Computer Testing Supplement for IA.indb - Aviation Supplies ...

More documents

Recommendations

Info

Computer Testing Supplement for Inspection Authorization 2008 U.S. Department of Transportation FEDERAL AVIATION ADMINISTRATION Flight Standards Service
Page 4: Preface This publication was prepar
Page 7 and 8: SECTION II—AIRWORTHINESS DIRECTIV
Page 9 and 10: viii
Page 11 and 12: 1-2
Page 13 and 14: Alert Area. An alert area is establ
Page 15 and 16: Consensus standard means, for the p
Page 17 and 18: Flammable, with respect to a fluid
Page 19 and 20: Interstate air transportation means
Page 21 and 22: V FE means maximum flap extended sp
Page 23 and 24: Public aircraft means any of the fo
Page 25 and 26: Rotorcraft-load combination means t
Page 27 and 28: Weight-shift-control aircraft means
Page 29 and 30: MEA means minimum en route IFR alti
Page 31 and 32: V REF means reference landing speed
Page 33 and 34: 1-24
Page 35 and 36: (c) The acrobatic category is limit
Page 37 and 38: General §23.1301 Function and inst
Page 39 and 40: 1-30 (8) For each engine, an indica
Page 41 and 42: 1-32 Instruments: Installation §23
Page 43 and 44: (f) For commuter category airplanes
Page 45 and 46: (f) Each system must be designed so
Page 47 and 48: 1-38 (ii) A means must be accessibl
Page 49 and 50: (d) If the ability to reset a circu
Page 51 and 52: (c) Rear position light. The rear p
Page 53 and 54:
Where -- (a) Area A includes all di
Page 55 and 56:
§23.1416 Pneumatic de-icer boot sy
Page 57 and 58:
§23.1441 Oxygen equipment and supp
Page 59 and 60:
(f) If an automatic dispensing unit
Page 61 and 62:
(g) Each recorder container must: 1
Page 63 and 64:
23.1522 Auxiliary power unit limita
Page 65 and 66:
(d) Paragraphs (b)(1) through (b)(3
Page 67 and 68:
(e) The system voltage of each dire
Page 69 and 70:
1-60 (i) The maximum operating limi
Page 71 and 72:
(c) In addition to paragraph (a) of
Page 73 and 74:
23.1589 Loading information. The fo
Page 75 and 76:
1-66
Page 77 and 78:
Subpart B—Flight General 27.21 Pr
Page 79 and 80:
§27.1303 Flight and navigation ins
Page 81 and 82:
§27.1321 Arrangement and visibilit
Page 83 and 84:
§27.1335 Flight director systems.
Page 85 and 86:
(d) No explosive or toxic gases emi
Page 87 and 88:
§27.1387 Position light system dih
Page 89 and 90:
§27.1397 Color specifications. Eac
Page 91 and 92:
§27.1419 Ice protection. (a) To ob
Page 93 and 94:
(b) Each nonejectable recorder cont
Page 95 and 96:
§27.1519 Weight and center of grav
Page 97 and 98:
1-88 (3) The maximum allowable torq
Page 99 and 100:
§27.1551 Oil quantity indicator. E
Page 101 and 102:
(c) Weight and loading distribution
Page 103 and 104:
A27.3 Content. The contents of the
Page 105 and 106:
§39.17 What must I do if a change
Page 107 and 108:
(c) The holder of a repairman certi
Page 109 and 110:
1-100 (3) The name of the person pe
Page 111 and 112:
1-102 regulations, on each inoperat
Page 113 and 114:
§ 43.17 Maintenance, preventive ma
Page 115 and 116:
(4) Appliance major alterations. Al
Page 117 and 118:
1-108 (9) Refinishing decorative co
Page 119 and 120:
(c) Except as provided in paragraph
Page 121 and 122:
(j) Each person performing an annua
Page 123 and 124:
1-114 Table II—Test Tolerances Te
Page 125 and 126:
1-116 (iv) For Classes 1B, 2B, and
Page 127 and 128:
§ 45.13 Identification data. (a) T
Page 129 and 130:
§ 45.22 Exhibition, antique, and o
Page 131 and 132:
1-122 aircraft, an amateur-built ai
Page 133 and 134:
1-124 (2) For which an Airplane or
Page 135 and 136:
1-126 (2) The name and address (pri
Page 137 and 138:
(9) Fuel gauge indicating the quant
Page 139 and 140:
(b) Each emergency locator transmit
Page 141 and 142:
1-132 (2) Notwithstanding paragraph
Page 143 and 144:
1-134 (ii) In the airspace from the
Page 145 and 146:
1-136 (2) Firefighting operations.
Page 147 and 148:
1-138 (i) An explanation of the pro
Page 149 and 150:
§ 91.413 ATC transponder tests and
Page 151 and 152:
(c) For the purposes of this sectio
Page 153 and 154:
2-2
Page 155 and 156:
2-4
Page 157 and 158:
2-6
Page 159 and 160:
2-8 2. Visually inspect each bolt a
Page 161 and 162:
2-10
Page 163 and 164:
2-12
Page 165 and 166:
2-14
Page 167 and 168:
(d) An alternate method of complian
Page 169 and 170:
2-18 NOTE 1: Do not stop drill thes
Page 171 and 172:
(f) An alternative method of compli
Page 173 and 174:
(c) Compliance with the requirement
Page 175 and 176:
2-24 END OF SECTION 2
Page 177 and 178:
3-2
Page 179 and 180:
3-4
Page 181 and 182:
3-6
Page 183 and 184:
3-8
Page 185 and 186:
3-10
Page 187 and 188:
3-12
Page 189 and 190:
3-14
Page 191 and 192:
3-16
Page 193 and 194:
3-18
Page 195 and 196:
3-20
Page 197 and 198:
3-22
Page 199 and 200:
3-24
Page 201 and 202:
3-26
Page 203 and 204:
3-28
Page 205 and 206:
3-30
Page 207 and 208:
3-32
Page 209 and 210:
applicable to the aircraft. ultimat
Page 211 and 212:
3-36
Page 213 and 214:
3-38
Page 215 and 216:
3-40
Page 217 and 218:
3-42
Page 219 and 220:
3-44
Page 221 and 222:
3-46 Table 11.1—Instrument air co
Page 223 and 224:
3-48 PRESSURE DROP PER TEN FOOT LEN
Page 225 and 226:
TABLE 11-7. Examples of determining
Page 227 and 228:
3-52 Wire Size 8 6 4 2 1 0 00 000 0
Page 229 and 230:
(1) The wire size should be suffici
Page 231 and 232:
L 1=24 feet maximum run length for
Page 233 and 234:
FIGURE 11-2. Conductor chart, conti
Page 235 and 236:
FIGURE 11-4a. Single copper wire in
Page 237 and 238:
FIGURE 11-5. Bundle derating curves
Page 239 and 240:
3-64
Page 241 and 242:
3-66
Page 243 and 244:
3-68
Page 245 and 246:
3-70
Page 247 and 248:
4-2
Page 249 and 250:
(4) Group IV - Engine Ratings. Cove
Page 251 and 252:
Example: 4LIA (sometimes 4LAI) (1 )
Page 253 and 254:
I. Model 208, Caravan (cont’d) En
Page 255 and 256:
I. Model 208, Caravan (cont’d) 4
Page 257 and 258:
II. - Model 208B, Caravan (cont’d
Page 259 and 260:
Data Pertinent to All Models (cont
Page 262 and 263:
U.S. DEPARTMENT OF TRANSPORTATION F
Page 264 and 265:
TCDS E4EA PAGE 3 I. MODELS (cont.)
Page 266 and 267:
TCDS E4EA PAGE 5 I. MODELS (cont.)
Page 268 and 269:
TCDS E4EA PAGE 7 II. MODELS PT6A-38
Page 270 and 271:
TCDS E4EA PAGE 9 II. MODELS (contin
Page 272 and 273:
TCDS E4EA PAGE 11 IV. MODELS (conti
Page 274 and 275:
TCDS E4EA PAGE 13 NOTES NOTE 1. Max
Page 276 and 277:
TCDS E4EA PAGE 15 NOTE 2. (Cont.) O
Page 278 and 279:
TCDS E4EA PAGE 17 Tachometer (Tacho
Page 280 and 281:
TCDS E4EA PAGE 19 NOTE 5. External
Page 282 and 283:
TCDS E4EA PAGE 21 NOTE 13. (Cont.)
Page 284 and 285:
Page No. 1 2 Rev. No. 1 1 DEPARTMEN
Page 286 and 287:
Page No. 1 2 3 Rev. No. 3 2 2 DEPAR
Page 288:
P60GL Page 3 of 3 NOTE 2. Blade Mod
Page 291 and 292:
E252 Page 2 Model C90-8F C90-12F, -
Page 294 and 295:
DEPARTME0NT OF TRANSPORTATION FEDER
Page 296 and 297:
Center of Gravity Range (+84.0) to
Page 298 and 299:
Maximum Weight Normal Category: 240
Page 300 and 301:
Page 7 of 43 2A13 Propeller Spinner
Page 302 and 303:
Page 9 of 43 2A13 Fuel Capacity 84
Page 304 and 305:
Page 11 of 43 2A13 Manufacturer's S
Page 306 and 307:
Page 13 of 43 2A13 Propeller Spinne
Page 308 and 309:
Page 15 of 43 2A13 XI - Model PA-28
Page 310 and 311:
Lbs. Empty Weight C. G. Range None
Page 312 and 313:
Page 19 of 43 2A13 Propeller and Pr
Page 314 and 315:
Page 21 of 43 2A13 Takeoff - 2550 l
Page 316 and 317:
Page 23 of 43 2A13 Propeller and Pr
Page 318 and 319:
Oil Capacity 8 quarts at (+27.5) (6
Page 320 and 321:
Center of Gravity Range (+82.0) to
Page 322 and 323:
Propeller Spinner Hartzell P/N C356
Page 324 and 325:
Page 31 of 43 2A13 Engine Limits Fo
Page 326 and 327:
Page 33 of 43 2A13 Manufacturer's S
Page 328 and 329:
Page 35 of 43 2A13 For aircraft equ
Page 330 and 331:
Page 37 of 43 2A13 MODEL AFM/POH RE
Page 332 and 333:
Page 39 of 43 2A13 Unusable Fuel an
Page 334 and 335:
Page 41 of 43 2A13 NOTE 12 Maximum
Page 336:
Page 43 of 43 2A13 NOTE 23 McCauley
Page 339 and 340:
3A19 Page 2 of 19 I - Model 150, Mo
Page 341 and 342:
3A19 Page 4 of 19 III - Model 150G,
Page 343 and 344:
3A19 Page 6 of 19 V - Model 150L, 2
Page 345 and 346:
3A19 Page 8 of 19 VI - Model A150L
Page 347 and 348:
3A19 Page 10 of 19 VIII - Model A15
Page 349 and 350:
3A19 Page 12 of 19 X - Model A152 (
Page 351 and 352:
3A19 Page 14 of 19 Data Pertinent t
Page 353 and 354:
Page 355 and 356:
Page 358 and 359:
DEPARTMENT OF TRANSPORTATION FEDERA
Page 360 and 361:
Model Lycoming O-540 -J1A5D, -J2A5D
Page 362 and 363:
Page 5 of 8 E-295 -J1A5D -J2A5D -J3
Page 364 and 365:
NOTE 8. Fuel grade, compression and
Page 366 and 367:
Page 368 and 369:
Page 3 of 24 A7CE I - Model 411, Mo
Page 370 and 371:
Page 5 of 24 A7CE III - Model 402,
Page 372 and 373:
Page 7 of 24 A7CE III - Model 402,
Page 374 and 375:
Page 9 of 24 A7CE IV - Model 421, M
Page 376 and 377:
V - Model 414 (cont'd) Maximum Weig
Page 378 and 379:
VI - Model 421B (cont'd) Empty Wt.
Page 380 and 381:
Page 15 of 24 A7CE VII - Model 421C
Page 382 and 383:
Page 17 of 24 A7CE VIII - Model 414
Page 384 and 385:
Page 19 of 24 A7CE X - Model 425, C
Page 386 and 387:
Page 21 of 24 A7CE X - Model 425 (c
Page 388 and 389:
Page 23 of 24 A7CE NOTE 1. Current
Page 390 and 391:
Page 392 and 393:
Rev. 66 Page 3 of 37 3A13 II - Mode
Page 394 and 395:
Rev. 66 Page 5 of 37 3A13 III - Mod
Page 396 and 397:
Rev. 66 Page 7 of 37 3A13 IV - Mode
Page 398 and 399:
Rev. 66 Page 9 of 37 3A13 VI - Mode
Page 400 and 401:
Rev. 66 Page 11 of 37 3A13 VIII - M
Page 402 and 403:
Rev. 66 Page 13 of 37 3A13 IX - Mod
Page 404 and 405:
Rev. 66 Page 15 of 37 3A13 XI - Mod
Page 406 and 407:
Rev. 66 Page 17 of 37 3A13 XI - Mod
Page 408 and 409:
Rev. 66 Page 19 of 37 3A13 XII - Mo
Page 410 and 411:
Rev. 66 Page 21 of 37 3A13 Data Per
Page 412 and 413:
Page 414 and 415:
Page 416 and 417:
Page 418 and 419:
Page 420 and 421:
Rev. 66 Page 31 of 37 3A13 TR182, C
Page 422 and 423:
Page 424 and 425:
Rev. 66 Page 35 of 37 3A13 increase
Page 426:
Rev. 66 Page 37 of 37 3A13 Addition
Page 429 and 430:
A7SO 2 of 16 Propeller and Propelle
Page 431 and 432:
Page 433 and 434:
Page 435 and 436:
Page 437 and 438:
A7SO 10 of 16 Propeller and Propell
Page 439 and 440:
A7SO 12 of 16 Certification Basis M
Page 441 and 442:
A7SO 14 of 16 MODEL AFM/POH REPORT
Page 443 and 444:
A7SO 16 of 16 NOTE 8 Model PA-34-20
Page 445 and 446:
A11EA Page 2 Center of gravity (C.G
Page 447 and 448:
A11EA Page 4 III - Model AA-1B, Tra
Page 449 and 450:
A11EA Page 6 Fuel capacity 24 gal.
Page 451 and 452:
A11EA Page 8 All Models: NOTE 3. De
Page 453 and 454:
1A6 Page 2 of 15 Maximum Baggage 50
Page 455 and 456:
1A6 Page 4 of 15 Fuel Capacity 36 g
Page 457 and 458:
1A6 Page 6 of 15 Oil Capacity 2 gal
Page 459 and 460:
1A6 Page 8 of 15 Oil Capacity 2 gal
Page 461 and 462:
1A6 Page 10 of 15 4. Propeller (wit
Page 463 and 464:
1A6 Page 12 of 15 Electrical Equipm
Page 465 and 466:
1A6 Page 14 of 15 *405. Ross Contro
Page 468 and 469:
Page No. 1 2 3 4 5 6 Rev. No. 35 36
Page 470 and 471:
Page 3 E-273 Model O-470-H O-470-G,
Page 472 and 473:
Page 5 E-273 NOTE 6. O-470-B, -G, -
Page 474 and 475:
Page 476 and 477:
P57GL Page 3 of 5 Maximum Diameter
Page 478:
P57GL Page 5 of 5 NOTE 8. Not appli
Page 481 and 482:
P-920, Revision 29 Page 2 of 12 Max
Page 483 and 484:
P-920, Revision 29 Page 4 of 12 Cer
Page 485 and 486:
P-920, Revision 29 Page 6 of 12 Not
Page 487 and 488:
P-920, Revision 29 Page 8 of 12 Hub
Page 489 and 490:
P-920, Revision 29 Page 10 of 12 Hu
Page 491 and 492:
P-920, Revision 29 Page 12 of 12 Hu
Page 493 and 494:
2A4 2 I - Model 680 (cont’d) Airp
Page 495 and 496:
2A4 4 II. - Model 680-E (cont’d)
Page 497 and 498:
2A4 6 IV - MODEL 680-F (cont’d) b
Page 499 and 500:
2A4 8 V - Model 560-F (cont’d) Le
Page 501 and 502:
2A4 10 VI - Model 680-FL (cont’d)
Page 503 and 504:
2A4 12 VIII - MODEL 680-T (cont’d
Page 505 and 506:
2A4 14 IX - MODEL 680-V, 11 PCLM (N
Page 507 and 508:
2A4 16 XI - MODEL 681 (cont’d) Pr
Page 509 and 510:
2A4 18 XII - MODEL 690 (cont’d) M
Page 511 and 512:
2A4 20 XIV - MODEL 690A, 11 PCLM (N
Page 513 and 514:
2A4 22 XV - MODEL 690B (cont’d) A
Page 515 and 516:
2A4 24 XVI - MODEL 690C (cont’d)
Page 517 and 518:
2A4 26 XVIII - MODEL 695A, 11 PCLM
Page 519 and 520:
2A4 28 XIX - MODEL 690D (cont’d)
Page 521 and 522:
2A4 30 XX - MODEL 695B (cont’d) C
Page 523 and 524:
2A4 32 Equipment The basic required
Page 525 and 526:
2A4 34 NOTE 20: Model 695A Serial N
Page 527 and 528:
E-284 2 Certification basis: Regula
Page 529 and 530:
E-284 4 NOTE 8. For all models - we
Page 531 and 532:
A9CE Page 2 of 17 I. Model 188, AGw
Page 533 and 534:
A9CE Page 4 of 17 III. Model 188A,
Page 535 and 536:
A9CE Page 6 of 17 IV. Model A188A,
Page 537 and 538:
A9CE Page 8 of 17 V. Model 188B, AG
Page 539 and 540:
A9CE Page 10 of 17 VI. Model A188B
Page 541 and 542:
A9CE Page 12 of 17 NOTE 1. Current
Page 543 and 544:
A9CE Page 14 of 17 (d) (1) On flap
Page 545 and 546:
A9CE Page 16 of 17 The following ad
Page 548 and 549:
Page 550 and 551:
Rev. 77 3 3A12 II. Model 172A, Mode
Page 552 and 553:
Rev. 77 5 3A12 III. Model 172C (con
Page 554 and 555:
Rev. 77 7 3A12 V. Model 172I, 4 PCL
Page 556 and 557:
Rev. 77 9 3A12 VI. Model 172L (cont
Page 558 and 559:
Rev. 77 11 3A12 VII. Model 172M (co
Page 560 and 561:
Rev. 77 13 3A12 VIII. Model 172N (c
Page 562 and 563:
Rev. 77 15 3A12 X. Model 172Q (cont
Page 564 and 565:
Rev. 77 17 3A12 DATA PERTINENT TO A
Page 566 and 567:
Page 568 and 569:
Page 570 and 571:
Page 572 and 573:
Rev. 77 25 3A12 XI - Model 172R (co
Page 574 and 575:
Rev. 77 27 3A12 XI - Model 172R (co
Page 576 and 577:
Rev. 77 29 3A12 XII - Model 172S (c
Page 578:
Rev. 77 31 3A12 Data Pertinent to M
Page 581 and 582:
A16CE 2 Propeller and Landplane Pro
Page 583 and 584:
A16CE 4 Models 207A & T207A *Airspe
Page 585 and 586:
A16CE 6 (b) S/N 20700315 and up "Th
Page 587 and 588:
A16CE 8 B. Applicable to Models 207
Page 589 and 590:
A16CE 10 NOTE 3. Reserved. (10) (a)
Page 592 and 593:
Page 594 and 595:
Page 3 of 43 3A21 II - Model 210A (
Page 596 and 597:
Page 5 of 43 3A21 IV - Model 210-5
Page 598 and 599:
VI - Model 210E (cont’d) *Maximum
Page 600 and 601:
Page 9 of 43 3A21 VIII - Model 210F
Page 602 and 603:
Page 11 of 43 3A21 X - Model 210G,
Page 604 and 605:
Page 13 of 43 3A21 XII - Model 210J
Page 606 and 607:
Page 15 of 43 3A21 Models 210K/210L
Page 608 and 609:
Page 17 of 43 3A21 2. Model T210M (
Page 610 and 611:
Page 19 of 43 3A21 XV - Model P210N
Page 612 and 613:
Page 21 of 43 3A21 Model T210N (con
Page 614 and 615:
XVIII - Model T210R, 210R (cont’d
Page 616 and 617:
Page 25 of 43 3A21 Certification ba
Page 618 and 619:
Page 27 of 43 3A21 (4) On fuel sele
Page 620 and 621:
NOTE 2. (cont’d) (8) Near the eng
Page 622 and 623:
Page 31 of 43 3A21 NOTE 2. (cont’
Page 624 and 625:
Page 626 and 627:
Page 628 and 629:
Page 630 and 631:
Page 632 and 633:
NOTE 2. (cont’d) K. (22) On the m
Page 634:
NOTE 5. Service information applica
Page 637 and 638:
A3SO Page 2 of 31 I. - Model PA-32-
Page 639 and 640:
A3SO Page 4 of 31 II. - Model PA-32
Page 641 and 642:
A3SO Page 6 of 31 III. - Model PA-3
Page 643 and 644:
A3SO Page 8 of 31 IV. - Model PA-32
Page 645 and 646:
A3SO Page 10 of 31 V. - Model PA-32
Page 647 and 648:
A3SO Page 12 of 31 VII. - Model PA-
Page 649 and 650:
A3SO Page 14 of 31 VIII. - Model PA
Page 651 and 652:
A3SO Page 16 of 31 IX. - Model PA-3
Page 653 and 654:
A3SO Page 18 of 31 XI. - Model PA-3
Page 655 and 656:
A3SO Page 20 of 31 XII. - Model PA-
Page 657 and 658:
A3SO Page 22 of 31 XIII. - Model PA
Page 659 and 660:
A3SO Page 24 of 31 Oil Capacity 12
Page 661 and 662:
A3SO Page 26 of 31 23.967(e)(2) as
Page 663 and 664:
A3SO Page 28 of 31 Eff. 11/26/90; F
Page 665 and 666:
A3SO Page 30 of 31 Models PA-32-260
Page 667 and 668:
END OF SECTION 4
Page 669 and 670:
5-2
Page 671 and 672:
NOTICE Weight and balance or operat
Page 673 and 674:
OMB Control No. 2120-0018 09/30/200
Page 675:
5-8
show all

Computer Testing Supplement for IA.indb - Aviation Supplies ...

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?