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13 of 16 A7SO Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: MODEL AFM/POH REPORT NO. APPROVED SERIAL EFFECTIVITY PA-34-200 (Seneca) PA-34-200T (Seneca II) AFM VB-353 7/2/71 34-E4, 34-7250001 through 34-7250214 AFM VB-423 5/20/72 34-7250001 through 34-7250189 when Piper Kit 760-607 is installed; 34-7250190 through 34-7250214 when Piper Kit 760-611 is installed; and 34-7250215 through 34-7350353 AFM VB-563 5/14/73 34-7450001 through 34-7450220 AFM Supp. VB-588 7/20/73 34-7250001 through 34-7450039 when propeller with dampers are installed AFM Supp. VB-601 11/9/73 34-7250001 through 34-745017 when ice protection system is installed AFM VB-628 7/18/74 34-7570001 through 34-7670371 POH VB-850 8/23/76 34-7770001 through 34-8170092 POH VB-1140 6/30/80 34-7770001 through 34-8170092 when Piper Kit 764-048V is installed AFM VB-1245 3/9/84 34-7570001 through 34-7670371 when Piper Kit 765-110 is installed
A7SO 14 of 16 MODEL AFM/POH REPORT NO. APPROVED SERIAL EFFECTIVITY PA-34-220T (Seneca III) POH VB-1110 1/8/81 34-8133001 through 34-8633031, and 3433001 through 3433172 POH VB-1150 2/20/81 34-8133001 through 34-8633031, and 3433001 through 3433172 when Piper Kit 764-099V is installed POH VB-1257 10/20/89 3448001 through 3448037 POH VB-1259 11/20/89 3448001 through 3448037 when Piper Kit 766-203 is installed PA-34-220T POH VB-1556 11/5/93 3448038 through 3448079 (Seneca IV) POH VB-1558 12/6/93 3448038 through 3448079 when Piper Kit 766-283 is installed POH VB-1615 7/12/95 3447001 through 3447029 POH VB-1620 7/12/95 3447001 through 3447029 when Piper Kit 766-608 is installed PA-34-220T POH VB-1638 12/6/96 3449001 and up (Seneca V) POH VB-1649 1/23/97 3449001 and up when Piper Kit 766-632 is installed POH VB-1930 10/25/05 3449311 and 3449323 and up when Avidyne Entegra System is installed. NOTE 1 Current Weight and Balance Report, including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. The certificated empty weight and corresponding center of gravity locations must include undrainable system oil (not included in oil capacity) and unusable fuel as noted below: Fuel: 30.0 lb. at (+103.0) for PA-34 series, except Model PA-34-220T (Seneca V), S/N 3449001 and up Fuel: 36.0 lb. at (+103.0) for Model PA-34-220T (Seneca V), S/N 3449001 and up Oil: 6.2 lb. at (+ 39.6) for Model PA-34-200 Oil: 12.0 lb. at (+ 43.7) for Models PA-34-200T and PA-34-220T NOTE 2 All placards required in the approved Airplane Flight Manual or Pilot's Operating Handbook and approved Airplane Flight Manual of Pilot's Operating Handbook supplements must be installed in the appropriate location. NOTE 3 The Model PA-34-200; S/N 34-E4, 34-7250001 through 34-7250189, may be operated at a maximum takeoff weight of 4200 lb. when Piper Kit 760-607 is installed. S/N 34-7250190 through 34-7250214 may be operated at a maximum takeoff weight of 4200 lb. when Piper Kit 760-611 is installed. NOTE 4 The Model PA-34-200; S/N 34-E4, 34-7250001 through 34-7250189, may be operated without spinner domes or without spinner domes and rear bulkheads when Piper Kit 760-607 has been installed. S/N 34-7250190 through 34-7250214 may be operated without spinner domes or without spinner domes and rear bulkhead when Piper Kit 760-611 has been installed. The Model PA-34-200; S/N 34-7250215 through 34-7450220, and the Model PA-34-200T; S/N 34-7570001 through 34-8170092, may be operated without spinner domes or without spinner domes and rear bulkheads.
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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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Page 359 and 360:
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
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 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 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: 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 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 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
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V - Model 560-F, 7 PCLM (Normal Cat
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9 2A4 VI - Model 680-FL (cont’d)
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11 2A4 VII - MODEL 680-FL(P) (cont
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13 2A4 IX - MODEL 680-V, 11 PCLM (N
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15 2A4 X - MODEL 680-W (cont’d) D
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17 2A4 XI - MODEL 681 (cont’d) Se
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19 2A4 XIII - MODEL 685 (cont’d)
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XIV - MODEL 690A (cont’d) Maximum
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23 2A4 XVI - MODEL 690C, 11 PCLM (N
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25 2A4 XVII - MODEL 695 (cont’d)
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27 2A4 XVIII - MODEL 695A (cont’d
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29 2A4 XIX - MODEL 690D (cont’d)
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31 2A4 Specifications Pertinent to
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33 2A4 NOTE 6: Model 680FL S/N 1471
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Page No. 1 2 3 4 Rev. No. 9 9 9 9 R
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3 E-284 NOTE 4. The "6" in the engi
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Page 532 and 533:
Page 3 of 17 A9CE II. Model A188, A
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III. Model 188A, AGwagon "A" & "B"
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V. Model 188B, AGpickup (cont'd) *E
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Page 9 of 17 A9CE VI. Model A188B (
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VII. Model T188C (cont'd) Number of
Page 542 and 543:
Page 13 of 17 A9CE Reference weight
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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
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3A12 4 Rev. 77 II. Model 172A, Mode
Page 553 and 554:
3A12 6 Rev. 77 IV. Model 172D, Mode
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3A12 8 Rev. 77 V. Model 172I, Model
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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
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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
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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
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