For miscellaneous technical amendments to this part 43, see Amdt. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 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. The tag or record must include the part number, serial number, and current life status of the part. 27, 2001; Amdt. (e) Logging pilot-in-command flight time. 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. (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. Docket No. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. (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. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. If you have questions or comments regarding a published document please 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. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 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. 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). Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (a) Maintenance record entries. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Record data. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. (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.. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 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. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 43.2 Records of overhaul and rebuilding. 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. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. will bring you directly to the content. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (ii) Monocoque or semimonocoque wings or control surfaces. (i) Power output (static and idle r.p.m. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 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. (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. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (xiv) The repair or replacement of internal elements of blades. No. 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. (x) Wing main ribs and compression members. (2) Powerplant major alterations. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. ___, 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. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 43.9 Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411(a)(1), and 135.419 of this chapter). (vi) Installation of parts not approved for the propeller. (xxiii) The repair of portions of skin sheets by making additional seams. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. 43.15 Additional performance rules for inspections. 7572; 49 U.S.C. 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 [Amdt. [Amdt. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 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. Of the three maintenance records, the airframe (logbook) is the most permanent. (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. 27, 2001; Amdt. 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. The interrogations should be made at a nominal rate of 50 interrogations per second. 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. Choosing an item from (3) Propeller major repairs. 1, 1966; Amdt. (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. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. 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. 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. (vi) Barometric scale error. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. The official, published CFR, is updated annually and available below under (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. 23, 1964, as amended by Amdt. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 1993, 29 FR 5451, Apr. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (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). (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. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 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. 43.12 Maintenance records: Falsification, reproduction, or alteration. 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 tests in (e) through (j) apply only to Mode S transponders. 23, 1964, as amended by Amdt. 27, 2001; Amdt. (1) Airframe major alterations. (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. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 43-7, 32 FR 7587, May 24, 1967; Amdt. No. FAA-2015-1621, Amdt. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. 1993, 29 FR 5451, Apr. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. 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. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (2) Bolts - for improper torquing and lack of safetying. Search & Navigation (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. 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. (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. (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. (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. 43-39, 69 FR 44863, July 27, 2004]. 1993, 29 FR 5451, Apr. [Doc. 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. 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. the requirements of parts 91K, 121, 125, 133, 135, and 145. View the most recent official publication: These links go to the official, published CFR, which is updated annually. FAA STANDARDS FOR ELECTRONIC RECORDS. full text search results the hierarchy of the document. The term logbook originated with the ship's log a . (4) Permanent marking. 1993, 29 FR 5451, Apr. (d) Performance requirements. You didn't ask that though. The date the work was completed. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. The software release life cycle is the process of developing, testing, and distributing a software product. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . For the purposes of this section the following definitions apply. 14. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 6(c), Dept. 43-28, 52 FR 20028, June 16, 1987; Amdt. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 23, 1964, unless otherwise noted. 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