# TCDS E23NE: Porsche K.-G. Dr. Ing.h.c.F. - Type: Type certificate data sheet - Status: Historical - Holder: Porsche K.-G. Dr. Ing.h.c.F. - Revision: 4 - Revised: January 1, 2009 - Product: Engine - Certification basis: Part 21 - Registered aircraft: 14, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/ec/fa/ecfa47d44a70bb1b323f2bca6bbb6d136d37b76c236b41627d7a3c178fbb76c6 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6C024B1760287D668625758A005D6EE9.0001 - Page: https://openairdocs.org/tcds/E23NE ## Models (3) As the data sheet lists them. - PFM3200N01 - PFM3200N02 - PFM3200N03 ## 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 REV. 4 4 3 3 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" " ---" INDICATES "DOES NOT APPLY" NOTICE: ALL PAGES ARE REFORMATTED. SIGNIFICANT CHANGES, IF ANY ARE BLACK-LINED IN THE LEFT MARGIN. THE TC HAS BEEN CANCELED, EFFECTIVE JANUARY 1, 2009. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E23NE TCDS NUMBER E23NE REVISION: 4 DATE: January 1, 2009 PORSCHE MODELS: PFM3200N01 PFM3200N02 PFM3200N03 Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E23NE) 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 Dr. Ing. h.c.F. Porsche Aktiengesellschaft 7251 Weissach G e r m a n y 1. Former Type Certificate Holder is Dr. Ing. h.c.F. Porsche AKTIENGESELLSCHAFT. 2. Only standard airworthiness certificates issued prior to January 1, 2009 are valid. 3. Production of this product under the TC ceases. 4. Futur unsafe conditions existing in the product may result in an airworthiness directive requiring correction of the unsafe condition before further flight. Since there is no entity responsible for compliance with 14 CFR § 21.99(a), “Required design changes”, the existence of an unsafe condition may result in permanently grounding the aircraft with these engines installed. 5. Replacement parts may not be available in the future. I. MODELS PFM3200N01 PFM3200N02 PFM3200N03 TYPE Ducted fan air-cooled 6 cylinder, horizonta lly opposed 4 stroke cycle reciprocating engine with 2 OHC, propeller reduction gear, NA, fuel injected. RATINGS Maximum continuous at sea level, shaft power, KW/hp Takeoff at sea level, shaft power, KW/hp Maximum economy, shaft power, KW/hp Basic layout Cylinder bore, mm/in. Piston stroke, mm/in. Displacement, cc/in. Compression ratio Prop gear ratio 156/209 156/209 125/167 95/3.74 74.4/2.93 3164/193 9.2:1 .442 - - - - - - - - - - - - - - - - 162/217 162/217 130/174 - - - - - - 10.5:1 - - E23NE Page 2 COMPONENTS Fuel control Fuel pump Ignition system Alternators 35A 55A 70A Starter Bosch/Teldix P/N 0 438 060 056 Bosch/Teldix P/N 0 580 254 944 Magneti Marelli-system No. 71505405, spark plug: Bosch WB 4 DTC Bosch/Teldix P/N's 0 120 488 113 0 120 469 826 0 120 468 021 Bosch P/N 0 001 111 001 - - - - - - - - - - - - - - - - - - - - I. MODELS PFM3200N01 PFM3200N02 PFM3200N03 PRINCIPAL DIMENSIONS Length, mm/in. Width, mm/in. Height, mm/in. 973/38.31 854/33.62 610/24.02 - - - - - - - - - - - - WEIGHT (dry) Basic engine, kg/lbs. (excludes exhaust system) 179.2/402.9 - - - - CENTER OF GRAVITY (excludes exhaust system, propeller governor, air pumps) Rear from prop flange, mm/in. Below axis of prop centerline, Mm/in. Left of axis of prop, mm/in. 500/19.69 120/4.72 8/0.315 - - - - - - - - FUEL (See NOTE 8) OIL (See NOTE 9) CERTIFICATION BASIS FAR 33, effective February 1, 1965, Amendment 9. Type Certificate No. E23NE, issued August 30, 1985. The aviation authority for Germany, Luftfahrt-Bundesamt, originally type certificated this engine. The FAA validated this product under U.S. Type certificate Number E23NE. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Germany. EASA issued Certification Information No: 2008-02, dated July 1, 2008, to revoke its type certificate for the Porsche PFM3200 series engines. IMPORT REQUIREMENTS As of January 1, 2009, new product is no longer eligible for import to the United States. NOTES NOTE 1. The above engine models inco rporate the following characteristics: Model Characteristic N01 Oil cooler in return line, thermostat not on engine. N02 Full flow oil cooler, thermostat on engine. N03 Basically N01 with higher power output, use AVGAS only. E23NE Page 2 NOTE 2. The following accessory driv e provisions are incorporated: Speed Ratio Maximum Torque (Nm/lb.-in.) Overhang Drive Rotation to Engine Continuous Static (Nm/lb.-in.) Type of Drive Starter CW 14.33:1 11.97.3 19/168 3.5/31 * Alternator CCW 1.663:1 7/62 90/796 5.74/50.8 * Vacuum Pump CW 0.553:1 3/26.5 30/265 .35/3.1 AND 20000 Propeller Governor CCW 0.371: 1 2/17.7 45/398 1.3/11.5 AND 20010 High Tension Distributor CCW 0.5:1 0.1/0.9 50/442 0.52/4.6 * CCW = Counterclockwise CW = Clockwise * = supplied with engine as standard equipment NOTE 3. Ratings are based on ambient conditions: International Standard Atmosphere, sea level. NOTE 4. Engine operating limits are as follows: Condition Power KW/hp Engine Speed, rpm** Fuel Flow lb./hr. Oil Pressure, psi Oil Temperature, øC/øF Fuel Pressure psi Takeoff and Max. Cont. 156/209*(N01,2) 162/217*(N03) 5,300+ 110 116 120/248 58-80 Min. Idle ___ 900*** 5 4.4 40/104 58-80 Starting ___ ___ ___ 116 -25/-13 58-80 *This rating is uninstalled power at sea level and 15øC/59øF air inlet temperature. Fuel enrichment is on providing best power output. Power tolerance is -0, +5% as delivered from Porsche. **Propeller speed is equal to .442 times the engine speed. ***Idle speed shall be set at 1100 to 1200 rpm. +Allowed adjustment tolerance is +/- 1% NOTE 5. External engine component maximum limiting temperatures are specified in the Porsche PFM3200 Installation Manual. NOTE 6. Information regarding approved fuel filter and o il filter replacement parts is specified in the Porsche PFM3200 Operator's Manual. NOTE 7. The following fuels are eligible for the PFM 3200 engine: Fuels conforming to the Porsche PFM3200 Installation Manual and/or Operator's Manual. NOTE 8. The following oils are eligible for the PFM3200 engine: Oils conforming to the Porsche PFM3200 Installation Manual and/or Operator's Manual. NOTE 9. Engine performance data are specified in the Porsche PFM3200 Installation Manual. E23NE Page 2 NOTE 10. Engine operating procedure is specifi ed in the Porsche PFM3200 Operator's Manual. NOTE 11. Lightning protection require ments and electromagnetic interference emitted by the ignition system including cables are specified in the Porsche PFM3200 Installation Manual. NOTE 12. Voltage limits for the ignition control system are 18-32 volts. NOTE 13. Each of the documents listed below must stat e that it is approved by the European Aviation Safety Agency (EASA) or, for approvals made before September 28, 2003 by Luftfahrt-Bundesamt (Germany). Any such documents including those approved under a delegated authority, are accepted by the FAA and are considered FAA approval. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals, These approvals pertain to the type design only. ---THE END--- ``` ## ADs (1, in force first) - [AD 99-04-15](https://openairdocs.org/ad/99-04-15): Porsche K.-G., Dr. Ing.h.c.F. PFM3200N01, PFM3200N02 and PFM3200N03. Effective Apr 12, 1999 ## Registered aircraft by registry model (OpenAirDocs) - [Porsche PFM3200N03](https://openairdocs.org/engine/porsche-pfm3200n03): 14 aircraft (registry code 51002) - [Porsche PFM3200N01](https://openairdocs.org/engine/porsche-pfm3200n01): 0 aircraft (registry code 51004) - [Porsche PFM3200N02](https://openairdocs.org/engine/porsche-pfm3200n02): 0 aircraft (registry code 51005) ## STCs approved under this data sheet (1) - [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc. --- 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.