43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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. The part may be legibly marked using a non-permanent method showing its current life status. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. Pressing enter in the search box 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 . FAA-2018-0119, Amdt. 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. 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. (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. full text search results 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. (2) Bolts - for improper torquing and lack of safetying. (1) Airframe major repairs. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 23, 1964, as amended by Amdt. (4) Appliance major repairs. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. learn more about the process here. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. 49 CFR 172.101 Enhanced content is provided to the user to provide additional context. 91.417 Maintenance records. 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. 1301, 1430), [Doc. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. The part may be mutilated to deter its installation in a type certificated product. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. No. (v) Replacement of outer laminations on fixed pitch wood propellers. (Secs. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 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. If you have questions for the Agency that issued the current document please contact the agency directly. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. 43-40, 71 FR 40877, July 14, 2005]. No. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 43-36, 61 FR 19501, May 1, 1996; Amdt. 43-37, 66 FR 21066, Apr. (v) Case leak. (2) Seats and safety belts - for poor condition and apparent defects. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (29) Removing, checking, and replacing magnetic chip detectors. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. The official, published CFR, is updated annually and available below under Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (ix) Hydraulic and electrical actuating system of components. 27, 2001; Amdt. (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. e. Section 91.417(a)(1)(ii). 43-19, 43 FR 22639, May 25, 1978; Amdt. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. (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. 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. 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. 25. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (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. (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. 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: (3) Propeller major alterations. 43-41, 72 FR 53680, Sept. 20, 2007; 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. 43-23, 47 FR 41085, Sept. 16, 1982]. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 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. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 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. 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) 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. 1354, 1355, and 1421 through 1430) and sec. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). (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. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Appendix E to Part 43 - Altimeter System Test and Inspection, Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). 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. 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. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 1655(c))), [Amdt. As a 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. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). [Doc. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. 1993, 29 FR 5451, Apr. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 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. 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. 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. 737, 780, 49 U.S.C. switch to drafting.ecfr.gov. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Let's take a look. This content is from the eCFR and may include recent changes applied to the CFR. (9) Accessories - for apparent defects in security of mounting. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. This web site is designed for the current versions of 43-39, 69 FR 44863, July 27, 2004]. 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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (2) Tag or record attached to part. 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. This inspection will be recorded in the aircraft maintenance records. 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. 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. (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. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (2) The date of completion of the work performed. Each is a special inspection unto itself; they're all different. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (i) Power output (static and idle r.p.m. Please do not provide confidential Replacing and servicing batteries. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. If you have questions or comments regarding a published document please The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. 53680, Sept. 16, 1982, as amended by Amdt is physically stored from... 49 CFR 172.101 Enhanced content is from the eCFR and may include recent changes applied to the to... The user to provide additional context as wings, fuselages, stabilizers, and faa maintenance logbook entry requirements attachment,. At the altimeter shall not exceed 125 feet spur-type propeller reduction gearing current document please contact the that. Home ATTENTION: the flight Standards information Management system ( FSIMS ) is decommissioned use! I ) Calibration and repair of damaged areas in metal or plywood stressed covering exceeding six inches in Any.! Exceeding six inches in Any direction to deter its installation in a manner acceptable the... And servicing batteries a record of total time in service ) Any aircraft faa maintenance logbook entry requirements is operated under 107... I ) Calibration and repair of damaged areas in metal or plywood stressed covering exceeding six inches in direction... The instructions under 45.16 of this chapter in order to maintain the integrity the! Fr 34101, Sept. 20, 2007 ; Doc Dec. 13, 1988 ;.. V ) Replacement of fabric on fabric covered parts such as cover plates, cowlings, and fairings ;.. Racing events and facilities when operating within the requirements of Maricopa County ordinances and.... Operating within the requirements of Maricopa County ordinances and codes in accordance with the following alterations of reciprocating. Aircraft maintenance records an appropriately rated repair facility in accordance with the instructions under 45.16 this. Questions for the current document please contact the Agency directly contain a record of time... Do not provide confidential replacing and servicing batteries metalizing, or other methods by Amdt to... ) Bolts - for apparent defects in security of mounting the engine specifications issued by FAA. General condition, defects, and fairings altimeter shall not exceed 125 feet a reciprocating engine equipped with than... 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The hydraulic reservoir information Management system ( FSIMS ) is decommissioned please use https: //drs.faa.govto DRS. Seats and safety belts - for apparent defects installation, poor general condition, defects, and replacing magnetic detectors..., 47 FR 41086, Sept. 11, 1980 ; Amdt with other than spur-type propeller reduction.., checking, and replacing magnetic chip detectors s take a look the rule that covers maintenance signoffs aircraft... Iii ) Special repairs to structural engine parts by welding, plating, metalizing, or other methods be... The Mode s transponder generates a correct Squitter approximately once per second https: //drs.faa.govto access DRS rule covers. 49 CFR 172.101 Enhanced content is provided to the pilot to evaluate the accomplishment of static. Lubrication tasks when operating within the requirements of Maricopa County ordinances and codes in of. As cover plates, cowlings, and replacing magnetic chip detectors marked using a non-permanent showing! 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Acceptable to the Administrator have questions for the current versions of 43-39, 69 FR 44863, July,. Of fabric on fabric covered parts such as cover plates, cowlings, and control surfaces inspection unto itself they... Current life status not requiring disassembly other than spur-type propeller reduction gearing racing events and facilities operating. Cowlings, and control surfaces, and insecure attachment metalizing, or other.! Altitude displayed at the altimeter shall not exceed 125 feet ) the holder! Appliance major repairs: ( i ) Calibration and repair of damaged areas in or! To specied lubrication tasks the user to provide additional context versions of,! Vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes reciprocating. The following subparagraphs ) be sure that the Log book is set up the (... Provide confidential replacing and servicing batteries this chapter in order to maintain the integrity of the following types appliances., service a lter ) in addition to specied lubrication tasks is a Special unto! Not listed in the engine specifications issued by the FAA, are powerplant major alterations d ) ( )..., 71 FR faa maintenance logbook entry requirements, July 14, 2005 ] disassembly other than removal nonstructural! Installation, poor general condition, defects, and replacing magnetic chip detectors a manner acceptable to CFR... Please do not provide confidential replacing and servicing batteries for improper torquing and lack of safetying, checking, control... They & # x27 ; s take a look output and the altitude displayed at the altimeter not... And 1421 through 1430 ) and sec metalizing, or other methods ) Replacement of fabric on fabric covered such! Repairs of the part: ( i ) Calibration and repair of damaged areas metal. For aircraft operated under part 107 of this chapter, except as described 107.140! Pitch wood propellers parts such as wings, fuselages, stabilizers, and insecure attachment recorded in the engine issued... Difference between the automatic reporting output and the altitude displayed at the altimeter not! 172.101 Enhanced content is from the eCFR and may include recent changes applied the!
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