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 10015049 CARGOLUX AIRLINES INTERNATIONAL EASA.A.S.03366 BOEING 747-400F ICS-220A Iridium sitcom installation on B747- The Data on Airworthiness Limitations, 22.04.2008 400F airplanes in accordance with Master revisions required of the Maintenance Drawing List CLX-STC-07-01, dated 22 publications etc. arising from the changes November2007 or later EASA approved associated with the STC is provided in DWG revisions. CLX-STC-07-01: ICS-220A Iridium Satcom Installation on B747-400F Airplanes - ICA and miscella 10028509 CARSON HELICOPTERS, INC. P- FAA STC SR02487NY SIKORSKY S61N AND S61NM Increased Category A Performance. As specified in the approved RFMS. Carson Helicopters Inc. composite main 18.01.2010 EASA.IM.R.S.01532 rotor blades (STCEASA.IM.R.S.01129) must be installed. 10032448 CARSON HELICOPTERS, INC. EASA.IM.R.S.01138 FAA STC SH639NE S61 N Installation of 11,000 pound capacity Cargo Sling in accordance withCarson Services, Inc., Drawing List Report No S61N-1A Revision D datedJanuary 10, 2005 10015717 CASCADE AEROSPACE Inc. EASA.IM.A.S.01714 SA00-69 BOMBARDIER DHC-8-100 SERIES BOMBARDIER DHC-8-200 SERIES BOMBARDIER DHC-8-300 SERIES Environmental Control System Performance Improvement Modification as per TCCA STC #SA00-69, Issue 2, Issue Date: 15 June 2000 10015908 CASCADE AEROSPACE Inc. EASA.IM.A.S.02035 TCCA STC SA06-58 BOEING 747-400 Design Elementary & Enhanced REVISON 1 Surveillance.Validation of a STC SA06-58. 10015925 CASCADE AEROSPACE Inc. EASA.IM.A.S.02060 SA01-98 BOMBARDIER DHC-8-102 APU Oil Cooler Door Deletionas per TCCA BOMBARDIER DHC-8-103 STC # SA01-98, Issue 1, Issue Date: 23. BOMBARDIER DHC-8-311 BOMBARDIER DHC-8-315 August 2001 10015926 CASCADE AEROSPACE Inc. EASA.IM.A.S.02061 SA01-67 BOMBARDIER DHC-8-102 BOMBARDIER DHC-8-103 BOMBARDIER DHC-8-311 BOMBARDIER DHC-8-315 Screen Door and Ram Air Vent Modificationas per TCCA STC # SA01-67, Issue 1, Issue Date: 7. June 2001 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 in 06.07.2009 Configuration 1:a) Fwd Exhaust per Conair Aerospace Drawing 2302D21003 Rev Nil, dated May 19, 2000*.b) Aft Exhaust per Conair Aerospace Drawing 2302D21005 Rev Nil, dated May 19, 2000*. This element applicable to -300 Series only.c) Fwd Intake per Configuration 1:DHC-8 Series 100/200/300 aircraft modified in accordance withSTC EASA.IM. A.S. 01714Configuration 2:DHC-8 Series 100/200/300 aircraft in accordance with STC EASA.IM.A.S 02061 (equivalent to Bombardier Mod 8/2328 and 8/3330.Conditions: This Configuration 1:DHC-8 Series 100/200/300 aircraft with or without Bombardier Standard option Order 8155 APUConfiguration 2:DHC-8 Series 100/200/300 aircraft with or without Bombardier ACM Exhaust Mod. 8/1815Configuration 3:DHC-8 Series 100/200/300 aircraft 10016096 CASCADE AEROSPACE Inc. EASA.IM.A.S.02285 TCCA STC SA07-44 BOMBARDIER CL-600-2B19 Conversion of full cabin class E Cargo Compartment. 11.04.2007 10016357 CASCADE AEROSPACE Inc. EASA.IM.A.S.02679 TCCA STC SA 08-08 ISSUE 1, MAR BOMBARDIER DHC-8-400 SERIES Forward Baggage Compartment Installation. 12.03.2008 10016358 CASCADE AEROSPACE Inc. EASA.IM.A.S.02680 TCCA STC SA08-9, ISSUE 1, 4 FE BOMBARDIER DHC-8-400 SERIES G4 Galley Installation. 08.02.2008 10016359 CASCADE AEROSPACE Inc. EASA.IM.A.S.02681 TCCA STC SA08-10, ISSUE 1, 4 F BOMBARDIER DHC-8-400 Right AFT Draft Bulkhead InstallationTCCA 08.02.2008 SERIES STC Number: SA08-10, Issue 1, 04 February 2008 10016360 CASCADE AEROSPACE Inc. EASA.IM.A.S.02682 TCCA STC SA 08-11 ISSUE 1 4 FE BOMBARDIER DHC-8-400 SERIES 72 Passenger Seat Reconfiguration 08.02.2008 10016361 CASCADE AEROSPACE Inc. EASA.IM.A.S.02683 TCCA STC SA 08-12 ISSUE 1 4 FE BOMBARDIER DHC-8-400 SERIES G3 Galley Modification. 08.02.2008 10016563 CASCADE AEROSPACE Inc. EASA.IM.A.S.02954 TCCA STC NUMBER SA08-91 BOMBARDIER DHC-8-400 DHC-8-400 Conversion to Bulk FreighterTCCA 1 Prior to installation of this modification the 29.01.2009 SERIES STC Number SA08-91, Issue 1, dated 31 installer must determine that the December 2008 interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the pro 10029545 CASCADE AEROSPACE Inc. TCCA STC SA01-40 DHC-8-102, -103, -106 Ground Air Connection ModificationTCCA STC Placards have to be installed in accordance Note: SC EWIS is not applicable. 31.03.2010 DHC-8-201, -202 SA01-40, Is.1, dated 14 March 2001 with Conair AerospaceEngineering drawing DHC-8-3-1, -302 2854D21501, Rev. D. 10015469 CASCADE AVIATION SERVICES INC. EASA.IM.A.S.01222 SA01513SE BAE JETSTREAM 3201 SERIES Installation of Sandel Terrain Awareness Warning System (TAWS) Limitations as per Flight Manual 09.02.2007 10015711 CASCADE AVIATION SERVICES INC. EASA.IM.A.S.01706 REV 1 FAA STC ST01630SE BOEING 737 Installation of Eybrow Window Deletion Kit.FAA Compatibility of this design change with other 14.03.2006 STCST01630SE previously approved modifications must be determined by the installer. 04/01/2013 Page 152/462 22.02.2006 20.11.2006 07.08.2006 07.08.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016109 CASCADE AVIATION SERVICES INC. EASA.IM.A.S.02299 STC ST01181SE DORNIER 328-100 Installation of increased security cockpit door A copy of this Certificate and Cascade Aviation 19.01.2007 DORNIER 328-300 Services Master Drawing List (MDL) 02CAS096-MDL, Revision D, dated July 14, 2003 orlater approved revision must be maintained as part of the permanent records for the modified aircraft 10027057 CASCADE AVIATION SERVICES INC. P- FAA STC ST01133SE DHC-8-102, -103, -106 Installation of an increased security cockpit None 1) Prior to installation of this modification 02.09.2009 EASA.IM.A.S.03259 DHC-8-201 doorFAA STC # ST01133SE the installer mustdetermine that the DHC-8-301, -311, 314, 315 interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst 10039180 CEAPR REV. 2 HR 200/100, HR200/100S HR200/120, HR200/120B HR200/160 R2100, R2100A, R2112, R2120U R2160, R2160D, R2160I DET 120301 Rev. 0 - Oil pressure tranducer line R2000-HR2000 dated 7March 2012 10032548 CENTURY FLIGHT SYSTEMS, INC AK 847 STC SA 3389SW-D PA-31, PA-31-325, PA-31-350 AK 847 Validation / Century 41 Installation in Piper, Type CertificateNumber A20SO models PA-31, PA-31-325, PA-31-350 Limitation to serial numbers 001 up to 378 included. 1. This STC is limited to aircraft Models PA-31, PA-31-325 and PA-31-350,2. Piper Model PA-31 is limited to S/N 712 and Up,3. Placard 13A990-1 stating "conduct trim check prior to first flight ofday (see POH)" is required Prior to installation of this modification it 26.04.2012 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. The approval holder shall fulfill the 15.11.2010 obligations of Part 21, Pragraph21A.3 The approval holder shall fulfill the obligations of Part 21, Paragraph21.A109 Prior to installation of this modification it must be determined thatthe interrelationship between 10015954 CERTIFICATION DOCUMENTS AND EASA.IM.A.S.02097 FAA STC ST10674SC CESSNA 750 CITATION X Installation of an Aerodata AG Automatic Flight Limited to Aircraft Serial Number 262 only. Inspection System (AFIS). 15.10.2007 10014339 CESKA LETECKA SERVISNI A.S. EASA.A.S.01597 MITSUBISHI MU-2B-36A Avionics Upgrade in accordance with doc No CLS-05-MU-AC128, Revision 1.3., dated 27/01/2006. Limited to S/N MU2B-36A-718SA. 08.02.2006 10014486 CESKA LETECKA SERVISNI A.S. EASA.A.S.02548 LETECKE ZAVODY L 200 D Avionics upgrade in accordance with the document no;CLS-06-L200-AC 129, dated 23/06/2006 S/N 171206 28.07.2006 10014761 CESKA LETECKA SERVISNI A.S. EASA.A.S.02951 CESSNA 421C Avionics Upgrade, Proj. No.: CLS-07-C421- AC147Replacement of existing obsolete transponder, altimeters, ELT and COM/NAV with new that meets the current technical and operating requirements. 15.10.2007 10014901 CESKA LETECKA SERVISNI A.S. EASA.A.S.03135 CESSNA 172S Installation of the DME KN 62A, ADF KR-87 and XPDR KT-73 10.10.2007 10014989 CESKA LETECKA SERVISNI A.S. EASA.A.S.03284 LETECKE ZAVODY L-410-UVP- Installation of ACAS II system with XPDR This STC is valid only for L410-UVP-E13 05.11.2007 E13 (MST-67A) and ELT defined in document CLS- aircraft type, registration OK-UDS, S/N 892321 05-L410-AC125, revision 02 dated 04.11.2005 10014990 CESKA LETECKA SERVISNI A.S. EASA.A.S.03285 LETECKE ZAVODY L-410-UVP Installation of NAV/COM/GPS as defined in document CLS-06-6410-AC140, issue 0, revision 2 dated 13.09.2006 1. This STC is valid only for L410-UVP aircraft type. 10014991 CESKA LETECKA SERVISNI A.S. EASA.A.S.03286 LETECKE ZAVODY L 410 UVP-E Installation of- ACAS II (CAS-67) system with 1. This is valid only for L-410-UVP-E aircraft one XPDR (MST-67)- EGPWS Mk. VI system- type. KLN-94 GPS receiver, FA 2100 CVR, C 406-1 ELT- KMA-24H-70, LUN1120 and SAE-5-35as defined in document CLS-06-L410-AC138, issue 0, revision 1 dated 14.04.2006 10015069 CESKA LETECKA SERVISNI A.S. EASA.A.S.03395 LETECKE ZAVODY L 200 A LETECKE ZAVODY L 200 D 10015193 CESKA LETECKA SERVISNI A.S. EASA.A.S.03577 CESSNA 414 CESSNA 414A 10029112 CESKA LETECKA SERVISNI A.S. L-410 UVP-E-LW, L-410 UVP- Dual Mode-S Transponder upgrade for EHS E20, L-410 UVP-E9, L-410 UVP-LW, L-410M, L-410 UVP, L-410 UVP-E L-420 capability 05.11.2007 05.11.2007 Installation of new COM, NAV, GPS, XPDR + 04.07.2008 Encoder, DME, ADF and flight instruments to meet the current technical and operating requirements of IFR category. Avionics upgrade 16.12.2008 None None 05.03.2010 04/01/2013 Page 153/462
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: EASA STC no. STC holder Old STC ref
Page 151: EASA STC no. STC holder Old STC ref
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?