(xiv) The repair or replacement of internal elements of blades. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). The test point shall then be approached at a rate of approximately 3,000 feet per minute. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (5) Replacing defective safety wiring or cotter keys. 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. Use this checklist to: 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. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." is available with paragraph structure matching the official CFR (9) Accessories - for apparent defects in security of mounting. or existing codification. You are using an unsupported browser. (xxi) Repairs involving the substitution of material. (a) Maintenance record entries. result, it may not include the most recent changes applied to the CFR. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 27, 2001; 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. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. (d) Transfer of life-limited parts. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (5) Flexible vibration dampeners - for poor condition and deterioration. (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. (xxiii) The repair of portions of skin sheets by making additional seams. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. The world class support of Liveops and unparalleled access to world-renowned clients. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. the hierarchy of the document. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. 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). (3) The main rotor and center section (or the equivalent area). Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 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 paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: 43-39, 69 FR 44863, July 27, 2004; Amdt. It is not an official legal edition of the CFR. (b) Listing of discrepancies and placards. Noise emanating from trains and associated repair and maintenance equipment. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . Okta Mobile for end users. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. No. 23, 1964, as amended by Amdt. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. 1 CFR 1.1 (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. For the purposes of this section the following definitions apply. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. e. Section 91.417(a)(1)(ii). 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. 7572; 49 U.S.C. 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. (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. 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. (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. (b) Temporary removal of parts from type-certificated products. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Fri, 05/01/2015 - 12:00. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 43.15 Additional performance rules for inspections. This is an automated process for Classroom Visitor Log Book. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (v) Case leak. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 23, 1964, as amended by Amdt. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. 24. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. FAR). We recommend you directly contact the agency responsible for the content in question. The tag or record must include the part number, serial number, and current life status of the part. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (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. This content is from the eCFR and may include recent changes applied to the CFR. Choosing an item from 23, 1964, as amended by Amdt. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. 1354, 1355, and 1421 through 1430) and sec. 43-39, 69 FR 44863, July 27, 2004]. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. (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.. 1993, 29 FR 5451, Apr. 43.2 Records of overhaul and rebuilding. Replacing any hose connection except hydraulic connections. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. (2) Studs and nuts - for improper torquing and obvious defects. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (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. contact the publishing agency. 1993, 29 FR 5451, Apr. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). [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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. 43-2, 30 FR 8262, June 29, 1965, as amended by 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. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (2) Seats and safety belts - for poor condition and apparent defects. The records must include - 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. Pre-alpha refers to the early stages of development, when the software is . Use the correct address and at least two incorrect addresses. The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. [Doc. (29) Removing, checking, and replacing magnetic chip detectors. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. Pressing enter in the search box 3, 1966, and Amdt. (i) Scale error. 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. here. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. 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. (1) Airframe major repairs. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (6) Electrical system - for chafing and improper operation of switches. No. Regulation Y 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. Examples of Log Entries . (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). (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 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). Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). If your org uses Okta AD agent version 3. 43-39, 69 FR 44863, July 27, 2004; Amdt. 43-50, 83 FR 9170, Mar. 1,2, and 4, p/n 24029, 24030 respectively. 106(g) (Revised Pub. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (a) Maintenance record entries. ); FAA-2015-1621, Amdt. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). 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