TCDS E4EA

* PAGE 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 REV. 30 28 28 28 29 29 28 28 28 29 28 29 29 28 29 29 29 29 28 29 29 29 30 29 29 29 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" NOT APPLICABLE NOTE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E4EA TCDS NUMBER E4EA REVISION: 30 DATE: June 16, 2021 PRATT & WHITNEY CANADA CORP. MODELS: PT6A-6 PT6A-6A PT6A-6B PT6A-6/C20 PT6A-11 PT6A-11AG PT6A-15AG PT6A-20 PT6A-20A PT6A-20B PT6A-21 PT6A-25 PT6A-25A PT6A-25C PT6A-27 PT6A-28 PT6A-29 PT6A-34 PT6A-34B PT6A-34AG PT6A-35 PT6A-36 PT6A-38 PT6A-41 PT6A-41AG PT6A-42 PT6A-42A PT6A-45 PT6A-45A PT6A-45B PT6A-45R PT6A-50 PT6A-52 PT6A-60A PT6A-60AG PT6A-61 PT6A-65B PT6A-65R PT6A-65AR PT6A-65AG PT6A-65SC PT6A-110 PT6A-112 PT6A-114 PT6A-114A PT6A-116 PT6A-121 PT6A-135 PT6A-135A PT6A-140 PT6A-140A PT6A-140AG PT6B-9 PT6D-114A Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E4EA) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations, provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. TYPE CERTIFICATE (TC) HOLDER: Pratt & Whitney Canada Corp. 1000 Marie-Victorin Longueuil, Quebec, Canada J4G 1A1 TYPE I Free turbine turbo-prop / 3 axial plus one centrifugal stage compressor / single annular combustion chamber, single-stage gas generator turbine / single-stage power turbine MODELS PT6A-6, -6A, -6B, -6/C20, -11, -11AG, -15AG, -20, -20A -20B, -21, -25, -25A, -25C, -27, -28, -29, -34, -34B, -34AG, -35, -36, -110, -112, -114, -114A, -116, -121, -135, -135A, -140, -140A, -140AG, PT6D-114A TYPE II Free turbine turbo-prop / 3 axial plus one centrifugal stage comp / single annular combustion chamber / single stage gas generator turbine / two stage power turbine MODELS PT6A-38, -41, -41AG, -42, -42A, -45, -45A, -45B, -45R, -50, -52, -60A, -60AG, -61 TYPE III Free turbine turbo-prop / 4 axial plus one centrifugal stage comp / single annular combustion chamber / single stage gas generator turbine / two stage power turbine MODELS PT6A-65B, -65R, -65AR, -65AG, -65SC TYPE IV Free turbine turboshaft 3 axial plus one centrifugal stage comp / single annular combustion chamber / single stage gas generator turbine / single stage power turbine MODELS PT6B-9 TCDS E4EA PAGE 2 I. MODELS PT6A-6 PT6A-6A PT6A-6B PT6A-11, -11AG PT6A-20, -20A, - 20B,-6/C20 RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp. Output rpm (max) 525 500 62 2,200 38,100 578 550 70 2,200 38,100 - - - - - - - - - - - - - - - - - - - - 500 2,100 - - - - - - - - - - - - - - - - - - - - - - - - 528(580,11AG) 500(550,-11AG) 70(75,-11AG) - - - - 528(580,-11AG) 500(550,-11AG) - -(75, 11AG) - - - - 475 - - 579 550 72 - - - - 579 550 72 - - - - 500 - - I. MODELS (Cont.) PT6A-21,- 25, -25A PT6A-25C PT6A-15AG, -27, -28 PT6A-29 PT6A-34,-34AG, - 34B, -36 RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp Output rpm (max) 580 550 75 2,200 38,100 580 550 75 2,200 38,100 500 2,100 783 750 82 - - - - 783 750 82 - - - - 720 - - 715 680 90 - - - - 715 680 90 - - - - 620 - - 778 750 71 - - - - 778 750 71 - - - - 750 - - 783 - - 82 - - - - 783 - - 82 - - - - 720 - - TCDS E4EA PAGE 3 I. MODELS (Cont.) PT6A-35 PT6A-110 PT6A-112 PT6A-114 PT6A-114A RATINGS Maximum continuous at sea level Equivalent shaft hp Shaft hp Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp. Output rpm (max) 787 750 93 2,190 38,100 787 750 93 2,190 38,100 720 2,100 502 475 68 1,900 - - 502 475 68 1,900 - - 455 1,825 528 500 70 - - - - 528 500 70 - - - - 475 - - 632 600 79 - - - - 632 600 79 - - - - 600 - - 725 675 124 - - - - 725 675 124 - - - - 675 - - I. MODELS (Cont.) PT6A-116 PT6A-121 PT6A-135,- 135A PT6D-114A PT6A-140 RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp. Output rpm (max) 736 700 89 1,900 38,100 736 700 89 1,900 38,100 672 1,825 647 615 80 - - - - 647 615 80 - - - - 591 - - 787 750 93 - - - - 787 750 93 - - - - 720 - - 729 680 124 6,188 38,100 729 680 124 6,188 - - 680 5,940 912 867 119 1900 38,850 912 867 119 1900 38850 867 1825 TCDS E4EA PAGE 4 I. MODELS (Cont.) PT6A-140AG PT6A-140A RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp. Output rpm (max) 911 867 117 1900 38850 911 867 117 1900 38850 867 1825 945 900 113 - - - - 945 900 113 - - - - 900 - - II. MODELS (Cont.) PT6A-38 PT6A-41, -41AG, -42 -42A PT6A-45 PT6A-45A, -45B RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp. Output rpm (max) 801 750 127 2,000 38,100 801 750 127 2,000 38,100 700 1,900 903 850 134 - - 38,100 903 850 134 - - 38,100 800 - - 1,070 1,020 127 1,700 - - 1,174 1,120 136 1,700 - - 900 1,650 - - - - - - - - 39,000 1,229 1,173 - - 140(-45B) - - 39,000 - - - - TCDS E4EA PAGE 5 II. MODELS (Cont.) PT6A-45R PT6A-50 PT6A-52 PT6A-60A PT6A-60AG PT6A-61 RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp. Output rpm (max) 1,070 1,020 127 1,700 39,000 1,254 1,197 141 1,700 39,000 900 1,650 1,022 973 124 1,210 38,100 1,174 1,120 136 1,210 38,500 1,120 1,210 898 850 120 2000 39,000 898 850 120 2000 39,000 800 1900 1,113 1,050 157 1,700 - - 1,113 1,050 157 1,700 - - 900 1,650 1,081 1,020 154 - - - - - - - - - - - - - - - - - - 902 850 132 2,000 - - 902 850 132 2,000 - - 800 1,900 III. MODELS PT6A-65B PT6A-65R PT6A-65AR PT6A-65AG PT6A-65SC RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Alternative takeoff (5 min. at sea level) Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Maximum reverse Shaft hp. Output rpm (max) 1,249 1,173 189 1,700 39,000 1,249 1,173 189 1,700 39,000 --- --- --- --- --- 900 1,650 - - - - - - - - - - 1,459 1,376 209 - - - - 1,308 1,230 195 1,700 39,000 - - - - 1,298 1,220 194 - - - - 1,509 1,424 214 - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1,381 1,300 202 - - - - --- --- --- --- --- - - - - 1167 1110 143 - - - - 1167 1110 143 - - - - --- --- --- --- --- - - - - TCDS E4EA PAGE 6 IV. MODELS (Cont.) PT6B-9 RATINGS Maximum continuous at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm Takeoff (5 min.) at sea level Equivalent shaft hp. Shaft hp. Jet thrust, lb. Output rpm Gas generator rpm --- 500 124 6,230 38,100 --- 550 136 6,230 38,100 COMPONENTS/ CONFIGURATION Includes basic engine, fuel and ignition systems but excludes propeller governor (-6, -20 and PT6D-114A models only) and ignition power source. FUEL Fuels conforming to the current P&WC specification CPW 204, CPW46 and CPW381 (for AG engines). Refer to the current revision of Service Bulletins or Maintenance manuals as follows for approved fuel types: SB 1244 - PT6A-6, 6A, 6B, 6/C20, 20, 20A, 20B, 21, 27, 28, 34, 34B, 36, 114, 114A, 116, 135, 135A, 35, 25, 25A, 25C SB 12044 - PT6A-110, 112, 121, 11 SB 12144 - PT6A-15AG, 11AG SB 1344 - PT6A-34AG SB 1604 - PT6D-114A SB 3044 - PT6A-38, 41, 42, 42A, 45A, 45B, 45R SB 13044 - PT6A-52, 60A, 61, 65B, 65R, 65AR SB 13244 - PT6A-60AG, 65AG SB 4044 - PT6A-50 Maintenance Manual 3075742 PT6A-140 Maintenance Manual 3079582 PT6A-140AG Maintenance Manual 3077182 PT6A-140A Maintenance Manual 3135622 PT6A-65SC Emergency use of MIL-G-5572, Grades 80/07, 91/98, 100/130 and 115/145 is permitted for a total time period not exceeding 150 hours during any overhaul period. It is not necessary to purge the unused fuel from the system when switching fuel type LUBRICATING OILS The following oils are eligible for these engines: Refer to the current revision of Service Bulletins or Maintenance manuals as follows for approved fuel types: SB 1001 - PT6A-6, 6A, 6B, 6/C20, 20, 20A, 20B, 21, 27, 28, 34, 34AG, 34B, 36, 114, 114A, 116, 135, 135A, 35, 25, 25A, 25C SB 12001 - PT6A-11, 11AG, 15AG, 110, 112, 121 SB 1601 - PT6D-114A SB 3001 - PT6A-38, 41, 42, 42A, 45A, 45B, 45R SB 13001 - PT6A-52, 60A, 60AG, 61, 65AG, 65B, 65R, 65AR SB 4001 - PT6A-50 Maintenance Manual 3075742 PT6A-140 Maintenance Manual 3079582 PT6A-140AG Maintenance Manual 3077182 PT6A-140A Maintenance Manual 3135622 PT6A-65SC TCDS E4EA PAGE 7 PRINCIPLE DIMENSIONS AND WEIGHT I. MODELS PT6A-6 PT6A-6A PT6A-6B PT6A-11, -11AG PT6A-20, -20A, -20B,-6/C20 PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius (excluding exhaust ports) 61.89 18.29 10.85 - - - - - - - - - - - - - - - - 11.50 - - - - -10.85 WEIGHT (DRY) 280 284 - - 339 340(-11AG) 286(20, 6/C20) 289(20A, 20B) CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline 4.20 --- 0.34 0.32 4.40 --- - - - - - - --- - - - - 3.18 --- 0.26 0.36 4.14(20, 6/C20 4.58(20A, 20B) --- 0.45 0.07(20, 6/C20) 0.08(20A, 20B) REDUCTION GEAR RATIO .0668:1 - - - - - - - - I. MODELS (Continued) PT6A-21, -25, -25A PT6A-25C PT6A-15AG, -27, -28 PT6A-29 PT6A-34, -34AG, -34B,-36 PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius (excluding exhaust ports) 61.89((62.91,- 25,-25A) 18.29(23.00, - 25, -25A) 10.85(16.00, - 25, -25A) 62.91 23.00 16.00 61.89 18.29 11.50 - - - - - - - - - - - - WEIGHT (DRY) 337 (-21) 362 (-25) 352 (-25A) 355 337 - - 340 (353 -34B) CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline 3.04(-21) 3.00(-25, -25A) --- 0.32(-21) 0.47(-25, -25A) 0.20(-21) 0.29(-25, -25A) 3.00 --- 0.47 0.29 3.04 --- 0.32 0.20 - - --- - - - - - -(3.38 -34B) --- - -(0.37 -34B) - -(0.38 -34B) REDUCTION GEAR RATIO .0668:1 .0663:1 - - - - - - TCDS E4EA PAGE 8 I. MODELS (Continued) PT6A-110 PT6A-112 PT6A-114 PT6A-114A PT6A-116 PRINCIPAL DIMENSIONS, in. Length, in. Nominal diameter Maximum radius (excluding exhaust ports) 61.89 18.29 11.50 - - - - - - 61.89 18.29 11.73 - - 18.06 11.50 WEIGHT (DRY) 343 - - 359 360 348 CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline 3.80 --- 0.26 0.34 - - --- - - - - 3.88 --- - - 0.38 - - - - - - - - 3.87 --- 0.25 0.35 REDUCTION GEAR RATIO 0.0576:1 - - - - - - - - I. MODELS (Continued) PT6A-121 PT6A-135, -135A PT6D-114A PT6A-35 PT6A-140 PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius (excluding exhaust ports) 61.89 18.29 11.50 - - - - - - 52.8 18.29 11.73 61.89 - - - - 64.14 18.92 14.32 WEIGHT (DRY) 343 347 297 334 416.7 CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline 3.8 --- 0.26 0.34 3.87 --- 0.25 0.35 0.19 --- 0.31 0.25 3.87 --- 0.25 0.35 4.27 --- 0.47 0.36 REDUCTION GEAR RATIO 0.0576:1 - - 0.1875 0.0663:1 0.0582:1 TCDS E4EA PAGE 9 I. MODELS (Continued) PT6A-140AG PT6A-140A PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius (excluding exhaust ports) 64.14 18.62 11.40 - - - - - - WEIGHT (DRY) 385 - - CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline 4.47 0.33 0.26 - - - - - - REDUCTION GEAR RATIO 0.0582:1 - - II. MODELS (Continued) PT6A-38 PT6A-41, -41AG, -42 -42A PT6A-45 PT6A-45A, -45B PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius (excluding exhaust ports) 66.47 18.29 12.84 - - - - - - 72.62 - - - - - - - - - - WEIGHT (DRY) 405 419 445 - - CENTER OF GRAVITY (dry weight)(in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline 2.49 --- 0.32 0.19 - - --- - - - - 5.38 --- 0.12 0.27 5.38 --- 0.12 0.27 REDUCTION GEAR RATIO 0.0663:1 - - 0.0568:1 - - TCDS E4EA PAGE 10 II. MODELS (Continued) PT6A- 45R PT6A-50 PT6A-60A PT6A-61 PT6A- 60AG PT6A-52 PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius (excluding exhaust ports) 72.62 18.29 12.84 79.89 - - 15.44 72.09 18.29 12.84 66.76 - - - - 72.09 - - - - 66.76 - - - - WEIGHT (DRY) 459 622 487 443 489 449 CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline 5.38 --- 0.12 0.27 --- See NOTE See NOTE See NOTE 5.22 --- .300 .28 2.630 --- - - .29 5.22 --- - - .28 2.51 --- .260 .330 REDUCTION GEAR RATIO 0.0568:1 0.0438:1 0.0568:1 0.0663:1 0.0568:1 0.0663:1 NOTE: For PT6A-50 C.G. location (dry weight) is 27.69 in. behind forward mounting ring, 0.27 in. below horizontal centerline and 0.15 in. left of vertical centerline. III. MODELS PT6A-65B PT6A-65R PT6A-65AR PT6A-65AG PT6A-65SC PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius 74.79 18.29 12.84 - - - - - - - - - - - - - - - - - - 73.64 18.77 15.08 WEIGHT (DRY) 495 496 501 - - 517 CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline 3.75 --- 0.29 .17 - - --- - - - - - - --- - - - - - - --- - - - - 3.5 --- .31 .24 REDUCTION GEAR RATIO 0.0568:1 - - - - - - - - IV. MODELS PT6B-9 PRINCIPAL DIMENSIONS, in. Length Nominal diameter Maximum radius (excluding exhaust ports) 58.68 18.06 10.85 WEIGHT (DRY) 255 CENTER OF GRAVITY (dry weight) (in.) Forward of mount plane Aft of forward mount plane Below engine centerline Right of engine centerline --- 22.08 0.13 0.52 REDUCTION GEAR RATIO 0.1889:1 TCDS E4EA PAGE 11 CERTIFICATION BASIS Applicable to the following engines and serial numbers: FAR 21.29, CAR 13. (Except Serial numbers shown below which were certified under FAR 21.21, FAR Part 33 and amendments 33-1 to 33-5 see NOTE below. MODEL SERIAL NUMBER APPLICATION ISSUED/REVISED WITHDRAWN PT6A-6 PT6A-6A PT6A-6B PT6B-9 PT6A-11 PT6A-11AG PT6A-15AG PT6A-20 PT6A-20A PT6A-20B PT6A-6/C20 PT6A-21 PT6A-25 PT6A-25A PT6A-25C PT6A-27 PT6A-28 PT6A-29 PT6A-34 PT6A-34B PT6A-34AG PT6A-35 PT6B-35F PT6A-36 All All All All All All All All All except 024103-024160 All All All All except 058013-058018 058025-058040 058042-058047 058049-058055 058059-058064 058068-058073 058077-058084 058089-058204 All All All except 044878-040879 040883-040884 040894-040895 040899-040921 040929-040934 040937-040943 040946-040949 040982-040988 040993-040999 041006-041007 041015-041021 041027-041032 041036 041041-041044 041050-041053 041060-041063 041067-041098 041105-041110 041113-041146 041152-041156 041162-041175 041180-041194 041199-041201 All except 050676-050925 050928-050934 All All except 056071-056075 056080-056081 056086-056090 056098-056107 054011, 054012 only prior to 054007 All All All All June 4, 1962 April 6, 1965 November 30, 1967 June 4, 1962 August 19, 1977 January 10, 1979 January 9, 1978 April 9, 1965 February 19, 1973 August 20, 1973 February 19, 1973 December 2, 1974 May 5, 1976 December 13, 1976 March 5, 1990 November 15, 1966 January 27, 1969 October 6, 1967 April 29, 1971 July 20, 1976 February 3, 1977 October 24, 2001 August 10, 1979 December 13, 1973 December 31, 1963 May 28, 1965 December 20, 1967 May 28, 1965 September 16, 1977 May 17, 1979 January 27, 1978 October 29, 1965 March 9, 1973 October 2, 1973 March 9, 1973 December 10, 1974 May 6, 1976 December 28, 1976 June 8, 1990 December 20, 1967 March 11, 1969 October 28, 1968 November 11, 1971 August 4, 1976 February 14, 1977 May 29, 2002 March 26, 1982 December 13, 1973 July 17, 2020 TCDS E4EA PAGE 12 PT6A-38 PT6A-40 PT6A-41 PT6A-41AG PT6A-42 PT6A-42A PT6A-45 PT6A-45A PT6A-45B PT6A-45 PT6A-50 PT6A-60 PT6A-60A PT6A-60AG PT6A-61 PT6A-61A PT6A-65B PT6A-65R PT6A-65AR PT6A-65AG PT6A-110 PT6A-112 PT6A-114 PT6A-114A PT6A-116 PT6A-121 PT6A-135 PT6A-135A PT6D-114A PT6A-52 PT6A-65SC 079156, 079157 only prior to 079153 All All All All All All All All All All All All All All All All All All All All All All All All All All All All All All May 12, 1975 April 19, 1983 August 30, 1973 December 21, 1978 July 11, 1979 September 21, 1998 May 12, 1975 March 25, 1976 March 2, 1979 June 25, 1980 September 21, 1976 April 20, 1982 April 19, 1983 October 1, 1996 April 20, 1982 January 6, 1984 April 20, 1982 April 20, 1982 January 6, 1984 July 23, 1987 August 8, 1980 October 12, 1978 December 21, 1982 October 4, 1989 October 4, 1984 April 12, 1982 September 9, 1977 February 3, 1982 October 30, 1996 May 26, 2006 January 27, 2020 May 30, 1975 July 13, 1983 October 2, 1973 May 17, 1979 October 12, 1979 December 4, 1998 May 30, 1975 April 22, 1976 March 29, 1979 August 1, 1980 October 22, 1976 March 15, 1983 November 7, 1983 October 10, 1996 March 15, 1983 May 1, 1985 September 17, 1982 September 17, 1982 May 1, 1985 August 19, 1987 February 15, 1981 October 30, 1978 May 21, 1984 March 19, 1990 May 1, 1985 August 3, 1982 September 12, 1977 April 29, 1982 September 22, 1997 May 31, 2007 April 12, 2021 July 17, 2020 July 17, 2020 July 17, 2020 The PT6A-65SC model complies with 14 CFR Part 34, Amendment 5A, effective October 23, 2013. See Note 11 for detailed summary of the certification basis for fuel venting and exhaust emissions. 14 CFR Part 33, effective February 1, 1965, including Amendments 33-1 through 33-20. The following models comply with 14 CFR Part 34, Amendment 5A, effective October 23, 2013. See Note 11 for detailed summary of the certification basis for fuel venting and exhaust emissions. MODEL S/N DATE OF APPLICATION DATE OF TYPE CERTIFICATE NO. E4EA ISSUED/REVISED PT6A-140 ALL March 9, 2011 December 17, 2012 PT6A-140AG ALL May 15, 2014 October 1, 2015 PT6A-140A ALL May 15, 2014 October 1, 2015 NOTE: This Type Certificate Data Sheet reflects the certification basis and approval for those serial numbered model PT6A, PT6B and PT6D series engines listed under "Certification Basis". Two Type Certificates have been issued for administrative purposes: E4EA under FAR 21.29 for engines produced in Canada and E2NE under FAR 21.21 for engines produced in the United States. The type design for each model engine, regardless of where produced, is identical. The information on this Type Certificate Data Sheet applies to all Pratt & Whitney model PT6A, PT6B and PT6D series engines, including: (A) Those serial numbered engines listed on and certificated under FAA Type Certificate E2NE, originally issued to Pratt & Whitney Aircraft Division of United Technologies Corporation, East Hartford, Connecticut, U.S.A. and reissued to Pratt & Whitney of Canada Ltd. (Formerly United Aircraft of Canada, Ltd.), Longueuil, Quebec, Canada. (B) Those serial numbered engines listed above under "Certification Basis," certificated under this Type Certificate, E4EA, issued to Pratt & Whitney Canada Corp, Longueuil, Quebec, Canada. TCDS E4EA PAGE 13 NOTES NOTE 1. ENGINE RATINGS: The engine ratings are based on static sea level condition 29.92 in Hg pressure, compressor intake screen installed, no external accessory loads and no airbleed. These ratings are available up to the following compressor inlet air (dry) temperatures. Maximum Continuous Takeoff Maximum Continuous Takeoff PT6A-6, -6A, -6B 64oF 70oF PT6A-60AG 63oF 79oF PT6A-20, -20A, -20B,-6/C20 70 70 PT6A-61 115 115 PT6A-11 108 108 PT6A-65B 101 110 PT6A-11AG 90 90 PT6A-65R 101 82, 76(1) PT6A-21 91 91 PT6A-65AR 101 82, 84(1) PT6A-25,-25A 93 93 PT6A-65AG 101 71 PT6A-25C 87 87 PT6A-65SC 131 131 PT6A-15AG, -27 71 71 PT6A-110 101 101 PT6A-28 70 70 PT6A-112 133 133 PT6A-29 73 73 PT6A-114 136 136 PT6A-34, -34B,-34AG 86 86 PT6A-114A 115 115 PT6A-35,-135A 93 93 PT6A-116 105 105 PT6A-36 97 97 PT6A-121 104 104 PT6A-38 102 102 PT6A-135 85 85 PT6A-41, -41AG, -42 106 106 PT6A-140 80 102 PT6A-42A 106 106 PT6A-140A 87.8 98.6 PT6A-45 79 59 PT6A-140AG 78.8 111.2 PT6A-45A 79 46