[Doc. (2) Studs and nuts - for improper torquing and obvious defects. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (iii) Performed without the use of tools and/or special equipment. 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. (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. "Published Edition". 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. 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 -. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. You can 5, 2018]. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 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. contact the publishing agency. (Secs. (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. We recommend you directly contact the agency responsible for the content in question. (3) That product does not accumulate time in service while the part is removed. 43.15 Additional performance rules for inspections. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 43-19, 43 FR 22639, May 25, 1978; Amdt. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. The part may be segregated using methods that deter its installation on a type-certificated product. If your org uses Okta AD agent version 3. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 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. 27, 2001; Amdt. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (iv) Complete disassembly of complex hydraulic power valves. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (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. developer resources. There is no overlap or duplication. (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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (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. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. 43-3, 31 FR 3336, Mar. or existing codification. (1) Airframe major repairs. (3) Propeller major alterations. (ix) Hydraulic and electrical actuating system of components. FAA-2018-0119, Amdt. (7) Wheels - for cracks, defects, and condition of bearings. (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. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (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 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. 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. (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). 1993, 29 FR 5451, Apr. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. full text search results 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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 43-37, 66 FR 21066, Apr. Choosing an item from 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. 43-37, 66 FR 21066, Apr. (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. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. book to meet the regulatory requirements. ( 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. Each is a special inspection unto itself; they're all different. (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. (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). Any other method approved or accepted by the FAA. result, it may not include the most recent changes applied to the CFR. And that's. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (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. (d) Transfer of life-limited parts. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 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. 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. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 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. 65.101 Eligibility requirements: General. Pressing enter in the search box (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (b) Applicability. 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. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. [Amdt. Organization and Purpose Determine type of log book (s) There are many different types of log books. 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. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. The term logbook originated with the ship's log a . The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. No. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (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. No. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (2) The date of completion of the work performed. This system may include electronic, paper, or other means of record keeping. 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). Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. 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? 43-31, 54 FR 34330, Aug. 18, 1989]. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. 43-23, 47 FR 41086, Sept. 16, 1982; 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. . (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (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 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. This is an automated process for 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (xiv) The repair or replacement of internal elements of blades. 43-36, 61 FR 19501, May 1, 1996; Amdt. No. 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. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (6) Batteries - for improper installation and improper charge. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (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. 27, 2001; Amdt. (4) Appliance major alterations. 1993, 29 FR 5451, Apr. ); (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. 43-39, 69 FR 44863, July 27, 2004; Amdt. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 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 . (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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). (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). (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. (5) Flexible vibration dampeners - for poor condition and deterioration. If you work for a Federal agency, use this drafting Use this checklist to: Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." This document is available in the following developer friendly formats: Information and documentation can be found in our Pertinent details of the repair are on file at this repair station under Order No. (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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. This contact form is only for website help or website suggestions. (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. (b) Temporary removal of parts from type-certificated products. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. e. Section 91.417(a)(1)(ii). (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (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. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. 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. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (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. (29) Removing, checking, and replacing magnetic chip detectors. However, this often becomes a "gotcha" moment for anyone auditing the logbook. [Amdt. 1993, 29 FR 5451, Apr. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 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. Navigate by entering citations or phrases (xv) Main seat support braces and brackets. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. will also bring you to search results. Use the surveillance formats UF = 4 and 5. Acceptable methods include: (1) Record keeping system. 6(c), Dept. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 3. (3) Anti-icing devices - for improper operations and obvious defects. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). 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). (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. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 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. 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. 1993, 29 FR 5451, Apr. [Amdt. The date of completion. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. No. (2) Tag or record attached to part. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 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. According to the FAA, the aircraft owner is right. 43-40, 71 FR 40877, July 14, 2005]. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. FAA-2021-0237; Amdt. Additional performance rules for inspections. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (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. (21) Replacing any hose connection except hydraulic connections. Okta Mobile for end users. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 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. 43-39, 69 FR 44863, July 27, 2004; Amdt. (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. (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. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (xii) Overhaul of controllable pitch propellers. 23, 1964, as amended by Amdt. (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. 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