CM-PIFS Approval of Engine Use with a Thrust Reverser CS-E 10(b) Final CM & CRD published Installations and Fuel

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1 Hydromechanical CM-HS Respecting Brake Energy Qualification Limits CS-25 CM-PIFS Approval of Engine Use with a Thrust Reverser CS-E 10(b) Cabin Safety CM-CS Use of Aircraft Materials Fire Test Handbook # CS (including Appendix F) DOT/FAA/AR-00/12 CS CS CS CS Part 21 CM-21.A-J-00X Definition of initial flights for helicopters Annex Part 21 to Commission On hold Regulation (EC) 1702/2003 Avionic CM - AS - 00X Aspen integrated cockpit lay-out n/a Cancelled CM-SWCEH Development assurance of airborne electronic hardware CS & CM-SWCEH Development assurance of airborne electronic hardware CS & CM-SWCEH Development assurance of airborne electronic hardware CS & Final CM published (editorials only) Editorial change in section 6 to reflect that the guidance provided in section 6 is repealed and superseded Effects (SEE) Caused by Atmospheric Radiation, dated 08/01/2018 1

2 CM-SWCEH Software aspects of certification CS & CM-SWCEH Software aspects of certification CS & CM-SWAEH Software aspects of certification CS & Avionic CM-AS-00X Certification considerations for helicopter installations of portable GPS Structures CM-S Compliance with CS-25 Bird Strike Requirements CS (e) CS CS (b)(c ) n/a Superseded by EASA CM-SWCEH-002 Software Aspects of Certification, Issue 01 Revision 01 Final CM published (editorials only) Superseded by ED Decision 2017/020/R Annex II AMC D Airborne Software Development Assurance Using EUROCAE ED-12 and RTCA DO-178. The Proposed CM published for public consultation has been repealed and replaced by ED Decision 2017/020/R Annex II AMC D Airborne Software Development Assurance Using EUROCAE ED-12 and RTCA DO-178. Cancelled Cabin Safety CM-CS Access to and Opening of Type III and IV Exits on Aeroplanes with Passenger Seating Capacities of 19 or Fewer CM-PIFS Large transport aircraft - Fire withstanding capabilities of composite wing containing fuel tank CS (c)(4)(ii) Amendment 9 JAR/CS (c)(2) pre-amendment 9 General CM-GEN-CNX Electronic access to manufacturer data n/a Cancelled CS-25 Part 21 CM-21.A-J Service Bulletins (SB) related to Airworthiness Directives (ADs) Article 21A.263 (c)(3) of Annex Part 21 to Commission Regulation (EC) No. 1702/2003 2

3 Cabin Safety CM-CS Trim and Stability behaviour on water for Ditching and Emergency Floats Installations CS 27/29.751(b) CS 27/29.801(d) On hold Avionic CM-AS Quality of recording of cockpit voice recorders CS-23, CS-25, CS-27 & CS-29, in particular CS XX.1457, CS XX.1301 CS XX.1309 Electrical CM-ES Certification of Power Supply for Portable Electronic Devices CS , CS (a), CS , CS , CS (a)(1), CS (a), CS (a), CS (a), CS , CS , CS 25 Subpart H Avionic CM-AS Clarifications to AMC AMC Avionic CM-AS Clarifications to AMC Revision 1 AMC Final CM published (editorials only) Avionic CM-AS Clarifications to AMC Issue 2 AMC Final CM published (editorials only) Electrical CM-ES Electrical Wiring Interconnection System Instructions for Continued Airworthiness Electrical CM-ES Electrical Wiring Interconnection System Instructions for Continued Airworthiness CS Appendix H25.4(a)(3) and H25.5 CS Appendix H25.4(a)(3) and H25.5 Final CM published (editorials only) CM-PIFS Turbine Over-speed Resulting from Shaft Failure CS-E 510(g)(2), CS-E 840, CS-E 850 CM-PIFS Rotorcraft - Oil Low Pressure Warning CS Definitions CS (b)(1) CM-PIFS Guidance for Rain and Hail Ingestion Testing for Turbine Engines Ice Accretion CM-PIFS Guidance for Rain and Hail Ingestion Testing for Turbine Engines Short Hail Burst CS-E 790 CS-E 540 Cabin Safety CM-CS Helicopter External Loads Personal Carrying Device System CS-29 CS-27 Flight CM-FT Night Vision Image System CS-29 CS-27 (FAA AC 29-2C Change 2 MG16) Structures CM-S Application of CS (c)(2) 1.33 Wear and Tear Factor CS (c )(2) Frequent Removal of Interior Structures 3

4 Rotor and Transmission CM-RTS Large Helicopter Main Gearbox Certification Requirements CS-29 (AC and AC A) Cabin Safety CM-CS Installation of Cargo Seat Bags on Passenger Seats CS , CS , EU-OPS 1270 Hydromechanical CM-HS Consideration of Common Mode Failures and Errors in Flight Control Functions CM-PIFS Engine Critical Parts - Damage Tolerance Assessment Manufacturing and Surface Induced Anomalies CM-PIFS Regulatory Differences CS-E vs CFR 14 Part 33 (for validation by EASA of FAA certified engine types) CS , (c)(1), (a)(1) & (b), CS , , , CS-E 515 CS-E Cancelled CM-PIFS Fuel Specification Changes CS-23, CS-25, CS-27, CS-29, CS-E Structures CM-S Application of standard fasteners (nuts and bolts) within the scope of CS XXX.602 and CS XXX.607 to be used in critical installations Part 21 CM-21.A-K Installation of new parts and appliances without an EASA Form 1 in European Light Aircraft Hydromechanical CS VLA.607, CS VLR.607, CS VLR.602, CS , CS , CS , CS and CS , CS , CS E 515, CS P 160 Article 21.A.307 of Annex 1 Part 21 to 748/2012 Article M.A.502 of Annex 1 Part M to 593/2012 CM-HS Ram Air Turbine Blade Release CS (d), (b)(1)(ii), (d) AMC (d) Cabin Safety CM-CS Flammability Testing of Interior Materials CS (a) and (d), , CS-25 Appendix F Parts I, IV and V, at Amendment 12 Avionic CM-AS Acceptance of Electronic Flight Instrument that have no equipment approval in Small Aeroplanes (ELA1) Structures CM-S Composite Materials Shared Databases - Acceptance of Composite Specifications and Design Values Developed using the NCAMP Process On hold CS-LSA.15 (ASTM F , 8,3 8.4, 8.6) CS , CS , CS , CS- VLA 1301, CS-VLA 1309 CS 2X.603, CS 2X.605, CS 2X.613, CS E- 70 and -170 Structures CM-S Bonded Repair Size Limits in accordance with CS-23, CS-25, CS-27, CS-29 and AMC CS2x.603, AMC

5 Avionic CM-AS Airworthiness Considerations for Lead (Pb) Free Electronics in Airborne CS/JAR 23, 25, 27, 29, CS-E,, CS- ETSO The proposed CM published for public consultation has been repealed Avionic CM-AS Single Event Effects caused by Atmospheric Radiations n/a Cabin Safety CM-CS Width of Aisle CS The Proposed CM published for public consultation has been repealed and replaced by 'proposed' CM-CS-007 Issue 01 Revision 01 Cabin Safety CM-CS Width of Aisle CS Flight CM-FT One Engine Inoperative Ferry Flight 3 or More Engines CS , CS , CS On hold Aircraft MCSD CM-MCSD Development of OSD for Maintenance Certifying Staff 21.A.15/21.A.16A/21.A.16.B/related AMC&GM MMEL CM-MMEL Engine Time Limited Dispatch (TLD) and Master Minimum CS-MMEL, CS-E 1030 Equipment List (MMEL) CS-25 CM-CS Regulatory Significant Standards Differences for pair CS-25 Amendment 12 vs CFR 14 Part 25 Amendment 1 through 136 CS-25 EP CM-EP-00X Flight Manual revisions that introduce reductions in maximum take-off weights and their effect on an aircraft s noise certification status CS-23, CS-25, CS-36 Cancelled Structures CM-S Certification, Type Design Definition, Material and Process Qualification for Composite Light Aircraft CM-PIFS Turbine Engine Relighting In Flight CS-E 910 Part 21.A.4, Part 21.A.20(b), Part 21.A.31, Part 21.A.33 CS-LSA 15 CS VLA.572, CS 22/VLA.603, CS 22/VLA.605, CS 22/VLA.613, CS 22/VLA.615, CS 22/VLA.619, CS 22/VLA.627 5

6 Avionic CM-AS Certification aspects of integrated modular avionics CS , CS , CS , CS CS , CS , CS , CS CS , CS , CS , CS CS , CS , CS , CS Avionic CM-AS Certification of airborne systems using Light Amplification by Stimulated Emission of Radiation (LASER) with high energy CS , CS , CS , CS , CS , CS , CS , CS The Proposed CM published for public consultation has been repealed and replaced by AMC. CM-PIFS Determination of an Unsafe Condition for Risk of Rotorcraft Engine In Flight Shut Down (IFSD) & Power Loss Article 21.A.3A and 21.A.3B of Annex Part 21 to Commission Regulation (EC) No. 748/2012, amended by Commission Regulations (EU) 7/2013 and 69/2014 DASA CM-DASA Vibration Health Monitoring: Prioritisation of Maintenance Alerts Structures CM-S Post Certification Actions to Verify the Continued Integrity of Rotorcraft Critical Parts n/a CS 27/29.602, CS (b), CS and CS (b) Hydromechanical CM-HS CS 27/ Safety considerations covering External Loads CS ; CS and related AC Rotor and Transmission CM-RTS Rotor Drive System Gearbox TBO Development CS Definitions, CS (b) (b) CS Avionic CM-AS Installation of ELTs CS XX.1301, 1309, 1529, 1581 Cabin Safety CM-CS Large Aeroplane Evacuation Certification Requirements Cabin Crew Members Assumed to be On Board Cabin Safety CM-CS Large Aeroplane Evacuation Certification Specifications Cabin Crew Members Assumed to be On Board Flight CM-FT-00X Category A and H-V diagram Aircraft Flight Manual Limitations for Large Rotorcraft during Performance Class 2 Operations CS CS CS29.1, CS29.87, CS , CS , CAT.POL.H.300 The Proposed CM published for public consultation has been repealed and replaced by by 'proposed' CM-CS-008 Issue 01 Revision 01 Cancelled 6

7 Electrical CM-ES Guidance to Certify an Aircraft as PED tolerant CS (b)(1), CS (a)(1), CS (a), CS (a), CS (a), CS (a), CS (a), CS (a), CS , CS , CS , CS Instructions for Continued Airworthiness CM-ICA Completeness and Timely Availability of Instructions for Continued Airworthiness CS , CS , CS , CS , CS , CS , CS 31GB.82, CS 31HB.82, CS 31TGB.82, 30, CS-E 25, CS-LSA.30, 30, CS-VLA 1529, CS VLR.1529, 748/2012, 21.A.61, 21.A.107, 21.A.120, 21.A.449 and 21.A.609 CS , CS , CS , CS , CS , CS , CS 31GB.82, CS 31HB.82, CS 31TGB.82, 30, CS-E 25, CS-LSA.30, 30, CS-VLA 1529, CS VLR.1529, 748/2012, 21.A.61, 21.A.107, 21.A.120, 21.A.449 and 21.A.609 CS , CS , CS , CS , CS , CS , CS 31GB.82, CS 31HB.82, CS 31TGB.82, 30, CS-E 25, CS-LSA.30, 30, CS-VLA 1529, CS VLR.1529, Structures CM-S Additive manufacturing CS X.571, CS X.603, CS X.605, CS X.613, CS-E 70, CS-E 100 (a), 170, 240, 60, GM21.A.91, 21.A.101, 21.A.133, 21.A.433, GM 21.A.435, 21.A.437, 21.A.447, 21.A.805, Structures CM-S Cabin Interior Abuse Loads CS , CS , CS , CS

8 Structures CM-S Composite Materials - The Safe Design and Use of Monocoque Sandwich Structures in Critical Structure Applications AMC (CS23 commuter aircraft, CS25, CS27, and CS29) CM-PIFS Critical Parts Lifing Shortfall 21.A.3, GM 21.A.3, CS-E 510, CS-E 515 Final CM and CRD published CM-PIFS The integrity of nickel powder metallurgy rotating critical parts for gas turbines Structures CM-S Compliance to CS 27_ a(4) for changes affecting surrounding structure (including external installations) CS-E 515 CS 27/29.865, CS 27/ CM-PIFS Fire protection - Burner type selection for fire testing All CS rules where fire withstanding compliance demonstration capability to an engine/apu fire threat is performed using testing Under development Part 21 CM-21.A/21.B Criteria for the determination of the Agency's level of involvement in product certification 21.A.15 (b)(5) and (6), 21.A.93 (b)(3)(ii) and (iii), 21.A.113 (b), 21.B.100, 21.B.103 (a)(2), 21.B.107 (a)(2), 21.B.110 (a)(2), 21.B.115 (a)(2) and 21.B.117 (b) Note: As proposed per EASA Opinion 07/2016. Environmental Control CM-ECS Minimum qualification standards for oxygen cylinders used CS-23, CS-25, CS-27, CS-29 on board aircraft Flight CM-FT Night Vision Image System CS27 Book 2 AMC 27 General (MG16), CS29 Book 2 AMC 29 General (MG16) Structures CM-S Certification of Vibration Health Monitoring (VHM) for compliance with Commission Regulation (EU) 2016/1199 introducing Annex V (Part-SPA) of Regulation (EU) No 965/2012 Subpart K, Helicopter Offshore Operations (HOFO) CS , (EU) No 965/2012 Subpart K, Annex V (Part-SPA) Part 21 CM-21.A-E Approved Model List Changes 21.A.57, 21.A.61, 21.A.62, 21.A.91, 21.A.93, 21.A.97, 21.A.114, 21.A.117, 21.A.119, 21.A.120A, 21.A.120B Part 21 CM-21.A-D Interpretation to 21.A.103(a)(2)(i) 21.A.103(a)(2)(i) Public consultation ongoing Expiry date public consultation: 21/03/2018 8

9 Cabin Safety CM-CS Test Methodology for Simple and Obvious Means CS , CS , CS , CS-25 Under development App. S, S25.20(b) Cabin Safety CM-CS Passenger cabin with incomplete airworthiness compliance Under development classification of changes to allow limited flight operations CS.25, 21.A.91 Avionic CM-AS Certification of Aircraft with databases CS-23, CS-25, CS-27, CS-29 (1301, 1309, Under development 1529) Maintenance Review Board CM-MRB Maintenance Review Board Report / Maintenance Type Board Report Development Process CS xx.1529 Appendix H H25.3(b)(1) Avionic CM-AS FLARM system installations in CS-23, CS 27 and CS-29 aircraft CS-23, CS-27, CS-29 Public consultation ongoing Expiry date public consultation: 21/03/2018 9

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