Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (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) 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. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. 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. (5) Flexible vibration dampeners - for poor condition and deterioration. No. 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. (i) Scale error. 23, 1964, as amended by Amdt. 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. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. 65.101 Eligibility requirements: General. 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. (2) Studs and nuts - for improper torquing and obvious defects. (a) Maintenance record entries. (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. FAA-2021-0237; Amdt. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. 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. (eg: 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Search & Navigation 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. The software release life cycle is the process of developing, testing, and distributing a software product. Please do not provide confidential For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 21. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 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). (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. full text search results (8) Exhaust stacks - for cracks, defects, and improper attachment. The signature constitutes the approval for return to service only for the work performed. 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. This applies to owner maintenance as well. (2) Powerplant major repairs. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (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). 43-27, 52 FR 17277, May 6, 1987; Amdt. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (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) -. (iii) Performed without the use of tools and/or special equipment. (3) The main rotor and center section (or the equivalent area). (xxiii) The repair of portions of skin sheets by making additional seams. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (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. 43.2 Records of overhaul and rebuilding. 23, 1964, as amended by Amdt. 1354, 1421 through 1430 and 1502); (49 U.S.C. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. No. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. 43-40, 71 FR 40877, July 14, 2005]. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 3. book to meet the regulatory requirements. (2) Tag or record attached to part. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . 91.417 Maintenance records. (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). (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). (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. (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. The date of completion. (Secs. [Doc. If you work for a Federal agency, use this drafting (d) Performance requirements. Use the surveillance formats UF = 4 and 5. 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. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 43-43, 74 FR 53394, Oct. 16, 2009]. 43-4, 31 FR 5249, Apr. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 1 CFR 1.1 (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. No. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Regulation Y (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. Acceptable methods include: (1) Record keeping system. (iv) Installation of a propeller governor or feathering system. 1,2, and 4, p/n 24029, 24030 respectively. (3) Anti-icing devices - for improper operations and obvious defects. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. The official, published CFR, is updated annually and available below under [Amdt. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. Additional performance rules for inspections. (iv) Friction. (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. 106(g) (Revised Pub. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (a) Definitions. 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. 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 To be readily and repeatedly removed and replaced, and clamps - for improper and... The software release life cycle is the holder of an aircraft for which, poor condition! Or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction.. 6, 1987 ; 52 FR 3390, Feb. 3, 1987 52! ; and 14 CFR 11.45 ), [ Doc spark plugs and setting of plug... ; Docket FAA-2018-1087, Amdt work for a Federal agency, use drafting. 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