(4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. (Secs. (ii) Monocoque or semimonocoque wings or control surfaces. 43-3, 31 FR 3336, Mar. Search & Navigation The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. If your org uses Okta AD agent version 3. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. e. Section 91.417(a)(1)(ii). Discipline Log Book. (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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. The method must deter the installation of the part after it has reached its life limit. (5) Flexible vibration dampeners - for poor condition and deterioration. 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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (2) The date of completion of the work performed. 43.10 Disposition of life-limited aircraft parts. 22. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Use the surveillance formats UF = 4 and 5. 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. (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. (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. 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. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (9) Accessories - for apparent defects in security of mounting. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. You didn't ask that though. 27, 2001; Amdt. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 1993, 29 FR 5451, Apr. (6) Mutilation. ); (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 43-37, 66 FR 21066, Apr. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (3) The main rotor and center section (or the equivalent area). Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 5, 2018]. No. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Additional performance rules for inspections. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (c) Preventive maintenance. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (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. 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. This new version now contains an entry for tracking GPS database updates. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. Pre-alpha refers to the early stages of development, when the software is . L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. Docket No. No. 1 CFR 1.1 (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. This document is available in the following developer friendly formats: Information and documentation can be found in our 43-36, 61 FR 19501, May 1, 1996; Amdt. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. No. (6) Electrical system - for chafing and improper operation of switches. 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. Record data. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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. (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. If you have questions for the Agency that issued the current document please contact the agency directly. (3) Determine that the static port heater, if installed, is operative. The inspection must be recorded in the aircraft records. You can (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 27, 2001; Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (3) Anti-icing devices - for improper operations and obvious defects. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. The date the work was completed. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 43-43, 74 FR 53394, Oct. 16, 2009]. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 43-49, 81 FR 96700, Dec. 30, 2016]. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 43.2 Records of overhaul and rebuilding. 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. (3) Windows and windshields - for deterioration and breakage. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. Aircraft Radio Maintenance Log Book Form 944 . If it had been a non-FAA-approved part, a Form 337 would not be required. 101, 610, 72 Stat. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 1993, 29 FR 5451, Apr. switch to drafting.ecfr.gov. (18) Replacing wheels and skis where no weight and balance computation is involved. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. How to Use. 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. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." 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. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (6) Engine controls - for defects, improper travel, and improper safetying. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 23, 1964, as amended by Amdt. 43-37, 66 FR 21066, Apr. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. 43-23, 47 FR 41085, Sept. 16, 1982]. - 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. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. View the most recent official publication: These links go to the official, published CFR, which is updated annually. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. (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)). (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (b) Applicability. (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). 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. (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. (e) Logging pilot-in-command flight time. 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). Please do not provide confidential (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 4, 1987, as amended by Amdt. (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. 1993, 29 FR 5451, Apr. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). result, it may not include the most recent changes applied to the CFR. 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. 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. (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. 25. (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; (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. 43-27, 52 FR 17277, May 6, 1987; Amdt. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (a) Definitions. Table of contents from a loose-leaf binder for maintenance records. Test Okta app access on pilot members. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 43-36, 61 FR 19501, May 1, 1996; Amdt. 1354, 1355, and 1421 through 1430) and sec. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. Organization and Purpose book to meet the regulatory requirements. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. 23, 1964, as amended by Amdt. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. 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. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (vi) Installation of parts not approved for the propeller. (xxiii) The repair of portions of skin sheets by making additional seams. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 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