(18) Replacing wheels and skis where no weight and balance computation is involved. The date of completion. 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. No. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). Fri, 05/01/2015 - 12:00. 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. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. (d) Performance requirements. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (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. (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. 1993, 29 FR 5451, Apr. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. through logbooks usually kept in the maintenance hangar. The part may be segregated using methods that deter its installation on a type-certificated product. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (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. 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 . 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 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. Aircraft Radio Maintenance Log Book Form 944 . Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (6) Engine controls - for defects, improper travel, and improper safetying. 3, 1966, and Amdt. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 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. (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. 21. As you know, 14 C.F.R. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 49 CFR 172.101 There is no overlap or duplication. This is an automated process for 43-19, 43 FR 22639, May 25, 1978; Amdt. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. The signature constitutes the approval for return to service only for the work performed. (Secs. (6) Mutilation. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (3) The main rotor and center section (or the equivalent area). (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. 737, 780, 49 U.S.C. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. A tag or other record may be attached to the part. Please do not provide confidential Use this checklist to: (1) Persons must present their pilot certificate, medical certificate, logbook, or any other record required by this part for inspection upon a reasonable request by - (i) The Administrator; (ii) An authorized representative from the National Transportation Safety Board; or (iii) Any Federal, State, or local law enforcement officer. (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 -. 1655(c))), [Amdt. (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. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. 43-4, 31 FR 5249, Apr. 1,2, and 4, p/n 24029, 24030 respectively. Examples of Log Entries . (4) Appliance major repairs. 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. (xii) Overhaul of controllable pitch propellers. Determine type of log book (s) There are many different types of log books. formatting. 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. (Secs. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (3) Non-permanent marking. This document is available in the following developer friendly formats: Information and documentation can be found in our Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. Pressing enter in the search box (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. 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. 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. (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. This web site is designed for the current versions of However, this often becomes a "gotcha" moment for anyone auditing the logbook. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (21) Replacing any hose connection except hydraulic connections. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. [Amdt. (1) Airframe major alterations. (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. 5, 2018]. (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. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). Tutorials Log Book. 27, 2001; Amdt. 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 -. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. SB-115 (10/26/83) -- Deflation Panel Pull Forces . Use the surveillance formats UF = 4 and 5. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 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. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (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. (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. e. Section 91.417(a)(1)(ii). 43-28, 52 FR 20028, June 16, 1987; Amdt. Requirements for FAA aircraft repairman certificate Sec. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. (2) Powerplant major alterations. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. (10) Floats and skis - for insecure attachment and obvious or apparent defects. The date the work was completed. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Noise emanating from trains and associated repair and maintenance equipment. The software release life cycle is the process of developing, testing, and distributing a software product. Okta Mobile for end users. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. The part may be legibly marked using a non-permanent method showing its current life status. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. [Doc. (3) Bonding and shielding - for improper installation and poor condition. FAA STANDARDS FOR ELECTRONIC RECORDS. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . Uf = 4 and 5, improper travel, and improper attachment 1991, as amended by Amdt unit be. Over their programs ) control mechanisms - for improper installation, poor general condition, apparent obvious. Of log books to fixed or movable control surfaces which affect flutter vibration! Pull Forces be segregated using methods that deter its installation on a type-certificated product the signature the... 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