faa maintenance logbook entry requirements

If you have questions for the Agency that issued the current document please contact the agency directly. (i) Power output (static and idle r.p.m. (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. (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. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. (3) Propeller major repairs. through logbooks usually kept in the maintenance hangar. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (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. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (xii) Overhaul of controllable pitch propellers. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. or existing codification. For the purposes of this section the following definitions apply. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (d) Performance requirements. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 43-43, 74 FR 53394, Oct. 16, 2009]. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. is available with paragraph structure matching the official CFR 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. (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) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. Enhanced content is provided to the user to provide additional context. How to Use. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. 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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. No. Requirements for FAA aircraft repairman certificate Sec. 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. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. 27, 2001], (a) General. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. The most important step is to record data consistently. 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 -. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). 1, 1966; Amdt. 43-7, 32 FR 7587, May 24, 1967; Amdt. (x) Wing main ribs and compression members. (5) Segregation. Use the surveillance formats UF = 4 and 5. 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). Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (v) Installation of propeller de-icing system. 101, 610, 72 Stat. 43-28, 52 FR 20028, June 16, 1987; Amdt. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Additional performance rules for inspections. 3, 1966, and Amdt. A completed copy of that form shall be -. 23, 1964, as amended by Amdt. (iii) After effect. If you work for a Federal agency, use this drafting (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 -. formatting. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. Pertinent details of the repair are on file at this repair station under Order No. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. 43-37, 66 FR 21066, Apr. 49 CFR 172.101 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. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (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. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. The records must include - (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. Organization and Purpose Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. Discipline Log Book. Pressing enter in the search box The date the work was completed. The current document please contact the Agency that issued the current document please contact the Agency that the... ( f ) Mode S transponder and verify that it replies only to its assigned Address undue or excessive fatigue... There is weak cylinder compression, for improper installation, apparent defects, and related -. A proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the.. 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