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FAA AC 43-207 : 2002

Current

Current

The latest, up-to-date edition.

CORRELATION, OPERATION, DESIGN, AND MODIFICATION OF TURBOFAN/JET ENGINE TEST CELLS

Published date

12-01-2013

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CHAPTER 1. INTRODUCTION
100. General
101. Background
102. Calibration and Correlation Standards and Methods
103. Alternative Correlation Methods
104. Definitions of Terms
CHAPTER 2. CONFIGURATION AND CONSTRUCTION
200. General Design Considerations
201. Test Cell Configurations
Figure 2-1. Test Cell Configuration: "L" Type
Figure 2-2. Test Cell Configuration: "U" Type
Figure 2-3. Test Cell Configuration: Folded Inlet Type
202. Engine Test Cell Major Components/Systems
Figure 2-4. Typical Thrust Mount Design
CHAPTER 3. MEASUREMENT SYSTEMS, CALIBRATION, AND CORRELATION
300. Measurement Systems
301. Instrument Calibration
302. Thrust Calibration
303. Factors Influencing Correlation
304. Performance Measurement
305. Factors Affecting Performance
306. Data Acquisition
CHAPTER 4. TEST CELL CORRELATION
400. Correlation Accuracy Assurance
401. Correlation Procedures
402. Correlation Report
403. Maintaining Correlation
404. Facility Operations Manual
APPENDIX 1. RELATED TEST CELL PUBLICATIONS AND MATERIALS
APPENDIX 2. ENGINE TEST CELL APPROVAL SCHEDULE FLOW CHART
APPENDIX 3. SAMPLE CORRELATION PLOTS
APPENDIX 4. GLOSSARY OF ACRONYMS AND ABBREVIATIONS

Gives guidance regarding test cell correlation procedures for test cells used for in-service acceptance testing of turbofan and turbojet engines. Discusses the effects of the design, operation, and modification of a test cell and engine test hardware on engine performance. Also provides guidance on conducting, evaluating, and maintaining test cell correlation.

DocumentType
Standard
PublisherName
Federal Aviation Administration
Status
Current

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FAA AC 39-6 : 0 ANNOUNCEMENT OF AVAILABILITY - SUMMARY OF AIRWORTHINESS DIRECTIVES
FAA AC 145-3 : 1981 GUIDE FOR DEVELOPING AND EVALUATING REPAIR STATION INSPECTION PROCEDURES MANUALS
FAA AC 43-4 : A CORROSION CONTROL FOR AIRCRAFT
FAA AC 33-5 : 0 TURBINE ENGINE ROTOR BLADE CONTAINMENT/DURABILITY
FAA AC 45-3 : 2010 INSTALLATION, REMOVAL, OR CHANGE OF IDENTIFICATION DATA AND IDENTIFICATION PLATES ON AIRCRAFT ENGINES
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