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 10040231 JET AVIONICS AVIATION & MARINE PA-31T CHEYENNE II General avionic improvement/installation - None. Prior to installation of this modification it 19.06.2012 Replacement of GPS, MovingMap, must be determined that Stormscope, Weather Radar system, TCAI I. heinterrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10016135 JET ENGINEERING LLC EASA.IM.A.S.02331 FAA STC ST01943LA DC-9-81 (MD-81) Installation of a JET Engineering, Ltd. This installation is done concurrently with STC 14.06.2007 DC-9-81 (MD-82) Advanced Jet Nozzles on the above airplane EASA.IM.E.S.01012, installation of Jet DC-9-81 (MD-83) model(s) when powered by Pratt & Whitney Engineeirng, Ldt. Turbine Exhaust Cone DC-9-81 (MD-87) JT8D-21JT8D-217, 7A, -217C, 219 engines Mixer(TECM), which modifies the Pratt & Whitney JT8D-217, JT8D-217A, -217C, -219 engines. 10016698 JET ENGINEERING LLC EASA.IM.E.S.01012 FAA STC ST01944LA PRATT & WHITNEY JT8D-217 Installation of a JET Engineering, Ltd. Turbine This installation must be done concurrently with 05.03.2007 PRATT & WHITNEY JT8D-217A Exhaust Cone Mixer (TECM) STC EASA.IM.A.S.02331, installation of Jet PRATT & WHITNEY JT8D-217C Engineering, Ltd. Advanced Jet Nozzles which PRATT & WHITNEY JT8D-219 modifies the airplane engine installation.Approval of this change in type design applies to the above engine model(s) o 10015249 JET ENGINEERING TECHNICAL SUPPORT 10031570 JET ENGINEERING TECHNICAL SUPPORT EASA.A.S.03688 BAE JETSTREAM 41 Mode-S Enhanced Surveillance (EHS) Upgrade P-EASA.A.S.03968 DORNIER 328-100, 328-300 Installation of Emergency Lighting Power Supply System 10016549 JETAIRE AEROSPACE, LLC EASA.IM.A.S.02929 REV. 2 FAA STC ST01466LA-D B737-300/-400 Installation of fire protection systems, lower cargo compartment Class Dto Class C conversion. Original FAA STC ST01466LA-D for B737-300;this revision is implementing the validation of FAA STC ST00749LA-D forB737- 400. 10015707 JETPROP, LLC. EASA.IM.A.S.01698 LBA STC SA1189 PIPER PA-46-310P PIPER PA-46-350P 10016000 JETPROP, LLC. EASA.IM.A.S.02158 ST00541SE PIPER PA-46-310P PIPER PA-46-350P 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. The install Installation of the following engines, propellers 1. This STC is valid only in connection with and associated hardware:Pratt & whitney PT6A-FAA STC SA00859AT (EMZ 0721/1076)2. 34 engine limited to 560 SHP at 2200 This airplane/engine/propeller combination is RPMPratt & Whitney PT6A-35 engine limited life limited. The life limit for the modified to 560 SHP at 2190 RPMPratt & Whitney airplane shall be detrmined by usingthe PT6A-21 engine limited to 550 SHP at 2200 minimum value calculated by the following f RP Installation of PWC PT6A-34/-35/-21 turboprop PT6A-34, rated at 560 HP, 2200 RPMPT6Aengines in any combination withHartzell 35, rated at 560 HP, 2190 RPMPT6A-21, Propellers:HC-E4N-3I/E8501B-3.5HC-E4N- rated at 550 HP, 2200 RPMThis 3M/E8190KHC-E4N-3N/D8292HC-E4N- airplane/engine/propeller combination is life 3N/D8292(B,K)-2and MT-Propeller:MTV-16-1- limited. The life limit for the modified airplane E-C-F-R(P)/CFR206-58aon Piper PA-46-310P shall be determined by using the minimum and PA-46-350P airp value calcul 10015892 JOE'S AIRCRAFT MODS LLC EASA.IM.A.S.02012 FAA STC SA564NE CESSNA F172-N Installation of a Textron Lycoming Model O-360- A4A, -A4M or -A4N engine and a Sensinech Model 76EM8S14-0-60 fixed Pitch metal propeller. 10034129 KAWAK AVIATION TECHNOLOGIES, INC. REV. 1 FAA STC SR01561SE KAMAN K-1200 Title: Auxiliary Hydraulic System, K-Max K1200 Helicopter Model 36300,DWG 36300, REV B, 25th June 2005Description: Auxiliary hydraulic power source provides hydraulic powerfor external implements used in fire fighting, logging, and agriculturaloperation. 10015824 KELOWNA FLIGHTCRAFT Ltd. EASA.IM.A.S.01896 SA04-32 BOMBARDIER CL-215-6B11 TCCA STC SA04-32 issue 3SPZ-4500 Honeywell AFCS and Universal UNS 1K/1L FMS 16.12.2008 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. 26.08.2010 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. 29.08.2012 26.10.2005 24.04.2008 08.11.2007 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. 21.03.2011 04/01/2013 Page 298/462 17.07.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10028498 KEYSTONE HELICOPTER P- REV. 1 FAA STC SR01127NY-D S-76A, S-76B, S-76C Installation of a Keystone Medical Interior - See As specified in the approved RFMS. RFMS N° 00549 is required for this 03.02.2010 CORPORATION EASA.IM.R.S.01562 Conditions installation with configurations 1,2,3,4,5 and 6 The following configurations are approved for this installation: Configuration No. 1 -P/N 02076-10E000- 1 Lifeport litter base installedwith one or two litters, control cab 10028501 KEYSTONE HELICOPTER CORPORATION 10028503 KEYSTONE HELICOPTER CORPORATION 10029641 KEYSTONE HELICOPTER CORPORATION 10030668 KEYSTONE HELICOPTER CORPORATION P- EASA.IM.R.S.01563 P- EASA.IM.R.S.01564 FAA STC SR00910NY S-76A, S-76B, S-76C Structural provisions for the installation of a Spectrolab SX5Searchlight to the left or right side of the S76. FAA STC SR00642NY S-76A, S-76B, S-76C Installation of a Liquid Oxygen System for Medevac use As specified in the approved RFMS. This STC covers the structural provisions 18.01.2010 for the installation of an SX5searchlight. Wiring and associated control of the SX5 and assessment ofthe effects on aircraft performance and handling must be the subject ofseparate modification action. Prior to ins - This approval should not be incorporated in any aircraft of thisspecific model on which other approved modifications are incorporated,unless it is determined that the interrelationship between this changeand any other previously incorporated approved mod Not Applicable 18.01.2010 FAA STC SR02588NY-D S-76C Installation of Goodrich Auxiliary Utility Hoist As specified in the approved RFMS Installation of the Auxiliary Hoist requires: 1. Pre-installation of the Goodrich Primary Hoist p/n 42325-18-1 inaccordance with Sikosrsky TC Option 33776-061154.and 2. On aircraft with Turbomeca Arriel 1S1 or 2S1 engines,pre-installation of FAA STC SR0161 FAA STC SR02597NY-D S92A Installation of a tail mounted, forward facing camera. 08.04.2010 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. 30.06.2010 10041473 KMLEX AVIATION INC. TCCA STC Q-LSA10-047/D FALCON 50EX Relocation of Radio Altimeter Restricted to S/N 278 Prior to installation of this modification it 19.09.2012 ConverterValidation of TCCA STC N° Q- must be determined thatthe LSA10-047/D issue dated November 04, 2010. interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10041475 KMLEX AVIATION INC. TCCA STC Q-LSA10-048/D FALCON 50EX Replacement of Aft lavatory faucet adapter - Dassault Falcon 50EXaircraft MSN 278Validation of TCCA STC N° Q-LSA10- 048/D issue dated November 04, 2010. 10015415 KNH AVIATION SERVICES, INC. EASA.IM.A.S.01136 FAA STC ST09993SC FAIRCHILD DORNIER DO 328- 300 FAA STC ST09993SC; 12 Seats configuration 1. This STC may be installed only in (extended to 14 seats throught minor change, combination with Change Notice CN-F0535, - part of Avcraft CN-F 0535)Installation of F0040,-F0125 owned by Avcraft Germany interior shell, cabinetry ,seats, card tables, and RUAG minor Changes “In Seat Power monitors, entertainment system, system wiring, Supply and FI Switch” and “Installation of and lavatory in accordance with Double Latches on drawers” .2. The water pumping syste 10015482 KNH AVIATION SERVICES, INC. EASA.IM.A.S.01242 FAA STC ST09468AC DORNIER D328-100 installation of a corporate/executive interior 1. According to the application as forwarded by FAA letter dated 27 April 2005 and FAA STC ST09468AC, the approval is limited to the aircraft S/N 30952. Furthermore this installation has to be performed in combination with the installation of FAA STC ST094 Restricted to S/N 278 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. 19.09.2012 04/01/2013 Page 299/462 20.06.2006 15.08.2005
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:
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: EASA STC no. STC holder Old STC ref
Page 297: EASA STC no. STC holder Old STC ref
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?