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 10041959 APICAL INDUSTRIES, Inc. FAA STC NO. SR02425LA A119, A119 MK II EASA Validation of FAA STC No. SR02425LA None. Prior to installation of this modification it 26.10.2012 "Installation of ApicalIndustries, Inc. Cable must be determined thatthe Cutter Kit". interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10042766 APICAL INDUSTRIES, Inc. FAA STC SR02373LA EC130B4 Installation of Fresh Air Vents in accordance with Apical Industries,Inc. Master Document List MD130-3. This STC is the validation of FAA STC SR02373LA (date of issuanceSeptember 12, 2012). 10016824 APOLLO SPRAY SYSTEMS EASA.IM.R.S.01194 SR01215CH ROBINSON R44 Installation of Apollo Spray system DTM-4 agricultural sprayer onto Robinson R44 helicopter. EASA validation of FAA STC SR01215CH 10042428 APPAREO SYSTEMS, L.L.C. FAA STC SR02797CH AS350B1, AS350B2, AS350B3, AS350BA. 10015635 ARC AVIONICS CORP. EASA.IM.A.S.01591 FAA STC ST02959AT BOEING 737-300 SERIES BOEING 737-400 SERIES BOEING 737-500 SERIES 10015665 ARC AVIONICS CORP. EASA.IM.A.S.01641 FAA STC SA2890AT FAIRCHILD SWEARINGEN SA 226 FAIRCHILD SWEARINGEN SA 227 10016083 ARC AVIONICS CORP. EASA.IM.A.S.02267 FAA STC03354AT BOEING 737-200 BOEING 737-300 10016084 ARC AVIONICS CORP. EASA.IM.A.S.02269 FAA ST03356AT BOEING 737-200 BOEING 737-300 10016085 ARC AVIONICS CORP. EASA.IM.A.S.02270 REV. 2 FAA ST03362AT BOEING 737-200 BOEING 737-300 10016086 ARC AVIONICS CORP. EASA.IM.A.S.02271 FAA STC ST03363AT BOEING 737-200 BOEING 737-300 10016298 ARC AVIONICS CORP. EASA.IM.A.S.02595 FAA STC ST03458AT BOEING 737-300 BOEING 737-400 BOEING 737-500 Installation of Vision 1000 System in accordance with Vision 1000 MasterDocument List 606586-000011This STC is the validation of FAA STC SR02797CH (date of issuanceDecember 28, 2009) Installation of Collins Model 700 High Frequency (HF) Communication System and HF Antenna 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. 18.12.2012 Certified in restricted category.All limitations of RFM supplement apply. None If the holder agrees to permit another person to use this certificate tomodify the product, the holder shall give to the other person writtenevidence of that permission.Prior to installation of this modification it must be determined Installation of a Honeywell Model CAS 67A Prior to installation of this modification the Traffic Alert and Collision Avoidance System II installer must determine that the (TCAS II) with Single Mode-S Transponder interrelationship between this modification and MST 67A iaw FAA STC SA02890AT. any other previously installed modification will FAIRCHILD SWEARINGEN SA 26 introduce no adverse effect upon the airworthiness of the product. The install Installation of a single Universal Avionics Class “A” TAWS system on 737-300 series aircraft. 12.02.2007 30.11.2012 thatthe interrelations According to FAA STC ST02959AT 17.11.2005 The aircraft has to be equipped with a Universal EFIS to display the TAWS terrain. EASA Approved Flight Manual Supplement ARC Avionics document 730-061505 Rev A for Boeing 737-300 series aircraft, dated Feb 8 2007 is a part of this STC. Installation of a dual Universal Avionics UNS- The aircraft have to be equipped with a 1F FMS sys on Boeing 737-300 aircraft Universal Avionics EFIS as it provides the Installation includes 2 Nav Control Units Navigation Displays and Data Concentrator (NCU)in the EE bay and 2 GPS antennas. Units M integrate the aircraft sensors and Center pedestal pilot and co-pilot Control communications. FAA Approved Flight Manual Display Units (CDU). Nav data can be selected Supplement, ARC Avionics document 730an 120605 Installation of a dual Universal Avionics UNS- 1F Flight ManagementSystem (FMS) or UNS- 1Fw WAAS capabe FMS, on- Boeing 737-200 and 737-300 aircraft without EFIS (Configuration I)- Boeing 737-300 aircraft with original Honeywell or Collins EFIS(Configuration Installation of a single Universal Avionics Class “A” TAWS system on 737-200 series aircraft. 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. The aircraft has to be equipped with a Universal EFIS to display in the center pedestal in order to display the TAWS terrain. This MFD can be part of this installation, or pre-existing as the 737-200 series Aircraft. EASA Approved Flight manual Supplement Installation upgrade to replace the existing - AFM Document, ARC Avionics Document system with either Honeywell or Collins Dual 730-030806, for Boeing 737-300, -400, -500 Enhanced Mode S Transponder system. The series aircraft, dated 2 July 2007, or later existing Omni directional antenna is compatible EASA approved revision. with the new system and will not be replaced. The two Honeywell TRA-67A or Col 04/01/2013 Page 80/462 05.09.2008 03.07.2007 31.05.2007 28.04.2011 27.06.2007 10.01.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10034376 ARCHEION HOLDINGS L.L.C. FAA STC ST03529AT 1. B757-200 Installation of an Avionica satLINK None Prior to installation of this modification it 30.03.2011 2. B757-300 Communication Management System 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 10015815 ARINC INC. EASA.IM.A.S.01886 FAA STC SA00558DE-D BEECH 200, 200C, B200, B200C, BEECH 300, 300LW, B300, B300C 10015823 ARMSTRONG AEROSPACE EASA.IM.A.S.01895 FAA STC ST01872CH B737-200, 737-300, 737-400, B737-500, 737-600, 737-700, B737-800, 737-900 Installation of a Pilot and Co-Pilot Digital Air Data Unit Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) System on Boeing 737 Series aircraft 10042075 ARMSTRONG AEROSPACE EASA.IM.A.S.00252 MD-90-30 stc-easa.i.m.a.s.00252-aerospace engineering solutions Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter.ST01997CH in accordance with Armstrong Aerospace Master Data ListDocument No. DC104-3063-00, Revision A, dated 21 June 2004 or late 10015590 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.01501 FAA STC ST01742CH BOEING 747-400 SERIES BOEING 747-400D BOEING 747-400F 10015662 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.01639 FAA STC ST01773CH BOEING 777-200 BOEING 777-300 Installation of Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) system Installation of Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) 10015664 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.01640 FAA STC ST02108CH BOEING 767-300 Installation of Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) 10015725 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.01737 ST02202CH BOEING 757-200 Installation of Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) 10015789 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.01845 ST01797CH AIRBUS A320 Installation of a Honeywell RESCU 406 AF AIRBUS A321 Emergency Locator Transmitter (ELT) 10016211 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.02458 FAA ST02404CH AIRBUS A318 AIRBUS A319 AIRBUS A320 AIRBUS A321 10016363 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.02685 FAA STC ST02501CH AIRBUS B4-603 AIRBUS B4-605R 10016553 ARMSTRONG AEROSPACE Inc. EASA.IM.A.S.02935 FAA STC ST01837CH BOEING 747-200B BOEING 747-200C BOEING 747-200F BOEING 747-300 Activation of Honeywell Runway Awareness and Advisory System (RAAS). 1. Airplane Flight Manual Supplement:AFMS Document 34-07-0002-00, Revision IR, dated 19 August 2004 or Document 34-07-0026-00, Revision IR or later approved revision isrequired on board for the IS&S ADDU installation,or, AFMS Document 34-07-0002- 01, Revisi Compatibility of this design change with other previously approved modifications must be determined by the installer. 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. 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. 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. Instructions for Continued Airworthiness (ICA), ref. DC113-1020-00, Section 2, revision D, dated June 17, 2005 or later EASA approved revision Activation of Honeywell Runway Awareness This STC is only applicable on Honeywell and Advisory System (RAAS)(Validation of the EGPWS P/N identified through the 'Associated FAA STC n° ST02501CH)This STC consists in Technical Documentation' fitted with the activating the RAAS function on EGPWS Hardware/Software configuration up to ref : 226/226 Installation of Honeywell RESCU 406AF/AFN Airplane Flight Manual Supplements Armstrong Emergency Locator Transmitter (ELT) System. Aerospace Doc. No. DC303-1003-00, Rev.C, approved 4 February 2008 or later approved revision is required on board of the modified aircraft.Instruction for Continued Airworthiness, Armstron Aerospace Doc. No. DC1 02.01.2006 25.04.2006 1- Subject to compliance with the 15.10.2004 provisions of Par 21 Subpart E, thisSTC and associated data shall remain valid until surrendered, withdrawnor otherwise terminated 2- If transfer of this Certificate is requested under Part 21A.116, theSTC will be reissued 04/01/2013 Page 81/462 25.10.2005 25.10.2005 25.11.2005 26.01.2006 17.05.2006 31.10.2007 13.05.2008 12.09.2008
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: EASA STC no. STC holder Old STC ref
Page 79: EASA STC no. STC holder Old STC ref
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

Create successful ePaper yourself

Delete template?

Save as template?