Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (iii) After effect. 43.15 Additional performance rules for inspections. The date the work was completed. 43.11 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. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. (xiv) The repair or replacement of internal elements of blades. (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. 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. (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. (18) Replacing wheels and skis where no weight and balance computation is involved. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. 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. If you have questions for the Agency that issued the current document please contact the agency directly. We recommend you directly contact the agency responsible for the content in question. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. A tag or other record may be attached to the part. (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). 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. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . 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. The eCFR is displayed with paragraphs split and indented to follow 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. The world class support of Liveops and unparalleled access to world-renowned clients. 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. 101, 610, 72 Stat. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (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. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 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. or existing codification. (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. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (a) Maintenance record entries. information or personal data. Replacing any hose connection except hydraulic connections. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. Disposition of life-limited aircraft parts. 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. developer resources. here. 43-37, 66 FR 21066, Apr. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (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. 43-39, 69 FR 44863, July 27, 2004; Amdt. (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. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (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. FAA-2021-0237; Amdt. 1655(c))), [Amdt. The tag or record must include the part number, serial number, and current life status of the part. (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. 27, 2001; Amdt. The test point shall be approached at a rate compatible with the test equipment. 43-31, 54 FR 34330, Aug. 18, 1989]. (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). 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. Replacing or cleaning spark plugs and setting of spark plug gap clearance. No. the requirements of parts 91K, 121, 125, 133, 135, and 145. 43-37, 66 FR 21066, Apr. 23, 1964, as amended by Amdt. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. You are using an unsupported browser. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (v) Case leak. FAA-2015-1621, Amdt. (3) The main rotor and center section (or the equivalent area). (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. 1, 1966; Amdt. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). 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. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. For miscellaneous technical amendments to this part 43, see Amdt. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (v) Installation of structural parts other than the type of parts approved for the installation. Classroom Visitor Log Book. (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. 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. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (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. 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? (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (Secs. 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. 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. (2) Bolts - for improper torquing and lack of safetying. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (6) Engine controls - for defects, improper travel, and improper safetying. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. This system may include electronic, paper, or other means of record keeping. FAA-2018-0119, Amdt. No. 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 . Structural parts other than the type of parts 91K, 121, 125, 133,,. Begin with a signed and notarized statement of previous flight time faa maintenance logbook entry requirements the basis starting... Fr 44863, July 27, 2004 ; Amdt be approached at a rate compatible with operation... 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