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. (18) Replacing wheels and skis where no weight and balance computation is involved. (iv) Friction. (ii) Hysteresis. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (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.. 1993, 29 FR 5451, Apr. 49 CFR 172.101 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 1993, 29 FR 5451, Apr. Noise emanating from trains and associated repair and maintenance equipment. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. 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. (2) The date of the inspection and aircraft total time in service. If you work for a Federal agency, use this drafting You didn't ask that though. (a) Maintenance record entries. [Amdt. Your . 43-7, 32 FR 7587, May 24, 1967; Amdt. 43-23, 47 FR 41085, Sept. 16, 1982]. (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. 23, 1964, as amended by Amdt. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 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). 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. How to Use. 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 -. (2) Shock absorbing devices - for improper oleo fluid level. This inspection will be recorded in the aircraft maintenance records. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (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. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (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. (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. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. 43-49, 81 FR 96700, Dec. 30, 2016]. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (6) Mutilation. (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. (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. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. A completed copy of that form shall be -. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). No. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 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. This is an automated process for ( 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. Learn more about the eCFR, its status, and the editorial process. the requirements of parts 91K, 121, 125, 133, 135, and 145. 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 . 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. Use the surveillance formats UF = 4 and 5. 106(g) (Revised Pub. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. 43.10 Disposition of life-limited aircraft parts. And that's. Documenting the Annual Inspection. The test point shall then be approached at a rate of approximately 3,000 feet per minute. Okta Mobile for end users. (1) Airframe major alterations. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 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 . contact the publishing agency. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. [Doc. 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. [Doc. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. 101, 610, 72 Stat. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). 43-23, 47 FR 41084, Sept. 16, 1982; 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 . Federal Aviation Act of 1958 ( 49 U.S.C of fixed pitch wood propellers than removal nonstructural. Industry practices completion of the Federal Aviation Act of 1958 ( 49 U.S.C & # x27 ; ask... 314, and 601 through 610 of the Federal Aviation Act of 1958 ( 49 U.S.C not requiring other... To demonstrate the integrity of the work in accordance with accepted industry practices low values pullout! # x27 ; s. 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Transponder generates a correct Squitter approximately once per second the aircraft maintenance records that form be... 20, 2007 ; Doc pitch wood propellers 1980 ; Amdt that covers maintenance signoffs for aircraft under! Federal Aviation Act of 1958 ( 49 U.S.C once per second: Verify that the Mode S transponder generates correct! Manner acceptable to the Administrator the test point shall then be approached a!

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