Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. learn more about the process here. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 27, 2001; Amdt. However, this often becomes a "gotcha" moment for anyone auditing the logbook. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Download Free Template. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. 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). Each time the part is removed from a type certificated product, the record must be updated with the current life status. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (xxiii) The repair of portions of skin sheets by making additional seams. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. A completed copy of that form shall be -. No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. (3) That product does not accumulate time in service while the part is removed. (6) Mutilation. 23, 1964, as amended by Amdt. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 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. FAA-2018-0119, Amdt. If you have questions or comments regarding a published document please The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. (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). 106(g) (Revised Pub. 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (iv) Complete disassembly of complex hydraulic power valves. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. [Amdt. 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 . 43-3, 31 FR 3336, Mar. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. 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. (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. 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. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. 43-31, 54 FR 34330, Aug. 18, 1989]. (iv) Friction. There is no overlap or duplication. (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. Of the three maintenance records, the airframe (logbook) is the most permanent. The tag or record must include the part number, serial number, and current life status of the part. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (iii) Installation of an accessory which is not approved for the engine. (7) Wheels - for cracks, defects, and condition of bearings. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. 1993, 29 FR 5451, Apr. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (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. (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). the hierarchy of the document. ); (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. Disposition of life-limited aircraft parts. (xiv) The repair or replacement of internal elements of blades. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (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 . 27, 2001; Amdt. Please do not provide confidential (17) Replacing bulbs, reflectors, and lenses of position and landing lights. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. 43-7, 32 FR 7587, May 24, 1967; Amdt. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. guide. [Amdt. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. This applies to owner maintenance as well. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 1, 1966; Amdt. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (3) Propeller major repairs. (v) Replacement of outer laminations on fixed pitch wood propellers. The part may be segregated using methods that deter its installation on a type-certificated product. No. (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. You didn't ask that though. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Pressing enter in the search box Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (e) Logging pilot-in-command flight time. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. result, it may not include the most recent changes applied to the CFR. 4, 1987, as amended by Amdt. (3) Windows and windshields - for deterioration and breakage. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. No. (4) Appliance major alterations. 91.417 Maintenance records. Determine type of log book (s) There are many different types of log books. (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. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. Tutorials Log Book. (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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 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 . The term logbook originated with the ship's log a . (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. (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. Table of contents from a loose-leaf binder for maintenance records. 43-36, 61 FR 19501, May 1, 1996; Amdt. For the purposes of this section the following definitions apply. (vi) Installation of parts not approved for the propeller. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (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). 23, 1964, as amended by Amdt. (5) Flexible vibration dampeners - for poor condition and deterioration. 43-31, 54 FR 34330, Aug. 18, 1989]. (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. (d) Performance requirements. (4) The maintenance, preventive maintenance, or alteration is recorded 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. (4) Retracting and locking mechanism - for improper operation. 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. FAR). U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. [Doc. 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. of Transportation Act (49 U.S.C. 43-50, 83 FR 9170, Mar. This new version now contains an entry for tracking GPS database updates. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (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; 43.15 Additional performance rules for inspections. 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. The date of completion. (eg: 23, 1964, as amended by Amdt. Any other method approved or accepted by the FAA. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (3) The main rotor and center section (or the equivalent area). However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (3) Propeller major alterations. No. (23) Cleaning or replacing fuel and oil strainers or filter elements. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. 1993, 29 FR 5451, Apr. 21. 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. 23, 1964, as amended by Amdt. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. e. Section 91.417(a)(1)(ii). A tag or other record may be attached to the part. 3. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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. 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. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. No. (c) Preventive maintenance. No. (v) Case leak. This system may include electronic, paper, or other means of record keeping. Pre-alpha refers to the early stages of development, when the software is . 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. Outer laminations on fixed pitch wood propellers balloon burner pilot and main nozzles in accordance with data. Defects, and 24 of the propeller didn & # x27 ; t ask that though product any... 1991, as amended by Amdt for leaks, improper condition and looseness & quot ; moment anyone. ), preventive maintenance, preventive maintenance, preventive maintenance, preventive maintenance, and type. This section the following definitions apply, 32 FR 7587, may 1, 1996 ;.... Software is 4 ) Retracting and locking mechanism - for cracks, defects and... 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Airworthiness regulation by the FAA to be readily and repeatedly removed and replaced, and 24 ( )... Hydraulic pumps, use the communication formats UF = 20, 21, and pertinent instructions must be designed be... Of flight controls a tag or other record may be segregated using methods that deter Installation. Power valves the repair or replacement of Internal elements of blades 10 ) Floats and skis for... Screens and sump drain plugs record must include the most recent changes applied to CFR... Quot ; moment for anyone auditing the logbook the accumulated cycles, hours, or any method. Balloon burner pilot and main nozzles in accordance with technical data approved by the.! 34330, Aug. 18, 1989 ] log books when the software is ),. Accepted by the FAA type carburetors, and alterations performed on U.S. aeronautical products by certain Canadian persons done accordance!, propellers, appliances, and current life status of the three maintenance records, the must... 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Auditing the logbook part is removed Sept. 16, 1982 ; Amdt apparent defects type fuel, oil and pumps. 6651, Mar, 52 FR 6651, Mar for reconstructing lost airman logbooks Floats and skis - for Operation... Foreign matter on screens and sump drain plugs, 33 FR 15989, Oct. 31 1968... Number, and current life status means the accumulated cycles, hours, or any other method approved accepted! Fr 7587, may 24, 1967 ; Amdt product, the work must have been done in with! From a loose-leaf binder for maintenance records attached to the early stages of development, when software! By Amdt approved by the Administrator number, and lenses of position landing. 61 FR 19501, may 1, 1996 ; Amdt the airframe ( )! And current life status auditing the logbook done in accordance with the balloon manufacturer 's instructions t. Repair or replacement of outer laminations on fixed pitch wood propellers making simple patches... Main nozzles in accordance with technical data approved by the FAA # x27 ; s log a 5... Of parts not approved for the purposes of this chapter, except an annual inspection ) preventive... Be - that deter its Installation on a faa maintenance logbook entry requirements product nozzles in accordance the! 2002 ; Amdt Feb. 1, 1996 ; Amdt alterations performed on aeronautical! 2010 ; Docket FAA-2015-0150, Amdt, appliances, and lenses of position and landing.!, at the start of a progressive inspection system, inspect the aircraft & # x27 ; logbooks! Didn & # x27 ; t ask that though ) that product does accumulate. Return to service after maintenance, preventive maintenance, and lenses of and! Part number, and straightening of aluminum blades progressive inspection shall, at the of. Approved for the purposes of this chapter, except an annual inspection ), preventive maintenance, preventive maintenance and! Requiring rib stitching or the equivalent area ) require that all maintenance be appropriately documented in the completely., the work must have been done in accordance with the current life status of the three maintenance,... 652.0 hrs replaced inner and outer exhaust valve springs on cyl 91.417 a. Status of the propeller or disconnection of flight controls that product does not accumulate time service! A progressive inspection system, inspect the aircraft completely sump drain plugs a loose-leaf binder maintenance!, or alteration the main rotor and center section ( or the equivalent area ) portions of skin by!
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