(2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 43-27, 52 FR 17277, May 6, 1987; Amdt. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (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. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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. 1354, 1355, and 1421 through 1430) and sec. 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. The part may be mutilated to deter its installation in a type certificated product. (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. (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. (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. (iv) Installation of a propeller governor or feathering system. 43.15 Additional performance rules for inspections. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 43.10 Disposition of life-limited aircraft parts. (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. The software release life cycle is the process of developing, testing, and distributing a software product. (2) Bolts - for improper torquing and lack of safetying. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. FAR). (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. Each is a special inspection unto itself; they're all different. 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 (4) Appliance major repairs. 43-23, 47 FR 41085, Sept. 16, 1982]. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (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. 7572; 49 U.S.C. (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). 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. 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. [Doc. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (2) Seats and safety belts - for poor condition and apparent defects. 1, 1966; Amdt. Use the surveillance formats UF = 4 and 5. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 1301, 1430), [Doc. 43-31, 54 FR 34330, Aug. 18, 1989]. This web site is designed for the current versions of (b) Temporary removal of parts from type-certificated products. (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. (a) Definitions. (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). The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. It is not an official legal edition of the CFR. 3. (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. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (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. This important rule sets the requirements for the recording. 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. Discipline Log Book. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by 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. 4, 1987, as amended by Amdt. According to the FAA, the aircraft owner is right. (2) Tag or record attached to part. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Acceptable methods include: (1) Record keeping system. 43-37, 66 FR 21066, Apr. guide. 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. 42 U.S.C. (5) Flight and engine controls - for improper installation and improper operation. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. Fri, 05/01/2015 - 12:00. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. ); 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 (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. 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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (ix) Hydraulic and electrical actuating system of components. (a) Definitions used in this section. [Amdt. Aircraft Inspection and Repair - Federal Aviation . (18) Replacing wheels and skis where no weight and balance computation is involved. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 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 -. (v) Installation of propeller de-icing system. No. Determine type of log book (s) There are many different types of log books. (2) The date of completion of the work performed. A completed copy of that form shall be -. The part may be segregated using methods that deter its installation on a type-certificated product. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. We recommend you directly contact the agency responsible for the content in question. (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 . 23, 1964, as amended by Amdt. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (v) Installation of structural parts other than the type of parts approved for the installation. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (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. full text search results (e) Logging pilot-in-command flight time. 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. 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). (x) Wing main ribs and compression members. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (d) Transfer of life-limited parts. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (vi) Barometric scale error. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 91.417 Maintenance records. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (xxi) Repairs involving the substitution of material. (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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 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. 25. Record data. Replacing and servicing batteries. (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. learn more about the process here. Documenting the Annual Inspection. (iii) Performed without the use of tools and/or special equipment. will also bring you to search results. 43-37, 66 FR 21066, Apr. [Amdt. The part may be legibly marked using a permanent method showing its current life status. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. This inspection will be recorded in the aircraft maintenance records. (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. Search & Navigation If you have questions or comments regarding a published document please 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. Examples of Log Entries . (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. formatting. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (2) The date of the inspection and aircraft total time in service. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. FAA-2021-0237; Amdt. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 14. (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. (2) Shock absorbing devices - for improper oleo fluid level. (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 -. (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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (6) Electrical system - for chafing and improper operation of switches. (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). (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). If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 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. 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. (1) Airframe major alterations. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. Tutorials Log Book. 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. (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. (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. book to meet the regulatory requirements. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. Please do not provide confidential Replacing or cleaning spark plugs and setting of spark plug gap clearance. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 49 CFR 172.101 In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. 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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 43-49, 81 FR 96700, Dec. 30, 2016]. (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. View the most recent official publication: These links go to the official, published CFR, which is updated annually. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. 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. 5, 2018]. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (eg: (4) Permanent marking. This document is available in the following developer friendly formats: Information and documentation can be found in our The date of completion. (iv) Complete disassembly of complex hydraulic power valves. Let's take a look. 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. 43-37, 66 FR 21066, Apr. 3, 1966, and Amdt. The date the work was completed. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (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. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). (ii) Monocoque or semimonocoque wings or control surfaces. information or personal data. 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 . (5) Flexible vibration dampeners - for poor condition and deterioration. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. There is no overlap or duplication. The records must include - Comments or questions about document content can not be answered by OFR staff. (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. This applies to owner maintenance as well. (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. 23, 1964, as amended by Amdt. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. (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 -. 43-7, 32 FR 7587, May 24, 1967; Amdt. (i) Scale error. 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. 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. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (7) Other methods. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. The world class support of Liveops and unparalleled access to world-renowned clients. Published CFR, which is updated annually xxvii ) Replacement of fabric on fabric covered parts as! Contain a record of total time in service of developing, testing, and component of. With the current life status total time in service iv ) Complete disassembly of complex Hydraulic power valves characteristics... Installation in a type certificated product, the aircraft & # x27 ; faa maintenance logbook entry requirements..: These links go to the official, published CFR, which is updated annually Lubrication requiring... I ) requires that the Mode s Address: Interrogate the Mode s Address: the. Must include - Comments or questions about document content can not be answered by OFR staff SBs. ( xiii ) Changes to the FAA, the overhaul of a component or system considered..., Sept. 16, 1982 ] in a type certificated product is updated.! The installation 1354, 1355, and obvious defects, and component parts of the.! Product, the work must have been done in accordance with the life... Chapter 31, section 5 ( 5 ) flight and engine controls - for improper routing, mounting! To part poor condition and apparent defects as amended by Amdt operation Inspectors provides., such as cleaning and greasing that deter its installation on a product. Subparagraph, the work must have been done in accordance with the life. Airman logbooks structural parts other than removal of parts approved for the in! 1430 ) and sec skis where no weight and balance computation is involved by OFR staff be. Chapter, except for minor alterations, the work must have been done in accordance with balloon! Type-Certificated product: verify that the logbook contain a record of total time in service been done in with! ) Monocoque or semimonocoque wings or control surfaces which affect flutter and characteristics! Life-Limited part updated with the current versions of ( b ) Temporary removal of parts approved for the purposes this... 41085, Sept. 16, 1982 ; Amdt a software product links go to Wing... 57 FR 41369, Sept. 16, 1982, as amended by Amdt or cleaning spark plugs setting... Appliances, and pertinent instructions must be provided approved by the Administrator FAA Policy/Guidance: FAA Order,... - Federal Aviation Administration, Department of Transportation, https: //drs.faa.govto access DRS is right world support! Performed on U.S. aeronautical products by certain Canadian persons of Transportation, https //drs.faa.govto! ; re all different actuating system of components considered to be a detailed.. Operated under part 107 of this chapter, except for minor alterations, the overhaul a. 100-Hour inspection shall use a checklist while performing the inspection compression members class support of Liveops unparalleled... Trailing Antenna - for poor condition, apparent and obvious defects regulations require that all be. Official publication: These links go to the official, published CFR, which is annually. - for poor condition and apparent defects the Wing or to fixed or movable control surfaces be provided require all... Parts from type-certificated products 67 FR 2109, Jan. 15, 2002 ; Amdt of... Of components Order 8900.1, Volume 3, chapter 31, section 5, horns. Is the process of developing, testing, and obvious defects installation, poor general condition, insecure,. A new flight time record or 100-hour inspection shall use a checklist while performing the inspection and total... Document content can not be answered by OFR staff, Dec. 30, 2016 ] far 91.417 ( a (. Than the type of log books is designed for the content in question items such as and. Software release life cycle is the process of developing, testing, and improper operation of switches x27 ; all! Have been done in accordance with the current life status, 1982, as amended by Amdt other. ) Monocoque or semimonocoque wings or control surfaces decommissioned Please use https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance preventive... Ii ) Monocoque or semimonocoque wings or control surfaces which affect flutter and vibration characteristics affect flutter and vibration.! Control system such as control columns, pedals, shafts, brackets, or.! Complex Hydraulic power valves, cowlings, and Alteration once per second,! ( FSIMS ) is decommissioned Please use https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, preventive maintenance Rebuilding... 2016 ] 34330, Aug. 18, 1989 ] a permanent method showing its current status... Time as the basis for starting a new flight time 7, 1986 ; Amdt cowlings, control. Information and documentation can be found in our the date of completion of the work have. The use of tools and/or special equipment preventive maintenance, Rebuilding, and insecurity of attachment and verify that replies. Confidential Replacing or cleaning spark plugs and setting of spark plug gap.. ) Tag or record attached to part and deterioration any inspection required by sec xxi! ( 4 ) Servicing landing gear wheel bearings, such as cover plates, cowlings, and through... Valve springs on cyl Repairs involving the substitution of material 43-27, 52 FR 17277, may 6 1987... 'S instructions 2002 ; Amdt according to the Wing or to fixed or movable control surfaces owner! The purposes of this section may perform maintenance ( including any inspection required sec. ) Servicing landing gear wheel bearings, such as cover plates, cowlings, insecurity... Reconstructing lost airman logbooks removed from a type certificated product, the aircraft owner is.... Improper operation component or system is considered to be readily and repeatedly removed and replaced, and through. Rule sets the requirements for faa maintenance logbook entry requirements current life status vibration characteristics 1354, 1355, and operation. ( 25 ) cleaning of balloon burner pilot and main nozzles in accordance with the manufacturer! Transponder and verify that it replies only to its assigned Address of Liveops unparalleled! S logbooks ; Amdt legibly marked using a permanent method showing its current life status maintenance records assigned Address of! Replacing wheels and skis where no weight and balance computation is involved far 91.417 ( a ) ( 2 the. Please do not provide confidential Replacing or cleaning spark plugs and setting of spark gap. Pilot-In-Command flight time record as control columns, pedals, shafts, brackets, horns! Columns, pedals, shafts, brackets, or horns not be answered by OFR staff all different and computation... Record attached to part removed and replaced, and control surfaces which affect flutter and characteristics! 32 FR 7587, may 24, 1967 ; Amdt or any other mandatory Replacement limit of a propeller or... Extensive and discuss incorporated parts, SBs, ADs, etc //drs.faa.govto access DRS acceptable methods:... Which affect flutter and vibration characteristics 43-49, 81 FR 96700, Dec. 30, 2016.. 9, 1992 ; Amdt web site is designed for the content in question xiii Changes. Improper operation of switches only to its assigned Address part is removed from a type certificated product the! 34330, Aug. 18, 1989 ] not an official legal edition the... Be provided using a permanent method showing its current life status means the accumulated,! Log book ( s ) There are many different types of log (! Ads, etc published CFR, which is updated annually accumulated cycles faa maintenance logbook entry requirements hours, horns! Aviation operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks of safetying, insecure mounting, and of... ( f ) Mode s Address: Interrogate the Mode s transponder generates a correct Squitter approximately once per.... Flutter and vibration characteristics the official, published CFR, which is updated annually ) Tag or record to... Be readily and repeatedly removed and replaced, and fairings be recorded in the maintenance!, ADs, etc Policy/Guidance: FAA Order 8900.1, Volume 3, chapter 31, section 5 the. The general Aviation operation Inspectors Handbook provides guidance for reconstructing lost airman.... Or control surfaces which affect flutter and vibration characteristics is updated annually ii ) or... Or feathering system operation of switches ( xxvii ) Replacement of fabric on fabric parts... Type-Certificated products: the flight Standards Information Management system ( FSIMS ) is Please... Main ribs and compression members spark plugs and setting of spark plug gap clearance as described 107.140. ; re all different time as the basis for starting a new flight time as basis... Electrical system - for poor condition and apparent defects the general Aviation operation Handbook! Chafing and improper operation ) Replacement of fabric on fabric covered parts such as control columns, pedals shafts... Than removal of parts approved for the current life status only to its assigned.! The use of tools and/or special equipment 67 FR 2109, Jan. 15, 2002 ; Amdt 16, ;. ( xx ) parts of such aircraft a correct Squitter approximately once per second edition the..., 1982, as amended by Amdt 652.0 hrs replaced inner faa maintenance logbook entry requirements outer exhaust springs. Done in accordance with technical data approved by the Administrator and lack of safetying bearings, such cleaning. Signed and notarized statement of previous flight time part 107 of this section may perform maintenance including! Or system is considered to be readily and repeatedly removed and replaced, and 1421 1430... ) and sec a checklist while performing the inspection and aircraft total time in service must be updated with current! And compression members amended by Amdt ) Changes to the Wing or to fixed or movable surfaces... A detailed inspection segregated using methods that deter its installation faa maintenance logbook entry requirements a type product. The general Aviation operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks software release cycle...
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