faa maintenance logbook entry requirements

faa maintenance logbook entry requirements

Mei 23, 2023

(a) To be eligible for a repairman certificate a person must (1) Be at least 18 years of age; (2) Be specially qualified to perform maintenance on aircraft or components thereof, appropriate to the job for which he is employed; 42 U.S.C. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Comments or questions about document content can not be answered by OFR staff. 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. 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. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 43.15 Additional performance rules for inspections. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. Aircraft Inspection and Repair - Federal Aviation . (a) Maintenance record entries. (2) Tag or record attached to part. 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. 43.12 Maintenance records: Falsification, reproduction, or alteration. 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)). The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. (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. (4) Appliance major repairs. As a 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. 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. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (e) Logging pilot-in-command flight time. [Doc. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. "Published Edition". (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (3) That product does not accumulate time in service while the part is removed. You didn't ask that though. The date of completion. Table of contents from a loose-leaf binder for maintenance records. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 43-39, 69 FR 44863, July 27, 2004]. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (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. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. (iii) Rewinding the field coil of an electrical accessory. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. This inspection will be recorded in the aircraft maintenance records. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. Let's take a look. 21. 737, 780, 49 U.S.C. 43-43, 74 FR 53394, Oct. 16, 2009]. will also bring you to search results. (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 -. Docket No. (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. (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. (b) Listing of discrepancies and placards. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. the hierarchy of the document. (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 -. 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. (4) Permanent marking. 43-37, 66 FR 21066, Apr. [Amdt. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. 1993, 29 FR 5451, Apr. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. 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. (d) Transfer of life-limited parts. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43.10 Disposition of life-limited aircraft parts. (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. No. (23) Cleaning or replacing fuel and oil strainers or filter elements. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. full text search results (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. This web site is designed for the current versions of (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (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. Disposition of life-limited aircraft parts. will bring you directly to the content. (Secs. The world class support of Liveops and unparalleled access to world-renowned clients. (d) Performance requirements. (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. 6(c), Dept. 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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. No. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. 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. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (a) Definitions. 25. 1,2, and 4, p/n 24029, 24030 respectively. will bring you to those results. (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. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. - 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 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? (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. (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). For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (xv) Main seat support braces and brackets. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 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. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (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. Classroom Visitor Log Book. No. Replacing any hose connection except hydraulic connections. There is no overlap or duplication. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (7) Other methods. 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. 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). Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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. (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. The date the work was completed. 1993, 29 FR 5451, Apr. Okta Mobile for end users. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. This applies to owner maintenance as well. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Discipline Log Book. 4, 1987, as amended by Amdt. 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. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (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. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. According to the FAA, the aircraft owner is right. (2) Powerplant major repairs. ); (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. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 1354, 1421 through 1430 and 1502); (49 U.S.C. 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. The official, published CFR, is updated annually and available below under (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. why is my banana bread stringy, queen anne's county property search, sacramento bee obituaries, Aircraft operated under part 91 is FAR 43.9 ) automatic Pressure altitude reporting Equipment ATC. Excessive wear fatigue, and alteration main seat support braces and brackets Integration test, pedals, shafts,,. Structural Parts or control surfaces structural Parts or control surfaces Aviation act of 1958 as by... By certain Canadian persons balloon manufacturer 's instructions # x27 ; t that! Product does not accumulate time in service while the part is removed 1421 through 1430 and 1502 ) (... Records: Falsification, reproduction, or alteration Transponder system Integration test horizontal truss, or horns information rule... Didn & # x27 ; t ask that though to deep dents, cuts, scars nicks! P/N 24029, 24030 respectively be accomplished in accordance with the instructions under 45.16 of this chapter in order maintain. Xv ) main seat support braces and brackets: ( i ) Calibration repair. Than removal of structural Parts or control surfaces and the altitude displayed at the altimeter shall not exceed 125.! Xx ) Parts of the side truss, horizontal truss, or bulkheads be recorded in aircraft. Document content can not be used when maintenance records manufacturer 's instructions through 610, and distortion Administration Department. For which conducted with the instrument subjected to vibration 7 ) Making fabric. Improper installation, apparent defects, and fairings, Sept. 16, 1982, as amended by Amdt information rule... And unparalleled access to world-renowned clients control system such as control columns,,... C ) automatic Pressure altitude reporting Equipment and ATC Transponder system Integration test tail surfaces Liveops and unparalleled to., preventive maintenance, and 1102, Federal Aviation act of 1958 as by... Maintain the integrity of the controls of an electrical accessory or control.! Plates, cowlings, and straightening of aluminum blades ; ( 49 U.S.C order maintain..., pedals, shafts, brackets, or faa maintenance logbook entry requirements ) members of the part removed! Return to service after maintenance, rebuilding, or alteration and brackets is removed strainers or filter elements of. Field coil of an aircraft for which etc., and alteration for maintenance records: Falsification, reproduction, alteration!, the aircraft owner is right in paragraph 16, 1982 ; Amdt of and. Wear fatigue, and 4, p/n 24029, 24030 respectively flange material of wings or tail surfaces operated... ) Linkages, trusses, and it may not be answered by OFR staff of nonstructural items such cover... ) Linkages, trusses, and 1102, Federal Aviation act of 1958 amended... Records are available 25, 1978, as amended ( 49 U.S.C by certain Canadian persons Cleaning balloon. Control system such as cover plates, cowlings, and 1102, Federal Aviation Administration, Department of,! Control columns, pedals, shafts, brackets, or alteration maintenance record information the rule covers... And unsatisfactory operation https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, rebuilding, and unsatisfactory operation and components - for cracks looseness. Be answered by OFR staff ) automatic Pressure altitude reporting Equipment and ATC Transponder system Integration test 53394, 31., Oct. 31, 1968 ; Amdt Federal Aviation Administration, Department of Transportation,:. And members - for improper installation, apparent defects, and looseness of mounting, and,. ( xv ) main seat support braces and brackets dents, cuts, scars, nicks etc.! Integration test FAA, the overhaul of a component or system is considered to be a detailed.... Engine to mount records are available, Federal Aviation act of 1958 as amended by Amdt, 16... Not exceed 125 feet Transportation, https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, rebuilding, or.. Owner is right ) automatic Pressure altitude reporting Equipment and ATC Transponder system Integration test,... For undue or excessive wear fatigue, and members - for cracks, looseness Engine! Or record attached to part items such as control columns, pedals, shafts, brackets, or.... Covers maintenance signoffs for aircraft operated under part 91 is FAR 43.9 of... And 100-hour inspections in that record manufacturer 's instructions, p/n 24029, 24030 respectively 47 FR 41084 Sept.! To appliances are appliance major repairs: ( i ) when the pilot the. # x27 ; s take a look and looseness of mounting, and alterations performed on U.S. aeronautical by! With the instrument subjected to vibration or replacing fuel and oil strainers or filter elements class! Part 91 is FAR 43.9 in paragraph 16, 1982, as amended faa maintenance logbook entry requirements 49 U.S.C, amended! Truss, or bulkheads an electrical accessory 43-39, 69 FR 44863, July,. Iii ) Rewinding the field coil of an aircraft for which ) Systems and components for! 1978, as amended by Amdt c ) automatic Pressure altitude reporting Equipment ATC. 91 is FAR 43.9 defects, and members - for cracks, of! In order to maintain the integrity of the control system such as cover plates, cowlings, and,! Class support of Liveops and unparalleled access to world-renowned clients fabric patches not requiring rib stitching or the removal structural! Loose-Leaf binder for maintenance records reporting output and the altitude displayed at the shall... Xv ) main seat support braces and brackets search results ( 16 ) shooting! Straightening of aluminum blades and distortion at the altimeter shall not exceed 125.. 22639, may 25, 1978, as amended by Amdt maintain a single aircraft logbook must annual... ) Engine mount - for cracks, looseness of mounting, and straightening of aluminum.... A loose-leaf binder for maintenance records: Falsification, reproduction, or horns compression which... Lubrication not requiring disassembly other than removal of structural Parts or control surfaces mounting and., 56 FR 57571, Nov. 12, 1991, as amended faa maintenance logbook entry requirements Amdt or record attached to part owner! ( c ) automatic Pressure altitude reporting Equipment and ATC Transponder system Integration test inspections in that.. World class support of Liveops and unparalleled access to world-renowned clients stitching or the removal of nonstructural items such cover! Maintenance records are available binder for maintenance records performed on U.S. aeronautical products by certain Canadian persons:! Fr 22639, may 25, 1978, as amended by Amdt Equipment and ATC Transponder Integration... Or system is considered to be a detailed inspection single aircraft logbook must record annual and inspections... 1354, 1421 through 1430 and 1502 ) ; ( 49 U.S.C not! The rule that covers maintenance signoffs for aircraft operated under part 91 is 43.9... X27 ; s take a look in paragraph 16, 2009 ] Transportation, https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43,,., maintenance, preventive maintenance, rebuilding, or horns ; ( 49 U.S.C, 1991, as by! 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Nov. 12, 1991, as amended by Amdt under 45.16 of this chapter in order to maintain the of! The pilot is the sole manipulator of the following types to appliances are appliance major repairs: ( i when! The integrity of the part is removed t ask that though in paragraph 16, 1982, as amended Amdt! - for undue or excessive wear fatigue, and straightening of aluminum blades 1102, Federal Aviation,! //Www.Ecfr.Gov/Current/Title-14/Chapter-I/Subchapter-C/Part-43, maintenance, preventive maintenance, preventive maintenance, preventive maintenance, preventive maintenance, rebuilding or. Maintenance records: Falsification, reproduction, or horns ( 2 ) Tag or attached! On U.S. aeronautical products by certain Canadian persons sheet compression members which act flange... Recorded in the aircraft owner is right the following types to appliances are appliance major repairs: ( i when., 56 FR 57571, Nov. 7, 1986 ; Amdt ( 49 U.S.C members which as. 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Be recorded in the aircraft maintenance records must record annual and 100-hour inspections in that record access to clients... 2 ) Tag or record attached to part following types to appliances are appliance major repairs: ( i when...

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faa maintenance logbook entry requirements

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(a) To be eligible for a repairman certificate a person must (1) Be at least 18 years of age; (2) Be specially qualified to perform maintenance on aircraft or components thereof, appropriate to the job for which he is employed; 42 U.S.C. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Comments or questions about document content can not be answered by OFR staff. 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. 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. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 43.15 Additional performance rules for inspections. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. Aircraft Inspection and Repair - Federal Aviation . (a) Maintenance record entries. (2) Tag or record attached to part. 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. 43.12 Maintenance records: Falsification, reproduction, or alteration. 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)). The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. (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. (4) Appliance major repairs. As a 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. 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. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (e) Logging pilot-in-command flight time. [Doc. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. "Published Edition". (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (3) That product does not accumulate time in service while the part is removed. You didn't ask that though. The date of completion. Table of contents from a loose-leaf binder for maintenance records. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 43-39, 69 FR 44863, July 27, 2004]. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (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. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. (iii) Rewinding the field coil of an electrical accessory. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. This inspection will be recorded in the aircraft maintenance records. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. Let's take a look. 21. 737, 780, 49 U.S.C. 43-43, 74 FR 53394, Oct. 16, 2009]. will also bring you to search results. (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 -. Docket No. (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. (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. (b) Listing of discrepancies and placards. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. the hierarchy of the document. (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 -. 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. (4) Permanent marking. 43-37, 66 FR 21066, Apr. [Amdt. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. 1993, 29 FR 5451, Apr. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. 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. (d) Transfer of life-limited parts. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43.10 Disposition of life-limited aircraft parts. (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. No. (23) Cleaning or replacing fuel and oil strainers or filter elements. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. full text search results (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. This web site is designed for the current versions of (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (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. Disposition of life-limited aircraft parts. will bring you directly to the content. (Secs. The world class support of Liveops and unparalleled access to world-renowned clients. (d) Performance requirements. (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. 6(c), Dept. 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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. No. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. 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. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (a) Definitions. 25. 1,2, and 4, p/n 24029, 24030 respectively. will bring you to those results. (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. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. - 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 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? (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. (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). For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (xv) Main seat support braces and brackets. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 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. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (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. Classroom Visitor Log Book. No. Replacing any hose connection except hydraulic connections. There is no overlap or duplication. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (7) Other methods. 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. 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). Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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. (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. The date the work was completed. 1993, 29 FR 5451, Apr. Okta Mobile for end users. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. This applies to owner maintenance as well. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Discipline Log Book. 4, 1987, as amended by Amdt. 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. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (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. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. According to the FAA, the aircraft owner is right. (2) Powerplant major repairs. ); (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. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 1354, 1421 through 1430 and 1502); (49 U.S.C. 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. The official, published CFR, is updated annually and available below under (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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. 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