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 10038286 RAM AIRCRAFT, LIMITED CESSNA 414 Modification of Cessna 414 in acc. with FAA This approval is limited to Hartzell None 03.02.2012 PARTNERSHIP STC SA09469SC-D: Aircraftmodified in accordance with RAM Master Drawing No. 1982, Revision K, FAAapproved September 23, 2009 and Installation of modified TCM enginemodel TSIO-520-NB in accordance with FAA STC SE0 propellers:PHC-C3YF-2UF/FC7663D(B)-2Q 10015448 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01191 FAA STC SA01129AT-D RAYTHEON 1900C Installation and peration of a Lockheed 1.FAA approved Airplane Flight Manual 31.08.2005 Martin/Fairchild FDR F1000, solid State flight Supplement AFMS96060, dated 18 APR 1997 data Recorder installed.Master Drawing List or later approved revision, is a required part of MDL9606 Initial Revision, dated January 10, this STC.2. This STC is approved only for the 1997 or later FAA approved revision. product configuration as defined in the approved design data referred to in the pa 10015506 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01384 FAA STC SA4899SW BOMBARDIER CL-600-2B16 Installation of Wulfsberg Flitefone IV/VI Communication System 10015507 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01385 SA5953SW BOMBARDIER CL-600-1A11 (CL- FAA STC SA5953SW. Installation of a nose 600 BOMBARDIER CL-600-2A12 (CL- 601 BOMBARDIER CL-600-2B16 gear door ground release mechanism 10015508 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01386 SA7457SW BOMBARDIER CL-600-2B16 FAA STC SA7457SW. Installation of Sperry LSZ-850 Lightning Sensor System 10015509 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01387 FAA STC SA7583SW BOMBARDIER CL-600-2B16 Installation of Sperry Primus 870 Weather Radar System 10015510 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01388 FAA STC SA7871SW BOMBARDIER CL-600-2B16 FAA STC SA7871SW. Installation of air driven generator inspection window 10015511 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01389 FAA STC SA7878SW BOMBARDIER CL-600-2B16 Installation of a DPI Labs 1800 Membrane Switch Control System 10015512 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01390 FAA STC SA7881SW BOMBARDIER CL-600-2B16 FAA STC SA7881SW. Installation of Sensor S67-1572 Global Positioning Antenna 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. 10015513 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01391 FAA STC SA7880SW BOMBARDIER CL-600-2B16 Installation of an alternate location for the refuel panel 25.07.2005 10015514 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01392 FAA STC SA7873SW BOMBARDIER CL-600-2B16 FAA STC SA7873SW. Installation of a cockpit Overhead Panel Extension 25.07.2005 10015515 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01393 FAA STC SA7872SW BOMBARDIER CL-600-2B16 FAA STC SA7872SW. Installation of a cockpit Center Pedestal Extension 25.07.2005 10015516 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01394 FAA STC SA7869SW BOMBARDIER CL-600-2B16 FAA STC SA7869SW. Installation of access door 25.07.2005 10015517 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01395 FAA STC SA7870SW BOMBARDIER CL-600-2B16 FAA STC SA7870SW. Installation of a Rosen Sun Visor System 25.07.2005 10015518 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01396 FAA STC SA7879SW BOMBARDIER CL-600-2B16 Installation of a cabin emergency lighting system 25.07.2005 10015519 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01397 FAA STC SA7886SW BOMBARDIER CL-600-2B16 Installation of a cabin oxygen system 11.08.2005 10015520 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01398 FAA STC SA7887SW BOMBARDIER CL-600-2B16 Installation of a Cabin Water System 25.07.2005 10015521 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01399 SA3703SW BOMBARDIER CL-600-2B16 FAA STC SA3703 SW. Installation of Thrust Reverser Access Panel in the Lower Nacelle 10015522 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01400 FAA STC SA4900SW BOMBARDIER CL-600-2B16 FAA STC SA4900SW.Installation of Dual Baker M1045 Cockpit Audio Systems with a Baker M1050 Cabin Paging/Chime Amplifier 10015523 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01401 FAA STC SA7460SW BOMBARDIER CL-600-2B16 Installation of Honeywell CG1230AC10 Lasertrack Navigation System 10015524 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01402 FAA STC SA5718SW BOMBARDIER CL-600-1A11 (CL- Installation of Airshow 100/200 Cabin Video 600 BOMBARDIER CL-600-2A12 (CL- 601 BOMBARDIER CL-600-2B16 System 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 366/462 25.07.2005 25.07.2005 25.07.2005 25.07.2005 25.07.2005 25.07.2005 25.07.2005 25.07.2005 25.07.2005 25.07.2005 25.07.2005
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015525 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01403 SA5830SW BOMBARDIER CL-600-1A11 (CL- FAA STC SA5830SW. Installation of Radio 25.07.2005 600 BOMBARDIER CL-600-2A12 (CL- 601 BOMBARDIER CL-600-2B16 Master Switch System 10015526 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01404 SA7451SW BOMBARDIER CL-600-2B16 Installation of a Dual EFIS Master Switch System 25.07.2005 10015527 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01405 FAA STC SA7454SW BOMBARDIER CL-600-2B16 Installation of Shepherd Security System 25.07.2005 10015528 RAYTHEON AIRCRAFT SERVICES, INC. EASA.IM.A.S.01406 FAA STC SA7459SW BOMBARDIER CL-600-2B16 Installation of a Dual FMS Master Switch System 10015915 RCM NORMALIZING EASA.IM.A.S.02045 SA5202NM COMMANDER AIRCRAFT 112 Validation of FAA STC SA5202NM: Installation of Lycoming engine model IO-360-C1D6 modified in accordance with STC SE5203NM & Propeller Hartzell HC-E3YR-1RF/F7392. 10016700 RCM NORMALIZING EASA.IM.E.S.01014 FAA STC SE5203NM LYCOMING ENGINES IO-360- C1D6 Installation of turbocharger and induction air intercooler in accordance with “Drawing List Report No. 1” dated August 20, 1990, orlater FAA approved revision. 10014230 RECTIMO AVIATION EASA.A.S.01393 PIPER PA-28-181, ARCHER III GNS 430 installation with MD 41-1488 (HSI and AP coupled)Installation of GNS 430 and MD 41-1488 coupled with KI 525A 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. 25.07.2005 See AFM Supplement No. 1. 25.06.2007 Compatibility of this design change with previously approved modifications must he determined by the installer. The installation should not be incorporated in any engine unless it is determined that the interrelationship between this installation and any p Limited to S/N 2843066 F-GSMDGPS use is forbidden for BRNAV and approachAuto Pilot coupling is forbidden under 2000 ft AGL 10015015 RECTIMO AVIATION EASA.A.S.03319 PARTENAVIA P68C Installation of a COM/NAV/GPS GARMIN GNS This STC is limited to the S/N 279. 430 (BRNAV without coupling to the auto-pilot) a COM/NAV GARMIN SL 30, a stormscope L3 WX 500 and an ELT ARTEX ME 406. 22.01.2008 10015112 RECTIMO AVIATION EASA.A.S.03459 PIPER PA-28R-201T Replacement of : King KX155, KI209 and Applicable to S/N 7803232 F-GHYY.GPS use Garmin GPS 155 by Garmin GNS430 coupled is limited to Day VFR flights in sight of ground to HSI and autopilot. Installation of a RMI KI 229.Removal of King KX155, KI209 and Garmin GPS 155 Installation of King RMI KI 229, Garmin GNS 430 with MD 41 coupled to HSI KI5 or water. 10034509 REGENT AEROSPACE CORPORATION FAA STC ST02274LA B777-222 Interior modifications in accordance with Regent Aerospace CorporationMaster Data List MDL-4100, Revision E, dated November 25, 2009. FAA STCST02274LA refers. Limited to B777-222 aircraft serial number 30214 only 31.05.2007 20.07.2007 22.09.2008 Prior to installation of this modification it 08.04.2011 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. 10016335 REVUE THOMMEN AG EASA.IM.A.S.02644 FAA STC ST10685SC LEARJET 60 Installation of Revue Thommen 3A43 Standby Altimeter. 12.03.2008 10016337 REVUE THOMMEN AG EASA.IM.A.S.02646 FAA STC ST10684SC LEARJET 45 Installation of Revue Thommen 3A43 Standby Altimeter. 12.03.2008 10015602 ROCKWELL COLLINS AEROSPACE EASA.IM.A.S.01538 ST01205NY BOMBARDIER CL-600-2B16 Installation of Head Up Guidance System (HGS) Model 2100 (Phase 2) 15.08.2005 10016646 ROCKWELL COLLINS AEROSPACE EASA.IM.A.S.03089 REV. 2 FAA STC ST01100SE DHC-8-401 & DHC-8-402 Updates for Flight Management System (FMS) None HGS 4100.FAA acceptance letter 130S-09- 387, dated 21.09.2009. None 12.04.2010 10015727 ROCKWELL COLLINS AEROSPACE & EASA.IM.A.S.01743 REV. 3 FAA STC ST01390LA CL-600-2C10, CL-600-2D15 Installation of Head-Up Guidance System None Prior to installation of this modification it 21.04.2011 CL-600-2D24, CL-600-2E25 (HGS) Model 4200.Addition of CL-600-2E25 must be determined thatthe (CRJ 1000) to HGS 4200 STC interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10016677 ROCKWELL COLLINS AEROSPACE & EASA.IM.A.S.03193 FAA STC ST00129SE BOMBARDIER DHC-8-100 SERIES BOMBARDIER DHC-8-200 SERIES BOMBARDIER DHC-8-300 SERIES Validation of the FAA STC ST00129SE for the HGS 2800 on the Dash 8-100/200/300 Series Aircraft (editorial change). 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. 04/01/2013 Page 367/462 27.04.2009
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:
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: EASA STC no. STC holder Old STC ref
Page 365: EASA STC no. STC holder Old STC ref
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?