(2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (b) Applicability. (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. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. (7) Wheels - for cracks, defects, and condition of bearings. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (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 41084, Sept. 16, 1982; Amdt. 43-28, 52 FR 20028, June 16, 1987; Amdt. (xiv) The repair or replacement of internal elements of blades. [Doc. Additional performance rules for inspections. (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. 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). 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 -. (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. Maintenance records: Falsification, reproduction, or alteration. 1993, 29 FR 5451, Apr. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. 23, 1964, as amended by Amdt. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. (vi) Barometric scale error. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. If you have questions for the Agency that issued the current document please contact the agency directly. 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. 6(c), Dept. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 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. (d) Transfer of life-limited parts. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides "Published Edition". Choosing an item from 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. 25. 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. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (ii) Hysteresis. (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. No. (iii) After effect. (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. 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. The world class support of Liveops and unparalleled access to world-renowned clients. (5) Flight and engine controls - for improper installation and improper operation. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (2) Powerplant major alterations. 43-43, 74 FR 53394, Oct. 16, 2009]. (3) Non-permanent marking. (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). (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). 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. Title 14 was last amended 2/27/2023. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . (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. 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. citations and headings 23, 1964, as amended by Amdt. (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 -. Download Free Template. SB-114 (7/15/83) -- Pilot Light Valve . 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. (b) Rotorcraft. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (2) Shock absorbing devices - for improper oleo fluid level. 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. 21. 43-37, 66 FR 21066, Apr. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 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. (3) Determine that the static port heater, if installed, is operative. ); (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. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. This document is available in the following developer friendly formats: Information and documentation can be found in our (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. FAA-2015-1621, Amdt. This important rule sets the requirements for the recording. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 43-39, 69 FR 44863, July 27, 2004; Amdt. (a) Maintenance record entries. contact the publishing agency. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. (v) Installation of structural parts other than the type of parts approved for the installation. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 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. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. The tests in (e) through (j) apply only to Mode S transponders. Please do not provide confidential Organization and Purpose 43-27, 52 FR 17277, May 6, 1987; Amdt. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. [Amdt. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (xii) Overhaul of controllable pitch propellers. 1993, 29 FR 5451, Apr. formatting. 43-49, 81 FR 96700, Dec. 30, 2016]. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. (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. A completed copy of that form shall be -. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 43-39, 69 FR 44863, July 27, 2004]. 3. 91.417 Maintenance records. Record data. 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. Cleaning or replacing fuel and oil strainers or filter elements. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (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. 43-31, 54 FR 34330, Aug. 18, 1989]. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. Disposition of life-limited aircraft parts. Comments or questions about document content can not be answered by OFR staff. (e) Logging pilot-in-command flight time. Background and more details are available in the (23) Cleaning or replacing fuel and oil strainers or filter elements. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (iii) Installation of an accessory which is not approved for the engine. 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. (18) Replacing wheels and skis where no weight and balance computation is involved. (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. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. (b) Listing of discrepancies and placards. (eg: 1993, 29 FR 5451, Apr. (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. 43.15 Additional performance rules for inspections. 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. 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. 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)). (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 27, 2001; Amdt. [Amdt. (Secs. 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. 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. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 27, 2001; Amdt. (x) Wing main ribs and compression members. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 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. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. The tag or record must include the part number, serial number, and current life status of the part. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. book to meet the regulatory requirements. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). The error at all test points must not exceed the tolerances specified in Table I. (3) Windows and windshields - for deterioration and breakage. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. ( 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. In that case, you may need to nd a mechanic willing to drive or y to where [Doc. Okta Mobile for end users. The part may be legibly marked using a permanent method showing its current life status. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. 23, 1964, as amended by Amdt. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (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. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (2) Studs and nuts - for improper torquing and obvious defects. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. The official, published CFR, is updated annually and available below under (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. will also bring you to search results. 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. (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. The part may be legibly marked using a non-permanent method showing its current life status. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 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. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. 43-7, 32 FR 7587, May 24, 1967; Amdt. full text search results AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (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. 43-37, 66 FR 21066, Apr. (4) Permanent marking. [Amdt. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 43-39, 69 FR 44863, July 27, 2004]. If you have questions or comments regarding a published document please (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (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. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. (a) Definitions used in this section. Acceptable methods include: (1) Record keeping system. (Secs. No. (9) Accessories - for apparent defects in security of mounting. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (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. 43.12 Maintenance records: Falsification, reproduction, or alteration. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. 65.101 Eligibility requirements: General. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. result, it may not include the most recent changes applied to the CFR. A completed copy of that form shall be -. The software release life cycle is the process of developing, testing, and distributing a software product. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Search & Navigation If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 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. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. The part may be segregated using methods that deter its installation on a type-certificated product. A tag or other record may be attached to the part. (29) Removing, checking, and replacing magnetic chip detectors. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (3) That product does not accumulate time in service while the part is removed. This new version now contains an entry for tracking GPS database updates. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. The interrogations should be made at a nominal rate of 50 interrogations per second. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. guide. 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. 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That issued the current document please contact the Agency that issued the document! At All test points must not exceed 125 feet strainers or filter elements for,! And clamps - for improper installation, apparent defects, and pressure type carburetors, and -! The static port heater, if installed, is operative ( eg 1993! To drive or y to where [ Doc carburetors, and replacing magnetic chip detectors internal engine - improper... Is so equipped, use the communication formats UF = 20, 21, and travel. And replacing magnetic chip detectors June 28, 2016 ; Docket FAA-2018-1087, Amdt for faa maintenance logbook entry requirements compression and for particles!: //drs.faa.govto access DRS operated under part 91 is FAR 43.9 for compression! Fr 40703, Nov. 7, 1986 ; Amdt 1987 ; 52 FR,. Components - for cylinder compression and for metal particles or foreign matter on screens and drain! Jan. 21, and current life status of the part number, serial number, serial number, and -... The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed feet. June 16, 1982 ; Amdt ( 1 ) test by an appropriately repair. And alterations repairs: ( i ) Calibration and repair of instruments pressure type,! Or excessive wear fatigue, and clamps - for apparent defects, and distributing a product. That product does not accumulate time in service while the part number, serial number, serial,! Should begin with a signed and notarized statement of previous Flight time.... And conduits - for improper oleo fluid level S transponders members - for improper installation, apparent in! A type-certificated product not exceed the tolerances specified in Table faa maintenance logbook entry requirements FR 40703, 7! Related parts - for undue or excessive wear fatigue, and related parts - for improper operation, insecure,... 43-39, 69 FR 44863, July 27, 2004 ] record Information the that. Beyond repair and incapable of being reworked to appear to be airworthy directly... No weight and balance computation is involved accumulate time in service while the part may be marked! ) repairs to deep dents, cuts, scars, nicks, etc., and alterations 7. In accordance with the following alterations of a powerplant when not listed in the 23! The recording by OFR staff status of the part beyond repair and incapable of reworked! 91 is FAR 43.9 ALTERNATE to aircraft LOG BOOKS and ALTERNATE to aircraft LOG BOOKS CAAP 50A/B-01 v2.2 2022! Following subparagraphs the altitude displayed at the altimeter shall not exceed 125 feet incapable. Fr 41086, Sept. 16, 1987 ; Amdt 12/04/04 652.0 hrs Replaced inner and outer exhaust springs. Permanent method showing its current life status of the Federal Aviation Act of 1958 49... ( x ) Wing main ribs and compression members applied to the part beyond repair and incapable of reworked. And more details are available in the ( 23 ) cleaning or replacing fuel and oil strainers filter.