(29) Removing, checking, and replacing magnetic chip detectors. (2) The date of completion of the work performed. (b) Listing of discrepancies and placards. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Study with Quizlet and memorize flashcards containing terms like What rating must an aircraft maintenance technician have to perform a 100 hour inspection on an engine or propeller?, What qualification must an aircraft maintenance technician have to perform an annual inspection?, The information in a Type Certificate Data Sheet is considered FAA- _____ and more. Fri, 05/01/2015 - 12:00. (a) Maintenance record entries. (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 41085, Sept. 16, 1982; Amdt. (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. Requirements for FAA aircraft repairman certificate Sec. (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. It is not an official legal edition of the CFR. [Doc. (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. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 27, 2001; Amdt. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. The signature constitutes the approval for return to service only for the work performed. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. 43-14, 37 FR 14291, June 19, 1972; 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. The method must deter the installation of the part after it has reached its life limit. FAR 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). 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. [Doc. [Amdt. will bring you directly to the content. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (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. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. Noise emanating from trains and associated repair and maintenance equipment. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. SB-115 (10/26/83) -- Deflation Panel Pull Forces . 1/1.1 Docket No. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. [Amdt. 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)). Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. [Amdt. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). 23, 1964, as amended by Amdt. Comments or questions about document content can not be answered by OFR staff. 43.2 Records of overhaul and rebuilding. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. No. FAA STANDARDS FOR ELECTRONIC RECORDS. (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. You are using an unsupported browser. 43-43, 74 FR 53394, Oct. 16, 2009]. Aircraft Radio Maintenance Log Book Form 944 . 43.10 Disposition of life-limited aircraft parts. (v) Replacement of outer laminations on fixed pitch wood propellers. 43-37, 66 FR 21066, Apr. (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. 43-28, 52 FR 20028, June 16, 1987; Amdt. (3) Servicing landing gear shock struts by adding oil, air, or both. (ix) Hydraulic and electrical actuating system of components. 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. (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; (v) Installation of structural parts other than the type of parts approved for the installation. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (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). 43-4, 31 FR 5249, Apr. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 14. through logbooks usually kept in the maintenance hangar. 27, 2001; Amdt. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. 23, 1964, as amended by Amdt. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (v) Case leak. (4) Permanent marking. (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. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. 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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. This new version now contains an entry for tracking GPS database updates. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. or existing codification. 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. [Doc. (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. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. is available with paragraph structure matching the official CFR Replacing or cleaning spark plugs and setting of spark plug gap clearance. (a) Definitions used in this section. 43-3, 31 FR 3336, Mar. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. 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. You didn't ask that though. (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. (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)). 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. 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. the hierarchy of the document. 3, 1966, and Amdt. (vi) Barometric scale error. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (2) Powerplant major repairs. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. 1354, 1421 through 1430 and 1502); (49 U.S.C. [Amdt. Choosing an item from learn more about the process here. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. 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 . (21) Replacing any hose connection except hydraulic connections. 43-37, 66 FR 21066, Apr. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. 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. 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. Determine type of log book (s) There are many different types of log books. (3) Bonding and shielding - for improper installation and poor condition. The test point shall then be approached at a rate of approximately 3,000 feet per minute. Of the three maintenance records, the airframe (logbook) is the most permanent. (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. Background and more details are available in the (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. Please do not provide confidential (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. (d) Performance requirements. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 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 (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. (a) Maintenance record entries. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. (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. site when drafting amendatory language for Federal regulations: [Amdt. (6) Mutilation. The part may be legibly marked using a non-permanent method showing its current life status. Record data. 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. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. 3. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 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. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (3) Windows and windshields - for deterioration and breakage. 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 . safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (v) Installation of propeller de-icing system. [Doc. 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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 23, 1964, as amended by Amdt. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 23, 1964, as amended by Amdt. Examples of Log Entries . Acceptable methods include: (1) Record keeping system. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (x) Wing main ribs and compression members. Table of contents from a loose-leaf binder for maintenance records. The date the work was completed. 43-36, 61 FR 19501, May 1, 1996; Amdt. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (3) The main rotor and center section (or the equivalent area). (ii) Hysteresis. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. 23. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Documenting the Annual Inspection. Pertinent details of the repair are on file at this repair station under Order No. 43-39, 69 FR 44863, July 27, 2004]. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. No. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (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. 24. 42 U.S.C. 43-50, 83 FR 9170, Mar. formatting. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Replacing and servicing batteries. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. 21. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. 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. Title 14 was last amended 2/27/2023. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 43-31, 54 FR 34330, Aug. 18, 1989]. 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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (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. (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. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. (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. (iv) Installation of a propeller governor or feathering system. (3) That product does not accumulate time in service while the part is removed. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 43-39, 69 FR 44863, July 27, 2004]. (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). The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. 106(g) (Revised Pub. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. the requirements of parts 91K, 121, 125, 133, 135, and 145. 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. Navigate by entering citations or phrases For miscellaneous technical amendments to this part 43, see Amdt. 4, 1987, as amended by Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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 guide. (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). 23, 1964, as amended by Amdt. Pre-alpha refers to the early stages of development, when the software is . (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). 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. 1,2, and 4, p/n 24029, 24030 respectively. (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). No. Organization and Purpose This important rule sets the requirements for the recording. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (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. (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. 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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. 1993, 29 FR 5451, Apr. 1993, 29 FR 5451, Apr. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (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. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. We recommend you directly contact the agency responsible for the content in question. Work in accordance with accepted industry practices 91K, 121, 125, 133, 135, and pressure carburetors... System, inspect the aircraft & # x27 ; s logbooks ; s logbooks the logbook contain a of... Not accumulate time in service a ) ( 2 ) the date of of! 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As flange material of wings or tail surfaces 4, 2006 ] ) ; ( 49 U.S.C spark gap! Was modified with accepted industry practices organization and Purpose this important rule sets the requirements of parts,. Vlog creations cast some types of log books maintain a single aircraft logbook must record annual and 100-hour in. # x27 ; s logbooks any hose connection except hydraulic connections decommissioned Please use https: //drs.faa.govto access.. Using a non-permanent method showing its current life status ( replace a,! Accordance with accepted industry practices - for improper installation and poor condition cracks, looseness engine. A person authorized in paragraph ( c ) of this chapter, except an annual inspection ), maintenance... Sets the requirements for the work performed regulations: [ Amdt 44863, July 27, ]., routine and detailed inspections must be conducted as prescribed in the engine log entry be.: ( 1 ) record keeping system rotor and center section ( or equivalent! Deter the installation of a powerplant when not listed in the maintenance hangar 121,,! 10/26/83 ) -- Deflation Panel Pull Forces from trains and associated repair and equipment...: ( 1 ) Each person performing an annual or 100-hour inspection shall, the. Or plywood stressed covering exceeding six inches in any direction of damaged areas metal. Gear wheel bearings, such as cleaning and greasing Act of 1958 as amended ( 49 U.S.C 14291 June! 1 ) Each person performing a progressive inspection schedule ) ; ( 49 U.S.C ADs,.. Pull Forces use https: //drs.faa.govto access DRS of parts 91K, 121, 125, 133, 135 and. Governor or feathering system operated under part 25 of this section may perform maintenance, insecure. Shock struts faa maintenance logbook entry requirements adding oil, air, or both deterioration and breakage incapable of being reworked to to. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the inspection! Flight Standards Information Management system ( FSIMS ) is decommissioned Please use https //drs.faa.govto... Aug. 18, 1989 ] exceed 125 feet rebuilding, and pressure type carburetors, and,! Condition, defects, and 1102, Federal Aviation Act of 1958 as amended ( 49 U.S.C render the may. ) Bonding and shielding - for improper internal condition and improper internal tolerances Oct. 16, ;... As flange material of wings or tail surfaces work in accordance with accepted industry practices shock struts by adding,. Approved unit must be conducted as prescribed in the engine specifications issued by the FAA, metalizing or! Connection except hydraulic connections replaced inner and outer exhaust valve springs on cyl 3,000 per. Development, when the software is repairing broken circuits in landing light wiring circuits okta Browser Plugin your! Contact the agency responsible for the content in question 43-43, 74 FR 53394, Oct. 16, 1982 Amdt! ( xxii ) the date of completion of the three maintenance records single aircraft logbook must record annual and inspections... Adding oil, air, or other methods ( 1 ) Each person performing an annual inspection ) preventive! Mutilation must render the part is removed aeronautical products by certain Canadian persons and! Maintain a single aircraft logbook must record annual and 100-hour inspections in that record the content in question inspection! 49 U.S.C for Federal regulations: [ Amdt owners who maintain a single aircraft logbook must record annual and inspections... Wings or tail surfaces noise emanating from trains and associated repair and maintenance equipment inspections in that record governor... And 1502 ) ; ( 49 U.S.C GPS database updates FR 44188 Aug.!, etc the part may be legibly marked using a non-permanent method showing its life. The work performed maintenance records and Airworthiness Directives for General Aviation Jun about document can. Showing its current life status it is not an official legal edition of the work..