# TCDS E00060EN: Trace Engines LP - Type: Type certificate data sheet - Status: Current - Holder: Trace Engines LP - Revision: 7 - Revised: January 28, 2015 - Product: Engine - Certification basis: Part 1, Part 3, Part 33 - Registered aircraft: 1, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/b7/b1/b7b17408fd70d82d40f3226918c4195bbdf625cf6e4e9b870f0b9ed83de5afed - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7831D245EFEF7C9C86257DE300661E44.0001 - Page: https://openairdocs.org/tcds/E00060EN ## Models (2) As the data sheet lists them. - OE600A - TE600D ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text U.S DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E00060EN TCDS NUMBER E00060EN REVISION: 7 DATE: JANUARY 28, 2015 TRACE ENGINES, LP MODELS: OE600A & TE600D Engines of models described herein conforming with this data sheet (which is part of Type Certificate number E00060EN) 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: Trace Engines, LP 3000 West Interstate 20 Midland, Texas 79701 TYPE CERTIFICATE HOLDER RECORD: Orenda Recip, Inc. transferred TC E00060EN to Trace Engines, LP on June 30, 2006 1. MODELS OE600A TE600D TYPE An eight cylinder reciprocating engine in a 90° “V” configuration, aluminum block with iron cylinder liners, with a geared propeller drive and two valves per cylinder operated by pushrods off a single camshaft. The engine is fuel injected, turbosupercharged, liquid cooled, dry sump lubricated with a rear mounted accessory gearbox and magneto type ignition system. RATINGS (See NOTE 1) Max. continuous, hp., engine rpm Takeoff (5 min.) hp., engine rpm Manifold pressure (in. Hg) Max. continuous Takeoff Critical altitude (ft) Max. continuous Takeoff 500-4200 600-4400 50.0 52.0 20,000 10,000 500-4200 600-4400 50.0 50.0 20,000 10,000 REDUCTION GEAR RATIO 0.4675:1 0.4675:1 FUEL (See NOTE 3) Min. grade aviation gasoline Temperature (°F) at fuel pump, max. 100LL (Blue) 150 100LL (Blue) 150 OIL, LUBRICATION Approved oils Temperature Pressure Capacity, min. (US qts) Refer to Maintenance Manual, Chapter 72 See NOTE 2 See NOTE 3 16 See NOTE 2 See NOTE 3 16 IGNITION (dual) Magnetos Timing (degrees BTC) Spark Plugs TCM/Bendix S-1200 series 38±1 Two per cylinder. Refer to Installation Manual Section 3.5.3 for approved spark plug types. Description: revised note 3 to psig from psia *PAGE 1 2 3 REV. 7 7 6 LEGEND: "- -" INDICATES “SAME AS PRECEDING MODEL” "---" “NOT APPLICABLE” NOTE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN. TCDS E00060EN Page 2 of 3 1. MODELS (cont.) OE600A TE600D BORE AND STROKE – in. 4.433 x 4.000 4.433 x 4.000 DISPLACEMENT, cu. in. 495 495 COMPRESSION RATIO 8.0:1 8.0:1 TURBOCHARGER See NOTE 5 See NOTE 5 WEIGHT (dry) lb. Includes all engine supplied, engine mounted components, and the fuel servo, turbocharger, wastegate, wastegate controller, and pressure relief valve. 730 710 C.G. Location Refer to Installation Manual Section 1.3 PROPELLER SHAFT Propeller mounting flange ARP880A ARP880A PRINCIPAL DIMENSIONS (in) Refer to Installation Manual Figure 1 Refer to Installation Manual Figure 1 CERTIFICATION BASIS FAR 33, effective February 1, 1965, Amendments 33-1 through 33-15 inclusive. TYPE CERTIFICATE E00060EN MODELS APPLICATION DATE ISSUED/AMENDED OE600A DEC 12, 1994 MAY 8, 1998 TE600D DEC 16, 2010 JANUARY 21, 2015 NOTES NOTE 1. The engine ratings are based on dry sea level static ICAO standard atmosphere conditions and include extraction of airframe services equivalent to 18 HP. The quoted ratings are obtainable on a test stand with the specified fuel and oil, with intake, exhaust and induction system parameters as defined in the Installation Manual. The allowable power operating envelope at altitudes above the standard density critical altitude for Maximum Continuous power of 20,000 feet is defined in the Installation Manual Section 1.5. NOTE 2. MAXIMUM PERMISSIBLE TEMPERATURES: Engine Coolant 240°F Engine Oil 230°F Exhaust Gas Turbocharger Inlet Temperature (T.I.T.) OE600A 1650°F TE600D 1750°F NOTE 3. FUEL & OIL PRESSURE LIMITS Engine Oil Pressure Limits (psig) Idle – 40 Min – 60 Max – 120 Fuel Pump Inlet Pressure (psig) Min – 0 Max – 60 Fuel Servo Inlet Pressure (psig) Min – 50 Max – 115 TCDS E00060EN Page 3 of 3 NOTE 4. ACCESSORY DRIVE PROVISIONS Accessory Drive Pad Rotation Facing Drive Pad Drive Ratio Max Torque (in-lb.) Max Weight (lb.) Max Overhang Moment (in-lb.) Continuous Static Tachometer Propeller Governor Alternator Customer Service (2) CW CW CCW CW 0.50:1 0.61:1 1.76:1 1.00:1 4.0 8.8 37.7 48.0 75 375 825 375 1.0 3.7 12.75 3.2 1.5 9.1 44.6 8.7 CW – Clockwise CCW – Counter Clockwise NOTE 5. Turbochargers approved for use on the OE600A engine are AlliedSignal model TA94 as listed in OE600A Bill of Material T15000, and Hartzell Technologies T81 as listed in TE600D Bill of Material T15005-1 NOTE 6. Deleted NOTE 7. The Instructions for Continued Airworthiness required by FAR Part 33 have been approved for the OE600A. This Revision, Rev #6 is evidence that the Instructions for Continued Airworthiness required by FAR Part 33 have been approved for the TE600D. -------END------- ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Orenda OE600A](https://openairdocs.org/engine/orenda-oe600a): 1 aircraft (registry code 47911) - [Trace TE600D](https://openairdocs.org/engine/trace-te600d): 0 aircraft (registry code 59525) --- 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.