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 10014337 AIR FRANCE EASA.A.S.01594 AIRBUS A330-203 Air France A330 "Ulysse" cabin reconfiguration The approval of this STC is limited to Airbus 12.10.2005 MSN 422, 443, 448, 458, 465, in accordance with Change Approval Sheet A330-203 Serial Numbers 422, 443, 448, 458, MSN 498, 500, 502, 503, 516, No. CAS-A330-04-001 dated 16/09/2005 (or 465, 481, 498, 500, 502, 503, 516, 519. The later EASA approved revision) Limitations and conditions defined in the EASA Datasheet are applicable.A copy of this STC and the CAS must be enclosed in 10014338 AIR FRANCE EASA.A.S.01596 BOEING 747-400 Air France B747-400 Big Bins modification. 1. The approval of this modification is limited to This is a revision to the EASA STC Ref 2004- the Boeing B747-400 MSN 24969, 24990, 4528, to extend the applicability to Boeing747- 25344, 25600, 25601, 25602, 32868, 32869, 400 , F-GEXA, MSN 24154.The general 32871, 25238, 25302, 25559, 25628, 25630, description is included in the Air France Letter 24154, 24155.The limitations and conditions BL.NI 10 003/EB and in the AEO 47-25 defined in the EASA Datasheet are appli 10014361 AIR FRANCE EASA.A.S.01627 FAA STC ST02348NY BOEING 767-300 Cabin Reconfiguration with an increased seating configuration for LOT Polish Airlines. 10014375 AIR FRANCE EASA.A.S.01650 BOEING 747-200 BOEING 747-300 Suppression of climb inhibition above flight level 300 on TCAS computer in accordance with AEO 47-34-0714 Revision 1 dated 17/10/2005 10014380 AIR FRANCE EASA.A.S.01658 BOEING 767 Emergency Escape Path Marking System 08.02.2006 10014451 AIR FRANCE EASA.A.S.02504 BOEING 737-800 KLM 737-800, -900 Recaro Seats Installation - Compatibility of this design change with other 11.05.2006 BOEING 737-900 previously approved modifications must be determined by the installer.- The installation is limited to the B 737-800, -900 listed in the CP- B737-06-001 Rev2, March 28th 2006.- As indicated in the doc. CP-B73 10014454 AIR FRANCE EASA.A.S.02508 BOEING 767-300 Cabin Reconfiguration -- 26.06.2006 10014456 AIR FRANCE EASA.A.S.02510 AIRBUS A330-343 Cabin Reconfiguration with the Installation of new B/C Seating Configuration as per Air France Change Approval Sheet n° CAS A330- 05-012 30.04.2007 10014570 AIR FRANCE EASA.A.S.02674 BOEING 767 B767 Cabin Reconfiguration from KLM to Aeroflot. 20.07.2007 10014601 AIR FRANCE EASA.A.S.02724 BOEING 767-300 Enhanced Surveillance Dual ATC Mode S Installation 23.02.2007 10014719 AIR FRANCE EASA.A.S.02896 BOEING 757-200 Installation of ATC Mode S Elementary and Certification basis as FAA TCDS 28.03.2007 Enhanced Surveillance A2NMIncluding:TGL 13 Rev 1, 01/06/2003EASA AMC-20.13, 02/12/2005JAA TGM 21/07, 01/10/2003. 10014822 AIR FRANCE EASA.A.S.03034 BOEING 767-300 Installation of Elementary Surveillance Dual This STC is approved only for the product 26.02.2007 ATS Mode S. configuration as defined in the approved design data referred to in the paragraphs "Description" and “Associated Technical Documentation”. Compatibility with other aircraft/engine configurations shall be determined 10014865 AIR FRANCE EASA.A.S.03089 AIRBUS A340-300 A340 FINNAIR Cabin and IFE Upgrade Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10015195 AIR FRANCE EASA.A.S.03581 REV 1 BOEING 777-200 BOEING 777-300 ADS-B Out Activation. None. 05.09.2008 10015245 AIR FRANCE EASA.A.S.03681 BOEING 747-400 ADS-B Out Installation and Activation as per 1. Prior to installation of this modification the 10.12.2008 Air France Service Bulletin B747-08-004-34- installer must determine that the 001 rev. 0 or later approved revisions. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. 10017148 AIR GRISCHA HELIKOPTER AG EASA.R.S.01251 REV. 1 FOCA STC 56-30-01 AS 350 B3 Bubble Window RH Installation P/N 1. When the bubble window is used for vertical Prior to installation of this modification the 21.03.2011 030603/350BW according FOCA Data reference, the followingapplies: If the pilot installer must determinethat the Sheet56-30-01.Installation of P/N cannot firmly hold the collective pitch lever interrelationship between this modification 030603/350BW according to FOCA data sheet whenin the position intended for vertical and any otherpreviously installed 56-30-01at issue 3.Revision 1: This is a change reference through the bubblewindow, an modification will introduce no adverse to EASA.R.S.01251 issued 23/03/2006 approved collective pitch lever exte effect uponthe airworthiness of the whichwas based on STC FOCA 56 product. 04/01/2013 Page 52/462 19.10.2005 24.04.2006 23.11.2005 18.09.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10017167 AIR MACH S.R.L. EASA.R.S.01275 EUROCOPTER FRANCE AS 350 Kit Air Mach ELIRAI TV-99-Internal Rack/ This installation should not be incorporated in 10.05.2006 B2 Installation of electronic equipment for radio any aircraft unless it is determined that the bridge interrelationship between this installation and any previously approved configuration will not introduce any adverse effefct upon the airworthiness of the aircraf 10017168 AIR MACH S.R.L. EASA.R.S.01276 EUROCOPTER FRANCE AS Kit Air Mach ELIRAI TV-99-Internal Rack/ This installation should not be incorporated in 10.05.2006 355F1 Installation of electronic equipment for radio any aircraft unless it is determined that the EUROCOPTER FRANCE AS bridge interrelationship between this installation and 355F2 any previously approved configuration will not introduce any adverse effefct upon the airworthiness of the aircraf 10016871 AIR METHODS CORPORATION EASA.IM.R.S.01247 FAA STC SR00032DE-D AGUSTA BELL 412 Installation of Air Methods Corporation 1. Single and dual patient configurations are 11.01.2007 BELL 412 Emergency Medical System interior that to be installed in strict accordance with Air provides 3 patient locations to be configured Methods Corporation Maintenance Manual one oftwo ways using an Intensive Care AMMS 050-0110 rev N/C dated 156 April 1993 Transport Litter (ICTL) and Ferno stretchers. or later approved revision and FAA approved Rotorcraft Flight Manual Supplemen 10029569 AIR METHODS CORPORATION REV. 1 FAA STC SR00705DE-D S-76A, S-76B, S-76C Installation of Articulated Patient Loading System (APLS).Note: The STC amendment adds an ALLFA litter as an option. 10030372 AIR METHODS CORPORATION FAA STC SR00250DE-D MD900 Installation of an EMS Interior in a MD902 Helicopter Required pre-modification Sikorsky cabin Prior to installation of this modification it 19.08.2011 medical interior GA dwg. no.09076B10E001-1 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. If damage or excess wear warrants structural repair or alteration to thefloor system, preapproval authorized by the holder of this STC isrequired in accordance with AMMS 050- 0167, Rev. (-), dated June 13, 1996or later FAA accepted revision.The multi-purpo Prior to installation of this modification it 11.06.2010 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. 10031942 AIR METHODS CORPORATION FAA STC SR00702DE-D BELL 429 Installation of Supplemental Strobe Lights None Prior to installation of this modification it 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 23.09.2010 10032603 AIR METHODS CORPORATION FAA STC SR00701DE-D 429 Installation of a controllable Searchlight none Prior to installation of this modification it 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. 17.11.2010 10032617 AIR METHODS CORPORATION FAA STC SR00704DE-D BELL 429 Installation of Emergency Medical Services Interior and Systems None Prior to installation of this modification it 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 17.11.2010 10032620 AIR METHODS CORPORATION FAA STC SR00710DE-D BELL 429 Installation of Scene and Patient Loading Lights None Prior to installation of this modification it 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 17.11.2010 04/01/2013 Page 53/462
Page 1 and 2: EASA STC no. STC holder Old STC ref
Page 51: EASA STC no. STC holder Old STC ref
Page 103 and 104:
EASA STC no. STC holder Old STC ref
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:
Page 309 and 310:
Page 311 and 312:
Page 313 and 314:
Page 315 and 316:
Page 317 and 318:
Page 319 and 320:
Page 321 and 322:
Page 323 and 324:
Page 325 and 326:
Page 327 and 328:
Page 329 and 330:
Page 331 and 332:
Page 333 and 334:
Page 335 and 336:
Page 337 and 338:
Page 339 and 340:
Page 341 and 342:
Page 343 and 344:
Page 345 and 346:
Page 347 and 348:
Page 349 and 350:
Page 351 and 352:
Page 353 and 354:
Page 355 and 356:
Page 357 and 358:
Page 359 and 360:
Page 361 and 362:
Page 363 and 364:
Page 365 and 366:
Page 367 and 368:
Page 369 and 370:
Page 371 and 372:
Page 373 and 374:
Page 375 and 376:
Page 377 and 378:
Page 379 and 380:
Page 381 and 382:
Page 383 and 384:
Page 385 and 386:
Page 387 and 388:
Page 389 and 390:
Page 391 and 392:
Page 393 and 394:
Page 395 and 396:
Page 397 and 398:
Page 399 and 400:
Page 401 and 402:
Page 403 and 404:
Page 405 and 406:
Page 407 and 408:
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?