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

More documents

Recommendations

Info

TCDS E4EA PAGE 17 Tachometer (Tachometer and overspeed governor <strong>for</strong> PT6A-6,-6A,-6B and-20 only) C 0.1264(PT6A-15AG, -25C,-27,-28,-29,-34,- 34B,-34AG,-35,-36,- 38,-40,-41,-41AG,- 42,-42A,-52, -61,- 61A) 0.1263 (B-35F); 0.1273(PT6A-6,-6A,- 6B,-11,-11AG,-20,- 20A,-20B,-6/C20,-21,- 25,-25A,-110,-112 114, 114A, -116, 121,- 135,-135A); 0.1405 (45, 45A, 45B, 45R, 60, 60A, 60AG, 65B, 65R, 65AR, 65AG) 7 100 10 NOTE 4. (Cont'd) Driven by Power Rotating Facing Speed Ratio Maximum Torque Maximum Turbine Drive Pad (to Turbine) Continuous Static Overhang (in. - lbs.) Propeller Governor C 0.1264(PT6A-15AG, 50 850 25 and Overspeed -25C,-27,-28,-29,-34,-34B,- Governor* 34AG,-35,-36,-38,-40,-41,- 41AG,-42,-42A,-52,-61,-61A) 0.1273(PT6A-6,-6A,-6B,-11,- 11AG,-20,-20A,-20B,-6/C20,- 21,-25,-25A,-110,-112 114, 114A, -116, 121,-135,- 135A); 0.1405(PT6A-45, 45A, 45B, 45R, 60, 60A, 60AG, 65B, 65R, 65AR, 65AG) * May be an optional drive, which is not included in the basic engine weight, is included. The hydraulic pump drive requires the aircraft accessory drive to complete the train. Cabin pressurization may be provided by the approved combination of the Beech Aircraft Corporation Gearbox No. 50-9903 with the Godfrey Engineering type 9 cabin supercharger, mounted directly on the accessories gearbox. PT6A-38,-40,-41,-41AG,-42,-42A are approved <strong>for</strong> operation with an accessory mounted on the reduction gearbox and belt driven from the propeller assembly provided that the accessory is mounted and driven in accordance with the location dimensions and weight prescribed in Sheet 5 of Drawing Number 3018500, revision dated August 20, 1973. C = Clockwise CC = Counterclockwise
TCDS E4EA PAGE 18 Accessory Drive Provisions: (PT6A-50 only) Maximum Driven by Gas Rotating Facing Speed Ratio Maximum Torque Overhang Generator Turbine Drive Pad (to Turbine) Continuous Static (in. - lbs.) Tachometer Accessory Gearbox CC 0.112 7 100 10 Starter and/or Generator C 0.293 170 1600 230 Hydraulic Pump* CC 0.204 150 800 30 Driven by Power Turbine Tachometer CC 0.1400 7 100 10 Alternator C 0.529 120 1600 105 Prop. Governor CC 0.1400 100 1700 40 Prop. Overspeed Governor CC 0.1400 50 850 25
Page 2:
Computer Testing Supplement for Ins
Page 6 and 7:
Table of Contents Preface .........
Page 8 and 9:
• A7S0, Piper PA-34-200 • A11EA
Page 10 and 11:
Section I: Title 14 of the Code of
Page 12 and 13:
§ 1.1 General definitions. PART 1
Page 14 and 15:
Category B, with respect to transpo
Page 16 and 17:
(1) An ETOPS group 1 Significant Sy
Page 18 and 19:
Glider means a heavier-than-air air
Page 20 and 21:
Long-range communication system (LR
Page 22 and 23:
Overseas air transportation means t
Page 24 and 25:
Rated maximum continuous augmented
Page 26 and 27:
(2) With respect to turbine engines
Page 28 and 29:
ETOPS means extended operations. EW
Page 30 and 31:
SSALS means simplified short approa
Page 32 and 33:
(2) May is used in a permissive sen
Page 34 and 35:
§ 23.1 Applicability. PART 23—AI
Page 36 and 37:
(i) The highest weight selected by
Page 38 and 39:
[Doc. No. 4080, 29 FR 17955, Dec. 1
Page 40 and 41:
significantly reduce the capability
Page 42 and 43:
(1) The instrument that most effect
Page 44 and 45:
[Amdt. 23-1, 30 FR 8261, June 29, 1
Page 46 and 47:
(2) Each exposed sight gauge used a
Page 48 and 49:
[Doc. No. 4080, 29 FR 17955, Dec. 1
Page 50 and 51:
(c) Main power cables (including ge
Page 52 and 53:
(c) Rear position light installatio
Page 54 and 55:
system is observed from a distance,
Page 56 and 57:
(c) For those airplanes required to
Page 58 and 59:
(d) As used in this section: (1) BT
Page 60 and 61:
§23.1457 Cockpit voice recorders.
Page 62 and 63:
23.1511 Flap extended speed. (a) Th
Page 64 and 65:
23.1541 General. (a) The airplane m
Page 66 and 67:
(1) Each fuel tank selector control
Page 68 and 69:
(2) Stating that recovery must be i
Page 70 and 71:
(3) Acrobatic category airplanes. A
Page 72 and 73:
(4) The effect on landing distances
Page 74 and 75:
ecommended at these periods. Howeve
Page 76 and 77:
Subpart A—General §27.1 Applicab
Page 78 and 79:
(3) The portion of the total weight
Page 80 and 81:
warn the pilot of the occurrence of
Page 82 and 83:
(c) Except as provided in paragraph
Page 84 and 85:
(2) Compliance with paragraph (a)(1
Page 86 and 87:
§27.1365 Electric cables. (a) Each
Page 88 and 89:
§27.1391 Minimum intensities in th
Page 90 and 91:
where: Ie=effective intensity (cand
Page 92 and 93:
(2) By installing a continually ene
Page 94 and 95:
§27.1505 Never-exceed speed. (a) T
Page 96 and 97:
(i) The maximum value determined by
Page 98 and 99:
(b) Each arc and line must be wide
Page 100 and 101:
(2) Oil filler openings must be mar
Page 102 and 103:
(ii) The maximum safe wind for oper
Page 104 and 105:
PART 39—AIRWORTHINESS DIRECTIVES
Page 106 and 107:
PART 43—MAINTENANCE, PREVENTIVE M
Page 108 and 109:
§ 43.5 Approval for return to serv
Page 110 and 111:
is permanently removed from use on
Page 112 and 113:
(b) Rotorcraft. Each person perform
Page 114 and 115:
Appendix A to Part 43—Major Alter
Page 116 and 117:
(2) Powerplant major repairs. Repai
Page 118 and 119:
(31) Removing and replacing self-co
Page 120 and 121:
(3) Internal engine—for cylinder
Page 122 and 123:
(vi) Barometric scale error. At con
Page 124 and 125:
Appendix F to Part 43—ATC Transpo
Page 126 and 127:
§ 45.1 Applicability. This part pr
Page 128 and 129:
§ 45.14 Identification of critical
Page 130 and 131:
§ 45.25 Location of marks on fixed
Page 132 and 133:
§ 91.1 Applicability. PART 91—GE
Page 134 and 135:
hospital, or doctor, or other perso
Page 136 and 137:
§§ 91.27-91.99 [Reserved] § 91.2
Page 138 and 139:
(i) Airplanes with a third attitude
Page 140 and 141:
(11) On and after January 1, 2004,
Page 142 and 143:
(iv) Required to be operational by
Page 144 and 145:
(5) Accept necessary barometric pre
Page 146 and 147:
§ 91.407 Operation after maintenan
Page 148 and 149:
(g) Inspection program approved und
Page 150 and 151:
(iii) The time since last overhaul
Page 152 and 153:
Section II: Airworthiness Directive
Page 154 and 155:
MESSERSCHMITT-BOLKOW-BLOHM-GMBH AND
Page 156 and 157:
AGUSTA, COSTRUZIONI AERONAUTICHE GI
Page 158 and 159:
BEECH =============================
Page 160 and 161:
d. Coat entire portion of bolt that
Page 162 and 163:
AIR TRACTOR, INC. =================
Page 164 and 165:
BENDIX ============================
Page 166 and 167:
ENSTROM ===========================
Page 168 and 169:
BEECH =============================
Page 170 and 171:
BEECH AIRCRAFT CORPORATION ========
Page 172 and 173:
PRATT & WITHEY AIRCRAFT OF CANADA,
Page 174 and 175:
(j) Install a CT stator assembly, a
Page 176 and 177:
Section III: Exhibits • Exhibit 1
Page 178 and 179:
Rivet identifi cation and part numb
Page 180 and 181:
Aircraft rivet identification. EXHI
Page 182 and 183:
Aircraft rivet identification. (con
Page 184 and 185:
Thickness “t” in inches No. of
Page 186 and 187:
Page 188 and 189:
Page 190 and 191:
Recommended radii for 90° bends in
Page 192 and 193:
Minimum Bend Radius for Aluminum Al
Page 194 and 195:
3-19 RADIUS THICKNESS 1/32 .031 1/1
Page 196 and 197:
EXHIBIT 10 K-chart for determining
Page 198 and 199:
. . DATUM D C.G. L . . NOSE WHEEL T
Page 200 and 201:
COMPUTED WEIGHING POINT (C MAIN WHE
Page 202 and 203:
NOSE SCALE 464 LBS. TARE 10 LBS. We
Page 204 and 205:
FULL OIL EXHIBIT 14 Example of chec
Page 206 and 207:
FULL OIL EXHIBIT 15 Example of chec
Page 208 and 209:
1. GENERAL. The minimum airworthine
Page 210 and 211:
Utility Category Aircraft (FAR 23)
Page 212 and 213:
EXHIBIT 17 Turnbuckle safetying gui
Page 214 and 215:
Straight-shank terminal dimensions
Page 216 and 217:
BEND RADIUS INCHES 3 — 2 — 1
Page 218 and 219:
MINIMUM BEND RADIUS (INCHES) 16 15
Page 220 and 221:
211. GENERAL. This chapter contains
Page 222 and 223:
differential of 5.53 in. Hg, i.e.,
Page 224 and 225:
DC wire and circuit protector chart
Page 226 and 227:
Where: T1 T2 TR I2 Imax TABLE 11-9.
Page 228 and 229: 11-67. METHODS FOR DETERMINING CURR
Page 230 and 231: (1) The wire run is 15.5 feet long,
Page 232 and 233: STEP 1: Refer to the “single wire
Page 234 and 235: FIGURE 11-3. Conductor chart, inter
Page 236 and 237: FIGURE 11-4b. Single copper wire in
Page 238 and 239: FIGURE 11-6. Altitude derating curv
Page 240 and 241: Minimum Equipment List Page MINIMUM
Page 242 and 243: EXHIBIT 24 Bend Allowance = 2π (R
Page 244 and 245: EXHIBIT 25 c = 2π a 2 + b 2 2 Circ
Page 246 and 247: Section IV: Type Certificate Data S
Page 248 and 249: TCDS BACKGROUND INFORMATION Type Ce
Page 250 and 251: Coded Entries Many aircraft and eng
Page 252 and 253: DEPARTMENT OF TRANSPORTATION FEDERA
Page 254 and 255: I. Model 208, Caravan (cont’d) 3
Page 256 and 257: II. - Model 208B, Caravan (cont’d
Page 258 and 259: Data Pertinent to All Models (cont
Page 260: Data Pertinent to All Models (cont
Page 263 and 264: TCDS E4EA PAGE 2 IV. MODEL TYPE (se
Page 265 and 266: TCDS E4EA PAGE 4 I. MODELS (Cont.))
Page 267 and 268: TCDS E4EA PAGE 6 I. MODELS (cont.)
Page 269 and 270: TCDS E4EA PAGE 8 II. MODELS PT6A-45
Page 271 and 272: TCDS E4EA PAGE 10 III. MODELS (cont
Page 273 and 274: TCDS E4EA PAGE 12 PT6A-28 PT6A-29 P
Page 275 and 276: TCDS E4EA PAGE 14 NOTE 1.(continued
Page 277: TCDS E4EA PAGE 16 Maximum Continuou
Page 281 and 282: TCDS E4EA PAGE 20 NOTE 7. The maxim
Page 283 and 284: TCDS E4EA PAGE 22 NOTE 13. (Cont'd)
Page 285 and 286: P9NE 2 NOTE 2. Blade Model Designat
Page 287 and 288: P60GL Page 2 of 3 Certification Bas
Page 290 and 291: Page No. 1 2 3 Rev. No. 29 29 29 Re
Page 292: E-252 Page 3 The Model 0-200-C is s
Page 295 and 296: 2A13 Page 2 of 43 Center of Gravity
Page 297 and 298: 2A13 Page 4 of 43 Propeller Spinner
Page 299 and 300: 2A13 Page 6 of 43 Propeller Spinner
Page 301 and 302: 2A13 Page 8 of 43 VI - Model PA-28-
Page 303 and 304: 2A13 Page 10 of 43 Center of Gravit
Page 305 and 306: 2A13 Page 12 of 43 Empty Weight C.
Page 307 and 308: 2A13 Page 14 of 43 X - Model PA-28R
Page 309 and 310: 2A13 Page 16 of 43 Control Surface
Page 311 and 312: 2A13 Page 18 of 43 Engine Limits Fo
Page 313 and 314: 2A13 Page 20 of 43 Manufacturer's S
Page 315 and 316: 2A13 Page 22 of 43 Center of Gravit
Page 317 and 318: 2A13 Page 24 of 43 XVI - B. Model P
Page 319 and 320: 2A13 Page 26 of 43 No. of Seats Nor
Page 321 and 322: 2A13 Page 28 of 43 Airspeed Limits
Page 323 and 324: 2A13 Page 30 of 43 Propeller and Pr
Page 325 and 326: 2A13 Page 32 of 43 Engine Limits Fo
Page 327 and 328: 2A13 Page 34 of 43 Manufacturer's S
Page 329 and 330:
2A13 Page 36 of 43 PA-28-236: CAR 3
Page 331 and 332:
2A13 Page 38 of 43 (Continued) MODE
Page 333 and 334:
2A13 Page 40 of 43 NOTE 3 The Model
Page 335 and 336:
2A13 Page 42 of 43 NOTE 20 PA-28-18
Page 338 and 339:
DEPARTMENT OF TRANSPORTATION FEDERA
Page 340 and 341:
II - Model 150D, Model 150E, Model
Page 342 and 343:
IV - Model A150K, Aerobat, 2 PCLM (
Page 344 and 345:
V - Model 150L (cont’d) Page 7 of
Page 346 and 347:
VII - Model 150M (cont’d) Page 9
Page 348 and 349:
IX - Model 152 (cont'd) Page 11 of
Page 350 and 351:
X - Model A152 (cont’d) Page 13 o
Page 352 and 353:
Data Pertinent to All Models (cont
Page 354 and 355:
Page 17 of 19 3A19 Data Pertinent t
Page 356:
Data Pertinent to All Models (cont
Page 359 and 360:
E-295 Page 2 of 8 Model Lycoming O-
Page 361 and 362:
E-295 Page 4 of 8 Certification bas
Page 363 and 364:
E-295 Page 6 of 8 NOTE 5. These mod
Page 365 and 366:
E-295 Page 8 of 8 NOTE 12. When equ
Page 367 and 368:
A7CE Page 2 of 24 Propeller and or
Page 369 and 370:
A7CE Page 4 of 24 II - Model 401, M
Page 371 and 372:
A7CE Page 6 of 24 III - Model 402,
Page 373 and 374:
A7CE Page 8 of 24 IV - Model 421, M
Page 375 and 376:
A7CE Page 10 of 24 V - Model 414 (N
Page 377 and 378:
A7CE Page 12 of 24 VI - Model 421B
Page 379 and 380:
A7CE Page 14 of 24 VII - Model 421C
Page 381 and 382:
A7CE Page 16 of 24 VIII - Model 414
Page 383 and 384:
A7CE Page 18 of 24 IX - Model 402C
Page 385 and 386:
A7CE Page 20 of 24 X - Model 425 (c
Page 387 and 388:
A7CE Page 22 of 24 X - Model 425 (c
Page 389 and 390:
A7CE Page 24 of 24 NOTE 3. (cont'd.
Page 391 and 392:
3A13 Page 2 of 37 Rev. 66 I - Model
Page 393 and 394:
3A13 Page 4 of 37 Rev. 66 II - Mode
Page 395 and 396:
3A13 Page 6 of 37 Rev. 66 IV - Mode
Page 397 and 398:
3A13 Page 8 of 37 Rev. 66 V - Model
Page 399 and 400:
3A13 Page 10 of 37 Rev. 66 VII - Mo
Page 401 and 402:
3A13 Page 12 of 37 Rev. 66 VIII - M
Page 403 and 404:
3A13 Page 14 of 37 Rev. 66 X - Mode
Page 405 and 406:
3A13 Page 16 of 37 Rev. 66 Model TR
Page 407 and 408:
3A13 Page 18 of 37 Rev. 66 Model 18
Page 409 and 410:
3A13 Page 20 of 37 Rev. 66 Data Per
Page 411 and 412:
Page 413 and 414:
Page 415 and 416:
3A13 Page 26 of 37 Rev. 66 Long ran
Page 417 and 418:
3A13 Page 28 of 37 Rev. 66 (3) On t
Page 419 and 420:
Page 421 and 422:
3A13 Page 32 of 37 Rev. 66 XIII - M
Page 423 and 424:
3A13 Page 34 of 37 Rev. 66 Special
Page 425 and 426:
3A13 Page 36 of 37 Rev. 66 Oil Capa
Page 428 and 429:
Page 430 and 431:
Maximum Weight S/N 34-7250215 throu
Page 432 and 433:
5 of 16 A7SO Maximum Weight 4570 lb
Page 434 and 435:
Maximum Weight 4773 lb. - Ramp 4750
Page 436 and 437:
Oil Capacity 8 qts. per engine (5 q
Page 438 and 439:
11 of 16 A7SO Control Surface Movem
Page 440 and 441:
13 of 16 A7SO Equipment The basic r
Page 442 and 443:
15 of 16 A7SO The Model PA-34-200T;
Page 444 and 445:
Page No. 1 2 3 4 5 6 7 8 Rev. No. 1
Page 446 and 447:
Page 3 A11EA 3. McCauley Model 1A10
Page 448 and 449:
Oil capacity 6 qt. at (+39) (2 qt.
Page 450 and 451:
UTILITY CATEGORY AA-1 AA-1A Maximum
Page 452 and 453:
Page 454 and 455:
Page 3 of 15 1A6 Maximum Baggage50
Page 456 and 457:
Page 5 of 15 1A6 Fuel Capacity 36 g
Page 458 and 459:
Page 7 of 15 1A6 Fuel Capacity 36 g
Page 460 and 461:
Page 9 of 15 1A6 Required Equipment
Page 462 and 463:
Page 11 of 15 1A6 105. Vacuum pump
Page 464 and 465:
Page 13 of 15 1A6 (w) FAA-DOA appro
Page 466:
Page 15 of 15 1A6 (3) On left side
Page 469 and 470:
E-273 Page 2 Model O-470-A O-470-E
Page 471 and 472:
E-273 Page 4 NOTE 3. The following
Page 473 and 474:
E-273 Page 6 NOTE 13. The following
Page 475 and 476:
P57GL Page 2 of 5 Maximum Diameter
Page 477 and 478:
P57GL Page 4 of 5 NOTE 3. Pitch Con
Page 480 and 481:
DEPARTMENT OF TRANSPORTATION P-920
Page 482 and 483:
Page 3 of 12 P-920, Revision 29 Max
Page 484 and 485:
Note 2: Blade Model Designation (Se
Page 486 and 487:
Note 9: Special Limits Page 7 of 12
Page 488 and 489:
Page 9 of 12 P-920, Revision 29 Hub
Page 490 and 491:
Page 11 of 12 P-920, Revision 29 Hu
Page 492 and 493:
Page 494 and 495:
3 2A4 II. - Model 680-E (cont’d)
Page 496 and 497:
5 2A4 III. - Model 720 (cont’d) L
Page 498 and 499:
V - Model 560-F, 7 PCLM (Normal Cat
Page 500 and 501:
9 2A4 VI - Model 680-FL (cont’d)
Page 502 and 503:
11 2A4 VII - MODEL 680-FL(P) (cont
Page 504 and 505:
13 2A4 IX - MODEL 680-V, 11 PCLM (N
Page 506 and 507:
15 2A4 X - MODEL 680-W (cont’d) D
Page 508 and 509:
17 2A4 XI - MODEL 681 (cont’d) Se
Page 510 and 511:
19 2A4 XIII - MODEL 685 (cont’d)
Page 512 and 513:
XIV - MODEL 690A (cont’d) Maximum
Page 514 and 515:
23 2A4 XVI - MODEL 690C, 11 PCLM (N
Page 516 and 517:
25 2A4 XVII - MODEL 695 (cont’d)
Page 518 and 519:
27 2A4 XVIII - MODEL 695A (cont’d
Page 520 and 521:
29 2A4 XIX - MODEL 690D (cont’d)
Page 522 and 523:
31 2A4 Specifications Pertinent to
Page 524 and 525:
33 2A4 NOTE 6: Model 680FL S/N 1471
Page 526 and 527:
Page No. 1 2 3 4 Rev. No. 9 9 9 9 R
Page 528 and 529:
3 E-284 NOTE 4. The "6" in the engi
Page 530 and 531:
Page 532 and 533:
Page 3 of 17 A9CE II. Model A188, A
Page 534 and 535:
III. Model 188A, AGwagon "A" & "B"
Page 536 and 537:
V. Model 188B, AGpickup (cont'd) *E
Page 538 and 539:
Page 9 of 17 A9CE VI. Model A188B (
Page 540 and 541:
VII. Model T188C (cont'd) Number of
Page 542 and 543:
Page 13 of 17 A9CE Reference weight
Page 544 and 545:
Page 15 of 17 A9CE Fuel Flows at Fu
Page 546:
NOTE 8. 14 volt electrical system 1
Page 549 and 550:
3A12 2 Rev. 77 I. Model 172 (cont'd
Page 551 and 552:
3A12 4 Rev. 77 II. Model 172A, Mode
Page 553 and 554:
3A12 6 Rev. 77 IV. Model 172D, Mode
Page 555 and 556:
3A12 8 Rev. 77 V. Model 172I, Model
Page 557 and 558:
3A12 10 Rev. 77 VI. Model 172L (con
Page 559 and 560:
3A12 12 Rev. 77 VIII. Model 172N (c
Page 561 and 562:
3A12 14 Rev. 77 IX. Model 172P (con
Page 563 and 564:
3A12 16 Rev. 77 DATA PERTINENT TO A
Page 565 and 566:
Page 567 and 568:
Page 569 and 570:
Page 571 and 572:
Page 573 and 574:
3A12 26 Rev. 77 XI - Model 172R (co
Page 575 and 576:
3A12 28 Rev. 77 Data Pertinent to M
Page 577 and 578:
3A12 30 Rev. 77 XII - Model 172S (c
Page 580 and 581:
Page 582 and 583:
3 A16CE Control Surface Movements W
Page 584 and 585:
5 A16CE Data Pertinent to All Model
Page 586 and 587:
7 A16CE (6) On cargo door: "Baggage
Page 588 and 589:
9 A16CE (7) Near the manifold press
Page 590:
11 A16CE NOTE 5. The marking of the
Page 593 and 594:
Page 2 of 43 3A21 I - Model 210 (co
Page 595 and 596:
Page 4 of 43 3A21 III - Model 210B,
Page 597 and 598:
V - Model 210D (cont’d) Empty wt.
Page 599 and 600:
Page 8 of 43 3A21 VII - Model T210F
Page 601 and 602:
Page 10 of 43 3A21 IX - Model T210G
Page 603 and 604:
XI - Model T210J (cont’d) Page 12
Page 605 and 606:
Page 14 of 43 3A21 XIII Model 210K/
Page 607 and 608:
Page 16 of 43 3A21 XIV - Model 210M
Page 609 and 610:
Page 18 of 43 3A21 XV - Model P210N
Page 611 and 612:
Page 20 of 43 3A21 Model 210N (cont
Page 613 and 614:
XVII - Model P210R (cont’d) Fuel
Page 615 and 616:
Model T210R (cont’d) Fuel Capacit
Page 617 and 618:
Page 26 of 43 3A21 NOTE 2. (cont’
Page 619 and 620:
Page 28 of 43 3A21 NOTE 2. (4) On f
Page 621 and 622:
Page 623 and 624:
Page 625 and 626:
Page 627 and 628:
NOTE 2. (cont’d) J. (10) Page 36
Page 629 and 630:
NOTE 2. (cont’d) J. (21) Near the
Page 631 and 632:
Page 633 and 634:
Page 42 of 43 3A21 NOTE 2. K. (26)
Page 636 and 637:
Page 638 and 639:
A3SO Page 3 of 31 I. - Model PA-32-
Page 640 and 641:
A3SO Page 5 of 31 II. - Model PA-32
Page 642 and 643:
A3SO Page 7 of 31 III. - Model PA-3
Page 644 and 645:
A3SO Page 9 of 31 V. - Model PA-32R
Page 646 and 647:
A3SO Page 11 of 31 VI. - Model PA-3
Page 648 and 649:
A3SO Page 13 of 31 VII. - Model PA-
Page 650 and 651:
A3SO Page 15 of 31 IX. - Model PA-3
Page 652 and 653:
A3SO Page 17 of 31 X. - Model PA-32
Page 654 and 655:
A3SO Page 19 of 31 XI. - Model PA-3
Page 656 and 657:
A3SO Page 21 of 31 XII. - Model PA-
Page 658 and 659:
A3SO Page 23 of 31 XIV. - Model PA-
Page 660 and 661:
A3SO Page 25 of 31 PA-32R-301, S/N
Page 662 and 663:
A3SO Page 27 of 31 23.1329, 23.1351
Page 664 and 665:
A3SO Page 29 of 31 AFM Supp. VB-357
Page 666 and 667:
A3SO Page 31 of 31 32R-8029121, 32R
Page 668 and 669:
Section V FAA FORMS • FAA Form 33
Page 670 and 671:
5-3 Form Approved Electronic Tracki
Page 672 and 673:
Paperwork Reduction Act Statement:
Page 674 and 675:
END OF SECTION 5 5-7
show all

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

Create successful ePaper yourself

Delete template?

Save as template?