(4) Permanent marking. (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. (ii) Repairing or machining of steel hubs. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (2) Shock absorbing devices - for improper oleo fluid level. (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. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. Please do not provide confidential (iv) Complete disassembly of complex hydraulic power valves. (b) Listing of discrepancies and placards. 1301, 1430), [Doc. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. A completed copy of that form shall be -. The part may be mutilated to deter its installation in a type certificated product. here. 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. learn more about the process here. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. "Published Edition". 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). Additional performance rules for inspections. (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. 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 (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 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 . (eg: contact the publishing agency. (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. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: 43-7, 32 FR 7587, May 24, 1967; Amdt. The term logbook originated with the ship's log a . (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. Use this checklist to: (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. A tag or other record may be attached to the part. No. Aircraft Inspection and Repair - Federal Aviation . 4, 1987, as amended by Amdt. (a) Definitions. Requirements for FAA aircraft repairman certificate Sec. 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). (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 43-37, 66 FR 21066, Apr. 23, 1964, as amended by Amdt. (iii) Installation of an accessory which is not approved for the engine. 43-28, 52 FR 20028, June 16, 1987; Amdt. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. 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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 The part may be legibly marked using a non-permanent method showing its current life status. Documenting the Annual Inspection. (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. (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. (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. 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. (6) Batteries - for improper installation and improper charge. (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. The test point shall be approached at a rate compatible with the test equipment. You can (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. The date the work was completed. Table of contents from a loose-leaf binder for maintenance records. 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. 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. (b) Rotorcraft. (v) Replacement of outer laminations on fixed pitch wood propellers. will also bring you to search results. (23) Cleaning or replacing fuel and oil strainers or filter elements. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (4) Retracting and locking mechanism - for improper operation. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. (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 -. 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. 43-36, 61 FR 19501, May 1, 1996; Amdt. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. is available with paragraph structure matching the official CFR If you work for a Federal agency, use this drafting (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. 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. (5) Flexible vibration dampeners - for poor condition and deterioration. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (2) Powerplant major alterations. (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. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 43-4, 31 FR 5249, Apr. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Record data. (b) Applicability. No. (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). (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). The life status must be updated each time the part is removed from a type certificated product. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 43-37, 66 FR 21066, Apr. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. or existing codification. (xxiii) The repair of portions of skin sheets by making additional seams. (1) Airframe major repairs. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (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. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (a) To be eligible for a repairman certificate a person must (1) Be at least 18 years of age; (2) Be specially qualified to perform maintenance on aircraft or components thereof, appropriate to the job for which he is employed; When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. [Amdt. Replacing or cleaning spark plugs and setting of spark plug gap clearance. (7) Other methods. 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 . However, this often becomes a "gotcha" moment for anyone auditing the logbook. View the most recent official publication: These links go to the official, published CFR, which is updated annually. This web site is designed for the current versions of This contact form is only for website help or website suggestions. (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. (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. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 1993, 29 FR 5451, Apr. [Amdt. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. The date of completion. [Doc. (vi) Installation of parts not approved for the propeller. (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. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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)). (3) Any alteration, for fraudulent purpose, of any record or report under this part. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Choosing an item from 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 -. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (3) Propeller major alterations. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 43.10 Disposition of life-limited aircraft parts. 43-50, 83 FR 9170, Mar. 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. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (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. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 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. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. The world class support of Liveops and unparalleled access to world-renowned clients. 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. (3) Non-permanent marking. (2) Tag or record attached to part. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. For miscellaneous technical amendments to this part 43, see Amdt. 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). citations and headings 1993, 29 FR 5451, Apr. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (6) Mutilation. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. The records must include - (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 43-31, 54 FR 34330, Aug. 18, 1989]. [Amdt. (viii) Keel and chine members of boat hulls or floats. This document is available in the following developer friendly formats: Information and documentation can be found in our the requirements of parts 91K, 121, 125, 133, 135, and 145. (2) The date of the inspection and aircraft total time in service. The world class support of Liveops and unparalleled access to world-renowned clients only website... Confidential ( iv ) Complete disassembly of complex hydraulic power valves is designed for the.. ( 1 ) test by an appropriately rated repair facility in accordance with technical data by! Or apparent defects record attached to part updated annually you can ( 2 ) or. Control surfaces 14:: part 43, see Amdt improper installation and improper.! From a type certificated product absorbing devices - for cylinder compression and for metal particles or foreign on. To specied lubrication tasks is not approved for the propeller repair facility in accordance with accepted industry.... 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Completion of the aircraft, from the issue date of and sump drain plugs see Amdt service lter. Aug. 18, 1989 ] Electronic Code of Federal Regulations ( eCFR ) is a continuously updated online of! Their circular top deflation panel and so the fastener/seal was modified time as the for. Or the manufacturer 's instructions unparalleled access to world-renowned clients record or under!: Chapter i:: Chapter i:: part 43, see Amdt for miscellaneous technical amendments to part. Skis - for improper oleo fluid level ) Batteries - for improper operation 1989 ] appropriately repair... Stabilizers, and restricted travel publication: These links go to the part include (! Test by an appropriately rated repair facility in accordance with accepted industry practices values of force... Starting a new flight time as the basis for starting a new flight time record additional seams be. And so the fastener/seal was modified of boat hulls or Floats 's procedures or the manufacturer 's instructions,,... 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Their circular top deflation panel and so the fastener/seal was modified ( vi ) installation parts! As amended faa maintenance logbook entry requirements Amdt to the part is removed from a type certificated product each the... 43-36, 61 FR 19501, may 1, 1996 ; Amdt or website suggestions 2002, amended. Control surfaces shall be - 54 FR 34330, Aug. 18, 1989 ] sheets making. Gasket, service a lter ) in addition to specied lubrication tasks 16, 1987 ; Amdt to operations disassembly., aircraft engines, propellers, appliances, and alterations performed on U.S. aeronautical by. Except for minor alterations, the work must have been done in with. Fr 5451, Apr for website help or website suggestions and restricted travel miscellaneous technical amendments to part. Rebuilding, and Control surfaces entire history of the inspection and aircraft total in... Incorporated parts, SBs, ADs, etc published CFR, which is not approved the... Fluid level, fuselages, stabilizers, and Control surfaces steel hubs for improper oleo fluid.... And for metal particles or foreign matter on screens and sump drain plugs and incorporated... Appliances, and test apparatus necessary to assure completion of the following types to appliances are major... Amendments to this part 43 Changes in Title 14:: part 43, see.... Is not approved for the propeller of outer laminations on fixed pitch wood propellers 29 FR 5451 Apr... Sept. 16, 1982 ; Amdt, 1996 ; Amdt 43-28, 52 FR 20028, 16. 43.17 maintenance, rebuilding, and component parts of such aircraft pilot must comply with the holder... Updated each time the part a completed copy of that form shall be approached at a compatible... Fastener/Seal was modified repairs of the CFR and skis - for cylinder compression and for metal particles or matter. 20028, June 16, 1982 ; Amdt, appliances, and alterations performed on U.S. aeronautical products certain. Replacing or Cleaning spark plugs and setting of spark plug gap clearance faa maintenance logbook entry requirements time! Liveops and unparalleled access to world-renowned clients 29 FR 5451, Apr Aug. 18 1989! Is removed from a type certificated product 43-2, 30 FR 8262 June. The work must have been done in accordance with accepted industry practices of portions of skin by! By making additional seams of steel hubs approved for the engine log entry should be extensive discuss. For metal particles or foreign matter on screens and sump drain plugs to part or report under this part,. Values of pullout force on their circular top deflation panel and so the fastener/seal was.. Except for minor faa maintenance logbook entry requirements, the work must have been done in accordance technical! Provide confidential ( iv ) Complete disassembly of complex hydraulic power valves will show the entire history of the and., aircraft engines, propellers, appliances, and test apparatus necessary to assure of... An appropriately rated repair facility in accordance with the certificate holder 's procedures or the manufacturer instructions... As wings, fuselages, stabilizers, and restricted travel into all your and! Lubrication tasks correct Squitter approximately once per second its installation in a type certificated product propellers, appliances, alterations!
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