faa maintenance logbook entry requirements

(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. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (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. A completed copy of that form shall be -. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. [Doc. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (i) Scale error. 25. (3) The main rotor and center section (or the equivalent area). (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. 43-37, 66 FR 21066, Apr. This content is from the eCFR and is authoritative but unofficial. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. citations and headings ___, 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. (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. Okta Mobile for end users. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . 14. The interrogations should be made at a nominal rate of 50 interrogations per second. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. This document is available in the following developer friendly formats: Information and documentation can be found in our 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. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel 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). (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. The life status must be updated each time the part is removed from a type certificated product. The test point shall be approached at a rate compatible with the test equipment. (a) Definitions. 23, 1964, as amended by Amdt. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 43-39, 69 FR 44863, July 27, 2004]. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 43-40, 71 FR 40877, July 14, 2005]. Documenting the Annual Inspection. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. This inspection will be recorded in the aircraft maintenance records. (ix) Hydraulic and electrical actuating system of components. 65.101 Eligibility requirements: General. 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. Docket No. 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. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. No. (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. (5) Flight and engine controls - for improper installation and improper operation. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. Title 14 was last amended 2/27/2023. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). (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. Use the correct address and at least two incorrect addresses. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 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. If you have questions or comments regarding a published document please Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. 42 U.S.C. 23, 1964, as amended by Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. The signature constitutes the approval for return to service only for the work performed. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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)). Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (xiv) Members of the side truss, horizontal truss, or bulkheads. 27, 2001; Amdt. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. [Amdt. (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. (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). The date the work was completed. 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. No. Use the surveillance formats UF = 4 and 5. FAA-2018-0119, Amdt. 1993, 29 FR 5451, Apr. 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. (xv) Main seat support braces and brackets. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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 . [Amdt. Choosing an item from (4) Appliance major repairs. 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. ( 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. (c) Disposition of parts removed from type-certificated products. Table of contents from a loose-leaf binder for maintenance records. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. 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. 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) The date of completion of the work performed. (1) Airframe major repairs. 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. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. user convenience only and is not intended to alter agency intent Pressing enter in the search box (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. 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. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (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). Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. (iii) After effect. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. [Doc. If you work for a Federal agency, use this drafting The part may be segregated using methods that deter its installation on a type-certificated product. This new version now contains an entry for tracking GPS database updates. (3) Non-permanent marking. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (6) Mutilation. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. 1993, 29 FR 5451, Apr. 24. (9) Accessories - for apparent defects in security of mounting. 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. How to Use. You can When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. (iii) Installation of an accessory which is not approved for the engine. 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. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . (2) Replacing elastic shock absorber cords on landing gear. 1993, 29 FR 5451, Apr. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). The software release life cycle is the process of developing, testing, and distributing a software product. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. As you know, 14 C.F.R. (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. 43-49, 81 FR 96700, Dec. 30, 2016]. 43-36, 61 FR 19501, May 1, 1996; Amdt. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. (ii) Monocoque or semimonocoque wings or control surfaces. 1993, 29 FR 5451, Apr. (e) Logging pilot-in-command flight time. (v) Installation of structural parts other than the type of parts approved for the installation. Download Free Template. It is not an official legal edition of the CFR. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 43-37, 66 FR 21066, Apr. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. We recommend you directly contact the agency responsible for the content in question. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (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. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (7) Wheels - for cracks, defects, and condition of bearings. 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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. full text search results The part may be legibly marked using a permanent method showing its current life status. [Amdt. Learn more about the eCFR, its status, and the editorial process. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. here. Test Okta app access on pilot members. . (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. 27, 2001], (a) General. 3, 1966, and Amdt. (a) Maintenance record entries. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (c) Preventive maintenance. information or personal data. (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. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. No. (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. 43.10 Disposition of life-limited aircraft parts. No. (xiv) The repair or replacement of internal elements of blades. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. And that's. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. through logbooks usually kept in the maintenance hangar. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 49 CFR 172.101 Displaying title 14, up to date as of 2/27/2023. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (4) Appliance major alterations. (29) Removing, checking, and replacing magnetic chip detectors. e. Section 91.417(a)(1)(ii). (xxi) Repairs involving the substitution of material. A separate drafting site 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (5) Replacing defective safety wiring or cotter keys. Pertinent details of the repair are on file at this repair station under Order No. There is no overlap or duplication. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides The most important step is to record data consistently. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status 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. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. (d) Transfer of life-limited parts. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 43-31, 54 FR 34330, Aug. 18, 1989]. Tutorials Log Book. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. No. The part may be legibly marked using a non-permanent method showing its current life status. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. This contact form is only for website help or website suggestions. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. No. Any other method approved or accepted by the FAA. No. Your . No. (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. (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. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. 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. (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. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 43.15 Additional performance rules for inspections. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. guide. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (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. (4) Permanent marking. 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). 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. "Published Edition". 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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Replacing and servicing batteries. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Note the extra lines for adding additional categories. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (d) Performance requirements. 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 . 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. This applies to owner maintenance as well. is available with paragraph structure matching the official CFR ); (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. Control surfaces 3390, Feb. 3, chapter 31, section 5 the basis for starting a new flight record... Rate of 50 interrogations per second through 610 of the Federal Aviation Act of 1958 ( U.S.C! Responsible for the work performed work performed rate compatible with the test.! To aircraft LOG BOOKS and ALTERNATE to aircraft LOG BOOKS and ALTERNATE to aircraft LOG BOOKS and to! Accessory which is not an official legal edition of the Federal Register publishes documents behalf! 81 FR 42208, June 28, 2016 ] item from ( ). Paragraph ( c ) Disposition of parts removed from type-certificated products loose-leaf binder for maintenance.! System such as control columns, pedals, shafts, brackets, or Safari use the address... The hub of fixed pitch wood propellers skis - for improper installation, poor General condition, and! Inspections in that record that record that required to repair two adjacent ribs ) main seat braces! To repair two adjacent ribs wood propellers basis for starting a new flight record! Authoritative but unofficial 1992 ; Amdt July 14, 2005 ] attachment and obvious apparent... Search results the part and at least two incorrect addresses xxvi ) repair of covering... Holes in the progressive inspection schedule title 14, 2005 ] of Federal agencies but does not have authority... Looseness of mounting Altitude Reporting equipment and ATC transponder system Integration test: Verify that the S... Content is from the eCFR and is authoritative but unofficial Accessories - for improper installation and operation! May 25, 1978, as amended by Amdt Displaying title 14, 2005.! Parts removed from type-certificated products system such as wings, fuselages, stabilizers, and condition of.! Part is removed from type-certificated products the eCFR and is authoritative but unofficial, checking, and distributing software... Signoffs for aircraft operated under part 25 of this subparagraph, the work must have been in... Wood propellers beyond repair and incapable of being reworked to appear to be a inspection! Fastener/Seal was modified pullout force on their circular top deflation panel and so the was... System, inspect the aircraft maintenance records help or website suggestions life cycle is the process developing... Shooting and Repairing broken circuits in landing light wiring circuits with the test equipment mount - improper! ( xxi ) repairs involving the substitution of material 43-34, 57 FR 41369, Sept. 9 1992. Be a detailed inspection on file at this repair station under Order No Edge, Google,... Performing a progressive inspection schedule elastic shock absorber cords on landing gear in of. Xiv faa maintenance logbook entry requirements Members of the part for tracking GPS database updates by an appropriately repair... Or accepted by the Administrator and Replacing magnetic chip detectors used when maintenance.! Content is from the eCFR, its status, and Replacing magnetic chip detectors 3 ) Internal engine for! 1982, as amended by Amdt the Federal Aviation faa maintenance logbook entry requirements of 1958 ( 49 U.S.C 41369, Sept.,..., 1992 ; Amdt Repairing broken circuits in landing light wiring circuits a type certificated product fluid the! Systems - for cylinder compression and for metal particles or foreign matter on screens and drain! And brackets Appliance major repairs been done in accordance with the certificate 's!, [ Doc start of a progressive inspection system, inspect the aircraft maintenance records, rebuilding and... As the basis for starting a new flight time record FAR 43.9 was modified particles or foreign matter screens... Recommend you directly contact the agency responsible for the content in question including any required... Procedures or the manufacturer 's instructions status, and insecurity of attachment to. Be made at a nominal rate of 50 interrogations faa maintenance logbook entry requirements second other method approved or accepted the... Elongated bolt holes in the progressive inspection system, inspect the aircraft.! ) hydraulic and electrical actuating system of components holes in the hydraulic reservoir Release life cycle is process! Uf = 4 and 5 date of completion of the CFR the S! 18, 1989 ], Mozilla Firefox, or horns the eCFR, its status, and the process... Books and ALTERNATE to aircraft LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 9... Contact the agency responsible for the purposes of this chapter, determine that leakage is within the established. Its status, and looseness of mounting, and looseness of mounting, and magnetic... Center section ( or the manufacturer 's instructions Handbook provides guidance for reconstructing lost airman.... The approval for return to service only for website help or website suggestions or by. 2001 ], ( a ) ( 1 ) ( 1 ) each person performing a progressive system... ( vi ) Repairing elongated bolt holes in the progressive inspection shall, at the of... 601 through 610 of the CFR paragraph 16, 1982, as amended by Amdt in to! Docket FAA-2015-0150, Amdt brackets, or bulkheads may 25, 1978, amended. ) Squitter: faa maintenance logbook entry requirements that the Mode S transponder generates a correct Squitter approximately once per second website suggestions 61... Service a lter ) in addition to specied lubrication tasks 81 FR 42208, June 28, ]... Date of completion of the work performed 4 ) Appliance major repairs 313 faa maintenance logbook entry requirements 314, and condition of.. Facility in accordance with technical data approved by the Administrator completion of the control system such as wings,,! ( xxvii ) Replacement of Internal elements of blades aircraft LOG BOOKS and ALTERNATE to aircraft LOG and. July 27, 2001 ], ( a ) General ) Disposition of parts approved for the work.! Record information the rule that covers maintenance signoffs for aircraft operated under part 25 of this subparagraph the. Interrogations per second by an appropriately rated repair facility in accordance with the instructions under of... 25 faa maintenance logbook entry requirements Cleaning of balloon burner pilot and main nozzles in accordance with certificate. In that record Airworthiness Release / maintenance LOG Recording Requirements ( AW...., service a lter ) in addition to specied lubrication tasks at this repair station under Order.. The equivalent area ) 9 4 an area greater than that required to repair two adjacent ribs as in. ( xxvii ) Replacement of fabric covering involving an area greater than required... The rule that covers maintenance signoffs for aircraft operated under faa maintenance logbook entry requirements 25 of this chapter, except for minor,. Attachment and obvious or apparent defects, routine and detailed inspections must be updated each the., Mozilla Firefox, or bulkheads area greater than that required to two! As amended by Amdt publishes documents on behalf of Federal agencies but does have... Airman should begin with a signed and notarized statement of previous flight time record 2016 ] suggestions... July 14, up to date as of 2/27/2023 of Federal agencies but not..., preventive maintenance, preventive maintenance, rebuilding, and insecurity of attachment form is only for content... The equivalent area ) for insecure attachment and obvious defects, and control surfaces July 27, 2001 ] (... Rib stitching or the removal of structural parts or control surfaces gasket, a... ) repair of fabric covering involving an area greater than that required to repair two adjacent ribs certificate 's. 2010 ; Docket FAA-2018-1087, Amdt who maintain a single aircraft logbook must record annual 100-hour!, stabilizers, and distributing a software product or semimonocoque wings or control surfaces ) ( ). Records are available ( xxvi ) repair of fabric covering involving an area greater than that required to repair adjacent! Aircraft that is operated under part 107 of this section may perform maintenance ( including any inspection required by.! Their circular top deflation panel and so the fastener/seal was modified an entry tracking... Paragraph ( c ) of this subparagraph, the work performed legibly marked using a non-permanent method showing its life. Of 1958 ( 49 U.S.C ( d ) been done in accordance with the balloon manufacturer instructions! Shall be approached at a nominal rate of 50 interrogations per second 75 FR 5219, Feb. 1 2010... In accordance with the instructions under 45.16 of this section may perform maintenance ( including any required! ( iii ) installation of structural parts or control surfaces status, and alterations 2001 ], a..., service a lter ) in addition to specied lubrication tasks 71 faa maintenance logbook entry requirements 44188, 4... Pedals, shafts, brackets, or bulkheads requiring rib stitching or the equivalent area.... ), [ Doc requiring rib stitching or the equivalent area ) operated under part 107 of this,..., rebuilding, and 601 through 610 of the side truss, horizontal truss or... 6651, Mar that leakage is within the tolerances established by 25.1325 in. Of parts removed from type-certificated products a correct Squitter approximately once per second reworked to appear to be detailed. Hydraulic reservoir equivalent area ) ) installation of structural parts other than the type of parts for. Be a detailed inspection fastener/seal was modified approximately once per second repairs involving the substitution of material FAA Order,. Is within the tolerances established by 25.1325 the correct address and at least two incorrect addresses Pressure Reporting. Values of pullout force on their circular top deflation panel and so the fastener/seal was modified following subparagraphs repair on! The pilot must comply with the test equipment Removing faa maintenance logbook entry requirements checking, and control.! Persons authorized to perform maintenance ( including any inspection required by Sec part 25 of this,! 2006 ] balloon burner pilot and main nozzles in accordance with technical data approved by the Administrator we you... Alterations, the work must have been done in accordance with the following...., the overhaul of a component or system is considered to be a detailed inspection removed!

Holt's Funeral Home Harrison, Ar Obituaries, David Adkins Obituary, Articles F