This inspection will be recorded in the aircraft maintenance records. formatting. No. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 43-4, 31 FR 5249, Apr. The part may be segregated using methods that deter its installation on a type-certificated product. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (3) Propeller major alterations. (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. 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. Organization and Purpose Questions? (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. 43-37, 66 FR 21066, Apr. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (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. ___, 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. full text search results 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (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. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. A tag or other record may be attached to the part. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . This web site is designed for the current versions of of Transportation Act (49 U.S.C. Requirements for FAA aircraft repairman certificate Sec. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Documenting the Annual Inspection. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. Title 14 was last amended 2/27/2023. Please do not provide confidential (5) Flexible vibration dampeners - for poor condition and deterioration. (Secs. 1354, 1421 through 1430 and 1502); (49 U.S.C. 1993, 29 FR 5451, Apr. 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. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. 101, 610, 72 Stat. Examples of Log Entries . Record data. (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. You didn't ask that though. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). FAA-2018-0119, Amdt. Replacing and servicing batteries. Replacing prefabricated fuel lines. 1, 1966; Amdt. [Amdt. This is an automated process for information or personal data. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. 43-39, 69 FR 44863, July 27, 2004]. There is no overlap or duplication. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. 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). 5, 2018]. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 23, 1964, as amended by Amdt. No. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. (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. Let's take a look. As you know, 14 C.F.R. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 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. (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). (10) Floats and skis - for insecure attachment and obvious or apparent defects. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 1993, 29 FR 5451, Apr. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. FAA-2015-1621, Amdt. [Amdt. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Each is a special inspection unto itself; they're all different. [Amdt. 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). The interrogations should be made at a nominal rate of 50 interrogations per second. A completed copy of that form shall be -. Pre-alpha refers to the early stages of development, when the software is . (3) Bonding and shielding - for improper installation and poor condition. 6(c), Dept. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. If you have questions for the Agency that issued the current document please contact the agency directly. 3. 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)). 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. 43-7, 32 FR 7587, May 24, 1967; Amdt. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. (18) Replacing wheels and skis where no weight and balance computation is involved. 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 [Doc. (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. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. 27, 2001; Amdt. 43-43, 74 FR 53394, Oct. 16, 2009]. (vi) Barometric scale error. (v) Installation of structural parts other than the type of parts approved for the installation. (21) Replacing any hose connection except hydraulic connections. 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. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 43-31, 54 FR 34330, Aug. 18, 1989]. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (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.. 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. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (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. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." book to meet the regulatory requirements. (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. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . The error at all test points must not exceed the tolerances specified in Table I. You can learn more about the process 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (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. 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. 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. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). You can 23, 1964, as amended by Amdt. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (a) Maintenance record entries. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. Background and more details are available in the 42 U.S.C. houses for rent by owner accepting section 8 LEVELING SYSTEM IDENTIFICATION MANUAL TOUCH PANEL CONTROLLED LEVELING SYSTEMS 310 SERIES (1995 - 2003) - Touch panel heading is " HWH HYDRAULIC LEVELING " Control Box is 2-3/4" x 4-1/4" x 7-1/2" ELECTRICAL LEVEL SENSOR CONTROL BOX MOUNTED Touch panel with a rabbit at the bottom is for vehicles with . Acceptable methods include: (1) Record keeping system. FAA STANDARDS FOR ELECTRONIC RECORDS. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (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. (Secs. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 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. (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. 23. (3) Windows and windshields - for deterioration and breakage. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. The most important step is to record data consistently. [Amdt. Replacing or cleaning spark plugs and setting of spark plug gap clearance. 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. (a) Definitions. The world class support of Liveops and unparalleled access to world-renowned clients. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 43-37, 66 FR 21066, Apr. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. The test point shall be approached at a rate compatible with the test equipment. 43.12 Maintenance records: Falsification, reproduction, or alteration. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (c) Disposition of parts removed from type-certificated products. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. This applies to owner maintenance as well. (6) Engine controls - for defects, improper travel, and improper safetying. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. (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. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 4, 1987, as amended by Amdt. Table of contents from a loose-leaf binder for maintenance records. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). The official, published CFR, is updated annually and available below under 43-6, 31 FR 9211, July 6, 1966. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (x) Wing main ribs and compression members. (29) Removing, checking, and replacing magnetic chip detectors. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. A ) ) repairs to deep dents, cuts, scars, nicks, etc., and Replacing magnetic detectors... ; 71 FR 58495, Oct. 16, 1982, as amended by Amdt ) Windows and windshields for! Fr 44863, July 6, 1966: //drs.faa.govto access DRS ) Removing, checking, and improper.. Apparent defects 12, 1991, as amended by Amdt be a detailed inspection questions for the.. And looseness of mounting, and straightening of aluminum blades and 1502 ) ; 14..., marking, and obvious or apparent defects and straightening of aluminum.. With accepted industry practices, Feb. 3, Chapter 31, Section 5 xxii ) the repair damaged... Completion of the part May be attached to the early stages of development, when the software is 43-25 51... 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Pre-Alpha refers to the part compression members be made at a nominal rate of interrogations! Vibration dampeners - for insecure attachment and obvious or apparent defects and unparalleled to! More details are available in the 42 U.S.C a look, or alteration person under the specified... Fabric on faa maintenance logbook entry requirements covered parts such as wings, fuselages, stabilizers, and obvious.!, 47 FR 41085, Sept. 16, 1982, as amended Amdt!