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. 65.101 Eligibility requirements: General. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (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. (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. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. SB-114 (7/15/83) -- Pilot Light Valve . (4) Appliance major alterations. 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. The method must deter the installation of the part after it has reached its life limit. 23, 1964, as amended by Amdt. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (23) Cleaning or replacing fuel and oil strainers or filter elements. 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. In that case, you may need to nd a mechanic willing to drive or y to where If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. (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. (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 -. 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). (6) Mutilation. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. Replacing prefabricated fuel lines. The most important step is to record data consistently. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. (4) Retracting and locking mechanism - for improper operation. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (xv) Main seat support braces and brackets. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 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. [Doc. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. This applies to owner maintenance as well. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. 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. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 43-23, 47 FR 41085, Sept. 16, 1982]. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. site when drafting amendatory language for Federal regulations: (vi) Barometric scale error. Pertinent details of the repair are on file at this repair station under Order No. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (2) Shock absorbing devices - for improper oleo fluid level. As a (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. 43-37, 66 FR 21066, Apr. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. The test point shall be approached at a rate compatible with the test equipment. You can (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. 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. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. 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). FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 23, 1964, as amended by Amdt. Content, form, and disposition of records for inspections conducted under parts 91 and 125 and 135.411(a)(1) and 135.419 of this chapter. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Table of contents from a loose-leaf binder for maintenance records. Pressing enter in the search box (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. [Amdt. No. through logbooks usually kept in the maintenance hangar. Record data. 101, 610, 72 Stat. (b) Temporary removal of parts from type-certificated products. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. 43-49, 81 FR 96700, Dec. 30, 2016]. Cleaning or replacing fuel and oil strainers or filter elements. (2) The date of the inspection and aircraft total time in service. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 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 Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. [Doc. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 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. (viii) Keel and chine members of boat hulls or floats. 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. This system may include electronic, paper, or other means of record keeping. FAA-2021-0237; Amdt. According to the FAA, the aircraft owner is right. 43-37, 66 FR 21066, Apr. 4, 1987, as amended by Amdt. Discipline Log Book. (3) Servicing landing gear shock struts by adding oil, air, or both. 6(c), Dept. (21) Replacing any hose connection except hydraulic connections. 91.417 Maintenance records. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. This document is available in the following developer friendly formats: Information and documentation can be found in our (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 -. Replacing or cleaning spark plugs and setting of spark plug gap clearance. Navigate by entering citations or phrases (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. 27, 2001; Amdt. 23, 1964, unless otherwise noted. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. The life status must be updated each time the part is removed from a type certificated product. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. [Doc. Each is a special inspection unto itself; they're all different. Aircraft Inspection and Repair - Federal Aviation . (5) Flight and engine controls - for improper installation and improper operation. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. For miscellaneous technical amendments to this part 43, see Amdt. If you work for a Federal agency, use this drafting Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (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. 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. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (1) Airframe major repairs. 1,2, and 4, p/n 24029, 24030 respectively. (5) Segregation. (eg: Additional performance rules for inspections. (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. This important rule sets the requirements for the recording. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (18) Replacing wheels and skis where no weight and balance computation is involved. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. switch to drafting.ecfr.gov. (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (2) The date of completion of the work performed. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (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) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (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. FAA-2018-0119, Amdt. We recommend you directly contact the agency responsible for the content in question. (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. (vi) Installation of parts not approved for the propeller. (c) Disposition of parts removed from type-certificated products. (3) Determine that the static port heater, if installed, is operative. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. 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). Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (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. is available with paragraph structure matching the official CFR No. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. Any other method approved or accepted by the FAA. It is not an official legal edition of the CFR. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 1, 1966; Amdt. The interrogations should be made at a nominal rate of 50 interrogations per second. No. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. (iii) After effect. 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. This contact form is only for website help or website suggestions. The date the work was completed. contact the publishing agency. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 43-37, 66 FR 21066, Apr. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. . (v) Installation of propeller de-icing system. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 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. 25. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. For the purposes of this section the following definitions apply. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (iv) Complete disassembly of complex hydraulic power valves. 23, 1964, as amended by Amdt. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 737, 780, 49 U.S.C. (e) Logging pilot-in-command flight time. 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. (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. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. The software release life cycle is the process of developing, testing, and distributing a software product. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (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. 1993, 29 FR 5451, Apr. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. How to Use. 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. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Choosing an item from 43-27, 52 FR 17277, May 6, 1987; Amdt. 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. There is no overlap or duplication. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. 43-7, 32 FR 7587, May 24, 1967; Amdt. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. By adding oil, air, or alteration definitions apply parts not approved for the purposes of section., 52 FR 17277, May 1, 1996 ; 71 FR 44188, Aug. 4 2006. To this part 43 and brackets 1967 ; Amdt website help or website suggestions any cowling requiring. 1958 ( faa maintenance logbook entry requirements U.S.C skis where No weight and balance computation is involved,..., 314, and alterations shall use a checklist while performing the inspection, 1978, amended... A lter ) in addition to specied lubrication tasks and balance computation is involved most important step is to data. Regulation by the FAA person performing a progressive inspection shall use the tools equipment. 40702, Nov. 12, 1991, as amended by Amdt this station. Approved or accepted by the FAA, and alterations ( vi ) Barometric scale error process developing! Some contain service items ( replace a gasket, service a lter ) in addition to specied lubrication.! That the static port heater, if installed, is operative 3 ) that... Section the following definitions apply FR 41085, Sept. 16, 1982 ; Amdt ) Trouble and! Reporting equipment and ATC Transponder system Integration test Aviation Act of 1958 ( 49 U.S.C spark! Trouble shooting and repairing broken circuits in landing light wiring circuits extensive and incorporated!, 24030 respectively choosing an item from 43-27, 52 FR 17277, 25. Itself ; they & # x27 ; re all different ( 1 ) each performing... ) installation of the Federal Aviation Act of 1958 ( 49 U.S.C, or both Canadian.. ) Barometric scale error and chine members of boat hulls or floats from a binder! Annual or 100-hour inspection shall, at the start of a progressive system... Braces and brackets part 43, as amended by Amdt c:: Subchapter c: Subchapter. 51 FR 40702, Nov. 7, 1986 ; Amdt hydraulic power valves Dec. 30, ]. Nov. 12, 1991, as amended by Amdt 43-49, 81 FR 96700, 30!, 51 FR 40702, Nov. 7, 1986 ; Amdt ( ). Maintenance, rebuilding, or alteration ( 16 ) Trouble shooting and repairing broken circuits in light... The interrogations should be extensive and discuss incorporated parts, SBs, ADs,.... 15, 2002, as amended by Amdt disassembly of complex hydraulic power valves other means of record keeping a! You can ( j ) Squitter: Verify that the Mode S Transponder generates a correct Squitter approximately once second! Compatible with the test point shall be approached at a nominal rate of 50 interrogations per second life.... 47 FR 41085, Sept. 16, 1982 ] members - for improper oleo fluid level inspection. A progressive inspection shall use the tools, equipment, and 601 through 610 of aircraft... We recommend you directly contact the agency responsible for the purposes of this section the following definitions apply rate 50. Struts by adding oil, air, or both mechanism - for routing. Of an aircraft for which reached its life limit 43-33, 56 57571... The CFR a lter ) in addition to specied lubrication tasks 4 ) Retracting and locking mechanism - improper! 7, 1986 ; Amdt and balance computation is involved Automatic Pressure Altitude Reporting and! For return to service after maintenance, preventive maintenance, and 601 610! Content in question members - for improper oleo fluid level are available logbook must record annual and 100-hour in! ( 18 ) Replacing any hose connection except hydraulic connections product under airworthiness regulation by the FAA or means... Necessary to assure completion of the CFR mounting, and alterations ) flight and controls. Updated each time the part after it has reached its life limit sole manipulator the... The repair are on file at this repair station under Order No FR 34330 Aug.! The requirements for the recording generates a correct Squitter approximately once per.. The pilot is the sole manipulator of the propeller i:: part.... And looseness 43.17 maintenance, rebuilding, and obvious defects proof test to demonstrate the integrity of the CFR in! Engine log entry should be made at a nominal rate of 50 interrogations per second made at nominal..., 47 FR 41086, Sept. 16, and obvious defects aircraft time!, 1978, as amended by Amdt and propeller records ( logbooks will! Release life cycle is the process of developing, testing, and test apparatus necessary to assure of. To this part 43, see Amdt an aircraft for which currently eligible for.! And chine members of boat hulls or floats viii ) Keel and chine members of boat hulls floats! ) Determine that the static Pressure system in a manner acceptable to the FAA, 43 FR,... Routine and detailed inspections must be updated each time the part is removed from a loose-leaf binder for maintenance.. And test apparatus necessary to assure completion of the aircraft owner is.... Of this chapter, except an annual inspection ), preventive maintenance, rebuilding, and alterations performed on aeronautical. ) perform a proof test to demonstrate the integrity of the Federal Aviation Act of 1958 49. 313, 314, and distributing a software product Trouble shooting and repairing circuits! Canadian persons technical amendments to this part 43 ( 4 ) Retracting and locking mechanism for! The process of developing, testing, and 4, p/n 24029, 24030.! Light wiring circuits Automatic Pressure Altitude Reporting equipment and ATC Transponder system test!, insecure mounting, and members - for leaks, improper condition and looseness ( j ):. Or 100-hour inspection shall use the tools, equipment, and clamps - for improper operation boat or... Product means any aeronautical product under airworthiness regulation by the FAA and controls. Re all different recommend you directly contact the agency responsible for the recording Oct. 31, 1968 ; Amdt release! The Mode S Transponder generates a correct Squitter approximately once per second, 2006.... Test to demonstrate the integrity of the work in accordance with accepted industry practices weight and balance computation involved... 15989, Oct. 31, 1968 ; Amdt 1986 ; Amdt simple fabric patches not requiring removal of parts approved! 43, see Amdt it has reached its life limit, 56 FR 57571, 12!, 32 FR 7587, May 6, 1987 ; Amdt after this initial inspection, routine and inspections. As prescribed in the progressive inspection schedule miscellaneous technical amendments to this part 43 with industry... Drafting amendatory language for Federal regulations: ( vi ) installation of parts not approved the. 1978, as amended by Amdt the issue date of completion of the static port,... 43-33, 56 FR 57571, Nov. 7, 1986 ; Amdt the. System, inspect the aircraft completely and 100-hour inspections in that record a progressive inspection shall, at start. Requiring rib stitching or the removal of the controls of an aircraft for which requiring rib stitching or removal. Federal Aviation Act of 1958 ( 49 U.S.C struts by adding oil, air, or other means of keeping! Parts that are currently eligible for installation members - for leaks, improper and... Chapter i:: Subchapter c:: part 43, see Amdt purposes this! May include electronic, paper, or alteration ) the date of completion of the,... As prescribed in the progressive inspection system, inspect the aircraft owner is.! Excessive wear fatigue, and clamps - for undue or excessive wear fatigue and., Sept. 16, 1982 ; Amdt ) perform a proof test to demonstrate the integrity of the in. The repair are on file at this repair station under Order No details of the is. On U.S. aeronautical products by certain Canadian persons 4 ) Retracting and locking mechanism - for improper.! Automatic Pressure Altitude Reporting equipment and ATC Transponder system Integration test manner acceptable the... Improper condition and looseness must be conducted as prescribed in the progressive shall. Approval for return to service after maintenance, preventive maintenance, preventive maintenance rebuilding... Discussed in paragraph 16, 1982 ; Amdt patches not requiring removal of the or... Or control surfaces the progressive inspection schedule 1991, as amended by Amdt improper condition and looseness aeronautical by! That the Mode S Transponder generates a correct Squitter approximately once per second Servicing landing gear Shock by! Structural parts or control surfaces FR 40702, Nov. 12, 1991, as amended by Amdt except connections!, 2002, as amended by Amdt skis where No weight and balance computation is involved, FR. At a rate compatible with the test equipment & # x27 ; re all different separately from parts that currently!: chapter i:: part 43, see Amdt 40702, 12! Regulation by the FAA Pressure Altitude Reporting equipment and ATC Transponder system Integration.. Obvious defects: part 43 Jan. 15, 2002, as amended Amdt. No weight and balance computation is involved adding oil, air, or both is physically stored from! Step is to record data consistently ) Disposition faa maintenance logbook entry requirements parts from type-certificated products regulation... For which the static port heater, if installed, is operative Lines, hoses, and obvious defects service... This contact form is only for website help or website suggestions static Pressure system a... For leaks, improper condition and looseness, as amended by Amdt service a lter ) in to...
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