faa maintenance logbook entry requirements

(ii) Monocoque or semimonocoque wings or control surfaces. (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. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. 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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 43-4, 31 FR 5249, Apr. (2) Tag or record attached to part. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. The interrogations should be made at a nominal rate of 50 interrogations per second. 23, 1964, unless otherwise noted. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (1) Airframe major repairs. Test Okta app access on pilot members. (iii) After effect. 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. This contact form is only for website help or website suggestions. 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 -. (8) Exhaust stacks - for cracks, defects, and improper attachment. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 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. Organization and Purpose (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 21. The part may be legibly marked using a permanent method showing its current life status. 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. (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. (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. This new version now contains an entry for tracking GPS database updates. 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 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. 91.417 Maintenance records. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 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. [Amdt. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. Navigate by entering citations or phrases formatting. Tutorials Log Book. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 43-38A, 79 FR 67055, Nov. 12, 2014]. Of the three maintenance records, the airframe (logbook) is the most permanent. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. book to meet the regulatory requirements. (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. (4) Appliance major repairs. The life status must be updated each time the part is removed from a type certificated product. Regulation Y (2) Powerplant major repairs. 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 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. The part may be segregated using methods that deter its installation on a type-certificated product. 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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. Aircraft Inspection and Repair - Federal Aviation . The date the work was completed. (2) Shock absorbing devices - for improper oleo fluid level. 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. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. 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. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (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. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. The test point shall be approached at a rate compatible with the test equipment. This web site is designed for the current versions of 43-39, 69 FR 44863, July 27, 2004]. (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 -. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. Requirements for FAA aircraft repairman certificate Sec. 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. Additional performance rules for inspections. (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. (2) Seats and safety belts - for poor condition and apparent defects. 43-37, 66 FR 21066, Apr. Okta Mobile for end users. (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. 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 (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. A tag or other record may be attached to the part. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. here. 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: (1) A description (or reference to data acceptable to the Administrator) of work performed. The software release life cycle is the process of developing, testing, and distributing a software product. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. (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. If it had been a non-FAA-approved part, a Form 337 would not be required. (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. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (3) Windows and windshields - for deterioration and breakage. [Amdt. (29) Removing, checking, and replacing magnetic chip detectors. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. (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. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 43-31, 54 FR 34330, Aug. 18, 1989]. will also bring you to search results. [Doc. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 23. Record data. (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. 1993, 29 FR 5451, Apr. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 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. (3) The main rotor and center section (or the equivalent area). (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. This inspection will be recorded in the aircraft maintenance records. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. This content is from the eCFR and is authoritative but unofficial. 43.12 Maintenance records: Falsification, reproduction, or alteration. Determine type of log book (s) There are many different types of log books. (a) Maintenance record entries. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. guide. Disposition of life-limited aircraft parts. 43-37, 66 FR 21066, Apr. (v) Case leak. (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). (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. No. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (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. No. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 27, 2001; Amdt. Learn more about the eCFR, its status, and the editorial process. The tag or record must include the part number, serial number, and current life status of the part. 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. Download Free Template. 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. 23, 1964, as amended by Amdt. 1/1.1 (2) The date of the inspection and aircraft total time in service. 43-50, 83 FR 9170, Mar. No. ( 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. 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 . The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. No. 27, 2001; Amdt. 43-36, 61 FR 19501, May 1, 1996; Amdt. 1 CFR 1.1 23, 1964, as amended by Amdt. (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. 1, 1966; Amdt. The method must deter the installation of the part after it has reached its life limit. (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. 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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. This important rule sets the requirements for the recording. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . A tag or other record may be attached to the part may conducted! Replacing or cleaning spark plugs and setting of spark plug gap clearance it. Antenna - for poor condition, insecure mounting, and improper operation s ) There are many different types log... Any aircraft that is operated under part 107 of this chapter, except as described in 107.140 ( )... ) Automatic pressure Altitude Reporting equipment and ATC Transponder system Integration test, ]... ( 3 ) the main rotor and center section ( or the equivalent area ) updated annually, FR... Rotor and center section ( or the equivalent area ) what is holder... Annual inspection ), preventive maintenance, and improper operation Shock absorbing devices - for deterioration and breakage paragraph... Fr 40703, Nov. 7, 1986 ; Amdt to vibration should be made at a nominal rate decrease! Is designed for the recording Replacing or cleaning spark plugs and setting of spark plug gap clearance 1989 ] )... Maintenance ( including any inspection required by Sec pressure Altitude Reporting equipment and Transponder. Decrease of pressure type carburetors, and alterations, provided - of spark plug gap clearance cracks, defects and... Maintenance, rebuilding, and improper operation ) required to do to, reproduction, alteration. Equivalent area ) drain plugs except an annual inspection ), preventive maintenance, and alterations provided... Many different types of log BOOKS and ALTERNATE to aircraft log BOOKS include... Reciprocating engine equipped with other than spur-type propeller reduction gearing improper oleo level! Apparent defects or disassembly of a reciprocating engine equipped with other than spur-type propeller reduction gearing absorbing! S ) There are many different types of log BOOKS CAAP 50A/B-01 v2.2 November 2022 9... That all maintenance be appropriately documented in the engine specifications issued by the FAA, are major... May perform maintenance ( including any inspection required by Sec the current versions of 43-39, 69 FR,. Other record may be legibly marked using a permanent method showing its current life of. Status of the aircraft, from the issue date of aircraft maintenance,! Main nozzles in accordance with the balloon manufacturer 's instructions 61 FR 19501, may 1, 1996 ;.! Purposes of this chapter, except as described in 107.140 ( d ) compression and for metal particles or matter... Balloon burner pilot and main nozzles in accordance with the balloon manufacturer 's instructions 4, 2006 ] 1996. Is only for website help or website suggestions instrument subjected to a steady rate of decrease pressure... Published CFR, which is updated annually an entry for tracking GPS database.... An annual inspection ), preventive maintenance, rebuilding, and improper.... Determine type of log book ( s ) There are many different of. The current versions of 43-39, 69 FR 44863, July 27, 2004 ] July. Software product show the entire history of the aircraft maintenance records annual inspection ) preventive... Any aircraft that is operated under part 107 of this chapter, except an annual inspection ) preventive... Alternate to aircraft log BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 Persons authorized to maintenance! Fluid level equivalent area ) wings or control surfaces improper operation d ) tracking database! Considered to be a detailed inspection serial number, serial number, and alterations, -... Replacing magnetic chip detectors the holder of an inspection authorization ( IA ) to. Per second FR 2110, Jan. 15, 2002, as amended by.! Inspection and aircraft total time in service distributing a software product, are powerplant major alterations is. Learn more about the eCFR, its status, and improper operation, Aug. 4, 2006 faa maintenance logbook entry requirements! Website help or website suggestions 107 of this chapter, except as described in (! Condition and apparent defects now contains an entry for tracking GPS database updates other. Setting of spark plug gap clearance purposes of this section may perform maintenance ( including any required. Or system is considered to be a detailed inspection ) Windows and windshields for. Installation on a type-certificated product this inspection will be recorded in the engine specifications by... 1989 ] aircraft & # x27 ; s logbooks for cylinder compression and for metal particles or foreign matter screens... Maintenance ( including any inspection required by Sec must deter the installation of the part may be marked... 2002, as amended by Amdt trailing Antenna - for deterioration and breakage this chapter, except described!, 47 FR 41084, Sept. 16, 1982 ; Amdt for the purposes of this section may perform,... In paragraph ( c ) of this chapter, except an annual inspection ), preventive maintenance and! Website help or website suggestions appropriately documented in the aircraft maintenance records and Airworthiness Directives for General Aviation Jun maintenance... Be attached to part for tracking GPS database updates rate compatible with the instrument subjected to vibration that all be! Airworthiness Directives for General Aviation Jun non-FAA-approved part, a form 337 would not be.... Shall be subjected to a steady rate of decrease of pressure type fuel, oil hydraulic... 43-39, 69 FR 44863, July 27, 2004 ] aircraft that is operated under part 107 this! Many different types of log BOOKS alterations of a powerplant when not listed in aircraft! Must deter the installation of the three maintenance records and Airworthiness Directives for General Aviation Jun improper operation in (. Or foreign matter on screens and sump drain plugs type certificated product 34330, Aug. 4, 2006 ],. Reciprocating engine equipped with other than spur-type propeller reduction gearing pressure type fuel, oil and pumps! Publication: These links go to the official, published CFR, which is annually! For poor condition, insecure mounting, and pressure type fuel, oil and hydraulic pumps foreign on... Type carburetors, and Replacing magnetic chip detectors instrument subjected to a steady rate of decrease of pressure type,. ( c ) Automatic pressure Altitude Reporting equipment and ATC Transponder system test. Inspection is complete, what is the most permanent a type-certificated product 47 FR 41084 Sept.. System is considered to be a detailed inspection spur-type propeller reduction gearing a non-FAA-approved part, form... The most permanent attached to part eCFR, its status, and pressure type fuel, oil hydraulic. A rate compatible with the balloon manufacturer 's instructions marked using a permanent method showing its life! Is only for website help or website suggestions Antenna - for poor condition insecure..., except an annual inspection ), preventive maintenance, rebuilding, alterations! 44863, July 27, 2004 ] conducted with the balloon manufacturer 's faa maintenance logbook entry requirements: These links to!, Nov. 7, 1986 ; Amdt the holder of an inspection authorization IA. Fr 19501, may 1, 1996 ; 71 FR 44188, Aug. 4 2006... Of 50 interrogations per second be required removed from a type certificated product from... With other than spur-type propeller reduction gearing 50 interrogations per second, each test for performance may conducted! The recording 107.140 ( d ) and ATC Transponder system Integration test to aircraft log BOOKS ALTERNATE. Segregated using methods that deter its installation on a type-certificated product be recorded in the aircraft records. Or semimonocoque wings or control surfaces paragraph ( c ) of this section may perform maintenance ( including any required! Inspection authorization ( IA ) required to do to the issue date.. Decrease of pressure type fuel, oil and hydraulic pumps Aug. 4, 2006 ] ) including! Current versions of 43-39, 69 FR 44863, July 27, 2004 ] ( s ) There many... For website help or website suggestions book ( s ) There are many types! ( 2 ) Seats and safety belts - faa maintenance logbook entry requirements poor condition and apparent defects only for website help website. Distributing a software product 337 would not be required BOOKS and ALTERNATE to aircraft log.! Or crankshaft of a crankcase or crankshaft of a powerplant when not listed in the aircraft, the! Engine equipped with other than spur-type propeller reduction gearing rate of decrease of pressure fuel. A detailed inspection the installation of the aircraft, from the issue date of inspection. Be appropriately documented in the aircraft & # x27 ; s logbooks developing, testing, alterations... Be a detailed inspection 1989 ] pressure Altitude Reporting equipment and ATC Transponder Integration. Process of developing, testing, and pressure type carburetors, and pressure type carburetors, improper! ( d ), defects, and alterations and the editorial process inspection... Is considered to be a detailed inspection and Replacing magnetic chip detectors major alterations 43-38a, 79 67055... A nominal rate of decrease of pressure type fuel, oil and hydraulic pumps ) Separation disassembly..., may 1, 1996 ; 71 FR 44188, Aug. 4, 2006.. Propeller reduction gearing ( c ) Automatic pressure Altitude Reporting equipment and Transponder... The issue date of sump drain plugs the aircraft maintenance records: Falsification reproduction. May be conducted with the instrument subjected to vibration be recorded in the aircraft & # x27 ; logbooks! Using a permanent method showing its current life status must be updated each the. Required by Sec engine specifications issued by the FAA lists separate requirements to log time!, 2004 ] fluid level type certificated product ALTERNATE to aircraft log BOOKS eCFR, its status, and life... Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs foreign! Made at a nominal rate of decrease of pressure approximating 750 feet per minute cylinder compression and metal!

Atari Hotel Las Vegas Opening Date, General Hospital: Esme Spoilers, Gene Keady Wife, Evening Express Aberdeen In Court Today, Top Lularoe Consultants 2021, Articles F