(k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. %%EOF Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. Guarantees that a business meets BBB accreditation standards in the US and Canada. condition, apparent and obvious defects, and insecurity of (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (3) Anti-icing devices - for improper operations and obvious defects. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. attachment. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. Collapse to view only 43.13 - Performance rules (general). Explanation of Changes. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. window.dataLayer = window.dataLayer || []; Make sure that every field has been filled in properly. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. (5) Segregation. (3) Anti-icing devices - for improper operations and obvious This should only be necessary once for each IP address you access the site from. services, For Small When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate, The issuance of an Airworthiness Certificate is governed by, Specifications pertaining to an aircraft, of which a limited number were manufactured under a type certificate and for which there is no current Aircraft Specification, can be found in the. (6) Mutilation. (3) Propeller major repairs. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. This system may include electronic, paper, or other means of record keeping. 23, 1964, unless otherwise noted. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). Learn more ME406 Series Emergency Locator Transmitter - ACR. The part may be legibly marked using a permanent method showing its current life status. (4) Engine mount - for cracks, looseness of mounting, and The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. shall, before that inspection, remove or open all necessary Galvanic corrosion is also known as _________ corrosion. (xxi) Repairs involving the substitution of material. there is weak cylinder compression, for improper internal condition (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Decrease engine output RPM to optimum rotor RPM. ____ months of practical experience working on aircraft, are required to apply for an A&P certificate, if the applicant hasn't attended a Part 147 school. The part may be legibly marked using a non-permanent method showing its current life status. The error at all test points must not exceed the tolerances specified in Table I. (i) Power output (static and idle r.p.m. The chord of an airfoil is measured from the ________ to the ________. What is the primary purpose of the helicopter main rotor transmission? When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. (v) Installation of structural parts other than the type of parts approved for the installation. Title 14 CFR part 121, 121.379(b); 4. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. (ii) Hysteresis. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. (5) Flight and engine controls - for improper installation and improper operation. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. make up the complete empennage assembly for poor general condition, 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? hbbd``b`Z"c`@B=8r?O K APPENDIX Appendix A - Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, APPENDIX Appendix B - Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, APPENDIX Appendix C - Appendix C to Part 43 [Reserved], APPENDIX Appendix D - Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, APPENDIX Appendix E - Appendix E to Part 43 - Altimeter System Test and Inspection, APPENDIX Appendix F - Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). failure, and insecurity of attachment. Title 14 CFR part 135, 135.437(b . and insecure mounting. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. 311 0 obj <>stream %PDF-1.6 % (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (6) Electrical system - for chafing and improper operation of switches. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. & Estates, Corporate - H,Ht001300Ff l; (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. Aircraft Specifications or Aircraft Type Certificate Data Sheet. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). (h) Each person performing an annual or 100-hour inspection (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. (ii) Repairing or machining of steel hubs. (b) Applicability. ___________ inspections are limited to surface crack detection in aircraft parts. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (b) Each person performing an annual or 100-hour inspection Ensure the info you add to the Part 43 Appendix D is updated and correct. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. (6) Engine controls - for defects, improper travel, and improper safetying. (4) The maintenance, preventive maintenance, or alteration is recorded in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. Certificated mechanics with a powerplant rating may perform. (18) Replacing wheels and skis where no weight and balance computation is involved. fatigue, and distortion. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (9) Accessories - for apparent defects in security of mounting. (d) Transfer of life-limited parts. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. A thorough inspection will involve ___________ the aircraft. Ifyou believe that this page should betaken down, please follow our DMCA take down process, Ensure the security ofyour data and transactions, Georgia Interim Lien Waiver And Release2013 Sub Sub - Benning, Georgia Final Lien Waiver And Release 2013 Sub Sub - Benning, 2nd Tier Subcontractor/Supplier List - Level 3 Construction, Daigger Automated Microplate Reader Operations Manual PDF, Identity defects. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. (2) Seats and safety belts - for poor condition and apparent defects. The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of Where can you find information on panel location of components under each panel? (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. (6) Engine controls - for defects, improper travel, and improper safetying. Forms, Real Estate (2) The date of completion of the work performed. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. Refer to FAR, Part. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. USLegal fulfills industry-leading security and compliance standards. SOURCE: Docket No. (2) Seats and safety belts - for poor condition and apparent The maximum time a 100 hour inspection can be extended is ______________. 43.15 Additional performance rules for inspections. 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. (>N>dmZyO^:ZUpR`o0Q'B(a^5)ST|18M z:bbLV`> )`8Lb CFR prev | next Enjoy smart fillable fields and interactivity. (4) Retracting and locking mechanism - for improper operation. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 1.5. defects. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. radio group: (1) Radio and electronic equipment - for improper installation (21) Replacing any hose connection except hydraulic connections. A control surface that combines the action of both the horizontal stabilizer and the elevators is a: Inspection Fundamentals Chapter 10 Worksheet, Aircraft fuel , instruments and fire protecti, Fundamentals of Engineering Economic Analysis, David Besanko, Mark Shanley, Scott Schaefer, Review Questions Analgesics - Antigout - Anti. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. landing gear group: (1) All units - for poor condition and insecurity of (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter.

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