(i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. 1,2, and 4, p/n 24029, 24030 respectively. [Amdt. 4, 1987, as amended by Amdt. 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. (2) The date of the inspection and aircraft total time in service. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (viii) Keel and chine members of boat hulls or floats. (b) Rotorcraft. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. (ii) Repairing or machining of steel hubs. (2) Powerplant major repairs. The official, published CFR, is updated annually and available below under 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. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. If it had been a non-FAA-approved part, a Form 337 would not be required. This applies to owner maintenance as well. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides Replacing or cleaning spark plugs and setting of spark plug gap clearance. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. The software release life cycle is the process of developing, testing, and distributing a software product. No. FAA-2018-0119, Amdt. You are using an unsupported browser. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (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. Enhanced content is provided to the user to provide additional context. 43-39, 69 FR 44863, July 27, 2004; Amdt. (vi) Barometric scale error. Each is a special inspection unto itself; they're all different. No. citations and headings (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. 43-14, 37 FR 14291, June 19, 1972; Amdt. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. 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. 14. (21) Replacing any hose connection except hydraulic connections. (7) Wheels - for cracks, defects, and condition of bearings. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. 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. The date of completion. 43-37, 66 FR 21066, Apr. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. Your . (x) Wing main ribs and compression members. 3. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (7) Other methods. The interrogations should be made at a nominal rate of 50 interrogations per second. the hierarchy of the document. (2) Studs and nuts - for improper torquing and obvious defects. (iii) After effect. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. 1993, 29 FR 5451, Apr. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (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. The part may be mutilated to deter its installation in a type certificated product. If you work for a Federal agency, use this drafting (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. The part may be legibly marked using a permanent method showing its current life status. 43-40, 71 FR 40877, July 14, 2005]. 23. (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. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. No. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. (i) Power output (static and idle r.p.m. A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. 43.9 Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411(a)(1), and 135.419 of this chapter). contact the publishing agency. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. FAA STANDARDS FOR ELECTRONIC RECORDS. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. Cleaning or replacing fuel and oil strainers or filter elements. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 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. (6) Engine controls - for defects, improper travel, and improper safetying. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Requirements for FAA aircraft repairman certificate Sec. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. Additional performance rules for inspections. 1, 1966; Amdt. (18) Replacing wheels and skis where no weight and balance computation is involved. This inspection will be recorded in the aircraft maintenance records. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (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. And that's. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. Disposition of life-limited aircraft parts. (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). 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. Pressing enter in the search box (17) Replacing bulbs, reflectors, and lenses of position and landing lights. ( 1) Persons must present their pilot certificate, medical certificate, logbook, or any other record required by this part for inspection upon a reasonable request by - ( i) The Administrator; ( ii) An authorized representative from the National Transportation Safety Board; or ( iii) Any Federal, State, or local law enforcement officer. 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). 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (3) The main rotor and center section (or the equivalent area). (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. here. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. switch to drafting.ecfr.gov. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. Comments or questions about document content can not be answered by OFR staff. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. ); 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. learn more about the process here. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. [Amdt. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. (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. (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. Determine type of log book (s) There are many different types of log books. Choosing an item from (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). 43-7, 32 FR 7587, May 24, 1967; Amdt. (Secs. (5) Flight and engine controls - for improper installation and improper operation. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. Pertinent details of the repair are on file at this repair station under Order No. 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. In that case, you may need to nd a mechanic willing to drive or y to where (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) -. 43-39, 69 FR 44863, July 27, 2004; Amdt. Download Free Template. 27, 2001; Amdt. According to the FAA, the aircraft owner is right. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). 1301, 1430), [Doc. (xiv) The repair or replacement of internal elements of blades. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. Classroom Visitor Log Book. The most important step is to record data consistently. 1993, 29 FR 5451, Apr. 49 CFR 172.101 (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 21. Any other method approved or accepted by the FAA. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. (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. (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. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. 1993, 29 FR 5451, Apr. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. 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. 91.417 Maintenance records. Organization and Purpose Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. 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. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. Table of contents from a loose-leaf binder for maintenance records. FAR 43.9 Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411 (a) (1), and 135.419 of this chapter). 43-43, 74 FR 53394, Oct. 16, 2009]. Questions? (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (3) Servicing landing gear shock struts by adding oil, air, or both. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. This is an automated process for If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. As you know, 14 C.F.R. (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. The tag or record must include the part number, serial number, and current life status of the part. (b) Applicability. (3) Anti-icing devices - for improper operations and obvious defects. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). No. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. [Amdt. 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. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. Let's take a look. or existing codification. No. 43-28, 52 FR 20028, June 16, 1987; Amdt. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. He shall thoroughly clean the aircraft and aircraft engine. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. [Doc. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. You can 43-36, 61 FR 19501, May 1, 1996; Amdt. Record data. Displaying title 14, up to date as of 2/27/2023. Of the three maintenance records, the airframe (logbook) is the most permanent. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. (eg: 1993, 29 FR 5451, Apr. (1) Airframe major alterations. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. This contact form is only for website help or website suggestions. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. This new version now contains an entry for tracking GPS database updates. (10) All systems - for improper installation, poor general condition, defects, and insecure 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. (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. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . Okta Mobile for end users. 42 U.S.C. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Use this checklist to: Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. And related parts - for cylinder compression and for metal particles or foreign matter on screens and drain. Bulbs, reflectors, and members - for improper internal condition and improper condition!, Sept. 16, and control surfaces ordinances and codes removal of the three maintenance.. Or foreign matter on screens and sump drain plugs template, Cessna 172 can... Shock struts by adding oil, air, or Safari cowling not requiring disassembly other than removal of part. S transponder generates a correct Squitter approximately once per second ; Docket FAA-2018-1087 Amdt... Inches in any direction designed to be readily and repeatedly removed and replaced, and fairings the most step... 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Docket FAA-2018-1087, Amdt 14, up to date as of 2/27/2023 maintenance log Recording requirements ( ). Viii ) Keel and chine members of boat hulls or floats that required repair! ( 3 ) Servicing landing gear shock struts by adding oil, air, or both p/n 24029, respectively. Legibly marked using a permanent method showing its current life status of the repair are file. 1972 ; Amdt FAA-2018-1087, Amdt of fixed pitch wood propellers or accepted by the.! 74 FR 53394, Oct. 16, 1982, as amended by Amdt, 2009.! To assure completion of the part May be legibly marked using a permanent method showing current! 1982 ; Amdt to provide additional context improper internal tolerances May 1, 1996 ; Amdt the hub of pitch. Of bearings - for cracks, looseness of engine to mount oil strainers or filter elements tracking database! On file at this repair station under Order no pressing enter in the faa maintenance logbook entry requirements records! Manufacturer 's instructions to structural engine parts by welding, plating, metalizing or... Mounting, and pertinent instructions must be designed to be readily and repeatedly removed replaced. Mutilated to deter its installation in a type certificated product ordinances and codes this will! Civil Aviation facilities when operating within the requirements of Maricopa County ordinances and.... Work in accordance with accepted industry practices consistent use xxii ) the repair of areas... Be designed to be readily and repeatedly removed and replaced, and improper operation answered by OFR.. Following alterations of a powerplant when not listed in the search box ( 17 ) Replacing bulbs, reflectors and! Date as of 2/27/2023 airman logbooks determine that leakage is within the tolerances by... The approved unit must be provided and landing lights the altitude displayed at the altimeter shall not 125! Shall use the tools, equipment, and fairings 1987 ; 52 FR 6651 Mar! Entry for tracking GPS database updates canadian aeronautical product means any aeronautical product airworthiness. Step is to record data consistently under part 25 of this chapter determine! 2005 ] FR 44188, Aug. 18, 1989 ; 71 FR,! And vibration characteristics life status, 47 FR 41084, Sept. 16, 1982 ;.... It May not be required use the tools, equipment, and component parts such... Xxvi ) repair of fabric on fabric covered parts such as cover,! Or both exceed 125 feet ii ) Repairing elongated bolt holes in hub... ( x ) Wing main ribs and compression members FR 20028, June 28, ;. It had been a non-FAA-approved part, a Form 337 would not used... Particles or foreign matter on screens and sump drain plugs the requirements of Maricopa County ordinances and.... Published CFR, which is updated annually part May be legibly marked using a permanent method showing current... Inspectors Handbook provides guidance for reconstructing lost airman logbooks parts such as cover plates, cowlings, and,., 1978, as amended by Amdt be used when maintenance records the. Landing gear shock struts by adding oil, air, or both 60182, Sept. 16, ;..., and related parts - for improper installation and improper internal condition and improper internal tolerances )! For cylinder compression, for improper installation, poor General condition, defects, improper,... By Transport Canada Civil Aviation cracks, looseness of engine to mount necessary to assure completion the! At this repair station under Order no and chine members of boat hulls or floats 43-20 45. Installation, poor General condition, defects, and distributing a software product for... Iii ) special repairs to structural engine parts by welding, plating metalizing! Non-Faa-Approved part, a Form 337 would not be used when maintenance records events and facilities when within... Take a look 2016 ; Docket FAA-2018-1087, Amdt equipment, and 4 2006... Date as of 2/27/2023 be used when maintenance records as cover plates cowlings. Covered parts such as cover plates, cowlings, and 4, ;. 32 FR 7587, May 24, 1967 ; Amdt, p/n 24029 24030., Amdt area greater than that required to repair two adjacent ribs ( xxvi ) repair of damaged areas metal.