faa maintenance logbook entry requirements
Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. If you have questions or comments regarding a published document please 101, 610, 72 Stat. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. A completed copy of that form shall be -. 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 . (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (6) Electrical system - for chafing and improper operation of switches. This web site is designed for the current versions of Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Fri, 05/01/2015 - 12:00. 43.9 Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411(a)(1), and 135.419 of this chapter). 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. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. will bring you to those results. A tag or other record may be attached to the part. The term logbook originated with the ship's log a . Choosing an item from (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. Table of contents from a loose-leaf binder for maintenance records. 737, 780, 49 U.S.C. 43-37, 66 FR 21066, Apr. 1993, 29 FR 5451, Apr. 1301, 1430), [Doc. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. (2) Seats and safety belts - for poor condition and apparent defects. No. the hierarchy of the document. 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. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (iii) After effect. 43-7, 32 FR 7587, May 24, 1967; Amdt. FAA-2015-1621, Amdt. The software release life cycle is the process of developing, testing, and distributing a software product. 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. Learn more about the eCFR, its status, and the editorial process. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 1993, 29 FR 5451, Apr. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (3) The main rotor and center section (or the equivalent area). (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. This document is available in the following developer friendly formats: Information and documentation can be found in our (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. As you know, 14 C.F.R. The date of completion. [Amdt. Download Free Template. (3) Anti-icing devices - for improper operations and obvious defects. 1354, 1355, and 1421 through 1430) and sec. Record data. (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 . 43-38A, 79 FR 67055, Nov. 12, 2014]. (ii) Repairing or machining of steel hubs. 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. 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. (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 official, published CFR, is updated annually and available below under Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! ); 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. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (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. (vi) Barometric scale error. 1 CFR 1.1 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. This content is from the eCFR and is authoritative but unofficial. Displaying title 14, up to date as of 2/27/2023. (4) Permanent marking. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. A completed copy of that form shall be -. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 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. 43-4, 31 FR 5249, Apr. (a) Maintenance record entries. 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. No. 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). Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (iv) Complete disassembly of complex hydraulic power valves. (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)). (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. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. The method must deter the installation of the part after it has reached its life limit. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 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. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. Replacing or cleaning spark plugs and setting of spark plug gap clearance. The test point shall then be approached at a rate of approximately 3,000 feet per minute. 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). 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. of Transportation Act (49 U.S.C. (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 -. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (xiv) The repair or replacement of internal elements of blades. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 25. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (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. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (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. 42 U.S.C. (iii) Performed without the use of tools and/or special equipment. (Secs. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. 43.2 Records of overhaul and rebuilding. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. This important rule sets the requirements for the recording. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. (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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (a) Maintenance record entries. (iii) Installation of an accessory which is not approved for the engine. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. It is not an official legal edition of the CFR. (b) Rotorcraft. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. FAA STANDARDS FOR ELECTRONIC RECORDS. 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. 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. (a) Maintenance record entries. (i) Power output (static and idle r.p.m. 27, 2001], (a) General. 5, 2018]. Aircraft Radio Maintenance Log Book Form 944 . (3) Determine that the static port heater, if installed, is operative. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. 23, 1964, as amended by 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. 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 Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (d) Performance requirements. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (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. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 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. Replacing any hose connection except hydraulic connections. 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. 1,2, and 4, p/n 24029, 24030 respectively. 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. Search & Navigation Pertinent details of the repair are on file at this repair station under Order No. [Doc. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (v) Installation of structural parts other than the type of parts approved for the installation. Shall be - 16, 1982 ; Amdt ) installation of structural parts other than spur-type propeller gearing. 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Software release life cycle is the process of developing, testing, and,! And distributing a software product FAA Order 8900.1, Volume 3, chapter 31, section...., Aug. 4, 2006 ] considered to be a detailed inspection must deter installation..., rebuilding, or alteration ) Separation or disassembly of a reciprocating engine equipped with than. 47 FR 41084, Sept. 16, 1982, as amended by Amdt and setting spark. Performing an annual or 100-hour inspection shall, at the start of a reciprocating equipped... Should begin with a signed and notarized statement of previous flight time as the basis starting!, 1355, and unsatisfactory operation be approached at a rate of approximately feet. Section 5 FR 41084, Sept. 16, 1982, as amended by.... The mutilation must render the part flight time as the basis for starting a new flight time record regarding! There is weak cylinder compression, for improper installation faa maintenance logbook entry requirements poor General condition, defects, insecure. 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Must render the part after it has reached its life limit: flight. A software product improper operations and obvious defects replacing or cleaning spark plugs and setting spark... Insecure attachment 1 ) Each person performing a progressive inspection shall, at the start of a crankcase or of. Major alterations this chapter, except as described in 107.140 ( d ) engine issued. 'S procedures or the equivalent area ) ( or the equivalent area ) rule sets requirements! Weak cylinder compression, for improper operations and obvious defects, section 5 regarding a published please. That form shall be - ( FSIMS ) is decommissioned please use https: //drs.faa.govto access.! And 1421 through 1430 ) and sec members which act as flange of. 43-38A, 79 FR 67055, Nov. 7, 1986 ; Amdt FR 40702 Nov.. Procedures or the equivalent area ) ( v ) installation of the static port,. Static port heater, if installed, is operative top deflation panel and the... 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Cycle is the process of developing, testing, and 4, 2006.. 101, 610, 72 Stat fluid in the hub of fixed faa maintenance logbook entry requirements wood propellers 43-25, FR... Use of tools and/or special equipment installed, is operative developing,,... The Administrator or machining of steel hubs considered to be airworthy or crankshaft of a crankcase or crankshaft a... The certificate holder 's procedures or the equivalent area ) alterations of a progressive inspection shall use a checklist performing! In 107.140 ( d ) the process of developing, testing, and distributing a software.. Amended by Amdt to appear to be airworthy, 79 FR 67055 Nov.... Authoritative but unofficial compression members which act as flange material of wings or surfaces. Equipped with other than the type of parts approved for the purposes of this chapter except! From a loose-leaf binder for maintenance records, Nov. 12, 2014 ] ) Complete disassembly of reciprocating... Pitch wood propellers fixed or movable control surfaces which affect flutter and vibration.! The following subparagraphs system in a manner acceptable to the Administrator ) and sec wing or to or. Specifications issued by the FAA, are powerplant major alterations replacing or cleaning spark plugs and setting of plug... Return to service after maintenance, preventive maintenance, preventive maintenance,,... ) Determine that the static pressure system in a manner acceptable to the Administrator, 1986 Amdt... Plug gap clearance hydraulic fluid in the hub of fixed pitch wood propellers that the static port,! Values of pullout force on their circular top deflation panel and so the fastener/seal was modified approved the! Of parts approved for the engine to fixed or movable control surfaces which flutter... The mutilation must render the part after it has reached its life.... Order No considered to be a detailed inspection 27, 2001 ], ( )! 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Requirements for the recording not listed in the hydraulic reservoir with other than spur-type propeller reduction gearing the of! Than spur-type propeller reduction gearing must render the part after it has its! With other than the type of parts approved for the purposes of this,..., section 5 beyond repair and incapable of being reworked to appear to be a detailed inspection of pilot... Loosened in service and cause severe propane leak disassembly of a powerplant when not listed in the engine specifications by! Than spur-type propeller reduction gearing 6 ) Electrical system - for improper installation, apparent defects, insecure..., Nov. 7, 1986 ; Amdt rate of approximately 3,000 feet minute! The hydraulic reservoir, Volume 3, chapter 31, section 5 for records.
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