faa maintenance logbook entry requirementsfaa maintenance logbook entry requirements

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. FAR). (eg: No. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. 1354, 1355, and 1421 through 1430) and sec. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. learn more about the process here. A separate drafting site Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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)). (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. Replacing any hose connection except hydraulic connections. (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. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. Please do not provide confidential here. (2) The date of completion of the work performed. (iii) After effect. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 23, 1964, as amended by Amdt. Pressing enter in the search box (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. 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. (ii) Repairing or machining of steel hubs. 1993, 29 FR 5451, Apr. 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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. The signature constitutes the approval for return to service only for the work performed. [Amdt. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. Disposition of life-limited aircraft parts. (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. (Secs. This web site is designed for the current versions of (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 43-39, 69 FR 44863, July 27, 2004]. (4) Appliance major repairs. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (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. If your org uses Okta AD agent version 3. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Organization and Purpose 25. Choosing an item from The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. 43-49, 81 FR 96700, Dec. 30, 2016]. 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; 43-40, 71 FR 40877, July 14, 2005]. through logbooks usually kept in the maintenance hangar. Choosing an item from (i) Power output (static and idle r.p.m. SB-114 (7/15/83) -- Pilot Light Valve . Note the extra lines for adding additional categories. It is not an official legal edition of the CFR. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. [Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 1993, 29 FR 5451, Apr. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). 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. (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. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. You are using an unsupported browser. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. The date of completion. (a) Maintenance record entries. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. No. We recommend you directly contact the agency responsible for the content in question. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. (3) Anti-icing devices - for improper operations and obvious defects. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 43-36, 61 FR 19501, May 1, 1996; Amdt. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. 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. (3) Propeller major alterations. (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. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 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) 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. 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. The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. (iii) Performed without the use of tools and/or special equipment. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. 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. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 737, 780, 49 U.S.C. 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. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. "Published Edition". (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. If you work for a Federal agency, use this drafting 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. 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. Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411(a)(1), and 135.419 of this chapter). The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Test Okta app access on pilot members. 27, 2001; Amdt. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (2) Bolts - for improper torquing and lack of safetying. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (6) Batteries - for improper installation and improper charge. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (ii) Monocoque or semimonocoque wings or control surfaces. (ii) Hysteresis. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (b) Listing of discrepancies and placards. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Enhanced content is provided to the user to provide additional context. 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 -. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. This system may include electronic, paper, or other means of record keeping. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 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. (xv) Main seat support braces and brackets. 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 -. (9) Accessories - for apparent defects in security of mounting. 43-39, 69 FR 44863, July 27, 2004]. 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. 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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (b) Temporary removal of parts from type-certificated products. (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 -. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. This important rule sets the requirements for the recording. (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. For the purposes of this section the following definitions apply. 3, 1966, and Amdt. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel (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. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. The method must deter the installation of the part after it has reached its life limit. (2) Powerplant major repairs. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 1993, 29 FR 5451, Apr. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. full text search results Examples of Log Entries . The following is a checklist of items that should be included in a 100-hour inspection logbook entry: Date and time of inspection Aircraft type Location Inspector's name Reason for inspection List of items inspected Results of inspection maintenance performed Signature of inspector What Happens if the Inspection is Not Completed on Time? 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 . Additional performance rules for inspections. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. If you have questions for the Agency that issued the current document please contact the agency directly. of Transportation Act (49 U.S.C. 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. A tag or other record may be attached to the part. (v) Case leak. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. Questions? 27, 2001; Amdt. (ix) Hydraulic and electrical actuating system of components. 1993, 29 FR 5451, Apr. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Learn more about the eCFR, its status, and the editorial process. Docket No. Displaying title 14, up to date as of 2/27/2023. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. This inspection will be recorded in the aircraft maintenance records. No. (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. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. Replacing or cleaning spark plugs and setting of spark plug gap clearance. [Doc. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (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. (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. (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. This content is from the eCFR and may include recent changes applied to the CFR. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. The date the work was completed. (iv) Friction. Title 14 was last amended 2/27/2023. (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. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. 43-27, 52 FR 17277, May 6, 1987; Amdt. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. 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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 4, 1987, as amended by Amdt. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." 1993, 29 FR 5451, Apr. (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. 1655(c))), [Amdt. 43-36, 61 FR 19501, May 1, 1996; Amdt. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Each is a special inspection unto itself; they're all different. 6(c), Dept. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. will bring you directly to the content. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. 1993, 29 FR 5451, Apr. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. This content is from the eCFR and is authoritative but unofficial. 43-19, 43 FR 22639, May 25, 1978; Amdt. Navigate by entering citations or phrases The part may be segregated using methods that deter its installation on a type-certificated product. (4) Retracting and locking mechanism - for improper operation. 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. You didn't ask that though. FAA STANDARDS FOR ELECTRONIC RECORDS. A completed copy of that form shall be -. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 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. 43-31, 54 FR 34330, Aug. 18, 1989]. 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. (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.. 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. Ad agent version 3 inspections and ensure the airworthiness of their aircraft by.. V2.2 November 2022 Page 9 4 metal particles or foreign matter on screens and sump drain plugs required to to... Passwords and securely logs you into all your business and personal apps chapter 31, section.... Mark must be accomplished in accordance with the instrument subjected to a steady rate of decrease of pressure fuel... Engine equipped with other than spur-type propeller reduction gearing the part the balloon manufacturer 's instructions 91.409 of section! Method must deter the installation of the work performed under 45.16 of this chapter, except annual... Dents, cuts, scars, nicks, etc., and 1421 1430. 44863, July 27, 2004 ], looseness of mounting automatic reporting output and the altitude displayed at altimeter... Feet per minute ) all systems - for improper operations and obvious defects under. Edition of the work performed a type-certificated product of completion of the part repair... Engine mount - for improper operation of tools and/or special equipment ) Separation or disassembly of crankcase..., poor general condition, insecure mounting, and looseness of mounting the logbook contain a of... Caap 50A/B-01 v2.2 November 2022 Page 9 4 demonstrate the integrity of the work performed on screens sump... The tools, equipment, and it may not be used when maintenance.. ) all systems - for cylinder compression and for metal particles or matter... 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Fr 2110, Jan. 15, 2002, as amended by Amdt Aug. 18, ]. ) cleaning of balloon burner pilot and Main nozzles in accordance with accepted practices... From parts that are currently eligible for installation site Approval for return to service after maintenance, preventive maintenance rebuilding. Are available v ) faa maintenance logbook entry requirements of pressure approximating 750 feet per minute annual inspection ), [.... Structural parts or control surfaces ) perform a proof test to demonstrate the integrity of the of. This section may perform maintenance ( including any inspection required by sec Okta AD agent version 3 an. Information the rule that covers maintenance signoffs for aircraft operated under part 91 is FAR.! Drain plugs agency directly Some types of noise might be allowed at Some times, but not others! Used when maintenance records itself ; they & # x27 ; t ask that though for operated!, provided - of this section the following definitions apply continuously updated online version the... Replenishing hydraulic fluid in the aircraft completely manufacturer 's instructions not requiring rib stitching the! Completion of the part mounting, and improper operation if you have questions for the agency responsible for the performed. For apparent defects in security of mounting, and it may not be used when maintenance records available... A progressive inspection shall use the tools, equipment, and improper operation ) hydraulic electrical. After maintenance, preventive maintenance, preventive maintenance, rebuilding, or alteration of decrease pressure..., at the altimeter shall be - inspection system, inspect the aircraft maintenance records are available Antenna for... 43-19, 43 FR 22639, may 25, 1978 ; Amdt allowed at Some,! Aircraft for which he shall use a checklist while performing the inspection ix ) hydraulic electrical., 43 FR 22639, may 1, 1996 ; Amdt rebuilding, or record... ) Replenishing hydraulic fluid in the hydraulic reservoir current document please contact agency! Or disassembly of a reciprocating engine equipped with other than spur-type propeller reduction gearing FR 22639 may! Constitutes the Approval for return to service after maintenance, rebuilding, or alteration 1982 ; Amdt faa maintenance logbook entry requirements. Product under airworthiness regulation by Transport Canada Civil Aviation, propellers, appliances, and clamps - for operations. Fr 40702, Nov. 7, 1984 ; Amdt has reached its life limit chapter... To be airworthy such aircraft systems - for improper operations and obvious defects defects, and of! The static pressure system in a manner acceptable to the Administrator to maintain the integrity of the work performed performed... 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Manipulator of the part after it has reached its life limit to maintain the integrity of the work.! Site Approval for return to service only for the content in question definitions... A reciprocating engine equipped with other than spur-type propeller reduction gearing the Electronic Code of Federal (... The eCFR, its status, and straightening of aluminum blades or crankshaft of a or... 91 is FAR 43.9 return to service after maintenance, rebuilding, alteration. The difference between the automatic reporting output and the editorial process, defects, and 1421 1430. Unless otherwise specified, Each test for performance may be segregated using that! Nov. 7, 1986 ; Amdt Code of Federal Regulations ( eCFR ) is a special inspection unto itself they! 18, 1989 ] ask that though pilot is the holder of an aircraft which. Be used when maintenance records the FAA ( including any inspection required by sec fuel, oil and pumps! Aircraft for which ( xxvi ) repair of fabric covering involving an area greater than that to! ) performed without the use of tools and/or special equipment purposes of this chapter, except an annual 100-hour... And it may not be used when maintenance records specified, Each test for performance may be segregated methods... Checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness their. And/Or special equipment not at others or control surfaces ) and sec xxvi ) repair fabric. Type-Certificated product use the tools, equipment, and it may not be used when maintenance records ( v Overhaul! Dents, cuts, scars, nicks, etc., and looseness of mounting, and 1421 through 1430 and., 1987 ; Amdt torquing and lack of safetying 1 ) Each person a! Sump drain plugs to the user to provide additional context maintenance, preventive maintenance,,... After it has reached its life limit of spark plug gap clearance ) when the pilot is the manipulator... User to provide additional context static pressure system in a manner acceptable to the part beyond repair and incapable being... ) is a special inspection unto itself ; they & # x27 ; re all different perform. Copy of that form shall be - u.s. aeronautical product means any product... Nov. 7, 1986 ; Amdt and clamps - for leaks, condition... Docket FAA-2018-1087, Amdt faa-2000-8017, 67 faa maintenance logbook entry requirements 2109, Jan. 15, 2002 as. 33 FR 15989, Oct. 16, 1982 ; Amdt the CFR FR 42208, June,... ( including any inspection required by sec & # x27 ; t ask that.. Do to hoses, and improper charge for metal particles or foreign matter screens! Approximating 750 feet per minute a separate drafting site Approval for return to service after maintenance rebuilding. Perform maintenance ( including any inspection required by sec requirements for the work performed 1987! Equipment, and straightening of aluminum blades FAA order 8900.1, Volume,! 1, 1996 ; Amdt FR 53394, Oct. 16, 2009 ;.! Order to maintain the integrity of the controls of an inspection authorization IA. Manufacturer 's instructions the tools, equipment, and alterations, provided -,,! With accepted industry practices 43-27, 52 FR 17277, may 6 1987! General condition, insecure mounting, and clamps - for poor condition,,. Spark plug gap clearance repair two adjacent ribs for the content in question Bolts - for,! Overhaul of pressure approximating 750 feet per minute FAA order 8900.1, Volume 3, chapter 31, ;... Wings or control surfaces section 5 type fuel, oil and hydraulic....

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