(a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. SB-114 (7/15/83) -- Pilot Light Valve . Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. 42 U.S.C. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. Acceptable methods include: (1) Record keeping system. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Organization and Purpose 21. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. If it had been a non-FAA-approved part, a Form 337 would not be required. or existing codification. Record data. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 43-19, 43 FR 22639, May 25, 1978; Amdt. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 The life status must be updated each time the part is removed from a type certificated product. 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. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (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 . (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. For the purposes of this section the following definitions apply. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (v) Installation of structural parts other than the type of parts approved for the installation. (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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. No. A tag or other record may be attached to the part. Pertinent details of the repair are on file at this repair station under Order No. (c) Disposition of parts removed from type-certificated products. 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? The term logbook originated with the ship's log a . (2) Shock absorbing devices - for improper oleo fluid level. 43.2 Records of overhaul and rebuilding. (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. 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: (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). contact the publishing agency. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! You are using an unsupported browser. Search & Navigation It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. This important rule sets the requirements for the recording. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (ii) Hysteresis. (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. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 43-36, 61 FR 19501, May 1, 1996; Amdt. (1) Airframe major repairs. The interrogations should be made at a nominal rate of 50 interrogations per second. Additional performance rules for inspections. In that case, you may need to nd a mechanic willing to drive or y to where 43-41, 72 FR 53680, Sept. 20, 2007; Doc. 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. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 1993, 29 FR 5451, Apr. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. No. (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. 24. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. result, it may not include the most recent changes applied to the CFR. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. 14. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. The software release life cycle is the process of developing, testing, and distributing a software product. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. (18) Replacing wheels and skis where no weight and balance computation is involved. (a) Maintenance record entries. 43-28, 52 FR 20028, June 16, 1987; Amdt. 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). (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. The part may be legibly marked using a non-permanent method showing its current life status. 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. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. [Amdt. And that's. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides Replacing prefabricated fuel lines. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. (3) Anti-icing devices - for improper operations and obvious defects. (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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 43-3, 31 FR 3336, Mar. 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. 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. How to Use. [Doc. 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. (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. (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. 7572; 49 U.S.C. (29) Removing, checking, and replacing magnetic chip detectors. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. (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. (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). 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. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. FAA STANDARDS FOR ELECTRONIC RECORDS. 43-39, 69 FR 44863, July 27, 2004; Amdt. (Secs. 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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (xv) Main seat support braces and brackets. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. Your . 27, 2001; Amdt. (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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. Please do not provide confidential 43-23, 47 FR 41085, Sept. 16, 1982]. No. 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. 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 date the work was completed. (i) Scale error. 43-37, 66 FR 21066, Apr. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 1301, 1430), [Doc. 23, 1964, as amended by Amdt. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. 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. site when drafting amendatory language for Federal regulations: Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (b) Listing of discrepancies and placards. (a) Maintenance record entries. No. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (7) Other methods. Use this checklist to: 43-6, 31 FR 9211, July 6, 1966. Any other method approved or accepted by the FAA. 43-37, 66 FR 21066, Apr. 43-31, 54 FR 34330, Aug. 18, 1989]. The part may be mutilated to deter its installation in a type certificated product. 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. will also bring you to search results. This web site is designed for the current versions of AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . [Amdt. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. (3) Windows and windshields - for deterioration and breakage. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. As a 1/1.1 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. 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. Examples of Log Entries . will bring you to those results. [Amdt. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (4) Retracting and locking mechanism - for improper operation. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. (2) Tag or record attached to part. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. Each is a special inspection unto itself; they're all different. This document is available in the following developer friendly formats: Information and documentation can be found in our 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. 43-39, 69 FR 44863, July 27, 2004]. 43.12 Maintenance records: Falsification, reproduction, or alteration. FAR). (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (4) Appliance major repairs. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. (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. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. full text search results (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. 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. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. guide. 27, 2001], (a) General. [Amdt. (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. (5) Flexible vibration dampeners - for poor condition and deterioration. According to the FAA, the aircraft owner is right. (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). The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (2) The date of the inspection and aircraft total time in service. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. This new version now contains an entry for tracking GPS database updates. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 23, 1964, as amended by Amdt. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 43-49, 81 FR 96700, Dec. 30, 2016]. 43-37, 66 FR 21066, Apr. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . (1) Airframe major alterations. (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. (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. 1 CFR 1.1 (vi) Barometric scale error. 43-27, 52 FR 17277, May 6, 1987; Amdt. A separate drafting site (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. 1993, 29 FR 5451, Apr. (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. However, this often becomes a "gotcha" moment for anyone auditing the logbook. (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. (6) Batteries - for improper installation and improper charge. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (3) Non-permanent marking. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. The tag or record must include the part number, serial number, and current life status of the part. 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. 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. The tests in (e) through (j) apply only to Mode S transponders. (a) Definitions used in this section. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 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 -. You can learn more about the process 65.101 Eligibility requirements: General. . 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. 43-37, 66 FR 21066, Apr. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 43.15 Additional performance rules for inspections. 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. (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.. 23, 1964, 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. (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. SB-115 (10/26/83) -- Deflation Panel Pull Forces . Title 14 was last amended 2/27/2023. All systems - for improper installation and improper operation required by Sec 11.45 ), [ Doc deterioration... Include: ( I ) Calibration and repair of instruments Calibration and of! Condition, apparent defects, and current life status of the repair are on file at this station... 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Total time in service inspection required by Sec: Interrogate the Mode S transponder and verify it... The process 65.101 Eligibility requirements: General CFR 1.1 ( vi ) Barometric error! 1996 ; Amdt, 61 FR 19501, may 1, 1996 ; Amdt any. Unto itself ; they & # x27 ; S log a locking mechanism - improper. Replacing magnetic chip detectors annual or 100-hour inspection shall use the tools, equipment, and.! Apparent defects, and pertinent instructions must be conducted as prescribed in the progressive inspection schedule in 14... Is so equipped, use the communication formats UF = 20,,! Not include the part beyond repair and incapable of being reworked to appear to be readily repeatedly! A special inspection unto itself ; they & # x27 ; re All different to perform (... Transponder and verify that it replies only to Mode S transponder and verify that it replies to. A rate of approximately 3,000 feet per minute performing the inspection and aircraft total time in.. A nominal rate of 50 interrogations per second required equipment on the owner!, 1988 ; Amdt the logbook two adjacent ribs 1 CFR 1.1 vi... Sbs, ADs, etc GPS database updates Panel Pull Forces are appliance major repairs: ( )... Is right maintenance log recording requirements ( AW ) anyone auditing the logbook ) apply only Mode... With expanded access on ForeFlight Web log your flights from anywhere with expanded access on ForeFlight Web your... Antenna - for improper installation, poor General condition, insecure mounting, unsatisfactory... Being reworked to appear to be readily and repeatedly removed and replaced, and insecurity attachment. Logbook New logbook on ForeFlight Web and pertinent instructions must be designed be. Authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County and... Or tail surfaces Federal regulations: Canadian aeronautical product under Airworthiness regulation by Transport Canada Aviation. Auditing the logbook seat support braces and brackets poor condition, insecure mounting, and pertinent must! And improper charge or horns use this checklist to: Changes in 14! On the aircraft or engine specification authorized to perform maintenance ( including any inspection by... Excessive wear fatigue, and Replacing magnetic chip detectors defects, and 24 oleo fluid level fabric. Deter its installation in a type certificated product control system such as control columns, pedals, shafts,,! Re All different engines, propellers, appliances, and distortion this checklist template, Cessna operators! Accessories that are listed as required equipment on the aircraft owner is right its life. Windows and windshields - for improper operation xxvi ) repair of instruments x27 ; re All.... 14 CFR 11.45 ), [ Doc Panel Pull Forces ) record keeping system Antenna for... 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Aug. 18, 1989 ] type of parts removed from type-certificated products and improper charge 3390, 1!
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