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 10039248 ROSEN SUNVISOR SYSTEMS LLC FAA STC SA2367NM CL-600-1A11/-2A12/-2B16/-2B19 Cockpit Sunvisor Installation None Prior to installation of this modification it 20.04.2012 CL-600-2C10/-2D24 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. 10028673 ROSS FRESNO LLB EASA.IM.A.S.03153 CESSNA 441 SERIES 15.07.2009 10032879 ROTORCRAFT SUPPORT, Inc. FAA STC SR01456LA 407 Installation of Concorde RG407 Battery 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 06.12.2010 10017109 ROTORTECH LIMITED EASA.R.S.01085 EUROCOPTER FRANCE EC 155 B1 Compendium Modification. Compilation of 22 individual modifications associated with the installation of equipment and systems enabling the transfer of EC 155B1 S/N 6642 from FAA register (N84AZ) to the UK register (G-NIVA). 10033185 ROW 44, Inc. REV. 1 FAA STC ST02829CH B737-700/-800/-900 Installation of Row 44 Broadband Antenna System Provisions 10033186 ROW 44, Inc. REV. 2 FAA STC ST02836CH-D B737-700, -800, -900 Installation and activation of a Row 44 Broadband System 1. This STC is applicable to EC155B1 S/N 6642 only2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with 22.09.2005 other aircraft/engine configurations shall be The equipment for which these provisions are Prior to installation of this modification it 22.10.2012 intended has not beencertified. Additional must be determined thatthe approval is required for the installation of interrelationship between this modification thisequipment and must be evaluated to assure and any other previouslyinstalled satisfactory compliance withthe applicable modification and/ or repair will introduce airworthiness standards. no adverse effectupon the airworthiness of the product. - The Row 44 Wireless Broadband System is intended to provide internetconnection and email services to the airplane's cabin using portableelectronic devices (PEDs). Any other use of this equipment will require a reexamination of thecertification basis. - 10016327 ROYAL ATLANTIC AVIATION, INC. EASA.IM.A.S.02636 FAA STC SA02636AT CESSNA 441 SERIES Ground Recognition Strobe Light System 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. 10017127 RTE - STH EASA.R.S.01215 REV. 1 AS 355N New pilot/co-pilot manual quick release 1. Limited to the following AS 355 N aircrafts:pyrotechnic sub-system, P/N JD3448AB00100- S/N 5649, F-GSTH equipped with DGAC-F A0, for approved HEC devices ref: 01-STH- approved design changes ref. 01-STH-001 or 001 and 01-STH-002 and AAN 24527 01-STH-002-S/N 5543, F-GJAX equipped with DGAC-F approved design change ref. 01-STH- 001-S/N 5566, G-LINE equipped with CAA-UK a 10017135 RTE - STH EASA.R.S.01229 AS 332 C1 Installation for Human External Cargo (HEC) applications 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 also applicable on AS355N when equipped with EASA.R.S.01366. 10017165 RTE - STH EASA.R.S.01273 DGAC-F TC N° 168 AS 355 N Personnel transport aboard hooked baskets as rotorcraft-load combinations for human external cargo (HEC). 10017210 RTE - STH EASA.R.S.01366 DGAC FRANCE STC FAM AS 355 N Helicopter equipped with ARRIUS 1A modified • Engine operating limitations as defined in 98STH0595 namedARRIUS 1E.DGAC-F approved design the “Installation Manual” reference X319 HS change 98STH0595 relates toinstallation of two 0011.• Engine maintenance requirements modified ARRIUS 1A engines on the AS355N defined in Manuel d’entretien Turbomoteur helicopter. This installation allows increased engine performance required to perform GBF 124. Prior to installation of this modification it 08.11.2012 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. 04/01/2013 Page 376/462 22.09.2008 08.08.2006 21.12.2005 18.10.2007 23.03.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10039175 RUAG AEROSPACE EASA.A.S.00200 REV. 2 DHC-6-300 Minor change to STC EASA.A.S.00200 by None The approval holder shall fulfil the 16.04.2012 adding the option to install aThommen AD32 obligations of Part 21, instead of the Shadin ADC 2000 Installation of Paragraph21.A109. Prior to installation of TAWS class A Honeywell MK VI incl. KMD-850 this modification it must be determined indicator inaccordance with Certification thatthe interrelationship between this Program Doc. T6-100 modification and any other previouslyinstalled modification and/ or repai 10013955 RUAG AEROSPACE SERVICES GmbH EASA.A.S.00505 BOMBARDIER CL-600-1A11 (CL- Upgrade Dual Honeywell FMS NZ-2000- 1. This STC is approved only for the product 12.01.2005 600 PRNAV. configuration as defined in the approved design BOMBARDIER CL-600-2A12 (CL- data referred to in the paragraph "Description". 601 Compatibility with other aircraft/engine BOMBARDIER CL-600-2B16 (CL- configurations shall be determined by the 601 installer. 10013956 RUAG AEROSPACE SERVICES GmbH EASA.A.S.00506 BOMBARDIER CL-600-1A11 (CL- Mode-S Transmitter Collins TDR 94D upgrade - 1. This STC is approved only for the product 12.01.2005 600 ELS/EHS; Associated Technical configuration as defined in the approved design BOMBARDIER CL-600-2A12 (CL- Documentation: Master Document List 100C- data referred to in the paragraph "Description". 601 MDL, Airplane Flight Manual Supplement 100C- Compatibility with other aircraft/engine BOMBARDIER CL-600-2B16 (CL- AFMS, Continued Airworthiness Plan 100C- configurations shall be determined by the 601 CAWP installer. 10013980 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01008 CESSNA 525 Installation of Honeywell EGPWS MK V with 10.04.2007 CESSNA 525A RAAS 10013981 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01012 BOMBARDIER CL-600-2B16 Installation of Honeywell EGPWS MK V. 1. This STC is approved only for the product 12.04.2005 BOMBARDIER CL-600-2B16 (CL- configuration as defined in the approved design 601 data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10014020 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01075 CESSNA 560 Installation of an ACAS II (TCAS 2000, CH 7) 1. This STC is approved only for the product 27.01.2005 with Dual Mode S Transponders ACSS RCZ- configuration as defined in the approved design 852-ELS/EHS. data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10014021 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01076 CESSNA 501 Installation of Dual Mode S Transponders ACSS RCZ-852-EHS 01.03.2005 10014034 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01107 CESSNA 550 Installation of TCAS 2000, CH 7 with Dual Mode S transponders ACSS RCZ-852-EHS- Master Document List, Doc No 147A-MDL 31.01.2005 10014035 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01108 CESSNA 550 BRAVO Upgrade of GPWS to EGPWS 10.02.2005 10014044 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01122 CESSNA 560 Installation of ACAS II CAS 67A with Dual Mode S Transponder RCZ-833 J-ELS 17.03.2005 10014060 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01144 CESSNA 560 (CITATION V) Installation of ACAS II (ACSS TCAS 2000, CH7) with Dual Mode S Transponders RCZ- 833J ELS 10.03.2005 10014085 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01176 REV. 1 BOMBARDIER CL-600-1A11 (CL- Upgrade of the two existing Mode-S 29.02.2008 600 Transponders ACSS RCZ-852 by ACSS BOMBARDIER CL-600-2A12 (CL- Service Bulletin 8002246-001 for 601 ELS/EHS.Replacement of the Controller, BOMBARDIER CL-600-2B16 (601- Collins CTL-92 by Mode S Controller, Collins 3A CTL-92E.ACSS Mode-S transponder RCZ-852 BOMBARDIER CL-600-2B16 (601- ELS/EHS with Collins CTL-92E. 3R 10014161 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01293 BOEING DC-9-82 (MD-82) Installation of Mode S Transponder ACSS XS- 28.06.2005 BOEING DC-9-83 (MD-83) 950 ELS/EHS with Control Gables G7490-66 including associated Airplane Flight Manual Supplement 10014189 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01331 CESSNA 525 Installation of ACAS II System with Dual Mode S Transponder. ELS compliant and EHS capable 18.07.2005 10014195 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01337 BOMBARDIER BD-700-1A10 Installation of MicroQAR acc.046A-SD 21.06.2005 10014204 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01355 BOMBARDIER DHC-8-400 Installation of VDL 4000/A VHF Data Link Mode 4 (CNS Systems) and installation of a combined VHF/GPS Antenna 18.07.2005 10014205 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01356 CESSNA 500, CITATION Installation of a TWS/RMI Sandel ST 3400 (TAWS Class B) 24.08.2005 10014206 RUAG AEROSPACE SERVICES GmbH EASA.A.S.01357 CESSNA 500, CITATION Installation of Dual Mode - S Transponder System Garmin GTX-330D - Elementary Surveillance. (Removel of the exising Rockwell Collins TDR-90 transponder). Installation of two additional L-Band Antennas on top of the fuselage. 24.08.2005 04/01/2013 Page 377/462
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: EASA STC no. STC holder Old STC ref
Page 375: EASA STC no. STC holder Old STC ref
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?