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

More documents

Recommendations

Info

Rev. 77 9 3A12 VI. Model 172L (cont'd) Propeller and 3. Propeller Propeller Limits (cont’d) (a) McCauley 1C160/CTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370, not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in., not under 74 in. (b) Spinner, Dwg. 0550320 4. Propeller (a) McCauley 1A160/DTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370, not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in., not under 74 in. (b) Spinner, Dwg. 0550320 5. Propeller (Seaplane only) (a) McCauley 1A175/ETM 8042 Static rpm at maximum permissible throttle setting: Not over 2480, not under 2380 No additional tolerance permitted (see Note 3) Diameter: not over 80 in., not under 78.4 in. (b) Spinner, Dwg. 0550321 6. Propeller (a) McCauley 1C160/DTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370, not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in., not under 74 in. (b) Spinner, Dwg. 0550320 *Airspeed Limits Maneuvering 122 mph (106 knots) (CAS) Maximum structural cruising 140 mph (122 knots) Never exceed 174 mph (151 knots) Flaps extended 100 mph ( 87 knots) C.G. Range Landplane Normal category (+38.5) to (+47.3) at 2300 lbs. (+35.0) to (+47.3) at 1950 lbs. or less Utility category (+35.5) to (+40.5) at 2000 lbs. (+35.0) to (+40.5) at 1950 lbs. or less Straight line variation between points given. Empty Weight C.G. Range None Seaplane (Edo 89-2000 or 89A2000 floats) Normal category (+39.8) to (+45.5) at 2220 lbs. (+36.4) to (+45.5) at 1825 lbs. or less Straight line variation between points given. *Maximum Weight Landplane: Normal category 2300 lbs. Utility category 2000 lbs. Seaplane: Normal category 2220 lbs. Number of Seats 4 (2 at +34 to +46, 2 at +73) (Occupant on child's optional jump seat at +96) Maximum Baggage 120 lb. at +95 Fuel Capacity 42 gal. total, 38 gal. usable (two 21 gal. tanks in wings at +48) See Note 1 <strong>for</strong> weight of unusable fuel.
3A12 10 Rev. 77 VI. Model 172L (cont'd) Oil Capacity 2 gal. (-14.0), 1-1/2 gal. usable See Note 1 <strong>for</strong> data on undrainable oil. Control Surface Movements Wing flaps Takeoff 0� - 10� Landing 0� - 40� �2� Ailerons Up 20� �1� Down 15� �1� Elevator tab Up 28� +1�, -0� Down 13� +1�, -0� Elevator Up 28� +1�, -0� Down 23� +1�, -0� (Neutral position is with bottom of balance area flush with bottom of stabilizer.) Rudder (landplane) Right 16� �1� Left 16� �1� (seaplane) Right 19� �1� Left 15� �1� (Measured parallel to W.L.) Serial Numbers Eligible Model 172L: 17259224 through 17259903 (1971 model) Model 172L: 17259904 through 17260758 (1972 model) VII. Model 172M, Skyhawk, 4 PCL-SM (Normal Category), 2 PCLM (Utility Category, approved May 12, 1972 Engine Lycoming O-320-E2D *Fuel 80/87 minimum grade aviation gasoline *Engine Limits For all operations, 2700 rpm (150 hp) Propeller and 1. Propeller Propeller Limits (a) McCauley 1C160/CTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370, not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in., not under 74 in. (b) Spinner: Dwg. 0550320 2. Propeller (a) McCauley 1C160/DTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370, not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in., not under 74 in. (b) Spinner, Dwg. 0550320 3. Propeller (seaplane only) (a) McCauley 1A175/ATM 8042 Static rpm at maximum permissible throttle setting: Not over 2545, not under 2445 No additional tolerance permitted (see Note 3) Diameter: not over 80 in., not under 78.4 in. (b) Spinner, Dwg. 0550320 4. Propeller (seaplane only) (a) McCauley 1A175/ETM 8042 Static rpm at maximum permissible throttle setting: Not over 2545, not under 2445 No additional tolerance permitted (see Note 3) Diameter: not over 80 in., not under 78.4 in. (b) Spinner, Dwg. 0550320 *Airspeed Limits 17256493, 17260759 through 17265684 (CAS) Maneuvering 112 mph ( 97 knots) Maximum structural cruising 145 mph (126 knots) Never exceed 182 mph (158 knots) Flaps extended 100 mph ( 87 knots)
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:
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 and 278:
TCDS E4EA PAGE 16 Maximum Continuou
Page 279 and 280:
TCDS E4EA PAGE 18 Accessory Drive P
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:
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:
Page 354 and 355:
Page 17 of 19 3A19 Data Pertinent t
Page 356:
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: DEPARTMENT OF TRANSPORTATION FEDERA
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: 3A12 8 Rev. 77 V. Model 172I, Model
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 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: DEPARTMENT OF TRANSPORTATION FEDERA
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 ...

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

Delete template?

Save as template?