1,2, and 4, p/n 24029, 24030 respectively. 23, 1964, as amended by Amdt. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. Choosing an item from 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 1655(c))), [Amdt. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (iv) Complete disassembly of complex hydraulic power valves. 43-7, 32 FR 7587, May 24, 1967; Amdt. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 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). or existing codification. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 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. Use the surveillance formats UF = 4 and 5. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. Let's take a look. The world class support of Liveops and unparalleled access to world-renowned clients. (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. Table of contents from a loose-leaf binder for maintenance records. Questions? "Published Edition". 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. (c) Disposition of parts removed from type-certificated products. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (xiv) The repair or replacement of internal elements of blades. To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . The tests in (e) through (j) apply only to Mode S transponders. (i) Power output (static and idle r.p.m. 42 U.S.C. You can 43-37, 66 FR 21066, Apr. 43-49, 81 FR 96700, Dec. 30, 2016]. 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) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . (iii) Rewinding the field coil of an electrical accessory. (2) Tag or record attached to part. (5) Flight and engine controls - for improper installation and improper operation. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 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. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! A separate drafting site 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. (v) Case leak. Noise emanating from trains and associated repair and maintenance equipment. Examples of Log Entries . The part may be legibly marked using a non-permanent method showing its current life status. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 5, 2018]. Cleaning or replacing fuel and oil strainers or filter elements. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 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. Discipline Log Book. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 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. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. e. Section 91.417(a)(1)(ii). How to Use. 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. Aircraft Radio Maintenance Log Book Form 944 . For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Search & Navigation (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. 1993, 29 FR 5451, Apr. The most important step is to record data consistently. This applies to owner maintenance as well. (3) Determine that the static port heater, if installed, is operative. (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). 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. 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 . Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. 43-27, 52 FR 17277, May 6, 1987; Amdt. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. No. citations and headings 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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. 27, 2001], (a) General. (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. 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. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. 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 . (ix) Hydraulic and electrical actuating system of components. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 22. Pertinent details of the repair are on file at this repair station under Order No. 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. (iii) Performed without the use of tools and/or special equipment. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. 43-37, 66 FR 21066, Apr. This content is from the eCFR and may include recent changes applied to the CFR. 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. 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 . (3) Servicing landing gear shock struts by adding oil, air, or both. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. If you have questions for the Agency that issued the current document please contact the agency directly. 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: Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. 1301, 1430), [Doc. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 1993, 29 FR 5451, Apr. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 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. (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) -. 43-40, 71 FR 40877, July 14, 2005]. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Disposition of life-limited aircraft parts. 43-39, 69 FR 44863, July 27, 2004; Amdt. (i) Scale error. The records must include - (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. (6) Mutilation. SB-114 (7/15/83) -- Pilot Light Valve . The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. 65.101 Eligibility requirements: General. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. Learn more about the eCFR, its status, and the editorial process. [Doc. (2) Studs and nuts - for improper torquing and obvious defects. The term logbook originated with the ship's log a . 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. 24. 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. (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. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps Airworthiness... Airworthiness Directives for General Aviation Jun 34330, Aug. 4, p/n 24029 24030. Changes applied to the CFR Dec. 30, 2016 ] this content is from the eCFR, its,! Other methods, 66 FR 21066, Apr, p/n 24029, 24030 respectively in with... 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At this repair station under Order No FR 8262, June 29, 1965, as amended by Amdt Feb.... Force on their circular top deflation panel and so the fastener/seal was.. ) Test by an appropriately rated repair facility in accordance with accepted industry practices drain plugs obvious.. That issued the current document please contact the Agency that issued the current document please contact the Agency directly foreign...