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

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P60GL Page 3 of 3 NOTE 2. Blade Model Designation. X - X 106 G[X] - 0 NOTE 3. Not applicable. Basic Model Designation Reduction in diameter from basic, in inches. Characteristics of blade design (planform, etc.). Suffix [X] indicates blade butt staking dimensions for the actuating pin. Blade design diameter in inches. Letter designating direction of rotation; no letter (blank) indicates clockwise (viewed from downstream); L indicates counter-clockwise. Letter designating minor change not affecting eligibility or interchangeability. NOTE 4. Feathering. Feathering and unfeathering capability when installed with appropriate feather/unfeathering controls. Reversing. For installation as reversing propeller with appropriate reversing controls. NOTE 5. Left Hand Models. The left hand version of an approved model is eligible at the same rating and diameter limitations as listed for the right hand model. NOTE 6. Not applicable. NOTE 7. Accessories. (a) Propeller Deicing (1) Model 93KB blades with Goodrich deicer per Goodrich Report 59-728 and installed per McCauley drawing E-5128. (2) Model 100LA blades with Safeway deicer B-40245-50 per McCauley Report MC-2611 and installed per McCauley drawing E-5423. (3) Model 106GA blades with McCauley deicer B-40245-54 per McCauley Report MC-2611 and installed per McCauley drawing E-6368. (b) Propeller Spinner (1) Model 3GFR34C701/93KB and 3GFR34C704/93KB with spinner, reference McCauley drawing E-5146. (2) Model 3GFR34C702/100LA with spinner; reference McCauley drawing E-5424. (3) Model 3GFR34C703/106GA with spinner; reference McCauley drawing E-6383. NOTE 8. Not applicable. NOTE 9. Not applicable. NOTE 10. Special Notes. Aircraft installation must be approved as part of the aircraft type certificate upon compliance with the applicable aircraft airworthiness requirements. ... END ...
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Computer Testing Supplement for Ins
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Table of Contents Preface .........
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• A7S0, Piper PA-34-200 • A11EA
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Section I: Title 14 of the Code of
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§ 1.1 General definitions. PART 1
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Category B, with respect to transpo
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(1) An ETOPS group 1 Significant Sy
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Glider means a heavier-than-air air
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Long-range communication system (LR
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Overseas air transportation means t
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Rated maximum continuous augmented
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(2) With respect to turbine engines
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ETOPS means extended operations. EW
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SSALS means simplified short approa
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(2) May is used in a permissive sen
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§ 23.1 Applicability. PART 23—AI
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(i) The highest weight selected by
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[Doc. No. 4080, 29 FR 17955, Dec. 1
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significantly reduce the capability
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(1) The instrument that most effect
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[Amdt. 23-1, 30 FR 8261, June 29, 1
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(2) Each exposed sight gauge used a
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[Doc. No. 4080, 29 FR 17955, Dec. 1
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(c) Main power cables (including ge
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(c) Rear position light installatio
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system is observed from a distance,
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(c) For those airplanes required to
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(d) As used in this section: (1) BT
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§23.1457 Cockpit voice recorders.
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23.1511 Flap extended speed. (a) Th
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23.1541 General. (a) The airplane m
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(1) Each fuel tank selector control
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(2) Stating that recovery must be i
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(3) Acrobatic category airplanes. A
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(4) The effect on landing distances
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ecommended at these periods. Howeve
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Subpart A—General §27.1 Applicab
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(3) The portion of the total weight
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warn the pilot of the occurrence of
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(c) Except as provided in paragraph
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(2) Compliance with paragraph (a)(1
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§27.1365 Electric cables. (a) Each
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§27.1391 Minimum intensities in th
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where: Ie=effective intensity (cand
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(2) By installing a continually ene
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§27.1505 Never-exceed speed. (a) T
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(i) The maximum value determined by
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(b) Each arc and line must be wide
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(2) Oil filler openings must be mar
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(ii) The maximum safe wind for oper
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PART 39—AIRWORTHINESS DIRECTIVES
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PART 43—MAINTENANCE, PREVENTIVE M
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§ 43.5 Approval for return to serv
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is permanently removed from use on
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(b) Rotorcraft. Each person perform
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Appendix A to Part 43—Major Alter
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(2) Powerplant major repairs. Repai
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(31) Removing and replacing self-co
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(3) Internal engine—for cylinder
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(vi) Barometric scale error. At con
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Appendix F to Part 43—ATC Transpo
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§ 45.1 Applicability. This part pr
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§ 45.14 Identification of critical
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§ 45.25 Location of marks on fixed
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§ 91.1 Applicability. PART 91—GE
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hospital, or doctor, or other perso
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§§ 91.27-91.99 [Reserved] § 91.2
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(i) Airplanes with a third attitude
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(11) On and after January 1, 2004,
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(iv) Required to be operational by
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(5) Accept necessary barometric pre
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§ 91.407 Operation after maintenan
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(g) Inspection program approved und
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(iii) The time since last overhaul
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Section II: Airworthiness Directive
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MESSERSCHMITT-BOLKOW-BLOHM-GMBH AND
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AGUSTA, COSTRUZIONI AERONAUTICHE GI
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BEECH =============================
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d. Coat entire portion of bolt that
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AIR TRACTOR, INC. =================
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BENDIX ============================
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ENSTROM ===========================
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BEECH =============================
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BEECH AIRCRAFT CORPORATION ========
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PRATT & WITHEY AIRCRAFT OF CANADA,
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(j) Install a CT stator assembly, a
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Section III: Exhibits • Exhibit 1
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Rivet identifi cation and part numb
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Aircraft rivet identification. EXHI
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Aircraft rivet identification. (con
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Thickness “t” in inches No. of
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Page 188 and 189:
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Recommended radii for 90° bends in
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Minimum Bend Radius for Aluminum Al
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3-19 RADIUS THICKNESS 1/32 .031 1/1
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EXHIBIT 10 K-chart for determining
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. . DATUM D C.G. L . . NOSE WHEEL T
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COMPUTED WEIGHING POINT (C MAIN WHE
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NOSE SCALE 464 LBS. TARE 10 LBS. We
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FULL OIL EXHIBIT 14 Example of chec
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FULL OIL EXHIBIT 15 Example of chec
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1. GENERAL. The minimum airworthine
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Utility Category Aircraft (FAR 23)
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EXHIBIT 17 Turnbuckle safetying gui
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Straight-shank terminal dimensions
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BEND RADIUS INCHES 3 — 2 — 1
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MINIMUM BEND RADIUS (INCHES) 16 15
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211. GENERAL. This chapter contains
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differential of 5.53 in. Hg, i.e.,
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DC wire and circuit protector chart
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Where: T1 T2 TR I2 Imax TABLE 11-9.
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11-67. METHODS FOR DETERMINING CURR
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(1) The wire run is 15.5 feet long,
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STEP 1: Refer to the “single wire
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FIGURE 11-3. Conductor chart, inter
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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 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: P60GL Page 2 of 3 Certification Bas
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
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3A19 Page 2 of 19 I - Model 150, Mo
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3A19 Page 4 of 19 III - Model 150G,
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3A19 Page 6 of 19 V - Model 150L, 2
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3A19 Page 8 of 19 VI - Model A150L
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3A19 Page 10 of 19 VIII - Model A15
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3A19 Page 12 of 19 X - Model A152 (
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3A19 Page 14 of 19 Data Pertinent t
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DEPARTMENT OF TRANSPORTATION FEDERA
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Model Lycoming O-540 -J1A5D, -J2A5D
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Page 5 of 8 E-295 -J1A5D -J2A5D -J3
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NOTE 8. Fuel grade, compression and
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Page 3 of 24 A7CE I - Model 411, Mo
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Page 5 of 24 A7CE III - Model 402,
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Page 7 of 24 A7CE III - Model 402,
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Page 9 of 24 A7CE IV - Model 421, M
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V - Model 414 (cont'd) Maximum Weig
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VI - Model 421B (cont'd) Empty Wt.
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Page 15 of 24 A7CE VII - Model 421C
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Page 17 of 24 A7CE VIII - Model 414
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Page 19 of 24 A7CE X - Model 425, C
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Page 21 of 24 A7CE X - Model 425 (c
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Page 23 of 24 A7CE NOTE 1. Current
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Rev. 66 Page 3 of 37 3A13 II - Mode
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Rev. 66 Page 5 of 37 3A13 III - Mod
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Rev. 66 Page 7 of 37 3A13 IV - Mode
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Rev. 66 Page 9 of 37 3A13 VI - Mode
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Rev. 66 Page 11 of 37 3A13 VIII - M
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Rev. 66 Page 13 of 37 3A13 IX - Mod
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Rev. 66 Page 15 of 37 3A13 XI - Mod
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Rev. 66 Page 17 of 37 3A13 XI - Mod
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Rev. 66 Page 19 of 37 3A13 XII - Mo
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Rev. 66 Page 21 of 37 3A13 Data Per
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Page 414 and 415:
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Rev. 66 Page 31 of 37 3A13 TR182, C
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Rev. 66 Page 35 of 37 3A13 increase
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Rev. 66 Page 37 of 37 3A13 Addition
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A7SO 2 of 16 Propeller and Propelle
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Page 433 and 434:
Page 435 and 436:
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A7SO 10 of 16 Propeller and Propell
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A7SO 12 of 16 Certification Basis M
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A7SO 14 of 16 MODEL AFM/POH REPORT
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A7SO 16 of 16 NOTE 8 Model PA-34-20
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A11EA Page 2 Center of gravity (C.G
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A11EA Page 4 III - Model AA-1B, Tra
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A11EA Page 6 Fuel capacity 24 gal.
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A11EA Page 8 All Models: NOTE 3. De
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1A6 Page 2 of 15 Maximum Baggage 50
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1A6 Page 4 of 15 Fuel Capacity 36 g
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1A6 Page 6 of 15 Oil Capacity 2 gal
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1A6 Page 8 of 15 Oil Capacity 2 gal
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1A6 Page 10 of 15 4. Propeller (wit
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1A6 Page 12 of 15 Electrical Equipm
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1A6 Page 14 of 15 *405. Ross Contro
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Page No. 1 2 3 4 5 6 Rev. No. 35 36
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Page 3 E-273 Model O-470-H O-470-G,
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Page 5 E-273 NOTE 6. O-470-B, -G, -
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Page 476 and 477:
P57GL Page 3 of 5 Maximum Diameter
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P57GL Page 5 of 5 NOTE 8. Not appli
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P-920, Revision 29 Page 2 of 12 Max
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P-920, Revision 29 Page 4 of 12 Cer
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P-920, Revision 29 Page 6 of 12 Not
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P-920, Revision 29 Page 8 of 12 Hub
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P-920, Revision 29 Page 10 of 12 Hu
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P-920, Revision 29 Page 12 of 12 Hu
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2A4 2 I - Model 680 (cont’d) Airp
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2A4 4 II. - Model 680-E (cont’d)
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2A4 6 IV - MODEL 680-F (cont’d) b
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2A4 8 V - Model 560-F (cont’d) Le
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2A4 10 VI - Model 680-FL (cont’d)
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2A4 12 VIII - MODEL 680-T (cont’d
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2A4 14 IX - MODEL 680-V, 11 PCLM (N
Page 507 and 508:
2A4 16 XI - MODEL 681 (cont’d) Pr
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2A4 18 XII - MODEL 690 (cont’d) M
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2A4 20 XIV - MODEL 690A, 11 PCLM (N
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2A4 22 XV - MODEL 690B (cont’d) A
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2A4 24 XVI - MODEL 690C (cont’d)
Page 517 and 518:
2A4 26 XVIII - MODEL 695A, 11 PCLM
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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
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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
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A9CE Page 16 of 17 The following ad
Page 548 and 549:
Page 550 and 551:
Rev. 77 3 3A12 II. Model 172A, Mode
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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
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A16CE 10 NOTE 3. Reserved. (10) (a)
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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
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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
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Page 15 of 43 3A21 Models 210K/210L
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Page 17 of 43 3A21 2. Model T210M (
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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
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Page 27 of 43 3A21 (4) On fuel sele
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NOTE 2. (cont’d) (8) Near the eng
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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
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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
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