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 10014805 UNI AIR ENTREPRISE SAS EASA.A.S.03008 FALCON 20 CABIN INTERIOR REFURBISHMENT This STC is approved only for Mystere Falcon 20-E5 aircraft serial number 302.Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will 15.05.2007 10014824 UNI AIR ENTREPRISE SAS EASA.A.S.03037 BEECH 300 BEECH 300C 10014825 UNI AIR ENTREPRISE SAS EASA.A.S.03038 REV 1 BEECH 300 BEECH 300C FMS upgrade from UNS-1K to UNS-1K+ for compliance with P-RNAV Dual Installation of Collins TDR-94D with CTL- 92E for compliance with Enhanced Surveillance capability. This change is limited to the following serial numbersB300: S/N FL-111 thru FL-380; and FL-382B300C: S/N FM-9 thru FM-11; and FN-2 and subsequentThis change is limited to the configuration of aircraft / equipment type as listed under Item I – ‘De This change is limited to the following serial numbers:B300: S/N FL-111 thru FL-380; and FL-382B300C: S/N FM-9 thru FM-11; and FN- 2 and subsequent.This change is limited to the configuration of aircraft/equipment type as listed under Item I - Description D 10014853 UNI AIR ENTREPRISE SAS EASA.A.S.03077 BEECH B300 Installation of a Digital Flight Data Recorder 1. This STC is limited to the following S/N:Beech B300 S/N FL-111 through FL-380, FL-382Beech B300C S/N FM-9 through FM- 11, FN-2 and after2. Prior to installation of this modification the installer must determine that the interrelationship between th 10014875 UNI AIR ENTREPRISE SAS EASA.A.S.03100 Upgrade of ATC transponders for elementary surveillance (Mode S). To add elementary surveillance functionality in the ATC transponder and repalce KFS-578A control box by PS-578 to comply the ECAC airspace requirements in accordance with Master Data List MD 10014951 UNI AIR ENTREPRISE SAS EASA.A.S.03215 MYSTERE FALCON 50 Antenna and Cables installation provisions for satellite communication system. 1. STC nor applicable to Falcon 50EX version aircraft;2. 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 ad Design change applicable to Mystere Falcon 20 aircraft serial number 311. Design change applicable to Mystere Falcon 20 aircraft serial number 311. 10015156 UNI AIR ENTREPRISE SAS EASA.A.S.03523 MYSTERE FALCON 20 Installation of a forward partition door between entry area and cabin 10015172 UNI AIR ENTREPRISE SAS EASA.A.S.03546 MYSTERE FALCON 20 Installation of a passenger entertainment audio and video system in the cabin. 10015241 UNI AIR ENTREPRISE SAS P-EASA.A.S.03669 REV. 1 MYSTERE FALCON 50 (MF50) Iridium telecommunication system Installation limited to those Mystere Falcon 50 installationThis change is a revision of STC (MF50) aircraftpreviously modified i.a.w. Uni EASA.A.S.03669.This change allows Air Enterprise S.A.S. Supplemental installation of an alternative P /N of TypeCertificate (STC) "Antenna and cables transceiverand handsets as well as alternative installation provisions forsatellite location. communication system" approved under EASA.A.S.03 10031744 UNI AIR ENTREPRISE SAS MYSTERE FALCON 20 Enhanced Mode "S" compliance upgrade.Transponder and FMS software upgrade to meet the requirements for mode"S" Enhanced Surveillance downlink parameters. 10031773 UNI AIR ENTREPRISE SAS EASA.A.S.00307 REV. 1 CESSNA 550 (CITATION II) Installation of Honeywell EGPWS Mark VIIIThe STC has been revised to implement the alternative EGPWS computer P/N965-1210- 020 and the alternative EGPWS Configuration Module P/N700-1710-020. The approval holder shall fulfill the obligations of Part 21,Paragraph 21A.109. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ o 30.04.2007 11.09.2007 06.06.2007 06.09.2007 18.06.2008 19.05.2008 19.05.2008 13.08.2010 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 09.09.2010 Limited to: S/N 550-0001 through 550-0733 The maintenance tasks referred in Supplement to Cessna 550 MaintenanceManual ref. EGPWS UAE No 4 Revision 6 are required. The audio declutterfunction must be disabled. Prior to installation of this modification it 10.09.2010 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. 04/01/2013 Page 454/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10037035 UNI AIR ENTREPRISE SAS 200 Installation of gear override and steep This STC is applicable to aircraft s/n BY-91. Prior to installation of this modification it 26.10.2011 approach switches on TWASTW-950. 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. 10038465 UNI AIR ENTREPRISE SAS MF50 Enhanced Mode "S" compliance upgradeThis modification consists in the upgrade from mode "S" transponderelementary surveillance to mode "S" transponder enhanced surveillance tomeet the European airspace mandate for mode "S" EHS downlink parameters. 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. 17.02.2012 10039277 UNI AIR ENTREPRISE SAS MF 20GF Installation of Patch Iridium 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. 23.04.2012 10041337 UNI AIR ENTREPRISE SAS MF900 Installation of Iridium Satcom System ICS- 120B. None. None. 07.09.2012 10014173 UNIAIR EASA.A.S.01306 BEECH C90A Compliance with the B-RNAV requirements for 1. This STC is limited to aircraft s/n LJ-1303.2. 20.07.2005 the GPS System Trimble 2000 Approach + GPS System Trimble 2000 Approach + installation already approved with IFR priviledge. 10014237 UNIAIR EASA.A.S.01400 CORVETTE SN 601 Deviation to SB 34-12 - replacement of ADF in 1. This STC is limited to S/N 028 and S/N accordance with MDL UAE 010.05 rev 1 dated 0082. This STC is approved only for the 28.07.2005 11/07/05.Installation of ADF60 according to product configuration as defined in the option 85 aerospatiale instead of ADF approved design data referred to in the 206.Installation of option 85 on second ADF paragraph "Description". Compatibility with position instead of first position.Idmode other aircraft/engine configurations shall be dete 10015036 UNIAIR EASA.A.S.03349 REV. 1 MYSTERE FALCON 50 Installation of 220 VAC Electrical Power Supply None The approval holder shall fulfil the 10.04.2012 and Distribution inCabinNote: This STC obligations of Part 21, constitutes the extension of the approval Paragraph21.A109. Prior to installation of granted underEASA STC ref. this modification it must be determined EASA.A.S.03349 dated 19 May, 2008, to a thatthe interrelationship between this secondconfiguration. modification and any other previouslyinstalled modification and/ or repai 10015037 UNIAIR EASA.A.S.03350 REV. 1 MYSTERE FALCON 50 Installation of an In-Flight Passenger STC limited to those Mystere Falcon 50 The approval holder shall fulfil the 10.04.2012 Entertainment System in Cabin.Note: This STC (MF50) aircraft on which UniAirSTC 10015036 obligations of Part constitutes the extension of the approval Revision 1 "Installation of 220 VAC Electrical 21,Paragraph21.A109.Prior to installation granted underEASA STC ref. Power Supplyand Distribution in Cabin" has of this modification it must be determined EASA.A.S.03350 dated 19 May, 2008, to a been embodied. thatthe interrelationship between this and secondconfiguration. any other previously installedand/ or repair will introduce no adverse 10027898 UNIAIR P-EASA.A.S.03693 MF900 Installation of a Flight Data Recorder This design change is applicable on the basic Mystere Falcon 900aircraft, as per MF900 designation on EASA TCDS.A.062 10031335 UNIAIR EASA.A.S.00306 REV. 1 CESSNA CITATION II 550 Installation of a multi-functions display 1. AFM Supplement UAE No 47 issue 1 Honeywell type KMD-850 todisplay information Revision 1 dated 14 September 2004or later form the following systems:,,- ACAS II (CAS EASA-approved revision, is a required part of 67A),,- EGWPS (MK VIII) and,,- Weather radar this STC2. Or AFM Supplement UAE No 15 (ART 2000 or RS-181A) issue 2 revision 2 (for MSN 0609) orrevision 5 (for MSN 0190) or later EASA-approved revisio Prior to installation of this modification it 13.11.2009 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. Prior to installation of this modification the 02.06.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. 04/01/2013 Page 455/462
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:
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:
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: EASA STC no. STC holder Old STC ref
Page 453: EASA STC no. STC holder Old STC ref
show all

04/01/2013 Page 1/462 - EASA

Create successful ePaper yourself

Delete template?

Save as template?