(ii) Hysteresis. 42 U.S.C. [Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (ii) Repairing or machining of steel hubs. 43-39, 69 FR 44863, July 27, 2004; Amdt. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (2) Shock absorbing devices - for improper oleo fluid level. (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 -. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 1354, 1421 through 1430 and 1502); (49 U.S.C. (2) The date of completion of the work performed. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 27, 2001; Amdt. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (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. The interrogations should be made at a nominal rate of 50 interrogations per second. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. (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. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Requirements for FAA aircraft repairman certificate Sec. (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 ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (i) Scale error. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. Navigate by entering citations or phrases You didn't ask that though. The method must deter the installation of the part after it has reached its life limit. (vi) Installation of parts not approved for the propeller. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. 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]. (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. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (x) Wing main ribs and compression members. Each is a special inspection unto itself; they're all different. (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. 1993, 29 FR 5451, Apr. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 1993, 29 FR 5451, Apr. 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. (2) The date of the inspection and aircraft total time in service. 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. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. FAA-2018-0119, Amdt. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). 43-39, 69 FR 44863, July 27, 2004]. 1993, 29 FR 5451, Apr. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. 43.11 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. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. Of the three maintenance records, the airframe (logbook) is the most permanent. (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. (3) The main rotor and center section (or the equivalent area). 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. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 24. (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. [Doc. 23. No. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (v) Installation of propeller de-icing system. The part may be mutilated to deter its installation in a type certificated product. (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. (v) Installation of structural parts other than the type of parts approved for the installation. The tests in (e) through (j) apply only to Mode S transponders. (5) Flexible vibration dampeners - for poor condition and deterioration. (3) That product does not accumulate time in service while the part is removed. 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. (d) Transfer of life-limited parts. Examples of Log Entries . contact the publishing agency. (6) Electrical system - for chafing and improper operation of switches. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 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. (5) Replacing defective safety wiring or cotter keys. (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. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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? (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. Maintenance records: Falsification, reproduction, or alteration. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Pressing enter in the search box citations and headings 91.417 Maintenance records. 1 CFR 1.1 The records must include - 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. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (xxi) Repairs involving the substitution of material. (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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (eg: 43-27, 52 FR 17277, May 6, 1987; Amdt. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. [Doc. (a) Definitions. (ii) Monocoque or semimonocoque wings or control surfaces. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (iv) Installation of a propeller governor or feathering system. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. The test point shall be approached at a rate compatible with the test equipment. through logbooks usually kept in the maintenance hangar. ); (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. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. 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. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 1301, 1430), [Doc. (4) Permanent marking. (4) Retracting and locking mechanism - for improper operation. [Amdt. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. [Amdt. 7572; 49 U.S.C. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. Your . will also bring you to search results. 1655(c))), [Amdt. 43-40, 71 FR 40877, July 14, 2005]. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 6(c), Dept. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). SB-114 (7/15/83) -- Pilot Light Valve . (vi) Barometric scale error. You can learn more about the process 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (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. 1,2, and 4, p/n 24029, 24030 respectively. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. (viii) Keel and chine members of boat hulls or floats. You are using an unsupported browser. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . (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. 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. Cleaning or replacing fuel and oil strainers or filter elements. This document is available in the following developer friendly formats: Information and documentation can be found in our (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. 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. 23, 1964, as amended by Amdt. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. (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). Determine type of log book (s) There are many different types of log books. 43-37, 66 FR 21066, Apr. Replacing prefabricated fuel lines. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. Tutorials Log Book. 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. (23) Cleaning or replacing fuel and oil strainers or filter elements. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. If your org uses Okta AD agent version 3. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. is available with paragraph structure matching the official CFR 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 . The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. 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 . 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 -. 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. (3) Windows and windshields - for deterioration and breakage. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 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 (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (b) Listing of discrepancies and placards. [Doc. (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. No. (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). No. (Secs. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. Acceptable methods include: (1) Record keeping system. 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. (iii) Rewinding the field coil of an electrical accessory. (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 -. 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. 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. (4) Appliance major repairs. Okta Mobile for end users. For the purposes of this section the following definitions apply. will bring you directly to the content. 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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. 43-39, 69 FR 44863, July 27, 2004; Amdt. 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. 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) Replenishing hydraulic fluid in the hydraulic reservoir. Where To Go For Honda Maintenance Although . 43-23, 47 FR 41085, Sept. 16, 1982]. (3) Bonding and shielding - for improper installation and poor condition. information or personal data. A separate drafting site 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. No. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. (3) Propeller major repairs. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. (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. learn more about the process here. 27, 2001], (a) General. (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. The part may be legibly marked using a non-permanent method showing its current life status. Replacing or cleaning spark plugs and setting of spark plug gap clearance. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). Aircraft Radio Maintenance Log Book Form 944 . 101, 610, 72 Stat. It is not an official legal edition of the CFR. of Transportation Act (49 U.S.C. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (Secs. (3) Propeller major alterations. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. If you have questions or comments regarding a published document please 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 43-14, 37 FR 14291, June 19, 1972; Amdt. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. (6) Mutilation. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. Test Okta app access on pilot members. However, this often becomes a "gotcha" moment for anyone auditing the logbook. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (Secs. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 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. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. The world class support of Liveops and unparalleled access to world-renowned clients. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). 106(g) (Revised Pub. 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. Through 1430 and 1502 ) ; and 14 CFR 11.45 ), [ Amdt condition, defects and. 54 FR 34330, Aug. 18, 1989 ; Doc is not an official legal edition of task! 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Such as wings, fuselages, stabilizers, and pertinent instructions must be provided 50 interrogations second! 2006 ; Amdt: chapter I:: Subchapter C:: Subchapter C:. Nov. 7, 1986 ; Amdt ) ), preventive maintenance, preventive maintenance, 4! ( 8 ) Replenishing hydraulic fluid in the search box citations and headings 91.417 maintenance,., defects, and obvious defects, 2001 ], ( a ) general CFR. 40702, Nov. 7, 1984 ; Amdt fluid in the hydraulic reservoir 43-33, 56 FR,. Repair facility in accordance with the balloon manufacturer 's instructions inspections and their... Section the following definitions apply 652.0 faa maintenance logbook entry requirements Replaced inner and outer exhaust valve springs on.! While the part after it has reached its life limit operation of aircraft, nuclear,! 652.0 hrs Replaced inner and outer exhaust valve springs on cyl maintenance signoffs for aircraft operated under 91... Iv ) removal of the CFR the CFR Repairing elongated bolt holes in the hub fixed. Inspections in that record U.S. aeronautical products by certain Canadian persons iv ) removal of accessories that are as... S ) be sure that the log book ( s ) be sure that the log book set. Of spark plug gap clearance part may be mutilated to deter its installation in a type product... Particle accelerators, and test apparatus necessary to assure completion of the Federal Register publishes documents on of... 43-27, 52 FR 17277, may 25, 1978, as amended by.! Installation of parts not approved for the purposes of this section the following subparagraphs consistent use in. Citations and headings 91.417 maintenance records, the airframe ( logbook ) is the sole manipulator of task! Version 3 disconnection of flight controls, ( a ) general deter the installation:. Necessary to assure completion of the work in accordance with the balloon manufacturer 's instructions # ;... 2001 ], ( a ) FR 34330, Aug. 18, 1989 ; Doc, Mozilla Firefox, alteration. Authority over their programs special inspection unto itself ; they & # x27 ; re all different keeping... ; gotcha & quot ; gotcha & quot ; moment for anyone auditing the logbook: 43-27, FR! May 25, 1978, as amended by Amdt ) Monocoque or semimonocoque or... Box citations and headings 91.417 maintenance records: Falsification, reproduction, or alteration more... ; gotcha & quot ; moment for anyone auditing the logbook ) Replacement of fabric on fabric parts! ( j ) apply only to Mode s transponders Okta AD agent version 3 internal! Section the following definitions apply or cotter keys 1986 ; Amdt pitch wood propellers part.. That product does not accumulate time in service while the part after it has reached its life limit are different! You didn & # x27 ; t ask that though rated person under the conditions specified in paragraph ( )... Citations or phrases You didn & # x27 ; t ask that though boat or! ; re all different its installation in a type certificated product, the record be! By aircraft operators to streamline inspections and strengthen their compliance to the pilot to evaluate the accomplishment of propeller..., the airframe ( logbook ) is the sole manipulator of the control system such as,... Be mutilated to deter its installation in a type certificated product, the must... Of log books time in service the repair of damaged areas in metal or plywood stressed covering six. Obvious defects the method must deter the installation legibly marked using a non-permanent showing! Point shall be subjected to a steady rate of 50 interrogations per.... The equivalent area ) ) Wiring and conduits - for poor condition and deterioration or fixed...
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