text: Decision of the Management Board concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (“rulemaking procedure”), EASA MB/7/03, 27.6.2003.

identifier: AMC & GM to Part-66 — Issue 1, Amendment 1

beslut: ED Decision 2005/007/R

text: DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to

text: Regulation (EC) No 1592/2002 of 15 July 2002

text: on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency (hereinafter referred to as the “Agency”), and in particular Articles

text: and

text: thereof. Having regard to the

text: Commission Regulation (EC) No 2042/2003 of 28 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks. Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. The consultation period has been reduced to 6 weeks and no regulatory impact assessment has or will be carried out. This Agency Decision is published together with the CRD. (4) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance, as well as any guidance material for the application of the Basic Regulation and its implementing rules.

type: rubrik

text: OJ L 240, 7.9.2002, p. 1. 2 OJ L 315, 28.11.2003, p. 1.

text: (5) The Agency, pursuant to Article 43 of the Basic Regulation and articles 5(3) and 6 of the EASA rulemaking procedure , has widely consulted interested parties (see: NPA No 13-2005) on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received (see: CRD No 13-2005). HAS DECIDED:

text: Article 1

text: Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence to Decision No 2003/19/RM is amended by Annex I to this decision.

text: Article 2

text: This Decision shall enter into force on the day following its publication in the Official Publication of the Agency. Done at Cologne, 19 December 2005 P. Goudou Annex I “APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE The following aircraft type ratings will be used to ensure a common standard throughout the Member States. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under Regulation 1702/2003, this list being only intended for the purpose of maintenance. In order to keep this list current and type ratings consistent, where a Member State needs to issue a type rating that is not included in this list, such information should be first passed on to the Agency. 1. Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg, requiring type training and individual type rating.

text: Aerospaceline Guppy (RR Corp 501) Antonov AN72 (Lotarev D-36) Antonov AN124 (Lotarev D-18T) Aerospatiale N262 (Turbomeca Bastan) Aerospatiale SN601 (PWC JT15D) ATR 42 Non PEC (PWC 120) ATR 72 Non PEC (PWC 120) Airbus A300 B2/B4 (GE CF6) ATR 42/72 PEC (PWC 120) Airbus A300 B2/B4 (PW 4000) Airbus A300 B2/B4 (PW JT9D) BAe 1-11 (RRD Spey) Airbus A300-600 (GE CF6) BAe 125 (Honeywell TFE 731) Airbus A300-600 (PW 4000) BAe 125 (RR Corp Viper) Airbus A300-600 (PW JT9D) BAe 146 / RJ (Avco-Lyc ALF 500 Series) Airbus A310 (GE CF6) BAe 748 (RRD Dart) Airbus A310 (PW 4000) BAe 125 / Hawker 1000 (PWC 305) Airbus A310 (PW JT9D) BAe ATP (PWC 120) Airbus A318 (PW 6000) BAe Jetstream 31/32 (Honeywell TPE 331) Airbus A318/A319/A320/A321 (CFM56) BAe Jetstream 41 (Honeywell TPE 331) Airbus A319/A320/A321 (IAE V2500) Airbus A330 (GE CF6) Beech 300 (PWC PT6) Airbus A330 (PW 4000) Beech 350 (PWC PT6) Airbus A330 (RR Corp Trent 700) Beech 400 (PW JT15) Airbus A340 (CFM56) Beech 1900 (PWC PT6) Airbus A340 (RR Corp Trent 500) Airbus A380 (RR Corp Trent 900) Boeing B707/720 (PW JT3D) Airbus Beluga (GE CF6) Boeing B717-200 (RRD BR715) Boeing B727 (PW JT8D) Antonov AN12 (Ivchenko AI-20K) Boeing B727 (RR Corp Tay) Antonov AN22 (Kusnetsov NK-12MA) Boeing B737-100/200 (PW JT8D) Antonov AN24 (Ivchenko AI-24A) Boeing B737-300/400/500 (CFM56) Antonov AN26 (Ivchenko AI-24T) Boeing B737-600/700/800/900 (CFM 56) Antonov AN28 (Glushenkov TVD-10V) Boeing B747-100 (GE CF6) Antonov AN32 (Ivchenko AI-20M) Boeing B747-100 (PW JT9D) Antonov AN38 (Honeywell TPE 331) Boeing B747-100 (RR Corp RB211)

text: Boeing B747-200/300 (GE CF6) Dassault Falcon 2000EX EASy (PWC 308) Boeing B747-200/300 (PW JT9D) Boeing B747-200/300 (RR Corp RB211) Dornier DO 228 (Honeywell TPE 331) Boeing B747-400 (GE CF6) Dornier DO 328 (PWC 119) Boeing B747-400 (PW 4000) Dornier DO 328 (PWC 306) Boeing B747-400 (RR Corp RB211) Boeing B747SP (PW JT9D) Embraer EMB 110 (PWC PT 6) Boeing B747SP (RR Corp RB211) Embraer EMB 120 (PWC 118) Boeing B757-200/300 (PW 2000) Embraer EMB 135/145 (RR Corp AE3007A) Boeing B757-200/300 (RR Corp RB211) Embraer ERJ 170 100/200 (GE CF34) Boeing B767-200/300 (PW 4000) Boeing B767-200/300 (PW JT9D) Fairchild SA 226/227 (Honeywell TPE 331) Boeing B767-200/300 (RR Corp RB211) Fairchild SA 227 Metro III (PWC PT6) Boeing B767-200/300/400 (GE CF6) Boeing B777-200/300 (GE 90) Fokker F27 Series/FH227 (RRD Dart) Boeing B777-200/300 (PW 4000) Fokker F28 Series (RRD Spey) Boeing B777-200/300 (RR Corp Trent 800) Fokker F50 (PWC 125) Fokker F70/100 (RR Corp Tay) Bombardier BD100-1A10 (Honeywell AS907) Fokker VFW 614 (RR Corp M45H) Bombardier BD700-1A10 (RRD BR710) Fokker VFW 614 Attas (RR Corp M45H) Bombardier CL 600-1A11 (Avco-Lyc ALF502) Bombardier CL 600-2A12 (GE CF34) Gates Learjet 23 (CJ610) Bombardier CL 600-2B16 (GE CF34) Gates Learjet 24 (CJ610) Bombardier CL 600-2B19 (GE CF34) Gates Learjet 25 (CJ610) Bombardier CL 600-2C10 (GE CF34) Gates Learjet 31 (Honeywell TFE 731) Bombardier CL 600-2D24 (GE CF34) Gates Learjet 35 (Honeywell TFE 731) Bombardier DHC-7 (PWC PT6) Gates Learjet 36 (Honeywell TFE 731) Bombardier DHC-8-100/200/300 (PWC 120) Gates Learjet 45 (Honeywell TFE 731) Bombardier DHC-8-400 (PWC 150) Gates Learjet 55 (Honeywell TFE 731) Gates Learjet 60 (PWC 305) Canadair CL 215 (PW R2800) Canadair CL 415 (PWC 123) Gulfstream G100/Astra SPX (Honeywell TFE 731) Casa 212 (Honeywell TPE 331) Gulfstream G200/Galaxy (PWC 306) Casa 235 (GE CT7) Gulfstream GI (RRD Dart) Gulfstream GII & GIII (RRD Spey) Cessna 525/525A (Will FJ 44) Gulfstream GIV/G300/G400 (RR Corp Tay) Cessna 550/560 (PWC 530/535) Gulfstream GIV-X/G450 (RR Corp Tay) Cessna 550/560 (PWC JT15D) Gulfstream GV (RRD BR 710) Cessna 560 (PWC 545) Gulfstream GV-SP/G500/G550 (RRD BR 710) Cessna 650 (Honeywell TFE 731) Cessna 680 (PWC 306) IAI 1121/1123 (CJ610) Cessna 750 (RR Corp AE 3007C) IAI 1124 (Honeywell TFE 731) IAI 1125 (Honeywell TFE 731) Convair 440 (PW R2800) Convair 540/580 (RR Corp 501) Ilyushin IL-14 (Shvetsov Ash-82T) Convair 600/640 (RRD Dart) Ilyushin IL-18 (Ivchenko AI-20M) Ilyushin IL-62 (Kuznetsov NK-8-4) Dassault Falcon 10/100 (Honeywell TFE 731) Ilyushin IL-62 (Soloviev D-30KU) Dassault Falcon 20 (Honeywell TFE 731) Ilyushin IL-76 (Soloviev D-30KP) Dassault Falcon 20-5 (GE CF700) Ilyushin IL-86 (CFM 56) Dassault Falcon 50B (Honeywell TFE 731) Ilyushin IL-86 (Kuznetsov NK-86) Dassault Falcon 50EX (Honeywell TFE 731) Ilyushin IL-86 (Soloviev PS-90) Dassault Falcon 200 (Honeywell ATF 3-6) Ilyushin IL-96 (Soloviev PS-90A) Dassault Falcon 900B (Honeywell TFE 731) Ilyushin IL-96MK (PW 2037) Dassault Falcon 900C (Honeywell TFE 731) Ilyushin IL-114 (Klimov TV7) Dassault Falcon 900EX (Honeywell TFE 731) Ilyushin IL-114PC (PW 127) Dassault Falcon 900EX EASy/DX (Honeywell TFE 731) Let L-410/L-420 (Walter M601) Dassault Falcon 2000 (Honeywell CFE 738) Let 610 (GE CT7) Dassault Falcon 2000EX (PWC 308)

text: Lockheed Jetstar (Honeywell TFE 731) Mitsubishi MU-300 (PW JT15) Lockheed Jetstar (PW JT12) Lockheed L100 (RR Corp T56) PZL M 28 (PWC PT6) Lockheed L188 (RR Corp 501) Lockheed L382 (RR Corp 501) Rockwell Sabreliner (Honeywell TFE 731) Lockheed L1011 (RR Corp RB211) Rockwell Sabreliner (GE CF700) Rockwell Sabreliner (PW JT12) McD DC3 (PW R1830) McD DC4 (PW R2000) Saab 340 (GE CT-7) McD DC6 (PW R2800) Saab 2000 (RR Corp AE2100) McD DC7 (Wright R3350) McD DC8 (CFM56) Shorts 330/360 (PWC PT6) McD DC8 (PW JT3D) McD DC8 (RR Corp Conway) Tupolev TU 134 (Soloviev D-30-II) McD DC9 (PW JT8D) Tupolev TU 154 (Kusnetsov NK-8) McD DC10 (GE CF6) Tupolev TU 154 (Soloviev D-30KU) McD DC10 (PW JT9D) Tupolev TU 204 (Soloviev PS-90AT) McD MD11 (GE CF6) Tupolev TU 204 (RR RB211) McD MD11 (PW 4000) McD MD80 Series (PW JT8D) Yakovlev Yak-40 (Ivchenko AI-25) McD MD90 (V2500) Yakovlev Yak-42 (Lotarev D-36)

text: 2. Aeroplanes of 5700kg and below, requiring type training and individual type rating (A-tr).

text: Beech 90 (PWC PT6) Piaggio P180 Avanti (PWC PT6) Beech 200 Series (PWC PT6) Beech 99/100 Series (PWC PT6) Pilatus PC-12 (PWC PT6) Beech B100 (Honeywell TPE 331) Pilatus PC-12/45 (PWC PT6)

text: Bombardier DHC-6 (PWC PT6) Piper PA 42 (Honeywell TPE 331) Piper PA 42 (PWC PT6) Cessna 425 (PWC PT6) Piper PA 46-310P/-350P (PWC PT6) Cessna 441 (Honeywell TPE 331) Piper PA 46-500 Meridian (PWC PT6) Cessna 500/501/551 (PWC JT15D) Cessna 525B (Will FJ 44) Raytheon 390 (Williams FJ44) Cessna/Reims F406 (PWC PT6) Rockwell Commander 680T/V/681/690/695 Dornier DO228 (Honeywell TPE 331) (Honeywell TPE 331) Dornier Seastar CD2 (PWC PT6) Socata TBM 700 (PWC PT6) Embraer EMB-121 (PWC PT6)

text: 3. Aeroplanes multiple turbine engines (AMTE) of 5700kg and below, eligible to type examinations and group ratings.

text: Beech 65-90 (PWC PT6) Beech 99 (PWC PT6) Mitsubishi MU 2B (Honeywell TPE 331)

text: Britten Norman BN2T Islander (RR Corp 250) Nomad N24A (RR Corp 250)

text: Dornier DO 28D-6/128-6 (PWC PT6) Piaggio P-180 (PWC PT6)

text: Fairchild Swearingen SA 26-AT (Honeywell Piper PA 31T (PWC PT6) TPE 331)

text: Shorts SC7 Skyvan 3 Variant 100 (Honeywell TPE 331)

text: 4. Aeroplanes single turbine engine (ASTE) of 5700kg and below, eligible to type examinations and group ratings.

text: Bombardier DHC-2 (PWC PT6) Pilatus PC-6 (Turbomeca Astazou) Bombardier DHC-3 (PWC PT6) Pilatus PC-6 (Honeywell TPE 331) Pilatus PC-7 (PWC PT6) Cessna 206/207 (RR Corp 250) Pilatus PC-9 (PWC PT6) Cessna 208 Series (PWC PT6) SIAI-Marchetti SM1019 (RR Corp 250) Grob G 520 (Honeywell TPE 331) Trush S2R-T Series (PWC PT 6) Pilatus PC-6 (PWC PT6) Pilatus PC-6 (Lycoming GSO 480) / Pilatus PC-6 (Lycoming IGO 540)

text: 5. Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible to type examinations and group ratings.

text: Aero Commander 680E (Lycoming) Cessna T303 (RR Continental) Cessna T337 (RR Continental) Aircraft Industries L 200 Series (LOM) Grumman American GA-7 (Lycoming) Beech 55 (RR Continental) Beech 58 (RR Continental) Partenavia P68 (Lycoming) Beech 58P (RR Continental) Beech 60 (Lycoming) Piper PA 23 Series (Lycoming) Beech 65-80 (Lycoming) Piper PA 30 (Lycoming) Beech 76 (Lycoming) Piper PA 31 (Lycoming) Beech 95 Series (Lycoming) Piper PA 31P (Lycoming) Beech 95 Series (RR Continental) Piper PA 34 (Lycoming) Piper PA 34 (RR Continental) Britten Norman BN2 Islander (Lycoming) Piper PA 39 (Lycoming) Britten Norman BN2A Trislander (Lycoming) Piper PA 44 Series (Lycoming) Piper PA 60 Series (Lycoming) Cessna 310 Series (RR Continental) Cessna 335 (RR Continental) Rockwell 500S Shrike Commander (Lycoming) Cessna 337 (RR Continental) Rockwell Commander 680/680E/720 Cessna 340 (RR Continental) (Lycoming) Cessna 401/402 (RR Continental) Rockwell Commander 685 (Lycoming) Cessna 404 (RR Continental) Rockwell Commander 560F/680F (Lycoming) Cessna 414 (RR Continental) Cessna 421 (RR Continental)

text: 6. Aeroplane single piston engine – metal structure (ASPE-MS), eligible to type examinations and group ratings.

text: American AA-1 (Lycoming) Apex Aircraft R 3000 series (Lycoming) American AA-1A (Lycoming) American AA-5 (Lycoming) ARV 1 Super 2 (Hewland) American AG-5B (Lycoming) Beech 23 (Lycoming) Apex Aircraft R 2000 series (Lycoming) Beech 23 (RR Continental)

text: Beech 24 (Lycoming) Morane Saulnier Rallye 150 (Lycoming) Beech 33 Series (RR Continental) Morane Saulnier Rallye 180T (Lycoming) Beech 35 Series (RR Continental) Morane Saulnier Rallye 235E (Lycoming) Beech 36 (RR Continental) Moravan Z-142 (Walter) Bölkow BO 208 (RR Continental) Moravan Z-143 L (Lycoming) Bölkow BO 209 (Lycoming) Moravan Z-242 L (Lycoming) Moravan Z-526F (Walter) Bombardier DHC-2 (PW) Bombardier DHC-3 (PW) Piaggo P 149 D (Lycoming)

text: Cessna 120 (RR Continental) Piper PA 16 Series (Lycoming) Cessna 140 Series (RR Continental) Piper PA 18 (RR Continental) Cessna 150 Series (RR Continental) Piper PA 18 Series (Lycoming) Cessna 152 (Lycoming) Piper PA 20 Series (Lycoming) Cessna 170 Series (RR Continental) Piper PA 22 Series (Lycoming) Cessna 172 Series (Lycoming) Piper PA 24 Series (Lycoming) Cessna 172 Series (RR Continental) Piper PA 25 Series (Lycoming) Cessna 172 Series (Thielert) Piper PA 28 Series (Lycoming) Cessna 175 Series (Lycoming) Piper PA 28 Series (RR Continental) Cessna 175 Series (RR Continental) Piper PA 28-201T (RR Continental) Cessna 177 Series (Lycoming) Piper PA 28 Series (TAE) Cessna 180 Series (RR Continental) Piper PA 32 Series (Lycoming) Cessna 182 Series (Lycoming) Piper PA 38 Series (Lycoming) Cessna 182 Series (RR Continental) Piper PA 46 (Continental) Cessna 182 Series (SMA) Piper PA 46 (Lycoming) Cessna 185 Series (RR Continental) Cessna 195 (Jacobs) PZL-104 Wilga Series (PZL / Lycoming) Cessna 206 Series (RR Continental) PZL M 18 (PZL) Cessna 207 Series (RR Continental) PZL M 26 (Lycoming) Cessna 210 Series (RR Continental) Cessna P210N (RR Continental) Republic RC-3 (Lycoming)

text: Fuji FA-200 Series (Lycoming) Rockwell Commander 112 (Lycoming) Rockwell Commander 114 (Lycoming) Gippsland GA8 (Lycoming) SIAI-Marchetti S205 (Lycoming) Maule M4 (RR Continental) SIAI-Marchetti S208 (Lycoming) Maule M5-180C (Lycoming) Maule M5-235C (Lycoming) SOCATA TB9 (Lycoming) Maule M6-235 (Lycoming) SOCATA TB10 (Lycoming) Maule M7 Series (Lycoming) SOCATA TB20 (Lycoming) Maule MX-7-180 (Lycoming) SOCATA TB21 (Lycoming)

text: Mooney M20 (Lycoming) Symphony OMF-100-160 (Lycoming) Mooney M20 (Lycoming / RR Continental) Thrush S2R (PW) Morane Saulnier MS 892 (Lycoming) Morane Saulnier MS 893 (Lycoming) Morane Saulnier MS 894 (Franklin) Morane Saulnier Rallye 100 (RR Continental) Morane Saulnier Rallye 110ST (Lycoming)

text: 7. Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible to type examinations and group ratings. 8. Aeroplane single piston engine – wooden structure (ASPE-WS), eligible to type examinations and group ratings.

text: Apex Aircraft Cap 10 (Lycoming) Champion 8 Series (Lycoming) Apex Aircraft DR 300 series (Lycoming) Apex Aircraft DR 400 series (Lycoming) Christen A1 Husky (Lycoming)

text: Aviamilano P.19 (RR Continental) Emeraude CP301 (Continental)

text: Bellanca 17-30A (RR Continental) Piper J3C (Continental) Bellanca 7 Series (Lycoming) Piper PA 11 (Continental) Bellanca 8 Series (Lycoming) Piper PA 12 (Lycoming) Piper PA 15 (RR Continental) CAP 10 (Lycoming) Slingsby T61 (Stark) Champion 7 Series (Continental) Slingsby T67A (Lycoming) Champion 7 Series (Lycoming)

text: 9. Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible to type examinations and group ratings.

text: Diamond DA42 (TAE)

text: 10. Aeroplane single piston engine – composite structure (ASPE-CS), eligible to type examinations and group ratings.

text: Cirrus SR20 (Continental) Extra EA-400 (RR Continental)

text: Diamond DA20/DV20 (Rotax) Grob G115 Series (Lycoming) Diamond DA20 (RR Continental) Diamond DA40 (Lycoming) Ruschmeyer R90-230RG (Lycoming) Diamond DA40 D (TAE) Slingsby T67 Series Comp (Lycoming) Extra EA-300 (Lycoming)

text: 11. Multi-engine helicopters (MEH), requiring type training and individual type rating.

text: Agusta A109 Series (PW 206/207) Bell 214 (Lycoming T5508D) Agusta A109 Series (RR Corp 250) Bell 214 (T700) Agusta A109 (Turbomeca Arriel 1) Bell 222 (RR Corp 250) Agusta A109 Series (Turbomeca Arrius 2) Bell 222 (Lycoming LTS 101) Bell 230/430 (RR Corp 250) Agusta-Bell AB 139 (PWC PT6) Bell 412 (PWC PT6) Agusta/Westland EH-101 (GE CT700) Bell 430 (RR Corp 250)

text: Bell 212 (PWC PT6) Boeing 107 (CT58) Bell 214 (GE CT7) Boeing BV234 (Avco Lyc 5512)

text: Kamov KA-25 (Glushenkov GTD-3BM) EAC S-64-F (PW JFTD12) Kamov KA-27 (Isotov TV3)

text: Eurocopter AS 321/330 (Turbomeca Turmo) MD 900 (PW 206/207) Eurocopter AS 332 L2 (Turbomeca Makila 2A) MD 902 (PW 206/207) Eurocopter AS 332/332L/L1 (Turbomeca Makila 1A) Mil Mi-6 (Soloviev D-25V) Eurocopter AS 355 (RR Corp 250) Mil Mi-8 (Isotov TV2) Eurocopter AS 355 (Turbomeca Arrius 1) Mil Mi-10 (Soloviev D-25V) Eurocopter AS 365 N (Turbomeca Arriel 1) Mil Mi-17 (Isotov TV3) Eurocopter AS 365 N1, N2, N3 (Turbomeca Mil Mi-26 (Lotarev D-136) Arriel 1) Eurocopter AS 365 N1, N2, N3 (Turbomeca PZL W-3A Swidnik (Rzeszow PZL-10W) Arriel 2C) PZL W-3AS Swidnik (Rzeszow PZL-10W) Eurocopter BO 105 Series (RR Corp 250) Eurocopter EC 135 (Turbomeca Arrius 2B) Sikorsky S61N (GE CT58) Eurocopter EC 135 (PW 206) Sikorsky S64 (PW JTFD 12) Eurocopter EC155 (Turbomeca Arriel 2) Sikorsky S70 (GE CT700) Eurocopter EC 225 (Turbomeca Makila 2A) Sikorsky S76A (RR Corp 250) Eurocopter MBB-BK 117 A-1/-3/-4/-B-1/-2 Sikorsky S76A (Turbomeca Arriel 1) (LTS 101) Sikorsky S76B (PWC PT6) Eurocopter MBB-BK 117 C1 (Turbomeca Arriel Sikorsky S76C (Turbomeca Arriel 2) 1) Sikorsky S92A (GE CT7-8) Eurocopter MBB-BK 117 C2 (Turbomeca Arriel 1) Westland W30 (RR Corp Gem) Eurocopter SA 365 C Series (Turbomeca Arriel Westland Wessex (RR Corp Gnome) 1)

text: 12. Helicopters with turbine engines (HTE), eligible to type examinations and group ratings.

text: Agusta 204/205 (Lycoming T53) Eurocopter SE 3160 (Turbomeca Artouste IIIB) Agusta 206 RR Corp 250) Agusta A119 (PWC PT6) Kaman K-1200 (T53-17A-1)

text: Bell 47 Soloy (RR Corp 250) McD 369 (RR Corp 250) Bell 204/205 (Lycoming T53) Bell 206 (RR Corp 250) MD 500N (RR Corp 250) Bell 407 (RR Corp 250) MD 600N (RR Corp 250) MD 520 (RR Corp 250) Enstrom 480 (RR Corp 250) Mil Mi-2 (PZL GTD-350 III/IV) Eurocopter AS 350 (Turbomeca Arriel 1) Eurocopter AS 350 (Turbomeca Arriel 2B) Schweizer 269D (RR Corp 250) Eurocopter EC 120 (Turbomeca Arrius 2F) Eurocopter EC 130 (Turbomeca Arriel 2B) Sikorsky S55 (Wright Cyclone) Eurocopter SA 315 (Turbomeca Artouste IIIB) Sikorsky S55T (Honeywell TSE 331) Eurocopter SA 319 (Turbomeca Astazou XIVB) Sikorsky S58 (Wright Cyclone) Eurocopter SA 341G (Turbomeca Astazou IIIA) Sikorsky S58T (PWC PT6) Eurocopter SA 341J (Turbomeca Astazou XIVH) Eurocopter SA 360 (Turbomeca Astazou Sud-Ouest SO 1221 (Turbomeca Palouste IV) XVIIIA) Eurocopter SA 3180 (Turbomeca Astazou IIA) Westland S55 (PW R1340) Eurocopter SE 3130 (Turbomeca Artouste IIC)

text: 13. Helicopters with piston engines (HPE), eligible to type examinations and group ratings.

text: Bell/Agusta/Westland 47 (Lycoming) Hughes/Schweizer 269 (Lycoming) Brantly B2 (Lycoming) Kamov Ka-26D (Vedeneyev) Enstrom F28/F280 (Lycoming) Robinson R22/R44 Series (Lycoming) Hiller UH-12 (Lycoming) Schweizer 269D Series (Lycoming)

type: vagledning

utgivare: easa


text: OJ L 240, 7.9.2002, p. 1. Regulation as last amended by

text: Regulation (EC) No 1701/2003

text: (OJ L 27.9.2003, p. 5). OJ L 315, 28.11.2003, p. 1. Regulation as last amended by

text: Regulation (EC) No 707/2006

text: (OJ L 9.5.2006, p. 17).

text: Decision of the Management Board concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (“rulemaking procedure”), EASA MB/7/03, 27.6.2003. See: NPA No 03-2006 See: CRD No 03-2006

identifier: AMC & GM to Part-66 — Issue 1, Amendment 2

beslut: ED Decision 2006/006/R

publisher: Europeiska unionens byrå för luftfartssäkerhet

sprak: en

serie: amc-gm

text: ED Decision 2006/06/R 31/07/2006

type: stycke

text: European Aviation Safety Agency

text: DECISION No 2006/06/R OF THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY of 31-07-2006 amending Decision No 2005/07/R of 19 December 2005 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to

text: Regulation (EC) No 1592/2002

text: of the European Parliament and of the Council of 15 July 2002 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency (hereinafter referred to as the Basic Regulation), and in particular Articles

text: and

text: thereof. Having regard to the

text: Commission Regulation (EC) No 2042/2003 of 20 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks . Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part- 66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered a permanent rulemaking task for European Aviation Safety Agency (hereinafter referred to as the “Agency”). This decision represents the second update according to an accelerated procedure accepted by AGNA and SSCC. The consultation period has been reduced to 6 weeks and no regulatory impact assessment has or will be carried out. This Agency Decision is published together with the CRD.

text: ED Decision 2006/06/R 31/07/2006 (4) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance, as well as any guidance material for the application of the Basic Regulation and its implementing rules. (5) The Agency, pursuant to Article 43 of the Basic Regulation and Articles

text: and

text: 4 6 of the rulemaking procedure , has widely consulted interested parties on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received .

text: HAS DECIDED:

text: Article 1

text: Decision N° 2005/07/R is amended by this decision.

text: Article 2

text: This Decision shall enter into force on 7 August 2006. Done at Cologne, 31 July 2006 P. GOUDOU

text: ED Decision 2006/06/R 31/07/2006

text: Annex I APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE The following aircraft type ratings should be used to ensure a common standard throughout the Member States. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under Regulation 1702/2003 , this list being only intended for the purpose of maintenance. In order to keep this list current and type ratings consistent, where a Member State needs to issue a type rating that is not included in this list, such information should be first passed on to the Agency. 1. Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg, requiring type training and individual type rating.

text: Aerospaceline Guppy (RR Corp 501) Airbus A380 (RR Corp Trent 900) Airbus Beluga (GE CF6) Aerospatiale N262 (Turbomeca Bastan) Aerospatiale SN601 (PWC JT15D) Antonov AN12 (Ivchenko AI-20K) Antonov AN22 (Kusnetsov NK-12MA) Airbus A300 B2/B4 (GE CF6) Antonov AN24 (Ivchenko AI-24A) Airbus A300 B2/B4 (PW 4000) Antonov AN26 (Ivchenko AI-24T) Airbus A300 B2/B4 (PW JT9D) Antonov AN28 (Glushenkov TVD-10V) Airbus A300-600 (GE CF6) Antonov AN32 (Ivchenko AI-20M) Airbus A300-600 (PW 4000) Antonov AN38 (Honeywell TPE 331) Airbus A300-600 (PW JT9D) Antonov AN72 (Lotarev D-36) Airbus A310 (GE CF6) Antonov AN124 (Lotarev D-18T) Airbus A310 (PW 4000) Airbus A310 (PW JT9D) ATR 42 Non PEC (PWC 120) Airbus A318 (PW 6000) ATR 72 Non PEC (PWC 120) Airbus A318/A319/A320/A321 (CFM56) ATR 42/72 PEC (PWC 120) Airbus A319/A320/A321 (IAE V2500) Airbus A330 (GE CF6) BAe 1-11 (RRD Spey) Airbus A330 (PW 4000) Bae 125 (Honeywell TFE 731) Airbus A330 (RR Corp Trent 700) Bae 125 (RR Corp Viper) Airbus A340 (CFM56) BAe 146 / RJ (HoneywellAvco-Lyc ALF 500 Airbus A340 (RR Corp Trent 500) Series)

text: Commission Regulation (EC) No 1702/2003 of 24 September 2003

text: laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (OJ L 243, 27.9.2003, p. 6). Regulation as last amended by

text: Regulation (EC) No 706/2006

text: (OJ L 122, 9.5.2006, p. 16).

text: ED Decision 2006/06/R 31/07/2006

text: BAe 748 (RRD Dart) Bae 125 / Hawker 1000 (PWC 305) Casa 212 (Honeywell TPE331) BAe ATP (PWC 120) Casa 235 (GE CT7) BAe Jetstream 31/32 (Honeywell TPE 331) BAe Jetstream 41 (Honeywell TPE 331) Cessna 525/525A 525B (Williams FJ 44) Cessna 550/560 (PWC 530/535) Beech 200CT (PWC PT6) Cessna 550/560 (PWC JT15D) Beech 300 / 350 (PWC PT6) Cessna 560XL (PWC 545) Beech 350 (PWC PT6) Cessna 650 (Honeywell TFE731) Beech 400 (PWC JT15) Cessna 680 (PWC 306) Beech 1900 (PWC PT6) Cessna 750 (RR Corp AE3007C)

text: Boeing B 707/720 (PW JT3D) Consolidated PBY-5A (PW R1830) Boeing B 717-200 (RRD BR715) Boeing B 727 (PW JT8D) Convair 440 (PW R2800) Boeing B 727 (RRD Tay) Convair 540/580 (RR Corp 501) Boeing B 737-100/200 (PW JT8D) Convair 600/640 (RRD Dart) Boeing B 737-300/400/500 (CFM56) Boeing B 737-600/700/800/900 (CFM56) Dassault Falcon 10/100 (Honeywell TFE731) Boeing 737-900 (CFM56) Dassault Falcon (Honeywell CF700) Boeing B 747-100 (GE CF6) Dassault Falcon Series C,D,E,F (Honeywell Boeing B 747-100 (PW JT9D) CF700) Boeing B 747-100 (RR Corp RB211) Dassault Falcon Series G (Honeywell ATF 3) Boeing B 747-200/300 (GE CF6) Dassault Falcon 20 (Honeywell TFE731 GE Boeing B 747-200/300 (PW JT9D) CF700) Boeing B 747-200/300 (RR Corp RB211) Dassault Falcon 20-5 (GE CF700 Honeywell Boeing B 747-400 (GE CF6) TFE 731) Boeing B 747-400 (PW 4000) Dassault Falcon 50B (Honeywell TFE731) Boeing B 747-400 (RR Corp RB211) Dassault Falcon 50EX (Honeywell TFE731) Boeing B 747SP (PW JT9D) Dassault Falcon 200 (Honeywell ATF 3-6) Boeing B 747SP (RR Corp RB211) Dassault Falcon 900B (Honeywell TFE731) Boeing B 757-200/300 (PW 2000) Dassault Falcon 900C (Honeywell TFE731) Boeing B 757-200/300 (RR Corp RB211) Dassault Falcon 900EX (Honeywell TFE731) Boeing B 767-200/300 (PW 4000) Dassault Falcon 900EX EASy/DX (Honeywell Boeing B 767-200/300 (PW JT9D) TFE731) Boeing B 767-200/300 (RR Corp RB211) Dassault Falcon 2000 (Honeywell CFE 738) Boeing B 767-200/300/400 (GE CF6) Dassault Falcon 2000EX (PWC 308) Boeing 767-400 (GE CF6) Dassault Falcon 2000EX EASy (PWC 308) Boeing B 777-200/300 (GE 90) Boeing B 777-200/300 (PW 4000) Dornier DO 228 (Honeywell TPE 331) Boeing B 777-200/300 (RR Corp Trent 800) Dornier DO 328 (PWC 119) Boeing 777-300ER (GE 90) Dornier DO 328 (PWC 306)

text: Bombardier BD100-1A10 (Honeywell AS907) Embraer EMB 110 (PWC PT6) Bombardier BD700 Series-1A10 (RRD BR710) Embraer EMB 120 (PWC 118) Bombardier CL 600-1A11 (HoneywellAvco-Lyc Embraer EMB 135/145 (RR Corp AE3007A) ALF502) Embraer ERJ 170 100/200 (GE CF34) Bombardier CL 600-2A12 (GE CF34) Embraer ERJ 190 /195 (GE CF34) Bombardier CL 600-2B16 (GE CF34) Bombardier CL 600-2B19 (GE CF34) Fairchild SA 226/227 (Honeywell TPE331) Bombardier CL 600-2C10 (GE CF34) Fairchild SA 227 Metro III (PWC PT6) Bombardier CL 600-2D24 (GE CF34) Bombardier DHC-7 (PWC PT6) Fokker F27 Series/Maryland aircraft Industries Bombardier DHC-8-100/200/300 (PWC 120) F-27/FH227 Series (RRD Dart) Bombardier DHC-8-400 (PWC 150) Fokker F28 Series (RRD Spey) Fokker F50 (PWC 125) Bombardier (Canadair) CL 215 (PW R2800) Fokker F70/100 (RRD Corp Tay) Bombardier (Canadair) CL 415 (PWC 123) Fokker VFW 614 (RR Corp M45H)

text: ED Decision 2006/06/R 31/07/2006

text: Fokker VFW 614 Attlas (RR Corp M45H) McD DC3 (PW R1830) McD DC4 (PW R2000) Gates Learjet 23 (GE CJ610) McD DC6 (PW R2800) Gates Learjet 24 (GE CJ610) McD DC7 (Wright R3350) Gates Learjet 25 (GE CJ610) McD DC8 (CFM56) Gates Learjet 31 (Honeywell TFE731) McD DC8 (PW JT3D) Gates Learjet 35 (Honeywell TFE731) McD DC8 (PW JT4) Gates Learjet 36 (Honeywell TFE731) McD DC8 (RR Corp Conway) Gates Learjet 45 (Honeywell TFE731) McD DC9 (PW JT8D) Gates Learjet 55 (Honeywell TFE731) McD DC10 (GE CF6) Gates Learjet 60 (PWC 305) McD DC10 (PW JT9D) McD MD11 (GE CF6) Gulfstream G100/Astra SPX (Honeywell McD MD11 (PW 4000) TFE731) McD MD80 Series (PW JT8D) Gulfstream G200/Galaxy (PWC 306) McD MD90 (IAE V2500) Gulfstream GI (RRD Dart) Gulfstream GII & GIII (RRD Spey) Mitsubishi MU-300 (PWC JT15) Gulfstream GIV/G300/G400 (RRD Corp Tay) Gulfstream GIV-X/G450 (RRD Corp Tay) PZL M 28 (PWC PT6) Gulfstream GV (RRD BR 710) Raytheon Bae 125 (Honeywell TFE 731) Gulfstream GV-SP/G500/G550 (RRD BR 710) Raytheon Bae 125 (RR Corp Viper) Raytheon Bae 125 / Hawker 1000 (PWC 305) IAI 1121/1123 (GE CJ610) Beech Raytheon (Beech) 200CT (PWC PT6) IAI 1124 (Honeywell TFE731) Beech Raytheon (Beech) 300 / 350 (PWC PT6) IAI 1125 (Honeywell TFE731) Beech Raytheon (Beech) 350 (PWC PT6) Beech Raytheon (Beech) 400 (PWC JT15) Ilyushin IL-14 (Shvetsov Ash-82T) Beech Raytheon (Beech) 1900 (PWC PT6) Ilyushin IL-18 (Ivchenko AI-20M) Ilyushin IL-62 (Kuznetsov NK-8-4) Rockwell Sabreliner (Honeywell TFE731) Ilyushin IL-62 (Soloviev D-30KU) Rockwell Sabreliner (GE CF700) Ilyushin IL-76 (Soloviev D-30KP) Rockwell Sabreliner (PW JT12) Ilyushin IL-86 (CFM56) Ilyushin IL-86 (Kuznetsov NK-86) Saab 340 (GE CT-7) Ilyushin IL-86 (Soloviev PS-90) Saab 2000 (RR Corp AE2100) Ilyushin IL-96 (Soloviev PS-90A) Ilyushin IL-96MK (PW 2037) Shorts 330/360 (PWC PT6) Ilyushin IL-114 (Klimov TV7) Ilyushin IL-114PC (PWC 127) Tupolev TU 134 (Soloviev D-30-II) AI (Let) L-410/L-420 (Walter M601) Tupolev TU 154 (Kusnetsov NK-8) Let L-610 (GE CT7) Tupolev TU 154 (Soloviev D-30KU) Tupolev TU 204 (Soloviev PS-90AT) Lockheed Jetstar (Honeywell TFE731) Tupolev TU 204 (RR RB211) Lockheed Jetstar (PW JT12) Lockheed L18 (Wright C1820) Yakovlev Yak-40 (Ivchenko AI-25) Lockheed L100 (RR Corp 501T56) Yakovlev Yak-42 (Lotarev D-36) Lockheed L188 (RR Corp 501) Lockheed L382 (RR Corp T56501) Lockheed L1011 (RR Corp RB211)

text: ED Decision 2006/06/R 31/07/2006

text: 2. Aeroplanes of 5700kg and below, requiring type training and individual type rating (A-tr).

text: Aero Ae-270 (PWC PT6) Piper PA 42 (Honeywell TPE331) Piper PA 42 (PWC PT6) Bombardier DHC-6 (PWC PT6) Piper PA 46-310P/-350P (PWC PT6) Piper PA 46-310P (Continental) Cessna 425 (PWC PT6) Piper PA 46-350P (Lycoming) Cessna 441 (Honeywell TPE331) Piper PA 46-500 Meridian (PWC PT6) Cessna 500/501/551 (PWC JT15D) Cessna 501/551 (PW JT15D) Beech Raytheon (Beech) 90 Series (PWC PT6) Cessna 525/525A525B (Williams FJ 44) Beech Raytheon (Beech) 200 Series (PWC PT6) Cessna/Reims F406 (PWC PT6) Raytheon (Beech) 99 (PWC PT6) Beech Raytheon (Beech) 99/100 Series (PWC Dornier DO228 (Honeywell TPE 331) PT6) Dornier Seastar CD2 (PWC PT6) Beech Raytheon (Beech) B100 (Honeywell TPE331) Embraer EMB 110 (PWC PT6) Raytheon 390 (Williams FJ44) Embraer EMB-121 (PWC PT6) Twin Commander Extra EA-400-500 (RR 250) (Gulfstream/Rockwell/Aerocommander) 680T/V/681/690/695 Series (Honeywell Gates Learjet 23 (GE CJ610) TPE331)

text: Piaggo P166 (Lycoming) Socata TBM 700/850 (PWC PT6) Piaggio P180 Avanti (PWC PT6)

text: Pilatus PC-12 (PWC PT6) Vulcan Air AP68TP Series (RR corp 250) Pilatus PC-12/45 (PWC PT6)

text: 3. Aeroplanes multiple turbine engines (AMTE) of 5700kg and below, eligible for to type examinations and manufacturer group ratings.

text: Aero Commander AC 69 (PWC PT6) GAF Nomad N24A (RR Corp 250)

text: Beech 65-90 (PWC PT6) Piaggio P-180 (PWC PT6) Beech 99 (PWC PT6) Piper PA-31T (PWC PT6) Britten Norman BN2T Islander (RR Corp 250) PZL M 28 (PWC PT6) Dornier DO 28D-6/128-6 (PWC PT6) Shorts SC7 Skyvan 3 Variant 100 (Honeywell Fairchild Swearingen SA 26-AT (Honeywell TPE331) TPE331)

text: Mitsubishi MU 2B (Honeywell TPE331)

text: ED Decision 2006/06/R 31/07/2006

text: 4. Aeroplanes single turbine engine (ASTE) of 5700kg and below, eligible for to type examinations and group ratings.

text: Aermacchi (Allison 250-B) Pilatus PC-6 (PWC PT6) Aero Vodochody Ae 270 (PWC PT6) Pilatus PC-6 (Lycoming GSO 480) / Pilatus PC-6 (Lycoming IGO 540) Bombardier DHC-2 (PWC PT6) Pilatus PC-6 (Turbomeca Astazou) Bombardier DHC-3 (PWC PT6) Pilatus PC-6 (Honeywell TPE331) Pilatus PC-7 (PWC PT6) Cessna 206/207 (RR Corp 250) Pilatus PC-9 (PWC PT6) Cessna 208 Series (PWC PT6)

text: Grob G 520 (Honeywell TPE331) SIAI-Marchetti SM1019 (RR Corp 250) Moravan Zlin Z-37T/137T (Walter M601) Ayres Thrush S2R-T Series (PWC PT 6) PAC 750XL (PT6A-34)

text: 5. Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible for to type examinations and group ratings.

text: Aero Ae-45/145 (Walter) Piper PA 23 Series (Lycoming) Piper PA 30 (Lycoming) Aero Commander AC 50 (Lycoming) Piper PA 31 (Lycoming) Aero Commander 680E (Lycoming) Piper PA 31P (Lycoming) Aerostar PA-60 series (Lycoming TIO-540) Piper PA 34 (Lycoming) AI Aircraft Industries (Let) L 200 Series (LOM) Piper PA 34 (RR Continental) Piper PA 39 (Lycoming) Beech 55 (RR Continental) Piper PA 44 Series (Lycoming) Beech 58 (RR Continental) Piper Aerostar PA 60 Series (Lycoming) Beech 58P (RR Continental) Beech 60 (Lycoming) Beech Raytheon (Beech) 55 (RR Continental) Beech 65-80 (Lycoming) Beech Raytheon (Beech) 58 (RR Continental) Beech 76 (Lycoming) Beech Raytheon (Beech) 58P (RR Continental) Beech 95 Series (Lycoming) Beech Raytheon (Beech) 60 (Lycoming) Beech 95 Series (RR Continental) Beech Raytheon (Beech) 65-80 (Lycoming) Beech Raytheon (Beech) 76 (Lycoming) Britten Norman BN2 Islander (Lycoming) Beech Raytheon (Beech) 95 Series (Lycoming) Britten Norman BN2A Trislander (Lycoming) Beech Raytheon (Beech) 95 Series (RR Continental) Cessna 305 Series (Continental) Cessna 310 Series (RR Continental) Rockwell 500S Shrike Commander (Lycoming) Cessna 335 (RR Continental) Rockwell (Aero) Commander 680/680E/720 Cessna 337 (RR Continental) (Lycoming) Cessna 340 (RR Continental) Rockwell Commander (Gulfstream/Rockwell/ Cessna 401/402 (RR Continental) Aerocommander) 685 (Lycoming Continental) Cessna 404 (RR Continental) Twin Commander (Gulfstream/Rockwell/ Cessna 414 (RR Continental) Aerocommander) 500 Series/680 (Lycoming) Cessna 421 (RR Continental) Cessna T303 (RR Continental) Cessna T337 (RR Continental) Partenavia Vulcan Air P68 Series (Lycoming) Consolidated PBY-5A (PW R1830) Vulcan Air AP68TP Series (RR Corp 250) Grumman American GA-7 (Lycoming) (Detroit Diesel)

text: ED Decision 2006/06/R 31/07/2006

text: 6. Aeroplane single piston engine – metal structure (ASPE-MS), eligible for to type examinations and group ratings.

text: Aero AT-3 (Rotax) Cessna 185 Series (RR Continental) Cessna 188 (Continental) Aermacchi F260 (Lycoming) Cessna 195 (Jacobs) Cessna 206 Series (RR Continental) AI (Let) Z-37 (Avia) Cessna 207 Series (RR Continental) Cessna 210-P210 Series (RR Continental) American AA-1/-1A (Lycoming) Cessna P210N (RR Continental) American AA-1A (Lycoming) Cessna 305 Series (Continental) American AA-5/-5B (Lycoming) Cessna 336 (RR Continental) American AG-5B (Lycoming) Christen A1 Husky (Lycoming) Antonov AN2 (Shvecov) Evektor EV-97 (Rotax) Apex Aircraft (Robin) HR 100 series (Lycoming) Fuji FA-200 Series (Lycoming) Apex Aircraft (Robin) HR 100 series (Continental) Gippsland GA8 (Lycoming) Apex R1180 Series (Lycoming) Apex Aircraft (Robin) HR200/ R 2000 series Maule M4 (RR Continental) (Lycoming) Maule M5-180C (Lycoming) Apex Aircraft (Robin) R 3000 series (Lycoming) Maule M5-235C (Lycoming) Maule M6-235 (Lycoming) ARV 1 Super 2 (Hewland) Maule M7 Series (Lycoming) Maule MX-7-180 (Lycoming) Beech Raytheon (Beech) 23 Series (Lycoming) Beech Raytheon (Beech) A23 (RR Continental) Meteor FL53 (Continental) Beech Raytheon (Beech) 24 Series (Lycoming) Meteor FL 54 (Continental) Beech Raytheon (Beech) 33 Series (RR Meteor FL 55 (Lycoming) Continental) Beech Raytheon (Beech) 35 Series (RR Mooney M20 (Lycoming) Continental) Mooney M20 (Lycoming / RR Continental) Beech Raytheon (Beech) 36 (RR Continental) Morane Saulnier MS 892 (Lycoming) Bölkow BO 207 (RR Morane Saulnier MS 893 (Lycoming) Bölkow BO 208 (RR Continental) Morane Saulnier MS 894 (Franklin) Bölkow BO 209 (Lycoming) Morane Saulnier Rallye 100 (RR Continental) Morane Saulnier Rallye 110ST (Lycoming) Bombardier DHC-2 (PW) Morane Saulnier Rallye 150 (Lycoming) Bombardier DHC-3 (PW) Morane Saulnier Rallye 180T (Lycoming) Morane Saulnier Rallye 235E (Lycoming) Cessna 120 (RR Continental) Cessna 140 Series (RR Continental) Moravan (Zlin) Z-42/142 (Walter) Cessna 150 Series (RR Continental) Moravan (Zlin) Z-43 (Walter) Cessna 152 (Lycoming) Moravan (Zlin) Z-50 (Walter) Cessna 170 Series (RR Continental) Moravan (Zlin) Z-50L (Lycoming) Cessna 172 Series (Lycoming) Moravan (Zlin) Z-126/226 (Walter) Cessna 172 Series (RR Continental) Moravan (Zlin) Z-142 (Walter) Cessna 172 Series (Thielert) Moravan (Zlin) Z-143 L (Lycoming) Cessna 175 Series (Lycoming) Moravan (Zlin) Z-326/526/726 (Walter) Cessna 175 Series (RR Continental) Moravan (Zlin) Z-326 L (Lycoming) Cessna 177 Series (Lycoming) Moravan (Zlin) Z-242 L (Lycoming) Cessna 180 Series (RR Continental) Moravan (Zlin) Z-526FL (Walter Lycoming) Cessna 182 Series (Lycoming) Cessna 182 Series (RR Continental) Nardi FN333 (Continental) Cessna 182 Series (SMA)

text: ED Decision 2006/06/R 31/07/2006

text: Piaggo P 149 D (Lycoming) SAI OMF-100-160 (Lycoming) Pilatus PC-6 (Lycoming) GSO 480) / Pilatus PC- 6 (Lycoming IGO 540) SIAI-Marchetti S205 (Lycoming) SIAI-Marchetti S208 (Lycoming) Piper PA-16 Series (Lycoming) Piper PA-18 (RR Continental) SOCATA (Morane Saulnier) MS 892 Piper PA-18 Series (Lycoming) (Lycoming) Piper PA-20 Series (Lycoming) SOCATA (Morane Saulnier) MS 893 Piper PA-22 Series (Lycoming) (Lycoming) Piper PA-24 Series (Lycoming) SOCATA (Morane Saulnier) MS 894 (Franklin) Piper PA-25 Series (Lycoming) SOCATA (Morane Saulnier) Rallye 100 (RR Piper PA-28 Series (Lycoming) Continental) Piper PA-28 Series (RR Continental) SOCATA (Morane Saulnier) Rallye 110ST Piper PA-28-201T (RR Continental) (Lycoming) Piper PA-28 Series (TAE) SOCATA (Morane Saulnier) Rallye 150 Piper PA-32 Series (Lycoming) (Lycoming) Piper PA-38 Series (Lycoming) SOCATA (Morane Saulnier) Rallye 180T Piper PA-46 (Continental) (Lycoming) Piper PA-46 (Lycoming) SOCATA (Morane Saulnier) Rallye 235E (Lycoming) SOCATA TB9 (Lycoming) PZL-104 Wilga Series (PZL / Lycoming) SOCATA TB10 (Lycoming) PZL M 18 (PZL) SOCATA TB20 (Lycoming) PZL M 26 (Lycoming) SOCATA TB21 (Lycoming) SOCATA TB200 (Lycoming) Republic RC-3 (Lycoming) Symphony OMF-100-160 (Lycoming) Rockwell Commander 112 (Lycoming) Tecnam P92 (Rotax) Rockwell Commander 114 (Lycoming) Tecnam P2002 (Rotax) Saab 91A (Gypsy Major Lycoming) Thrush S2R (PW R-985) Saab 91B/C/D (Lycoming) Saab 91C (Lycoming) Saab 91D (Lycoming)

text: 7. Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for to type examinations and group ratings. 8. Aeroplane single piston engine – wooden structure (ASPE-WS), eligible for to type examinations and group ratings.

text: Apex Aircraft Cap 10 (Lycoming) Bellanca (Champion) 8 Series (Lycoming) Apex Aircraft HR 100 series (Lycoming) Boeing A75 series (Lycoming) Apex Aircraft HR 100 series (Continental) Boeing A75 series (Continental) Apex Aircraft (Robin) DR 300 series (Lycoming) Boeing A75 series (Jacobs) Apex Aircraft (Robin) DR 400 series (Lycoming) Boeing IB75 series (Pratt & Whitney) Apex Aircraft (Robin) R 1180 series (Lycoming) Aviamilano P.19 (RR Continental) Bölkow (Klemm) BO 2078 (Continental)

text: Bellanca 17-30A (RR Continental) CAP 10 (Lycoming) Bellanca (Champion) 7 Series (Lycoming)

text: ED Decision 2006/06/R 31/07/2006

text: Champion 7 Series (Continental) Piper PA-12 (Lycoming) Champion 7 Series (Lycoming) Piper PA-15 (RR Continental) Champion 8 Series (Lycoming) Partenavia P-64 (Lycoming) Christen A1 Husky (Lycoming) Partenavia P-66 (Lycoming) Jodel D 11 (Salmson) Jodel D 11 (Continental) Pitts S-1 Series (Lycoming) Jodel D 112 Series /D 127 (Continental) Pitts S-2 Series (Lycoming)

text: Slingsby T67A (Lycoming) Emeraude Scintex CP301 (Continental) Nipper T-66 (STARK) Waco YMF (Jacobs) Piper J3C (Continental) Piper PA-11 (Continental)

text: 9. Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for to type examinations and group ratings.

text: Diamond DA42 (TAE)

text: 10. Aeroplane single piston engine – composite structure (ASPE-CS), eligible for to type examinations and group ratings.

text: Cirrus SR20 (Continental) General Avia F20 (Lycoming)

text: Diamond DA20/DV20 (Rotax) Diamond DA20 (RR Continental) Grob G115/120 Series (Lycoming) Diamond DA40 (Lycoming) Diamond DA40 D (TAE) III Sky Arrow 650/710 (Rotax) Diamond H36/HK36 variants (Rotax) Ruschmeyer R90-230RG (Lycoming) D4 Fascination (Rotax) Sukkoi Su-29/31 (MGA) Extra EA-300 (Lycoming) Extra EA-400 (RR Continental) Slingsby T67B Series Comp (Lycoming)

text: Agusta A109 Series (PWC 206/207) Bell 214 (GE CT7) Agusta A109 Series (RRC Corp 250) Bell 214 (Lycoming Honeywell T5508D) Agusta A109 (Turbomeca Arriel 1) Bell 214 (T700) Agusta A109 Series (Turbomeca Arrius 2) Bell 222 (RR Corp 250) Bell 222 (Lycoming Honeywell LTS 101) Agusta-Bell AB 139 (PWC PT6) Bell 230/430 (RR Corp 250) Agusta/Westland EH-101 (GE CT700) Agusta AS61N (GE CT58) Bell 412 (PWC PT6) Bell 427 (PWC PW207D) Bell 206LT (RR Corp 250) Bell 430 (RR Corp 250) Bell 212 (PWC PT6)

text: ED Decision 2006/06/R 31/07/2006

text: Boeing 107 (GE CT58) Kamov KA-27 (Isotov TV3) Boeing BV234 (Avco Lycoming Honeywell Kamov Ka 32 (Klimov) 5512) Kamov Ka-26D (Vedeneyev)

text: Ericson EAC S-64-F (PW JFTD12) MD 900 (PWC 206/207) MD 901 (Turbomeca Arrius 2) Eurocopter AS 321/330 (Turbomeca Turmo) MD 902 (PWC 206/207) MD 900/902 (PWC Eurocopter AS 321/330 (Turbomeca Turmo) 206/207) Eurocopter AS 332 L2 (Turbomeca Makila 1A2) Eurocopter AS 332C/C1,332L/L1 (Turbomeca Mil Mi-2 (PZL GTD-350 III/IV) Makila 1A) Mil Mi-6 (Soloviev D-25V) Eurocopter AS 355 (RR Corp 250) Mil Mi-8 (Isotov TV2) Eurocopter AS 355 (Turbomeca Arrius 1) Mil Mi-10 (Soloviev D-25V) Eurocopter AS 365 N (Turbomeca Arriel 1) Mil Mi-17 (Isotov TV3) Eurocopter AS 365 N1, N2, N3 (Turbomeca Mil Mi-26 (Lotarev D-136) Arriel 1) PZL W-3A/3AS Swidnik (Rzeszow PZL-10W) Eurocopter AS 365 N1, N2, N3 (Turbomeca PZL W-3AS Swidnik (Rzeszow PZL-10W) Arriel 2C) Sikorsky S61N (GE CT58) Eurocopter BO 105 Series (RR Corp 250) Sikorsky S64 (Erickson) (PW JTFD JFTD 12) Eurocopter EC 135 (Turbomeca Arrius 2B) Sikorsky S70 (GE CT700 CT7) Sikorsky S70 Eurocopter EC 135 (PWC 206) (GE T700) Eurocopter EC155 (Turbomeca Arriel 2) Sikorsky S76A (RR Corp 250) Eurocopter EC 225 (Turbomeca Makila 2A) Sikorsky S76A (Turbomeca Arriel 1) Eurocopter MBB-BK 117 A-1/-3/-4/-B-1/-2 Sikorsky S76B (PWC PT6) (Honeywell LTS 101) Sikorsky S76C (Turbomeca Arriel 1) Eurocopter MBB-BK 117 C1/C2 (Turbomeca Sikorsky S76C (Turbomeca Arriel 2) Arriel 1) Sikorsky S92A (GE CT7-8) Eurocopter MBB-BK 117 C2 (Turbomeca Arriel 1) Westland W30 (RR Corp Gem) Eurocopter SA 365 C Series (Turbomeca Arriel Westland Wessex (RR Corp Gnome) 1)

text: Kamov KA-25 (Glushenkov GTD-3BM)

text: 12. Helicopters – Single with turbine engine (HSTE), eligible for to type examinations and group ratings.

text: Agusta AB204/ AB 205 (Lycoming Honeywell Eurocopter AS 350 (Turbomeca Arriel 2B) T53) Eurocopter EC 120 (Turbomeca Arrius 2F) Agusta AB 206 RR Corp 250) Eurocopter EC 130 (Turbomeca Arriel 2B) Agusta A119 (PWC PT6) Eurocopter SA 315B (Turbomeca Artouste IIIB) Eurocopter SE313/SA318 (Turbomeca Astazou Bell 47 Soloy (RR Corp 250) Eurocopter SA 319 (Turbomeca Astazou XIVB) Bell 204/205 (Lycoming Honeywell T53) Eurocopter SA 341G (Turbomeca Astazou IIIA) Bell 206 (RR Corp 250) Eurocopter SA 341J (Turbomeca Astazou XIVH) Bell 407 (RR Corp 250) Eurocopter SA 342 J (Turbomeca Astazou XIV) Agusta/Bell 204/205 (Honeywell T53) Eurocopter SA 360 (Turbomeca Astazou Agusta/Bell 206 (RR Corp 250) XVIIIA) Agusta AB 412 (PTCT-3) Eurocopter SA 3180 (Turbomeca Astazou IIA) Eurocopter SE 313B(Turbomeca Artouste IIC) Eurocopter SE316B/SE316C (Turbomeca Enstrom 480 (RR Corp 250) Artouste IIIB)

text: Eurocopter AS 350 (Turbomeca Arriel 1) Kaman K-1200 (T53-17A-1) Kaman K-1200 (Honeywell T53)

text: ED Decision 2006/06/R 31/07/2006

text: Schweizer 269D (RR Corp 250) Kamov Ka 32 (Klimov) Sikorsky S55 (Wright Cyclone) McD 369 (RR Corp 250) Sikorsky S55T (Honeywell TSE 331) Sikorsky S58 (Wright Cyclone) NH 300 Series (Lycoming) Sikorsky S58T (PWC PT6) MD (NH)(AMD) 500N Series (RR Corp 250) MD 600N (RR Corp 250) Sud-Ouest SO 1221 (Turbomeca Palouste IV) MD 520N (RR Corp 250) Westland S55 (PW R1340) Westland S55 (RR Mil Mi-2 (PZL GTD-350 III/IV) Gnome)”

text: 13. Helicopters – Single with piston engines (HSPE), eligible for to type examinations and group ratings.

text: Bell/Agusta/Westland 47 (Lycoming) Hughes/Schweizer 269 (Lycoming) Bell/Agusta/Westland 47 (Franklin) Agusta Bell 102 (PW S1H4) Kamov Ka-26D (Vedeneyev)

text: Bölkow BO 208 (RR Continental) Robinson R22/R44 Series (Lycoming) Brantly B2 (Lycoming) Sikorsky S55 (Wright Cyclone) Enstrom F28/F280 (Lycoming) Sikorsky S58 (Wright Cyclone)

text: Hiller UH-12 (Lycoming) Schweizer 269D Series (Lycoming)


text: ED Decision 2007/003/R 13/03/2007

text: DECISION No 2007/003/R

text: OF THE EXECUTIVE DIRECTOR OF THE AGENCY

text: of 13 March 2007

text: amending Annex IV of Decision N° 2003/19/RM of the Executive Director of the Agency of 28 November 2003 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003 of 20 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.

text: THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY,

text: Having regard to

text: Regulation (EC) No 1592/2002

text: of the European Parliament and of the Council of 15 July 2002 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency (hereinafter referred to as the Basic Regulation), and in particular Articles

text: and

text: thereof,

text: Having regard to the

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks ,

text: (1) Annex IV of Acceptable Means of Compliance to Part-66 of Decision 2003/19/RM is required to be up to date to reflect the need of introducing the concept of Critical Design Control Configuration Limitations (CDCCL).

text: (2) To achieve this requirement the text of the Annex IV of Acceptable Means of Compliance to Part-66 of Decision 2003/19/RM should be amended accordingly.

text: (3) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance, as well as any guidance material for the application of the Basic Regulation and its implementing rules.

text: OJ L 240, 7.9.2002, p. 1. Regulation as last amended by

text: Regulation (EC) No 1701/2003

text: (OJ L 243, 27.9.2003, p. 5). OJ L 315, 28.11.2003, p. 1. Regulation as amended by

text: Regulation (EC) No 707/2006

text: (OJ L 122, 9.5.2006, p. 17).

text: (4) The Agency, pursuant to Article 43 of the Basic Regulation and Articles 5(3) and 6 of the rulemaking procedure , has widely consulted interested parties on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received .

text: HAS DECIDED:

text: Article 1

text: The Annex IV of Acceptable Means of Compliance to Part-66 of Decision

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks, is hereby amended in accordance with the Annex 1 to this Decision.

text: Article 2

text: This Decision shall enter into force on 20 March 2007.

text: Done in Cologne, 13 March 2007

text: P. GOUDOU By delegation C. PROBST

text: Decision of the Management Board concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (“rulemaking procedure”), EASA MB/7/03, 27.6.2003. See: NPA No 22-2005 See: CRD No 22-2005

identifier: AMC & GM to Part-66 — Issue 1, Amendment 3

beslut: ED Decision 2007/003/R

text: European Aviation Safety Agency

text: Annex 1 to Decision 2007/003/R

text: The following paragraphs of Annex IV to Decision 2003/19/RM AMC to Part-66 are amended as follows:

text: Insert a new paragraph to AMC 66.A.45(d) and correct numbering for incorrectly numbered paragraph:

text: AMC 66.A.45(d) Type/task training and ratings

text: 3. Theoretical and practical training should also take into account critical aspects such as Critical Design Configuration Control Limitations. EASA guidance is provided for training in Appendix IV to AMC to 66.A.45(d). 3. 4 4. 5 5. 6 A programme of structure on-job-training (OJT) may be prepared to satisfy the practical training requirement 5. 7 Before grant of the aircraft type, the applicant should be able to: 6. 8 Insert a new Appendix IV to AMC Part-66: Appendix IV to AMC to 66.A.45(d) Fuel Tank Safety training This appendix includes general instructions for providing training on Fuel Tank Safety issues.

text: 1. Level of training required by this Annex is only level 2. Level 2 Detailed training Objectives: The attendant should, after the completion of the training: 1. know the history and the theoretical and practical elements of the subject, have an overview of Special Federal Aviation Regulations (SFARs) from 14 CFR SFAR 88 of the FAA and of JAA TGL 47, be able to give a detailed description of the concept of CDCCL, Airworthiness Limitations Items (ALI) and using theoretical fundamentals and specific examples,

text: 2. have the capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner.

text: 3. have detailed information on how the above items affect the aircraft in the scope of the activity of the organisation or in the fleet.

text: 4. understand and carry out activities with the use of manufacturer and regulatory authority data providing instructions on design and maintenance, such as Service Bulletins, Airworthiness Directives, Aircraft Maintenance Manual, Component Maintenance Manual etc.

text: 5. use easily the manufacturer’s documentation from various sources and apply corrective action where appropriate.

text: 6. identify the components or parts or the aircraft subject to FTS from the manufacturer’s documentation, plan the action or apply a Service Bulletin and an Airworthiness Directive. Continuing training The interval between continuing training shall be established by the organisation employing such personnel, but should not exceed two years. The continuing training shall include knowledge on evolution of material, tools, documentation and manufacturer’s or competent authority’s directives.

text: 2. The personnel directly involved in Fuel Tank Safety (FTS) systems shall be qualified according to the following table: Organisation Personnel Level of Continuing knowledge training Part-66 licence holders in The airworthiness review staff as 2 Yes a continuing airworthiness required by M.A.707. management organisation Part-66 licence holders in Maintenance organisation support 2 Yes aircraft and component and certifying staff maintenance organisations

text: 3. General requirements The training for the personnel designated in table above has to be carried out before any airworthiness review certificate is issued or any maintenance task is certified on an aircraft or a component. The training should be made in appropriate facilities containing examples of components, systems and parts affected by FTS issues and having access to aircraft or component where typical examples of FTS issues can be shown. The use of pictures, films and practical examples of the maintenance on fuel tank system is recommended. The training shall include a representative number of repair and inspections as required by the maintenance programme showing the necessity of using the manufacturer’s data.

text: 4. Characteristics of the training The following characteristics shall be taken into consideration when the level 2 training programmes are being established: a) understanding of the background and concepts of fuel tank safety as developed during the last 10 years, and b) how in maintenance organisations mechanics can recognise, interpret and handle the improvements that have been made or are being made during fuel tank system maintenance, c) awareness of any hazards working on the Fuel System, and especially with a Flammability Reduction System using nitrogen. a), b) and c) should be introduced in the training programme addressing the following issues: i) The theoretical background behind the fuel tank safety: the explosions of mixtures of fuel and air, the behaviour of those mixtures in an aviation environment, the effects of temperature and pressure, energy needed for ignition etc, the ‘fire triangle’, - Explain 2 concepts to prevent explosions: (1) ignition source prevention and (2) flammability reduction, ii) The major accidents and accident investigations and their conclusions, iii) SFARs from 14 CFR SFAR 88 of the FAA and JAA Internal Policy INT POL 25/12: reason of these documents, and what was the ultimate goal, margins of fuel system safety improvements (from 10-6 to 10-9, in fact improvement by a factor 100- 1000, to identify unsafe conditions and to correct them, to systematically improve fuel tank maintenance), iv) Explain the concepts that are being used: the results of SFAR 88 of the FAA and JAA INT/POL 25/12: modifications, airworthiness limitations and CDCCL, v) Where relevant information can be found by the mechanics and how to use and interpret this information (maintenance manuals, component maintenance manuals) vi) Fuel Tank Safety and Maintenance: fuel tank entry and exit procedures, clean working environment, what is meant by configuration control, wire separation, bonding of components etc, vii) Flammability reduction systems: reason for their presence, their effects, the hazards of an FRS using nitrogen for maintenance, safety precautions in maintenance/working with an FRS, viii) recording maintenance actions, recording measures and results of inspections.


text: OF THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY

text: OJ L 315, 28.11.2003, p. 1. Regulation as last amended by

text: Regulation (EC) No 376/2007 of 30 March 2007

text: (OJ L 94, 4.4.2007, p. 18). OJ L 240, 7.9.2002, p. 1. Regulation as last amended by

text: Regulation (EC) No 334/2007

text: (OJ L 88, 29.3.2007, p. 39).

text: Decision of the Management Board concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (“rulemaking procedure”), EASA MB/7/03, 27.6.2003. See: NPA No 19-2006 See: CRD No 19-2006

text: Commission Regulation (EC) No 1702/2003 of 24 September 2003

text: laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (OJ L 243, 27.9.2003, p. 6). Regulation as last amended by

text: Regulation (EC) No 375/2007

text: (OJ L 94, 4.4.2007, p. 3).

identifier: AMC & GM to Part-66 — Issue 1, Amendment 4

beslut: ED Decision 2007/009/R

title: AMC & GM to Part-66 — Issue 1, Amendment 4

text: ED Decision 2007/009/R 25/04/2007

text: European Aviation Safety Agency

text: DECISION NO 2007/009/R OF 25 APRIL 2007 amending Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence to Annex IV Acceptable Means of Compliance to Part 66 of Decision No. 2003/19/RM of the Executive Director of the Agency of 28 November 2003 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003 of 20 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks and repealing Decision No 2006/06/R of the Executive Director of the European Aviation Safety Agency of 31 July 2006 amending Decision No 2005/07/R of 19 December 2005 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to

text: Regulation (EC) No 1592/2002

text: of the European Parliament and of the Council of 15 July 2002 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency (hereinafter referred to as the Basic Regulation), and in particular Articles

text: and

text: thereof, Having regard to the

text: ED Decision 2007/009/R 25/04/2007

text: Whereas: (1) Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence to Annex IV Acceptable Means of Compliance to Part-66 of Decision No. 2003/19/RM (hereinafter referred to as Part-66 AMC Appendix 1) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered a permanent rulemaking task for the European Aviation Safety Agency (hereinafter referred to as the “Agency”). This decision represents the third amendment according to an accelerated procedure accepted by AGNA and SSCC. The consultation period has been reduced to 6 weeks and no regulatory impact assessment has been or will be carried out. This Agency Decision is published together with the CRD. (4) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance, as well as any guidance material for the application of the Basic Regulation and its implementing rules. (5) The Agency, pursuant to Article 43 of the Basic Regulation and Articles 5(3) and 6 of the rulemaking procedure , has widely consulted interested parties on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received . (6) Decision No 2006/06/R of the Executive Director of the European Aviation Safety Agency of 31 July 2006 should be repealed since it was erroneously issued as an amendment to Decision No 2005/07/R of 19 December 2005.

text: ED Decision 2007/009/R 25/04/2007 HAS DECIDED:

text: Article 1

text: Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence to Annex IV Acceptable Means of Compliance to Part-66 of Decision No 2003/19/RM is hereby amended by the Annex to this decision.

text: Article 2

text: Commission Regulation (EC) No 2042/2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks, is hereby repealed.

text: Article 3

text: This Decision shall enter into force on 2 May 2007. Done in Cologne on 25 April 2007 P. GOUDOU

text: ED Decision 2007/009/R 25/04/2007

text: Annex APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE

text: The following aircraft type ratings should be used to ensure a common standard throughout the Member States.

text: The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under Regulation 1702/2003 , this list being only intended for the purpose of maintenance.

text: In order to keep this list current and type ratings consistent, where a Member State needs to issue a type rating that is not included in this list, such information should be first passed on to the Agency.

text: ED Decision 2007/009/R 25/04/2007

text: 1. Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg, requiring type training and individual type rating

text: Boeing 737-100/200 (PW JT8D) Aerospatiale (Nord) 262 (Turbomeca Bastan) Boeing 737-300/400/500 (CFM56) Aerospatiale SN-601 (PWC JT15D) Boeing 737-600/700/800 (CFM56) Boeing 737-900 (CFM56) Airbus A300 B2/B4 (GE CF6) Boeing 747SR (GE CF6) Airbus A300 B2/B4 (PW 4000) Boeing 747-100 (GE CF6 RR RB211) Airbus A300 B2/B4 (PW JT9D) Boeing 747-100/747SR (PW JT9D) Airbus A300-600 (GE CF6) Boeing 747-200/300 (GE CF6) Airbus A300-600 (PW 4000) Boeing 747-200/300 (PW JT9D) Airbus A300-600 (PW JT9D) Boeing 747-200/300 (RR RB211) Airbus A310 (GE CF6) Boeing 747-400 (GE CF6) Airbus A310 (PW 4000) Boeing 747-400 (PW 4000) Airbus A310 (PW JT9D) Boeing 747-400 (RR RB211) Airbus A318 (PW 6000) Boeing 747SP (PW JT9D) Airbus A318/A319/A320/A321 (CFM56) Boeing 747SP (RR RB211) Airbus A319/A320/A321 (IAE V2500) Boeing 757-200/300 (PW 2000) Airbus A330 (GE CF6) Boeing 757-200/300 (RR RB211) Airbus A330 (PW 4000) Boeing 767-200/300 (PW 4000) Airbus A330 (RR Trent 700) Boeing 767-200/300 (PW JT9D) Airbus A340 (CFM56) Boeing 767-200/300 (RR RB211) Airbus A340 (RR Trent 500) Boeing 767-200/300/400ER (GE CF6) Airbus A380 (RR Trent 900) Boeing 767-400ER (GE CF6) Airbus A300-600ST Beluga (GE CF6) Boeing 777-200/300 (GE 90) Airbus UK (BAC) 1-11 (RRD Spey) Boeing 777-200/300 (PW 4000) Boeing 777-200/300 (RR Trent 800) Antonov AN12 (Ivchenko AI-20K) Antonov AN22 (Kusnetsov NK-12MA) Bombardier BD-100-1A10 (Honeywell AS907) Antonov AN24 (Ivchenko AI-24A) Bombardier BD-700 Series (RRD BR710) Antonov AN26 (Ivchenko AI-24) Bombardier CL-600-1A11 (Honeywell ALF502) Antonov AN28 (Glushenkov TVD-10V) Bombardier CL-600-2A12 (GE CF34) Antonov AN32 (Ivchenko AI-20M) Bombardier CL-600-2B16 (GE CF34) Antonov AN38 (Honeywell TPE331) Bombardier CL-600-2B19 (GE CF34) Antonov AN72 (Lotarev D-36) Bombardier CL-600-2C10 (GE CF34) Antonov AN124 (Lotarev D-18T) Bombardier CL 600-2D15 (GE CF34) Bombardier CL-600-2D24 (GE CF34) ATR 42 Non PEC (PWC 120) Bombardier DHC-7 (PWC PT6) ATR 72 Non PEC (PWC 120) Bombardier DHC-8-100/200/300 (PWC 120) ATR 42/72 PEC (PWC 120 Series) Bombardier DHC-8-400 (PWC 150)

text: BAe 1-11 (RRD Spey) Bombardier (Canadair) CL-215 (PW R2800) BAE Systems BAe 146/RJ (Honeywell ALF500 Bombardier (Canadair) CL-415 (PWC 123) Series) BAE Systems HS748 (RRD Dart) Casa C-212 (Honeywell TPE331) BAE Systems ATP/Jetstream 61 (PWC 120) Casa CN-235 (GE CT7) BAE Systems Jetstream 31/32 (Honeywell TPE331) Cessna 525B (Williams FJ 44) BAE Systems Jetstream 41 (Honeywell TPE331) Cessna 550/560 (PWC 530/535) Cessna 550/560 (PWC JT15D) Cessna 560XL (PWC 545) Boeing 707/720 (PW JT3D) Cessna 650 (Honeywell TFE731) Boeing 717-200 (RRD BR715) Cessna 680 (PWC 306) Boeing 727 (PW JT8D) Cessna 750 (RR Corp AE3007C) Boeing 727 (RRD Tay)

text: ED Decision 2007/009/R 25/04/2007

text: Consolidated PBY-5A (PW R1830) Gulfstream GIV-X/G450/G350 (RRD Tay) Gulfstream GV (RRD BR710) Kelowna (Convair) 440 (PW R2800) Gulfstream GV-SP/G500/G550 (RRD BR710) Kelowna (Convair) 580 (RR Corp 501) Kelowna (Convair) 600/640 (RRD Dart) IAI 1121/1123 (GE CJ610) IAI 1124 (Honeywell TFE731) Dassault Falcon 10/100 (Honeywell TFE731) IAI 1125 (Honeywell TFE731) Dassault Falcon 20 (GE CF700) Dassault Falcon 20-5 (Honeywell TFE731) Ilyushin IL-14 (Shvetsov Ash-82T) Dassault Falcon 50 (Honeywell TFE731) Ilyushin IL-18 (Ivchenko AI-20M) Dassault Falcon 50EX (Honeywell TFE731) Ilyushin IL-62 (Kuznetsov NK-8-4) Dassault Falcon 200 (Honeywell ATF 3-6) Ilyushin IL-62 (Soloviev D-30KU) Dassault Falcon 900B (Honeywell TFE731) Ilyushin IL-76 (Soloviev D-30KP) Dassault Falcon 900C (Honeywell TFE731) Ilyushin IL-86 (CFM56) Dassault Falcon 900EX (Honeywell TFE731) Ilyushin IL-86 (Kuznetsov NK-86) Dassault Falcon 900EX EASy/DX (Honeywell Ilyushin IL-86 (Soloviev PS-90) TFE731) Ilyushin IL-96 (Soloviev PS-90A) Dassault Falcon 2000 (Honeywell CFE 738) Ilyushin IL-96MK (PW 2037) Dassault Falcon 2000EX (PWC 308) Ilyushin IL-114 (Klimov TV7) Dassault Falcon 2000EX EASy (PWC 308) Ilyushin IL-114PC (PWC 127)

text: Dornier 228 (Honeywell TPE331) Aircraft Industries (Let) L-410/L-420 (Walter Dornier 328-100 (PWC 119) M601) Dornier 328-300 (PWC 306) Lockheed 1329 Jetstar (Honeywell TFE731) Embraer EMB-120 (PWC 118) Lockheed 1329 Jetstar (PW JT12) Embraer EMB-135/145 (RR Corp AE3007A) Lockheed L18 (Wright Cyclone C1820) Embraer ERJ-170/190 100/200 (GE CF34) Lockheed L100 (RR Corp 501) Embraer ERJ-190/195 (GE CF34) Lockheed L188 (RR Corp 501) Lockheed L382 (RR Corp T56 501) M7 Aerospace (Fairchild) SA226/SA227 Lockheed L-1011 (RR RB211) (Honeywell TPE331) M7 Aerospace (Fairchild) SA227 Metro III McD DC3 (PW R1830) (PWC PT6) McD DC-4 (PW R2000) McD DC-6 (PW R2800) Fokker F27 / Fairchild F-27/FH-227 (RRD Dart) McD DC-7 (Wright R3350) Fokker F28 Series (RRD Spey) McD DC-8-70 (CFM56) Fokker F50 (PWC 125/127) McD DC-8 (PW JT3D) Fokker F70/100 (RRD Tay) McD DC-8 (PW JT4) McD DC-8 (RR Conway) (Gates) Learjet 24 (GE CJ610) McD DC-9 (PW JT8D) (Gates) Learjet 24/25 (GE CJ610) McD DC-10/MD-10 (GE CF6) (Gates) Learjet 31 (Honeywell TFE731) McD DC-10 (PW JT9D) (Gates) Learjet 35 (Honeywell TFE731) McD MD-11 (GE CF6) (Gates) Learjet 35/36 (Honeywell TFE731) McD MD-11 (PW 4000) (Gates) Learjet 45 (Honeywell TFE731) McD MD-80 Series (PW JT8D) (Gates) Learjet 55 (Honeywell TFE731) McD MD-90 (IAE V2500) (Gates) Learjet 60 (PWC 305) PZL M 28 (PWC PT6) Gulfstream 100 / IAI 1125 / IAI Astra SPX (Honeywell TFE731) Raytheon (BAe) 125/Hawker 800/800XP/850XP Gulfstream (IAI) G150 (Honeywell TFE731) (Honeywell TFE731) Gulfstream (IAI) G200/Galaxy (PWC 306) Raytheon (BAe) 125 (RR Viper) Raytheon (BAe) 125 / Hawker 1000 (PWC 305) Gulfstream GI-159 (RRD Dart) Raytheon (Beech) 200CT (PWC PT6) Gulfstream GII & GIII G-1159 Series (RRD Raytheon (Beech) 300 (PWC PT6) Spey) Raytheon (Beech) 350 (PWC PT6) Gulfstream G-IV/G300/G400 (RRD Tay)

text: ED Decision 2007/009/R 25/04/2007

text: Raytheon (Beech) 400 / Mitsubishi MU-300 Tupolev TU 134 (Soloviev D-30-II) (PWC JT15) Tupolev TU 154 (Kusnetsov NK-8) Raytheon (Beech) 1900 (PWC PT6) Tupolev TU 154 (Soloviev D-30KU) Tupolev TU 204 (Soloviev PS-90AT) Sabreliner (Rockwell ) NA-265 (Honeywell Tupolev TU 204 (RR RB211) TFE731) Sabreliner (Rockwell ) NA-265 (GE CF700) Yakovlev Yak-40 (Ivchenko AI-25) Sabreliner (Rockwell ) NA-265 (PW JT12) Yakovlev Yak-42 (Lotarev D-36)

text: Saab (SF) 340 (GE CT7) Viking Air (De Havilland) DHC-7 (PWC PT6) Saab 2000 (RR Corp AE2100)

text: Shorts SD3 Series-30/SD3-60 (PWC PT6)

text: 2. Aeroplanes of 5700 kg and below, requiring type training and individual type rating (A-tr)

text: Aero Ae-270 (PWC PT6) Piper PA-42 (Honeywell TPE331) Piper PA-42 (PWC PT6) Bombardier DHC-6 (PWC PT6) Piper PA-46-310P (Continental) Piper PA-46-350P (Lycoming) Cessna P337 (Continental) Piper PA-46-500TP-Meridian (PWC PT6) Cessna 425 (PWC PT6) Cessna 441 (Honeywell TPE331) Raytheon (Beech) 90 Series (PWC PT6) Cessna 500 (PWC JT15D) Raytheon (Beech) 200 Series (PWC PT6) Cessna 501/551 (PWC JT15D) Raytheon (Beech) 99/100 Series (PWC PT6) Cessna 525/525A (Williams FJ 44) Raytheon (Beech) 100 Series (PWC PT6) Cessna/Reims F 406 (PWC PT6) Raytheon (Beech) B100 (Honeywell TPE331) Raytheon 390 (Williams FJ44) Dornier Seastar CD2 (PWC PT6) Twin Commander Embraer EMB-110 (PWC PT6) (Gulfstream/Rockwell/Aerocommander) Embraer EMB-121 (PWC PT6) 680/681/690/695 Series (Honeywell TPE331)

text: Extra EA-400-500 (RR Corp 250) Reims F406 (PWC PT6)

text: (Gates) Learjet 23 (GE CJ610) Socata TBM 700/850 (PWC PT6)

text: Mitsubishi MU-2B (Honeywell TPE331) Viking Air (De Havilland) DHC-6 (PWC PT6)

text: Piaggio P166 (Lycoming) Vulcanair AP.68TP Series (RR Corp 250) Piaggio P180 Avanti/Avanti II (PWC PT6)

text: Pilatus PC-12 (PWC PT6)

text: ED Decision 2007/009/R 25/04/2007

text: 3. Aeroplanes multiple turbine engines (AMTE) of 5700 kg and below, eligible for type examinations and manufacturer group ratings

text: ASTA (GAF) (Nomad)N24A (RR Corp 250) PZL M 28 (PWC PT6)

text: B-N Group (Britten-Norman) BN-2T (Islander) Shorts SC7 Skyvan 3 Variant 100 (Honeywell (RR Corp 250) TPE331)

text: Dornier DO 28D-6/128-6 (PWC PT6) Twin Commander (Gulfstream/Rockwell/ Aerocommander) 690 (Honeywell TPE 331) M7 Aerospace (Fairchild) SA26-AT (Honeywell TPE331)

text: Mitsubishi MU-2B (Honeywell TPE331)

text: Piper PA-31T (PWC PT6)

text: 4. Aeroplanes single turbine engine (ASTE) of 5700 kg and below, eligible for type examinations and group ratings

text: Aermacchi SF260TP (RR Corp 250) PAC 750XL (PWC PT6) Aero Vodochody Ae 270 (PWC PT6) Pilatus PC-6 (PWC PT6) Thrush (Ayres ) S2R-T Series (PWC PT6) Pilatus PC-6 (Turbomeca Astazou) Pilatus PC-6 (Honeywell TPE331) Bombardier DHC-2 (PWC PT6) Pilatus PC-7 (PWC PT6) Bombardier DHC-3 (PWC PT6) Pilatus PC-9 (PWC PT6)

text: Cessna (Soloy) 206/207 (RR Corp 250) Cessna 208 Series (PWC PT6) SIAI-Marchetti SM1019 (RR Corp 250) Grob G 520 (Honeywell TPE331) Viking Air DHC-2 (PWC PT6) Maule MX-7 (RR Corp 250) Viking Air DHC-3 (PWC PT6)

text: Moravan Zlin Z-37T/137T (Walter M601)

text: 5. Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible for type examinations and group ratings

text: Aermacchi AL60 (Continental) B-N Group (Britten-Norman) BN2 Islander Aermacchi AL60 (Lycoming) (Lycoming) B-N Group (Britten-Norman) BN2A Trislander Aero Ae-45/145 (LOM) (Lycoming)

text: Aero Commander AC 50 (Lycoming) Cessna 310 Series (Continental) Aircraft Industries (Let) L 200 Series (LOM) Cessna 335 (Continental) Cessna 337 (Continental) (not pressurised) Aerostar (Piper) PA-60 Series (Lycoming) Cessna 340 (Continental) Cessna 401/402 (Continental)

text: ED Decision 2007/009/R 25/04/2007

text: Cessna 404 (Continental) Raytheon (Beech) 58P (Continental) Cessna 414 (Continental) Raytheon (Beech) 60 (Lycoming) Cessna 421 (Continental) Raytheon (Beech) 65-80 (Lycoming) Cessna T303 (Continental) Raytheon (Beech) 76 (Lycoming) Cessna 337 (Continental) Raytheon (Beech) 95 Series (Lycoming) Raytheon (Beech) 95 Series (Continental) EADS Socata (Grumman) GA-7 (Lycoming) Grumman American GA-7 (Lycoming) STOL (Republic) UC-1 (Lycoming)

text: Piper PA-23 Series (Lycoming) Twin Rockwell Commander Piper PA-30 (Lycoming) (Gulfstream/Rockwell/ Aerocommander) 685 Piper PA-31 (Lycoming) (Continental) Piper PA-31P (Lycoming) Twin Commander (Gulfstream/Rockwell/ Piper PA-34 (Lycoming) Aerocommander) 500 Series/680 Series Piper PA-34 (RR Continental) (Lycoming) Piper PA-39 (Lycoming) Piper PA-44 Series (Lycoming) Piper Aerostar PA 60 Series (Lycoming) Vulcanair 68 P. Series (Lycoming) Vulcanair AP.68TP Series (RR Corp 250) Raytheon (Beech) 55 (Continental) Raytheon (Beech) 58 (Continental)

text: 6. Aeroplane single piston engine – metal structure (ASPE-MS), eligible for type examinations and group ratings

text: Aero AT-3 (Rotax) Bölkow BO 209 (Lycoming)

text: Aermacchi SF260 Series (Lycoming) Bombardier DHC-2 (PW) Bombardier DHC-3 (PW) Aircraft Industries (Let) Z-37 (LOM) Cessna 120 (Continental) American AA-1/-1A (Lycoming) Cessna 140 Series (Continental) American AA-5/-5B (Lycoming) Cessna 150 Series (Continental) Cessna 152 (Lycoming) Antonov AN2 (Shvetsov) Cessna 170 Series (Continental) Cessna 172 Series (Lycoming) APEX Apex Aircraft (Robin) HR 100 series Cessna 172 Series (Continental) (Lycoming) Cessna 172 Series (Thielert) APEX Apex Aircraft (Robin) HR 100 series Cessna 175 Series (Lycoming) (Continental) Cessna 175 Series (Continental) APEX Apex (Robin) R 1180 Series (Lycoming) Cessna 177 Series (Lycoming) Alpha Apex Aircraft (APEX/Robin) HR 200/ R Cessna 180 Series (Continental) 2000 series (Lycoming) Cessna 182 Series (Lycoming) APEX Apex Aircraft (Robin) R 3000 series Cessna 182 Series (Continental) (Lycoming) Cessna 182 Series (SMA) Cessna 185 Series (Continental) ARV 1 Super 2 (Hewland) Cessna 188 (Continental) Cessna 195 (Jacobs) Raytheon (Beech) 23 Series (Lycoming) Cessna 206 Series (Continental) Raytheon (Beech) A23 (Continental) Cessna 207 Series (Continental) Raytheon (Beech) 24 Series (Lycoming) Cessna 210/P210 Series (Continental) Raytheon (Beech) 33 Series (Continental) Regal Air (Cessna) 305 Series (Continental) Raytheon (Beech) 35 Series (Continental) Cessna 336 (Continental) Raytheon (Beech) 36 (Continental) Sky International (Christen/Aviat) A-1 Husky Bölkow BO 207 (Continental) (Lycoming) Bölkow BO 208 (Continental)

text: ED Decision 2007/009/R 25/04/2007

text: Evektor EV-97 (Rotax) PZL-101A Gawron (Ivchenko) Fuji FA-200 Series (Lycoming) PZL-104A Wilga (Ivchenko) PZL-104 Wilga Series (PZL) Gippsland GA8 (Lycoming) PZL M 18 (PZL) PZL M 26 (Lycoming) Lavia (Piper) PA-25 Series (Lycoming) PZL-104 Wilga (Lycoming)

text: Maule M4 (Continental) Maule M4 (Franklin) Sky Enterprises (Republic) RC-3 (Franklin Maule M5-180C (Lycoming) Lycoming)

text: Maule M5 (Franklin) M5 (Continental) CPAC, Inc (Rockwell/Commander) 112 Maule M5-235C (Lycoming) (Lycoming) Maule M6-235 (Lycoming) CPAC, Inc (Rockwell/Commander) 114 Maule M7 Series (Lycoming) (Lycoming)

text: Maule MX-7-180 (Lycoming) Saab 91A (Gypsy Major) Meteor FL53 (Continental) Saab 91 (Lycoming)

text: Meteor FL54 (Continental) Meteor FL55 (Lycoming) Symphony SAI OMF-100-160 (Lycoming)

text: Mooney M20B to M20S (Lycoming) SIAI-Marchetti S.205/S.208 (Lycoming) Mooney M20 (Continental) SIAI-Marchetti S.208 (Lycoming) SIAI-Marchetti S205 (Franklin)

text: Moravan Zlin Z-37T/137T (Walter M601) Moravan (Zlin) Z-42/142 (LOM) SOCATA (Morane Saulnier) MS 892 Moravan (Zlin) Z-43 (LOM) (Lycoming) Moravan (Zlin) Z-50 (LOM) SOCATA (Morane Saulnier) MS 893 (Lycoming) Moravan (Zlin) Z-50L (Lycoming) SOCATA (Morane Saulnier) MS 894 (Franklin) Moravan (Zlin) Z-126/226 (LOM) SOCATA (Morane Saulnier) Rallye 100 Moravan (Zlin) Z-143 L (Lycoming) (Continental) Moravan (Zlin) Z-326/526/726 (LOM) SOCATA (Morane Saulnier) Rallye 110ST Moravan (Zlin) Z-242 L (Lycoming) (Lycoming) Moravan (Zlin) Z-526L (Lycoming) SOCATA (Morane Saulnier) Rallye 150 (Lycoming) Nardi FN333 (Continental) SOCATA (Morane Saulnier) Rallye 180T (Lycoming) Partenavia P.64 (Lycoming) SOCATA (Morane Saulnier) Rallye 235E Partenavia P.66 (Lycoming) (Lycoming) SOCATA TB 9 (Lycoming) Piaggio P 149 D (Lycoming) SOCATA TB 10 (Lycoming) SOCATA TB 20 (Lycoming) Pilatus PC-6 (Lycoming) SOCATA TB 21 (Lycoming) SOCATA TB 200 (Lycoming) Piper PA-16 Series (Lycoming) Piper PA-18 (Continental) Tecnam P92 (Rotax) Piper PA-18 Series (Lycoming) Tecnam P96/P2002 (Rotax) Piper PA-20 Series (Lycoming) Piper PA-22 Series (Lycoming) Tiger (Grumman/American) AA-1/-1A Piper PA-24 Series (Lycoming) (Lycoming) Piper PA-25 Series (Lycoming) Tiger (Grumman/Amercian) AA-5/AG-5B Piper PA-28 Series (Lycoming) (Lycoming) Piper PA-28 Series (Continental) Piper PA-28 Series (Thielert) Thrush (Ayres) S2R (PW R-985) Piper PA-32 Series (Lycoming) Piper PA-38 Series (Lycoming) Yakovlev YAK-18T (Vedeneev) Piper PA-46 (Continental) Yakovlev YAK-50 (Vedeneev) Piper PA-46 (Lycoming) Yakovlev YAK-52 (Vedeneev)

text: ED Decision 2007/009/R 25/04/2007

text: Yakovlev YAK-55 (Vedeneev) Yakovlev YAK-12A/M (Ivchenko)

text: Viking Air (Bombardier) DHC-2 (PW R985) Viking Air (Bombardier) DHC-3 (PW R1340)

text: 7. Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for type examinations and group ratings 8. Aeroplane single piston engine – wooden structure (ASPE-WS), eligible for type examinations and group ratings

text: Alexandria Aircraft (Bellanca) 17-30A Jodel D 112 Series/D 127 (Continental) (Continental) Aircraft Industries L 200 Series (LOM) Scintex CP301 (Continental) APEX Apex Aircraft CAP 10 (Lycoming) APEX Apex Aircraft (Robin) DR 300 series Nipper T-66 (STARK) (Lycoming) APEX Apex Aircraft (Robin) DR 400 series Mooney M20/M20A (Lycoming) (Lycoming) APEX (Robin) DR 400RP (Porsche) Piper J3C (Continental) Piper PA-11 (Continental) Aviamilano P.19 (Continental) Piper PA-12 (Lycoming) Piper PA-15 (Continental) Bellanca 17-30A (Continental) Bellanca (Champion) 7 Series (Lycoming) Partenavia P.64 (Lycoming) Bellanca (Champion) 8 Series (Lycoming) Partenavia P.66 (Lycoming) Boeing A75 series (Lycoming) Boeing A75 series (Continental) Pitts S-1 Series (Lycoming) Boeing A75 series (Jacobs) Pitts S-2 Series (Lycoming) Boeing B75 series (Pratt & Whitney) Sky International (Pitts) S-1 Series (Lycoming) Bölkow (Klemm) BO207 K1.107/F.207 Sky International (Pitts) S-2 Series (Lycoming) (Continental) Bölkow F.207(Lycoming) Slingsby T67A (Lycoming)

text: Diamond DV22 (Rotax) Waco YMF (Jacobs)

text: Jodel D 11 (Salmson) Jodel D 11 (Continental)

text: 9. Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for type examinations and group ratings

text: Diamond DA42 (TAE Thielert)

text: ED Decision 2007/009/R 25/04/2007

text: 10. Aeroplane single piston engine – composite structure (ASPE-CS), eligible for type examinations and group ratings

text: Cirrus SR20 (Continental) Cirrus SR22 (Continental) Grob G115/120 Series (Lycoming) Diamond DA20/DV20 (Rotax) Diamond DA20 (Continental) III Sky Arrow 650/710 (Rotax) Diamond DA40 (Lycoming) Diamond DA40 D (TAE Thielert) Ruschmeyer R90-230RG (Lycoming) Diamond H36/HK36 variants (Rotax) Sukhoi SU-29 (Vedeneev) Aircraft Design (WD) D4 Fascination (Rotax) Sukhoi SU-31 (Vedeneev) Sukhoi SU-26 (Vedeneev) Extra EA-300 (Lycoming) Sukhoi Su-29/31 (MGA) Extra EA-400 (Continental) Slingsby T67B/T67C/T67M series (Lycoming) General Avia F.20/F.22 (Lycoming)

text: 11. Multi-engine helicopters (MEH), requiring type training and individual type rating

text: Agusta A109 Series (PWC 206/207) Eurocopter SA 365 N1, AS 365 N2 (Turbomeca Agusta A109 Series (RR Corp 250) Arriel 1) Agusta A109 (Turbomeca Arriel 1) Eurocopter AS 365 N3 (Turbomeca Arriel 2C) Agusta A109 Series (Turbomeca Arrius 2) Eurocopter BO 105 Series (RR Corp 250) Eurocopter EC 135 (Turbomeca Arrius 2B) Agusta-Bell Agusta AB139 / AW139 (PWC Eurocopter EC 135 (PWC 206) PT6) Eurocopter EC 155 (Turbomeca Arriel 2) Agusta/Westland EH-101 (GE CT700) Eurocopter EC 225 (Turbomeca Makila 2A) Agusta AS-61N (GE CT58) Eurocopter MBB-BK 117 A/B (Honeywell LTS 101) Bell 206LT (RR Corp 250) Eurocopter MBB-BK 117 C1 (Turbomeca Arriel Bell 212 / Agusta AB212 (PWC PT6) 1) Bell 214 (GE CT7) Eurocopter MBB-BK 117 C2 (Turbomeca Arriel Bell 214 (Honeywell T5508D) 1) Bell 222 (RR Corp 250) Eurocopter SA 365 C Series (Turbomeca Arriel Bell 222 (Honeywell LTS 101) 1) Bell 230 (RR Corp 250) Kamov KA-25 (Glushenkov GTD-3BM) Bell 412 / Agusta AB412 (PWC PT6) Kamov KA-27 (Isotov TV3) Bell 427 (PWC PW207D) Kamov Ka 32 (Klimov) Bell 430 (RR Corp 250) Kamov Ka-26D (Vedeneyev)

text: Boeing 107-II (GE CT58) MD Helicopters MD900 (Turbomeca Arrius 2) Boeing 234 (Honeywell 5512) MD Helicopters MD900 (PWC 206/207)

text: Eurocopter SA 321 (Turbomeca Turmo) Mil Mi-2 (PZL GTD-350 III/IV) Eurocopter SA 330 (Turbomeca Turmo) Mil Mi-6 (Soloviev D-25V) Eurocopter AS 332 L2 (Turbomeca Makila 1A2) Mil Mi-8 (Isotov TV2) Eurocopter AS 332C/C1/L/L1 (Turbomeca Mil Mi-10 (Soloviev D-25V) Makila 1A) Mil Mi-17 (Isotov TV3) Eurocopter AS 355 (RR Corp 250) Mil Mi-26 (Lotarev D-136) Eurocopter AS 355 (Turbomeca Arrius 1) Eurocopter SA 365 N (Turbomeca Arriel 1)

text: ED Decision 2007/009/R 25/04/2007

text: PZL-Swidnik W-3A/W-3AS (Rzeszow PZL- Sikorsky S-76C (Turbomeca Arriel 2) 10W) Sikorsky S-92A (GE CT7-8) PZL Kania (RR Corp 250) Westland W30 (RR Gem) Sikorsky S-61N (GE CT58) Westland Wessex (RR Gnome) Erickson (Sikorsky) S-64 (PW JFTD 12) Sikorsky S-70 (GE T700) Sikorsky S-76A (RR Corp 250) Sikorsky S-76A (Turbomeca Arriel 1) Sikorsky S-76B (PWC PT6) Sikorsky S-76C (Turbomeca Arriel 1)

text: 12. Helicopters – Single turbine engine (HSTE), eligible for type examinations and group ratings

text: Agusta A119 (PWC PT6) MD (NH)(AMD)500 Series MD Helicopters (Hughes) 369 series (RR Corp Bell (Soloy) 47 (RR Corp 250) 250) Bell 407 (RR Corp 250) MD 600N (RR Corp 250) Agusta AB204, AB205 / Bell 204, 205 MD 500N (RR Corp 250) (Honeywell T53) Agusta AB206 / Bell 206 (RR Corp 250) Schweizer 269D (RR Corp 250) Agusta AB 412 (PTCT-3) Sikorsky S-55T (Honeywell TSE331) Sikorsky S-58T (PWC PT6) Enstrom 480 (RR Corp 250) Sud-Ouest SO 1221 (Turbomeca Palouste IV) Eurocopter AS 350 (Turbomeca Arriel 1) Eurocopter AS 350 (Turbomeca Arriel 2B) Westland WS-55 (RR Gnome) Eurocopter EC 120 (Turbomeca Arrius 2F) Eurocopter EC 130 (Turbomeca Arriel 2B) Eurocopter SA 315B (Turbomeca Artouste) Eurocopter SE 313/SA 318(Turbomeca Astazou) Eurocopter SA 319 (Turbomeca Astazou XIV) Eurocopter SA 341 (Turbomeca Astazou) Eurocopter SA 342 J (Turbomeca Astazou XIV) Eurocopter SA 360 (Turbomeca Astazou XVIIIA) Eurocopter SE 313 B (Turbomeca Artouste) Eurocopter SA 316 B/SA 316 C (Turbomeca Artouste)

text: Kaman K-1200 (Honeywell T5317)

text: NH-300 Series (Lycoming)

text: ED Decision 2007/009/R 25/04/2007

text: 13. Helicopters – Single piston engines (HSPE), eligible for type examinations and group ratings

text: Bell/Agusta/Westland 47 (Lycoming) Schweizer (Hughes) 269 (Lycoming) Bell /Agusta/Westland 47 (Franklin) Agusta Bell AB-102 (PW S1H4) Robinson R22/R44 Series (Lycoming)

text: Bölkow BO 208 (RR Continental) SEI (Breda-Nardi) NH-300 Series (Lycoming)

text: Brantly B2 (Lycoming) Sikorsky S-55 (Wright Cyclone) Sikorsky S-58 (Wright Cyclone) Enstrom

text: (Lycoming) Schweizer 269 Series (Lycoming) Hiller UH-12 (Lycoming)


text: OF THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY

text: OF 18 DECEMBER 2007

text: AMENDING THE ANNEXES IV AND V TO DECISION NO 2003/19/RM OF THE EXECUTIVE DIRECTOR OF THE AGENCY OF 8 NOVEMBER 2003 ON ACCEPTABLE MEANS OF COMPLIANCE AND GUIDANCE MATERIAL TO COMMISSION REGULATION (EC) NO 2042/2003 OF 20 NOVEMBER 2003 ON THE CONTINUING AIRWORTHINESS OF AIRCRAFT AND AERONAUTICAL PRODUCTS, PARTS AND APPLIANCES, AND ON THE

text: APPROVAL OF ORGANISATIONS AND PERSONNEL INVOLVED IN THESE TASKS

text: “RE-ISSUANCE OF THE PART-66 AIRCRAFT MAINTENANCE LICENCE”

text: OJ L 240, 7.9.2002, p. 1. Regulation as last amended by

text: Commission Regulation (EC) No 334/2007

text: (OJ L 88, 29.3.2007, p. 39). 2 OJ L 315, 28.11.2003, p. 1. Regulation as last amended by

text: Commission Regulation (EC) No 376/2007

text: (OJ L 94, 4.4.2007, p. 18). 3 Management Board Decision concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (“Rulemaking Procedure”), EASA MB/08/07, 13.6.2007. 4 NPA 2007-04 is available at http://www.easa.europa.eu/home/r_archives.html 5 CRD 2007-04 is available at http://www.easa.europa.eu/home/r_archives.html

identifier: AMC & GM to Part-66 — Issue 1, Amendment 5

beslut: ED Decision 2007/018/R

text: ED Decision 2007/018/R 18 Dec 2007

text: European Aviation Safety Agency

text: DECISION NO 2007/018/R

text: THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY,

text: Having regard to the

text: Regulation (EC) No 1592/2002

text: of the European Parliament and of the Council of 15 July 2002 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency (hereinafter “The Basic Regulation”), and in particular Articles

text: and

text: thereof,

text: Having regard to the

text: Commission Regulation (EC) No 2042/2003 of 20 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks ,

text: Whereas:

text: (1) It is necessary to update Decision No 2003/19/RM of the Executive Director of the Agency of 28 November 2003 by revising the existing and including new AMCs and GM. (2) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance, as well as any guidance material for the application of the Basic Regulation and its implementing rules.

text: (3) The Agency, pursuant to

text: Article 43.1

text: (c) of the Basic Regulation and articles 5(3) and 6 of the EASA Rulemaking Procedure , has widely consulted interested parties (see: NPA 2007-04 ) on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received (see: CRD No 2007-04 ).

text: ED Decision 2007/018/R 18 Dec 2007 HAS DECIDED:

text: Article 1

text: Annexes IV and V to Decision No 2003/19/RM of the Executive Director of the Agency of the Executive Director of the Agency of 28 November 2003 on acceptable means of compliance and guidance material to

text: are hereby amended in accordance with Annex 1 to this Decision.

text: Article 2

text: This decision shall enter into force on 25 December 2007. It shall be published in the Official Publication of the Agency.

text: Done in Cologne, 18 December 2007

text: P. GOUDOU

text: ED Decision 2007/018/R 18 Dec 2007

text: Annex 1

text: In Annex IV to Decision No 2003/19/RM:

text: The paragraph AMC to 66.A.20(b)2 is modified as follows:

text: AMC 66.A.20 (b) 2 Privileges

text: The required 6-month experience should be on aircraft structure, powerplant and systems as appropriate to the category or subcategory and relevant to the type or group rating held. Experience should be supported by documentary evidence.

text: The 6 months maintenance experience in 2 years should be understood as consisting of two elements, duration and nature of the experience. The minimum to meet the requirements for these elements may vary depending on the size and complexity of the aircraft and type of operation and maintenance.

text: 1. Duration: Within an approved maintenance organization: - 6 months continuous employment within the same organisation; or - 6 months split up into different blocks, employed within the same or in different organisations.

text: The 6 months period can be replaced by 100 days of maintenance experience in accordance with the privileges, whether they have been performed within an approved organisation or as independent certifying staff according to M.A.801(b)2 or as a combination here of.

text: When certifying staff maintains and releases aircraft in accordance with M.A.801(b)2, in certain circumstances this number of days may even be reduced by 50% when agreed in advance by the competent authority. These circumstances consider the cases where the holder of a Part-66 licence happens to be the owner of an aircraft and carries out maintenance on his own aircraft, or where a licence holder maintains an aircraft operated for low utilization, that does not allow the licence holder to accumulate the required experience. This reduction should not be combined with the 20% reduction permitted when carrying out technical support, or maintenance planning, continuing airworthiness management or engineering activities. To avoid a too long period without experience, the working days should be spread over the intended 6 months period.

text: 2. Nature of the experience:

text: Depending on the category of the aircraft maintenance licence, the following activities are considered relevant for maintenance experience: - Servicing; - Inspection; - Operational and functional testing; - Trouble-shooting; - Repairing; - Modifying; - Changing component; - Supervising these activities; - Releasing aircraft to service.

text: For category A certifying staff, the experience should include exercising the privileges, by means of performing tasks related to the authorization on at least one aircraft type for each

text: ED Decision 2007/018/R 18 Dec 2007

text: licence subcategory. This means tasks as mentioned in AMC 145.A.30(g), including servicing, component changes and simple defect rectifications.

text: For category B1 and B2, for every aircraft included in the authorization the experience should be on that particular aircraft or on a similar aircraft within the same licence subcategory. Two aircraft can be considered as similar when they have similar technology, construction and comparable systems, which means equally equipped with the following (as applicable to the licence category): a) Propulsion systems (piston or turboprop or turbofan or turboshaft or jet-engine or push propellers); and b) Flight control systems (only mechanical controls or hydro-mechanically powered controls or electro-mechanically powered controls); and c) Avionic systems (analog systems or digital systems); and d) Structure (manufactured of metal or composite or wood).

text: As an alternative to the above: - In the case of B1 licence endorsed with group ratings (either manufacturer group or full group) as defined in 66.A.45(g) the holder may show experience on at least one aircraft type per group and per aircraft structure (metal, composite, wood). - In the case of a B2 licence endorsed with group ratings (either manufacturer group or full group) as defined in 66.A.45(g) the holder may show experience on at least one aircraft type per group.

text: For category C, the experience should cover at least one of the aircraft types endorsed on the authorization.

text: For a combination of categories, the experience should include some activities of the nature shown in paragraph 2 in each category.

text: A maximum of 20% of the experience duration required may be replaced by the following relevant activities on an aircraft type of similar technology, construction and with comparable systems: - Aircraft maintenance related training as an instructor/assessor or as a student; - Maintenance technical support/engineering; - Maintenance management/planning.

text: The experience should be documented in an individual log book or in any other recording system (which may be an automated one) containing the following data: a) Date; b) Aircraft type; c) Aircraft identification i.e. registration; d) ATA chapter (optional); e) Operation performed i.e. 100 FH check, MLG wheel change, engine oil check and complement, SB embodiment, trouble shooting, structural repair, STC embodiment…; f) Type of maintenance i.e. base, line; g) Type of activity i.e. perform, supervise, release; h) Category used A, B1, B2 or C.

text: Remark: as per article 5 of regulation 2042/2003, this experience requirement does not apply to: - Certifying staff issuing a certificate of release of aircraft as per M.A.607(b); - Pilot-owner certifying tasks according to M.A.803; and - Certifying staff according to 145.A30(j) and Appendix IV of Part-145.

text: ED Decision 2007/018/R 18 Dec 2007

text: A new AMC to 66.B.120 is added:

text: AMC 66.B.120

text: The competent authority should not carry out any investigation to ensure that the licence holder is in current maintenance practice as this is not a condition for the renewal of a licence. Ensuring the continued validity of the certification privileges is a matter for the approved Part- 145 / Subpart-F maintenance organization or the certifying staff in accordance with M.A.801(b)2 . For the purpose of ensuring the continued validity of the certification privileges the competent authority may, when periodically reviewing the organizations in accordance with 145.B.30 or M.B.604, or during on the spot checks, request the licence holder for documentary evidence of compliance with 66.A.20(b) when exercising certification privileges.

text: In Annex V to Decision No 2003/19/RM:

text: The paragraph GM to 66.B120 is deleted:

text: GM 66.B.120

text: The competent authority will not be carrying out any investigation to ensure that the licence holder is in current maintenance practice as this is a matter for the maintenance organisation approved under Part 145 in ensuring validity of the Part 145 certification authorisation.