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 10017052 DART AEROSPACE USA, Inc. EASA.IM.R.S.01477 FAA STC SR00914SE EUROCOPTER FRANCE SA Installation of DART Bearpaws P/N D315-670- 1. Prior to installation of this modification the 06.02.2009 315B 011 - Validation of FAA STC SR00914SE. 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.2. 10017053 DART AEROSPACE USA, Inc. EASA.IM.R.S.01478 FAA STC SR00848SE EUROCOPTER FRANCE SA Installation of Dart Aerospace Skidtube P/N 1. Prior to installation of this modification the 06.02.2009 315B D315-668-011 (LH) and -012 (RH). Validation installer must determine that the of FAA STC SR00848SE. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. 10017063 DART AEROSPACE USA, Inc. EASA.IM.R.S.01499 FAA STC SR01853SE EUROCOPTER DEUTSCHLAND 117-762 Skitube Installation in accordance with Prior to installation of this modification the 10.11.2008 MBB-BK FAA STC SR01853SE. 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 10017084 DART AEROSPACE USA, Inc. EASA.IM.R.S.01551 FAA STC SR01043SE AGUSTA A119 Cargo Mirror Installation.Note: This STC supersedes ENAC STC N-CS-014 being the validation of FAA STC SR01043SE dated 25 January 2002. 10029107 DART AEROSPACE USA, Inc. N-CS-022 FAA STC SR00949SE A119, AW119MKII FAA STC SR00949SE dated 21 August 2008 "Bearpaw Installation" 10033942 DART AEROSPACE USA, Inc. CAA UK 28081 AND 28082 FAA STC SR00646SE 1. AS350 B, AS350 B1, AS350 B2 D350-636 Skidtube Installations Note: This 1. AS350 B3, AS350 BA, AS350 D STC supersedes CAA Approval Notes 28081 2. AS355 E, AS355 F, AS355 F1 and 28082 and addsmodels AS355N and NP 2. AS355 F2, AS355 N, AS355 NP to applicability. 10038103 DART AEROSPACE USA, Inc. REV. 1 FAA STC SR01042SE EC135 P1(CDS) EC135 P1(CPDS) EC135 P2(CPDS), EC135 P2+ EC135 T1(CDS), EC135 T1(CPDS) EC135 T2(CPDS), EC135 T2+ Dart D135-692-011 Bearpaws in accordance with Dart Aerospace DrawingList No. MDL- D135-692, and installation of this system.This EASA STC is based on validation of FAA STC SR01042SE iaw the PTVP. 10038656 DART AEROSPACE USA, Inc. REV. 1 FAA STC SR02138SE AW139 EASA Validation of FAA STC SR02138SE "Installation of Dart D139-799Maintenance Kits". 1. 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.2. 11.05.2009 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. 05.03.2010 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. 21.02.2011 Approval of this change in type design applies only to Eurocopter EC135rotorcraft, which are equipped with standard skidtubes, high gearskidtubes, or float skidtubes as defined in the installationinstructions. Prior to installation of this modification it 27.01.2012 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. 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. 19.03.2012 10040294 DART AEROSPACE USA, Inc. REV. 1 FAA STC SR02024SE A119, AW119MKII Validation of FAA STC SR02024SE: D119-646 None Prior to installation of this modification it 06.07.2012 Replacement Sikdtube Ins. 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. 10041447 DASSAULT AIRCRAFT SERVICES (DAS) FAA STC ST02964NY-D MF50 Installation of Crane Eldec "SmartStem" Tire Pressure Sensor (TPS)System.Validation of FAA STC N° ST02964NY-D. 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. 18.09.2012 04/01/2013 Page 168/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10041722 DASSAULT AIRCRAFT SERVICES (DAS) FAA STC ST02962NY-D FALCON 2000, FALCON 2000EX Validation of FAA STC Number ST02962NY- None - EASA STC ref. EASA.IM.A.S.02889 is 11.10.2012 D. Installation of RockwellCollins, Inc. ADS-B a pre requisite for thisinstallation.- Out System.Description as per Associated Airplane Flight Manual Supplement ref. Technical Documentation F2XW-D0006-150 IR, dated10/10/2011 is required for this installation.- Instructions for Continued Airworthiness ref. F2XW-D0006-155 RevisionB 10041723 DASSAULT AIRCRAFT SERVICES (DAS) FAA STC ST02963NY-D MYSTERE-FALCON 50 Validation of FAA STC Number ST02963NY- D. Installation of RockwellCollins, Inc. ADS-B Out System.Description as per Associated Technical Documentation. None - EASA STC ref. EASA.IM.A.S.02889 is a pre requisite for thisinstallation.- Airplane Flight Manual Supplement ref. F5XW-D0008-150 IR, dated02/12/2011 is required for this installation.- Instructions for Continued Airworthiness ref. F5XW-D0008-155 IR, dated 10015765 DASSAULT FALCON JET EASA.IM.A.S.01803 SA8279SW-D FALCON 900EX Installation of the Auxiliary Battery System 08.02.2006 10015766 DASSAULT FALCON JET EASA.IM.A.S.01805 FAA STC SA8303SW-D FALCON 900EX Installation of the Water System Modifications This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 08.02.2006 10015767 DASSAULT FALCON JET EASA.IM.A.S.01806 FAA STC SA8270SW-D FALCON 900EX Installation of the Miscellaneous Structures This STC is approved only for the product 08.02.2006 (General / Mechanical) configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015768 DASSAULT FALCON JET EASA.IM.A.S.01807 FAA STC SA8287SW-D FALCON 900EX Installation of the Equipment Rack This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 08.02.2006 10015778 DASSAULT FALCON JET EASA.IM.A.S.01823 SA5611SW MYSTERE FALCON 200 Installation of the Collins Dual EFIS-85EFIS-85 1. EASA Approved Airplane Flight Manual 02.08.2006 (Standard II) Instrument & Flight Director Supplement for Collins Dual EFIS-85 System of Collins Dual EFIS-86 Instrument & (Standard II) Instrument and Flight Director Flight Director System System, Falcon Jet Report 35402-1, Rev. B, or later EASA approved revision is a required part of this STC2. EASA Approved Airplane Flig 10016016 DASSAULT FALCON JET EASA.IM.A.S.02182 ST10461SC-D FALCON 900 Mid Cabin Door Installation, Enflite This STC is Limited to F9EX-01056-501 Installations in Model Falcon 900EX. 27.10.2006 10016017 DASSAULT FALCON JET EASA.IM.A.S.02183 ST10510SC-D FALCON 900 Aircraft Compliance for Falcon 900EX S/N Limited to S/N 165. No duplicate Installation 27.10.2006 165. permitted. 10016018 DASSAULT FALCON JET EASA.IM.A.S.02184 ST10253SC-D FALCON 900EX Oxygen System Installation. 27.10.2006 10016025 DASSAULT FALCON JET EASA.IM.A.S.02193 ST09296SC-D FALCON 2000 FAA STC ST09296SC-D: "Service and Indirect Lighting System" 18.12.2006 10016026 DASSAULT FALCON JET EASA.IM.A.S.02194 SA8267SW-D FALCON 2000 FAA STC SA8267SW-D: "Auxiliary Battery System" 20.12.2006 10016027 DASSAULT FALCON JET EASA.IM.A.S.02195 SA8227SW-D FALCON 2000 FAA STC SA8227SW-D: Automatic Electrical -Systems or components connected to the 18.12.2006 Load Shed System shed system must have a separate approval different from STC SA8227SW-D -Shedded componentsare non essential equipment 10016468 DASSAULT FALCON JET EASA.IM.A.S.02814 FAA STC ST09733SC-D FALCON 2000 Installation of Cabin Master Switch. Validation of FAA STC ST09733SC-D. See those of original FAA STC ST09733SC-D Revision 2 dated 04th October 2002,AFM Supplement Report No. 37023-1, Revision A dated 25th July 2002 for F2M-01055-501 and - 503 installations.AFM Supplement Report No. 37023-2, Revision NC dated 04th October 2002 10016469 DASSAULT FALCON JET EASA.IM.A.S.02815 FAA STC SA8228W-D FALCON 2000 Installation of the Airborne Flight Information See those of original FAA STC SA8228SW-D System.Validation of FAA STC SA8228SW-D. Revision 2 dated 21st May 1999 or later revisions approved by EASA in accordance with EASAED Decision 2004/04/CF (or subsequent revisions of this decision). 04/01/2013 Page 169/462 11.10.2012 20.05.2008 20.05.2008
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: EASA STC no. STC holder Old STC ref
Page 167: EASA STC no. STC holder Old STC ref
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?