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Note 9: Special Limits Page 7 of 12 P-920, Revision 29 Table of Propeller - Engine Combinations Approved Vibrationwise <strong>for</strong> Use on Normal Category Single Engine Tractor Aircraft The maximum and minimum propeller diameters that can be used from a vibration standpoint are shown below. No reduction below the minimum diameter listed is permissible, since this figure includes the diameter reduction allowable <strong>for</strong> repair purposes. The engine models listed below are the configurations on the engine type certificate unless specifically stated otherwise. Modifications to the engine or airframe that alter the power of the engine models listed below during any phase of operation have the potential to increase propeller stresses and are not approved by this list. Such modifications include, but are not limited to, the addition of a turbocharger or turbonormalizer, increased boost pressure, increased compression ratio, increased RPM, altered ignition timing, electronic ignition, full authority digital engine controls (FADEC), or tuned induction or exhaust. Also, any change to the mass or stiffness of the crankshaft/counterweight assembly is not approved by this list. Hub Blade Max. Dia. Min. Dia. Model Model Engine Model (inches) (inches) Placards HC-C2YR F7068-( ) LYC IO-360-B1A, -B1B, -B1C, -B1D, -B1E, -B1F, -E1A, -F1A, LYC O-360-A1A, -A1AD, -A1C, -A1D, -A1F, -A1G, -A1H, -A1LD HC-C2YR F7068 LYC O-360-A1F6, -A1F6D, -A1G6, -A1G6D, -A1H6, -F1A6, -G1A6 LYC IO-360-A1B6, -A1B6D, -A1D6, -A1D6D, -B1F6, -C1C6, -C1D6, -C1E6, -C1E6D HC-C2YR- 1BFP HC-C2YR- 1BFP HC-C2YR- 1BFP F7497 LYC O-360-A1A, -A1C, -A1D, -A1F, -A1G, -A1H, -A1P F7497 LYC IO-360-A1A, -A1B, -A1C, -A1D, -C1A, -C1B, -C1C, -C1F, -D1A F7497 LYC IO-360-A1B6, -A1B6D, -A1D6, -A1D6D, -C1C6, -C1D6, -C1E6, -C1E6D 68 67 Stabilized operation is prohibited above 25 inches manifold pressure between 2300-2350 RPM and below 15 inches manifold pressure above 2600 RPM 68 66 none 74 72 none 74 72 Continuous operation is prohibited above 24 inches manifold pressure between 2350 and 2550 RPM 74 72 none BHC-C2YF 7663 TCM O-300-A, -B, -C, -D, -E 72 70 none HC-C2YF 7663 TCM IO-346-B 76 76 none BHC-C2YF 7663 TCM IO-360-A, -B, -C, -D, -E 76 72 none BHC-C2YF F7663( ) TCM IO-360-H, -HB 76 72 none HC-C2YL 7663 LYC O-290-D2A 72 70 none HC-C2YL 7663 LYC O-320-A3A, -A3B, -A3C, -B3A, -B3B, -B3C, -C3A, -C3B, -C3C, -D1A, -D1B, -D1D, -D1F, -E1A, -E1B, -E1C, -E1F, -E1J HC-C2YL 7663 LYC IO-320-A1A, -B1A, -B1B, -B1C, -B1D, -B1E, -C1A, -C1B, -D1A, -D1B, -D1C, -E1A, -E1B, -F1A HC-C2YK HC-C2YR 7666 F7666 LYC O-360-A1A, -A1AD, -A1C, -A1D, -A1F, -A1G, -A1LD, -B1A, -B1B, -C1A, -C1C, -C1F, -C1G, -D1A 72 70 none 72 70 none 76 72 Avoid continuous operation between 2000 and 2250 RPM
P-920, Revision 29 Page 8 of 12 Hub Blade Max. Dia. Min. Dia. Model Model Engine Model (inches) (inches) Placards HC-C2YK HC-C2YR HC-C2YK HC-C2YR 7666 F7666A LYC O-360-C1E, -C1F 76 72 Avoid continuous operation between 2000 and 2350 RPM F7666A-2Q LYC O-360-A1A, -A1C, -A1D, -A1F, -A1G, -B1A, -B1B, -C1A, -C1C, -C1F, -D1A HC-C2YK 7666 LYC IO-360-A1A, -A1B, -A1C, -C1A, -C1B, -C1C, -D1A 74 74 Avoid continuous operation between 2000 and 2250 RPM 74 72 Avoid continuous operation between 2000 and 2350 RPM HC-C2YK 7666 LYC IO-360-B1A, -B1C 74 72 Avoid continuous operation between 2000 and 2250 RPM HC-C2YK HC-C2YR HC-C2YK HC-C2YR HC-C2YK HC-C2YR F7666( )-3Q LYC IO-360-A3B6D 73 73 none F7666 F7666A LYC O-360-E1A6D 74 72 none F7666A-2 LYC O-360-A1F6D 74 73 none HC-C2YR F7666A-( )R LYC TO-360-E1A6D 74 72 none ( )HC-C2YK ( )HC-C2YR HC-C2YK HC-C2YR ( )7666( )-4Q LYC IO-360-B1A, -B1B, -B1D, -B1E, -B1F, -E1A, -F1A F7666A-4Q LYC O-360-A1A, -A1C, -A1D, -A1F, -A1G, -B1A, -B1B, -C1A, -C1C, -D1A 72 72 Avoid continuous operation between 2000 and 2250 RPM 72 72 Avoid continuous operation between 2000 and 2250 RPM HC-C2YK F7666A-4Q LYC IO-360-A1B6 72 72 none HC-C2YK HC-C2YR 7666-4Q LYC IO-360-A1A, -A1B, -A1C, -C1A, -C1B, -C1C, -D1A HC-C2YK 7666 LYC IO-360-B1A, -B1B, -B1C, -B1D, -B1E, -B1F, -E1A, -F1A HC-C2YK 7666 LYC IO-360-B1A, -B1B, -B1C, -B1D, -B1E, -B1F, -E1A, -F1A HC-C2YK HC-C2YR HC-C2YK HC-C2YR HC-C2YK HC-C2YR HC-C2YK HC-C2YR HC-C2YK HC-C2YR 7666 LYC IO-360-A1B6, -A1D6, -C1C6, -C1E6 7666 LYC IO-360-A1B6, -A1D6, -C1C6, -C1E6 72 72 Avoid continuous operation between 2000 and 2350 RPM 74 72 Avoid continuous operation between 2000 and 2250 RPM 76 74 1/2 Avoid continuous operation between 2000 and 2250 RPM 76 76 None when used with Hartzell C-1576 damper 76 76 Avoid continuous operation between 2000 and 2400 RPM 7666 LYC O-360-F1A6 74 72 none ( )7666 LYC IO-360-A1B6D 74 72 none 7666A F7666A LYC IO-360-C1C 74 72 1/2 Avoid continuous operation between 2000 and 2350 RPM
Page 2:
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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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
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Maximum Weight S/N 34-7250215 throu
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5 of 16 A7SO Maximum Weight 4570 lb
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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 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 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 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 532 and 533: Page 3 of 17 A9CE II. Model A188, A
Page 534 and 535: 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
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Page 13 of 17 A9CE Reference weight
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Page 15 of 17 A9CE Fuel Flows at Fu
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NOTE 8. 14 volt electrical system 1
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3A12 2 Rev. 77 I. Model 172 (cont'd
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3A12 4 Rev. 77 II. Model 172A, Mode
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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
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3A12 12 Rev. 77 VIII. Model 172N (c
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3A12 14 Rev. 77 IX. Model 172P (con
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3A12 16 Rev. 77 DATA PERTINENT TO A
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3A12 26 Rev. 77 XI - Model 172R (co
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3A12 28 Rev. 77 Data Pertinent to M
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3A12 30 Rev. 77 XII - Model 172S (c
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3 A16CE Control Surface Movements W
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5 A16CE Data Pertinent to All Model
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7 A16CE (6) On cargo door: "Baggage
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9 A16CE (7) Near the manifold press
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11 A16CE NOTE 5. The marking of the
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Page 2 of 43 3A21 I - Model 210 (co
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Page 4 of 43 3A21 III - Model 210B,
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V - Model 210D (cont’d) Empty wt.
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Page 8 of 43 3A21 VII - Model T210F
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Page 10 of 43 3A21 IX - Model T210G
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XI - Model T210J (cont’d) Page 12
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Page 14 of 43 3A21 XIII Model 210K/
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Page 16 of 43 3A21 XIV - Model 210M
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Page 18 of 43 3A21 XV - Model P210N
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Page 20 of 43 3A21 Model 210N (cont
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XVII - Model P210R (cont’d) Fuel
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Model T210R (cont’d) Fuel Capacit
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Page 26 of 43 3A21 NOTE 2. (cont’
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Page 28 of 43 3A21 NOTE 2. (4) On f
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NOTE 2. (cont’d) J. (10) Page 36
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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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