03; 28-1 through 28-3377; and 28-1760A) ( 2) Left 22° Right 22° (Effective on S/N 28-3378 through 28-4377) Manufacturer's Serial Nos. 28-03; 28-1 through 28-4377; and 28-1760A. III - Model PA-28-180 (Cherokee), 4 PCLM (Normal Category), Approved August 3, 1962; 2 PCLM (Utility Category), Approved December 6, 1966, for S/N 28-03; 28-671 through 28-5859; and 28-7105001 through 28-7205318. Engine Lycoming O-360-A3A or 0-360-A4A with carburetor setting 10-3878 or 10-4164-1 Fuel 91/96 minimum grade aviation gasoline Engine Limits S/N 28-671 through 28-1760, and 28-1760A (except S/N 28-1571 and S/N 28-1573) (See NOTE 4): Maximum permissible takeoff, 2475 r.p.m. For all other operations, 2700 r.p.m. (180 hp) S/N 28-1571; 28-1573; 28-1761 through 28-5859; and 28-7105001 through 28-7205318: For all operations, 2700 r.p.m. (180 hp) Propeller and Propeller Limits Sensenich M76EMM or 76EM8 on S/N 28-671 through 28-1760, and 28-1760A (except S/N 28-1571 and S/N 28-1573). Sensenich M76EMMS or 76EM8S5 on S/N 28-1571, 28-1573; 28-1761 through 28-5859; and 28-7105001 through 28-7205318. Static r.p.m. at maximum permissible throttle setting not over 2450 r.p.m., not under 2275 r.p.m. No additional tolerance permitted. Diameter: Not over or under 76". See NOTE 10. 2A13 Page 4 of 47 Propeller Spinner Piper P/N 14422-00 on S/N 28-671 through 28-1760, and 28-1760A. Piper P/N 63760-04 or 65805-00 on S/N 28-1761 through 28-5859; and 28-7105001 through 28-7205318. See NOTE 11. Airspeed Limits Never exceed 171 mph (148 knots) CAS Maximum structural cruising 140 mph (121 knots) CAS Maneuvering 129 mph (112 knots) CAS Flaps Extended 115 mph (100 knots) CAS Center of Gravity Range Utility Category (See NOTE 9) (+84.0) to (+86.5) at 1650 lb. or less (+85.8) to (+86.5) at 1950 lb. Normal Category (See NOTE 15) (S/N 28-671 through 28-5859) (+84.0) to (+95.9) at 1650 lb. or less (+85.9) to (+95.9) at 1975 lb. (+89.2) to (+95 9) at 2200 lb. (+92.1) to (+94.5) at 2400 lb. Normal Category (S/N 28-7105001 through 28-7205318) (+84.0) to (+95.9) at 1650 lb. or less (+87.0) to (+95.9) at 2150 lb. (+87.8) to (+95.9) at 2200 lb. (+91.0) to (+94.5) at 2400 lb. Straight Line Variation Between Points Given 2400 2200 2000 1800 1600 84 86 88 90 92 94 96 Normal Only Aft Limit Normal Aft Limit Utility Fuselage Station - Inches Normal & Utility 2400 2200 2000 1800 1600 84 86 88 90 92 94 96 Aft Limit Normal Fuselage Station - Inches (S/N 28-7105001 thru 28-7205318) Normal & Utility Aft Limit Utility Normal Only (S/N 28-671 thru 28-5859) Lbs. Lbs. Empty Weight C. G. Range None Page 5 of 47 2A13 Maximum Weight Normal Category: 2400 lb. Utility Category: 1950 lb. No. of Seats Normal Category: 4 (2 at +85.5, 2 at +118.1) Utility Category: 2 (2 at +85.5) Maximum Baggage Eligible Normal Category Only: 125 lb. at (+142.8) on S/N 28-671 through 28-1760, and 28-1760A. See NOTE 8. 200 lb. at (+142.8) on S/N 28-1761 through 28-5859, and 28-7105001 through 28-7205318. Fuel Capacity 50 gallons at (+95) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 quarts at (+32.5) (6 quarts usable) See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (± 2°) Up 0° Down 40° Ailerons (± 2°) Up 30° Down 15° Rudder (± 2°) Left 27° Right 27° Stabilator (± 1°) Up 18° Down 2° Stabilator Tab (± 1°) Up 3° Down 12° Nose Wheel Travel (± 2°) Left 30° Right 30° (Effective on S/N 28-671 through 28-3377) ( 2) Left 22° Right 22° (Effective on S/N 28-3378 through 28-5859, and 28-7105001 through 28-7205318) Manufacturer's Serial Nos. 28-03; 28-671 through 28-5859; and 28-7105001 through 28-7205318. The manufacturer is authorized to issue airworthiness certificates for airplane serial numbers: 28-4704 28-4745 28-4754 28-4763 28-4776 28-4791 28-4795 28-4826 28-4834 28-4859 28-4875 28-4879 28-4891 28-4907 28-4919 28-4922 28-4935 28-4945 28-4946 28-4947 28-4955 28-4959 28-4961 27-4964 28-4967 28-4968 28-4971 28-4975 28-4977 28-4985 28-4995 28-4999 28-5004 28-5007 28-5015 28-5017 28-5018 28-5019 28-5020 28-5023 28-5026 28-5027 28-5028 28-5031 28-5039 28-5041 28-5046 28-5051 28-5053 28-5057 28-5060 28-5061 28-5062 28-5063 28-5064 28-5066 through 28-5859, and 28-7105001 through 28-7205318 under the delegation option provisions of FAR 21. See NOTE 17 and 20. IV - Model PA-28S-160 (Cherokee), 4 PCSM (Normal Category), Approved February 25, 1963, for S/N 28-1 through 28-1760; and S/N 28-1760A. Engine Lycoming O-320-D2A with carburetor setting 10-3678-32 (See NOTE 18) Fuel 100/130 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (160 hp) Propeller and Propeller Limits McCauley 1A175-GM Static r.p.m. at maximum permissible throttle setting not over 2360 r.p.m., not under 2260 r.p.m. No additional tolerance permitted. Diameter: Not over 79", not under 78". 2A13 Page 6 of 47 Propeller Spinner Piper P/N 14422-00 spinner required. Airspeed Limits Never exceed 153 mph (133 knots) CAS Maximum structural cruising 140 mph (121 knots) CAS Maneuvering 129 mph (112 knots) CAS Flaps Extended 115 mph (100 knots) CAS Center of Gravity (+85.1) to (+93.5) at 1850 lb. or less (+87.0) to (+93.5) at 2100 lb. (+87.9) to (+93.5) at 2140 lb. Straight line variation between points given. Empty Weight C. G. Range None Maximum Weight 2140 lb. No. of Seats 4 (2 at +85.5, 2 at +118.1) Maximum Baggage 125 lb. at (+142.8) Fuel Capacity 50 gallons at (+95) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 quarts at (+32.5) (6 quarts usable) See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (±2°) Up 0° Down 40° Ailerons (±2°) Up 30° Down 15° Rudder (±2°) Left 27° Right 27° Stabilator (±1°) Up 18° Down 2° Stabilator Tab (±1°) Up 3° Down 12° Manufacturer's Serial Nos. 28-03; 28-1 through 28-1760; and 28-1760A. V - Model PA-28S-180 (Cherokee), 4 PCSM (Normal Category), Approved May 10, 1963, for S/N 28-671 through 28-5859, and 28-7105001 through 28-7105234. Engine Lycoming O-360-A3A or 0-360-A4A with carburetor setting 10-4164-1 See NOTE 19. Fuel 100/130 minimum grade aviation gasoline Engine Limits S/N 28-671 through 28-1760, and 28-1760A (except S/N 28-1571 and S/N 28-1573): Maximum permissible takeoff, 2350 r.p.m. For all other operations, 2700 r.p.m. (180 hp) See NOTE 4. S/N 28-1571; 28-1573; 28-1761 through 28-5859; and 28-7105001 through 28-7105234: For all operations, 2700 r.p.m. (180 hp) Propeller and Propeller Limits McCauley 1A200-FA8248 on S/N 28-671 to 28-1760, and 28-1760A. McCauley 1A200-DFA8248 on S/N 28-1761 through 28-5859, and 28-7105001 through 28-7105234. Static r.p.m. at maximum permissible throttle setting not over 2190 r.p.m., not under 2140 r.p.m. No additional tolerance permitted. Diameter: Not over 82", not under 81". Page 7 of 47 2A13 Propeller Spinner Spinner required. Piper P/N 14422-00 on S/N 28-671 through 28-1760, and 28-1760A. Piper P/N 63760-04 or 65805-00 on S/N 28-1761 through 28-5859, and 28-7105001 through 28-7105234. Airspeed Limits Never exceed 153 mph (133 knots) CAS Maximum structural cruising 140 mph (121 knots) CAS Maneuvering 129 mph (112 knots) CAS Flaps Extended 115 mph (100 knots) CAS Center of Gravity (+85.1) to (+92.5) at 1850 lb. or less (+87.0) to (+92.5) at 2100 lb. (+89.8) to (+92.5) at 2222 lb. Straight line variation between points given. Empty Weight C. G. Range None Maximum Weight 2222 lb. No. of Seats 4 (2 at +85.5, 2 at +118.1) Maximum Baggage 125 lb. at (+142.8) Fuel Capacity 50 gallons at (+95) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 quarts at (+32.5) (6 quarts usable) See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (±2°) Up 0° Down 40° Ailerons (±2°) Up 30° Down 15° Rudder (±2°) Left 27° Right 27° Stabilator (±1°) Up 18° Down 2° Stabilator Tab (±1°) Up 3° Down 12° Manufacturer's Serial Nos. 28-671 through 28-5859, and 28-7105001 through 28-7105234. See NOTE 30. The manufacturer is authorized to issue airworthiness certificates for airplane serial numbers: 28-4704 28-4745 28-4754 28-4763 28-4776 28-4791 28-4795 28-4826 28-4834 28-4859 28-4875 28-4879 28-4891 28-4907 28-4919 28-4922 28-4935 28-4945 28-4946 28-4947 28-4955 28-4959 28-4961 27-4964 28-4967 28-4968 28-4971 28-4975 28-4977 28-4985 28-4995 28-4999 28-5004 28-5007 28-5015 28-5017 28-5018 28-5019 28-5020 28-5023 28-5026 28-5027 28-5028 28-5031 28-5039 28-5041 28-5046 28-5051 28-5053 28-5057 28-5060 28-5061 28-5062 28-5063 28-5064 28-5066 through 28-5859, and 28-7105001 through 28-7105234 under the delegation option provisions of FAR 21. See NOTE 17 and 20. 2A13 Page 8 of 47 VI - Model PA-28-235 (Cherokee Pathfinder), 4 PCLM (Normal Category), Approved July 15, 1963, for S/N 28-10001 through 28-11378, and 28-7110001 through 28-7210023. Engine Lycoming O-540-B2B5, O-540-B1B5, or O-540-B4B5 with carburetor setting 10-4404, 10-5042, or 10-5054. (Baffle P/N 68759 required with 10-5054 setting.) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2575 r.p.m. (235 hp) Propeller and Propeller Limits McCauley 1P235PFA80 Static r.p.m. at maximum permissible throttle setting not over 2300 r.p.m., not under 2125 r.p.m. No additional tolerance permitted. Diameter: Not over 80", not under 78.5". or Hartzell HC-C2YK-1/8468A-4 or HC-C2YK-1( )F/F8468A-4 Pitch: High 27° ± 2°, Low 13.5° ± .2° at 30" station. Diameter: Not over 80", not under 80". Governor assembly: Hartzell F-4-3 ( ) or F-4-13 See NOTE 21. or Approved for Use with O-540-B4B5 Engine Only: Sensenich M80BMM or 80BM8 Pitch from 69" to 71". Static r.p.m. at maximum permissible throttle setting not over 2300 r.p.m., not under 2150 r.p.m. No additional tolerances permitted. Diameter: Not over 80", not under 78.5". Propeller Spinner Piper P/N 65209-00 or P/N 63760-03 with fixed pitch propeller. Spinner required. Piper P/N 65435-0 or P/N 68713 or P/N 66785 spinner tip and P/N 66786 spinner shell or P/N 67790-0 spinner, P/N 67791-0 bulkhead, P/N 67793-0 bulkhead and P/N 99499-0 plate. Two each P/N 67794-0 cuff, or Kit 760 452V with constant speed propeller. See NOTE 14. Airspeed Limits Never exceed 197 mph (171 knots) CAS Maximum structural cruising 156 mph (136 knots) CAS Maneuvering 138 mph (120 knots) CAS Flaps Extended 115 mph (100 knots) CAS Center of Gravity Range S/N 28-10001 through 28-11378 (See NOTE 16): (+81.5) to (+93.5) at 2100 lb. or less (+91.5) to (+93.5) at 2900 lb. S/N 28-7110001 through 28-7210023: (+85.1) to (+93.5) at 2100 lb. or less (+86.0) to (+93.5) at 2600 lb. (+91.5) to (+93.5) at 2900 lb. Straight line variation between points given. Empty Weight C. G. Range None Maximum Weight 2900 lb. No. of Seats 4 (2 at +85.5, 2 at +118.1) Maximum Baggage 200 lb. at (+142.8) Page 9 of 47 2A13 Fuel Capacity 84 gallons at (+95) (50 gallons in 2 wing tanks, 34 gallons in 2 tip tanks). See NOTE 1 for data on system fuel. Oil Capacity 12 quarts at (+34.1) (9 ¼ quarts usable) See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (±2°) Up 0° Down 40° Ailerons (±2°) Up 30° Down 15° Rudder (+2°) Left 27° Right 27° Stabilator (±1°) Up 18° Down 2° Stabilator Tab (±1°) Up 3° Down 12° Nose Wheel Travel (±2°) Left 30° Right 30° (Effective on S/N 28-10001 through 28-11039) (2) Left 22° Right 22° (Effective on S/N 28-11040 through 28-11378, and 28-7110001 through 28-7210023) Manufacturer's Serial Nos. 28-10001 through 28-11378, and 28-7110001 through 28-7210023. The manufacturer is authorized to issue airworthiness certificates for airplane serial numbers 28-11063, 28-11064, 28-11070, 28-11072 through 28-11378, and 28-7110001 through 28-7210023 under the delegation option provisions of FAR 21. See NOTE 17 and 20. VII - Model PA-28-140 (Cherokee Cruiser), 2 PCLM (Utility or Normal Category); 1950 lb. Maximum Weight, Approved February 14, 1964; 2150 lb. Maximum Weight, Approved June 17, 1965; for S/N 28-20001 through 28-26946, and 28-7125001 through 28-7725290. Engine Lycoming O-320-E2A with carburetor setting 10-3678-32 or O-320-E3D with carburetor setting 10-5009 Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations 2700 r.p.m (150 hp) Propeller and Propeller Limits For 1950 lb. maximum weight - Normal Category; S/N 28-20001 through 28-20939; or Utility Category, S/N 28-20001 through 28-26946, and 28-7125001 through 28-7725290: Sensenich M74DM or 74DM6 Static r.p.m. at maximum permissible throttle setting not over 2425 r.p.m., not under 2150 r.p.m. No additional tolerance permitted. Diameter: Not over 74", not under 72.5". For 2150 lb. maximum weight - Normal Category; S/N 28-20940 through 28-26946, and 28-7125001 through 28-7725290: Sensenich M74DM or 74DM6 Static r.p.m. at maximum permissible throttle setting not over 2425 r.p.m., not under 2275 r.p.m. No additional tolerance permitted. Diameter: Not over 74", not under 72.5". Propeller Spinner Piper P/N 14422-00. See NOTE 11. Airspeed Limits Never exceed 171 mph (148 knots) CAS Maximum structural cruising 140 mph (121 knots) CAS Maneuvering 129 mph (112 knots) CAS Flaps Extended 115 mph (100 knots) CAS 2A13 Page 10 of 47 Center of Gravity Range Utility Category (+84.0) to (+86.5) at 1650 lb. or less (+85.8) to (+86.5) at 1950 lb. Normal Category (+84.0) to (+95.9) at 1650 lb. or less (+85.9) to (+95.9) at 1975 lb. (+88.4) to (+95.9) at 2150 lb. Straight line variation between points given. 84 86 88 90 92 94 96 2250 2150 2050 1950 1850 1750 1650 Aft Limit Utility Normal & Utility Aft Limit Normal Normal Only Fuselage Station - Inches Lbs. Empty Weight C. G. Range None Maximum Weight Normal Category: 1950 lb. on S/N 28-20001 through 28-20939 (See NOTE 6). 2150 lb. on S/N 28-20940 through 28-26946, and 28-7125001 through 28-7725290. Utility Category: 1950 lb. on S/N 28-20001 through 28-26946, and 28-7125001 through 28-7725290. No. of Seats 2 at (+85.5) Maximum Baggage Eligible Normal Category Only: 100 lb. at (+117) on S/N 28-20001 through 28-20939 (See NOTE 12). 200 lb. at (+117) on S/N 28-20940 through 28-26946, and 28-7125001 through 28-7725290. 300 lb. at (+117 and +133) on S/N 28-20940 through 28-26946, and 28-7125001 through 28-7725290 (See NOTE 13). Fuel Capacity 50 gallon at (+95) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 quarts at (+32.5) (6 quarts usable) See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (±2°) Up 0° Down 40° Ailerons (±2°) Up 30° Down 15° Rudder (±2°) Left 27° Right 27° Stabilator (±1°) Up 18° Down 2° Stabilator Tab (±1°) Up 3° Down 12° Nose Wheel Travel (±2°) Left 30° Right 30° (Effective on S/N 28-20001 through 28-21845; 28-21931 through 28-21934; and 28-7425001 through 28-7725290) (±2°) Left 22° Right 22° (Effective on S/N 28-21846 through 28-21930; 28-21935 through 28-26946; and 28-7125001 through 28-7325674) Page 11 of 47 2A13 Manufacturer's Serial Nos. 28-20001 through 28-26946; and 28-7125001 through 28-7725290. The manufacturer is authorized to issue airworthiness certificates for airplane serial numbers 28-24677, 28-24682, 28-24697, 28-24698, 28-24700, 28-24703, 28-24704, 28-24705, 28-24706, 28- 24709, 28-24710, 28-24712, 28-24713, 28-24714, 28-24715 through 28-26946, and 28- 7125001 through 28-7725290 under the delegation option provisions of FAR 21. See NOTE 17 and 20. VIII - Model PA-28-140 (Cherokee Cruiser), 4 PCLM (Normal Category), 2 PCLM (Utility Category), Approved June 17, 1965, for S/N 28-20001 through 28-26946, and 28-7125001 through 28-7725290. Engine Lycoming O-320-E2A with carburetor setting 10-3678-32 or 10-5009 or O-320-E3D with carburetor setting 10-5009 Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations 2700 r.p.m. (150 hp) Propeller and Propeller Limits Sensenich M74DM or 74DM6 Static r.p.m. at maximum permissible throttle setting not over 2425 r.p.m., not under 2275 r.p.m. No additional tolerance permitted. Diameter: Not over 74", not under 72.5". Propeller Spinner Piper P/N 14422-00. See NOTE 11. Airspeed Limits Never exceed 171 mph (148 knots) CAS Maximum structural cruising 140 mph (121 knots) CAS Maneuvering 129 mph (112 knots) CAS Flaps Extended 115 mph (100 knots) CAS Center of Gravity Range Utility Category (+84.0) to (+86.5) at 1650 lb. or less (+85.8) to (+86.5) at 1950 lb. Normal Category (+84.0) to (+95.9) at 1650 lb. or less (+85.9) to (+95.9) at 1975 lb. (+88.4) to (+95 9) at 2150 lb. Straight line variation between points given. 84 86 88 90 92 94 96 2250 2150 2050 1950 1850 1750 1650 Aft Limit Utility Normal & Utility Aft Limit Normal Normal Only Fuselage Station - Inches Lbs. 2A13 Page 12 of 47 Empty Weight C. G. Range None Maximum Weight Normal Category: 2150 lb. Utility Category: 1950 lb. No. of Seats Normal Category: 4 (2 at +85.5, 2 at +117) Utility Category: 2 (2 at +85.5) Maximum Baggage Eligible Normal Category only: 100 lb. at (+117) on S/N 28-20001 through 28-20939 (See NOTE 12). 200 lb. at (+117) on S/N 28-20940 through 28-26946; and 28-7125001 through 28-7725290. 300 lb. at (+117 and +133) on S/N 28-20940 through 28-26946; and 28-7125001 through 28- 7725290 (See NOTE 13). Fuel Capacity 50 gallons at (+95) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 quarts at (+32.5) (6 quarts usable) See NOTE 1 for data on system oil. Control Surface Movements Wing flaps (±2°) Up 0° Down 40° Ailerons (±2°) Up 30° Down 15° Rudder (±2°) Left 27° Right 27° Stabilator (±1°) Up 18° Down 2° Stabilator Tab (±1°) Up 3° Down 12° Nose Wheel Travel (±2°) Left 30° Right 30° (Effective on S/N 28-20940 through 28-21845; 28-21931 through 28-21934; and 28-7425001 through 28-7725290) ( 2) Left 22° Right 22° (Effective on S/N 28-21846 through 28-21930; 28-21935 through 28-26946; and 28-7125001 through 28-7325674) Manufacturer's Serial Nos. 28-20001 through 28-26946, and 28-7125001 through 28-7725290. The manufacturer is authorized to issue airworthiness certificates for airplane serial numbers 28-24677, 28-24682, 28-24697, 28-24698, 28-24700, 28-24703, 28-24704, 28-24705, 28-24706, 28-24709, 28-24710, 28-24712, 28-24713, 28-24714, 28-24715 through 28-26946, and 28-7125001 through 28-7725290 under the delegation option provisions of FAR 21. See NOTE 17 and 20. IX - Model PA-28R-180 (Arrow), 4 PCLM (Normal Category), Approved June 8, 1967, for S/N 28R-30002 through 28R-31270, and 28R-7130001 through 28R-7130013. Engine Lycoming IO-360-B1E Injector Bendix type RSA-5ADI Parts List No. 2524297 Fuel 100/130 minimum grade aviation gasoline Engine limits For all operations, 2700 r.p.m. (180 hp) Propeller and Propeller Limits Hartzell constant speed Model HC-C2YK-( )/7666A-0 or HC-C2YK-1( )F/F7666A