31 July 2011 C1 CIVIL AVIATION DEPARTMENT HONG KONG ...

More documents

Recommendations

Info

HPMA No. Supp. Item Part Name Part No. Replacement Make ModelNo. No.For Eligibility EligibilityHPMA/141/0907 3 47 Assy-Floor A509262-245 A509262-245 Boeing 747-400PanelHPMA/141/0907 3 48 Assy-Floor A509262-246 A509262-246 Boeing 747-400PanelHPMA/141/0907 3 49 Assy-Floor A509262-247 A509262-247 Boeing 747-400PanelHPMA/141/0907 3 50 Assy-Floor A509262-248 A509262-248 Boeing 747-400PanelHPMA/141/0907 3 51 Assy-Floor A509262-249 A509262-249 Boeing 747-400PanelHPMA/141/0907 3 52 Assy-Floor A509262-250 A509262-250 Boeing 747-400PanelHPMA/141/0907 3 53 Assy-Floor A509262-251 A509262-251 Boeing 747-400PanelHPMA/141/0907 3 54 Assy-Floor A509262-252 A509262-252 Boeing 747-400PanelHPMA/141/0907 3 55 Assy-Floor A509262-253 A509262-253 Boeing 747-400PanelHPMA/141/0907 3 56 Assy-Floor A509262-254 A509262-254 Boeing 747-400PanelHPMA/141/0907 3 57 Assy-Floor A509262-255 A509262-255 Boeing 747-400PanelHPMA/141/0907 3 58 Assy-Floor A509262-256 A509262-256 Boeing 747-400PanelHPMA/141/0907 3 59 Assy-Floor A509262-239 A509262-239 Boeing 747-400PanelHPMA/141/0907 3 60 Assy-Floor A509262-263 A509262-263 Boeing 747-400PanelHPMA/141/0907 3 61 Assy-Floor A509262-264 A509262-264 Boeing 747-400PanelHPMA/141/0907 3 62 Assy-Floor A509262-265 A509262-265 Boeing 747-400PanelHPMA/141/0907 3 63 Assy-Floor A509262-266 A509262-266 Boeing 747-400PanelHPMA/141/0907 3 64 Assy-Floor A509262-267 A509262-267 Boeing 747-400AN-28 A2 P.531 January 2010
HPMA No. Supp. Item Part Name Part No. Replacement Make ModelNo. No.For Eligibility EligibilityPanelHPMA/141/0907 3 65 Floor Panel A509502-522 A509502-522 Boeing 747-400HPMA/141/0907 3 66 Floor Panel A509502-523 A509502-523 Boeing 747-400HPMA/141/0907 3 67 Floor Panel A509502-516 A509502-516 Boeing 747-400HPMA/141/0907 3 68 Floor Panel A509503-506 A509503-506 Boeing 747-400HPMA/141/0907 3 69 Floor Panel A509262-191 A509262-191 Boeing 747-400HPMA/141/0907 3 70 Floor Panel A509262-301 A509262-301 Boeing 747-400HPMA/141/0907 3 71 Floor Panel A509262-303 A509262-303 Boeing 747-400HPMA/141/0907 3 72 Floor Panel A509262-305 A509262-305 Boeing 747-400HPMA/141/0907 3 73 Floor Panel A509262-307 A509262-307 Boeing 747-400HPMA/141/0907 3 74 Floor Panel A509262-309 A509262-309 Boeing 747-400HPMA/141/0907 3 75 Floor Panel A509262-311 A509262-311 Boeing 747-400HPMA/141/0907 3 76 Floor Panel A509262-313 A509262-313 Boeing 747-400HPMA/141/0907 3 77 Floor Panel A509262-315 A509262-315 Boeing 747-400HPMA/141/0907 3 78 Floor Panel A509262-317 A509262-317 Boeing 747-400HPMA/141/0907 3 79 Floor Panel A509262-319 A509262-319 Boeing 747-400HPMA/141/0907 3 80 Floor Panel A509262-321 A509262-321 Boeing 747-400HPMA/141/0907 3 81 Floor Panel A509262-325 A509262-325 Boeing 747-400HPMA/141/0907 3 82 Floor Panel A509262-329 A509262-329 Boeing 747-400HPMA/141/0907 3 83 Floor Panel A509262-331 A509262-331 Boeing 747-400HPMA/141/0907 3 84 Floor Panel A509262-333 A509262-333 Boeing 747-400HPMA/141/0907 3 85 Floor Panel A509262-335 A509262-335 Boeing 747-400HPMA/141/0907 3 86 Floor Panel A509262-337 A509262-337 Boeing 747-400HPMA/141/0907 3 87 Floor Panel A509262-339 A509262-339 Boeing 747-400HPMA/141/0907 3 88 Floor Panel A509262-341 A509262-341 Boeing 747-400HPMA/141/0907 3 89 Floor Panel A509262-343 A509262-343 Boeing 747-400HPMA/141/0907 3 90 Floor Panel A509262-345 A509262-345 Boeing 747-400HPMA/141/0907 3 91 Floor Panel A505262-349 A505262-349 Boeing 747-400HPMA/141/0907 3 92 Floor Panel A509262-347 A509262-347 Boeing 747-400HPMA/141/0907 3 93 Floor Panel A509262-351 A509262-351 Boeing 747-400HPMA/141/0907 3 94 Floor Panel A509262-352 A509262-352 Boeing 747-400HPMA/141/0907 3 95 Floor Panel A509262-353 A509262-353 Boeing 747-400HPMA/141/0907 3 96 Floor Panel A509262-354 A509262-354 Boeing 747-40031 January 2010 AN-28 A2 P.6
Page 1 and 2:
CIVIL AVIATION DEPARTMENTHONG KONG,
Page 3 and 4:
NoticeNoIssue Date Subject30 5 30 S
Page 5 and 6:
NoticeNoIssue Date Subject65 * 1 31
Page 7 and 8:
[ * ] : Airworthiness Notices and/o
Page 9 and 10:
4.1 The contents list is re-issued
Page 11 and 12:
INTENTIONALLY LEFT BLANK31 January
Page 13 and 14:
Category B Helicopter. A single-eng
Page 15 and 16:
together necessary to provide thrus
Page 17 and 18:
Page 19 and 20:
Schedule 7Schedule 8Schedule 9− A
Page 21 and 22:
Page 23 and 24:
(b) Assembly - that items are fitte
Page 25 and 26:
(b)The holder of a Type Rated HKAR-
Page 27 and 28:
combination of theoretical and prac
Page 29 and 30:
continuation of certification privi
Page 31 and 32:
6 HKAR-66 Category B3 Aircraft Main
Page 33 and 34:
Certificates of Release to Service
Page 35 and 36:
3 Application3.1 The following appl
Page 37 and 38:
Airworthiness Notice No. 4Appendix
Page 39 and 40:
Page 41 and 42:
Page 43 and 44:
Government Printer, Hong Kong Speci
Page 45 and 46:
Airworthiness Notice No. 6Appendix
Page 47 and 48:
6.2 Foreign Airworthiness Directive
Page 49 and 50:
10.2 Light Aircraft Maintenance (CA
Page 51 and 52:
No. 21 Helicopter Public Address Sy
Page 53 and 54:
4 Requirement4.1 Bilingual Placard4
Page 55 and 56:
(1)No.(2)English Text(3)Chinese Tex
Page 57 and 58:
work detailed in the renewal form w
Page 59 and 60:
(e)any parachute including a parasc
Page 61 and 62:
Page 63 and 64:
(a)an aircraft of the type is regis
Page 65 and 66:
(b)A Rating granted in relation to
Page 67 and 68:
* 13.2 Radio-Coupled Automatic Pilo
Page 69 and 70:
Page 71 and 72:
Page 73 and 74:
Appendix Subject CAAIP Leaflet 11-2
Page 75 and 76:
AIRWORTHINESS NOTICE NO. 12APPENDIX
Page 77 and 78:
9 Due to the complexity and safety
Page 79 and 80:
Page 81 and 82:
Page 83 and 84:
handling organisations are made awa
Page 85 and 86:
NOTE: Resolution Advisories cannot
Page 87 and 88:
Page 89 and 90:
3.3 Organisations approved to HKAR-
Page 91 and 92:
7 Maintenance of Aircraft - Non-Com
Page 93 and 94:
9.5 Where it is intended to fit par
Page 95 and 96:
1 ApplicabilityAIRWORTHINESS NOTICE
Page 97 and 98:
Certificates of Release to Service
Page 99 and 100:
3.2 The organisation will be requir
Page 101 and 102:
one aircraft type or comparable tas
Page 103 and 104:
4 Limited AuthorisationsFlight Crew
Page 105 and 106:
which forms an integral part of the
Page 107 and 108:
Page 109 and 110:
4 CancellationThis Notice cancels A
Page 111 and 112:
It must be established by the owner
Page 113 and 114:
this Notice, then the following sta
Page 115 and 116:
7 Lease/Loan/Power-By-The-Hour Powe
Page 117 and 118:
Page 119 and 120:
in an aircraft, its engines or prop
Page 121 and 122:
When an aircraft is grounded at a l
Page 123 and 124:
Page 125 and 126:
aircraft, engine or propeller Type
Page 127 and 128:
All aircraft components must be rel
Page 129 and 130: AIRWORTHINESS NOTICE NO. 17APPENDIX
Page 131 and 132: accepted by CAD as in full complian
Page 133 and 134: (s) Manuals including:(1) * Mainten
Page 135 and 136: Note: ** Normally only required for
Page 137 and 138: INTENTIONALLY LEFT BLANK31 January
Page 139 and 140: 3.2 New Applications for Approvals
Page 141 and 142: Table 1:Classification of HKAR-1 Ce
Page 143 and 144: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 145 and 146: 5.1 Users of aircraft components an
Page 147 and 148: 9 CancellationThis Notice cancels N
Page 149 and 150: specialist organisation.2.4 Details
Page 151 and 152: 5 Guidance4.2.3 Log book entries mu
Page 153 and 154: of some component parts.2.3 The fun
Page 157 and 158: 4 ApplicationApplicant shall apply
Page 159 and 160: 3 Requirement and Applicability3.1
Page 161 and 162: e equipped with a ground proximity
Page 165 and 166: Performance Class 1 helicopter A he
Page 167 and 168: Part II, Chapter 5.7 Coding and reg
Page 169 and 170: 1 GeneralAIRWORTHINESS NOTICE NO. 2
Page 175 and 176: List of HKAR-147 approved maintenan
Page 177 and 178: Table 2:Non-Critical HPMA PartsHPMA
Page 179: HPMA No. Supp. Item Part Name Part
Page 183 and 184: HPMA No. Supp. Item Part Name Part
Page 187 and 188: (d)(e)(f)desiring to enhance cooper
Page 189 and 190: (c)(d)(e)in the case of serious non
Page 191 and 192: Certificate of Release to Service a
Page 193 and 194: (g)(h)(i)civil aircraft and/or airc
Page 197 and 198: Technical Records include but are n
Page 199 and 200: Party the opportunity to review and
Page 201 and 202: Authority in respect of any major m
Page 203 and 204: meanings as specified:(a)(b)(c)(d)(
Page 205 and 206: 2.5.6 Where maintenance involves th
Page 207 and 208: 4.1.1 A statement signed by the cur
Page 213 and 214: (d)The data obtained during the ins
Page 215 and 216: 6 Cancellationmean time, the provis
Page 219 and 220: a pressure gauge (reading up to 140
Page 221 and 222: unchanged. However engine power may
Page 225 and 226: and cabin crew seats as applicable,
Page 227 and 228: 4 Cancellationoperation is an all-c
Page 229 and 230: 2.6 ICAO has also published guidanc
Page 231 and 232:
(b)(c)Install a means for monitorin
Page 233 and 234:
when installed, shall be monitored.
Page 235 and 236:
Page 237 and 238:
4.3 It is recommended that in order
Page 239 and 240:
(c)(d)(e)(f)(g)(h)Ensure that any t
Page 241 and 242:
Minimum (RVSM) compliant aircraft.
Page 243 and 244:
Page 245 and 246:
shall be given in Overhaul Manuals.
Page 247 and 248:
Page 249 and 250:
Page 251 and 252:
(iii)Option Selectable Software (OS
Page 253 and 254:
3.3 Release of Required FLS or DFLD
Page 255 and 256:
een corrupted (e.g. making use of a
Page 257 and 258:
8 Procedure8.1 Configuration Contro
Page 259 and 260:
Page 261 and 262:
(f)That connecting a central electr
Page 263 and 264:
2.2 General Tool SelectionThe follo
Page 265 and 266:
2.5 Control and Suitability of Tool
Page 267 and 268:
epair, modification and partial or
Page 269 and 270:
Page 271 and 272:
4 ImplementationSub-section 1.2-5,
Page 273 and 274:
Page 275 and 276:
and paragraph 11.4 of Document DO-1
Page 277 and 278:
RELATIONSHIP BETWEEN FUNCTION CRITI
Page 279 and 280:
(b)Criticality Categories and Softw
Page 281 and 282:
Page 283 and 284:
3.2 Fatigue3.3 StressTiredness and
Page 285 and 286:
4 SummaryThe effects of illness, in
Page 287 and 288:
(vi)(vii)(viii)(ix)Drugs for the re
Page 289 and 290:
2.3 Each approved organisation is r
Page 291 and 292:
(paragraph 3).4.3 Overseas Organisa
Page 293 and 294:
Page 295 and 296:
Page 297 and 298:
7 Concessions against any inspectio
Page 299 and 300:
5 CancellationThis Notice cancels A
Page 301 and 302:
Page 303 and 304:
or revised service information, rev
Page 305 and 306:
NOTE: 'Designated' emergency exits
Page 307 and 308:
FAR/JAR 25.812(l)(1) requirement ca
Page 309 and 310:
Page 311 and 312:
Page 313 and 314:
Page 315 and 316:
Page 317 and 318:
although not required by this Notic
Page 319 and 320:
and 121-198 respectively. Similar a
Page 321 and 322:
Page 323 and 324:
Page 325 and 326:
C25inches(Ref para 5.1)(Ref para 4.
Page 327 and 328:
Page 329 and 330:
design to ensure repeatable in-serv
Page 331 and 332:
(d)(e)(f)(g)(h)Identify any feature
Page 333 and 334:
Page 335 and 336:
Box 4Box 5The question takes into a
Page 337 and 338:
IFE Scheduled Maintenance Tasks and
Page 339 and 340:
4 RequirementPortable oxygen equipm
Page 341 and 342:
CAD Approved Certificate will be re
Page 343 and 344:
2.5 Other potential benefits may ac
Page 345 and 346:
y organisations albeit too often on
Page 347 and 348:
(c)The Director-General will not, a
Page 349 and 350:
(e)(f)the person concerned has atte
Page 351 and 352:
Page 353 and 354:
Page 355 and 356:
AIRWORTHINESS NOTICE No. 74APPENDIX
Page 357 and 358:
Page 359 and 360:
3.4 The periods of operation or ela
Page 361 and 362:
Page 363 and 364:
power switching relays, their physi
Page 365 and 366:
Page 367 and 368:
(g)a process for conducting periodi
Page 369 and 370:
Page 371 and 372:
3.3 All aeroplanes defined in parag
Page 373 and 374:
Figure 2 MINIMUM ACCESS REQUIRED BY
Page 375 and 376:
acks must be in the upright (take-o
Page 377 and 378:
Page 379 and 380:
Certificate is made after the 16 Ju
Page 381 and 382:
2 Requirement2.1 Compliance with pa
Page 383 and 384:
should include adequate battery cap
Page 385 and 386:
(a)(b)reduction of the generating s
Page 387 and 388:
3.2 Applications for the approval o
Page 389 and 390:
3 ComplianceAll applicable aircraft
Page 391 and 392:
5 Additional Information5.1 EASA CS
Page 393 and 394:
Page 395 and 396:
to be operated under IFR with non-i
Page 397 and 398:
3.3 For example, class of emission
Page 399 and 400:
3.2 All aeroplanes flying for the p
Page 401 and 402:
Page 403 and 404:
Page 405 and 406:
and with the associated Declaration
Page 407 and 408:
Personnel Certification scheme. In
Page 409 and 410:
Quality Procedures.6 Suppliers and
Page 411 and 412:
Qualification: The proven ability o
Page 413 and 414:
continued standard of NDT work carr
Page 415 and 416:
5 Cancellation"guidance" of a Level
Page 417 and 418:
2.5 The test must be performed at a
Page 419 and 420:
shorter wavelength light.7 Cancella
Page 421 and 422:
3.6 Parts that cannot be returned t
Page 423 and 424:
5.6 Questionable part numbers, frau
Page 425 and 426:
case. If such evidence cannot be ob
Page 427 and 428:
This Notice cancels Airworthiness N
Page 429 and 430:
3 Compliancethat these requirements
Page 431 and 432:
unit and any other galley insert wh
Page 433 and 434:
With effect from 1 January 2009, al
Page 435 and 436:
Page 437 and 438:
The position of safety belt buckle
Page 439 and 440:
its removal from the water.5 Additi
Page 441 and 442:
4 Requirement4.1 Performance Levels
Page 443 and 444:
equired, the helicopter shall compl
Page 445 and 446:
3.9 Compliance requirements for hel
Page 447 and 448:
4.5 Type IVA FDR Requirements4.5.1
Page 449 and 450:
Page 451 and 452:
4.2.3 The following provides guidan
Page 453 and 454:
- Emergency tracheal catheter (or l
Page 455 and 456:
Page 457 and 458:
Page 459 and 460:
Page 461 and 462:
4.7 RNP AR APCHRNP equipages comply
Page 463 and 464:
2.5 ADS-B based surveillance provid
Page 465 and 466:
Page 467 and 468:
Page 469:
a. For the purpose of this Article,
show all

31 July 2011 C1 CIVIL AVIATION DEPARTMENT HONG KONG ...

Create successful ePaper yourself

Delete template?

Save as template?