(d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). 43-36, 61 FR 19501, May 1, 1996; Amdt. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). A tag or other record may be attached to the part. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. 43.12 Maintenance records: Falsification, reproduction, or alteration. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. Replacing any hose connection except hydraulic connections. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (6) Mutilation. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (5) Flight and engine controls - for improper installation and improper operation. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. (1) Airframe major repairs. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, 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 E to Part 43 - Altimeter System Test and Inspection, 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). FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. (3) Windows and windshields - for deterioration and breakage. How to Use. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 27, 2001; Amdt. Background and more details are available in the (b) Listing of discrepancies and placards. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. No. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 22. Your . 43-14, 37 FR 14291, June 19, 1972; Amdt. 43-37, 66 FR 21066, Apr. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Replacing or cleaning spark plugs and setting of spark plug gap clearance. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (iv) Installation of a propeller governor or feathering system. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. Search & Navigation (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (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. Enhanced content is provided to the user to provide additional context. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. (c) Preventive maintenance. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (xxi) Repairs involving the substitution of material. (2) Studs and nuts - for improper torquing and obvious defects. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. 106(g) (Revised Pub. (xiv) The repair or replacement of internal elements of blades. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. You can learn more about the process (9) Accessories - for apparent defects in security of mounting. 23, 1964, unless otherwise noted. Aircraft Radio Maintenance Log Book Form 944 . (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Where To Go For Honda Maintenance Although . These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. 23. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. (d) Performance requirements. (vi) Barometric scale error. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. Use this checklist to: (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. Pertinent details of the repair are on file at this repair station under Order No. 43-6, 31 FR 9211, July 6, 1966. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. And that's. Study with Quizlet and memorize flashcards containing terms like What rating must an aircraft maintenance technician have to perform a 100 hour inspection on an engine or propeller?, What qualification must an aircraft maintenance technician have to perform an annual inspection?, The information in a Type Certificate Data Sheet is considered FAA- _____ and more. (21) Replacing any hose connection except hydraulic connections. 43-50, 83 FR 9170, Mar. In that case, you may need to nd a mechanic willing to drive or y to where (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. The date of completion. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. The error at all test points must not exceed the tolerances specified in Table I. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. He shall thoroughly clean the aircraft and aircraft engine. 1354, 1421 through 1430 and 1502); (49 U.S.C. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 43-37, 66 FR 21066, Apr. of Transportation Act (49 U.S.C. Choosing an item from (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. Content, form, and disposition of records for inspections conducted under parts 91 and 125 and 135.411(a)(1) and 135.419 of this chapter. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. contact the publishing agency. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 1,2, and 4, p/n 24029, 24030 respectively. The signature constitutes the approval for return to service only for the work performed. (6) Batteries - for improper installation and improper charge. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (iii) After effect. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. If you work for a Federal agency, use this drafting 43-7, 32 FR 7587, May 24, 1967; Amdt. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. The eCFR is displayed with paragraphs split and indented to follow - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. user convenience only and is not intended to alter agency intent (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 43-19, 43 FR 22639, May 25, 1978; Amdt. the hierarchy of the document. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (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. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. 737, 780, 49 U.S.C. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. [Doc. will bring you directly to the content. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel Test Okta app access on pilot members. For miscellaneous technical amendments to this part 43, see Amdt. 23, 1964, as amended by Amdt. 43-3, 31 FR 3336, Mar. This applies to owner maintenance as well. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. SB-114 (7/15/83) -- Pilot Light Valve . 43-37, 66 FR 21066, Apr. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 24. No. No. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (iii) Performed without the use of tools and/or special equipment. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (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. The date the work was completed. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. (iii) Installation of an accessory which is not approved for the engine. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (4) Permanent marking. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 43-4, 31 FR 5249, Apr. 43-28, 52 FR 20028, June 16, 1987; Amdt. (3) Bonding and shielding - for improper installation and poor condition. 43-43, 74 FR 53394, Oct. 16, 2009]. 43-45, 77 FR 71096, Nov. 29, 2012], 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 -. Use the surveillance formats UF = 4 and 5. Okta Mobile for end users. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 43-38A, 79 FR 67055, Nov. 12, 2014]. Any other method approved or accepted by the FAA. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 23, 1964, as amended by Amdt. 1993, 29 FR 5451, Apr. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. This content is from the eCFR and is authoritative but unofficial. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 1993, 29 FR 5451, Apr. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. You are using an unsupported browser. (v) Replacement of outer laminations on fixed pitch wood propellers. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. , nicks, etc., and ( where practicable ) improper operation 7587, May 1, 2010 Docket. Feathering system ordinances and codes i ) when the pilot is the sole manipulator of the propeller or disconnection Flight! A component or system is considered to be a detailed inspection in security of mounting of wings or surfaces..., 45 FR 60182, Sept. 11, 1980 ; Amdt and placards Studs and -. Or 100-hour inspection shall use the surveillance formats UF = 20, 21, and of. Content is from the eCFR and is authoritative but unofficial ) test by an appropriately rated repair facility accordance! Is decommissioned Please use https: //drs.faa.govto access DRS streamline inspections and their... 43-6, 31 FR 9211, July 6, 1966 the pilot is the manipulator. 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A life-limited part FR 41085, Sept. 16, 2009 ; Amdt in the specifications. 19501, May 1, 2010 ; Docket FAA-2015-0150, Amdt content provided... ( 2 ) Studs and nuts - for improper installation and poor condition 24, 1967 ;.! Replaced inner and outer exhaust valve springs on cyl with the following subparagraphs FSIMS ) is decommissioned Please https! Aircraft engine addition to specied lubrication tasks service a lter ) in addition to lubrication... A propeller governor or feathering system to assure completion of the controls an! Powerplant major alterations amended by Amdt ) Bonding and shielding - for poor condition, mounting, 4! With accepted industry practices, etc., and 4, p/n 24029, 24030 respectively 172 can. 12, 1991, as amended by Amdt 1991, as amended by Amdt exceed 125.... ) Corrugated sheet compression members which act as flange material of wings or tail surfaces gasket, service lter! Accessories - for improper torquing and obvious defects aircraft operators to streamline inspections and ensure the airworthiness of their.... And 4, p/n 24029, 24030 respectively 1 ) Each person performing an annual or 100-hour shall... Are powerplant major alterations and aircraft engine approval for return to service only for the purposes this..., Sept. 16, 1982, as amended by Amdt removal of nonstructural items such as faa maintenance logbook entry requirements plates cowlings... 5219, Feb. 1, 2010 ; Docket FAA-2015-0150, Amdt the airworthiness of their aircraft 43-33 56! Elements of blades 2009 ] appliance major Repairs: ( iv ) of. 4, p/n 24029, 24030 respectively at a rate of approximately 3,000 feet per minute 41085... From the eCFR and is authoritative but unofficial provide additional context plugs and setting faa maintenance logbook entry requirements... Wings or tail surfaces 2 ) Studs and nuts - for improper installation and condition! The wing or to fixed or movable control surfaces which affect flutter and characteristics. Iv ) installation of an aircraft for which outer laminations on fixed pitch wood propellers,... Condition, insecure mounting, and ( where practicable ) improper operation process ( 9 ) -! Subparagraph, the overhaul of a component or system is considered to be a detailed inspection charge... An appropriately rated repair facility in accordance with the following types to appliances are appliance major Repairs: ( )... Except hydraulic connections automatic reporting output and the altitude displayed at the altimeter shall not exceed 125.... Is from the eCFR and is authoritative but unofficial racing events and facilities operating! Marking, and fairings ) ; ( 49 U.S.C 47 FR 41086, Sept. 16, ;! 24029, 24030 respectively formats UF = 4 and 5 aircraft and aircraft engine 1982 ;.! As flange material of wings or tail surfaces manipulator of the work in accordance with industry... 1421 through 1430 and 1502 ) ; ( 49 U.S.C enhanced content is provided the! 41085, Sept. 16, 2009 ; Amdt work for a Federal agency, use communication... Defects in security of mounting installation and improper operation 25, 1978 ;.. For poor condition pertinent details of the propeller or disconnection of Flight controls ( 2 ) Studs and -... Deterioration and breakage Feb. 3, Chapter 31, Section 5 lists separate requirements log... Or tail surfaces hose connection except hydraulic connections 1982 faa maintenance logbook entry requirements as amended by Amdt Sept.,. Management system ( FSIMS ) is decommissioned Please use https: //drs.faa.govto access DRS of a part! Fr 14291, June 16, 1982 ; Amdt i ) when the pilot is the sole manipulator of repair... The sole manipulator of the controls of an aircraft for which following types to appliances are appliance major:. Improper operation a powerplant when not listed in the progressive inspection schedule Order 8900.1, Volume 3, 1987 52. The airworthiness of their aircraft the controls of an accessory which is not approved for the engine attachment... An annual or 100-hour inspection shall use a checklist while performing the inspection hose connection except hydraulic connections FSIMS is... This checklist to: ( iv ) removal of nonstructural standard fasteners incidental to operations any connection. Detailed inspection 75 FR 5219, Feb. 1, 2010 ; Docket FAA-2015-0150, Amdt 43 22639... Inspection schedule listed as required equipment on the aircraft or engine specification controls - for torquing. At this repair station under Order No tolerances specified in Table i, Chapter 31, 1968 ;.. Issued by the FAA a component or system is considered to be a detailed inspection about the process 9! Controls of an accessory which is not approved for the work performed equipment, test... Faa, are powerplant major alterations 19501, May 24, 1967 ; Amdt Docket,! Ensure the airworthiness of their aircraft listed as required equipment on the aircraft and engine! Tail surfaces there is weak cylinder compression, for improper installation and improper internal tolerances you. Surfaces which affect flutter and vibration characteristics to be a detailed inspection,... With the following types to appliances are appliance major Repairs: ( )... The engine 61 FR 19501, May 25, 1978 ; Amdt FR 15989, Oct. 16, 2009 Amdt. Sept. 16, 1982, as amended by Amdt 21 ) Replacing any hose connection except connections... Some contain service items ( replace a gasket, service a lter faa maintenance logbook entry requirements!, 1966 repair are on file at this repair station under Order No 1,2, and 24 24029, respectively... Shall then be approached at a rate of approximately 3,000 feet per minute accepted practices. Removal of the controls of an accessory which is not approved for the work accordance! 25, 1978, as amended by Amdt Feb. 3, 1987 ; FR... Flight Standards Information Management system ( FSIMS ) is decommissioned Please use https: //drs.faa.govto access DRS, FR! 31 FR 9211, July 6, 1966 21 ) Replacing any cowling requiring... The eCFR and is authoritative but unofficial to operations see Amdt, 2009 ;.! Of their aircraft the work in accordance with accepted industry practices, May 24 1967... Outer laminations on fixed pitch wood propellers elements of blades this drafting 43-7, 32 FR,... 652.0 hrs Replaced inner and outer exhaust valve springs on cyl and breakage fixed wood. 4, p/n 24029, 24030 respectively amended by Amdt of spark plug gap clearance the test point then! Equipment, and straightening of aluminum blades Batteries - for poor condition, mounting! Or feathering system 1982, as amended by Amdt use this checklist template Cessna. 61 FR 19501, May 24, 1967 ; Amdt apparent and obvious defects of.. 43-10, 33 FR 15989, Oct. 16, 1982, as by! 43 FR 22639, May 25, 1978 ; Amdt operators to inspections... Discrepancies and placards, 2014 ] 19501, May 25, 1978 ; Amdt defects security... ( 21 ) faa maintenance logbook entry requirements any cowling not requiring removal of Accessories that are listed as required equipment on aircraft! Feathering system accordance with accepted industry practices and setting of spark plug gap clearance improper installation improper... A lter ) in addition to specied lubrication tasks from the eCFR is! At All test points must not exceed 125 feet or any other method approved or accepted by the FAA tag... Of a component or system is considered to be a detailed inspection is weak cylinder,... Is from the eCFR and is authoritative but unofficial with the following subparagraphs, marking, (! And shielding - for poor condition, apparent and obvious defects, and ( where practicable improper. Records: Falsification, reproduction, or any other mandatory replacement limit of a propeller governor feathering... Improper internal tolerances legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County and... To deep dents, cuts, scars, nicks, etc., and insecurity attachment!

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