04/01/2013 Page 1/462 - EASA

More documents

Recommendations

Info

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10034324 POLICE AVIATION SERVICES Ltd. MD902 CONFIG. P&W 206&207 Aircraft Role Configuration none The approval holder shall fulfill the obligations of Part 21, Paragraph21.A109Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair 25.03.2011 10036834 POLICE AVIATION SERVICES Ltd. REV. 1 VULCANAIR P.68.TC Airborne Surveillance System Installation None Prior to installation of this modification it 24.11.2011 'OBSERVER' must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10015338 PRATT & WHITNEY EASA.IM.A.S.00373 REV. 2 AIR TRACTOR AT-402 A AIR TRACTOR AT-501 AIR TRACTOR AT-502 B AIR TRACTOR AT-503 AIR TRACTOR AT-802 AIR TRACTOR AT-802 A BEECH 1900 BEECH 200 BEECH 300 BEECH C90 CESSNA 208 CESSNA 208A CESSNA 208B PILATUS PC-6/B-H2 PILATUS PC-6/B1-H2 PILATUS PC-6/B2-H2 PILATUS PC-6/B2-H4 10015554 PRATT & WHITNEY EASA.IM.A.S.01451 REV. 1 FAA STC SA00196BO BEECH 1900 BEECH 200 BEECH 300 BEECH C90 CESSNA 208 CESSNA 208A CESSNA 208B 10015834 PRATT & WHITNEY EASA.IM.A.S.01925 REV 1 FAA STC ST00228BO DC-9-81 (MD-81) DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87) MD-88 10016426 PRATT & WHITNEY EASA.IM.A.S.02765 FAA STC SA00095BO, LBA SA 1346 BEECH 1900 BEECH 1900C, AIRLINER BEECH 1900D BEECH 200 BEECH 200C BEECH 200CT BEECH 200T BEECH 300 BEECH 300LW BEECH A200 BEECH A200C BEECH A200CT BEECH B200 BEECH B200C BEECH B200CT BEECH B200T BEECH B300 BEECH B300C Installation of Pratt & Whitney Data Acquisition System ADAS+, p/n ADAS-K-010. 1. Compatibility of this modification with other previously approved modifications must be determined by the installer.2. This Major Change to STC EASA.IM.A.S.00373 is issued as a result of the validation of the Altair Avionics Corporation STC No SA0 Installation of Altair Avionics Corporation Data This STC is approved only for the product Transmission Unit in accordance with configuration as defined in the approved design instructions listed in Approved Model List (AML) data referred to in the paragraph "Description". DTU-T-225-1, Rev - or later approved Compatibility with other aircraft/engine revisions. FAA STC SA00196BO refers configurations shall be determined by the installer. Installation of P&W JT8D-200 Series Engines incorporating the improved forward Fan Case as described in the P&W SB JT8D 6478, Rev.1, dated 1 August 2007. 10016692 PRATT & WHITNEY EASA.IM.E.S.01006 FAA STC SE00033EN CFM56-3B1 Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module in accordance with P&W GMS Drawing List 880500-01C dated May 06, 2008 or later EASA-approved revisionEASA Certification Basis:1. Airworthiness This STC is approved only for the product configuration as defined in the approved design datareferred to in the paragraph "Description". Prior to installation of this modification the installermust determine that the interrelationship between this modific Installation of Pratt & Whitney Engine Services, 1. Pratt & Whitney Engine Services,Inc. Inc. Twin Engine Aircraft Data Acquisition Aircraft Flight Manual Supplement for System ADAS/ADAS+ Upgrade, P/N TWIN-K- Raytheon Aircraft Company Models 200, 010 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, 300, 300LW, B300C, 1900, 1900C, 1900D, Document No. TWIN-T-250-1, Revisi Limitations:1. The limitations of the EASA Engine Type Certificate Data Sheet E.066 issue 1, dated November 28, 2008 apply to this Supplemental Type Certificate.2. Life limits for the parts approved by this Supplemental Type Certificate are published 04/01/2013 Page 358/462 07.03.2008 11.04.2008 04.10.2007 07.03.2008 22.12.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016693 PRATT & WHITNEY EASA.IM.E.S.01007 FAA STC SE00034EN CFM56-3B1 Installation of Pratt & Whitney (P&W) Global Limitations:1. The limitations of the EASA 22.12.2008 Material Solutions (GMS) CFM56-3 High Engine Type Certificate Data Sheet E.066 Pressure Turbine Module in accordance with issue 1, dated November 28, 2008 apply to this P&W GMS Drawing List 880500-01D dated Supplemental Type Certificate.2. Life limits May 06, 2008 or later EASA-approved for the parts approved by this Supplemental revisionEASA Certification Basis:1. Airworthiness Sta Type Certificate are published 10016694 PRATT & WHITNEY EASA.IM.E.S.01008 FAA STC SE00035EN CFM56-3B1 Installation of Pratt & Whitney (P&W) Global Limitations:1. The limitations of the EASA 22.12.2008 Material Solutions (GMS) CFM56-3 Low Engine Type Certificate Data Sheet E.066 Pressure Turbine Module in accordance with issue 1, dated November 28, 2008 apply to this P&W GMS Drawing List 880500-01E dated Supplemental Type Certificate.2. Life limits May 06, 2008 or later EASA-approved for the parts approved by this Supplemental revisionEASA Certification Basis:1. Airworthiness Stan Type Certificate are published 10016695 PRATT & WHITNEY EASA.IM.E.S.01009 FAA STC SE00032EN CFM56-3B1 Installation of Pratt & Whitney (P&W) Global Limitations:1. The limitations of the EASA 22.12.2008 Material Solutions (GMS) CFM56-3 Fan and Engine Type Certificate Data Sheet E.066 Booster Module in accordance with P&W GMS issue 1, dated November 28, 2008 apply to this Drawing List 880500-01B dated March 14, Supplemental Type Certificate.2. Life limits 2008 or later EASA-approved revisionEASA for the parts approved by this Supplemental Certification Basis:1. Airworthiness Standar Type Certificate are published 10016702 PRATT & WHITNEY EASA.IM.E.S.01017 FAA STC SE00026EN ROLLS-ROYCE 250-C18 ROLLS-ROYCE 250-C18A ROLLS-ROYCE 250-C20 ROLLS-ROYCE 250-C20B ROLLS-ROYCE 250-C20F ROLLS-ROYCE 250-C20J ROLLS-ROYCE 250-C20R/1 ROLLS-ROYCE 250-C20R/2 ROLLS-ROYCE 250-C20S 10016703 PRATT & WHITNEY EASA.IM.E.S.01018 FAA STC SE00029EN, LBA EN0034 HONEYWELL INT. T5313B HONEYWELL INT. T5317 Installation of Pratt & Whitney Engine Services, 1. The IntelliStart Plus +TM ECU is desinged to Inc. IntelliStart Plus +TM Electronic Control Unit limit start temperatures and to provide an (ECU), P/N DPU-K-010 on the specified 250 electronic aid for recording engine trend and engine models. cycle data.2. The IntelliStart Plus +TM ECU is designed as non-essential, ground use only equipment and cannot be used Installation of Pratt & Whitney Engine Services, Inc. SmartCycle Plus Engine Monitoring System, P/N EMU-K-010-1 on the specified T53 engine models 1. SmartCycle Plus Engine MonitoringSystem is designed as an electronic aid for recording engine trend and cycle data.This system does not eliminate any scheduled maintenance or parts replacement based on time or any engine Instructions for Continued Airwo 10016704 PRATT & WHITNEY EASA.IM.E.S.01019 FAA STC SE00027EN ROLLS RROYCE 250-C Installation of Pratt & Whitney Engine Services, 1. The IntelStart Plus +TM ECU is desinged to Inc. IntelliStart Plus +TM Electronic Control Unit limit start temperatures and to provide an (ECU), P/N DPU-K-010 on the specified electronic aid for recording engine trend and engine models cycle data.2. The IntelliSTart Plus +TM ECU is designed as non-essential, ground use only equipment and cannot be used to 10016707 PRATT & WHITNEY EASA.IM.R.S.0048 REV. 1 N 2004-6170 AGUSTA AB-412 AGUSTA AB-412EP BELL 212 BELL 222 BELL 222B BELL 222U BELL 412 BELL 412 EP 10016799 PRATT & WHITNEY EASA.IM.R.S.01157 REV. 1 AGUSTA AB-412 AGUSTA AB-412EP BELL 212 BELL 412 BELL 412 EP Installation of Pratt & Whitney Engine Services, Inc. SmartCycle monitoring and recording system Installation of Pratt & Whitney Engine Services , Inc. Data Transmission Unit 1. Required maintenance, as prescribed in the applicable airframe or engine Instructions for Continued Airworthiness, shall not be predicted on the data obtained from Pratt & Whitney Engine Services, Inc., monitoring/recording system.2. This system shall 10016803 PRATT & WHITNEY EASA.IM.R.S.01163 REV. 1 SCHWEIZER AIRCRAFT 269D Installation of Pratt & Whitney Engine Services, 1. Engine must be modified in accordance with Inc. IntelliStart+ Electronic Control System and STC SE00027EN, which must be EASA Gine Trend Monitor P/N DPU-K-010-14 approved or accepted prior to installation.2. Reference STC SE0027EN for any additional limitations applicable to the engine installation3. This system is designed as an electr 10016827 PRATT & WHITNEY EASA.IM.R.S.01197 REV. 1 AGUSTA A-109 E Installation of a Pratt & Whitney Engine Services, Inc. Digital Aircraft Data Acquisition System ADASd 10016848 PRATT & WHITNEY EASA.IM.R.S.01224 REV. 1 AGUSTA A-109 E Installation of a Pratt & Whitney Engine Services, Inc. Dta Transmission Unit Data Transmission UnitDTU-K-010-7 14.03.2008 04.03.2008 14.03.2008 25.03.2008 07.03.2008 14.03.2008 1. Required maintenance, as prescribed in the 11.03.2008 applicable airframe or engine Instructions for Continued Airworthiness, shall not be predicated on the data obtained from the Pratt & Whitney Engine Services, Inc. monioring/recording system.2. This system shal 1. 109E with Pr & W: 206C Engine; 07.03.2008 04/01/2013 Page 359/462
Page 1 and 2:
EASA STC no. STC holder Old STC ref
Page 3 and 4:
Page 5 and 6:
Page 7 and 8:
Page 9 and 10:
Page 11 and 12:
Page 13 and 14:
Page 15 and 16:
Page 17 and 18:
Page 19 and 20:
Page 21 and 22:
Page 23 and 24:
Page 25 and 26:
Page 27 and 28:
Page 29 and 30:
Page 31 and 32:
Page 33 and 34:
Page 35 and 36:
Page 37 and 38:
Page 39 and 40:
Page 41 and 42:
Page 43 and 44:
Page 45 and 46:
Page 47 and 48:
Page 49 and 50:
Page 51 and 52:
Page 53 and 54:
Page 55 and 56:
Page 57 and 58:
Page 59 and 60:
Page 61 and 62:
Page 63 and 64:
Page 65 and 66:
Page 67 and 68:
Page 69 and 70:
Page 71 and 72:
Page 73 and 74:
Page 75 and 76:
Page 77 and 78:
Page 79 and 80:
Page 81 and 82:
Page 83 and 84:
Page 85 and 86:
Page 87 and 88:
Page 89 and 90:
Page 91 and 92:
Page 93 and 94:
Page 95 and 96:
Page 97 and 98:
Page 99 and 100:
Page 101 and 102:
Page 103 and 104:
Page 105 and 106:
Page 107 and 108:
Page 109 and 110:
Page 111 and 112:
Page 113 and 114:
Page 115 and 116:
Page 117 and 118:
Page 119 and 120:
Page 121 and 122:
Page 123 and 124:
Page 125 and 126:
Page 127 and 128:
Page 129 and 130:
Page 131 and 132:
Page 133 and 134:
Page 135 and 136:
Page 137 and 138:
Page 139 and 140:
Page 141 and 142:
Page 143 and 144:
Page 145 and 146:
Page 147 and 148:
Page 149 and 150:
Page 151 and 152:
Page 153 and 154:
Page 155 and 156:
Page 157 and 158:
Page 159 and 160:
Page 161 and 162:
Page 163 and 164:
Page 165 and 166:
Page 167 and 168:
Page 169 and 170:
Page 171 and 172:
Page 173 and 174:
Page 175 and 176:
Page 177 and 178:
Page 179 and 180:
Page 181 and 182:
Page 183 and 184:
Page 185 and 186:
Page 187 and 188:
Page 189 and 190:
Page 191 and 192:
Page 193 and 194:
Page 195 and 196:
Page 197 and 198:
Page 199 and 200:
Page 201 and 202:
Page 203 and 204:
Page 205 and 206:
Page 207 and 208:
Page 209 and 210:
Page 211 and 212:
Page 213 and 214:
Page 215 and 216:
Page 217 and 218:
Page 219 and 220:
Page 221 and 222:
Page 223 and 224:
Page 225 and 226:
Page 227 and 228:
Page 229 and 230:
Page 231 and 232:
Page 233 and 234:
Page 235 and 236:
Page 237 and 238:
Page 239 and 240:
Page 241 and 242:
Page 243 and 244:
Page 245 and 246:
Page 247 and 248:
Page 249 and 250:
Page 251 and 252:
Page 253 and 254:
Page 255 and 256:
Page 257 and 258:
Page 259 and 260:
Page 261 and 262:
Page 263 and 264:
Page 265 and 266:
Page 267 and 268:
Page 269 and 270:
Page 271 and 272:
Page 273 and 274:
Page 275 and 276:
Page 277 and 278:
Page 279 and 280:
Page 281 and 282:
Page 283 and 284:
Page 285 and 286:
Page 287 and 288:
Page 289 and 290:
Page 291 and 292:
Page 293 and 294:
Page 295 and 296:
Page 297 and 298:
Page 299 and 300:
Page 301 and 302:
Page 303 and 304:
Page 305 and 306:
Page 307 and 308: EASA STC no. STC holder Old STC ref
Page 357: EASA STC no. STC holder Old STC ref
Page 409 and 410:
Page 411 and 412:
Page 413 and 414:
Page 415 and 416:
Page 417 and 418:
Page 419 and 420:
Page 421 and 422:
Page 423 and 424:
Page 425 and 426:
Page 427 and 428:
Page 429 and 430:
Page 431 and 432:
Page 433 and 434:
Page 435 and 436:
Page 437 and 438:
Page 439 and 440:
Page 441 and 442:
Page 443 and 444:
Page 445 and 446:
Page 447 and 448:
Page 449 and 450:
Page 451 and 452:
Page 453 and 454:
Page 455 and 456:
Page 457 and 458:
Page 459 and 460:
Page 461 and 462:
show all

04/01/2013 Page 1/462 - EASA

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?