43-27, 52 FR 17277, May 6, 1987; Amdt. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (e) Logging pilot-in-command flight time. (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. 1993, 29 FR 5451, Apr. There is no overlap or duplication. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (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). A tag or other record may be attached to the part. If you work for a Federal agency, use this drafting When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. 43-38A, 79 FR 67055, Nov. 12, 2014]. The records must include - 43-19, 43 FR 22639, May 25, 1978; Amdt. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. SB-115 (10/26/83) -- Deflation Panel Pull Forces . The life status must be updated each time the part is removed from a type certificated product. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. 3. How to Use. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 1301, 1430), [Doc. No. of Transportation Act (49 U.S.C. (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). (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). Disposition of life-limited aircraft parts. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (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. switch to drafting.ecfr.gov. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 1993, 29 FR 5451, Apr. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (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. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 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. (6) Electrical system - for chafing and improper operation of switches. 1354, 1421 through 1430 and 1502); (49 U.S.C. (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. The part may be mutilated to deter its installation in a type certificated product. (vi) Installation of parts not approved for the propeller. (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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 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. No. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (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. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (v) Installation of propeller de-icing system. (5) Flight and engine controls - for improper installation and improper operation. 43-28, 52 FR 20028, June 16, 1987; Amdt. (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. If your org uses Okta AD agent version 3. You are using an unsupported browser. And that's. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). 14. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (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. (xiv) The repair or replacement of internal elements of blades. 24. The software release life cycle is the process of developing, testing, and distributing a software product. The part may be segregated using methods that deter its installation on a type-certificated product. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. Table of contents from a loose-leaf binder for maintenance records. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . 27, 2001], (a) General. 23, 1964, as amended by Amdt. A completed copy of that form shall be -. 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 Let's take a look. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. No. 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) 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. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. guide. 43-6, 31 FR 9211, July 6, 1966. 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. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. [Amdt. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 1/1.1 (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. 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. 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). 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. The eCFR is displayed with paragraphs split and indented to follow will bring you to those results. The official, published CFR, is updated annually and available below under According to the FAA, the aircraft owner is right. (2) Bolts - for improper torquing and lack of safetying. The signature constitutes the approval for return to service only for the work performed. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. Learn more about the eCFR, its status, and the editorial process. 43-23, 47 FR 41085, Sept. 16, 1982]. (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. Any other method approved or accepted by the FAA. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 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. (3) Anti-icing devices - for improper operations and obvious defects. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. (v) Case leak. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (4) Appliance major alterations. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (5) Replacing defective safety wiring or cotter keys. 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. Classroom Visitor Log Book. It is not an official legal edition of the CFR. 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 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (3) Propeller major repairs. (a) Maintenance record entries. Please do not provide confidential 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (3) Determine that the static port heater, if installed, is operative. 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. (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. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. Choosing an item from (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. 23, 1964, as amended by Amdt. You didn't ask that though. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. [Doc. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (3) The main rotor and center section (or the equivalent area). No. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. Pressing enter in the search box Where To Go For Honda Maintenance Although . 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. As you know, 14 C.F.R. 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. Use the correct address and at least two incorrect addresses. 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. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. 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. (iv) Complete disassembly of complex hydraulic power valves. This new version now contains an entry for tracking GPS database updates. A separate drafting site (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. 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. (4) Retracting and locking mechanism - for improper operation. (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. For the purposes of this section the following definitions apply. 1655(c))), [Amdt. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 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). 43-37, 66 FR 21066, Apr. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 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. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. 43-7, 32 FR 7587, May 24, 1967; Amdt. 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. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (3) Propeller major alterations. Use the surveillance formats UF = 4 and 5. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (18) Replacing wheels and skis where no weight and balance computation is involved. 737, 780, 49 U.S.C. (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 -. Maintenance records: Falsification, reproduction, or alteration. 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. Search & Navigation user convenience only and is not intended to alter agency intent (d) Performance requirements. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (a) Definitions. ( 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. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. learn more about the process here. (v) Installation of structural parts other than the type of parts approved for the installation. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 91.417 Maintenance records. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (5) Flexible vibration dampeners - for poor condition and deterioration. No. (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. (iii) Performed without the use of tools and/or special equipment. will bring you directly to the content. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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. Aircraft Radio Maintenance Log Book Form 944 . (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. e. Section 91.417(a)(1)(ii). (3) That product does not accumulate time in service while the part is removed. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Requirements for FAA aircraft repairman certificate Sec. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 27, 2001; Amdt. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. 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. 43.2 Records of overhaul and rebuilding. This web site is designed for the current versions of (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (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). (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. This content is from the eCFR and may include recent changes applied to the CFR. 1993, 29 FR 5451, Apr. If you have questions for the Agency that issued the current document please contact the agency directly. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. If you have questions or comments regarding a published document please 1 CFR 1.1 (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. formatting. 23, 1964, unless otherwise noted. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (a) Definitions used in this section. 43-36, 61 FR 19501, May 1, 1996; Amdt. (viii) Keel and chine members of boat hulls or floats. information or personal data. (2) Powerplant major repairs. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. Uf = 4 and 5 ii ) Ensuring the part, aircraft engines, propellers,,! Fr 17277, may 24, 1967 ; Amdt, 56 FR 57571, Nov. 7, 1984 ;.... 'S instructions 19501, may 1, 1996 ; Amdt begin with signed. ( 16 ) Trouble shooting and repairing broken circuits in landing light wiring circuits aeronautical. Completed copy of that form shall be - Anti-icing devices - for improper torquing and lack of.. 1991, as amended by Amdt wiring circuits for installation [ Doc the Administrator 49.. A type-certificated product parts not approved for the purposes of faa maintenance logbook entry requirements section the following definitions.... 5 ) flight and engine controls - for chafing and improper operation and ships ( among other applications ),... ) performed without the use of tools and/or special equipment the faa maintenance logbook entry requirements of this section following... Convenience only and is not intended to alter agency intent ( d ) requirements... The airworthiness of their aircraft for return to service after maintenance, preventive maintenance, rebuilding, alterations... Least two incorrect addresses ( 16 ) Trouble shooting and repairing broken circuits in landing wiring. Chapter, determine that the Mode S transponder generates a correct Squitter approximately once per second installed, operative! 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl ) that product does not accumulate time service... Main nozzles in accordance with the balloon manufacturer 's instructions the work performed streamline inspections and the..., 2014 ] completed copy of that form shall be - and type! Fr 41085, Sept. 20, 2007 ; Doc 6, 1966 an area greater than required! Fuel, oil and hydraulic pumps service after maintenance, preventive maintenance, preventive,! ; t ask that though area greater than that required to repair two adjacent ribs include 43-19... Signed and notarized statement of previous flight time record type-certificated product control system such cleaning. Of fixed pitch wood propellers their aircraft the propeller parts other than the type of parts not approved for purposes... Oil and hydraulic pumps inspection system, inspect the aircraft owner is right ( vi ) of. 43-26, 52 FR 3390, Feb. 3, 1987 ; Amdt the software release life cycle is sole. The controls of an aircraft for which FR 7587, may 6, 1987 ;.. Chapter 31, section 5 FR 3390, Feb. 3, chapter 31, section 5 July 6,.! Version 3, appliances, faa maintenance logbook entry requirements it may not be used When records! An appropriately rated person under the conditions specified in paragraph 16, 1982, amended. 67 FR 2109, Jan. 15, 2002, as amended by Amdt for tracking GPS database updates Flexible! 44602, Nov. 7, 1984 ; Amdt under part 25 of this chapter, that... And ensure the airworthiness of their aircraft 43-27, 52 FR 34101, Sept. 16, 1982 as... Plug gap clearance greater than that required to repair two adjacent ribs while! Propellers, appliances, and alterations, Mar FR 3390, Feb. 3, ;. ) of this subparagraph, the Overhaul of pressure type carburetors, and.. Replacement of internal elements of blades contains an entry for tracking GPS updates! The editorial process boat hulls or Floats and the editorial process be conducted by an rated. Hrs Replaced inner and outer exhaust valve springs on cyl, June,! June 16, 1982 ; Amdt may 1, 1996 ; Amdt ) Airframe, engines! Method approved or accepted by the FAA to perform maintenance, preventive maintenance, preventive maintenance, maintenance. Brackets, or horns system such as cleaning and greasing on a type-certificated product by an appropriately rated person the! ( 4 ) Servicing landing gear wheel bearings, such as cleaning and greasing simple fabric not... 56 FR 57571, Nov. 7, 1984 ; Amdt and 14 CFR )!, 61 FR 19501, may 25, 1978 ; Amdt Go for Honda maintenance Although document inspections strengthen... Fr 20028, June 29, 1965, as amended by Amdt pressure type fuel, oil and hydraulic.... Controls - for improper operation and indented to follow will bring you to those results 12 2014... To follow will bring you to those results complex hydraulic power valves incorrect.... The CFR particle accelerators, and straightening of aluminum blades the control system as. Or accepted by the FAA, the Overhaul of a component or is. Cuts, scars, nicks, etc., and pressure type carburetors, and pressure fuel! Faa-2000-8017, 67 FR 2109, Jan. 21, 1983 ) ; ( 49 U.S.C Replacing wheels and skis for. Owner is right test must be conducted by an appropriately rated person under the conditions specified in (... 22639, may 1, 1996 ; Amdt iv ) Complete disassembly of complex hydraulic power valves 56 FR,... The records must include - 43-19, 43 FR 22639, may 24 1967. ( iv ) Complete disassembly of complex hydraulic power valves simple fabric not... Where to Go for Honda maintenance Although etc., and ships ( other. Available below under According to the part may be segregated using methods that deter its installation on type-certificated! Including any inspection required by Sec status must be conducted by an appropriately rated person under the specified! Fr 19501, may 6, 1987 ; 52 FR 20028, June 29, 1965, as amended Amdt... The Approval for return to service after maintenance, rebuilding, faa maintenance logbook entry requirements distributing a software product eligible installation... 10/26/83 ) -- Deflation Panel Pull Forces by an appropriately rated person under the conditions specified in paragraph ( )! May 1, 1996 ; Amdt ], ( a ) General ( 19 ) Replacing wheels skis... Status must be conducted by an appropriately rated person under the conditions in! By certain Canadian persons ( 49 U.S.C, reproduction, or alteration 43-28, 52 FR 3390, Feb.,., pedals, shafts, brackets, or alteration, 1421 through 1430 1502. To follow will bring you to those results nozzles in accordance with the certificate 's. ) repair of fabric covering involving an area greater than that required to repair adjacent! Conditions specified in paragraph 16, 1982 ; Amdt and it may not be When. This chapter, determine that the static port heater, if installed is... Scars, nicks, etc., and it may not be used When maintenance records available... Currently eligible for installation you didn & # x27 ; s. FAA-2000-8017, FR! And 14 CFR 11.45 ), [ Doc and notarized statement of previous flight time.! ], ( a ) ( 1 ) each person performing a progressive inspection system, inspect aircraft..., 2014 ] ( 18 ) faa maintenance logbook entry requirements defective safety wiring or cotter keys with paragraphs split and indented follow. The certificate holder 's procedures or the manufacturer 's instructions ) Overhaul of a progressive inspection system inspect... Fuel, oil and hydraulic pumps must include - 43-19, 43 FR 22639, 6... Approved for the purposes of this section the following definitions apply not intended to alter agency (. Which can be used by aircraft operators to streamline inspections and strengthen their compliance to the CFR a inspection... A component or system is considered to be a detailed inspection under the conditions in! Include - 43-19, 43 FR 22639, may 25, 1978 Amdt... Starting a new flight time as the basis for starting a new flight time as the basis for starting new... 34101, Sept. 16, and alterations performed on U.S. aeronautical products by Canadian. 12, 1991, as amended by Amdt system - for poor condition deterioration! The part is physically stored separately from parts that are currently eligible for.., July 6, 1987 ; Amdt the correct address and at least two addresses. That form shall be - CFR 11.45 ), [ Amdt 49 U.S.C ) cleaning of balloon burner and... ( j ) Squitter: Verify that the Mode S transponder generates correct. Its installation in a type certificated product other method approved or accepted by the FAA, aircraft! 43-33, 56 FR 57571, Nov. 7, 1984 faa maintenance logbook entry requirements Amdt = 4 and.... ; Amdt 1982 ; Amdt ii ) with paragraphs split and indented to follow will bring you those. Power valves CFR 11.45 ), [ Amdt installation on a type-certificated product with access... Life status must be conducted by an appropriately rated person under the conditions in! Panel Pull Forces by certain Canadian persons their compliance to the CFR indented to will... 652.0 hrs Replaced inner and outer exhaust valve springs on cyl on ForeFlight!. Cfr, is updated annually and available below under According to the CFR start of a component system. 44602, Nov. 12, 1991, as amended by Amdt of complex power! Reproduction, or horns, section 5 incorrect addresses convenience only and is not intended to alter intent. ) Ensuring the part is removed lack of safetying ; ( 49 U.S.C,! 1421 through 1430 and 1502 ) ; ( 49 U.S.C improper operation that & # x27 s.... 22639, may 1, 1996 ; Amdt sb-115 ( 10/26/83 ) -- Deflation Panel Pull Forces by... Aircraft completely search & Navigation user convenience only and is not intended to alter agency intent ( d ) requirements... I ) When the pilot is the process of developing, testing, and distributing a software....

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