# TCDS E42NE: Pratt & Whitney Canada Corp. - Type: Type certificate data sheet - Status: Current - Holder: Pratt & Whitney Canada Corp. - Revision: 10 - Revised: November 7, 2014 - Product: Engine - Certification basis: Part 21, Part 33, Part 34 - Registered aircraft: 397, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/e4/b2/e4b26538c47645cd31d56563fa062f0f395f8455bf15ef0d8d52f962c86209ac - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/42E96DAA83683B2186257D8C0065762B.0001 - Page: https://openairdocs.org/tcds/E42NE ## Models (11) As the data sheet lists them. - PW207D1 - PW207D - PW207E - PW207D2 - PW206B2 - PW207C - PW206C - PW206A - PW206B - PW206E - PW206B3 ## 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 1 2 3 4 5 6 7 8 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" REV. 10 10 10 10 10 10 10 10 "---" NOT APPLICABLE NOTICE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E42NE TCDS NUMBER E42NE REVISION: 10 DATE: November 7, 2014 PRATT & WHITNEY CANADA MODELS: PW206A PW206E PW207D1 PW206B PW207C PW207D2 PW206B2 PW207D PW206B3 PW206C PW207E Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E42NE) 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. (Formerly: Pratt & Whitney Canada Inc.) 1000 Marie-Victorin Longueuil, Quebec Canada J4G 1A1 I. MODELS PW206A PW206B PW206C PW206E PW207C PW207D PW207E PW206B2 TYPE Twin-spool free turbine turboshaft engine incorporating a single stage centrifugal compressor, reverse flow annular combustor, and a single stage shrouded power turbine. RATINGS SHAFT HORSEPOWER / SEE NOTE 4 30 sec. OEI --- --- --- --- - - - 676 --- 734 2 min. OEI --- --- --- --- - - - 676 --- 716 30 min. OEI --- --- --- --- - - - 572 --- --- 2 1/2 min. OEI 676 573 653 682 745 --- 728 --- Continuous OEI 621 493 633 646 - - 572 646 542 Take-off (5 min) 621 431 561 646 572 - - 646 447 Max. Continuous 550 431 561 572 - - -- - - 431 I. MODELS (cont.) PW207D1 PW207D2 PW206B3 TYPE Twin-spool free turbine turboshaft engine incorporating a single stage centrifugal compressor, reverse flow annular combustor, and a single stage shrouded power turbine. RATINGS SHAFT HORSEPOWER / SEE NOTE 4 30 sec. OEI 758 758 734 2 min. OEI 730 730 716 30 min. OEI 689 689 --- 2 1/2 min. OEI --- --- --- Continuous OEI 681 681 542 Take-off (5 min) 621 621 451 Max. Continuous 610 610 435 TCDS E42NE Page 2 of 8 FUEL TYPE Fuel conforming to the current PWC Specification No. CPW 204 and later revisions. For further details refer to the applicable Maintenance Manual for each model (reference NOTE 13 for Maintenance Manual part number). OIL TYPE Synthetic type conforming to the current PWA Specification Number PWA 521 Type II. For approved brands refer to the applicable Maintenance Manual for each model (reference NOTE 13 for Maintenance Manual part number). EQUIPMENT/ COMPONENTS Fuel metering unit including fuel pump, engine electronic control unit, fuel control alternator and ignition system without power source, are included as standard equipment as per the approved Parts List. Required equipment also includes a chip detector, or other metallic debris-detecting device. For additional information, refer to Installation Manual and Illustrated Parts Catalogue. For output and accessory drive specifications, principal dimensions, weight and center of gravity location, refer to Installation Manual. CERTIFICATION BASIS For PW206A, FAR Part 33 effective February 1, 1965, and amendments 33-1 to 33-12, inclusive and Additional Airworthiness Requirement 533.101* (FAR 33.28 at amendment 33-15). For PW206B, PW206C, and PW206E, FAR Part 33 effective February 1, 1965, amendments 33-1 to 33-14, inclusive and Additional Airworthiness Requirement 533.101* (FAR 33.28 at amendment 33-15). For PW206B2,PW207D, PW207C and PW207E, FAR Part 33 effective February 1, 1965, amendments 33-1 to 33-14 inclusive, Additional Airworthiness Requirement 533.101* (FAR 33.28 at amendment 15), and amendment 33-18 for 30 second/2minute OEI ratings (33.7, 33.29, 33.67, 33.85, 33.88, 33.93). For PW207D1 & D2, FAR Part 33 effective February 1, 1965, amendments 33-1 to 33-14 inclusive, Additional Airworthiness Requirement 533.101* (FAR 33.28 at amendment 33-15), FAR Part 33.83 at amendment 33-17, plus amendment 33-18 for 30 second/2minute OEI ratings (33.7, 33.29, 33.67, 33.85, 33.88, 33.93). For PW206B3, 14 CFR part 33 effective February 1, 1965, amendments 33-1 to 33-14 inclusive, § 33.28 at amendment 33-15 (Canada’s Special Condition 2013-16), § 33.83 at amendment 33-17, and §§ 33.7, 33.29, 33.67, 33.85, 33.87, 33.88, 33.93 at amendment 33- 18 for 30-second/2-minute OEI ratings. P&WC has elected to comply with 14 CFR part 34, amendment 5, effective December 31, 2012. See note 20 for a detailed summary of the certification basis for fuel venting emissions for PW206B3. * Additional Airworthiness Requirement 533.101 “Electronic Engine Control Systems”, predates the FAA final rule FAR 33.28 at ammendmet 33-15 to address the approval of engines with Electronic Engine Control in Canada. Type Certificate E42NE MODEL APPLICATION DATE ISSUED/REVISED PW206A APRIL 15, 1991 MAY 24, 1993 PW206B DECEMBER 8, 1995 APRIL 23, 1996 PW206C APRIL 10, 1995 APRIL 23, 1996 PW206E JULY 25, 1996 SEPT. 15, 1997 PW207D MAY 28, 1998 FEB. 19, 1999 PW207E OCTOBER 21, 1999 APRIL 10, 2000 PW206B2 FEBRUARY 8, 2000 APRIL 29, 2002 PW207C JULY 20, 1999 SEPTEMBER 16, 2005 PW207D1 MAY 29, 2007 APRIL 10, 2009 PW207D2 MAY 29, 2007 APRIL 10, 2009 PW206B3 MARCH 13, 2013 NOVEMBER 7, 2014 TCDS E42NE Page 3 of 8 IMPORT REQUIREMENTS To be considered eligible for installation on U.S. - registered aircraft, each engine to be exported to the United States shall be accompanied by a certificate of airworthiness for export or certifying statement endorsed by the exporting cognizant civil airworthiness authority and containing the following language: (1) This engine conforms to its United States type design (Type Certificate Number E42NE) and is in a condition for safe operation. (2) This engine has been subjected by the manufacturer to a final operational check and is in a proper state of airworthiness. Reference FAR Section 21.500, which provides for the airworthiness acceptance of aircraft engines or propellers manufactured outside of the U.S. and for which a U.S. type certificate has been issued. Additional guidance is contained in FAA Advisory Circular 21-23, Airworthiness Certification of Civil Aircraft, Engines, Propellers and Related Products, Imported into the United States. NOTES I. MODELS PW206A PW206B PW206C PW206E PW207C PW207D PW207E PW206B2 NOTE 1.. ENGINE ROTOR SPEED LIMITS (RPM) Gas Generator Speed Maximum 30 sec OEI --- --- --- --- - - - 60,500 --- 60,500 2 min OEI --- --- --- --- - - - 59,300 --- 59,500 30 min OEI --- --- --- --- - - - 58,700 --- --- 2 1/2 min OEI 58,600 59,400 - - - - 59,750 --- 59,750 --- Continuous OEI 57,250 58,250 - - - - 57,900 - - - - 58,250 Take-off (5 min) 57,250 57,250 - - - - 57,900 - - - - - - Maximum Continuous 57,250 56,500 - - - - 56,400 - - - - 56,500 Transient (20 sec) 59,772 59,994 - - - - 60,348 * 60,348 * Starting (2 sec. max.) --- --- --- --- - - - --- --- --- (100% = 57,000) I. MODELS (cont.) PW207D1 PW207D2 PW206B3 NOTE 1. ENGINE ROTOR SPEED LIMITS (RPM) Gas Generator Speed Maximum 30 sec OEI 60,500 60,500 60,500 2 min OEI 59,300 59,300 59,500 30 min OEI 58,700 58,700 --- 2 1/2 min OEI --- --- --- Continuous OEI 57,900 57,900 57,900 Take-off (5 min) 57,900 57,900 57,900 Maximum Continuous 56,400 56,400 56,500 Transient (20 sec) * * * Starting (2 sec. max.) --- --- --- (100% = 57,000) TCDS E42NE Page 4 of 8 I. MODELS PW206A PW206B PW206C PW206E PW207C PW207D PW207E PW206B2 POWER TURBINE SPEED MAXIMUM 30 sec OEI --- --- --- --- - - - 41,606 --- 40,891 2 min OEI --- --- --- --- - - - 41,606 --- 40,891 30 min OEI --- --- --- --- - - - 41,606 --- --- 2 1/2 min OEI 41,606 40,891 40,806 41,606 40,806 --- 41,606 --- Continuous OEI 41,606 40,891 40,806 41,606 40,806 41,606 - - 40,891 Take-off (5 min) 41,606 40,891 40,806 41,606 40,806 41,606 - - 40,891 Maximum Continuous 41,606 40,891 40,806 41,606 40,806 41,606 - - 40,891 Transient (20 sec) 44,726 - - - - - - - - * 44,726 * Starting (2 sec. max.) --- --- --- --- - - - --- --- --- (100% =39,807 all except PW206B/B2/B3, 100%=39,123 for PW206B/B2/B3) I. MODELS (cont.) PW207D1 PW207D2 PW206B3 POWER TURBINE SPEED MAXIMUM 30 sec OEI 41,606 41,606 40,891 2 min OEI 41,606 41,606 40,891 30 min OEI 41,606 41,606 --- 2 1/2 min OEI --- --- --- Continuous OEI 41,606 41,606 40,891 Take-off (5 min) 41,606 41,606 41,282 Maximum Continuous 41,606 41,606 41,282 Transient (20 sec) * * * Starting (2 sec. max.) --- --- --- (100% =39,807 all except PW206B/B2/B3, 100%=39,123 for PW206B/B2/B3) I. MODELS PW206A PW206B PW206C PW206E PW207C PW207D PW207E PW206B2 OUTPUT SHAFT SPEED MAXIMUM 30 sec OEI --- --- --- --- - - - 6,271 --- 6,165 2 min OEI --- --- --- --- - - - 6,271 --- 6,165 30 min OEI --- --- --- --- - - - 6,721 --- --- 2 1/2 min OEI 6,271 6165 6151 6,271 6,151 --- 6271 --- Continuous OEI 6,271 6165 6151 6,271 6,151 6,271 - - 6,165 Take-off (5 min) 6,271 6165 6151 6,271 6,151 6,271 - - 6,165 Maximum Continuous 6,271 6165 6151 6,271 6,151 6,271 - - 6,165 Transient (20 sec) 6,741 - - - - - - 6,151 * 6741 * Starting (2 sec. max.) --- --- --- --- - - - --- --- --- *Refer to Installation Manual TCDS E42NE Page 5 of 8 I. MODELS (cont.) PW207D1 PW207D2 PW206B3 OUTPUT SHAFT SPEED MAXIMUM 30 sec OEI 6,271 6,271 6,165 2 min OEI 6,271 6,271 6,165 30 min OEI 6,271 6,271 --- 2 1/2 min OEI --- --- --- Continuous OEI 6,271 6,271 6,165 Take-off (5 min) 6,271 6,271 6,224 Maximum Continuous 6,271 6,271 6,224 Transient (20 sec) * * --- Starting (2 sec. max.) --- --- --- *Refer to Installation Manual I. MODELS PW206A PW206B PW206C PW206E PW207C PW207D PW207E PW206B2 NOTE 2. ENGINE INTERTURBINE TEMPERATURE LIMITS (C) 30 sec. OEI --- --- --- --- - - - 990 --- 990 2 min OEI --- --- --- --- - - - 950 --- 950 30 min OEI --- --- --- --- - - - 925 --- --- 2 1/2 min OEI 902 930 - - - - 970 --- 970 --- Continuous OEI 863 885 - - - - 900 - - - - - - Take-off (5 min) 863 854 863 - - 900 - - - - - - Maximum Continuous 820 820 - - - - 840 850 - - 835 Transient (20 sec) 960 972 - - - - 1000 * 1,000 * Starting (2 sec. max.) 875 875 - - - - 875 - - - - - - *Refer to Installation Manual I. MODELS(Cont.) PW207D1 PW207D2 PW206B3 NOTE 2. ENGINE INTERTURBINE TEMPERATURE LIMITS (C) 30 sec. OEI 990 990 990 2 min OEI 950 950 950 30 min OEI 925 925 --- 2 1/2 min OEI --- --- --- Continuous OEI 900 900 900 Take-off (5 min) - - - - 900 Maximum Continuous 850 850 835 Transient (20 sec) * * * Starting (2 sec. max.) - - - - 875 *Refer to Installation Manual TCDS E42NE Page 6 of 8 I. MODELS PW206A PW206B PW206C PW206E PW207C PW207D PW207E PW206B2 NOTE 3. MAXIMUM TORQUE LIMITS (FT-LB/N-M) 30 sec OEI --- --- --- --- - - - 569/771 --- 628/852 2 min OEI --- --- --- --- - - - 569/771 --- 613/833 30 min OEI --- --- --- --- - - - 481/652 --- --- 2 1/2 min OEI 569/771 491/665 560/759 574/778 639/866 --- 613/831 --- Continuous OEI 544/737 421/572 544/737 - - 554/751 481/652 544/737 464/629 Take-off (5 min) 544/737 369/500 481/652 544/737 491/666 481/652 544/737 383/519 Maximum Continuous 481/652 369/500 481/652 - - 491/666 481/652 - - 369/500 Transient (20 sec) 725/983 613/831 725/983 - - - - * 635/861 * Starting (2 sec. max.) --- --- --- --- - - - --- --- --- *Refer to Installation Manual I. MODELS (Cont.) PW207D1 PW207D2 PW206B3 NOTE 3. MAXIMUM TORQUE LIMITS (FT-LB/N-M) 30 sec OEI 638/865 638/865 628/851 2 min OEI 614/832 614/832 613/831 30 min OEI 580/786 580/786 --- 2 1/2 min OEI --- --- --- Continuous OEI 573/776 573/776 464/629 Take-off (5 min) 523/709 523/709 383/519 Maximum Continuous 513/695 513/695 369/500 Transient (20 sec) * * * Starting (2 sec. max.) --- --- --- *Refer to Installation Manual NOTE 4. The engine ratings are based on dry sea level static ICAO standard atmospheric conditions, with no external accessory loads and no airbleed. The quoted ratings are obtainable on a test stand with the specified fuel and oil, and with the reference intake and exhaust ducts specified in the Installation Manual. NOTE 5. Reserved. NOTE 6. ENGINE AIRBLEED LIMITS Max. external: 5% of inlet airflow. Max. during start: Nil. NOTE 7. Pressure Temperature Tank Capacity ENGINE OIL PRESSURE/TEMPERATURE LIMITS AND TANK CAPACITY Normal range: Refer to Installation Manual. Normal range: 71-110˚C PW206A & PW206E 71-120˚C, PW206B 71-125°C, PW206C & PW207E 71-128.5°C, PW207C 71-127°C, PW207D, PW207D1, PW207D2 71-129.5°C, PW206B2, B3 Starting Minimum: -45°C Totals: Liters 3.93/U.S. Gallons 1.038 [ PW206A,C,E, PW207C,D,E,D1,D2 Liters 4.525/ US Gallons 1.195 [ PW206B, B2, B3 TCDS E42NE Page 7 of 8 NOTE 8. Inlet Head Temperature Viscosity ENGINE FUEL LIMITS See Installation Manual for required inlet pressures and lift capability. Refer to Installation Manual. Maximum cold starting: 12 centistokes. NOTE 9. The uninstalled engine meets FAA requirements for operating in icing conditions. These engines also meet the requirements of Canadian Airworthiness Manual 533.68 for operation in icing conditions as defined in Canadian Airworthiness Manual 529, Appendix C. The Airframe Manufacturer must give appropriate consideration to installation effects as stated in the Installation Manual. NOTE 10. The software for the Electronic Engine Control (EEC) has been developed and tested in accordance with the provisions of "Flight Critical" category (Level 1) of RTCA/DO178A for the PW206A, PW206B, PW206C, and PW206E and the provisions of Flight Critical category (Level A) of RTCA D0178B for the PW206B2, PW207C, PW207D, PW207D1, PW207D2, PW207E, and PW206B3. NOTE 11. Lightning protection requirements and Electromagnetic Interference (EMI) emitted by the EEC system, including cables, are specified in the Installation Manual, Section 6. NOTE 12. The PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, PW207D1, PW207D2 and PW207E engine models are approved for multiple engine installations only. NOTE 13. APPROVED PUBLICATIONS 1. Transport Canada approved PW206A, PW206B, PW206C, PW206E, PW207C, PW207D, PW207D1, PW207D2, PW207E, PW206B2, and PW206B3 Installation Manuals. 2. Transport Canada approved Parts List for the first production engine. Model Parts List PW206A A3044400 PW206B A3117200 PW206B2 A3053245 PW206C A3120020 PW206E A3044220 PW207C 3053007 Rev K PW207D A3049028 PW207E A3053654 PW207D1 3071805 PW207D2 3073794 PW206B3 3078348 Rev A 3. Transport Canada approved Airworthiness Limitations Section of the following Maintenance Manuals. Maintenance Overhaul Model Manual P/N Manual P/N PW206A/PW206E/PW207E 3038324 3038325 PW206B/PW206B2/PW206B3 3039732 3039733 PW206C 3043322 3043323 PW207C 3043322 3043323 PW207D 3043612 3043613 PW207D1/ PW207D2 3071602 3071603 TCDS E42NE Page 8 of 8 NOTE 14. Prior to issue of Transport Canada accepted overhaul manual, overhauls are not permitted. NOTE 15. Service Bulletins, structural repair manuals, vendor manuals, aircraft flight manuals, and overhaul and maintenance manuals, which contain a statement that the document is Transport Canada approved, are accepted by the FAA and are considered FAA approved. These approvals pertain to the type design only. NOTE 16. The PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, PW207D1, PW207D2, PW207E, PW206B2, and PW206B3 EEC have not been fire tested and therefore, must not be mounted in a designated fire zone. Note 17. PW207D1 is a derivative of the PW207D with increased mechanical power and without fuel heater. The PW207D2 is identical to the PW207D1 but has a fuel heater installed. Note 18. At the 2 min OEI rating, the PW207D EEC limits the torque at 530 lb-ft. Note 19. Delete Note 20. Pratt & Whitney Canada has elected to comply with the following emissions standards promulgated in 14 CFR Part 34, Amendment 5, effective December 31, 2012, and 40 CFR Part 87, effective July 18, 2012, for: PW206B3. Fuel Venting Emission Standards: 14 CFR §§ 34.10(b) and 34.11; in addition, 40 CFR §§ 87.10(b) and 87.11. ----END---- ``` ## ADs (5, in force first) - [AD 2013-03-21](https://openairdocs.org/ad/2013-03-21): Power turbine (PT) disks · Pratt & Whitney Canada PW206B, PW206B2, PW206C and 5 more. Effective Mar 26, 2013 - [AD 2009-03-05](https://openairdocs.org/ad/2009-03-05): Compressor turbine (CT) disc bore · Pratt & Whitney Canada PW206A, PW206B, PW206B2 and 5 more. Effective Mar 27, 2009 - [AD 2004-17-03](https://openairdocs.org/ad/2004-17-03): Compressor turbine and power turbine blades for blade axial shift · Pratt & Whitney Canada PW206A and PW206E. Effective Sep 24, 2004 - [AD 2004-14-22](https://openairdocs.org/ad/2004-14-22): Automatic low-cycle- fatigue (LCF) · Pratt & Whitney Canada PW206B, PW206C, PW206E and 2 more. Effective Aug 3, 2004 - [AD 2003-16-10](https://openairdocs.org/ad/2003-16-10) (historical): Compressor turbine and power turbine blades · Pratt & Whitney Canada PW206A and PW206E. Effective Aug 29, 2003 ## Registered aircraft by registry model (OpenAirDocs) - [Pratt & Whitney Canada PW206B2](https://openairdocs.org/engine/pratt-whitney-canada-pw206b2): 146 aircraft (registry code 52288) - [Pratt & Whitney Canada PW207C](https://openairdocs.org/engine/pratt-whitney-canada-pw207c): 49 aircraft (registry code 52203) - [Pratt & Whitney Canada PW206B series](https://openairdocs.org/engine/pratt-whitney-canada-pw206b-series): 43 aircraft (registry code 52135) - [Pratt & Whitney Canada PW206C](https://openairdocs.org/engine/pratt-whitney-canada-pw206c): 43 aircraft (registry code 52160) - [Pratt & Whitney Canada PW207D](https://openairdocs.org/engine/pratt-whitney-canada-pw207d): 35 aircraft (registry code 52156) - [Pratt & Whitney Canada PW206B3](https://openairdocs.org/engine/pratt-whitney-canada-pw206b3): 29 aircraft (registry code 51948) - [Pratt & Whitney Canada PW206B](https://openairdocs.org/engine/pratt-whitney-canada-pw206b): 26 aircraft (registry code 52204) - [Pratt & Whitney Canada PW206A](https://openairdocs.org/engine/pratt-whitney-canada-pw206a): 14 aircraft (registry code 52151) - [Pratt & Whitney Canada PW207E](https://openairdocs.org/engine/pratt-whitney-canada-pw207e): 9 aircraft (registry code 52161) - [Pratt & Whitney Canada PW206E](https://openairdocs.org/engine/pratt-whitney-canada-pw206e): 3 aircraft (registry code 52183) --- 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.