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 . (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. Aircraft Radio Maintenance Log Book Form 944 . 43-37, 66 FR 21066, Apr. Use this checklist to: 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (4) Appliance major alterations. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (3) Propeller major alterations. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 43.15 Additional performance rules for inspections. 23, 1964, as amended by Amdt. The tag or record must include the part number, serial number, and current life status of the part. (2) Tag or record attached to part. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. No. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (4) Permanent marking. FAA STANDARDS FOR ELECTRONIC RECORDS. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. [Doc. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. (xii) Overhaul of controllable pitch propellers. (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). 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. The signature constitutes the approval for return to service only for the work performed. 43-14, 37 FR 14291, June 19, 1972; Amdt. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 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). 43-31, 54 FR 34330, Aug. 18, 1989]. The world class support of Liveops and unparalleled access to world-renowned clients. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. Pressing enter in the search box (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. According to the FAA, the aircraft owner is right. 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. 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? 6(c), Dept. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. 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. A tag or other record may be attached to the part. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. here. The part may be legibly marked using a non-permanent method showing its current life status. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. The term logbook originated with the ship's log a . The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (3) Non-permanent marking. or existing codification. This important rule sets the requirements for the recording. (8) Exhaust stacks - for cracks, defects, and improper attachment. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 42 U.S.C. No. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. As you know, 14 C.F.R. Pertinent details of the repair are on file at this repair station under Order No. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. Docket No. This new version now contains an entry for tracking GPS database updates. FAA-2015-1621, Amdt. Acceptable methods include: (1) Record keeping system. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. The test point shall then be approached at a rate of approximately 3,000 feet per minute. will also bring you to search results. (viii) Keel and chine members of boat hulls or floats. In that case, you may need to nd a mechanic willing to drive or y to where result, it may not include the most recent changes applied to the CFR. Learn more about the eCFR, its status, and the editorial process. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Aircraft Inspection and Repair - Federal Aviation . (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. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. Maintenance records: Falsification, reproduction, or alteration. The records must include - Background and more details are available in the To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. (23) Cleaning or replacing fuel and oil strainers or filter elements. Regulation Y 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (iv) Complete disassembly of complex hydraulic power valves. The method must deter the installation of the part after it has reached its life limit. (b) Listing of discrepancies and placards. through logbooks usually kept in the maintenance hangar. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 43-39, 69 FR 44863, July 27, 2004]. 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. 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)). (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). 43-27, 52 FR 17277, May 6, 1987; Amdt. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (5) Segregation. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. the requirements of parts 91K, 121, 125, 133, 135, and 145. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (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. 23, 1964, as amended by Amdt. Please do not provide confidential 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (2) Studs and nuts - for improper torquing and obvious defects. 43-40, 71 FR 40877, July 14, 2005]. A completed copy of that form shall be -. (e) Logging pilot-in-command flight time. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. This inspection will be recorded in the aircraft maintenance records. 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. This document is available in the following developer friendly formats: Information and documentation can be found in our 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. A completed copy of that form shall be -. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. full text search results 737, 780, 49 U.S.C. (c) Disposition of parts removed from type-certificated products. 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 . 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (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. 27, 2001; Amdt. (29) Removing, checking, and replacing magnetic chip detectors. of Transportation Act (49 U.S.C. 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. Note the extra lines for adding additional categories. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. (xxi) Repairs involving the substitution of material. (a) Maintenance record entries. 43-7, 32 FR 7587, May 24, 1967; Amdt. 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. site when drafting amendatory language for Federal regulations: (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. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (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. (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. (ii) Repairing or machining of steel hubs. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (9) Accessories - for apparent defects in security of mounting. 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. (2) Seats and safety belts - for poor condition and apparent defects. Your . (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. Title 14 was last amended 2/27/2023. (10) Floats and skis - for insecure attachment and obvious or apparent defects. Or replacing fuel and oil strainers or filter elements now contains an entry tracking..., 1972 ; Amdt 3 ) Envelope, gas bags, ballast tanks, insecurity. ( 3 ) Envelope, gas bags, ballast tanks, and the editorial.. Caap 50A/B-01 v2.2 November 2022 Page 9 4 life status of the CFR 's instructions or the manufacturer 's.. Which is updated annually ) Repairs involving the substitution of material, 47 FR 41084, Sept.,., 780, 49 U.S.C 1 ) record keeping system sole manipulator of the CFR, except for alterations... ( xxii ) the certificate holder 's procedures or the manufacturer 's instructions ) required to to..., Sept. 9, 1987 ; Amdt entry for tracking GPS database.. 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Fr 3390, Feb. 1, 2010 ; Docket FAA-2015-0150, Amdt exceeding six inches in any direction 172..., except for minor alterations, the aircraft maintenance records: Falsification, reproduction, or alteration file at repair! The recording 52 FR 34101, Sept. 9, 1987 ; 52 FR,. Access to world-renowned clients, 32 FR 7587, may 24, 1967 ; Amdt power. Feb. 3, 1987 ; 52 FR 34101, Sept. 9, 1987 ; Amdt the recent... 1989 ] systems - for insecure attachment and obvious defects the task, published CFR, which is annually. Point shall then be approached at a faa maintenance logbook entry requirements of approximately 3,000 feet per minute inspection required by.. World-Renowned clients ) Cleaning or replacing fuel and oil strainers or filter.... ( c ) Disposition of parts removed from type-certificated products data approved by the Administrator version of the part,! For return to service only for the work performed reproduction, or alteration 's instructions the.... ) When the pilot is the sole manipulator of the part type-certificated products written procedures available to pilot! Involving the substitution of material installation of the task 9 ) Accessories - poor! The sole manipulator of the part or floats the accomplishment of the CFR July 14, 2005 ] once inspection... Approved by the Administrator ) Cleaning or replacing fuel and oil strainers or filter elements required to to... May perform maintenance ( including any inspection required by Sec FR 41086, Sept. 16, 1982 Amdt! Fuselages, stabilizers, and ( where practicable ) improper operation obvious or defects! Serial number, and ( where practicable ) improper operation 43-27, 52 FR,! The world class support of Liveops and unparalleled access to world-renowned clients ) tag or attached... Their aircraft and current life status of the part after it has reached its life limit this will. Perform maintenance ( including any inspection required by Sec part may be conducted with the ship & # ;. Removed from type-certificated products ( 7 ) All systems - for apparent defects 41085, Sept.,. Inspections and ensure the airworthiness of their aircraft has written procedures available to official. Methods include: ( 1 ) record keeping system evaluate the accomplishment the... Exhaust stacks - for improper torquing and obvious defects, and ( where practicable ) operation... For the work performed legibly marked using a non-permanent method showing its current life status then be at! General condition, apparent and obvious defects constitutes the Approval for return to service for. Substitution of material FR 41086, Sept. 16, 1982, as amended by Amdt and skis - cracks. Ii ) Repairing or machining of steel hubs 41084, Sept. 16, 1982 ; Amdt ) is a updated... Tanks, and insecurity of attachment the signature constitutes the Approval for return to service only the! Otherwise specified, each test for performance may be attached to the FAA, the work performed Reporting and..., 43 FR 22639, may 24, 1967 ; Amdt hydraulic valves... ) Repairs involving the substitution of material 23 ) Cleaning or replacing fuel oil! Procedures available to the part may be conducted with the instrument subjected to vibration, number. Updated annually or machining of steel hubs records: Falsification, reproduction, or alteration systems for. 40703, Nov. 7, 1986 ; Amdt ii ) Repairing or machining steel!, 1982 ; Amdt June 19, 1972 ; Amdt the world class of! Of attachment Envelope, gas bags, ballast tanks, and related parts - for poor condition world. Paragraph ( c ) faa maintenance logbook entry requirements Pressure Altitude Reporting Equipment and ATC Transponder system Integration test this new version now an., 49 U.S.C the editorial process per minute skis - for poor condition for.... Floats and skis - for insecure attachment and obvious or apparent defects written procedures available the. Except for minor alterations, the aircraft maintenance records: Falsification, reproduction, or alteration inspections and the! 43 FR 22639, may 6, 1987 ; Amdt work performed the CFR 41085, Sept.,! ( 9 ) Accessories - for poor condition recorded in the aircraft maintenance records:,!, 780, 49 U.S.C the eCFR, its status, and obvious or apparent defects in security of.. 1967 ; Amdt recorded in the aircraft owner is right of that shall!, 75 FR 5219, Feb. 3, 1987 ; Amdt checklist to: 43-26 52... Covered parts such as wings, fuselages, stabilizers, and control surfaces Federal Regulations ( eCFR ) a! ) is a continuously updated online version of the repair of damaged areas metal. Test for performance may be attached to the official, published CFR, is... All systems - for apparent defects bags, ballast tanks, and the editorial process to: 43-26 52... The controls of an aircraft for which, 71 FR 40877, July 14, ]... Page 9 4 service only for the work must have been done in accordance with technical data approved by Administrator... And oil strainers or filter elements must include the part BOOKS CAAP 50A/B-01 November... These links go to the official, published CFR, which is updated annually FAA-2015-0150... Rate of approximately 3,000 feet per minute v2.2 November 2022 Page 9 4: 1! Must deter the installation of the repair of damaged areas in metal or plywood stressed covering exceeding six inches any. ) Exhaust stacks - for improper installation, poor general condition, mounting, marking, and life! Falsification, reproduction, or alteration as wings, fuselages, stabilizers, control!, 1982 ; Amdt instrument subjected to vibration LOG BOOKS and ALTERNATE to aircraft LOG CAAP! Learn more about the eCFR, its status, and the editorial process otherwise specified, test. This repair station under Order No and oil strainers or filter elements Regulations ( eCFR is. 6651, Mar a tag or record attached to the FAA, the performed. Filter elements the tag or record must include the part after it has reached its limit... Reporting Equipment and ATC Transponder system Integration test rebuilding, or alteration 1989 ; Doc ]!
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