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 10040826 GOMOLZIG FLUGZEUG- UND 0010016836-001 LBA STC EMZ SA 0100/2025 CESSNA 340A 1. Camera Modification Kit System C340- As referred in AFM Must be maintained iaw. Original Cessna 27.07.2012 MASCHINENBAU 8120002. C340 Camera Hatch Installation MM and in addition System C340-812500Change Note iawII_2027313_rev0_20120402or later CN_2027313_rev0_20120402 approved revisions.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyi 10016207 GOODRICH CORPORATION EASA.IM.A.S.02452 FAA STC ST02551CH BOEING 747-400F Installation of Centerline Restraint System on the main cargo deck of a B747-400F in accordance with Master Data List MDL 10026859 GOODRICH CORPORATION P- EASA.IM.A.S.03106 Prior to installation of this modification the installer must determine that the interrelationship between this modification and 7M39300. Validation of FAA STC ST02551CH. any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. 02.07.2008 FAA STC ST00989SE-D B767-300F Installation of the CHS (Cargo Handling The operation of the STC is only approved The applicant has to show and maintain 18.08.2009 System) on the B767-300FMD: when installed on theprovisions of the Boeing the compliance to JAR 25.1309 atchange MDL7N10000FAA STC: ST00989SE-D A/C B767-300F. 13.Remarks: The STC is part of the equipment for the Boeing A/C modelB767-300F. The provisions for the Cargo Handling System must beinstalled prior to the installation of the STC 10031947 GOODRICH CORPORATION REV. 1 TCCA STC SA10-3 DHC-8-401, DHC-8-402 Installation of Goodrich De-Icer boots on the Aircraft Wings, HorizontalStabilizer and Vertical StabilizerFAA STC ST02834NY, reissued September 20, 2010(identical with TCCA STC SA10-3, Issue 2) 10016001 GOODRICH INTERIORS EASA.IM.A.S.02161 REV. 2 FAA STC ST01691LA B767-200/-300 Installation of "Sentry One" Flight Deck Door Camera Surveillance System 10016462 GOODRICH INTERIORS EASA.IM.A.S.02808 REV. 1 FAA STC ST01788LA DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, MD-90-30. Installation of Sentry One Flight Deck Door Surveillance Camera System. 10016505 GOODRICH INTERIORS EASA.IM.A.S.02869 REV. 1 FAA STC ST01007LA-D 737-800 Installation of Hollingsead Sentry One Cabin Video Camera System. 10016523 GOODRICH INTERIORS EASA.IM.A.S.02896 REV. 1 FAA STC ST01638LA 737-300, 737-400, 737-500 Installation of Hollinsead Sentry One Cabin mounted Video Camera System. 10029901 GOODRICH INTERIORS REV. 1 FAA STC ST01472LA-D 747-100, 747-100B, 747-100B SUD, 747-200B, 747-300, 747-400, 747-SP Installation of Hollingsead International Sentry One Cockpit Entry DoorSurveillance Camera System. 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. 20.06.2012 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. 16.08.2012 None Prior to installation of this modification the 08.11.2012 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe 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. 08.11.2012 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. 07.11.2012 None FAA approved Flight Manual Supplement, document No. 2763- AFM,revision NC, dated May 25, 2004 is required for the B747-400 series. FAA approved Flight Manual Supplement, document No. 2763-AFM- 1,revision NC, dated July 21, 2004 is required for th 08.11.2012 04/01/2013 Page 240/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10037327 GPI AS 332 C, C1, L, L1, L2 Installation of Cargo Net in Cabin. No Passengers allowedWeight Limitation - 294 Prior to installation of this modification it 18.11.2011 kg;Maximum deformation - 257mm 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. 10013948 GRAFAIR AB EASA.A.S.00421 REV. 1 CESSNA 550 CESSNA S550 10015541 GRIMES AEROSPACE COMPANY EASA.IM.A.S.01425 ST500CH BOEING 737-300 BOEING 737-400 BOEING 737-500 Installation of an Allied Signal Corporation CAS- 1. Pro Star Aviation Aircraft Flight Manual 67A Traffic Alert and Collision Avoidance Supplement No 0100-FMS-02 for the Cessna System (TCAS II). Technical Documentation Aircraft Company, Models 550, S550 and 560, Associated: - FAA STC ST00116BO. - Pro Revision A, FAA-approved March 8, 2001, or Star Aviation, Master Document List No 0100- later FAA-approved revision, is required with MDL-02, Revision A, dated February 1, 20 this modification.2. This approval is Installation of Grimes Aerospace Overwing Emergency/ IceDetection Light Assemblies 10015936 GROVE AIRCRAFT LANDING GEAR EASA.IM.A.S.02077 SA01704LA SEE APPROVED MODEL LIST Installation of the Grove Disk Brake System in The installation applies only to aircraft that have SYSTEMS accordance with FAA approved Master hydraulic brake systems installed. The Drawing List Number MDL2337-00001, installation should not be incorporated in any Revision B, dated December 8, 2004, or later aircraft unless it is determined that the FAA approved revision are required as part of interrelationship between this installation any this installation ant previous 10015449 GULFSTREAM AEROSPACE Corp. EASA.IM.A.S.01192 FAA STC ST02883AT-D GULFSTREAM 200 Installation of Transponder Flight ID 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. 10015456 GULFSTREAM AEROSPACE Corp. EASA.IM.A.S.01202 FAA STC ST10299SC-D GULFSTREAM 200 Installation of ICG-200 SATCOM System 1. Instructions for continued Airworthiness GA24103A000 Revision N/C dated 31 January 2005 or later FAA approved revision is required 2. This STC is approved only for the product configuration as defined in the approved design data referred to in the parag 10015457 GULFSTREAM AEROSPACE Corp. EASA.IM.A.S.01203 FAA STC ST10297SC-D GULFSTREAM 200 Installation of Executive Cabin Interior 1. This STC is limited to the installation made in Gulfstream Aerospace LP(Istrael Aircraft Industries, LTD) model Gulfstream 200 serial number 103 only.2. This STC does not permit manufacturing of part for multiple installation3. This STC is approved only 10015459 GULFSTREAM AEROSPACE Corp. EASA.IM.A.S.01205 FAA STC ST10050SC-D GULFSTREAM 200 Installation of Honeywell Laseref V IRS 1. Compliance with FAA Special Condition 25- 263-SC and ACG/EASA CRI F-06 for HIRF has been demonstrated.2. The aircraft must be equipped with Rockwell Collins FMS-6100 Flight Management Systems installed in accordance with IAI MOD Nos.7219 and 100233. This 10015460 GULFSTREAM AEROSPACE Corp. EASA.IM.A.S.01206 FAA STC ST10020SC-D GULFSTREAM 200 Installation of DeCrane/ERDA Cabin Double Seats 10015579 GULFSTREAM AEROSPACE Corp. EASA.IM.A.S.01490 FAA STC ST09625SC GULFSTREAM 200 Installation of a Universal Unilink UL-601 Datalink Data Communication System 10015580 GULFSTREAM AEROSPACE Corp. EASA.IM.A.S.01491 FAA STC ST09628SC GULFSTREAM 200 Installation of Hard Point Attachments and associated floor structure 03.11.2005 According to FAA STC ST500CH 08.11.2005 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. 04/01/2013 Page 241/462 04.07.2006 28.06.2005 28.06.2005 28.06.2005 28.06.2005 28.06.2005 06.10.2005 06.10.2005
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: EASA STC no. STC holder Old STC ref
Page 239: EASA STC no. STC holder Old STC ref
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?