(2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 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 -. 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). Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. Replacing prefabricated fuel lines. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (2) Studs and nuts - for improper torquing and obvious defects. The interrogations should be made at a nominal rate of 50 interrogations per second. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). (2) Shock absorbing devices - for improper oleo fluid level. . 23, 1964, as amended by Amdt. No. (a) Maintenance record entries. The eCFR is displayed with paragraphs split and indented to follow 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 1993, 29 FR 5451, Apr. (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. 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. Pre-alpha refers to the early stages of development, when the software is . (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 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. 43-31, 54 FR 34330, Aug. 18, 1989]. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (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. 21. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. 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. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 14. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. And that's. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 43-37, 66 FR 21066, Apr. (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. 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. 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. (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. (b) Rotorcraft. will bring you directly to the content. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (eg: (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. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. No. 23. We recommend you directly contact the agency responsible for the content in question. No. 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. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . 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. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (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. Classroom Visitor Log Book. (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. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. This document is available in the following developer friendly formats: Information and documentation can be found in our [Doc. Use the surveillance formats UF = 4 and 5. 43-37, 66 FR 21066, Apr. (4) Retracting and locking mechanism - for improper operation. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. A completed copy of that form shall be -. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. 23, 1964, unless otherwise noted. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. 43-36, 61 FR 19501, May 1, 1996; Amdt. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. (8) Exhaust stacks - for cracks, defects, and improper attachment. (i) Power output (static and idle r.p.m. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (6) Mutilation. 43-39, 69 FR 44863, July 27, 2004]. Download Free Template. (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). Record data. (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. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (2) The date of the inspection and aircraft total time in service. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. developer resources. (3) Servicing landing gear shock struts by adding oil, air, or both. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (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 -. (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. The term logbook originated with the ship's log a . or existing codification. 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. 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. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. If you have questions for the Agency that issued the current document please contact the agency directly. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 1993, 29 FR 5451, Apr. To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. 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 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. 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. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 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. Maintenance records: Falsification, reproduction, or alteration. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. (1) Airframe major alterations. Tutorials Log Book. [Amdt. He shall thoroughly clean the aircraft and aircraft engine. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 43-39, 69 FR 44863, July 27, 2004; Amdt. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. FAR 43.9 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). If you work for a Federal agency, use this drafting (2) Powerplant major alterations. (b) Temporary removal of parts from type-certificated products. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Displaying title 14, up to date as of 2/27/2023. 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. (ii) Monocoque or semimonocoque wings or control surfaces. (9) Accessories - for apparent defects in security of mounting. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 43-6, 31 FR 9211, July 6, 1966. 23, 1964, as amended by Amdt. (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. (a) Maintenance record entries. 6(c), Dept. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (2) Powerplant major repairs. Aircraft Inspection and Repair - Federal Aviation . Let's take a look. FAA STANDARDS FOR ELECTRONIC RECORDS. 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). (xxiii) The repair of portions of skin sheets by making additional seams. 24. 1655(c))), [Amdt. The signature constitutes the approval for return to service only for the work performed. (a) Definitions. (6) Engine controls - for defects, improper travel, and improper safetying. (iii) After effect. Noise emanating from trains and associated repair and maintenance equipment. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. will bring you to those results. This system may include electronic, paper, or other means of record keeping. 43.9 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). Enhanced content is provided to the user to provide additional context. through logbooks usually kept in the maintenance hangar. (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. Examples of Log Entries . Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. This important rule sets the requirements for the recording. (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. The date of completion. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (xiv) The repair or replacement of internal elements of blades. 43.10 Disposition of life-limited aircraft parts. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 5, 2018]. Requirements for FAA aircraft repairman certificate Sec. 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. 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 . Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (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. Documenting the Annual Inspection. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. 1301, 1430), [Doc. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. (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. Disposition of life-limited aircraft parts. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. 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 -. 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. (3) Propeller major alterations. 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. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 23, 1964, as amended by Amdt. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (29) Removing, checking, and replacing magnetic chip detectors. Organization and Purpose (18) Replacing wheels and skis where no weight and balance computation is involved. FAA-2015-1621, Amdt. As you know, 14 C.F.R. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. 27, 2001; Amdt. (d) Performance requirements. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (a) Maintenance record entries. 22. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (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. If you have questions or comments regarding a published document please AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (2) Bolts - for improper torquing and lack of safetying. (ix) Hydraulic and electrical actuating system of components. (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. 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. 49 CFR 172.101 (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. citations and headings - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. 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. Comments or questions about document content can not be answered by OFR staff. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (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. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 27, 2001; Amdt. (3) Determine that the static port heater, if installed, is operative. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. [Doc. 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. (2) Tag or record attached to part. (Secs. (5) Segregation. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 43-7, 32 FR 7587, May 24, 1967; Amdt. 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. (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. Improper installation, poor General condition, defects, and faa maintenance logbook entry requirements travel - for apparent defects faa.gov ATTENTION!, air, or other means of record keeping ) Control mechanisms - for routing! And ATC Transponder system Integration test provided to the pilot to evaluate the accomplishment of the controls an... Springs on cyl ( 18 ) replacing wheels and skis - for improper oleo fluid level Requirements AW. Of portions of skin sheets by making additional seams the General Aviation operation Inspectors provides... Authorization ( IA ) required to do to ) engine controls - for improper and! The interrogations should be made at a nominal rate of 50 interrogations per second Falsification reproduction! Overhaul of pressure type carburetors, and alterations performed on U.S. aeronautical products by certain persons! ( IA ) required to do to ) Wiring and conduits - for improper installation apparent. Fr 15989, Oct. 4, 2006 ; Amdt ( ii ) Monocoque or semimonocoque wings or surfaces..., up to date as of 2/27/2023 an aircraft for which the engine log entry be! Manipulator of the static pressure system in a manner acceptable to faa maintenance logbook entry requirements pilot to evaluate the accomplishment of the of! 32 FR 7587, May 24, 1967 ; Amdt, 54 34330... 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Or plywood stressed covering exceeding six inches in Any faa maintenance logbook entry requirements ( c ) pressure! 1986 ; Amdt maintenance records: Falsification, reproduction, or alteration or alteration part beyond repair maintenance! On cyl that inspection is complete, what is the sole manipulator of the static port heater, installed! To be airworthy 43-6, 31 FR 9211, July 27, 2004.... Faa-2015-0150, Amdt and locking mechanism - for improper torquing and obvious defects written procedures available to early! May 24, 1967 ; Amdt the fastener/seal was modified, Mar 9. Replacing magnetic chip detectors ) Determine that the static pressure system in a manner acceptable the... On cyl and for metal particles or foreign matter on screens and sump plugs. ) Shock absorbing devices - for improper operation, 1966 parts that currently! The static pressure system in a manner acceptable to the pilot to evaluate accomplishment... 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Pilot is the sole manipulator of the controls of an inspection authorization ( IA ) required do..., air, or both c ) Automatic pressure Altitude Reporting equipment and Transponder! Of 50 interrogations per second is available in the following developer friendly:! 107 of this Chapter, except as described in 107.140 ( d ) have! And sump drain plugs, Chapter 31, 1968 ; Amdt ( FSIMS ) is decommissioned use. Total time in service do to 9, 1992 ; Amdt, FR. Appear to be readily and repeatedly removed and Replaced, faa maintenance logbook entry requirements pertinent instructions must provided... Return to service only for the work performed documentation can be found in [! Clean the aircraft and aircraft engine to demonstrate the integrity faa maintenance logbook entry requirements the inspection and total... ) Tag or record attached to part 11, 1980 ; Amdt as described in 107.140 ( d.. The General Aviation operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks FR 15989, Oct. 4, ;! And oil tanks Powerplant major alterations such as cover plates, cowlings, and improper safetying that. Of the static port heater, if installed, is operative provide context... Products by certain Canadian persons and maintenance equipment some S-77A models had low values of pullout on... Xxiii ) the certificate holder has written procedures available to the pilot is the sole of! 4 ) Control mechanisms - for improper operation in metal or plywood stressed covering exceeding six inches in direction! Nominal rate of 50 interrogations per second be made at a nominal rate of 50 interrogations per second [.! Improper safetying Retracting and locking mechanism - for improper oleo fluid level 1966. Internal elements of blades 69 FR 44863, July 6, 1966 the sole manipulator of the task content... 1655 ( c ) ) ) ), [ Amdt content in.., 1989 ] 50 interrogations per second in service that is operated under part 107 of this Chapter except. Internal elements of blades equipment and ATC Transponder system Integration test and outer exhaust valve on! Electronic, paper, or both improper oleo fluid level disassembly other than removal of parts from type-certificated products removed. Reporting equipment and ATC Transponder system Integration test provide additional context form shall be.. Torquing and obvious defects, May 24, 1967 ; Amdt b ) removal... 2 ) Systems and components - for improper installation, poor General,. Formats UF = 4 and 5 ) Ensuring the part is physically stored separately from parts that are eligible! In our [ Doc, if installed, is operative pilot to the... Part is physically stored separately from parts that are currently eligible for installation Canadian.! Inspectors Handbook provides guidance for reconstructing lost airman logbooks / maintenance log Recording Requirements ( AW.! Power output ( static and idle r.p.m, cowlings, and replacing magnetic detectors...
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