TCDS 1A10

Page No 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 Rev. No. 53 53 49 49 49 49 49 49 52 52 52 52 52 52 52 52 52 52 52 52 52 46 46 46 46 Page No 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 Rev. No. 46 49 52 52 52 52 52 52 52 52 52 52 46 49 49 49 49 49 51 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A10 Revision 53 Piper Aircraft, Inc PA-23 PA-23-160 PA-23-235 PA-23-250 PA-23-250(Navy UO-1) PA-E23-250 September 15, 2021 AIRCRAFT SPECIFICATION NO. 1A10 Type Certificate Holder Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 Type Certificate Holder Record The New Piper Aircraft, Inc transferred TC 1A10 to Piper Aircraft, Inc on August 7, 2006. I. - Model PA-23, Approved January 29, 1954, 4 PCLM (Normal Category) or 5 PCLM (Normal Category) when Item 605, 609 or 613 is installed. Engines 2 Lycoming O-320 Series ( Item 113A) (Carburetor setting No. 10-3678-11, 10-3678-12 or 10-3678-32) Fuel 80/87 minimum grade aviation gasoline Engine Limits All operations, 2700 r.p.m. (150 hp) Airspeed Limits Vne Never exceed 208 mph (181 knots) (CAS) Vno Maximum structural cruise 165 mph (143 knots) Vle Landing gear extended 125 mph (109 knots) Vp Maneuvering 124 mph (108 knots) Vfe Flaps extended 100 mph (87 knots) Center of Gravity Range (+94.0) to (+100.0) at 3500 lb. (Gear Extended) (+88.5) to (+100.0) at 2450 lb. or less Straight line variation between points given. (Moment due to retracting of landing gear - 760 in.-lb.) Empty Weight C. G. Range None Maximum Weight 3500 lb. See NOTE 3 for eligibility at 3800 lb. No. of Seats 4 (2 at +89, 2 at +126.5) 5 (2 at +89, 2 at +126.5, 1 at +150) when Item 605, 609 or 613 is installed. Maximum Baggage 200 lb. at (+150) (Rear compartment) See NOTE 2 for baggage with rear seat removed. 30 lb. at (+150) (Rear compartment) when Item 605, 609 or 613 installed. 1A10 Page 2 of 54 Fuel Capacity 72 gallons at (+113) (One 36 gallon tank in each wing) See Item 107 for auxiliary fuel tanks. Oil Capacity 4 gallons at (+59) (2 gallons in each engine) Control Surface Main Surfaces Aileron 30° Up 15° Down Movements Elevator 20° Up 15° Down Rudder 30° Left 30° Right Flaps 50° Down Tabs (main surface in neutral) Rudder 25° Left 25° Right Serial Numbers Eligible 23-1 through 23-1182 (except 23-1177). (See NOTE 3 for S/N eligible for 3,800 lb.) Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Items 1(a), 2(a), 3(a), 101(a), 102(a), 103(a), 105(a), 106(a), 201(a), 202(a), 205(a), 206, 301(a), 302(a), and 401(a). II. - Model PA-23-160, Approved October 14, 1957, 4 PCLM (Normal Category) or 5 PCLM (Normal Category) when Item 609 or 613 is installed. Engines 2 Lycoming O-320 Series (Item 113B) (Carburetor setting No. 10-3678-11, 10-3678-12 or 10-3678-32) Fuel 91/96 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (160 hp) Airspeed Limits Vne Never exceed 227 mph (197 knots) (CAS) Vno Maximum structural cruise 180 mph (156 knots) Vp Maneuvering 130 mph (113 knots) Vle Landing gear extended S/N 23-1177, 23-1183 through 23-1773, 23-1775 through 23-1870: 125 mph (109 knots) S/N 23-1774, 23-1871 through 23-2046: 150 mph (130 knots) Vfe Flaps extended S/N 23-1177, 23-1183 through 23-1773, 23-1775 through 23-1870: 100 mph (87 knots) S/N 23-1774, 23-1871 through 23-2046: 125 mph (109 knots) Center of Gravity Range (+95.0) to (+100.0) at 3800 lb. (Gear Extended) (+89.0) to (+100.0) at 2650 lb. or less Straight line variation between points given. (Moment due to retracting of landing gear - 760 in. -lb.) Empty Weight C. G. Range None Maximum Weight 3,800 lb. No. of Seats 4 (2 at +89, 2 at +126.5) 5 (2 at +89, 2 at +126.5, 1 at +150) when Item 609 or 613 is installed. Maximum Baggage 200 lb. at (+150) (Rear compartment) See NOTE 2 for baggage with rear seats removed. 30 lb. at (+150) (Rear compartment) when Item 609 or 613 is installed. Fuel Capacity 72 gallons at (+113) (One 36 gallon tank in each wing) Page 3 of 54 1A10 See Item 107 for auxiliary fuel tanks. Oil Capacity 4 gallons at (+59) (2 gallons each engine) Control Surface Movements Main Surfaces Aileron 30° Up 15° Down Elevator 20° Up 15° Down Rudder 30° Left 30° Right Flaps 50° Down Tabs (main surface in neutral) Rudder 25° Left 25° Right Serial Numbers Eligible 23-1177, 23-1183 through 23-2046. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Items 1(b), 2(a), 3(a), 101(a), 102(a), 103(b), 105(b), 106(a), 110, 201(b), 202(a), 205(a), 206, 301(a), 302(a), and 401(p). III. - Model PA-23-250 (Navy UO-1), Approved September 18, 1959; 5 PCLM (Normal Category) or 6 PCLM (Normal Category), Approved December 15, 1961, when Item 603(b) is installed. Engines 2 Lycoming O-540 series or IO-540 series (Eligible only on S/N 27-2000 through 27-4916, and 27-7304917 through 27-7554168) (See Item 113C) Fuel 91/96 minimum grade aviation gasoline Engine Limits For all operations, 2575 r.p.m. (250 hp) Airspeed Limits Vne Never exceed 249 mph (216 knots) (CAS) Vno Maximum structural cruise 198 mph (172 knots) Vle Landing gear extended 150 mph (130 knots) Vp Maneuvering (4,800 lb.) 145 mph (126 knots) Vp Maneuvering (5,200 lb.) 149 mph (129 knots) Vfe Flaps extended (Full down) 125 mph (109 knots) On S/N 27-2505 through 27-4916, and 27-7304917 through 27-7554168 when Item 625 is installed: Vfe Flaps extended (¼ down) 160 mph (139 knots) Vfe Flaps extended (½ down) 140 mph (122 knots) Center of Gravity Range (+98.0) to (+100.5) at 4,800 lb. (Gear Extended) (+92.5) to (+100.5) at 4,300 lb. (+85.7) to (+100.5) at 3,200 lb. or less S/N 27-2505 through 27-4916, and 27-7304917 through 27-7554168 (See required equipment list for operation at 5,200 lb.) (See NOTE 5 for eligibility for extended C.G. range): (+99.0) to (+100.5) at 5,200 lb. (+97.0) to (+100.5) at 5,000 lb. (+85.7) to (+100.5) at 3,200 lb. or less Straight line variation between points given. (Moment due to retracting of landing gear - 760 in.-lb.) Empty Weight C. G. Range None Maximum Weight 4,800 lb. S/N 27-2505 through 27-4916, and 27-7304917 through 27-7554168: 5,200 lb. - Takeoff (See required equipment list for operation at 5,200 lb.) 4,940 lb. - Landing 1A10 Page 4 of 54 Maximum Weight Maximum permissible weight with zero fuel: (continued) S/N 27-1 through 27-1999: 4,000 lb. S/N 27-2000 through 27-4916, and 27-7304917 through 27-7554168: 4,400 lb. (Normally aspirated) S/N 27-2505 through 27-4916, and 27-7304917 through 27-7554168: 4,500 lb. (Turbocharged) No. of Seats 5 (2 at +89, 2 at +126.5, 1 at +150) for S/N 27-1 through 27-1999 6 (2 at +89, 2 at +126.5, 2 at +157) for S/N 27-2000 through 27-4916, and 27-7304917 through 27-7554168. Maximum Baggage 200 lb. at (+150) (rear compartment) for S/N 27-1 through 27-1999 150 lb. at (+10) (forward compartment) for S/N 27-2000 through 27-4916, and 27-7304917 through 27-7554168 150 lb. at (+183) (rear compartment) for S/N 27-2000 through 27-4916, and 27-7304917 through 27-7554168. Fuel Capacity 144 gallons at (+113) (4 tanks, 2 in each wing, each tank 36 gallons) See NOTE 1 for unusable fuel data. Oil Capacity 6 gallons at (+55) (3 gallons each engine) Control Surface Main Surfaces Aileron 30° Up 15° Down Movements Stabilator (L.E.) 9° Up 9° Down Rudder 30° Left 35° Right Flaps 50° Down Tabs (main surface in neutral) Rudder 25° Left 19° Right Stabilator 8° Up 3° Down Stabilator * 5° Up 6° Down * S/N 27-4426, 27-4574 through 27-4916, and 27-7304917 through 27-7554168 See NOTE 4 for rudder and stabilator balance weights. Serial Numbers Eligible 27-1 through 27-4916, and 27-7304917 through 27-7554168. See NOTE 6 and NOTE 9 for airworthiness certification eligibility in the United States. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed, S/N 27-1 through 27-1999: Items 1(e); 2(d); 3(b); 101(b) or 101(c); 102(b); 103(d); 105(c); 106(a); 201(c); 202(b) or 202(c); 205(b); 206; 301(c); 302(a) or 302(b); 304(b), 304(c) or 304(e); 401(t); 601(c) or 601(d); and 612. S/N 27-2000 through 27-2504: Items 1(e); 2(d); 3(b); 101(b), 101(c) or 101(d); 102(b) or 102(c); 103(d); 105(c), 105(d), 105(f) or 105(h); 106(a); 201(c); 202(b) or 202(e); 205(b); 206; 301(d); 302(b) or 302(c); 304(b), 304(e) or 304(f); 401(z), 601(c) or 601(d), 603(b), and 612. S/N 27-2505 through 27-3836, 27-3838 through 27-3943 at 4,800 lb. Maximum Weight: Items 1(i); 2(e); 3(c); 101(f); 102(e) or 102(f); 103(e); 105(h); 106(e), 106(f) or 106(g); 114; 201(c); 202(b) or 202(c); 205(b); 206; 302(c); 304(b) or 304(e); 305; 401(aq); 601(c); 603(b); 608(c); 612, and 614. S/N 27-2505 through 27-3836, 27-3838 through 27-3943 at 5,200 lb. Maximum Weight: Items 1(i) or 1(j); 2(e); 3(c); 101(f); 102(f) or 102(g); 103(e); 105(h) or 105(i); 106(e), 106(f), 106(g) or 106(h); 114; 201(c) or 201(d); 202(b) or 202(c); 205(b); 206; 302(c); 304(b) or 304(e); 305(a); 401(ax); 601(c); 603(b); 608(c); 612; 614(a); 617; and 618. Page 5 of 54 1A10 Required Equipment (cont) S/N 27-3837, 27-3944 through 27-4425, 27-4427 through 27-4573: Items 1(i) or 1(j); 2(e); 3(c); 101(f); 102(f) or 102(g); 103(e); 105(h) or 105(i); 106(e), 106(g) or 106(h); 114; 201(d); 202(b) or 202(c); 205(b); 206; 302(c); 304(b) or 304(e); 305(b); 401(bv); 601(c); 603(b); 608(c); 612; 614(b); 617; and 618. S/N 27-4426, 27-4574 through 27-4916, and 27-7304917 through 27-7305134: Items 1(m) or 1(o); 2(e); 3(d); 101(f); 102(f); 103(e); 104(c); 105(i); 106(h); 114(a); 201(d); 202(b) or 202(c); 205(b); 206; 302(c); 303(f); 304(b), 304(e) or 306(a); 305(b); 401(c1); 601(c); 603(b); 608(c); 612(b); 617; and 618. S/N 27-7305135 through 27-7554168: Items 1(o); 2(e) or 2(f); 3(d); 101(f); 102(f); 103(e); 104(c); 105(i); 106(h); 114(a); 201(d); 202(b) or 202(c); 205(b); 206; 302(c); 303(f); 305(b); 306(b); and 401(c1). IV. - Model PA-23-235, 5 PCLM (Normal Category), Approved January 22, 1962. Same as Model PA-23-250, 5 PCLM, except for powerplants. Engines 2 Lycoming O-540 series (Item 113D) Carburetor Setting No. IO-4057-1 or IO-4404 Fuel 80/87 minimum grade aviation gasoline Engine Limits All operations, 2575 r.p.m. (235 hp) Airspeed Limits Vne Never exceed 249 mph (216 knots) (CAS) Vno Maximum structural cruise 198 mph (172 knots) Vle Landing gear extended 150 mph (130 knots) Vp Maneuvering 145 mph (126 knots) Vfe Flaps extended (Full down) 125 mph (109 knots) When Item 625 is installed: Vfe Flaps extended (¼ down) 160 mph (139 knots) Vfe Flaps extended (½ down) 140 mph (122 knots) Center of Gravity Range (Landing Gear Extended) (+98.0) to (+100.5) at 4,800 lb. (+92.5) to (+100.5) at 4,300 lb. (+85.7) to (+100.5) at 3,250 lb. or less Straight line variation between points given. (Moment due to retracting of landing gear -760 in.-lb.) Empty Weight C. G. Range None Maximum Weight 4,800 lb. No. of Seats 5 (2 at +89, 2 at +126.5, 1 at +150) Maximum Baggage 200 lb. at (+150) (Rear compartment) Fuel Capacity 144 gallons at (+113) (4 tanks, 2 in each wing, each tank 36 gallons) See NOTE 1 for unusable fuel data. Oil Capacity 6 gallons at (+55) (3 gallons each engine) 1A10 Page 6 of 54 Control Surface Main Surfaces Aileron 30° Up 15° Down Movements Stabilator (L.E.) 9° Up 9° Down Rudder 30° Left 35° Right Flaps 50° Down Tabs (main surface in neutral) Rudder 25° Left 19° Right Stabilator 8° Up 3° Down See NOTE 4 for rudder and stabilator balance weights. Serial Numbers Eligible 27-505 through 27-622. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Items 1(e), 2(d), 3(b), 101(b), 102(b), 103(d), 105(c), 106(a), 201(c), 202(b) or 202(c), 205(b), 206, 301(d), 302(a), 304(b) or 304(e), 401(ac), 601(c), and 612. V. - Model PA-E23-250, 6 PCLM, (Normal Category), Approved June 21, 1965. Engine 2 Lycoming IO-540 series (See Item 113C) Fuel 91/96 min. grade aviation gasoline Engine Limits For all operations, 2575 r.p.m. (250 hp) Airspeed Limits Vne Never exceed 249 mph (216 knots) (CAS) Vno Maximum structural cruise 198 mph (172 knots) Vle Landing gear extended 150 mph (130 knots) Vp Maneuvering 145 mph (126 knots) Vfe Flaps extended (Full down) 125 mph (109 knots) When Item 625 is installed: Vfe Flaps extended (¼ down) 160 mph (139 knots) Vfe Flaps extended (½ down) 140 mph (122 knots) Center of Gravity Range (+97.0) to (+100.5) at 4,995 lb. (Gear Extended) See NOTE 5 for eligibility for extended C. G. Range. (+85.7) to (+100.5) at 3,250 lb. or less Straight line variation between points given. Moment due to retracting of landing gear - 760 in.-lb. Empty Weight C. G. Range None Maximum Weight 4,940 lb. - Landing 4,995 lb. - Takeoff Maximum permissible weight with zero fuel: 4,400 lb. (Normally aspirated) 4,500 lb. (Turbocharged) No. of Seats 6 (2 at +89, 2 at +126.5, 2 at +157) Page 7 of 54 1A10 Maximum Baggage 150 lb. at (+10) (forward compartment) 150 lb. at (+183) (rear compartment) Fuel Capacity 144 gallons at (+113) (4 tanks, 2 in each wing, each tank 36 gallons) See NOTE 1 for unusable fuel data. Oil Capacity 6 gallons at (+55) (3 gallons each engine) Control Surface Movements Main Surfaces Aileron 30° Up 15° Down Stabilator (L.E.) 9° Up 9° Down Rudder 30° Left 35° Right Flaps 50° Down Tabs (main surface in neutral) Rudder 25° Left 19° Right Stabilator 8° Up 3° Down See NOTE 4 for rudder and stabilator balance weights. Serial Numbers Eligible 27-2505 through 27-4916, and 27-7304917 through 27-7554168. For S/N 27-7654001 through 27-8154030, see Section VI. See NOTE 9 for airworthiness certification eligibility in the United States. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: S/N 27-2505 through 27-3836, 27-3838 thorough 27-3943: Items 1(i) or 1(j); 2(e); 3(c); 101(f); 102(f) or 102(g); 103(e); 105(h) or 105(i); 106(e), 106(f), 106(g) or 106(h); 114; 201(c) or 201(d); 202(b) or 202(c); 205(b); 206; 302(c); 304(b) or 304(e); 305(a); 401(bh); 601(c); 603(b); 608(c); 612; 614(a); 617; and 618. S/N 27-3944 through 27-4425, 27-4427 through 27-4573: Items 1(i) or 1(j); 2(e); 3(c); 101(f); 102(f) or 102(g); 103(e); 105(h) or 105(i); 106(e), 106(g) or 106(h); 114; 201(d); 202(b) or 202(c); 205(b); 206; 302(c); 304(b) or 304(e); 305(b); 401(ca); 601(c); 603(b); 608(c); 612; 614(b); 617; and 618. S/N 27-4574 through 27-4916, and 27-7304917 through 27-7554168: Items 1(i) or 1(j); 2(e); 3(c); 101(f); 102(f); 103(e); 104(c); 105(i); 106(e) or 106(h); 114(a); 201(d); 202(b) or 202(c); 205(b); 206; 302(f); 304(b), 304(e) or 306(b); 401(cm); 601(c); 603(b); 608(c); 612; 617; and 618. VI. - Model PA-23-250, 6 PCLM, (Normal Category), Approved January 21, 1975. Same as Model PA-23-250 (6 PCLM), S/N 27-2505 through 27-4916, and 27-7304917 through 27-7554168, at 5,200 lb. maximum weight except required equipment. Engines 2 Lycoming I-540 series (See Item 113C) Fuel 91/96 minimum grade aviation gasoline Engine Limits All operations 2575 r.p.m. (250 hp) Airspeed Limits Vne Never exceed 249 mph (216 knots) (CAS) Vno Maximum structural cruise 198 mph (172 knots) Vle Landing gear extended 150 mph (130 knots) Vp Maneuvering 149 mph (129 knots) Vfe Flaps extended (full down) 125 mph (109 knots) Vfe Flaps extended (¼ down) 160 mph (139 knots) Vfe Flaps extended (½ down) 140 mph (122 knots) 1A10 Page 8 of 54 Center of Gravity Range (+99.0) to (+100.5) at 5,200 lb. ( Gear Extended) (+97.0) to (+100.5) at 5,000 lb. (+87.6) to (+100.5) at 3,540 lb. or less Straight line variation between points given. See NOTE 8 for eligibility for extended C. G. range. Moment due to retraction of landing gear is - 760 in.-lb. Empty Weight C.G. Range None Maximum Weight 5,200 lb. - Takeoff 4,940 lb. - Landing Maximum permissible weight with zero fuel: 4,400 lb. (normally aspirated) 4,500 lb. (turbocharged) No. of Seats 6 (2 at +89, 2 at +126.5, 2 at +157) Maximum Baggage 150 lb. at (+10) (forward compartment) 150 lb. at (+183) (rear compartment) Fuel Capacity 144 gallons at (+113) (4 tanks, 2 in each wing, each tank 36 gallons) (Each tank 34.3 gallons usable) See NOTE 1 for unusable fuel data. See Item 107(b) for optional fuel tanks. Oil Capacity 6 gallons at (+55) (3 gallons each engine) Control Surface Main Surfaces Aileron 30° Up 15° Down Movements Stabilator (L.E.) 9° Up 9° Down Rudder 30° Left 35° Right Flaps 50° Down Tabs (Main Surfaces Neutral) S/N 27-7654001 through 27-7854083, 27-7854085 through 27-8054000: Stabilator 3° 30' (+30', -0') (T. E. Up) 9° 30 ( 1°) (T. E Down) S/N 27-7854084, 27-8054001 through 27-8154030: Stabilator 5° ( 30') (T. E. Up) 6° ( 1°) (T. E Down) NOTE: Stabilator-flap trim interconnect must be rigged so that 50° of down flaps result in a stabilator trim tab position of 3.5°(T.E. Up). Rudder 25° Left 19° Right See NOTE 7 for Balance Requirements. Serial Numbers Eligible 27-7654001 through 27-8154030. See NOTE 9 for airworthiness certification eligibility in the United States. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the basic following items of equipment must be installed: Items 1(o); 2(f); 3(d); 101(g); 102(f); 103(g); 104(c), 104(d), 104(e) or 104(f); 105(j); 106(h); 201(f); 202(b) or 202(c); 205(c); 206(a); 302(d); 305(c); 307; 401(db); 603(b); 608(d); 612(b); 614(c); and 617. Page 9 of 54 1A10 Specifications Pertinent to All Models Datum 80 inches ahead of the wing leading edge outboard of tapered sections. Leveling Means Level from two rivnuts located right side of fuselage under stabilizer. Certification Basis Type Certificate No. 1A10 (CAR 3, dated November 1, 1949, including Amendments 3-1 through 3-9, dated December 15, 1952) S/N 27-2505 through 27-4916, and 27-7304917 through 27-8154030: CAR 3.242(a) as amended by Amendment 3-14, dated March 13, 1956, superseding original CAR 3.242. Production Basis Approved for manufacture of spare parts only under Production Certificate Number 206. Equipment A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by someone other than the aircraft manufacturer. An item marked with an asterisk may not have been manufactured under an FAA monitored or approved quality control system, and therefore conformity must be determined if the item is not identified by an FAA Form 8130-3, FAA-PMA or other evidence of FAA production approval. PA-23, PA-23-160 PA-23-235, PA-E23-250 PA-23-250, PA-23-250(NAVY UO-1) Propellers and Propeller Accessories 1. Two full feathering, constant speed propeller installations (a) Hartzell HC-82XG-2 with 7636D blades (Not eligible for Models PA-23 or PA-23-160, S/N 23-1068, and 23-1152 through 23-2046). Pitch settings at 30 in. station: Low 10°, High 80.5° (feathered). Diameter: Not over 76 inches, not under 74.5 inches. 63 lb. ea. (+35) ---- (b) Hartzell HC-82XG-2B with 7636D-4 blades. Pitch settings at 30 in station: Low 12°, High 80° (feathered). Diameter: Not over 72 inches, not under 70 inches. Item 401(j) required with Model PA-23 only. 63 lb. ea. (+35) ---- (c) Hartzell HC-82XL-2B with 7636D-4 blades. Pitch settings at 30 in station: Low 12°, High 80° (feathered). Diameter: Not over 72 inches, not under 70 inches. Item 401(j) required with Model PA-23 only. 63 lb. ea. (+35) ---- (d) Hartzell HC-82XL-2C with 7636D-4 blades. Pitch settings at 30 in station: Low 12°, High 80° (feathered). Diameter: Not over 72 inches, not under 70 inches. Item 401(j) required with Model PA-23 only. 63 lb. ea. (+35) ---- (e) Hartzell HC-82XK-2C1 with 8433-10 blades. Pitch settings at 30 in station: Low 15.5°, High 80° (feathered). Diameter: Not over 74 inches, not under 73 inches. Not eligible on Model PA-23-250, S/N 27-2505 through 27-4916, and 27-7304917 through 27- 8154030. 66 lb. ea. ---- (+29) 1A10 Page 10 of 54 PA-23, PA-23-160 PA-23-235, PA-E23-250 PA-23-250, PA-23-250(NAVY UO-1) Propellers and Propeller Accessories (continued) (f) Hartzell HC-A2XK-2 with 8433-10 blades. Pitch settings at 30 in station: Low 15.5°, High 80° (feathered). Diameter: Not over 74 inches, not under 73 inches. Not eligible on Model PA-23-250, S/N 27-2505 through 27-4916, and 27-7304917 through 27-8154030. 66 lb. ea. ---- (+29) (g) Hartzell HC-A2XL-2 with 7636D-4 blades. Pitch settings at 30 in station: Low 12°, High 80° (feathered). Diameter: Not over 72 inches, not under 70 inches. 63 lb. ea. (+35) ---- (h) Hartzell HC-A2XL-2 with 8433B-10 blades (24-v system. only). Pitch settings at 30 in station: Low 15.5°, High 80° (feathered). Diameter: Not over 74 inches, not under 73 inches. Item 401(w) and NOTE 2 (p) placard required. Eligible only on Model PA-23-250, S/N 27-1 through 27-1999. 67.5 lb. ea. ---- (+29) (i) Hartzell HC-E2YK-2RB with 8465-7R blades. Pitch settings at 30 in station: Low 14.5°, High 80° (feathered). Diameter: Not over 77 inches, not under 76 inches. Eligible only on Models PA-23-250 and PA-E23-250, S/N 27-2505 through 27-4916, and 27-7304917 through 27-8154030. Not eligible when Item 113C(g), 113C(h), or 113C(i) is installed. Not to be intermixed with Item 1(l), 1(m), or 1(o). 58.5 lb. ea. ---- (+24) (j) Hartzell HC-E2YR-2RB with 8465-7R blades. Pitch settings at 30 in. sta.: Low 14.5°, High 80° (feathered). Diameter: Not over 77 inches, not under 76 inches. Eligible only on Models PA-23-250 and PA-E23-250, S/N 27-2505 through 27-4916, and 27-7304917 through 27-8154030. Not eligible when Item 113C(g), 113C(h), or 113C(i) is installed. Not to be intermixed with Item 1(l), 1(m), or 1(o). 58.5 lb. ea. ---- (+24) (k) Hartzell HC-E2YR-2RB with 8465-7R blades. Pitch settings at 30 in. station: Low 15.2°, High 80° (feathered). Diameter: Not over 77 inches, not under 76 inches. Eligible only when 113C(g) is installed. Not to be intermixed with Item 1(n) or 1(p). 58.5 lb. ea. ----- (+24) (l) Hartzell HC-E2YK-2RBS with 8465-7R blades. Pitch settings at 30 in. station: Low 14.5°, High 80° (feathered). Diameter: Not over 77 inches, not under 76 inches. Eligible only on Models PA-23-250 and PA-E23-250, S/N 27-2505 through 27-4916, and 27-7304917 through 27-8154030. Not eligible when Item 113C(g), 113C(h), or 113C(i) is installed. Not to be intermixed with Items 1(i), 1(j), or 1(o). 60.25 lb. ea. ---- (+24) (m) Hartzell HC-E2YR-2RBS with 8465-7R blades. Pitch settings at 30 in. station: Low 14.5°, High 80° (feathered). Diameter: Not over 77 inches, not under 76 inches. Eligible only on Models PA-23-250 and PA-E23-250, S/N 27-2505 through 27-4916, and 27-7304917 through 27-8154030. Not eligible when Item 113C(g), 113C(h), or 113C(i) is installed. Not to be intermixed with Items 1(i) or 1(j). 60.25 lb. ea. ----- (+24) Page 11 of 54 1A10 PA-23, PA-23-160 PA-23-235, PA-E23-250 PA-23-250, PA-23-250(NAVY UO-1) Propellers and Propeller Accessories (continued) (n) Hartzell HC-E2YR-2RBS with 8465-7R blades. Pitch settings at 30 in station: Low 15.2°, High 80° (feathered). Diameter: Not over 77 inches, not under 76 inches. Eligible only when Item 113C(g) is installed. Not be intermixed with Item 1(k). 60.25 lb. ea. ---- (+24) (o) Hartzell HC-E2YR-2RBSF with F8465-7R blades. Pitch settings at 30 in station: Low 14.5°, High 80° (feathered). Diameter: Not over 77 inches, not under 76 inches.