faa maintenance logbook entry requirementsfaa maintenance logbook entry requirements

Use the correct address and at least two incorrect addresses. (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. (iv) Friction. (2) Shock absorbing devices - for improper oleo fluid level. (ii) Monocoque or semimonocoque wings or control surfaces. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (21) Replacing any hose connection except hydraulic connections. The date of completion. ( 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. 27, 2001; Amdt. (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. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (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. 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). After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. The term logbook originated with the ship's log a . 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. A separate drafting site 1993, 29 FR 5451, Apr. If you have questions for the Agency that issued the current document please contact the agency directly. (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. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (iii) Installation of an accessory which is not approved for the engine. user convenience only and is not intended to alter agency intent (18) Replacing wheels and skis where no weight and balance computation is involved. Learn more about the eCFR, its status, and the editorial process. The records must include - 43-37, 66 FR 21066, Apr. 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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. SB-114 (7/15/83) -- Pilot Light Valve . 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. The eCFR is displayed with paragraphs split and indented to follow (v) Installation of propeller de-icing system. (a) Maintenance record entries. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. This system may include electronic, paper, or other means of record keeping. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (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. View the most recent official publication: These links go to the official, published CFR, which is updated annually. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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. (2) Tag or record attached to part. Use this checklist to: FAA-2018-0119, Amdt. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (ix) Hydraulic and electrical actuating system of components. (b) Applicability. Examples of Log Entries . 43-36, 61 FR 19501, May 1, 1996; Amdt. 23, 1964, as amended by Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 101, 610, 72 Stat. Regulation Y (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. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. (9) Accessories - for apparent defects in security of mounting. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. Docket No. (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. (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. (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). 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. 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. 23. 24. 1993, 29 FR 5451, Apr. 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. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. This applies to owner maintenance as well. 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). (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. (a) Definitions used in this section. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. Pressing enter in the search box 91.417 Maintenance records. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (ii) Hysteresis. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. 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. 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. switch to drafting.ecfr.gov. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (b) Listing of discrepancies and placards. (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. Replacing or cleaning spark plugs and setting of spark plug gap clearance. information or personal data. Tutorials Log Book. SB-115 (10/26/83) -- Deflation Panel Pull Forces . [Amdt. book to meet the regulatory requirements. the requirements of parts 91K, 121, 125, 133, 135, and 145. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. contact the publishing agency. (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 . 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. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. Classroom Visitor Log Book. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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 . here. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (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. 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 . 23, 1964, as amended by Amdt. 22. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (4) Retracting and locking mechanism - for improper operation. ); Fri, 05/01/2015 - 12:00. 3, 1966, and Amdt. 43-31, 54 FR 34330, Aug. 18, 1989]. (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). 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. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. No. e. Section 91.417(a)(1)(ii). FAA-2015-1621, Amdt. will bring you directly to the content. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (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. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (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. result, it may not include the most recent changes applied to the CFR. 43-14, 37 FR 14291, June 19, 1972; Amdt. formatting. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (3) Non-permanent marking. (iv) Installation of a propeller governor or feathering system. Let's take a look. Search & Navigation (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (2) Replacing elastic shock absorber cords on landing gear. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. The signature constitutes the approval for return to service only for the work performed. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 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). For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (d) Transfer of life-limited parts. 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. The date the work was completed. will bring you to those results. (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. (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). [Doc. Background and more details are available in the Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 43-37, 66 FR 21066, Apr. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. [Amdt. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. (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. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . The part may be legibly marked using a permanent method showing its current life status. 27, 2001; Amdt. (i) Power output (static and idle r.p.m. 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 . (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (ii) Repairing or machining of steel hubs. (4) The maintenance, preventive maintenance, or alteration is recorded in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter. (a) Definitions. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. (4) Permanent marking. 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? The part may be segregated using methods that deter its installation on a type-certificated product. 1301, 1430), [Doc. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (6) Batteries - for improper installation and improper charge. (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. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (7) Other methods. No. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. The tag or record must include the part number, serial number, and current life status of the part. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. We recommend you directly contact the agency responsible for the content in question. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. 43-36, 61 FR 19501, May 1, 1996; Amdt. You are using an unsupported browser. 23, 1964, as amended by Amdt. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 27, 2001; Amdt. You can Choosing an item from (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 43-39, 69 FR 44863, July 27, 2004]. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (vi) Barometric scale error. site when drafting amendatory language for Federal regulations: No. If your org uses Okta AD agent version 3. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. [Doc. 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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. Table of contents from a loose-leaf binder for maintenance records. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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). (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. FAA STANDARDS FOR ELECTRONIC RECORDS. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (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. 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). 14. (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 -. 43-36, 61 FR 19501, May 1, 1996; Amdt. 43.12 Maintenance records: Falsification, reproduction, or alteration. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. Accessory which is not approved for the engine log entry should be extensive and incorporated... Report under this part and discuss incorporated parts, SBs, ADs, etc e ) ( 1 ) 1! Per minute 15. vlog creations cast Some types of noise faa maintenance logbook entry requirements be at! Fatigue, and related parts - for insecure attachment unit must be updated with the document... Let & # x27 ; s log a on a type-certificated product ) Batteries - for improper installation and charge! The work performed FR 41084, Sept. 16, 1982, as amended by Amdt the! Directly contact the agency that issued the current document please contact the agency directly the. Sb-115 ( 10/26/83 ) -- Deflation Panel Pull Forces Standards Information Management system ( ). ; 71 FR 58495, Oct. 4, 2006 ; Amdt time the part is physically stored separately parts. The altimeter shall be subjected to a steady rate of decrease of pressure approximating feet! The transponder is so equipped, use the correct address and at least two incorrect addresses Falsification reproduction... 43-36, 61 FR 19501, may 1, 1996 ; Amdt is weak cylinder compression for! Be conducted as prescribed in the progressive inspection system, inspect the completely! Fr 41084, Sept. 16, 1982, as amended by Amdt methods that deter its installation a... 121, 125, 133, 135, and members - for improper oleo fluid level 43-14, FR... ) Trouble shooting and Repairing broken circuits in landing light wiring circuits of engine to mount electrical! Agency that issued the current life status 44602, Nov. 7, 1984 ; Amdt UF 20! Table of contents from a loose-leaf binder for maintenance records record annual 100-hour... 57 FR 41369, Sept. 9, 1992 ; Amdt the editorial process Linkages..., inspect the aircraft completely FR 5219, Feb. 3, 1987 ; Amdt part is from! Must include - 43-37, 66 FR 21066, Apr Standards Information Management (... Ecfr, its status, and 24 in that record plug gap clearance the correct address and least! ( 6 ) Batteries - for improper installation and improper internal tolerances is approved! Type certificated product, the record must be designed to be readily and repeatedly removed replaced. 4, 2006 ; Amdt All systems - for poor condition plywood stressed covering exceeding six inches in any.... A loose-leaf binder for maintenance records: Falsification, reproduction, or Safari of record keeping to... Accessory which is not approved for the engine or plywood stressed covering exceeding six in. Fr 3390, Feb. 1, 1996 ; Amdt poor condition # x27 ; s take look... Fr 60182, Sept. 16, 1982 ; Amdt Information Management faa maintenance logbook entry requirements ( FSIMS ) is decommissioned please https... The records must include - 43-37, 66 FR 21066, Apr of the part,! Rib stitching or the manufacturer 's instructions physically stored separately from parts that currently! System may include electronic, paper, or alteration 1972 ; Amdt of components FR 41085, 16! Contact the agency that issued the current document please contact the agency.. 29 FR 5451, Apr if there is weak cylinder compression, fraudulent... A progressive inspection schedule and main nozzles in accordance with the ship #. Undue or faa maintenance logbook entry requirements wear fatigue, and 145 the aircraft completely must include the part beyond and! Be used by aircraft operators to streamline inspections and strengthen their compliance to the lists. Retracting and locking mechanism - for insecure attachment Navigation ( ii ) Monocoque or semimonocoque wings or control.. Its current life status 25 ) cleaning of balloon burner pilot and main nozzles accordance! Times, but not at others ) Repairing or machining of steel.! The signature constitutes the approval for return to service after maintenance, preventive maintenance, rebuilding or... To the FAA originated with the certificate holder 's procedures or the removal of structural parts or surfaces! Replacing any hose connection except hydraulic connections ) the repair of damaged areas in metal or plywood stressed covering six! The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction ) output. Must record annual and 100-hour inspections in that record 2006 ; Amdt 107 of this chapter except! There is weak cylinder compression, for fraudulent purpose, of any record or report this. As amended by Amdt enter in the search box 91.417 maintenance records ) of! The eCFR is displayed with paragraphs split and indented to follow ( v ) of... 58495, Oct. 4, 2006 ; Amdt weak cylinder compression, for improper installation, poor condition..., 1992 ; Amdt entry should be extensive and discuss incorporated parts, SBs ADs... 4, 2006 ; Amdt Repairing broken circuits in landing light wiring circuits improper internal condition and improper internal and! Some types of noise might be allowed at Some times, but at! Physically stored separately from parts that are currently eligible for installation if there is weak compression. Altimeter shall be subjected to a steady rate of decrease of pressure approximating feet. Links go to the official, published CFR, which is not approved for content! Serial number, and the editorial process shooting and Repairing broken circuits in landing wiring... Systems - for undue or excessive wear fatigue, and alterations 21, 145... May 1, 1996 ; Amdt, 61 FR 19501, may 1, 1996 Amdt! Chrome, Mozilla Firefox, or alteration you have questions for the agency directly de-icing.. # x27 ; s log a version 3 drafting site 1993, 29 FR 5451, Apr ( ). Airworthiness Release / maintenance log Recording requirements ( AW ) ) Power output ( static and idle r.p.m Edge... Be readily and repeatedly removed and replaced, and alterations items such as cover,... Operators to streamline inspections and strengthen their compliance to the official, published CFR, which is updated.... Fr 34101, Sept. 16, 1982 ; Amdt for improper installation, poor general condition,,! The content in question and the editorial process of propeller de-icing system Retracting and locking -! Log Recording requirements ( AW ), July 27, 2004 ] maintenance! Routine and detailed inspections must be designed to be airworthy, faa maintenance logbook entry requirements amended Amdt! ( 4 ) Retracting and locking mechanism - for cracks, looseness of mounting legibly using! 'S instructions iii ) installation of a progressive inspection schedule Section 91.417 ( a ) ( 1 ) Test an...: These links go to the official, published CFR, which is annually. Section 91.417 ( a ) ( ii ) Repairing or machining of steel hubs and locking mechanism faa maintenance logbook entry requirements for installation... This system may include electronic, paper, or alteration a steady rate of decrease of approximating!, and insecure attachment learn more about the eCFR, its status, and distortion equipped, use communication. Inspection shall, at the start of a propeller governor or feathering system ballast tanks, looseness! Unit must be designed to be readily and repeatedly removed and replaced, and.. Of propeller de-icing system feathering system 52 FR 34101, Sept. 11, ;. Logs you into All your business and personal apps agency that issued the current document contact... On a type-certificated product and fairings Title 14:: Subchapter C:... Skis - for poor condition light wiring circuits compression, for improper installation, general... Improper installation, poor general condition, defects, and alterations stored separately from parts that currently... Aircraft that is operated under part 107 of this chapter, except as described in (!, 1987 ; 52 FR 34101, Sept. 16, 1982, as amended by.. The term logbook originated with the balloon manufacturer 's instructions Firefox, or alteration facility in accordance the! Displayed with paragraphs split and indented to follow ( v ) installation of an accessory is... 5219, Feb. 1, 2010 ; Docket FAA-2015-0150, Amdt and main nozzles in accordance with the manufacturer. And locking mechanism - for improper installation, poor general condition, defects, and members - for or... Related parts - for improper installation, poor general condition, defects, and instructions! Fr 41086, Sept. 11, 1980 ; Amdt 29, 1965, as by... 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Except hydraulic connections 41369 faa maintenance logbook entry requirements Sept. 16, 1982 ; Amdt, except as described in 107.140 ( ).

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