Easy Access Rules For Engines (CS-E) (Amendment 5)
(Amendment 5)CS-E
Easy Access Rules for Engines (CS-E)(Amendment 5)EASA eRules: aviation rules for the 21st centuryRules and regulations are the core of the European Union civil aviation system. The aim of the EASAeRules project is to make them accessible in an efficient and reliable way to stakeholders.EASA eRules will be a comprehensive, single system for the drafting, sharing and storing of rules. Itwill be the single source for all aviation safety rules applicable to European airspace users. It will offereasy (online) access to all rules and regulations as well as new and innovative applications such asrulemaking process automation, stakeholder consultation, cross-referencing, and comparison withICAO and third countries’ standards.To achieve these ambitious objectives, the EASA eRules project is structured in ten modules to coverall aviation rules and innovative functionalities.The EASA eRules system is developed and implemented in close cooperation with Member States andaviation industry to ensure that all its capabilities are relevant and effective.Published February 202011The published date represents the date when the consolidated version of the document was generated.Powered by EASA eRulesPage 2 of 224 Feb 2020
Easy Access Rules for Engines (CS-E)(Amendment 5)DisclaimerDISCLAIMERThis version is issued by the European Union Aviation Safety Agency (EASA) in order to provide itsstakeholders with an updated, consolidated, and easy-to-read publication. It has been prepared byputting together the certification specifications with the related acceptable means of compliance.However, this is not an official publication and EASA accepts no liability for damage of any kindresulting from the risks inherent in the use of this document.Powered by EASA eRulesPage 3 of 224 Feb 2020
Easy Access Rules for Engines (CS-E)(Amendment 5)Note from the editorNOTE FROM THE EDITORThe content of this document is arranged as follows: the certification specifications (CS) are followedby the related acceptable means of compliance (AMC) paragraph(s).All elements (i.e. CS and AMC) are colour-coded and can be identified according to the illustrationbelow. The EASA Executive Director (ED) decision through which the point or paragraph wasintroduced or last amended is indicated below the paragraph title(s) in italics.Certification specificationED decisionAcceptable means of complianceED decisionThe format of this document has been adjusted to make it user-friendly and for reference purposes.Any comments should be sent to erules@easa.europa.eu.Powered by EASA eRulesPage 4 of 224 Feb 2020
Easy Access Rules for Engines (CS-E)(Amendment 5)Incorporated amendmentsINCORPORATED AMENDMENTSCS/AMC (ED DECISIONS)Incorporated ED DecisionCS/AMC Issue No, Amendment NoApplicability dateED Decision 2003/9/RMCS-E/ Initial issue24/10/2003ED Decision 2007/015/RCS-E/ Amendment 110/12/2007ED Decision 2009/018/RCS-E/ Amendment 218/12/2009ED Decision 2010/015/RCS-E/ Amendment 323/12/2010ED Decision 2015/009/RCS-E/ Amendment 413/3/2015ED Decision 2018/014/RCS-E/ Amendment 515/12/2018Note: To access the official versions, please click on the hyperlinks provided above.Powered by EASA eRulesPage 5 of 224 Feb 2020
Easy Access Rules for Engines (CS-E)(Amendment 5)Table of contentsTABLE OF CONTENTSDisclaimer . 3Note from the editor . 4Incorporated amendments . 5Table of contents . 6Preamble . 11SUBPART A – GENERAL. 16AMC General . 16CS-E 10 Applicability . 16AMC E 10(b) Thrust Reversers . 16CS-E 15 Terminology . 17CS-E 20 Engine Configuration and Interfaces . 19AMC E 20 Engine Configuration and Interfaces . 19AMC E 20(f) Power assurance data for engines with one or more OEI power ratings . 20CS-E 25 Instructions for Continued Airworthiness . 21AMC E 25 Instructions for continued airworthiness . 23CS-E 30 Assumptions. 26AMC E 30 Assumptions . 27CS-E 40 Ratings . 29AMC E 40 Ratings . 30AMC E 40(b)(3) and (b)(4) 30-Second OEI, 2-Minute OEI and 30-minute Power Ratings . 30AMC E 40(d) Operating Limitations . 31CS-E 50 Engine Control System . 33AMC E 50 Engine Control System . 35AMC E 50(e) Rotor integrity . 37AMC E 50(j) Controls - Engines having a 30-Second OEI Power Rating . 37CS-E 60 Provision for Instruments . 38AMC E 60 Provision for instruments . 39AMC E 60(d) Provision for instruments . 39CS-E 70 Materials and Manufacturing Methods. 40AMC E 70 Castings, Forgings, Welded Structures and Welded Components . 41CS-E 80 Equipment. 43AMC E 80 Equipment . 44CS-E 90 Prevention of Corrosion and Deterioration . 50CS-E 100 Strength . 50CS-E 110 Drawings and Marking of Parts – Assembly of Parts . 50Powered by EASA eRulesPage 6 of 224 Feb 2020
Easy Access Rules for Engines (CS-E)(Amendment 5)Table of contentsCS-E 120 Identification . 51CS-E 130 Fire Protection . 51AMC E 130 Fire Protection . 52CS-E 135 Electrical Bonding . 59AMC E 135 Electrical Bonding . 59CS-E 140 Tests - Engine Configuration . 60AMC E 140 Test - Engine configuration . 60CS-E 150 Tests - General Conduct of Tests . 61AMC E 150(a) Tests - General conduct of tests . 61CS-E 160 Tests - History . 61CS-E 170 Engine Systems and Component Verification. 62AMC E 170 Engine systems and component verification . 62CS-E 180 Propeller Functioning Tests . 63AMC E 180 Propeller Functioning Tests . 64CS-E 190 Engines for Aerobatic Use. 64SUBPART B — PISTON ENGINES: DESIGN AND CONSTRUCTION . 65CS-E 210 Failure Analysis . 65AMC E 210 Failure Analysis . 65CS-E 230 De-Icing and Anti-Icing Precautions . 65CS-E 240 Ignition . 65CS-E 250 Fuel System . 66CS-E 260 Engine Cooling System . 67CS-E 270 Lubrication System . 67CS-E 290 Hand Turning . 67SUBPART C — PISTON ENGINES, TYPE SUBSTANTIATION . 68CS-E 300 Conditions Applicable to All Tests . 68AMC E 300(f) Conditions Applicable to all Tests - Torque Measurement . 69CS-E 320 Performance Correction . 69AMC E 320 Performance correction . 69CS-E 330 Tests - General . 70CS-E 340 Vibration Tests . 70AMC E 340 Vibration Tests . 71CS-E 350 Calibration Tests . 71AMC E 350 Calibration Tests . 72CS-E 360 Detonation Tests . 72CS-E 370 Starting Tests . 72CS-E 380 Low Temperature Starting Tests. 73AMC E 380 Low Temperature Starting Tests . 73Powered by EASA eRulesPage 7 of 224 Feb 2020
Easy Access Rules for Engines (CS-E)(Amendment 5)Table of contentsCS-E 390 Acceleration Tests . 73CS-E 400 Over-speed Tests . 74CS-E 430 Water Spray Tests . 74CS-E 440 Endurance Test . 75AMC E 440(b)(3) Endurance Test - Schedule for Engine Incorporating a Turbocharger . 78CS-E 450 Ignition Tests. 78CS-E 460 Backfire Tests . 78CS-E 470 Contaminated Fuel . 79AMC E 470 Contaminated Fuel . 79SUBPART D – TURBINE ENGINES: DESIGN AND CONSTRUCTION . 80CS-E 500 Functioning . 80AMC E 500 Functioning - Control of Engines (Turbine Engines for Aeroplanes) . 80CS-E 510 Safety Analysis . 80AMC E 510 Safety analysis. 82CS-E 515 Engine Critical Parts . 89AMC E 515 Engine Critical Parts . 90CS-E 520 Strength . 101AMC E 520(a) Strength - High Cycle Fatigue . 102AMC E 520(c)(1) Strength - Shedding of Blades . 102AMC E 520(c)(2) Engine Model Validation . 102AMC E 520(d) Strength – Local Failures . 103CS-E 525 Continued Rotation. 104AMC E 525 Continued rotation . 104CS-E 540 Strike and Ingestion of Foreign Matter. 104AMC E 540 Strike and ingestion of foreign matter . 105CS-E 560 Fuel System . 105AMC E 560 Fuel System . 106CS-E 570 Oil System . 108AMC E 570 Oil system . 109CS-E 580 Air Systems. 110CS-E 590 Starter Systems . 110SUBPART E – TURBINE ENGINES: TYPE SUBSTANTIATION . 111CS-E 600 Tests - General . 111AMC E 600(e) Test - General . 111CS-E 620 Performance Correction . 111AMC E 620 Performance: Formulae . 112CS-E 640 Pressure Loads . 113AMC E 640 Pressure Loads . 114CS-E 650 Vibration Surveys . 115AMC E 650 Vibration Surveys . 116Powered by EASA eRulesPage 8 of 224 Feb 2020
Easy Access Rules for Engines (CS-E)(Amendment 5)Table of contentsCS-E 660 Fuel Pressure and Temperature . 126AMC E 660 Fuel Pump Tests (Turbine Engines for Aeroplanes) . 127CS-E 670 Contaminated Fuel . 127AMC E 670 Contaminated Fuel Testing . 127CS-E 680 Inclination and Gyroscopic Load Effects . 129AMC E 680 Inclination and Gyroscopic Load Effects . 129CS-E 690 Engine Bleed . 129AMC E 690 Engine bleed . 130CS-E 700 Excess Operating Conditions . 130AMC E 700 Excess Operating Conditions (Turbine Engines for Aeroplanes) . 131CS-E 710 Rotor Locking Tests . 132AMC E 710 Rotor locking tests . 132CS-E 720 Continuous Ignition. 133AMC E 720(a) Continuous Ignition . 133CS-E 730 Engine Calibration Test . 133AMC E 730 Calibration Tests . 133CS-E 740 Endurance Tests .
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Engines regulated by 40 CFR Part 86 typically include engines used in on-highway applications such as heavy-duty gasoline fueled engines (HDGEs), heavy-duty diesel fueled engines (HDDEs), and heavy-duty engines using alternate fuels (CNG, LPG and LNG). Engines regulated by 40 CFR Part 89 include compression-ignition engines used in nonroad .
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