23. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. Comments or questions about document content can not be answered by OFR staff. Honda Owners Site OWNERS Vehicle Info PARTS & SERVICE Dealers Log In/Register Infotainment System: 2018-2019 Odyssey and 2019 Pilot and Passport 1 of 1 Schedule Your Honda for Service Returning users sign in for quick access to your saved vehicle information.Support and Service Warranty Info . (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. (ix) Hydraulic and electrical actuating system of components. 1/1.1 (3) The main rotor and center section (or the equivalent area). Okta Mobile for end users. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (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. 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 official, published CFR, is updated annually and available below under (v) Installation of propeller de-icing system. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. The error at all test points must not exceed the tolerances specified in Table I. (2) Powerplant major repairs. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (21) Replacing any hose connection except hydraulic connections. If you have questions for the Agency that issued the current document please contact the agency directly. 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). (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. For the purposes of this section the following definitions apply. No. (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. (5) Flexible vibration dampeners - for poor condition and deterioration. 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. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. [Amdt. (vi) Barometric scale error. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 737, 780, 49 U.S.C. (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. 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. (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. Regulation Y (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. No. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 43-37, 66 FR 21066, Apr. (2) Bolts - for improper torquing and lack of safetying. The method must deter the installation of the part after it has reached its life limit. How to Use. (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. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. There is no overlap or duplication. (iii) Rewinding the field coil of an electrical accessory. (b) Temporary removal of parts from type-certificated products. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. (7) Other methods. (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. Displaying title 14, up to date as of 2/27/2023. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. (c) Preventive maintenance. 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. (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. 1993, 29 FR 5451, Apr. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. The interrogations should be made at a nominal rate of 50 interrogations per second. (b) Listing of discrepancies and placards. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. (2) Shock absorbing devices - for improper oleo fluid level. Table of contents from a loose-leaf binder for maintenance records. (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. ); (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). 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. through logbooks usually kept in the maintenance hangar. FAA-2015-1621, Amdt. This important rule sets the requirements for the recording. 43-23, 47 FR 41085, Sept. 16, 1982]. Use the surveillance formats UF = 4 and 5. . (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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. The part may be legibly marked using a permanent method showing its current life status. (Secs. contact the publishing agency. (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. 23, 1964, as amended by Amdt. (a) Maintenance record entries. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (a) Definitions. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. FAA STANDARDS FOR ELECTRONIC RECORDS. (Secs. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (xxi) Repairs involving the substitution of material. 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. Noise emanating from trains and associated repair and maintenance equipment. The tests in (e) through (j) apply only to Mode S transponders. (v) Case leak. 101, 610, 72 Stat. switch to drafting.ecfr.gov. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. (ii) Repairing or machining of steel hubs. 23, 1964, as amended by Amdt. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. (iii) Installation of an accessory which is not approved for the engine. the requirements of parts 91K, 121, 125, 133, 135, and 145. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. Choosing an item from (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. 1301, 1430), [Doc. Use the correct address and at least two incorrect addresses. (2) The date of completion of the work performed. 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. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (2) Tag or record attached to part. (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. No. 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. [Doc. [Amdt. (5) Segregation. This inspection will be recorded in the aircraft maintenance records. 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 -. 43.15 Additional performance rules for inspections. 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. (Secs. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 (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 -. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. Use this checklist to: Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. here. (6) Electrical system - for chafing and improper operation of switches. 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