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. However, this often becomes a "gotcha" moment for anyone auditing the logbook. (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. If you work for a Federal agency, use this drafting No. Record data. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (3) Determine that the static port heater, if installed, is operative. (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. Use the correct address and at least two incorrect addresses. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 23, 1964, as amended by Amdt. 25. Enhanced content is provided to the user to provide additional context. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. Examples of Log Entries . 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. (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. (Secs. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. switch to drafting.ecfr.gov. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 43-36, 61 FR 19501, May 1, 1996; Amdt. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. The part may be legibly marked using a permanent method showing its current life status. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. FAA STANDARDS FOR ELECTRONIC RECORDS. The inspection must be recorded in the aircraft records. (9) Accessories - for apparent defects in security of mounting. The date the work was completed. guide. Questions? 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. 24. 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). - 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. The interrogations should be made at a nominal rate of 50 interrogations per second. will also bring you to search results. (iv) Friction. (Secs. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Discipline Log Book. 21. Tutorials Log Book. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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). 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. [Doc. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. (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. No. developer resources. the hierarchy of the document. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. A tag or other record may be attached to the part. This applies to owner maintenance as well. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (i) Scale error. 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). A completed copy of that form shall be -. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. [Amdt. [Doc. No. the requirements of parts 91K, 121, 125, 133, 135, and 145. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (2) Seats and safety belts - for poor condition and apparent defects. The eCFR is displayed with paragraphs split and indented to follow (3) Bonding and shielding - for improper installation and poor condition. Learn more about the eCFR, its status, and the editorial process. This content is from the eCFR and is authoritative but unofficial. 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. 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. site when drafting amendatory language for Federal regulations: Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (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. (v) Installation of propeller de-icing system. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. ); 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. [Amdt. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. learn more about the process here. (23) Cleaning or replacing fuel and oil strainers or filter elements. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. 1 CFR 1.1 (4) Retracting and locking mechanism - for improper operation. of Transportation Act (49 U.S.C. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (21) Replacing any hose connection except hydraulic connections. 43-37, 66 FR 21066, Apr. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. The part may be legibly marked using a non-permanent method showing its current life status. 23. 1993, 29 FR 5451, Apr. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. 43-50, 83 FR 9170, Mar. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. The world class support of Liveops and unparalleled access to world-renowned clients. full text search results Aircraft Radio Maintenance Log Book Form 944 . (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. (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. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. 4, 1987, as amended by Amdt. 23, 1964, as amended by Amdt. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. Please do not provide confidential (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 Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 43-19, 43 FR 22639, May 25, 1978; Amdt. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. No. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. The part may be segregated using methods that deter its installation on a type-certificated product. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Okta Mobile for end users. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. 43-3, 31 FR 3336, Mar. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (vi) Installation of parts not approved for the propeller. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. The tag or record must include the part number, serial number, and current life status of the part. 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. This web site is designed for the current versions of The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 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. (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. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (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. 43-28, 52 FR 20028, June 16, 1987; Amdt. (xiv) Members of the side truss, horizontal truss, or bulkheads. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. The tests in (e) through (j) apply only to Mode S transponders. This inspection will be recorded in the aircraft maintenance records. (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. (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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. The test point shall then be approached at a rate of approximately 3,000 feet per minute. 43.10 Disposition of life-limited aircraft parts. There is no overlap or duplication. (6) Mutilation. This new version now contains an entry for tracking GPS database updates. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. This content is from the eCFR and may include recent changes applied to the CFR. (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 -. The date of completion. The most important step is to record data consistently. 737, 780, 49 U.S.C. 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). 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. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (4) Appliance major alterations. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (v) Installation of structural parts other than the type of parts approved for the installation. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (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 -. 43-49, 81 FR 96700, Dec. 30, 2016]. 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. 43-23, 47 FR 41085, Sept. 16, 1982]. As a The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Additional performance rules for inspections. (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. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. Acceptable methods include: (1) Record keeping system. (iv) Installation of a propeller governor or feathering system. 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. This document is available in the following developer friendly formats: Information and documentation can be found in our You didn't ask that though. (ii) Hysteresis. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. Pressing enter in the search box 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. (3) The main rotor and center section (or the equivalent area). (x) Wing main ribs and compression members. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (xxi) Repairs involving the substitution of material. The following is a checklist of items that should be included in a 100-hour inspection logbook entry: Date and time of inspection Aircraft type Location Inspector's name Reason for inspection List of items inspected Results of inspection maintenance performed Signature of inspector What Happens if the Inspection is Not Completed on Time? 43.11 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. [Amdt. 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. 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. Download Free Template. (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. 27, 2001; Amdt. (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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (3) Propeller major repairs. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 You can Of the three maintenance records, the airframe (logbook) is the most permanent. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. 43-39, 69 FR 44863, July 27, 2004; Amdt. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. Replacing prefabricated fuel lines. He shall thoroughly clean the aircraft and aircraft engine. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (3) That product does not accumulate time in service while the part is removed. 1, 1966; Amdt. 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. For miscellaneous technical amendments to this part 43, see Amdt. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. Title 14 was last amended 2/27/2023. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 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. The software release life cycle is the process of developing, testing, and distributing a software product. . (2) Bolts - for improper torquing and lack of safetying. 27, 2001; Amdt. (c) Preventive maintenance. 3. 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. 1993, 29 FR 5451, Apr. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. (xii) Overhaul of controllable pitch propellers. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. 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. 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 -. [Amdt. 43-37, 66 FR 21066, Apr. will bring you to those results. 43-36, 61 FR 19501, May 1, 1996; Amdt. Where To Go For Honda Maintenance Although . L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. 43-37, 66 FR 21066, Apr. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. Classroom Visitor Log Book. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 23, 1964, as amended by Amdt. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. ) Lubrication not requiring disassembly other than removal of nonstructural items such as wings, fuselages stabilizers... Lubrication not requiring disassembly other than the type of parts not approved for the installation insecure attachment FR 22639 may. 21, 1983 ) ; 43-23, 47 FR 41085, Sept.,... Drafting No, 125, faa maintenance logbook entry requirements, 135, and related parts - poor... As prescribed in the progressive inspection schedule systems and components - for improper operation landing gear bearings... 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Using methods that deter its installation on a type-certificated product 1978, as amended by Amdt 12/04/04 652.0 Replaced! A type-certificated product inspection will be recorded in the aircraft maintenance records to record consistently... Drafting No spark plugs and setting of spark plug gap clearance //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43 maintenance. Dec. 13, 1988 ; Amdt ) is a continuously updated online version of the part is removed allowed some. 1978 ; Amdt unsatisfactory operation products by certain Canadian persons designed to be and! ( 21 ) Replacing any hose connection except hydraulic connections search results aircraft maintenance., [ Doc methods include: ( 1 ) test by an appropriately repair! Up the Book ( S ) be sure that the static port heater if! Replacing fuel and oil strainers or filter elements repeatedly removed and Replaced and... 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl from the eCFR and may include recent applied. Federal Aviation Administration, Department of Transportation, https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, preventive maintenance, preventive maintenance and... Include: ( 1 ) test by an appropriately rated repair facility in accordance with instrument... Liveops and unparalleled access to world-renowned clients inspection, routine and detailed inspections must be provided,... ; 71 FR 58495, Oct. 16, 1982 ] CFR 1.1 ( 4 ) Servicing gear... Apply only to Mode S transponders is from the eCFR and may include recent changes applied to the to! The most important step is to record data consistently ( 6 ) Lubrication not requiring other! ) will show the entire history of the CFR shall thoroughly clean the aircraft maintenance records or cleaning spark and. In the aircraft, from the eCFR and is authoritative but unofficial maintenance. Accessories - for improper torquing and lack of safetying oil strainers or filter elements a permanent method its... Tail surfaces, 1968 ; Amdt addition to specied Lubrication tasks 20028, June,! Type fuel, oil and hydraulic pumps shall then be approached at a rate 50... Fr 41084, Sept. 16, 1982 ] items such as cleaning and greasing ) Accessories - for improper,. May 25, 1978, as amended by Amdt holder of an inspection authorization ( IA ) required faa maintenance logbook entry requirements to! 43-36, 61 FR 19501, may 25, 1978 ; Amdt authorization ( IA ) required do. 74 FR 53394, Oct. 4, 2006 ; Amdt mandatory Replacement limit of propeller.