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. (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. 737, 780, 49 U.S.C. ___, 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. 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. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 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. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (3) Servicing landing gear shock struts by adding oil, air, or both. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. the requirements of parts 91K, 121, 125, 133, 135, and 145. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. FAA STANDARDS FOR ELECTRONIC RECORDS. (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). The part may be legibly marked using a non-permanent method showing its current life status. No. (3) Determine that the static port heater, if installed, is operative. 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. 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. 43-39, 69 FR 44863, July 27, 2004]. (3) The main rotor and center section (or the equivalent area). (b) Rotorcraft. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. The tests in (e) through (j) apply only to Mode S transponders. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . (ix) Hydraulic and electrical actuating system of components. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (2) Shock absorbing devices - for improper oleo fluid level. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). 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. (7) Wheels - for cracks, defects, and condition of bearings. 43.15 Additional performance rules for inspections. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Use this checklist to: Aircraft Radio Maintenance Log Book Form 944 . (4) The maintenance, preventive maintenance, or alteration is recorded in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter. (23) Cleaning or replacing fuel and oil strainers or filter elements. This applies to owner maintenance as well. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (d) Transfer of life-limited parts. (6) Mutilation. The method must deter the installation of the part after it has reached its life limit. (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 -. Pressing enter in the search box Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Tutorials Log Book. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (4) Retracting and locking mechanism - for improper operation. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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. 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? 23, 1964, as amended by Amdt. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (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) -. will bring you directly to the content. 43-36, 61 FR 19501, May 1, 1996; Amdt. The world class support of Liveops and unparalleled access to world-renowned clients. Acceptable methods include: (1) Record keeping system. Okta Mobile for end users. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 43-36, 61 FR 19501, May 1, 1996; Amdt. (xv) Main seat support braces and brackets. (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. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. For miscellaneous technical amendments to this part 43, see Amdt. (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. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Each time the part is removed from a type certificated product, the record must be updated with the current life status. [Amdt. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (v) Replacement of outer laminations on fixed pitch wood propellers. Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. 1354, 1355, and 1421 through 1430) and sec. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Each is a special inspection unto itself; they're all different. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (2) The date of completion of the work performed. Docket No. 43.10 Disposition of life-limited aircraft parts. 1993, 29 FR 5451, Apr. This content is from the eCFR and may include recent changes applied to the CFR. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. Learn more about the eCFR, its status, and the editorial process. 7572; 49 U.S.C. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. 5, 2018]. Determine type of log book (s) There are many different types of log books. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (3) Propeller major alterations. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 23, 1964, as amended by Amdt. learn more about the process here. Enhanced content is provided to the user to provide additional context. (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. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and 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. information or personal data. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. 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. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 23, 1964, as amended by Amdt. If you have questions for the Agency that issued the current document please contact the agency directly. Record data. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. 41085, Sept. 16, 1982, as amended by Amdt ForeFlight Web the world class of! With expanded access on ForeFlight Web except for minor alterations, the Record must be with. Pic time in 61.51 ( e ) through ( j ) apply only to S... 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