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faa maintenance logbook entry requirements

43-36, 61 FR 19501, May 1, 1996; Amdt. Of the three maintenance records, the airframe (logbook) is the most permanent. Title 14 was last amended 2/27/2023. 43-3, 31 FR 3336, Mar. According to the FAA, the aircraft owner is right. (2) Powerplant major alterations. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (c) Disposition of parts removed from type-certificated products. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. 43.2 Records of overhaul and rebuilding. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Maintenance records: Falsification, reproduction, or alteration. 23. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). Please do not provide confidential The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. SB-115 (10/26/83) -- Deflation Panel Pull Forces . Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (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. Aircraft Inspection and Repair - Federal Aviation . Use this checklist to: Aircraft Radio Maintenance Log Book Form 944 . (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 65.101 Eligibility requirements: General. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. 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. (iii) Performed without the use of tools and/or special equipment. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. FAA-2018-0119, Amdt. developer resources. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. Pre-alpha refers to the early stages of development, when the software is . (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. The test point shall be approached at a rate compatible with the test equipment. 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. 25. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (7) Other methods. (iv) Friction. (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. The inspection must be recorded in the aircraft records. Enhanced content is provided to the user to provide additional context. switch to drafting.ecfr.gov. The part may be mutilated to deter its installation in a type certificated product. (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 -. If it had been a non-FAA-approved part, a Form 337 would not be required. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 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: (1) A description (or reference to data acceptable to the Administrator) of work performed. 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. There is no overlap or duplication. (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. (xii) Overhaul of controllable pitch propellers. (21) Replacing any hose connection except hydraulic connections. 22. (6) Mutilation. 43-49, 81 FR 96700, Dec. 30, 2016]. (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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). Organization and Purpose Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. The 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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The method must deter the installation of the part after it has reached its life limit. (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. 27, 2001; Amdt. 43.12 Maintenance records: Falsification, reproduction, or alteration. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. 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. (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. [Amdt. (xiv) Members of the side truss, horizontal truss, or bulkheads. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. 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 . [Amdt. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. Search & Navigation 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. 1993, 29 FR 5451, Apr. 43-37, 66 FR 21066, Apr. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (Secs. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Determine type of log book (s) There are many different types of log books. 23, 1964, as amended by Amdt. (b) Rotorcraft. 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). 6(c), Dept. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. ___, 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. Pertinent details of the repair are on file at this repair station under Order No. (iv) Complete disassembly of complex hydraulic power valves. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (3) Bonding and shielding - for improper installation and poor condition. 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. (2) Replacing elastic shock absorber cords on landing gear. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . here. No. (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. 43-36, 61 FR 19501, May 1, 1996; Amdt. 1993, 29 FR 5451, Apr. As you know, 14 C.F.R. (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). (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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (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. No. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (a) Definitions used in this section. 1354, 1421 through 1430 and 1502); (49 U.S.C. A completed copy of that form shall be -. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. The tests in (e) through (j) apply only to Mode S transponders. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). Comments or questions about document content can not be answered by OFR staff. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. 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. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 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. (7) Wheels - for cracks, defects, and condition of bearings. (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. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. No. (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. 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). (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (iii) After effect. 23, 1964, as amended by Amdt. Aviation Act of 1958 as amended by Amdt by the FAA lists separate requirements log. Removable or integral fuel tanks and oil tanks by legally authorized motor vehicle racing events and facilities when operating the! And poor condition part after it has reached its life limit Mode s.! 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29 de março de 2023

43-36, 61 FR 19501, May 1, 1996; Amdt. Of the three maintenance records, the airframe (logbook) is the most permanent. Title 14 was last amended 2/27/2023. 43-3, 31 FR 3336, Mar. According to the FAA, the aircraft owner is right. (2) Powerplant major alterations. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (c) Disposition of parts removed from type-certificated products. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. 43.2 Records of overhaul and rebuilding. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Maintenance records: Falsification, reproduction, or alteration. 23. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). Please do not provide confidential The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. SB-115 (10/26/83) -- Deflation Panel Pull Forces . Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (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. Aircraft Inspection and Repair - Federal Aviation . Use this checklist to: Aircraft Radio Maintenance Log Book Form 944 . (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 65.101 Eligibility requirements: General. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. 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. (iii) Performed without the use of tools and/or special equipment. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. FAA-2018-0119, Amdt. developer resources. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. Pre-alpha refers to the early stages of development, when the software is . (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. The test point shall be approached at a rate compatible with the test equipment. 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. 25. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (7) Other methods. (iv) Friction. (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. The inspection must be recorded in the aircraft records. Enhanced content is provided to the user to provide additional context. switch to drafting.ecfr.gov. The part may be mutilated to deter its installation in a type certificated product. (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 -. If it had been a non-FAA-approved part, a Form 337 would not be required. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 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: (1) A description (or reference to data acceptable to the Administrator) of work performed. 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. There is no overlap or duplication. (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. (xii) Overhaul of controllable pitch propellers. (21) Replacing any hose connection except hydraulic connections. 22. (6) Mutilation. 43-49, 81 FR 96700, Dec. 30, 2016]. (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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). Organization and Purpose Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. The 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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The method must deter the installation of the part after it has reached its life limit. (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. 27, 2001; Amdt. 43.12 Maintenance records: Falsification, reproduction, or alteration. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. 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. (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. [Amdt. (xiv) Members of the side truss, horizontal truss, or bulkheads. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. 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 . [Amdt. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. Search & Navigation 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. 1993, 29 FR 5451, Apr. 43-37, 66 FR 21066, Apr. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (Secs. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Determine type of log book (s) There are many different types of log books. 23, 1964, as amended by Amdt. (b) Rotorcraft. 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). 6(c), Dept. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. ___, 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. Pertinent details of the repair are on file at this repair station under Order No. (iv) Complete disassembly of complex hydraulic power valves. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (3) Bonding and shielding - for improper installation and poor condition. 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. (2) Replacing elastic shock absorber cords on landing gear. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . here. No. (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. 43-36, 61 FR 19501, May 1, 1996; Amdt. 1993, 29 FR 5451, Apr. As you know, 14 C.F.R. (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). (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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (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. No. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (a) Definitions used in this section. 1354, 1421 through 1430 and 1502); (49 U.S.C. A completed copy of that form shall be -. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. The tests in (e) through (j) apply only to Mode S transponders. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). Comments or questions about document content can not be answered by OFR staff. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. 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. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 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. (7) Wheels - for cracks, defects, and condition of bearings. (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. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. No. (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. 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). (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (iii) After effect. 23, 1964, as amended by Amdt. Aviation Act of 1958 as amended by Amdt by the FAA lists separate requirements log. Removable or integral fuel tanks and oil tanks by legally authorized motor vehicle racing events and facilities when operating the! And poor condition part after it has reached its life limit Mode s.! 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