TCDS A19SO

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 Rev. No. 23 9 18 10 17 6 17 17 17 18 23 23 23 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A19SO Revison 23 Piper Aircraft, Inc PA-44-180 PA-44-180T September 29, 2026 TYPE CERTIFICATE DATA SHEET NO. A19SO This data sheet, which is part of Type Certificate No. A19SO, prescribes conditions and limitations under which the product for which 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 A19SO to Piper Aircraft, Inc on August 7, 2006. IA. - Model PA-44-180, Seminole, 4 PCLM (Normal Category), Approved March 10, 1978. Engine 1 Lycoming O-360-E1A6D with carburetor setting 10-5092, 10-5219, or 10-6019 (Left Side) 1 Lycoming LO-360-E1A6D with carburetor setting 10-5092, 10-5219, or 10-6019 (Right Side) Fuel 100 or 100LL aviation grade fuel Engine Limits For all operations, 2700 r.p.m. (180 hp) Propeller and Propeller Limits Left Engine: 1 Hartzell, Hub Model HC-C2Y(K, R) -2CEUF, Blade Model FC7666A-2R or Hub Model HC-C3YR-2EUF, Blade Model FC7663-5R Right Engine: 1 Hartzell, Hub Model HC-C2Y(K, R) -2CLEUF, Blade Model FJC7666A-2R or Hub Model HC-C3YR-2LEUF, Blade Model FJC7663-5R Pitch Setting at 30" Station: Two-Blade Three-Blade High 79° - 81°, Low 12.4° ± 0.2° High 81° - 83°, Low 10.6° ± .1° Diameter: Not over 74 inches Diameter: Not over 73 inches Not under 72 inches Not under 72 inches Spinner: Two-Blade Three-Blade Hartzell P/N C-2285-3 Spinner Assy (Left) Hartzell P/N C-2285-3L Spinner Assy (Right) Hartzell P/N C-4558 Spinner Assy (Left) Hartzell P/N C4-558 Spinner Assy (Right) See NOTE 4. See NOTE 4. Governor Assembly: 1 Hartzell Hydraulic Governor Model E-3-2 (Left) 1 Hartzell Hydraulic Governor Model E-3-2L (Right) or 1 Hartzell Hydraulic Governor Model E-8-2L (Right) with synchrophaser (Piper Drawing No. 36889 Synchrophaser Installation, S/N 44-7995278 and up) A19SO Page 2 of 13 Airspeed Limits VNE (Never Exceed) 202 KIAS VNO (Maximum Structural Cruise) 169 KIAS VA (Maneuvering 3800 lb.) 135 KIAS VA (Maneuvering 2700 lb.) 112 KIAS VFE (Maximum Flaps Extended) 111 KIAS VLO (Maximum Landing Gear Operation) Extension 140 KIAS Retraction 109 KIAS VLE (Maximum Landing Gear Extended) 140 KIAS VMC (Minimum Control Speed) 56 KIAS C.G. Range (+89.0) to (+93.0) at 3800 lb. (+85.0) to (+93.0) at 3400 lb. (+84.0) to (+93.0) at 2800 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+819 in-lb.) 1800 2800 3400 LB 89.0 93.0 LB 3800 3400 2800 1800 INCHES 85.0 84.0 Empty Weight C.G. Range None Maximum Weight Ramp 3816 lb. Takeoff 3800 lb. Landing 3800 lb. Number of Seats 4 (2 at +80.5, 2 at +118.1) Maximum Baggage 200 lb. at +142.8 Fuel Capacity 110 gallons (2 nacelle tanks) at +95.0 (108 gallons usable) (See NOTE 1 for data on system fuel) Oil Capacity 6 quarts per engine (4 quarts per engine usable) (See NOTE 1 for data on system oil) Control Surface Movements Ailerons Up 23° (±2°) Down 17° (±2°) Stabilator Up 15° (±1°) Down 3° (±1°) Rudder Left 37° (+1°, -0°) Right 37° (+1°, -0°) Stabilator Trim Tab Down 9° (±1°) Up 4° (±1°) (Stabilator neutral) Wing Flaps Up 0° (±1°) Down 10°, 25°, 40° (±2°) Rudder Trim Tab Left 26° (±2°) Right 26° (±2°) (Rudder neutral) Nose Wheel Travel Left 30° (±1°) Right 30° (±1°) Manufacturer's Serial Numbers 44-7995001 through 44-8195026 (See NOTE 5 for airworthiness certification eligibility in the United States) Page 3 of 13 A19SO IB. - Model PA-44-180, Seminole, 4 PCLM (Normal Category), Approved March 10, 1978. Engine (See Note 6) 1 Lycoming O-360-A1H6 with carburetor setting 10-5219 or 10-6019 (Left Side) 1 Lycoming LO-360-A1H6 with carburetor setting 10-5219 or 10-6019 (Right Side) OR 1 Lycoming IO-360-B1G6 (Left Side) with fuel injector model RSA-5AD1, (Lycoming Part Number 61J28856) 1 Lycoming LIO-360-B1G6 (Right Side) with fuel injector model RSA-5AD1 (Lycoming Part Number 61J28856) Fuel 100 or 100LL aviation grade fuel Engine Limits For all operations, 2700 r.p.m. (180 hp) Propeller and Propeller Limits Left Engine: 1 Hartzell, Hub Model HC-C2Y(K, R) -2CEUF, Blade Model FC7666A-2R or 1 Hartzell Hub Model HC-C2YR-2CEUFP, Blade Model FC7497 *Hubs and blades must be both of same model both left and right; no intermixing Right Engine: 1 Hartzell, Hub Model HC-C2Y(K, R) -2CLEUF, Blade Model FJC7666A-2R or 1 Hartzell Hub Model HC-C2YR-2CLEUFP, Blade Model FJC7497 *Hubs and blades must be both of same model both left and right; no intermixing Pitch Setting at 30" Station: Blade Model FC7666A-2R Blade Model F(J)C7497 High 79° - 81°, Low 12.4° ± 0.2° High 79° - 81°, Low 12.8° ± 0.2° Diameter:Not over 74 inches Diameter:Not over 74 inches Not under 72 inches Not under 72.5 inches Spinner: Hartzell P/N C-2285-3 Spinner Assy (Left)* Hartzell P/N C-2285-3L Spinner Assy (Right)* *See Note 4 for carburated engines only (no intermixing permitted) or Hartzell P/N D-6974-1P (Left & Right) ** **no intermixing permitted with C-2285-3(L) Governor Assembly: 1 Hartzell Hydraulic Governor Model U-3-15 (Left) with unfeathering accumulator 1 Hartzell Hydraulic Governor Model U-3-15L (Right) with unfeathering accumulator Airspeed Limits VNE (Never Exceed) 202 KIAS VNO (Maximum Structural Cruise) 169 KIAS VA (Maneuvering - 3800 lb.) 135 KIAS VA (Maneuvering - 2700 lb.) 112 KIAS VFE (Maximum Flaps Extended) 111 KIAS VLO (Maximum Landing Gear Operation) Extension 140 KIAS Retraction 109 KIAS VLE (Maximum Landing Gear Extended) 140 KIAS VMC (Minimum Control Speed) 56 KIAS C.G. Range (+89.0) to (+93.0) at 3800 lb. (+85.0) to (+93.0) at 3400 lb. (+84.0) to (+93.0) at 2800 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+819 in-lb.) A19SO Page 4 of 13 89.0 93.0 LB 3800 3400 2800 1800 INCHES 85.0 84.0 1800 2800 3400 LB Empty Weight C.G. Range None Maximum Weight Ramp 3816 lb. Takeoff 3800 lb. Landing 3800 lb. Number of Seats 4 (2 at +80.5, 2 at +118.1) Maximum Baggage 200 lb. at +142.8 Fuel Capacity 110 gallons (2 nacelle tanks) at +95.0 (108 gallons usable) (See NOTE 1 for data on system fuel) Oil Capacity 8 quarts per engine (6 quarts per engine usable) (See NOTE 1 for data on system oil) Control Surface Movements Ailerons Up 23° (±2°) Down 17° (±2°) Stabilator Up 15° (±1°) Down 3° (±1°) Rudder Left 37° (+1°, -0°) Right 37° (+1°, -0°) Stabilator Trim Tab Down 9° (±1°) Up 4° (±1°) (Stabilator neutral) Wing Flaps Up 0° (±1°) Down 10°, 25°, 40° (±2°) Rudder Trim Tab Left 26° (±2°) Right 26° (±2°) (Rudder neutral) Nose Wheel Travel Left 30° (±1°) Right 30° (±1°) Manufacturer's Serial Numbers 4495001 through 4495013, and 4496001 and up II. - Model PA-44-180T, Turbo Seminole, 4 PCLM (Normal Category), Approved November 29, 1979. Engine 1 Lycoming TO-360-E1A6D with carburetor setting 10-5256 1 Lycoming LTO-360-E1A6D with carburetor setting 10-5256 Fuel 100 or 100LL aviation grade fuel Engine Limits For all operations, 36.5 in. Hg at 2575 r.p.m. (180 hp) Propeller and Propeller Limits Left Engine: 1 Hartzell, Hub Model HC-C2YR -2C ( )UF, Blade Model FC7666A-2R or FC7666AB-2R Right Engine: 1 Hartzell, Hub Model HC-C2YR-2CL ( ) UF, Blade Model FJC7666A-2R or FJC7666AB-2R Governor Assembly: 1 Hartzell Hydraulic Governor Model E-3-5 (Left) or 1 Hartzell Hydraulic Governor Model U-3-10 (Left) with unfeathering accumulator Page 5 of 13 A19SO 1 Hartzell Hydraulic Governor Model E-3-5L (Right) or 1 Hartzell Hydraulic Governor Model U-3-10L (Right) with unfeathering accumulator or 1 Hartzell Hydraulic Governor Model E-8-5L (Right) with Synchrophaser Installation, Piper Dwg. 86818-2 or 1 Hartzell Hydraulic Governor Model U-8-10L (Right) with unfeathering accumulator and Synchrophaser Installation, Piper Dwg. 86818-2 Propeller and Propeller Limits Pitch Setting at 30" Station: (continued) High 79° - 81°, Low 13.1° ± 0.2° Diameter: Not over 74 inches Not under 72 inches Spinner: Hartzell P/N C-2285-3 Spinner Assy (Left) Hartzell P/N C-2285-3L Spinner Assy (Right) See NOTE 4. Left Engine: 1 Hartzell, Hub Model HC-C3YR -2 ( )UF, Blade Model FC7663-5R or FC7663B-5R Right Engine: 1 Hartzell, Hub Model HC-C3YR-2L ( ) UF, Blade Model FJC7663-5R or FJC7663B-5R Governor Assembly: 1 Hartzell Hydraulic Governor Model E-3-5 (Left) or 1 Hartzell Hydraulic Governor Model U-3-10 (Left) with unfeathering accumulator 1 Hartzell Hydraulic Governor Model E-3-5L (Right) or 1 Hartzell Hydraulic Governor Model U-3-10L (Right) with unfeathering accumulator or 1 Hartzell Hydraulic Governor Model E-8-5L (Right) with Synchrophaser Installation, Piper Dwg. 86818-2 or 1 Hartzell Hydraulic Governor Model U-8-10L (Right) with unfeathering accumulator and Synchrophaser Installation, Piper Dwg. 86818-2 Pitch Setting at 30" Station: High 81° - 83°, Low 11.2° ± 0.1° Diameter: Not over 73 inches Not under 72 inches Spinner: Hartzell P/N C-4558 Spinner Assy (Left) Hartzell P/N C-4558 Spinner Assy (Right) See NOTE 4. "Avoid continuous operation at manifold pressures below 15" Hg above 12,000 feet altitude." Airspeed Limits VNE (Never Exceed) 202 KIAS VNO (Maximum Structural Cruise) 170 KIAS VA (Maneuvering - 3925 lb.) 137 KIAS VA (Maneuvering - 2700 lb.) 112 KIAS VFE (Maximum Flaps Extended) 111 KIAS VLO (Maximum Landing Gear Operation) Extension 140 KIAS Retraction 109 KIAS VLE (Maximum Landing Gear Extended) 140 KIAS VMC (Minimum Control Speed) 57 KIAS A19SO Page 6 of 13 C.G. Range (+89.7) to (+93.0) at 3925 lb. (+87.3) to (+93.0) at 3800 lb. (+85.0) to (+93.0) at 3400 lb. (+83.0) to (+93.0) at 2700 lb. or less 89.7 93.0 3925 2400 INCHES 85.0 83.0 2400 87.33925 34003400 27002700 3800 LB. Empty Weight C.G. Range None Maximum Weight Ramp 3943 lb. Takeoff 3925 lb. Landing 3800 lb. Number of Seats 4 (2 at +80.5, 2 at +118.1) Maximum Baggage 200 lb. at +142.8 Fuel Capacity 110 gallons (2 nacelle tanks) at +95.0 (108 gallons usable) (See NOTE 1 for data on system fuel) Oil Capacity 6 quarts per engine (4 quarts per engine usable) (See NOTE 1 for data on system oil) Maximum Operating Altitude 20,000 feet Control Surface Movements Ailerons (±2°) Up 23° Down 17° Stabilator (±1°) Up 15° Down 3° Rudder (+1°, -0°) Left 37° Right 37° Stabilator Trim Tab (±1°) Up 4 Down 9° (Stabilator neutral) Wing Flaps (±2°) Up 0° Down 40° Rudder Trim Tab (±2°) Left 26° Right 26° (Rudder neutral) Nose Wheel Travel (±1°) Left 30° Right 30° Manufacturer's Serial Numbers 44-8107001 through 44-8207020 DATA PERTINENT TO ALL MODELS Datum 78.4" forward of wing leading edge at wing station 106. Leveling Means Two screws left side fuselage below window. Page 7 of 13 A19SO Certification Basis Type Certificate No. A19SO issued March 10, 1978. Date of application for Type Certificate, January 17, 1976. PA-44-180: Federal Aviation Regulations (FAR) Part 23 effective February 1, 1965, through Amendment 23-16 effective February 14, 1975; FAR 23.1557(c)(1) as amended by Amendment 23-18 effective May 2, 1977; and FAR 36 effective December 1, 1969, through Amendment 36-4, effective February 3, 1975. Equivalent Safety Finding: FAR 23.1545(a). PA-44-180T: FAR 23 effective February 1, 1965, through Amendment 23-16 effective February 14, 1975; FAR 23.207 and 23.1091 as amended by Amendment 23-7 effective September 14, 1969; FAR 23.201 and 23.203 as amended by Amendment 23-14 effective December 20, 1973; FAR 23.1093 and 23.1557(c)(1) as amended by Amendment 23-18 effective May 2, 1977; FAR 23.1581(b)(2) as amended by Amendment 23-21 effective March 1, 1978; FAR 23.1545(a) as amended by Amendment 23-23 effective December 1, 1978; and FAR 36 effective December 1, 1969, through Amendment 36-9 effective April 3, 1978. Compliance with FAR 23.1441 as amended by Amendment 23-9 effective June 17, 1970, shown with optional supplemental oxygen. For PA-44-180 aircraft equipped with Piper factory installed Avidyne Entegra Systems (see Piper Report VB-1940), the additional certification basis for installation specific items only is: FAR 23.1301, 23.1327, and 23.1335 as amended by Amendment 23-20 effective September 1, 1977; FAR 23.1501 and 23.1541(a)(b) as amended by Amendment 23-21 effective March 1, 1978; FAR 23.603 and 23.605(a) as amended by Amendment 23-23 effective October 10, 1978; FAR 23.1529 as amended by Amendment 23-26 effective October 14, 1980; FAR 23.1523 as amended by Amendment 23-34 effective February 17, 1987; FAR 23.1322, 23.1331 and 23.1357(a)(2)(b)(c)(d) as amended by Amendment 23-43 effective May 10, 1993; FAR 23.305, 23.613, 23.773(a)(1)(2), 23.1525 and 23.1549(a)(b)(c) as amended by Amendment 23-45 effective September 7, 1993; FAR 23.301, 23.337(a)(1)(b)(1), 23.341(a), 23.473, 23.561(b)(3)(e), 23.607 and 23.611 as amended by Amendment 23-48 effective March 11, 1996; FAR 23.1303(a)(b)(f), 23.1307, 23.1309(a)(1)(3)(b)(c)(1)(2)(i)(iii)(3)(d)(e), 23.1311, 23.1321, 23.1323(a)(c), 23.1329(d)(e)(f)(g)(h), 23.1351(a)(1)(2)(i)(b)(1)(i)(2)(3)(d), 23.1353(d)(h), 23.1359(c), 23.1361(a)(b), 23.1365(a)(b)(d)(e)(f) and 23.1431(a)(b)(d)(e) as amended by Amendment 23-49 effective March 11, 1996; FAR 23.1325(a)(b)(1)(2)(i)(3), 23.1543(b)(c), 23.1545(a)(b), 23.1553, 23.1555(a)(b), 23.1581(a)(b)(2)(3)(f), 23.1583(m) and 23.1585(j) as amended by Amendment 23-50 effective March 11, 1996; FAR 23.777(a)(b), 23.955(a)(3) and 23.1337(a)(b)(1)(4)(c) as amended by Amendment 23-51 effective March 11, 1996; 23.1305(a)(1)(2)(3)(b)(2)(3)(i)(4)(i)(5) as amended by Amendment 23-52 effective July 25, 1996; and Special Condition for HIRF (Docket No. CE238, Special Condition 23- 178-SC), January 13, 2006. Eligible Serial Numbers 4496174, 4496224 and up. For PA-44-180 aircraft equipped with Piper factory installed Garmin G500 (see Piper Report VB-2314), the additional certification basis for installation specific items only is: {Unless otherwise noted in the table below, all sections are Amendment 23-16} Section Amendment Section Amendment 23.301 (a),(b),(c) 23-48 23.611 23-48 23.303 23.771(a) 23.305(a) 23-45 23.773(a)(2) 23-45 23.307(a) 23.777(a),(b) 23-51 23.337 23-48 23.867(a),(b),(c) 23-49 23.561(a),(b)(3) 23-48 23.1301 23-20 23.603 23-23 23.1303(a),(b),(c),(f) 23-49 23.605(a) 23-23 23.1307 23-49 23.607(a) 23-48 23.1308(a),(b),(c) 23-57 23.609 23.1309(a)(1)(3),(b) (c),(d),(e) 23-49 A19SO Page 8 of 13 Additional certification basis for installation specific items only (continued): {Unless otherwise noted in the table below, all sections are Amendment 23-16} Section Amendment Section Amendment 23.1311(a)(1)(2)(3)(4) (5)(6),(b),(c) 23-49 23.1367 23.1321(a)(b)(c)(d) (e)(f) 23-49 23.1381(a),(b) 23.1322(a),(b),(c),(d) (e) 23-43 23.1431(a),(b) 23-49 23.1323(a),(c) 23-49 23.1501 23-21 23.1325(b)(1),(b)(2)(i),(e) 23-50 23.1523 23-34 23.1327(a) 23-20 23.1525 23-45 23.1329(h) 23-49 23.1529 23-26 23.1331(a),(b)(1) 23-43 23.1541(a),(b) 23-21 23.1335 23-20 23.1543(b),(c) 23-50 23.1351(a)(1),(a)(2)(i) 23-49 23.1545(a),(b) 23-50 23.1353(h) 23-49 23.1559(c) 23-50 23.1357(a),(b),(d) 23-43 23.1581(a),(b),(c),(f) 23-50 23.1359(c) 23-49 23.1583(h),(m) 23-50 23.1365(a),(b),(d),(e) 23-49 23.1585(j) 23-50 Eligible Serial Numbers 4496325 and up. For PA-44-180 aircraft equipped with Piper factory installed Garmin G1000 Integrated Avionics System and 28 Volt Electrical System, the additional certification basis for installation specific items only is: 14 CFR Part 23 regulations: 23.21, 23.23(a), 23.25, 23.29, 23.207(a), 23.251, 23.301(a)(b)(c), 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.421(a), 23.473, 23.561(a)(b)(3)(e), 23.601, 23.603, 23.605(a), 23.607, 23.609, 23.611, 23.613, 23.625, 23.627, 23.729(e)(f), 23.771(a), 23.773(a)(1)(2), 23.777(a)(b), 23.867, 23.1041, 23.1043(a)(b)(c)(d), 23.1047, 23.1163(a)(b)(d), 23.1301, 23.1305(a)(1)(2)(3)(b)(2)(3)(i)(4)(i)(b)(5), 23.1306, 23.1307, 23.1308(a)(b)(c), 23.1309(a)(1)(3)(b)(c)(d)(e), 23.1311, 23.1321, 23.1322, 23.1323(a)(c), 23.1325(a)(b)(1)(2)(i), 23.1326, 23.1327(a), 23.1329(d)(g)(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i)(b)(1)(i)(3)(c)(4)(d), 23.1353, 23.1357, 23.1359(c), 23.1361(a)(c), 23.1365, 23.1367, 23.1381, 23.1431(a)(b)(e), 23.1501, 23.1507, 23.1523, 23.1525, 23.1529, 23.1541(a)(b), 23.1543(b)(c), 23.1545(a)(b), 23.1549(a)(b)(c), 23.1553, 23.1555(a)(b)(e)(1), 23.1563(a)(b), 23.1567(a), 23.1581(a)(c), 23.1583(g)(h)(m), 23.1585(j), 23.1589 as amended by Amdt. 23-61; 23.1303(a)(b)(c)(f) as amended by Amdt. 23-62. Eligible Serial Numbers: 4496331, 4496339 and up. For PA-44-180 aircraft equipped with Piper factory installed Garmin GFC700 Autopilot, the additional certification basis for installation specific items only is: 14 CFR Part 23 regulations: 23.21(b), 23.23(a)(b)(3), 23.25(a)(b), 23.29, 23.143(a)(b), 23.207(a)(b)(c)(d)(e), 23.301(a)(b)(c), 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.397, 23.399, 23.473, 23.561(a)(b)(3)(e), 23.601, 23.603, 23.605(a), 23.607, 23.609, 23.611, 23.613, 23.625, 23.627, 23.681, 23.683, 23.693, 23.771(a), 23.777(a)(b), 23.779(a)(2), 23.867, 23.1141(d), 23.1301(a)(b)(c)(d), 23.1306, 23.1308(a)(b)(c), 23.1309(a)(1)(3)(b)(1)(3)(c)(d)(e), 23.1321(c), 23.1322(a)(b)(c)(d)(e), 23.1329(a)(1)(b)(c)(d)(e)(f)(g)(h), 23.1335, 23.1351(a)(1)(2)(i), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365, 23.1367(a)(b)(c)(d), 23.1431(a)(b)(e), 23.1501, 23.1523, 23.1525, 23.1529, 23.1541(a)(b), 23.1555(a), 23.1581(a), 23.1583(g)(h)(m), 23.1585(a)(1)(j) as amended by Amdt. 23-61. Eligible Serial Numbers: 4496331, 4496367 and up. Page 9 of 13 A19SO For PA-44-180 aircraft equipped with Piper factory installed Garmin G1000NXi Phase I as installed by Piper drawing number 107600-002, the additional certification basis for installation specific items only is: 14 CFR Part 23 regulations: 23.21, 23.23(a), 23.25(a)(b), 23.29, 23.251, 23.301(a)(b)(c), 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.421(a), 23.473, 23.561(a)(b)(3)(e), 23.601, 23.603, 23.605(a), 23.607, 23.609, 23.611, 23.613, 23.625, 23.627, 23.729(e)(f), 23.771(a), 23.773(a)(2), 23.777(a)(b), 23.867, 23.903(a), 23.1041, 23.1043(a)(b)(c), 23.1047, 23.1163(a)(b)(d), 23.1301(a)(b)(c)(d), 23.1305(a)(1)(2) (3)(b)(2)(3)(i)(4)(i)(5), 23.1306, 23.1307, 23.1308(a)(b)(c), 23.1309(a)(1)(3)(b)(c)(d)(e), 23.1311(a)(1)(2)(3)(4)(6)(7)(b)(c), 23.1321(a)(b)(c)(d)(5)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(c), 23.1325(a)(b)(1)(2)(i), 23.1326(a), 23.1327(a), 23.1329(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i) (b)(1)(i)(3)(c)(4)(d), 23.1353(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1361(a), 23.1365, 23.1367(a)(b)(c)(d), 23.1381(a)(b)(c), 23.1383(a)(b)(c)(d), 23.1385(a)(b)(c)(d), 23.1387(a)(b)(c)(d)(e), 23.1389(a)(b)(c), 23.1391, 23.1393, 23.1395(a)(b), 23.1397(a)(b)(c), 23.1401(a)(b)(c)(d)(e)(f), 23.1431(a)(b), 23.1523, 23.1525, 23.1529, 23.1541(a)(b), 23.1543(b)(c), 23.1545(a)(b), 23.1549(a)(b)(c), 23.1553, 23.1555(a)(b)(e)(1), 23.1563(a)(b), 23.1567(a), 23.1581(a)(c), 23.1583(g)(h)(m), 23.1585(j), 23.1589 as amended by Amdt. 23-61. 14 CFR Part 23 Regulation 23.1303(a)(b)(c)(f) as amended by Amdt. 23-62 Eligible Serial Numbers: 4496395, 4496397 and up. For PA-44-180 aircraft equipped with Piper Lycoming IO-360-B1G6 and LIO-360-B1G6 Fuel Injected Engines as installed by Piper drawing number 107600-003 the additional certification basis for installation specific items only is: 14 CFR Part 23 Regulations 23.33(a)(d), 23.865, 23.901(a)(1)(2)(b)(1)(2), 23.903(a)(c)(1)(2)(d), ), 23.905(a)(b)(c), 23.907(a), 23.925(a)(c)(1)(2)(3), 23.951(a)(b)(1), 23.953(a), 23.954(a)(b)(c), 23.959, 23.961, 23.963, 23.965, 23.967, 23.969, 23.971, 23.973, 23.975(a), 23.977, 23.991(a)(1)(b), 23.993, 23.994, 23.995, 23.997, 23.999, 23.1011, 23.1017, 23.1019(b), 23.1021, 23.1023, 23.1027, 23.1091(a)(b)(1)(2)(3), 23.1103, 23.1121(a)(b)(c)(d)(e)(f), 23.1123, 23.1141(a)(b)(c)(d), 23.1143, 23.1145, 23.1147, 23.1149, 23.1153, 23.1182, 23.1183, 23.1189, 23.1191, 23.1193, 23.1521(a)(b)(1)(c)(1)(4)(d), as amended by Amdt. 23-16 14 CFR Part 23 Regulations 23.1101 as amended by Amdt. 23-43; 14 CFR Part 23 Regulations 23.955(a)(c)(1)(3)(e)(3), 23.1093(a)(5), 23.1107 as amended by Amdt. 23-51; 14 CFR Part 23 Regulations 23.21, 23.23, 23.25(a)(b), 23.29, 23.301, 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.473, 23.561(a)(b)(3)(e), 23.601, 23.603, 23.605(a), 23.607, 23.609, 23.611, 23.613, 23.625, 23.627, 23.777(a)(b), 23.779(b)(1), 23.1041, 23.1043, 23.1047, 23.1163, 23.1301(a)(b)(c)(d), 23.1305(a)(1)(2)(3)(4)(b)(2)(3)(i)(4)(i)(5), 23.1309(a)(1)(a)(3)(b)(f), 23.1337(a)(1)(2)(3)(b)(1)(4)(c)(d)(1), 23.1351(b)(1)(i), 23.1357(a)(b)(c), 23.1359(c), 23.1365(c), 23.1431(b), 23.1529, 23.1541(a)(b), 23.1549(a)(b)(c), 23.1553, 23.1555(a)(b)(c)(1)(3)(4)(d)(e)(1)(2), 23.1581(a), 23.1583(g)(h)(m), 23.1585(j), 23.1589 as amended by Amdt. 23-61; Eligible Serial Numbers: 4496404, 4496417 and up. A19SO Page 10 of 13 For PA-44-180 aircraft equipped with Piper factory installed Garmin G1000NXi Phase II as installed by Piper drawing number 107600-002 or 107600-003, the additional certification basis for installation specific items only is: 14 CFR Part 23 Regulation 23.903(d) as amended by Amdt. 23-16 14 CFR Part 23 Regulations 23.21, 23.23, 23.25(a)(b), 23.29, 23.251, 23.301(a)(b)(c), 23.303, 23.305(a)(b), 23.307(a), 23.337(a)(b), 23.341(a)(c), 23.473, 23.561(a)(b)(3)(e), 23.601, 23.603, 23.605(a), 23.607, 23.609, 23.611, 23.613, 23.625, 23.627, 23.729(e)(f), 23.771(a), 23.773(a)(1)(2), 23.777(a)(b), 23.867, 23.1301(a)(b)(c)(d), 23.1305(a)(1)(2)(3)(b)(2)(3)(i)(4)(i)(5), 23.1306, 23.1307, 23.1308(a)(b)(c), 23.1309(a)(1)(3)(b)(c)(d)(e), 23.1311(a)(1)(2)(3)(4)(6)(7)(b)(c), 23.1321(a)(b)(c)(d)(5)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(c), 23.1325(a)(b)(1)(2)(i), 23.1326(a)(b), 23.1327(a), 23.1329(d)(e)(g)(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i)(b)(1)(i)(ii)(iii)(3)(c)(4)(d), 23.1353(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1361(a), 23.1365, 23.1367(c)(d), 23.1381(a)(b)(c), 23.1431(a)(b)(e), 23.1501, 23.1523, 23.1525, 23.1529, 23.1541(a)(b), 23.1543(b)(c), 23.1545(a)(b), 23.1549(a)(b)(c), 23.1553, 23.1555(a)(b)(e)(1), 23.1581(a)(c), 23.1583(g)(h)(m), 23.1585(j), 23.1589(a) as amended by Amdt. 23-61 14 CFR Part 23 Regulation 23.1303(a)(b)(c)(f) as amended by Amdt. 23-62 Eligible Serial Numbers: 4496432, 4496447 and up. For PA-44-180 aircraft equipped with Piper factory installed Garmin G5 Standby Instrument as installed by Piper drawing number 107600-002 or 107600-003, the additional certification basis for installation specific items only is: 14 CFR Part 23.303, 23.307(a), 23.1381(a)(b) as amended by Amndt. 23-0 14 CFR Part 23.771(a) as amended by Amndt. 23-14 14 CFR Part 23.1541(a)(b) as amended by Amndt. 23-21 14 CFR Part 23.601, 23.603, 23.605(a) as amended by Amndt. 23-23 14 CFR Part 23.1529 as amended by Amndt. 23-26 14 CFR Part 23.1322(a)(e), 23.1357(a)(b)(c)(d) as amended by Amndt. 23-43 14 CFR Part 23.305, 23.613(a)(b), 23.773(a)(2) as amended by Amndt. 23-45 14 CFR Part 23.301(a), 23.337(a)(b), 23.607(b) as amended by Amndt. 23-48 14 CFR Part 23.1307, 23.1309(b)(1)(e), 23.1321(c)(e), 23.1351(a)(1)(2)(i), 23.1359, 23.1365(a)(b)(c)(d)(e) as amended by Amndt. 23-49 14 CFR Part 23.1325(a)(b), 23.1543(b), 23.1581(a)(b)(d)(f) as amended by Amndt. 23-50 14 CFR Part 23.25(a)(b), 23.29 as amended by Amndt. 23-61 14 CFR Part 23.251(a), 23.561(a)(b)(3)(c), 23.777(a)(b), 23.853(a), 23.1301(a)(b)(c), 23.1303(a)(b)(c)(f), 23.1309(a)(1)(2), 23.1311(a)(1)(2)(3)(6)(7)(b), 23.1323(a)(b)(c), 23.1331(a)(b)(1)(c), 23.1353(h), 23.1431(a)(b), 23.1545(a)(b)(c), 23.1555(a)(b), 23.1583(m), 23.1585(a) as amended by Amndt. 23-62