# TCDS A25SO: Piper Aircraft Inc. - Type: Type certificate data sheet - Status: Current - Holder: Piper Aircraft Inc. - Revision: 42 - Revised: February 16, 2026 - Product: Aircraft, Small Airplane - Certification basis: Part 23, Part 25 - Registered aircraft: 1,692, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/f0/aa/f0aa3d15bf1b28a7fd4b449a5af6f19045d4a93df4e78f391c300e26af1f7bfd - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155755324920260217142718.0001 - Page: https://openairdocs.org/tcds/A25SO ## Models (6) As the data sheet lists them. - PA-46-600TP - PA-46-310P (Malibu) - PA-46-500TP (Malibu Meridian) - PA-46-350P (Malibu Mirage) - PA-46R-350T - PA-46-701TP ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. No. 42 16 34 35 24 23 36 41 38 38 29 37 41 36 41 35 38 36 38 39 Page No. 21 22 23 24 25 Rev. No. 41 41 38 42 41 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A25SO Revision 42 Piper PA-46-310P PA-46-350P PA-46-500TP PA-46R-350T PA-46-600TP PA-46-701TP February 16, 2026 TYPE CERTIFICATE DATA SHEET NO. A25SO This data sheet, which is part of Type Certificate No. A25SO, 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 A25SO to Piper Aircraft, Inc on August 7, 2006. I. - Model PA-46-310P (Malibu), 6 PCLM (Normal Category), Approved September 27, 1983. Engine Teledyne Continental, TC No. E8CE, Model TSI0-520-BE Fuel 100/100LL minimum grade aviation gasoline Engine Limits For all operations: 2600 RPM and 38" Hg MAP (310 HP), sea level to 24,000 ft. 2600 RPM and 35" Hg MAP above 24,000 ft. 2400 RPM and 31" Hg MAP maximum when leaned to 50  F lean of peak, any altitude. Propeller and Propeller Limits Hartzell, TC No. P-920, Hub BHC-C2YF-1BF, Blade F8052 ( ) Pitch: High 38.0   1, Low 16.0  0.2 at 30" station. Diameter: Not over 80", not under 78". Spinner: Hartzell D-4810 or D-4810P. Governor: Hartzell Model E-5-2. Airspeed Limits VNE (Never Exceed) 203 KIAS V NO (Maximum Structural Cruise) 173 KIAS V A (Maneuvering 4100 lb.) 135 KIAS V A (Maneuvering 2450 lb.) 103 KIAS V FE (Maximum Flaps Extended) 120 KIAS V LO (Maximum Landing Gear Operation) Extension 170 KIAS Retraction 130 KIAS V LE (Maximum Landing Gear Extended) 200 KIAS A25SO Page 2 of 25 C.G. Range (Gear Extended) WT. FWD. LIMIT AFT LIMIT (LB.) IN. AFT OF DATUM IN. AFT OF DATUM 4100 143.3 in. 147.1 in. 3680 136.1 in. 147.1 in. 2450 or less 130.7 in. 147.1 in. Empty Weight C.G. Range None Maximum Weight Ramp : 4118 lb. Takeoff : 4100 lb. Landing : 3900 lb. No. of Seats 6 (2 at +135.5, 2 at +177.0, 2 at +218.75) Maximum Baggage 100 lb. at (+88.6) (Fwd.) 100 lb. at (+248.23) (Aft) Fuel Capacity 122 gals. at (+150.31) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 8 qts. at (+53.5) See NOTE 1 for data on system oil. Maximum Operating Altitude 25,000 ft. Maximum Cabin Operating Pressure Differential 5.5 PSID Control Surface Movements Ailerons (1) Up 18 Down 18 Elevator (.5) Up 23.5 Down 14.5  Rudder (+1, -0) Left 26 Right 30 Elevator (+0, -1) Down 24.5 Up 19 Trim Tab (Elevator Neutral) Wing Flaps S/N 46-8408001 to 46-8508109 Up 0 (1) Down 35 (+0, -1) Wing Flaps S/N 46-8608001 and up Up 0 (1) Down 35 (1) Manufacturer's Serial Numbers 46-8408001 through 46-8408087, 46-8508001 through 46-8508109, 46-8608001 through 46-8608067, 4608001 through 4608140. II. - Model PA-46-350P (Malibu Mirage), 6 PCLM (Normal Category), Approved August 30, 1988. Engine Textron Lycoming, TC No. E14EA, Model TIO-540-AE2A Fuel 100/100LL mínimum grade aviation gasoline Engine Limits For all operations: 2500 RPM and 42.0" Hg MAP (350 HP), sea level to 20,600 ft. 42 - 1.6" Hg MAP decrease per each 1000 ft. altitude increase, 20,600 ft. to 25,000 ft. Propeller and Propeller Limits Hartzell, TC No. P42GL, Hub HC-I2YR-1BF, Blade F8074 (standard 2 blade-Serial Numbers 4622001 through 4622200 and 4636001 through 4636195) Pitch: High 40.5   0.5 Low 17.6  0.2 at 30" station. Diameter: Not over 80", not under 79". Spinner: Hartzell A-2298-3P. Governor: Hartzell Model V-5-2 or V-11-1 The following limitation is applicable to the two-bladed aluminum propeller installation: A25SO Page 3 of 25 Do not exceed 36” MAP below 2400 RPM Do not exceed 32” MAP below 2300 RPM Hartzell, TC No. P33EA, Hub HC-I3YR-1E, Blade 7890K, 3-blade, Serial Numbers 4636132 and up Pitch: High 38.7°  0.5 Low 13.65  0.15 at 30" station. Diameter: 80" Spinner: Hartzell D-6750P. Governor: Hartzell Model V-5-2 or V-11-1 Hartzell, TC No. P33EA, Hub HC-I3Y1R-1N, Blade N7605C+2, or N7605CK+2, 3- blade, Serial Numbers 4636460, 4636463 and up Pitch: High 38.0°  1.0 Low 14.0  0.2 at 30" station. Diameter: 80" Spinner: Hartzell D-6750-1P. Governor: Hartzell Model V-5-2, V-11-1 or S-1-30 Airspeed Limits VNE (Never Exceed) 198 KIAS V NO (Maximum Structural Cruise) 168 KIAS V A (Maneuvering 4340 lb.) (S/N 4636196 & up) 133 KIAS V A (Maneuvering 4300 lb.) 133 KIAS V A (Maneuvering 2450 lb.) 100 KIAS V FE (Maximum Flaps Extended) 116 KIAS V LO (Maximum Landing Gear Operation) Extension 165 KIAS Retraction 126 KIAS V LE (Maximum Landing Gear Extended) 195 KIAS C.G. Range (Gear Extended) WT. FWD. LIMIT AFT LIMIT (LB.) IN. AFT OF DATUM IN. AFT OF DATUM 4300 (4340) 143.3 in. (144.1 in) 147.1 in. 4100 (4123) 139.1 in. (139.6 in) 147.1 in. 4000 137.0 in. 146.5 in. 2450 130.7 in. 137.6 in 2400 130.7 in. 137.3 in. Note: Numbers in parentheses apply to serial numbers 4636196 and up. Empty Weight C.G. Range None Maximum Weight Ramp : 4318 lb. (4358 lb.) Takeoff : 4300 lb. (4340 lb.) Landing : 4100 lb. (4123 lb.) Note: Numbers in parentheses apply to serial numbers 4636196 and up. No. of Seats 6 (2 at +135.5, 2 at +177.0, 2 at +218.75) Maximum Baggage 100 lb. at (+88.6) (Fwd.) 100 lb. at (+248.23) (Aft) Fuel Capacity 122 gals. at (+150.31) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 12 qts. at (+53.5) See NOTE 1 for data on system oil. Maximum Operating Altitude 25,000 ft. A25SO Page 4 of 25 Maximum Cabin Operating Pressure Differential 5.5 PSID (+0.1, -0.15) Control Surface Movements Ailerons (1) Up 18 Down 18 Elevator (0.5) Up 23.5 Down 14.5 Rudder (+1, -0) Left 26 Right 30 Elevator Trim Tab (+0, -1) (Elevator Neutral) Down 24.5 Up 19 Wing Flaps Up 0 (1) Down 10 (2) 20 (+2, -0) 36 (+0, -1) Manufacturer's Serial Numbers 4622001 through 4622200, and 4636001 and up. III. – Model PA-46-500TP (Malibu Meridian), 6PCLM (Normal Category), Approved September 27, 2000. Engine Pratt & Whitney Canada, PT6A-42A (per PWC Build Specifications BS1011, BS1192 or BS1430) Fuel Jet A and A-1 fuels conforming to Pratt & Whitney Specification 522 or Service Bulletin 3044, CPW204. (Fuels shall conform to the specification as listed or to subsequent revisions thereto.) MIL-DTL-85470 Fuel System Icing Inhibitor or equivalent must be used in the fuel in the amount up to 0.15% by volume. Oil (Engine & Gearbox) PWC PT6 Engine Service Bulletin No. 3001 lists approved brand oils. Engine Limits Takeoff and max continuous power 500 SHP Compressor Turbine Speed (Ng) 39000 RPM (104%)* Propeller Speed (Np) 2205 RPM* * See Note 5 Propeller and Propeller Limits Hartzell, T.C. No. P10NE, Hub HC-E4N-3Q, Blade E8501B-3.5 Pitch: Low 19.0  + 0.1at 30” station. Diameter: Not over 82.5”, not under 81.5”. Spinner: Hartzell D-630-5P Governor: Woodward Model 210 638 or Woodward Model 210 695 Airspeed Limits V MO (Maximum Operating Speed) 188 KIAS VO (Operating Maneuvering Speed) 127 KIAS VFE (Flaps Extended Speed for 10 Flaps) 168 KIAS VFE (Flaps Extended Speed for 20 Flaps) 135 KIAS VFE (Flaps Extended Speed for 36 Flaps) 118 KIAS VLO (Maximum Landing Gear Operation) Extension 168 KIAS Retraction 129 KIAS VLE (Maximum Landing Gear Extended) 168 KIAS C.G. Range For airplanes S/N 4697001, 4697003 through 4697156: WT. (LB.) FWD LIMIT IN. AFT OF DATUM AFT LIMIT IN. AFT OF DATUM 4892 140.22 in. 147.10 in. 4850 140.06 in. 147.10 in. 4100 137.23 in. 147.10 in. 3508 135.00 in. 143.67 in 3000 135.00 in. 140.75 in A25SO Page 5 of 25 For airplanes S/N 4697157 and up and earlier airplanes having Kit 767-360 installed: WT. (LB.) FWD LIMIT IN. AFT OF DATUM AFT LIMIT IN. AFT OF DATUM 5134 141.13 in. 147.10 in. 5092 140.97 in. 147.10 in. 4892 140.22 in. 147.10 in. 4850 140.06 in. 147.10 in. 4100 137.23 in. 147.10 in. 3508 135.00 in. 143.67 in. 3000 135.00 in. 140.75 in. Empty Weight C.G. Range None Maximum Weight RAMP (LB.) TAKEOFF (LB.) LANDING (LB.) MZFW (LB.) For airplanes S/N 4697001, 4697003 through 4697156: 4892 4850 4850 For airplanes S/N 4697157 and up and earlier airplanes having Kit 767-360 installed: 5134 5092 4850 4850 No. of Seats 6 (2 at +135.5, 2 at 177.0, 2 at 218.75) Maximum Baggage 100 lbs. at (+248.23) Fuel Capacity 173 gallons at (+148.75) (2 wing tanks) 170 gallons (1140 lbs.) useable See Note 1 for data on system fuel. Oil Capacity 12 quarts at (+77.76) See Note 1 for data on system oil. Maximum Operating Altitude 30,000 ft. OAT Operating Limitation For airplanes S/N 4697001, 4697003 through 4697173: +46 C (+115ºF) maximum -34C (-30ºF) minimum with Jet-A -41C (-42ºF) minimum with Jet A-1 For airplanes S/N 4697174 and up and S/N 4697001, 4697003 through 4697158 having Piper Kit 767-380 installed and S/N 4697159 through 4697173 having Piper Kit 767-381 installed: +46C (+115ºF) maximum -54C (-65ºF) minimum Minimum Fuel Temperature For airplanes S/N 4697159 and up and S/N 4697001, 4697003 through 4697158 having Piper Kit 767-380 installed: -34C (-30ºF) minimum for starting with Jet-A/A-1 -34C (-30ºF) minimum in-flight with Jet-A -41C (-42ºF) minimum inflight with Jet A-1 NOTE: When a mixture of Jet A and Jet A-1 is present in the fuel tanks, the Jet A minimum fuel temperature limits must be observed. Maximum Cabin Operating Pressure Differential 5.5 PSID (+0.1, -0.15) Control Surface Movements Aileron (+ 1 ) Up 18 Down 18  Elevator (+.5 ) Up 23.5  Down 14.5  Elevator Trim Tab (+0 ,-1) Up 19  Down 24.5  (Elevator Neutral) A25SO Page 6 of 25 Rudder (+1 -0) Left 26  Right 30  Rudder Trim Tab (+1 ) Left 13.5  Right 13  (Rudder Neutral) Wing Flaps Up 0  (+1) Down 10  (+2) 20  (+2,-0) 36  (+0,-1) Manufacturer’s Serial Numbers 4697001, 4697003 and up IV. - Model PA-46R-350T (Malibu Matrix), 6 PCLM (Normal Category), Approved October 26, 2007. Engine Textron Lycoming, TC No. E14EA, Model TIO-540-AE2A Fuel 100/100LL mínimum grade aviation gasoline Engine Limits For all operations: 2500 RPM and 42.0" Hg MAP (350 HP), sea level to 20,600 ft. 42 - 1.6" Hg MAP decrease per each 1000 ft. altitude increase, 20,600 ft. to 25,000 ft. Propeller and Propeller Limits Hartzell, TC No. P33EA, Hub HC-I3YR-1E, Blade 7890K or 7890B, 3-blade Pitch: High 38.7°  0.5 Low 13.65  0.15 at 30" station. Diameter: 80" Spinner: Hartzell D-6750P. Governor: Hartzell Model V-11-1 Hartzell, TC No. P33EA, Hub HC-I3Y1R-1N, Blade N7605+2 or N7605K+2, or N7605C+2, or N7605CK+2 3-blade, Serial Numbers 4692123 and up Pitch: High 38.0°  1.0 Low 14.0  0.2 at 30" station. Diameter: 80" Spinner: Hartzell D-6750-1P. Governor: Hartzell Model V-11-1 or S-1-30 Airspeed Limits VNE (Never Exceed) 198 KIAS V NO (Maximum Structural Cruise) 168 KIAS V A (Maneuvering 4340 lb.) 133 KIAS V A (Maneuvering 2900 lb.) 108 KIAS V FE (Maximum Flaps Extended for 10°) 165 KIAS V FE (Maximum Flaps Extended for 20°) 130 KIAS V FE (Maximum Flaps Extended for 36°) 116 KIAS V LO (Maximum Landing Gear Operation) Extension 165 KIAS Retraction 126 KIAS V LE (Maximum Landing Gear Extended) 195 KIAS C.G. Range (Gear Extended) WT. FWD. LIMIT AFT LIMIT (LB.) IN. AFT OF DATUM IN. AFT OF DATUM 4340 144.1 in 147.1 in. 4123 139.6 in 147.1 in. 4000 137.0 in. 146.5 in. 2900 132.5 in. 140.2 in Empty Weight C.G. Range None Maximum Weight Ramp : 4358 lb. Takeoff : 4340 lb. Landing : 4123 lb. A25SO Page 7 of 25 No. of Seats 6 (2 at +135.5, 2 at +177.0, 2 at +218.75) Maximum Baggage 100 lb. at (+88.6) (Fwd.) 100 lb. at (+248.23) (Aft) Fuel Capacity 122 gals. at (+150.31) (2 wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 12 qts. at (+53.5) See NOTE 1 for data on system oil. Maximum Operating Altitude 25,000 ft. Control Surface Movements Ailerons (1) Up 18 Down 18 Elevator (0.5) Up 23.5 Down 14.5  Rudder (+1, -0) Left 26 Right 30 Elevator Trim Tab (+0, -1) (Elevator Neutral) Down 24.5 Up 19 Wing Flaps Up 0 (1) Down 10 (2) 20 (+2, -0) 36 (+0, -1) Manufacturer's Serial Numbers 4692001 through 4692214 V. – Model PA-46-600TP (M600), 6PCLM (Normal Category), Approved June 16, 2016. Engine Pratt & Whitney Canada, PT6A-42A (per PWC Build Specification BS1322 or BS1415) Fuel Jet A and A-1 fuels conforming to Pratt & Whitney Specification 522 or Service Bulletin 3044, CPW204. (Fuels shall conform to the specification as listed or to subsequent revisions thereto.) MIL-DTL-85470 Fuel System Icing Inhibitor or equivalent must be used in the fuel in the amount up to 0.15% by volume. Oil (Engine & Gearbox) PWC PT6 Engine Service Bulletin No. 3001 lists approved brand oils. Engine Limits Takeoff and max continuous power 600 SHP Compressor Turbine Speed (Ng) 39000 RPM (104%)* Propeller Speed (Np) 2205 RPM* * See Note 5 Propeller and Propeller Limits Hartzell, T.C. No. P10NE, Hub HC-E4N-3Q, Blade E8501K-3.5*1 Pitch: Low 19.0  + 0.1at 30” station. Diameter: Not over 82.5”, not under 81.5”. Spinner: Hartzell D-630-5P Governor: Woodward Model 210695 Hartzell, T.C. No. P00015CH, Hub 5D3-N338A1, Blade 78D01B Pitch: Low 17.7  + 0.1at 30” station Feather 83.2  + 0.5at 30” station Reverse -11.0 + 0.5at 30” station Diameter: 82.5 inches (No additional reduction permitted) Spinner: Hartzell Standard: 106917(P) or Light Weight: 105951(P) Governor: Woodward Model 210695 Airspeed Limits V MO (Maximum Operating Airspeed) 250 KCAS M MO (Maximum Operating Mach) 0.55 M VO (Maximum Operating Maneuvering Speed) 6000 lbs 151 KCAS 3750 lbs 119 KCAS VFE (Flaps Extended Speed for T/O Flaps) Flaps Extended Speed for T/O Flaps 145 KCAS Flaps Extended Speed for LND Flaps 108 KCAS VLE (Maximum Landing Gear Extended) 168 KCAS A25SO Page 8 of 25 VLO (Maximum Landing Gear Operation) V LOE Extension 168 KCAS V LOR Retraction 128 KCAS C.G. Range For airplanes S/N 4698001 and up: WT. (LB.) FWD LIMIT IN. AFT OF DATUM AFT LIMIT IN. AFT OF DATUM 6050 144.00 in. 146.00 in. 6000 144.00 in. 146.00 in. 5850 141.26 in 146.00 in. 5800 141.15 in. 146.00 in. 4850 139.05 in. 146.00 in. 3925 137.00 in 142.40 in 3500 137.00 in 140.00 in Empty Weight C.G. Range None Maximum Weight RAMP (LB.) TAKEOFF (LB.) LANDING (LB.) MZFW (LB.) For airplanes S/N 4698001 and up: 6050 6000 5800 4850 No. of Seats 6 (1 at +140.6, 1 at 141.8, 2 at 171.9, 2 at 223.8) Maximum Baggage 100 lbs. at (+248.23) Fuel Capacity 263.2 gallons at (+148.90) (2 wing tanks) 260 gallons (1742 lbs.) useable See Note 1 for data on system fuel. Oil Capacity 12 quarts at (+77.76) See Note 1 for data on system oil. Maximum Operating Altitude 30,000 ft. OAT Operating Limitation +46 C (+115ºF) maximum -54C (-65ºF) minimum Minimum Fuel Temperature -34 C (-30ºF) minimum for starting with Jet-A/A-1 -34C (-30ºF) minimum in-flight with Jet-A -41C (-42ºF) minimum inflight with Jet A-1 NOTE: When a mixture of Jet A and Jet A-1 is present in the fuel tanks, the Jet A minimum fuel temperature limits must be observed. Maximum Cabin Operating Pressure Differential 5.5 PSID (+0.1, -0.15) Control Surface Movements Aileron (+ 1) Up 24.7 Down 20 Elevator (+.5) Up 13  Down   Elevator Trim Tab (+0,-1) Up 19 Down  (Elevator Neutral) Rudder (+1-0) Left 20 Right 30 Rudder Trim Tab (+1) Left 13.5 Right 13 (Rudder Neutral) Wing Flaps Up 0 (+1) Down 15 (+1) 35 (+1) Manufacturer’s Serial Numbers 4698001, 4698004 and up A25SO Page 9 of 25 VI. – Model PA-46-701TP (M700), 6PCLM (Normal Category), Approved February 29, 2024. Engine Pratt & Whitney Canada, PT6A-52 (per PWC Build Specification BS1435) Fuel Jet A and A-1 fuels conforming to Pratt & Whitney Specification 522 or Service Bulletin 3044, CPW204. (Fuels shall conform to the specification as listed or to subsequent revisions thereto.) MIL-DTL-85470 Fuel System Icing Inhibitor or equivalent must be used in the fuel in the amount up to 0.15% by volume. Oil (Engine & Gearbox) PWC PT6 Engine Service Bulletin No. 13001 lists approved brand oils. Engine Limits Takeoff and max continuous power 700 SHP Compressor Turbine Speed (Ng) 39000 RPM (104.1%) Propeller Speed (Np) 2205 RPM* * See Note 8 Propeller and Propeller Limits Hartzell, T.C. No. P00015CH, Hub 5D3-N338A1, Blade 78D01B Pitch: Low 17.7  + 0.1at 30” station Feather 83.2  + 0.5at 30” station Reverse -11.0 + 0.5at 30” station Diameter: 82.5 inches (No additional reduction permitted) Spinner: Hartzell 105951(P) Governor: Woodward Model 210695 Airspeed Limits V MO (Maximum Operating Airspeed) 250 KCAS M MO (Maximum Operating Mach) 0.55 M VO (Maximum Operating Maneuvering Speed) 6000 lbs 151 KCAS 3750 lbs 119 KCAS VFE (Flaps Extended Speed for T/O Flaps) Flaps Extended Speed for T/O Flaps 145 KCAS Flaps Extended Speed for LND Flaps 108 KCAS VLE (Maximum Landing Gear Extended) 168 KCAS VLO (Maximum Landing Gear Operation) V LOE Extension 168 KCAS V LOR Retraction 128 KCAS C.G. Range For airplanes S/N 46020001 and up: WT. (LB.) FWD LIMIT IN. AFT OF DATUM AFT LIMIT IN. AFT OF DATUM 6050 144.00 in. 146.00 in. 6000 144.00 in. 146.00 in. 5850 141.26 in 146.00 in. 5800 141.15 in. 146.00 in. 5050 139.49 in. 146.00 in. 3925 137.00 in 142.40 in 3500 137.00 in 140.00 in Empty Weight C.G. Range None Maximum Weight RAMP (LB.) TAKEOFF (LB.) LANDING (LB.) MZFW (LB.) For airplanes S/N 46020001 and up: 6050 6000 5800 5050 No. of Seats 6 (1 at +140.6, 1 at 141.8, 2 at 171.9, 2 at 223.8) A25SO Page 10 of 25 Maximum Baggage 100 lbs. at (+248.23) Fuel Capacity 263.2 gallons at (+148.90) (2 wing tanks) 260 gallons (1742 lbs.) useable See Note 1 for data on system fuel. Oil Capacity 12 quarts at (+77.76) See Note 1 for data on system oil. Maximum Operating Altitude 30,000 ft. OAT Operating Limitation +46 C (+115ºF) maximum -54C (-65ºF) minimum Minimum Fuel Temperature -34 C (-30ºF) minimum for starting with Jet-A/A-1 -34C (-30ºF) minimum in-flight with Jet-A -41C (-42ºF) minimum in-flight with Jet A-1 NOTE: When a mixture of Jet A and Jet A-1 is present in the fuel tanks, the Jet A minimum fuel temperature limits must be observed. Maximum Cabin Operating Pressure Differential 5.5 PSID (+0.1, -0.15) Control Surface Movements Aileron (+ 1) Up 24.7 Down 20 Elevator (+.5) Up 13  Down   Elevator Trim Tab (+0,-1) Up 19 Down  (Elevator Neutral) Rudder (+1-0) Left 20 Right 30 Rudder Trim Tab (+1) Left 25 Right 13 (Rudder Neutral) Wing Flaps Up 0 (+1) Down 15 (+1) 35 (+1) Manufacturer’s Serial Numbers 46020001 and up DATA PERTINENT TO ALL MODELS Datum 100 in. forward pressure bulkhead. Leveling Means Top or bottom fuselage at B.L. 0 (constant section). Certification Basis Type Certificate No. A25SO issued September 27, 1983. Date of application for Type Certificate, August 22, 1979. PA-46-310P and PA-46-350P: FAR Part 23, effective February 1, 1965, as amended by Amendment 23-25, effective March 6, 1980; FAR 25.783(e) as amended by Amendment 25-54, effective October 14, 1980; FAR 25.831(c) and (d) as amended by Amendment 25-41, effective September 1, 1977; and FAR 36, Appendix F through Amendment 36-15, effective May 6, 1988 when equipped with 2 blade propeller or FAR 36, Appendix G through Amendment 36-16, effective December 18, 1988 when equipped with optional 3 blade propeller. No equivalent safety findings. Special Conditions No. 23-ACE-53, Docket No. 082CE. For PA-46-350P aircraft equipped with Piper factory installed Avidyne Entegra system (See Piper Report VB-1954), the additional certification basis for installation specific items only is: FAR 23.1529 as amended by Amendment 23-26, effective 14 October 1980; FAR 23.1523 as amended by Amendment 23-34, effective 17 February 1987; FAR 23.1322, 23.1331, 23.1357 (a)(2), (b), (c), (d) as amended by Amendment 23-43, effective 10 May 1993; FAR 23.305, 23.613, 23.773 (a)(2), 23.1525, 23.1549 (a) as amended by Amendment 23-45, effective 7 September 1993; FAR 23.301, 23.337 (a)(1), (b)(1), 23.341 (a), 23.473, A25SO Page 11 of 25 23.561 (b)(3), (e), 23.571 (a), 23.607, 23.611, as amended by Amendment 23-48, effective 11 March 1996; FAR 23.1303 (a), (b), (f), 23.1307, 23.1309 (a), (a)(1), (a)(2), (b),(e), 23.1311 (a)(2), (a)(3), (a)(4), (a)(5), (a)(6), (a)(7), (b), (c), 23.1321 (a), (c), (d), (e), 23.1323 (a), (c), 23.1329, 23.1351 (a)(1), (a)(2)(i), (b)(2), (b)(3), 23.1353 (d), (h), 23.1359 (c), 23.1365 (a), (b), (d), (e), (f), 23.1431 (a), (b) as amended by Amendment 23-49, effective 11 March 1996; FAR 23.1325 (a), (b)(1), (b)(2)(ii), (b)(3), (c), (e), 23.1543 (b), (c), 23.1545 (a), (b)(3), (b)(4), (c), 23.1555 (a), (b), 23.1563, 23.1581 (a), (b)(2), (b)(3), (f), 23.1583 (m), 23.1585 (j) as amended by Amendment 23-50, effective 11 March1996; FAR 23.777 (a), (b), 23.1337 as amended by Amendment 23-51, effective 11 March 1996; FAR 23.1305 (a)(1), (a)(2), (a)(3), (b)(2), (b)(3), (b)(4), (b)(5), (b)(6)(i) as amended by Amendment 23-52, effective 25 July 1996; Special Condition for HIRF (Docket # CE215, Special Condition 23- 154-SC), January 7, 2005. Eligible Serial Numbers: 4636375 and up. For the PA-46-350P Mirage aircraft equipped with Hartzell propeller HC-I3Y1R- 1N/N7605C+2, or N7605CK+2 (See Piper Report VB-2132) the additional certification basis for installation specific items only is: FAR 23.905 (a), (b), (d) as amended by Amendment 23-43, effective 10 May 1993; 23.907 as amended by Amendment 23-59, effective 24 October 2008; and FAR 36, Appendix G through Amendment 36-28, dated 3 February 2006. Eligible Serial Numbers: 4636460, 4636463 & up. For PA-46-350P aircraft equipped with Piper factory installed Garmin G1000 system and GFC 700 AFCS (See Piper Drawing 106800), the additional certification basis for installation specific items only as amended by Amendment 23-59 dated December 23, 2008, is: 14 CFR 23.23 14 CFR 23.25 14 CFR 23.251 14 CFR 23.301 (a), (b), (c) 14 CFR 23.305 14 CFR 23.337 14 CFR 23.341 (a), (c) 14 CFR 23.397 (a) 14 CFR 23.473 14 CFR 23.561 (a), (b)(3), (e) 14 CFR 23.607 14 CFR 23.611 14 CFR 23.613 14 CFR 23.677 (b), (d) 14 CFR 23.773 (a) (1), (a)(2) 14 CFR 23.777 (a), (b), (d) 14 CFR 23.841 (b)(5), (6) 14 CFR 23.867 14 CFR 23.1141 (a), (b), (c), (d) 14 CFR 23.1303 (a), (b), (c), (f) 14 CFR 23.1305 (a) (1), (a)(2), (a)(3), (b)(2), (b)(4)(i), (b)(5), (b)(6)(i) 14 CFR 23.1307 14 CFR 23.1308 (a)(l), (a)(2), (a)(3), (b), (c) 14 CFR 23.1309 (a)(I), (a)(2), (b), (c), (e) 14 CFR 23.1311 (a) (1), (a)(2), (a)(3), (a)(4), (a)(5), (a)(6), (a)(7), (b), (c) 14 CFR 23.1321 (a), (c), (d)(5), (e) 14 CFR 23.1322 (a), (b), (c), (d), (e) 14 CFR 23.1323 (a), (c) 14 CFR 23.1325 (a), (b)(I), (b)(2)(ii) 14 CFR 23.1326 14 CFR 23.1329 (a)(1), (b), (d), (e), (f), (g), (h) 14 CFR 23.1331 (a), (b), (c) 14 CFR 23.1337 (b)(I), (b)(4) 14 CFR 23.1351 (a)(I), (a)(2)(i), (b)(I)(i) 14 CFR 23.1353 (h) 14 CFR 23.1357 (a)(2), (b), (c), (d) A25SO Page 12 of 25 14 CFR 23.1359 (c) 14 CFR 23.1365 (a), (b), (d), (e), (f) 14 CFR 23.1431 (a), (b), (e) 14 CFR 23.1507 14 CFR 23.1523 14 CFR 23.1525 14 CFR 23.1529 14 CFR 23.1543 (b)(c) 14 CFR 23.1545 (a), (b) (1), (b)(2), (b)(3), (b) (4) 14 CFR 23.1549 (a), (b), (c) 14 CFR 23.1553 14 CFR 23.1555 (a), (b), (d)(2) 14 CFR 23.1559 (c) 14 CFR 23.1563 (a)(b) 14 CFR 23.1567 (a) 14 CFR 23.1581 14 CFR 23.1583 14 CFR 23.1585 Eligible Serial Numbers: 4636460, 4636463 and up PA-46-350P serial numbers 4636375 through 4636459, 4636461 and 4636462 affected by Piper Service Bulletin SB1195B, only in the area of the communications antenna installations, the following additional certification basis is applicable: 14 CFR 23.571(c) as amended by Amendment 23-48, effective March 11, 1996; 14 CFR 23.573(b) as amended by Amendment 23-45, effective September 7, 1993. PA-46-350P aircraft equipped with Piper factory installed Enviro Cabin Pressure Control System, the additional certification basis for installation specific items only is: 23.303, 23.307, 23.601, 23.609, 23.627, 23.843(b) as amended by Amendment 23-0 effective February 1, 1965; 23.625 as amended by Amendment 23-7 effective September 14, 1969; 23.29, as amended by Amendment 23-21 effective March 1, 1978; 23.603, 23.605(a) as amended by Amendment 23-23 effective December 1, 1978; 23.607, 23.613 as amended by Amendment 23-25 effective March 3, 1980; 23.1529 as amended by Amendment 23-26 effective October 14, 1980; 23.831(b) as amended by Amendment 23- 42 effective February 4, 1991; 23.1322 (a)(b)(c)(d) as amended by Amendment 23- 43effective May 10, 1993; 23.305 as amended by Amendment 23-45 effective September 7, 1993; 23.301(a)(b)(c), 23.337, 23.341(a)(c), 23.473, 23.561(a)(b))(3)(e)23.611 as amended by Amendment 23-48 effective March 11, 1996; 23.841(a)(b)(1)(2)(3)(4)(b)(5)(6)(7)(8)(9), 23.867, 23.1307, 23.1351(a)(1)(i) as amended by Amendment 23-49 effective March 11, 1996; 23.25, 23.1325(b)(1)(2)(ii)(3)23.1581(a)23.1583(h)(m)23.1585(j) as amended by Amendment 23-50 effective March 11, 1996; 23.1308(a)(b)(c) as amended by Amendment 23-57 effective September 5, 2007; 23.1306, as amended by Amendment 23-61 effective August 8, 2011; 23.1301(a)(b)(c), 23.1309(a)(1)(2)b)(c)(d) as amended by Amendment 23-62 effective January 31, 2012. Eligible Serial Numbers: 4636633, 4636652 and up. PA-46-350P aircraft equipped with Piper factory installed G1000 Phase III Integrated Avionics the additional certification basis for installation specific items only is: 23.21, 23.23(a), 23.25(a)(b), 23.29, 23.143(a)(b), 23.207(b), 23.251, 23.301(a)(b)(c), 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.365(a)(b)(d), 23.473, 23.561(a)(b)(3)(e), 23.571(a), 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)(4)(i)(5)(6)(i), 23.1306, 23.1307, 23.1308(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(d)(e), 23.1311(a)(1)(2)(3)(4)(5)(6)(7)(b)(c), 23.1321(a)(c)(d)(5)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(c), 23.1325(a)(b)(1)(2)(ii), 23.1326(a)(b), 23.1327(a), 23.1329(d)(e)(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i)(b)(1)(i)(3)(c)(4)(d), 23.1353(a)(b)(c)(d)(e)(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1361(a)(c), 23.1365, 23.1367(a)(b)(c)(d), 23.1381(a)(b)(c), 23.1416(c), 23.1419(c), 23.1431(a)(b)(e), 23.1501(a)(b), 23.1523, 23.1525, 23.1529, 23.1541(a)(b), 23.1543(b)(c), 23.1545(a)(b)(1)(2)(3)(4), 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 as amended by Amendment 23-61 A25SO Page 13 of 25 effective June 8, 2011; 23.1303(a)(b)(c)(f) as amended by Amendment 23-62 effective January 31, 2012. Eligible Serial Numbers: 4636633, 4636652 and up. PA-46-350P aircraft equipped with Piper factory installed G1000NXi Integrated Avionics the additional certification basis for installation specific items only is: 14CFR 23.23(a)(b)(3), 23.25(a)(b), 23.29, 23.301(a)(b)(c), 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, 23.699, 23.771(a), 23.777(a)(b), 23.867, 23.1301(a)(b)(c)(d), 23.1305(a)(1)(2)(3)(b)(2)(4)(i)(5)(6)(i), 23.1306, 23.1308(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(d)(e), 23.1311(a)(1)(2)(3)(4)(5)(6)(7)(b)(c), 23.1321(a)(c)(d)(5)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(c), 23.1325(a)(b)(1)(2)(ii), 23.1326, 23.1327(a), 23.1329(a)(1)(b)(c)(d)(e)(f)(g)(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i)(c)(4)(d), 23.1353(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365, 23.1367(a)(b)(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 Amendment 23-61 effective June 8, 2011; 14 CFR 23.1303(a)(b)(c)(f) as amended by Amendment 23-62 effective January 31, 2012. Eligible Serial Numbers: 4636716, 4636720 and up. PA-46-350P aircraft with G1000NXi Integrated Avionics upgraded with software that incorporates a landing gear warning inhibit function and wireless local area network capabilities per Piper Drawing 107990-11, the additional certification basis is: 14 CFR 23.2010, 23.2500(b), 23.2505, 23.2510, 23.2600(b), and 23.2605(b)(c) as amended by Amendment 23-64 effective August 30, 2017. Eligible Serial Numbers: 4636716, 4636720 and up. PA-46-350P aircraft equipped with optional non-Halon fire extinguisher additional certification basis for installation specific items only is: 14 CFR 23.851, 23.1301, 23.1529 as amended by Amendment. 23-62 Effective January 31, 2012. Eligible Serial Numbers: 4636795 and up. PA-46-500TP: FAR 23, effective February 1, 1965, as amended by Amendment 23-25, effective March 6, 1980 unless otherwise indicated herein; FAR 23.1529 as amended by Amendment 23-26, effective October 14, 1980; FAR 23.441 as amended by Amendment 23-28, effective April 28, 1982; FAR 23.994 and 23.995 as amended by Amendment 23-29, effective March 26, 1984; FAR 23.781 as amended by Amendment 23-33, effective August 11, 1986; FAR 23.173, 23.333, 23.443, and 23.1165 as amended by Amendment 23-34, effective February 17, 1987; FAR 23.2, 23.783(a), (b), (e)(2) and (e)(3), and 23.1413 as amended by Amendment 23-36, effective September 14, 1988; FAR 23.331, 23.351, 23.421, 23.423, 23.425, 23.427, 23.831, 23.939, and 23.1163 as amended by Amendment 23-42, effective February 4, 1991; FAR 23.905, 23.937, 23.943, 23.951, 23.957, 23.961, 23.967, 23.971, 23.977, 23.991, 23.993, 23.997, 23.999, 23.1011, 23.1019, 23.1021, 23.1027, 23.1103, 23.1123, 23.1145, 23.1189, 23.1193, 23.1322, 23.1331, 23.1357, 23.1385, 23.1387, 23.1441, 23.1443, and 23.1445 as amended by Amendment 23-43, effective May 10, 1993; FAR 23.23, 23.141, 23.181, 23.251, 23.305, 23.321, 23.361, 23.397, 23.479, 23.485, 23.571, 23.572, 23.621, 23.655, 23.731, 23.733, 23.773, 23.1507, 23.1525, 23.1527, 23.1549, 23.1557, and 23.1563 as amended by Amendment 23-45, effective September 7,1993; FAR 23.301, 23.335, 23.337, 23.341, 23.343, 23.345, 23.347, 23.349, 23.371, 23.391, 23.393, 23.399, 23.415, 23.457, 23.473, 23.499, 23.561, 23.575, 23.611, 23.629, 23.657, 23.673, 23.725, and 23.865 as amended by FAR 23-48, effective March 11,1996; FAR 23.677, 23.723, 23.735, 23.745, 23.775, 23.841, 23.853, 23.867, 23.1303, 23.1307, 23.1309, 23.1311, 23.1321, 23.1323, 23.1326, 23.1329, 23.1353, 23.1359, 23.1361, 23.1383, 23.1401, 23.1447, 23.1451, and 23.1453 as amended by Amendment 23-49, effective March 11, 1996; FAR 23.3, 23.25, 23.33, 23.45, 23.49, 23.51, 23.53, 23.63, 23.65, 23.69, 23.71, 23.73, 23.75, 23.77, 23.143, 23.145, 23.153, 23.155, 23.157, 23.161, 23.175, 23.177, 23.201, 23.203, 23.207, 23.221, 23.233, 23.235, 23.253, 23.1325, 23.1511, 23.1521, 23.1543, 23.1553, 23.1555, 23.1559, 23.1567, 23.1581, 23.1583, 23.1585, 23.1587, and 23.1589 as amended by Amendment 23-50, effective March 11, 1996; FAR 23.777, 23.779, 23.901, 23.903, 23.907, 23.925, 23.929, 23.933, A25SO Page 14 of 25 23.955, 23.959, 23.963, 23.965, 23.973, 23.975, 23.1013, 23.1041, 23.1043, 23.1045, 23.1091, 23.1093, 23.1121, 23.1141, 23.1143, 23.1153, 23.1181, 23.1183, 23.1191, and 23.1337 as amended by Amendment 23-51, effective March 11, 1996; and FAR 23.1305 as amended by Amendment 23-52, effective July 25, 1996. In addition, FAR 34.11, effective September 10, 1990, and FAR 36, Appendix G, Amendment 36-22. Equivalent Level of Safety (ELOS) for FAR 23.955(f)(3), June 6, 2000. Special Condition 23-123-SC (Docket CE153), August 27, 1999. Compliance with the requirements of FAR 23.1419 as amended by Amendment 23-14, effective December 20, 1973, has been established , provided the required ice protection systems are installed and functioning properly. For aircraft equipped with Piper factory installed Avidyne Entegra system and S-Tec Magic 1500 DFCS (See Piper Report VB-1919), the additional certification basis for installation specific items only is: FAR 23.1523 as amended by Amendment 23-34; FAR 23.613 as amended by Amendment 23-45; 14 CFR Part 23 regulations FAR 23.607 as amended by Amendment 23-48; FAR 23.1351, 23.1365, and 23.1431 as amended by Amendment 23-49; FAR 23.1545 and 23.1563 as amended by Amendment 23-50; Special Condition for HIRF (Docket # CE215, Special Condition 23-154-SC), January 7, 2005. Eligible Serial Numbers: 4697198, 4697216 and up. For aircraft equipped with Piper factory installed G1000 system and GFC700 AFCS (see Piper Report VB-1988), the additional certification basis for installation specific items only is: 14 CFR 23.1523 as amended by Amendment 23-34; 14 CFR 23.613, 23.672 as amended by Amendment 23-45; 14 CFR 23.607 as amended by Amendment 23-48; 14 CFR 23.1351, , 23.1365, and 23.1431 as amended by Amendment 23-49; 14 CFR 23.1545 and , 23.1563 as amended by Amendment 23-50; Special Condition for HIRF (Docket # CE215, Special Condition 23-154-SC), January 7, 2005. Eligible Serial Numbers: 4697340, 4697399and up. PA-46-500TP serial numbers 4697001, 4697003 through 4697423 affected by Piper Service Bulletin SB1195B, only in the area of the communications antenna installations, the following additional certification basis is applicable: 14 CFR 23.571(c), 23.573(b) as amended by Amendment 23-45, effective September 7, 1993. PA-46-500TP aircraft equipped with Piper factory installed Enviro Cabin Pressure Control System, the additional certification basis for installation specific items only is: 23.303, 23.307, 23.601, 23.609, 23.627, 23.843(b) as amended by Amendment 23-0 effective February 1, 1965; 23.625 as amended by Amendment 23-7 effective September 14, 1969; 23.29 as amended by Amendment 23-20 effective September 9, 1977; 23.29, as amended by Amendment 23-21 effective March 1, 1978; 23.603, 23.605(a) as amended by Amendment 23-23 effective December 1, 1978; 23.607, 23.613 as amended by Amendment 23-25 effective March 3, 1980; 23.1529 as amended by Amendment 23-26 effective October 14, 1980; 23.831(b) as amended by Amendment 23-42 effective February 4, 1991; 23.1322 (a)(b)(c)(d) as amended by Amendment 23-43effective May 10, 1993; 23.305 as amended by Amendment 23-45 effective September 7, 1993; 23.301(a)(b)(c), 23.337, 23.341(a)(c), 23.473, 23.561(a)(b))(3)(e)23.611 as amended by Amendment 23-48 effective March 11, 1996; 23.841(a)(b)(1)(2)(3)(4)(b)(5)(6)(7)(8)(9), 23.867, 23.1307, 23.1351(a)(1)(i) as amended by Amendment 23-49 effective March 11, 1996; 23.25, 23.1325(b)(1)(2)(ii)(3)23.1581(a)23.1583(h)(m)23.1585(j) as amended by Amendment 23-50 effective March 11, 1996; 23.1308(a)(b)(c) as amended by Amendment 23-57 effective September 5, 2007; 23.1306, as amended by Amendment 23-61 effective August 8, 2011; 23.1301(a)(b)(c), 23.1309(a)(1)(2)b)(c)(d) as amended by Amendment 23-62 effective January 31, 2012. Eligible Serial Numbers: 4697549, 4697569, 4697582 and up. PA-46-500TP aircraft equipped with Piper factory installed G1000 Phase III Integrated Avionics the additional certification basis for installation specific items only is: 23.21, 23.23(a), 23.25(a)(b), 23.29, 23.143(a)(b), 23.207(b), 23.251, 23.301(a)(b)(c), 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.365(a)(b)(d), 23.473, 23.561(a)(b)(3)(e), 23.571(a), 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), A25SO Page 15 of 25 23.1305(a)(1)(2)(3)(c)(1)(2)(3)(4)(5)(6)(8),(e)(1)(2), 23.1306, 23.1307, 23.1308(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(d)(e), 23.1311(a)(1)(2)(3)(4)(5)(6)(7)(b)(c), 23.1321(a)(c)(d)(5)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(c), 23.1325(a)(b)(1)(2)(ii), 23.1326(a)(b), 23.1327(a), 23.1329(d)(e)(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i)(b)(1)(i)(3)(c)(4)(d), 23.1353(a)(b)(c)(d)(e)(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1361(a)(c), 23.1365, 23.1367(a)(b)(c)(d), 23.1381(a)(b)(c), 23.1416(c), 23.1419(c), 23.1431(a)(b)(e), 23.1501(a)(b), 23.1523, 23.1525, 23.1529, 23.1541(a)(b), 23.1543(b)(c), 23.1545(a)(b)(1)(2)(3)(4), 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 as amended by Amendment 23-61 effective June 8, 2011; 23.1303(a)(b)(c)(f) as amended by Amendment 23-62 effective January 31, 2012. Eligible Serial Numbers: 4697549, 4697569, 4697582 and up. PA-46-500TP aircraft equipped with Piper factory installed G1000NXi Integrated Avionics the additional certification basis for installation specific items only is: 14CFR 23.23(a)(b)(3), 23.25(a)(b), 23.29, 23.301(a)(b)(c), 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, 23.699, 23.771(a), 23.777(a)(b), 23.867, 23.1301(a)(b)(c)(d), 23.1305(a)(1)(2)(3)(c)(1)(2)(3)(4)(5)(6)(8)(e), 23.1306, 23.1308(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(d)(e), 23.1311(a)(1)(2)(3)(4)(5)(6)(7)(b)(c), 23.1321(a)(c)(d)(5)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(c), 23.1325(a)(b)(1)(2)(ii), 23.1326, 23.1327(a), 23.1329(a)(1)(b)(c)(d)(e)(f)(g)(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i)(c)(4)(d), 23.1353(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365, 23.1367(a)(b)(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 Amendment 23-61 effective June 8, 2011; 14 CFR 23.1303(a)(b)(c)(f) as amended by Amendment 23-62 effective January 31, 2012. Eligible Serial Numbers: 4697626, 4697631 and up. PA-46-500TP aircraft equipped with optional non-Halon fire extinguisher additional certification basis for installation specific items only is: 14 CFR 23.851, 23.1301 as amended by Amendment. 23-62 effective January 31, 2012. Eligible Serial Numbers: 4697684 and up. PA-46R-350T: For those portions of the airplane that are unchanged from the Model PA-46-350P: FAR Part 23, effective February 1, 1965, as amended by Amendment 23- 25, effective March 6, 1980; FAR 25.783(e) as amended by Amendment 25-54, effective October 14, 1980; FAR 25.831(c) and (d) as amended by Amendment 25-41, effective September 1, 1977. No equivalent safety findings. Special Conditions No. 23-ACE-53, Docket No. 082CE. For the Avidyne Entegra system installation (See Piper Report VB-1954) and modifications to that installation (See Piper Report VB-2008) the following additional requirements are applicable: FAR 23.1529 as amended by Amendment 23-26, effective 14 October 1980; FAR 23.1523 as amended by Amendment 23-34, effective 17 February 1987; FAR 23.1322, 23.1331, 23.1357 (a)(2), (b), (c), (d) as amended by Amendment 23- 43, effective 10 May 1993; FAR 23.305, 23.613, 23.773 (a)(2), 23.1525, 23.1549 (a) as amended by Amendment 23-45, effective 7 September 1993; FAR 23.301, 23.337 (a)(1), (b)(1), 23.341 (a), 23.473, 23.561 (b)(3), (e), 23.571 (a), 23.607, 23.611, as amended by Amendment 23-48, effective 11 March 1996; FAR 23.1303 (a), (b), (f), 23.1307, 23.1309 (a), (a)(1), (a)(2), (b),(e), 23.1311 (a)(2), (a)(3), (a)(4), (a)(5), (a)(6), (a)(7), (b), (c), 23.1321 (a), (c), (d), (e), 23.1323 (a), (c), 23.1329, 23.1351 (a)(1), (a)(2)(i), (b)(2), (b)(3), 23.1353 (d), (h), 23.1359 (c), 23.1365 (a), (b), (d), (e), (f), 23.1431 (a), (b) as amended by Amendment 23-49, effective 11 March 1996; FAR 23.1325 (a), (b)(1), (b)(2)(ii), (b)(3), (c), (e), 23.1543 (b), (c), 23.1545(a), (b)(3), (b)(4), (c), 23.1555 (a), (b), 23.1563, 23.1581 (a), (b)(2), (b)(3), (f), 23.1583 (m), 23.1585 (j) as amended by Amendment 23-50, effective 11 March1996; FAR 23.777 (a), (b), 23.1337 as amended by Amendment 23-51, effective 11 March 1996; FAR 23.1305 (a)(1), (a)(2), (a)(3), A25SO Page 16 of 25 (b)(2), (b)(3), (b)(4), (b)(5), (b)(6)(i) as amended by Amendment 23-52, effective 25 July 1996 Special Condition for HIRF (Docket # CE215, Special Condition 23-154-SC), January 7, 2005. For modifications specific to the PA-46R-350T airplane (see Piper Report VB-2008) the following additional requirements are applicable: FAR 23.1529 and Appendix G (Sec G23.1 and G23.2) as amended by Amendment 23-26, effective 14 October 1980; Appendix G (Sec G23.3) as amended by Amendment 23-34 effective 17 February 1987; FAR 23.2 as amended by Amendment 23-36 effective 14 September 1988; Appendix G (Sec G23.4) as amended by Amendment 23-37, effective 18 August 1990; FAR 23.831 as amended by Amendment 23-42, effective 4 February 1991; FAR 23.905, 23.1357, 23.1441, 23.1443, and 23.1445 as amended by Amendment 23-43, effective 10 May 1993; FAR 23.613, 23.773, 23. 851, and 23.1527 as amended by Amendment 23-45, effective 7 September 1993; FAR 23.561, 23.572,, 23.575, 23.607, and 23.611 as amended by Amendment 23-48, effective 11 March 1996; FAR 23.775, 23.783, 23.853, 23.1309, 23.1311, 23.1321, 23.1323, 23.1351, 23.1447, 23.1451, 23.1453, and Appendix F (Sec F23) as amended by Amendment 23-49, effective 11 March 1996; FAR 23.25, 23.1325, 23.1543, 23.1545, and 23.1589 as amended by Amendment 23-50, effective 11 March 1996; FAR 23.907 and 23.1191 as amended by Amendment 23-51, effective 11 March 1996; and FAR Part 36, effective December 1, 1969, as amended by Amendment 36-1, dated December 1, 1969 through Amendment 36-28, dated 3 February 2006 For the PA-46R-350T Matrix aircraft equipped with Hartzell propeller HC-I3Y1R- 1N/N7605+2 or HC- I3Y1R-1N/N7605K+2 or HC-I3Y1R-1N/N7605C+2 or HC-I3Y1R- 1N/N7605CK+ (See Piper Report VB-2132) the additional certification basis for installation specific items only is: 23.907 as amended by Amendment 23-59, effective 24 October 2008. Eligible Serial Numbers: 4692123 & up. For PA-46R-350T aircraft equipped with Piper factory installed Garmin G1000 system and GFC 700 AFCS (See Piper Drawing 106900), the additional certification basis for installation specific items only as amended by Amendment 23-59 dated December 23, 2008, is: 14 CFR 23.23 14 CFR 23.25 14 CFR 23.251 14 CFR 23.301 (a), (b), (c) 14 CFR 23.305 14 CFR 23.337 14 CFR 23.341 14 CFR 23.397 (a) 14 CFR 23.473 14 CFR 23.561 (a), (b)(3), (e) 14 CFR 23.607 14 CFR 23.611 14 CFR 23.613 14 CFR 23.677 (b), (d) 14 CFR 23.773 (a)(l), (a)(2) 14 CFR 23.777 (a), (b), (d) 14 CFR 23.867 14 CFR 23.1141 (a), (b), (c), (d) 14 CFR 23.1303 (a), (b), (c), (f) 14 CFR 23.1305 (a)(l), (a)(2), (a)(3), (b)(2), (b)(4)(i), (b)(5), (b)(6)(i) 14 CFR 23.1307 14 CFR 23.1308 (a) (1), (a)(2), (a)(3), (b), (c) 14 CFR 23.1309 (a) (1), (a)(2), (b), (c), (e) 14 CFR 23.1311 (a)(l), (a)(2), (a)(3), (a)(4), (a)(5), (a)(6), (a)(7), (b), (c) 14 CFR 23.1321 (a), (c), (d)(5), (e) 14 CFR 23.1322 (a), (b), (c), (d), (e) 14 CFR 23.1323 (a), (c) 14 CFR 23.1325 (a), (b)(l), (b)(2)(i) 14 CFR 23.1326 A25SO Page 17 of 25 14 CFR 23.1329 (a) (1), (b), (d), (e), (f), (g), (h), 14 CFR 23.1331 (a), (b), (c) 14 CFR 23.1337 (b)(l), (b)(4) 14 CFR 23.1351 (a)(l), (a)(2)(i), (b)(l)(i) 14 CFR 23.1353 (h) 14 CFR 23.1357 (a)(2), (b), (c), (d) 14 CFR 23.1359 (c) 14 CFR 23.1365 (a), (b), (d), (e), (f) 14 CFR 23.1431 (a), (b), (e) 14 CFR 23.1441 (b), (c), (e) 14 CFR 23.1507 14 CFR 23.1523 14 CFR 23.1525 14 CFR 23.1529 14 CFR 23.1543 (b)(c) 14 CFR 23.1545 (a), (b) (1), (b)(2), (b)(3), (b) (4) 14 CFR 23.1549 (a), (b), (c) 14 CFR 23.1553 14 CFR 23.1555 (a), (b), (d)(2) 14 CFR 23.1559 (c) 14 CFR 23.1563 (a) (b) 14 CFR 23.1567 (a) 14 CFR 23.1581 14 CFR 23.1583 14 CFR 23.1585 14 CFR 23.1589 Eligible Serial Numbers: 4692134 and up PA-46-600TP: The PA-46-600TP is a derivative product from the PA-46-500TP. As such, the regulations that were applicable to the basic PA-46-500TP that are not affected by the changed product (PA-46-600TP) remain at the original amendment levels. Those regulations that are affected by the change are FAR 23, effective February 1, 1965, as amended by 14 CFR Part 23 Amendment 23-62, effective January 31, 2012 The following regulations have been granted approval at the amendment levels specified herein: 14 CFR 23.701, 23.783, 23.785, 23.807 as amended by Amendment 23-25 effective March 6, 1980 14 CFR 23.1419 as amended by Amendment 23-43 effective May 10, 1993 14 CFR 23.251, 23.571, 23.572 as amended by Amendment 23-45 effective September 7, 1993 14 CFR 23.783(a)(b)(e)(2)(3), 23.1353 as amended by Amendment 23-49 effective March 11, 1996 14 CFR 34.11 as amended by Amendment 34-4 effective June 29, 2009 14 CFR 36 as amended by Amendment 36-28 effective February 3, 2006 14 CFR 23.562 and 23.573 are not included in the certification basis Aircraft is approved for Flight Into Known Icing. This aircraft is approved for single pilot operation. The following ELOS have been issued for this model: ELOS #AT13893AT-A-P-1: Equivalent Level of Safety Finding for Digital Display of Engine and Propeller Flight Data 14 CFR 23.1305(c)(2)(5), 23.1311(a)(6), 23.1549 ELOS #AT13893AT-A-F-1: Equivalent Level of Safety Finding for Control Forces 14 CFR 23.145(b)(2)(4) ELOS #AT13893AT-A-A-1: Equivalent Level of Safety Finding for Material Design Values 14 CFR 23.613 A25SO Page 18 of 25 ELOS #AT13893AT-A-G-9: Amendment 23-62 Equivalent Level of Safety 14 CFR 23.45, 23.51, 23.63, 23.73, 23.77, 23.161, 23.181, 23.221, 23.251, 23.253, 23.831, 23.1527, 23.1545, 23.1583 ELOS - FAA Project AT2572AT-A: Equivalent Level of Safety for 14 CFR 23.955(f)(3), June 6, 2000 14 CFR 23.955(f)(3) Eligible Serial Numbers: 4698001 and up For the PA-46-600TP M600 aircraft equipped with Hartzell propeller model 5D3- N338A1/78D01B the additional certification basis for installation specific items only is: 14 CFR 23.25(a)(b), 23.29(a)(b), 23.33(a)(d)(1)(2)(ii), 23.45((a)(1)(2)(b)(1)(3)(d)(1)(2)(e)(1)(2)(f)(g)(1)(4), 23.49(a)(2)(3)(4)(5)(6)(b)(c)(1)(2)(d), 23.51(a)(2)(b)(2)(i)(ii), 23.53(a)(b)(1)(2)(3), 23.65(b)(1)(2)(3)(4), 23.69(a)(1)(2)(3)(4), 23.71, 23.75(a)(1)(b)(c)(d)(e), 23.77(b)(1)(2)(3)(4), 23.143, 23.145(b)(2)(4), 23.201(a)(b)(1)(3)(c)(d)(e)(f(1)(2)(5)(i)((iii)(6)(7), 23.203(a)(1)(2)(b)(1)(2)(3)(4)(4)(5)(6)(c)(1)(2)(5)(i)(iii)(6)(7), 23.251(a)(b)(c)(d), 23.301(a)(b)(c), 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.601, 23.603, 23.605(a), 23.607, 23.609, 23.611, 23.613, 23.625, 23.627, 23.629(a)(c)(e), 23.901(a)(b)(1)(2)(e), 23.903(e)(3)(f)(g), 23.905(a)(b)(c)(d), 23.907(a)(2)(b)(c), 23.925(a)(d), 23.929, 23.933(b), 23.1027, 23.1041, 23.1043(a)(1)(2)(3)(b)(c), 23.1045, 23.1153, 23.1301(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(d), 23.1501(a)(b), 23.1521(a)(b)(1)(4)(c)(1)(e), 23.1529, 23.1541(a)(1)(2), 23.1549, 23.1581(a), 23.1583(b)(m), 23.1585(a)(b)(j), 23.1587(a) as amended by Amendment 23-62, effective December 2, 2011; 14 CFR 23.1419 as amended by Amendment 23-43 effective May 10, 1993; 21.93 as amended by Amendment 21-97, effective January 8, 2013. Eligible Serial Numbers: 4698001 & up For the PA-46-600TP M600 aircraft equipped with Garmin G3000 installed per Piper Drawing 46F34A000-002 the additional certification basis for installation specific items only is: 14 CFR 23.23(a)(b)(3), 23.25(a)(b), 23.29, 23.301(a)(b)(c), 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, 23.699(b)(1)(2), 23.729(e)(f), 23.771(a), 23.773(a)(1)(2), 23.777(a)(b), 23.867, 23.1301(a)(b)(c), 23.1303(a)(b)(c)(f), 23.1305(a)(1)(2)(3)(c)(1)(2)(3)(4)(5)(6)(8)(e), 23.1306, 23.1308(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(d), 23.1310(a)(1)(2)(4)(b), 23.1311(a)(1)(2)(3)(4)(5)(6)(7)(b)(c), 23.1321(a)(c)(d)(5)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(c), 23.1325(a)(b)(1)(2)(ii), 23.1326, 23.1327(a), 23.1329(a)(1)(b)(c)(d)(e)(f)(g)(h), 23.1335, 23.1337(b)(1)(4), 23.1351(a)(1)(2)(i)(c)(4)(d)(1), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365, 23.1367(a)(b)(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)(4)(d), 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(a) as amended by Amendment 23-62, effective January 31, 2012; 23.1353(h) as amended by Amendment 23-49, effective March 11, 1996; Eligible Serial Numbers: 4698061, 4698081 & up For the PA-46-600TP M600 aircraft equipped with the Emergency Autoland (HALO) option installed by Piper Drawing 46G00A000-002 and 46G22A000-001 the additional certification basis for installation specific items only is: 14 CFR 23.251 as amended by Amendment 23-45, effective September 7, 1993; 14 CFR 23.1353(h) as amended by Amendment 23-49, effective March 11, 1996; 14 CFR 23.21(b), 23.23(a)(b)(3), 23.25(a)(b), 23.29, 23.301(a)(b)(c), 23.303, 23.305, 23.307, 23.337, 23.341(a)(c), 23.405, 23.473, 23.561(a)(b)(3)(e), 23.601, 23.603, A25SO Page 19 of 25 23.605(a), 23.607, 23.609, 23.611, 23.613, 23.625, 23.627, 23.671(a), 23.681, 23.683, 23.685, 23.697(a), 23.729(e), 23.735(a)(b)(c)(d), 23.771(a), 23.777(a)(b), 23.779(a)(2)(b)(1)(2), 23.867, 23.905(b), 23.951(a)(b)(c), 23.954, 23.955(a)(f)(1), 23.961, 23.991(b), 23.993(a)(b)(c)(d)(e), 23.994, 23.995(b)(1)(c)(d), 23.1141(c)(e)(g)(2), 23.1155, 23.1189(c), 23.1301(a)(b)(c), 23.1303, 23.1305(a)(1)(2)(3)(5)(c)(1)(2)(3)(4)(5)(6)(8)(e)(1)(2), 23.1306, 23.1308(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(1)(2)(3)(d), 23.1310(a)(1)(2)(4)(b), 23.1311(a)(1)(2)(3)(6)(7)(b), 23.1321(a)(c)(e), 23.1322(a)(b)(c)(d)(e), 23.1326, 23.1327(a)(1), 23.1329(a)(1)(b)(c)(e)(f)(g), 23.1335, 23.1337(b)(1), 23.1351(a)(1)(2)(i), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365, 23.1367(a)(b)(c)(d), 23.1381(a)(b)(c), 23.1431(a)(b)(e), 23.1501, 23.1521(a)(b)(1)(3)(4)(c)(1)(3), 23.1523, 23.1525, 23.1529, 23.1541(a)(b), 23.1555(a)(b)(e)(1)(2), 23.1581(a)(c), 23.1583(g)(h)(m), 23.1585(j), 23.1589(a) as amended by Amendment 23-62, effective January 31, 2012; Eligible Serial Numbers: 4698061, 4698081 & up For the PA-46-600TP M600 aircraft equipped with the Normal Use Autothrottle option installed by Piper Drawing 46G00A000-003 and 46F76A020-003 the additional certification basis for installation specific items only is: 14 CFR Part 21, 21.93 (b) as amended by Amendment 21-97 effective March 11, 2013; 14 CFR Part 23, 23.1353 (h) as amended by Amendment 23-49 effective March 11, 1996; 14 CFR Part 23, 23.21 (b), 23.23 (a)(b)(3), 23.25 (a)(1)(iii), 23.143 (a)(1)(2)(3)(4)(5)(b)(c), 23.145 (b)(2)(4), 23.771 (a), 23.777 (a)(b), 23.779 (b), 23.781 (b), 23.1141 (c)(e), 23.1301 (a)(b), 23.1306, 23.1308 (a)(b)(c), 23.1309 (a)(1)(2)(b)(c)(1)(2)(3)(d), 23.1310 (a)(1)(2)(4)(b), 23.1311 (a)(2)(6)(7), 23.1321 (a)(c)(e), 23.1322 (a)(b)(c)(d)(e), 23.1327 (a)(1), 23.1335, 23.1351 (a)(1)(2)(i)(b)(1), 23.1357 (a)(b)(c)(d), 23.1359 (c), 23.1365, 23.1367 (a)(b)(c)(d), 23.1381 (a), 23.1431 (a)(b)(e), 23.1501 (a)(b), 23.1521 (a), 23.1523 (a)(b)(c), 23.1525, 23.1529, 23.1541 (a)(b), 23.1543 (b), 23.1555 (a)(b), 23.1581 (a)(c), 23.1583 (b)(1)(2)(m), 23.1585(j) as amended by Amendment 23-62 effective January 31, 2012; 14 CFR Part 23, 23.2010 (a)(b), 23.2500 (a)(1)(2)(b), 23.2510 (a)(b)(c), 23.2600 (a)(b), 23.2605 (a)(b)(c) as amended by Amendment 23-64 effective August 30, 2017; Eligible Serial Numbers: 4698061, 4698081 & up For the PA-46-600TP M600 aircraft equipped with System Software Release 7 and GDL 60 Datalink installed by Piper Drawing 46F34A000 the additional certification basis for installation specific items only is: 14 CFR 21.93(b) as amended through Amendment 21-97, effective March 3, 2013; 14 CFR 23.1353(h) as amended through Amendment 23-49, effective March 11, 1996; 14 CFR 23.23(a)(b)(3), 23.25(a)(b), 23.301(a)(b)(c), 23.303, 23.305, 23.307(a), 23.561(a)(b)(3)(e), 23.603, 23.605(a), 23.607, 23.609(a), 23.611, 23.613(a)(b), 23.627, 23.771(a), 23.867, 23.1301(a)(b)(c), 23.1306, 23.1308(a)(b)(c), 23.1309(a)(1)(2)(b)(c)(d), 23.1310(a)(1)(2)(4)(b), 23.1311(a)(1)(2)(3)(4)(6)(7), 23.1321(e), 23.1322(e), 23.1351(a)(1)(2)(i), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365, 23.1431(a)(b)(e), 23.1501(a)(b), 23.1523, 23.1525, 23.1529, 23.1581(a)(c), 23.1583(g)(h)(m), 23.1585(j), 23.1589(a) as amended through Amendments 23-62, effective January 31, 2012; 23.2010(a)(b), 23.2500(a)(2)(b), 23.2505, 23.2510, 23.2600(b), 23.2605(a)(b)(c), 23.2610(a)(b)(c) as amended through Amendment 23-64, effective August 30, 2017; Eligible Serial Numbers 4698061, 4698081 & up PA-46-701TP: The PA-46-701TP is a derivative product from the PA-46-600TP. As such, the PA-46-701TP certification basis was derived from the PA-46-600TP, which includes regulations applicable to the basic PA-46-500TP. Those regulations that are affected by the change (from the PA-46-500TP) are 14 CFR Part 23, effective February 1, 1965, as amended by 14 CFR Part 23 Amendment 23-62, effective January 31, 2012. A25SO Page 20 of 25 The following regulations at the amendment levels specified herein provide clarification of the applicable certification basis: 14 CFR Part 23, effective February 1, 1965, as amended by 14 CFR Part 23 Amendment 23- 62, effective January 31, 2012. Except as follows: 14 CFR 23.701, 23.783, 23.785, 23.807 as amended by Amendment 23-25 effective March 6, 1980 14 CFR 23.1419 as amended by Amendment 23-43 effective May 10, 1993 14 CFR 23.251, 23.571, 23.572 as amended by Amendment 23-45 effective September 7, 1993 14 CFR 23.783(a)(b)(e)(2)(3), 23.1353 as amended by Amendment 23-49 effective March 11, 1996 For landing gear warning inhibit function and wireless local area network capabilities, the additional certification basis for installation specific items only is: 14 CFR Part 23.2010(a)(b), 23.2500(a)(2)(b), 23.2505, 23.2510, 23.2600(b), 23.2605(a)(b)(c), 23.2610(a)(b)(c) as amended by Amendment 23-64, effective August 30, 2017; For aircraft equipped with the Normal Use Autothrottle option, the additional certification basis for installation specific items only is: 14 CFR 23.2010(a)(b), 23.2500(a)(1)(2)(b), 23.2510(a)(b)(c), 23.2600(a)(b), 23.2605(a)(b)(c) as amended by Amendment 23-64, effective August 30, 2017. 14 CFR 34.11 as amended by Amendment 34-4 effective June 29, 2009 14 CFR 36 as amended by Amendment 36-31 effective November 3, 2017 14 CFR 23.562 and 23.573 are not included in the certification basis Aircraft is approved for Flight Into Known Icing. This aircraft is approved for single pilot operation. The following ELOS apply to this model: ELOS #AT13893AT-A-P-1: Equivalent Level of Safety Finding for Digital Display of Engine and Propeller Flight Data 14 CFR 23.1305(c)(2)(5), 23.1311(a)(6), and 23.1549 ELOS #AT13893AT-A-F-1: Equivalent Level of Safety Finding for Control Forces 14 CFR 23.145(b)(2)(4) ELOS #AT13893AT-A-A-1: Equivalent Level of Safety Finding for Material Design Values 14 CFR 23.613 ELOS #AT13893AT-A-G-9: Amendment 23-62 Equivalent Level of Safety 14 CFR 23.45, 23.51, 23.63, 23.73, 23.77, 23.161, 23.181, 23.221, 23.251, 23.253, 23.831, 23.1527, 23.1545, 23.1583 ELOS - FAA Project AT2572AT-A: Equivalent Level of Safety for 14 CFR 23.955(f)(3), June 6, 2000 14 CFR 23.955(f)(3) Eligible Serial Numbers: 46020001 and up Production Basis Production Certificate No. 206. Production Limitation Record issued and the manufacturer authorized to issue airworthiness certificate under the delegation option provisions of FAR 21. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. A25SO Page 21 of 25 In addition, one of the following items of equipment are required: 1. DOA No. SO-1 approved Airplane Flight Manual Piper Report FT 157, Appendix D or Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1200 for Model PA-46-310P, S/N 46-8408001 through 46-8608067, and 4608001 through 4608007. 2. DOA No. SO-1 approved Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1300 for Model PA-46-310P, S/N 4608008 through 4608140. 3. DOA No. SO-1 approved Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1332 for Model PA-46-350P, S/N 4622001 through 4622200. 4. DOA No. SO-1 approved Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1609 for Model PA-46-350P, S/N 4636001 through 4636020. 5. DOA No. SO-1 approved Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1602 for Model PA-46-350P, S/N 4636021 through 4636131. 6. DOA No. SO-1 approved Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1446 for Model PA-46-350P, S/N4636132 through 4636195. For S/N 4636160 special supplement VB-1855 is required. 7. DOA No. SO-1 approved Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1710 for Model PA-46-350P, S/N 4636196 through 4636374. 8. DOA No. SO-1 approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1689 for Model PA-46-500TP, S/N 4697001, 4697003 through 4697156. 9. DOA No. SO-1 approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1751 for Model PA-46-500TP, (1999 kg) S/N 4697001, 4697003 through 4697156 10. DOA No. SO-1 approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1835 for Model PA-46-500TP (5092 lb. MTOGW) S/N 4697157 through 4697173 and earlier airplanes having Kit 767- 360 installed. 11. DOA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1888 for Model PA-46-500TP S/N 4697174 and up. 12. DOA No. 510620-CE approved Pilot's Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1912 for Model PA-46-500TP S/N's 4697198, 4697216 and up equipped with standard Avidyne Entegra System. 13. DOA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1948 for Model PA-46-500TP, (1999 kg) S/N’s 4697198, 4697216 and up. 14. DOA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report No. VB-1950 for PA-46-350P S/N’s 4636375 and up. 15. DOA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2007 for PA-46R-350T S/N’s 4692001 and up. 16. DOA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-1993 for PA-46-500TP S/N’s 4697340, 4697399 and up equipped with Garmin G1000 System and GFC700 FCS. 17. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2182 for PA-46-500TP (1999 kg) S/N’s 4697340, 4697399 and up equipped with Garmin G1000 System and GFC700 System. 18. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2121 for PA-46-350P S/N’s 4636460, 4636463 and up equipped with Garmin G1000 System and GFC700 AFCS. 19. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2122 for PA-46R-350T S/N’s 4692134 and up equipped with Garmin G1000 System and GFC700 AFCS. A25SO Page 22 of 25 20. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2543 for PA-46-500TP S/N’s 4697549, 4697569, 4697582 and up equipped with Garmin G1000 Phase III System and Enviro Cabin Pressure Control System. 21. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2561 for PA-46-350P S/N’s 4636633, 4636652 and up when equipped with Garmin G1000 Phase III System and Enviro Cabin Pressure Control System. 22. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2366 for PA-46-600TP S/N’s 4698001 and up. 23. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2747 for PA-46-350P S/N’s 4636716, 4636720 and up. 24. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2748 for PA-46-500TP S/N’s 4697626, 4697631 and up. 25. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2872 (1999 kg) for PA-46-500TP S/N’s 4697626, 4697631 and up. 26. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2793 for PA-46-600TP S/N’s 4698061, 4698081 and up. 27. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2793 Rev 4, or later FAA approved version, for PA-46-600TP when equipped with the optional Emergency Autoland (HALO) system S/N’s 4698061, 4698081 and up. 28. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2793 Rev 10, or later FAA approved version, for PA-46-600TP when equipped with the optional Normal Use Autothrottle system S/N’s 4698061, 4698081 and up. 29. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2793 Rev 13, or later FAA approved version, for PA-46-600TP equipped with G3000 Software Release 7 and GDL 60 datalink S/N’s 4698061, 4698081 and up. 30. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2747 Rev 8, or later FAA approved version, for PA-46-350P equipped with landing gear warning inhibit function and wireless local area network capabilities SN’s 4636716, 4636720 and up 31. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2818 for PA-46-701TP S/N’s 46020001 and up. 32. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2747 Rev 11, or later FAA approved version, for PA-46-350P equipped with optional non-Halon fire extinguisher, effective for SN’s 4636795 and up 33. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2748 Rev 10, or later FAA approved version, for PA-46-500TP equipped with optional non-Halon fire extinguisher, effective for S/N’s 4697684 and up. 34. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2793 Rev 15, or later FAA approved version, for PA-46-600TP equipped with optional non-Halon fire extinguisher, effective for S/N’s 4698198 and up. 35. ODA No. 510620-CE approved Pilot’s Operating Handbook and FAA approved Airplane Flight Manual Report VB-2818 Rev 3, or later FAA approved version, for PA-46-701TP equipped with optional non-Halon fire extinguisher, effective for S/N’s 46020001 and up. Noise Characteristics The corrected noise level of the Model PA-46-310P is 74.8 dB(A) at the Maximum Normal Operating Power at 2600 rpm. The noise level stated above has been approved by the Federal Aviation Administration in noise level test flights conducted A25SO Page 23 of 25 in accordance with FAR 36, "Noise Standards: Aircraft Type and Airworthiness Certification." The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the Model PA-46-350P is 74.7 dB(A) at the Maximum Normal Operating Power at 2500 rpm. The noise level stated above has been approved by the Federal Aviation Administration in noise level test flights conducted in accordance with FAR 36, "Noise Standards: Aircraft Type and Airworthiness Certification." The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the Model PA-46-350P equipped with the optional 3 blade propeller is 79.7 dB(A) at the Maximum Normal Operating Power at 2500 rpm. The noise level stated above has been approved by the Federal Aviation Administration in noise level flight tests conducted in accordance with FAR 36, "Noise Standards: Aircraft Type and Airworthiness Certification." The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the Model PA-46-350P equipped with the optional 3 blade propeller HC-I3Y1R-1N/N7605C+2 or HC-I3Y1R-1N/N7605CK+2 is 81.0 dB(A) at the Maximum Normal Operating Power at 2500 rpm. The noise level stated above has been approved by the Federal Aviation Administration in noise level flight tests conducted in accordance with FAR 36, "Noise Standards: Aircraft Type and Airworthiness Certification." The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the model PA-46-500TP equipped with the standard 4 blade propeller is 73.7 dB(A) at 4850 lbs. takeoff weight and 76.8 dB(A) at 5092 lbs. takeoff weight at the Maximum Normal Operating Power at 2000 RPM. This noise level has been approved by the Federal Aviation Administration in noise level flight tests conducted in accordance with FAR 36, “Noise Standards: Aircraft Type and Airworthiness Certification.” The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the model PA-46R-350T is 81.3 dB(A) at the Maximum Normal Operating Power at 2500 rpm. The noise level stated above has been approved by the Federal Aviation Administration in noise level flight tests conducted in accordance with FAR 36, “Noise Standards: Aircraft Type and Airworthiness Certification.” The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the Model PA-46R-350T equipped with the optional 3 blade propeller HC-I3Y1R-1N/N7605+2 or HC-I3Y1R-1N/N7605K+2 or HC-I3Y1R- 1N/N7605C+2 or HC-I3Y1R-1N/N7605CK+2 is 81.0 dB(A) at the Maximum Normal Operating Power at 2500 rpm. The noise level stated above has been approved by the Federal Aviation Administration in noise level flight tests conducted in accordance with FAR 36, "Noise Standards: Aircraft Type and Airworthiness Certification." The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the model PA-46-600TP equipped with the standard 4 blade propeller is 75.8 dB(A) at 6000 lbs. takeoff weight at the Maximum Normal Operating Power at 2000 RPM. This noise level has been approved by the Federal Aviation Administration in noise level flight tests conducted in accordance with FAR 36, “Noise Standards: Aircraft Type and Airworthiness Certification.” The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the model PA-46-600TP equipped with the optional 5 blade propeller is 75.8 dB(A) at 6000 lbs. takeoff weight at the Maximum Normal Operating Power at 2000 RPM. This noise level has been evaluated and approved by the Federal Aviation Administration by analysis in accordance with FAR 36, “Noise Standards: Aircraft Type and Airworthiness Certification.” The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. The corrected noise level of the model PA-46-701TP is 73.1 dB(A) at 6000 lbs. takeoff weight at the Maximum Normal Operating Power at 2000 RPM. This noise level has been evaluated and approved by the Federal Aviation Administration by analysis in accordance with FAR 36, “Noise Standards: Aircraft Type and Airworthiness A25SO Page 24 of 25 Certification.” The aircraft noise is in compliance with FAR 36 noise standards applicable to this type. NOTE 1. Current Weight and Balance Report, including list of equipment included in certificated empty weight and loading instructions, when necessary, must be provided for each aircraft at the time of original certification. The certified empty weight and corresponding center of gravity locations must include undrainable system oil (not included in oil capacity) and unusable fuel as noted below: (a) PA-46-310P Fuel: 12 lb. at (+152.37) Oil: 2.8 lb. at (+53.5) (b) PA-46-350P & PA-46R-350T Fuel: 12 lb. at (+152.37) Oil: 3.8 lb. at (+61.0) (c) PA-46-500TP Fuel: 20.1 lbs. at (+144.37) Oil: 5.55 lbs. at (+77.76) (d) PA-46-600TP & PA-46-701TP Fuel: 20.1 lbs. at (+148.9) Oil: 5.55 lbs. at (+77.76) NOTE 2 All placards (including electronic placards) required in the POH and AFM must be displayed in the appropriate locations. The following placard must be displayed in clear view of the pilot: PA-46-310P and PA-46-350P: "The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the Normal Category. Other operating limitations which must be complied with when operating this airplane in this category are contained in the Airplane Flight Manual. No acrobatic maneuvers, including spins, approved." PA-46-500TP and PA-46R-350T: "This aircraft must be operated as a Normal Category Airplane in compliance with the operating limitations stated in the form of placards, markings and manuals. No acrobatic maneuvers, including spins, approved. This aircraft is approved for VFR, IFR day and night icing flight when equipped in accordance with the airplane flight manual." PA-46-600TP (may be an electronic placard): "This aircraft must be operated as a Normal Category Airplane in compliance with the operating limitations stated in the form of placards, markings and manuals. No acrobatic maneuvers, including spins, approved. This aircraft approved for V.F.R., I.F.R. day and night icing flight when equipped in accordance with the airplane flight manual." PA-46-701TP (electronic placard): "This aircraft must be operated as a Normal Category Airplane in compliance with the operating limitations stated in the form of placards, markings and manuals. This aircraft approved for V.F.R., I.F.R., day and night icing flight when equipped in accordance with the airplane flight manual. No acrobatic maneuvers, including spins, approved." NOTE 3 The life limits on components are contained in Chapter 4 of the appropriate Airplane Maintenance Manual for the models listed below: (a) PA-46-310P – Airplane Maintenance Manual 761-783. (b) PA-46-350P – Airplane Maintenance Manual 761-783 for Serial Numbers 4622001 through 4622200, Airplane Maintenance Manual 761-876 for Serial Numbers 4636001 and Up. (c) PA-46-500TP – Airplane Maintenance Manual 767-005 for Serial Numbers 4697001, 4697003 through 4697398 less 4697340. Airplane Maintenance Manual 767-072 for Serial Numbers 4697340, 4697399 and Up. (d) PA-46R-350T – Airplane Maintenance Manual 761-876. A25SO Page 25 of 25 (e) PA-46-600TP – Airplane Maintenance Manual 767-617. (f) PA-46-701TP – Airplane Maintenance Manual 767-120. NOTE 4 PA-46-350P serial numbers 4636196 and up incorporate additional structural strengthening of the wing landing gear that affects the maximum weights and C.G. range. This accounts for differences with respect to serial numbers 4622001 through 4622200 and 4636001 through 4636195. NOTE 5 Model PA-46-500TP and PA-46-600TP The maximum propeller shaft overspeed limit for the PT6A-42A is 100% (2205 r.p.m.) of all ratings. 91% propeller shaft speed is defined as 2000 r.p.m. and is the normal steady state operating limit. Gas generator speeds up to 104.1% are permissible for 10 seconds and 101.7% for unlimited periods subject to applicable temperature and other limits. 100% gas generator speed is defined as 37,468. NOTE 6 Model PA-46-500TP: Minimum propeller speed (N p) corresponding to minimum idle gas generator speed (Ng) is 1200 RPM. Model PA-46-600TP & PA-46-701TP: Minimum propeller speed (Np) corresponding to minimum idle gas generator speed (Ng) is 1180 RPM. NOTE 7 PA-46-500TP serial numbers 4697131, 4697137, and 4697666 were never manufactured. NOTE 8 Model PA-46-701TP The maximum propeller shaft overspeed limit for the PT6A-52 is 100% (2205 r.p.m.) of all ratings. 91% propeller shaft speed is defined as 2000 r.p.m. and is the normal steady state operating limit. 100% gas generator speed is defined as 37,468. ...END... ``` ## ADs (40, in force first) - [AD 2023-25-02](https://openairdocs.org/ad/2023-25-02): Control Column Section · Piper PA-46-350P, PA-46-500TP and PA-46-600TP. Effective Dec 19, 2023 - [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023 - [AD 2022-11-10](https://openairdocs.org/ad/2022-11-10): Wing Spar · Piper PA-46-600TP. Effective Jun 27, 2022 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2021-09-02](https://openairdocs.org/ad/2021-09-02): VACUUM SYSTEM · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Apr 16, 2021 - [AD 2019-12-12](https://openairdocs.org/ad/2019-12-12): Bulkhead · Piper PA-46-600TP. Effective Jul 12, 2019 - [AD 2018-14-01](https://openairdocs.org/ad/2018-14-01): Fuselage Skin · Piper PA-46-600TP. Effective Jul 25, 2018 - [AD 2017-16-03](https://openairdocs.org/ad/2017-16-03): Wing Spar · Piper PA-46-600TP. Effective Aug 9, 2017 - [AD 2016-01-01](https://openairdocs.org/ad/2016-01-01): Wings · Piper PA-46-500TP. Effective Feb 17, 2016 - [AD 2015-13-09](https://openairdocs.org/ad/2015-13-09): Cabin Pressure Control System · Piper PA-46-350P and PA-46-500TP. Effective Jul 13, 2015 - [AD 2013-13-01](https://openairdocs.org/ad/2013-13-01): Fuel Storage · Piper PA-46-310P, PA-46-350P, PA-46-500TP and 1 more. Effective Jul 10, 2013 - [AD 2011-06-10](https://openairdocs.org/ad/2011-06-10): Engine Indicating · Piper PA-46-310P, PA-46-350P and PA-46R-350T. Effective May 6, 2011 - [AD 2010-13-07](https://openairdocs.org/ad/2010-13-07): Engine Exhaust. · Piper PA-32R-301T and PA-46-350P. Effective Jul 28, 2010 - [AD 2009-07-08](https://openairdocs.org/ad/2009-07-08): 35-amp and 250-amp current limiters · Piper PA-46-350P and PA-46R-350T. Effective May 5, 2009 - [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009 - [AD 2008-26-11](https://openairdocs.org/ad/2008-26-11): Stall vane heater · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Jan 28, 2009 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2004-15-19](https://openairdocs.org/ad/2004-15-19): Protective Cover Over Percussion Caps or Silicon Tube Installed Over the End of the Trigger Mechanism Pin of the Oxygen Generators · Piper PA-46-500TP. Effective Sep 13, 2004 - [AD 2004-14-12](https://openairdocs.org/ad/2004-14-12): Control wheel attaching hardware · Piper PA-28-161, PA-28-181, PA-28R-201 and 8 more. Effective Aug 10, 2004 - [AD 2004-03-32](https://openairdocs.org/ad/2004-03-32): Electronic control modules · Piper PA-46-500TP. Effective Mar 29, 2004 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 2001-12-01](https://openairdocs.org/ad/2001-12-01): Inboard Flap Drive Bellcrank Assemblies · Piper PA-46-310P, PA-46-350P and PA-46-500TP. Effective Jun 29, 2001 - [AD 2001-10-09](https://openairdocs.org/ad/2001-10-09): Automatic Flight Control Systems · Aerostar PA-60-700P (Aerostar 700P), 208, 208B and 15 more. Effective Jun 15, 2001 - [AD 99-16-06](https://openairdocs.org/ad/99-16-06): Wing Attach Fittings · Piper PA-46-350P. Effective Sep 24, 1999 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 98-04-26](https://openairdocs.org/ad/98-04-26): AFM - Limitations Section - Icing · Piper PA-46-310P and PA-46-350P. Effective Mar 13, 1998 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 95-23-12](https://openairdocs.org/ad/95-23-12): Placard - Manifold Pressure Limits · Piper PA-46-350P. Effective Jan 8, 1996 - [AD 92-18-08](https://openairdocs.org/ad/92-18-08): Flight Control Systems · Piper PA-46-310P and PA-46-350P. Effective Oct 2, 1992 - [AD 92-15-14](https://openairdocs.org/ad/92-15-14): Air-Driven Attitude Gyro · Piper PA-46-310P and PA-46-350P. Effective Aug 22, 1992 - [AD 92-13-06](https://openairdocs.org/ad/92-13-06): Elevator Guide Tube · Piper PA-46-310P and PA-46-350P. Effective Aug 21, 1992 - [AD 92-13-07](https://openairdocs.org/ad/92-13-07): Empennage Countersunk Rivets · Piper PA-46-310P and PA-46-350P. Effective Aug 21, 1992 - [AD 88-25-08](https://openairdocs.org/ad/88-25-08): Engine Cooling System · Piper PA-46-310P. Effective Jan 3, 1989 - [AD 87-04-01](https://openairdocs.org/ad/87-04-01): Air Valve Linkage · Piper PA-46-310P. Effective Feb 24, 1987 - [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986 - [AD 2021-04-07](https://openairdocs.org/ad/2021-04-07) (historical): VACUUM SYSTEM · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Mar 30, 2021 - [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008 - [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008 - [AD 99-15-04 R1](https://openairdocs.org/ad/99-15-04-R1) (historical): Turbine Inlet Temperature System Calibration · Piper PA-46-310P and PA-46-350P. Effective Jul 28, 2000 - [AD 99-15-04](https://openairdocs.org/ad/99-15-04) (historical): Turbine Inlet Temperature System Calibration · Piper PA-46-310P and PA-46-350P. Effective Aug 31, 1999 ## Registered aircraft by registry model (OpenAirDocs) - [Piper PA 46-350P](https://openairdocs.org/model/piper-pa-46-350p): 665 aircraft (registry codes 7104620, 7104619, 7104627, 7104618) - [Piper PA46-500TP](https://openairdocs.org/model/piper-pa46-500tp): 374 aircraft (registry codes 7104622, 7104623) - [Piper PA-46-310P](https://openairdocs.org/model/piper-pa-46-310p): 215 aircraft (registry codes 7104605, 7104611, 7104624) - [Piper PA-46-600TP](https://openairdocs.org/model/piper-pa-46-600tp): 189 aircraft (registry codes 7104650, 7104652) - [Piper PA46R-350T](https://openairdocs.org/model/piper-pa46r-350t): 101 aircraft (registry code 7104610) - [Piper PA-46-701TP](https://openairdocs.org/model/piper-pa-46-701tp): 95 aircraft (registry codes 7107573, 7105752) - [New Piper PA-46-500TP](https://openairdocs.org/model/new-piper-pa-46-500tp): 36 aircraft (registry code 7104606) - [New Piper PA46-350P](https://openairdocs.org/model/new-piper-pa46-350p): 9 aircraft (registry code 7104607) - [New Piper PA-46-350P](https://openairdocs.org/model/new-piper-pa-46-350p): 7 aircraft (registry code 7104608) - [New Piper PA-46-310P](https://openairdocs.org/model/new-piper-pa-46-310p): 1 aircraft (registry codes 7104612, 7104603) - [Piper/Hov-Aire PA 46-350P](https://openairdocs.org/model/piper-hov-aire-pa-46-350p): 0 aircraft (registry code 7104602) ## STCs approved under this data sheet (227, first 50) - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA12506NY](https://openairdocs.org/stc/SA12506NY): Installation of de-ice heaters (also known as horizontal tail heaters) and associated parts on the left hand and right hand of the horizontal stabilizer. Sterling Helicopter - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc. - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA12438IB](https://openairdocs.org/stc/SA12438IB): MT-Propeller Entwicklung MTV-37-1-E-C-F-R(P)/CFR205-353( ). MT-Propeller Entwicklung GmbH - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes.. Concorde Battery Corporation - [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc. - [STC SA02017WI](https://openairdocs.org/stc/SA02017WI): The Installation of the Parker-Meggitt iPRESS™ System. 3S Certification LLC - [STC SA12017SE](https://openairdocs.org/stc/SA12017SE): Installation of improved Static Ports. Aero Mech Incorporated - [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc. - [STC SA04188NY](https://openairdocs.org/stc/SA04188NY): Installation of LAI CoolView Windshields and Windows. Lee Aerospace Inc. - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA11893IB](https://openairdocs.org/stc/SA11893IB): Installation of the Pratt & Whitney PT6A-135A engine. MT-Propeller Entwicklung GmbH - [STC SA01843CH](https://openairdocs.org/stc/SA01843CH): Replacement of certain Goodrich pneumatic deicer boots.. SMR Aquisition LLC dba SMR Technologies Inc. - [STC SA04734NY](https://openairdocs.org/stc/SA04734NY): Installation of LAI LH Heated Windshield. Lee Aerospace Inc. - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft.. Michelin North America Inc. - [STC SA03825AT-D](https://openairdocs.org/stc/SA03825AT-D): Installation of a Forward Vision EVS-100 and EVS-600 Infrared Camera System in the Piper PA-46-310P, PA-46-350P and PA-46-350T Models. Summit Aviation Inc. - [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC - [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC - [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics - [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp. - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Genesys Aerosystems Inc. - [STC SA01705WI](https://openairdocs.org/stc/SA01705WI): Installation of the Garmin G950 Integrated Flight Deck Installation. Aeronautix LLC - [STC SA01834WI](https://openairdocs.org/stc/SA01834WI): Installation of a modified Climate Control System. Cutter Aviation Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King) - [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King) - [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA04181NY](https://openairdocs.org/stc/SA04181NY): Installation of the KFC 230 Aerocruze Automatic Flight Control System. Honeywell International Inc - [STC SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA01050DE](https://openairdocs.org/stc/SA01050DE): Installation of aircraft main battery replacement. Concorde Battery Corporation - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA01006WI-D](https://openairdocs.org/stc/SA01006WI-D): Installation of Bendix/King KMD 850 Multi-Function Display System and the optional Bendix/King KMH 980/KMH 880 Multi-Hazard Awareness Systems/KTA 870 Traffic Awareness System/KTA 970 Traffic Alert and Collision Avoidance System and KDR 510 VHF Datalink System.. Honeywell International Inc All 227: https://openairdocs.org/tcds/A25SO/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.