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

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P57GL Page 5 of 5 NOTE 8. Not applicable. NOTE 9. Not applicable. (6) Model 3AF32C512/82NEA with plain or electric deice or liquid anti-ice spinner; reference D-5370 Dome, D-5499-1 and -3 Bulkhead and D-5309 and D-5310 Installation. (7) Model 3AF36C514/80VMFA with plain or electric deicing spinner; reference E-6190 Dome, E-6178 Bulkhead and D-6176 Installation. (8) Model 3AF32C515/82NLA with electric deice spinner; reference D-5215 Installation. (9) Model 3AF37C516/90LFB per assembly drawing E-7110. (10) Model 3AF37C510/90LFB per assembly drawing E-7272. (11) Model 3AF32C522/82NJA per assembly drawing E-7315. (12) Model 3AF32C523/L82NJA per assembly drawing E-7316. (13) Model 3AF32C524/90UMB per assembly drawing E-7549. (14) Model 3AF36C525/80VMF[X] per assembly drawing E-7507. (15) Model B3DF36C526/80HJ[X] per assembly drawing E-7527. (16) Model B3DF36C527/L80HJ[X] per assembly drawing E-7528. (17) Model 3AF32C528/82NE[X] per assembly drawing E-7552. 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
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FIGURE 11-6. Altitude derating curv
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Minimum Equipment List Page MINIMUM
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EXHIBIT 24 Bend Allowance = 2π (R
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EXHIBIT 25 c = 2π a 2 + b 2 2 Circ
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Section IV: Type Certificate Data S
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TCDS BACKGROUND INFORMATION Type Ce
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Coded Entries Many aircraft and eng
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DEPARTMENT OF TRANSPORTATION FEDERA
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I. Model 208, Caravan (cont’d) 3
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II. - Model 208B, Caravan (cont’d
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Data Pertinent to All Models (cont
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TCDS E4EA PAGE 2 IV. MODEL TYPE (se
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TCDS E4EA PAGE 4 I. MODELS (Cont.))
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TCDS E4EA PAGE 6 I. MODELS (cont.)
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TCDS E4EA PAGE 8 II. MODELS PT6A-45
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TCDS E4EA PAGE 10 III. MODELS (cont
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TCDS E4EA PAGE 12 PT6A-28 PT6A-29 P
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TCDS E4EA PAGE 14 NOTE 1.(continued
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TCDS E4EA PAGE 16 Maximum Continuou
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TCDS E4EA PAGE 18 Accessory Drive P
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TCDS E4EA PAGE 20 NOTE 7. The maxim
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TCDS E4EA PAGE 22 NOTE 13. (Cont'd)
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P9NE 2 NOTE 2. Blade Model Designat
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P60GL Page 2 of 3 Certification Bas
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Page No. 1 2 3 Rev. No. 29 29 29 Re
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E-252 Page 3 The Model 0-200-C is s
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2A13 Page 2 of 43 Center of Gravity
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2A13 Page 4 of 43 Propeller Spinner
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2A13 Page 6 of 43 Propeller Spinner
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2A13 Page 8 of 43 VI - Model PA-28-
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2A13 Page 10 of 43 Center of Gravit
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2A13 Page 12 of 43 Empty Weight C.
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2A13 Page 14 of 43 X - Model PA-28R
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2A13 Page 16 of 43 Control Surface
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2A13 Page 18 of 43 Engine Limits Fo
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2A13 Page 20 of 43 Manufacturer's S
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2A13 Page 22 of 43 Center of Gravit
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2A13 Page 24 of 43 XVI - B. Model P
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2A13 Page 26 of 43 No. of Seats Nor
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2A13 Page 28 of 43 Airspeed Limits
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2A13 Page 30 of 43 Propeller and Pr
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2A13 Page 32 of 43 Engine Limits Fo
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2A13 Page 34 of 43 Manufacturer's S
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2A13 Page 36 of 43 PA-28-236: CAR 3
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2A13 Page 38 of 43 (Continued) MODE
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2A13 Page 40 of 43 NOTE 3 The Model
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2A13 Page 42 of 43 NOTE 20 PA-28-18
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II - Model 150D, Model 150E, Model
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IV - Model A150K, Aerobat, 2 PCLM (
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V - Model 150L (cont’d) Page 7 of
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VII - Model 150M (cont’d) Page 9
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IX - Model 152 (cont'd) Page 11 of
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X - Model A152 (cont’d) Page 13 o
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Page 17 of 19 3A19 Data Pertinent t
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E-295 Page 2 of 8 Model Lycoming O-
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E-295 Page 4 of 8 Certification bas
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E-295 Page 6 of 8 NOTE 5. These mod
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E-295 Page 8 of 8 NOTE 12. When equ
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A7CE Page 2 of 24 Propeller and or
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A7CE Page 4 of 24 II - Model 401, M
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A7CE Page 6 of 24 III - Model 402,
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A7CE Page 8 of 24 IV - Model 421, M
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A7CE Page 10 of 24 V - Model 414 (N
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A7CE Page 12 of 24 VI - Model 421B
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A7CE Page 14 of 24 VII - Model 421C
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A7CE Page 16 of 24 VIII - Model 414
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A7CE Page 18 of 24 IX - Model 402C
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A7CE Page 20 of 24 X - Model 425 (c
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A7CE Page 22 of 24 X - Model 425 (c
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A7CE Page 24 of 24 NOTE 3. (cont'd.
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3A13 Page 2 of 37 Rev. 66 I - Model
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3A13 Page 4 of 37 Rev. 66 II - Mode
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3A13 Page 6 of 37 Rev. 66 IV - Mode
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3A13 Page 8 of 37 Rev. 66 V - Model
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3A13 Page 10 of 37 Rev. 66 VII - Mo
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3A13 Page 12 of 37 Rev. 66 VIII - M
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3A13 Page 14 of 37 Rev. 66 X - Mode
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3A13 Page 16 of 37 Rev. 66 Model TR
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3A13 Page 18 of 37 Rev. 66 Model 18
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3A13 Page 20 of 37 Rev. 66 Data Per
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3A13 Page 26 of 37 Rev. 66 Long ran
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3A13 Page 28 of 37 Rev. 66 (3) On t
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3A13 Page 32 of 37 Rev. 66 XIII - M
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3A13 Page 34 of 37 Rev. 66 Special
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3A13 Page 36 of 37 Rev. 66 Oil Capa
Page 428 and 429: DEPARTMENT OF TRANSPORTATION FEDERA
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: DEPARTMENT OF TRANSPORTATION FEDERA
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: P57GL Page 4 of 5 NOTE 3. Pitch Con
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
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A9CE Page 10 of 17 VI. Model A188B
Page 541 and 542:
A9CE Page 12 of 17 NOTE 1. Current
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A9CE Page 14 of 17 (d) (1) On flap
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A9CE Page 16 of 17 The following ad
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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
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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 (
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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
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
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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
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
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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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