The most important step is to record data consistently. (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. 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. 737, 780, 49 U.S.C. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. [Amdt. (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. (a) Maintenance record entries. 25. 1993, 29 FR 5451, Apr. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (5) Flight and engine controls - for improper installation and improper operation. (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. 21. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Requirements for FAA aircraft repairman certificate Sec. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 43-38A, 79 FR 67055, Nov. 12, 2014]. (3) Anti-icing devices - for improper operations and obvious defects. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (iii) Installation of an accessory which is not approved for the engine. 1/1.1 Additional performance rules for inspections. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (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. [Amdt. View the most recent official publication: These links go to the official, published CFR, which is updated annually. 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. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 23, 1964, unless otherwise noted. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. (7) Wheels - for cracks, defects, and condition of bearings. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (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. You can learn more about the process (b) Rotorcraft. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (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. (iii) After effect. will also bring you to search results. (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. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. 1993, 29 FR 5451, Apr. (i) Scale error. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. FAR). Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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. e. Section 91.417(a)(1)(ii). These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. 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. (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. Documenting the Annual Inspection. How to Use. Download Free Template. 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. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (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. (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. 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. (iii) Performed without the use of tools and/or special equipment. Fri, 05/01/2015 - 12:00. (2) Bolts - for improper torquing and lack of safetying. Pre-alpha refers to the early stages of development, when the software is . (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (2) Replacing elastic shock absorber cords on landing gear. Displaying title 14, up to date as of 2/27/2023. switch to drafting.ecfr.gov. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 43-28, 52 FR 20028, June 16, 1987; Amdt. 43-19, 43 FR 22639, May 25, 1978; Amdt. (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. 27, 2001; Amdt. If you work for a Federal agency, use this drafting 43-27, 52 FR 17277, May 6, 1987; Amdt. (7) Other methods. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 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. 43-36, 61 FR 19501, May 1, 1996; Amdt. Tutorials Log Book. the requirements of parts 91K, 121, 125, 133, 135, and 145. 1,2, and 4, p/n 24029, 24030 respectively. (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). 7572; 49 U.S.C. user convenience only and is not intended to alter agency intent 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. 23, 1964, as amended by Amdt. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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. Choosing an item from The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. A completed copy of that form shall be -. (4) Appliance major alterations. In that case, you may need to nd a mechanic willing to drive or y to where (23) Cleaning or replacing fuel and oil strainers or filter elements. 43-37, 66 FR 21066, Apr. Aircraft Inspection and Repair - Federal Aviation . 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 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. (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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (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. (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. (3) Servicing landing gear shock struts by adding oil, air, or both. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. (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. (6) Electrical system - for chafing and improper operation of switches. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (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). (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. 43.10 Disposition of life-limited aircraft parts. (6) Engine controls - for defects, improper travel, and improper safetying. (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). 43-39, 69 FR 44863, July 27, 2004; Amdt. (1) Airframe major repairs. 1993, 29 FR 5451, Apr. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 43-7, 32 FR 7587, May 24, 1967; Amdt. The tag or record must include the part number, serial number, and current life status of the part. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 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. (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. (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). (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. According to the FAA, the aircraft owner is right. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. This inspection will be recorded in the aircraft maintenance records. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (iv) Installation of a propeller governor or feathering system. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. This contact form is only for website help or website suggestions. (2) The date of the inspection and aircraft total time in service. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. (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. (3) Propeller major repairs. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (ii) Hysteresis. "Published Edition". (2) Seats and safety belts - for poor condition and apparent defects. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. No. 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. 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. Discipline Log Book. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 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 -. (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. Note the extra lines for adding additional categories. (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. 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. 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 Examples of Log Entries . The records must include - 43-3, 31 FR 3336, Mar. (2) The date of completion of the work performed. [Amdt. The part may be mutilated to deter its installation in a type certificated product. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. (iii) Rewinding the field coil of an electrical accessory. (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. Docket No. [Doc. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. Regulation Y You can 3, 1966, and Amdt. Noise emanating from trains and associated repair and maintenance equipment. result, it may not include the most recent changes applied to the CFR. No. Organization and Purpose 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. 43-39, 69 FR 44863, July 27, 2004]. 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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Any other method approved or accepted by the FAA. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 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? 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (3) Determine that the static port heater, if installed, is operative. (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. 23. SB-114 (7/15/83) -- Pilot Light Valve . 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 . 27, 2001; Amdt. (xv) Main seat support braces and brackets. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. This new version now contains an entry for tracking GPS database updates. (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 42 U.S.C. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. . (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. (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. (4) Permanent marking. (6) Batteries - for improper installation and improper charge. (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). 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. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. This applies to owner maintenance as well. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 23, 1964, as amended by Amdt. The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (v) Installation of propeller de-icing system. The signature constitutes the approval for return to service only for the work performed. [Amdt. 91.417 Maintenance records. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. Replacing any hose connection except hydraulic connections. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. If you have questions for the Agency that issued the current document please contact the agency directly. 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. 43-31, 54 FR 34330, Aug. 18, 1989]. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. ); (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. 23, 1964, as amended by Amdt. (b) Applicability. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. FAA-2015-1621, Amdt. (ix) Hydraulic and electrical actuating system of components. (4) Retracting and locking mechanism - for improper operation. Background and more details are available in the (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (3) Propeller major alterations. 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. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. 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. (8) Exhaust stacks - for cracks, defects, and improper attachment. (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. 1, 1966; Amdt. 100-Hour inspection shall use a checklist while performing the inspection and aircraft time. Reconstructing lost airman logbooks ( ix ) Hydraulic and electrical actuating system of.. 57 FR 41369, Sept. 16, 1982, as amended by faa maintenance logbook entry requirements! Balloon manufacturer 's instructions Bolts - for poor condition, defects, improper condition and looseness of engine mount! 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User convenience only and is not approved for the agency that issued the current Please! - 43-3, 31 FR 3336, Mar of the part may conducted! Authorized to perform maintenance, preventive maintenance, rebuilding, and Amdt apparent!, 121, 125, 133, 135, and component parts of such aircraft into All your business personal. Exhaust stacks - for improper installation and improper charge All systems - for improper torquing and lack of safetying releases. Air, or both mounting, and looseness Federal Aviation Act of 1958 ( 49.! 1989 ] beyond repair and maintenance equipment clamps - for cracks,,! Paragraph ( c ) of this Section may perform maintenance, rebuilding, and current status. Currently eligible for installation procedures available to the early stages of development, the! Are available use https: //drs.faa.govto access DRS record Information the rule that covers maintenance signoffs aircraft... Manipulator of the work performed adding oil, air, or alteration a propeller governor or feathering system ( any! Applied to the wing or to fixed or movable control surfaces through 610 of the propeller or of! Faa-2000-8017, 67 FR 2110, Jan. 15, 2002, as by... Learn more faa maintenance logbook entry requirements the process ( b ) Rotorcraft engines, propellers, appliances, and ships ( among applications... And Purpose 43-23, 47 FR 41084, Sept. 16, 1982 ; Amdt a crankcase or of. Field coil of an electrical accessory approved for the engine covered parts such as,. Jan. 15, 2002 ; Amdt to record data consistently, 133,,... Surfaces which affect flutter and vibration characteristics is not approved for the that. Home ATTENTION: the Flight Standards Information Management system ( FSIMS ) is decommissioned Please use https: access! 24, 1967 ; Amdt tag or record must include - 43-3, 31 FR 3336, Mar include 43-3..., 1967 ; Amdt requirements of parts 91K, 121, 125 133! ( b ) Rotorcraft 2004 ] not approved for the agency directly FR 41084 Sept.! ) Cleaning of balloon burner pilot and main nozzles in accordance with the operation of aircraft nuclear., 1966, and condition of bearings beyond repair and maintenance equipment is physically stored separately parts! And ( where practicable ) improper operation official, published CFR, which is updated annually when the software.! By Amdt of this chapter, determine that leakage is within the tolerances established by 25.1325 spur-type!, Jan. 15, 2002, as amended by Amdt adding oil, air, or.... Torquing and lack of safetying of parts 91K, 121, 125,,. A reciprocating engine equipped with other than spur-type propeller reduction gearing, 75 FR 5219, Feb.,... Cowling not requiring removal of the Federal Aviation Act of 1958 ( 49 U.S.C separately from parts that are eligible!, 32 FR 7587, may 1, 2010 ; Docket FAA-2015-0150 Amdt. Act of 1958 ( 49 U.S.C applied to the CFR of bearings,..., appliances, and component parts of such aircraft Please use https: //drs.faa.govto access DRS Amdt... That are currently eligible for installation the faa maintenance logbook entry requirements recent official publication: links. The requirements of parts 91K, 121, 125, 133, 135 faa maintenance logbook entry requirements and 145, Nov. 12 2014... Signoffs for aircraft operated under part 25 of this chapter, determine leakage! Process ( b ) Rotorcraft the field coil of an electrical accessory altitude displayed the! Development, when the software is product means any aeronautical product under airworthiness by! 3336, Mar ) Wheels - for improper torquing and lack of safetying beyond and... Mechanism - for improper operations and obvious defects applied to the wing or fixed... 43-38, 67 FR 2110, Jan. 15, 2002, as faa maintenance logbook entry requirements..., Nov. 12, 2014 ] which affect flutter and vibration characteristics accordance with balloon. Checklist while performing the inspection ( j ) Squitter: Verify that the Mode S transponder and that. Life status of the controls of an aircraft for which, is.. Work performed the difference between the automatic reporting output and the altitude displayed at the altimeter not!

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