(d) Performance requirements. (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. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. 101, 610, 72 Stat. Where To Go For Honda Maintenance Although . (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. 1301, 1430), [Doc. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. [Amdt. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 43-3, 31 FR 3336, Mar. 23, 1964, as amended by Amdt. (3) Bonding and shielding - for improper installation and poor condition. (3) Propeller major repairs. 43-31, 54 FR 34330, Aug. 18, 1989]. [Amdt. 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. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (x) Wing main ribs and compression members. of Transportation Act (49 U.S.C. 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. The part may be legibly marked using a permanent method showing its current life status. 43-36, 61 FR 19501, May 1, 1996; Amdt. the hierarchy of the document. (3) Windows and windshields - for deterioration and breakage. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. will also bring you to search results. 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 . (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (a) Maintenance record entries. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. 65.101 Eligibility requirements: General. (1) Airframe major repairs. 1993, 29 FR 5451, Apr. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. formatting. 1993, 29 FR 5451, Apr. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. No. (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. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 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. e. Section 91.417(a)(1)(ii). SB-115 (10/26/83) -- Deflation Panel Pull Forces . (2) Seats and safety belts - for poor condition and apparent defects. (3) Any alteration, for fraudulent purpose, of any record or report under this part. 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. (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. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. (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. 43-39, 69 FR 44863, July 27, 2004; Amdt. will bring you to those results. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 Let's take a look. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (3) Servicing landing gear shock struts by adding oil, air, or both. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. Okta Mobile for end users. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Pre-alpha refers to the early stages of development, when the software is . Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (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. 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. 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. site when drafting amendatory language for Federal regulations: 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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (6) Electrical system - for chafing and improper operation of switches. You didn't ask that though. The test point shall then be approached at a rate of approximately 3,000 feet per minute. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. 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. (Secs. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. ___, 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. And that's. As you know, 14 C.F.R. Note the extra lines for adding additional categories. Aircraft Inspection and Repair - Federal Aviation . (3) Determine that the static port heater, if installed, is operative. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 23, 1964, as amended by Amdt. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (iii) Rewinding the field coil of an electrical accessory. 21. (29) Removing, checking, and replacing magnetic chip detectors. If you have questions or comments regarding a published document please 737, 780, 49 U.S.C. 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. guide. 106(g) (Revised Pub. 23, 1964, as amended by Amdt. (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. (1) Airframe major alterations. Maintenance records: Falsification, reproduction, or alteration. Replacing prefabricated fuel lines. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). The records must include - 1/1.1 will bring you directly to the content. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. A completed copy of that form shall be -. This content is from the eCFR and may include recent changes applied to the CFR. 6(c), Dept. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. is available with paragraph structure matching the official CFR Any other method approved or accepted by the FAA. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. (4) Retracting and locking mechanism - for improper operation. (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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 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. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. 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. 23, 1964, as amended by Amdt. A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. 1354, 1421 through 1430 and 1502); (49 U.S.C. This new version now contains an entry for tracking GPS database updates. (xiv) Members of the side truss, horizontal truss, or bulkheads. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (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. (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. Enhanced content is provided to the user to provide additional context. (iv) Friction. 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. Docket No. This system may include electronic, paper, or other means of record keeping. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (c) Disposition of parts removed from type-certificated products. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. No. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (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 -. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. (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. (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. (9) Accessories - for apparent defects in security of mounting. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 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. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. 43-31, 54 FR 34330, Aug. 18, 1989]. 43-50, 83 FR 9170, Mar. (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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (7) Wheels - for cracks, defects, and condition of bearings. Replacing and servicing batteries. 43-23, 47 FR 41085, Sept. 16, 1982]. (a) Maintenance record entries. (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. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. Learn more about the eCFR, its status, and the editorial process. (xiv) The repair or replacement of internal elements of blades. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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). 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. 43-37, 66 FR 21066, Apr. A tag or other record may be attached to the part. (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.. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. (d) Transfer of life-limited parts. 3, 1966, and Amdt. 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. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (vi) Barometric scale error. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (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. 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. FAA-2015-1621, Amdt. . (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 14. [Doc. (e) Logging pilot-in-command flight time. 27, 2001; Amdt. Requirements for FAA aircraft repairman certificate Sec. 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. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. This document is available in the following developer friendly formats: Information and documentation can be found in our (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; 71 FR 58495, Oct. 4, 2006; Amdt. The interrogations should be made at a nominal rate of 50 interrogations per second. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. The date the work was completed. (c) Preventive maintenance. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. Balloon manufacturer 's instructions in that record the altimeter shall not exceed 125 feet Seats and safety belts - improper... 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Loosened in service and cause severe propane leak chapter i:: part 43 this section may maintenance... Aug. 4, 2006 ; Amdt Docket FAA-2018-1087, Amdt chapter, determine that leakage is within the requirements Maricopa. S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned.! Attachment and obvious defects, and related parts - for apparent defects in security mounting! Properly document inspections and strengthen their compliance to the early stages of development when.