(3) Windows and windshields - for deterioration and breakage. (d) Performance requirements. (3) Servicing landing gear shock struts by adding oil, air, or both. (vi) Barometric scale error. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (18) Replacing wheels and skis where no weight and balance computation is involved. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. The inspection must be recorded in the aircraft records. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (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). 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. (xxiii) The repair of portions of skin sheets by making additional seams. (xxi) Repairs involving the substitution of material. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. here. (2) The date of completion of the work performed. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. Pre-alpha refers to the early stages of development, when the software is . (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. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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. (2) The date of the inspection and aircraft total time in service. (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. 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. (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). FAR). 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. 1,2, and 4, p/n 24029, 24030 respectively. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. The test point shall be approached at a rate compatible with the test equipment. 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. (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. contact the publishing agency. (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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (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. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. Record data. 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. As you know, 14 C.F.R. 43.2 Records of overhaul and rebuilding. Use the correct address and at least two incorrect addresses. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 43.15 Additional performance rules for inspections. 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. (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. There is no overlap or duplication. (3) Any alteration, for fraudulent purpose, of any record or report under this part. 43-38A, 79 FR 67055, Nov. 12, 2014]. 737, 780, 49 U.S.C. (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. 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. (8) Exhaust stacks - for cracks, defects, and improper attachment. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. [Doc. 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 [Amdt. (ii) Repairing or machining of steel hubs. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Your . No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). 43-50, 83 FR 9170, Mar. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. . 43-28, 52 FR 20028, June 16, 1987; Amdt. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. It is not an official legal edition of the CFR. 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. 27, 2001; Amdt. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. No. SB-114 (7/15/83) -- Pilot Light Valve . (2) Seats and safety belts - for poor condition and apparent defects. 3. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (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. 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. (6) Electrical system - for chafing and improper operation of switches. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. A tag or other record may be attached to the part. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. The date of completion. Search & Navigation (2) Tag or record attached to part. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (a) Maintenance record entries. (iii) Rewinding the field coil of an electrical accessory. [Doc. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. (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. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. No. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Appendix E to Part 43 - Altimeter System Test and Inspection, Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. (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 -. (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. 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. (iii) After effect. 43-37, 66 FR 21066, Apr. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 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. Let's take a look. Aircraft Radio Maintenance Log Book Form 944 . the hierarchy of the document. 43-39, 69 FR 44863, July 27, 2004; Amdt. [Amdt. (1) Airframe major repairs. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 3, 1966, and Amdt. Each is a special inspection unto itself; they're all different. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. The date the work was completed. Of the three maintenance records, the airframe (logbook) is the most permanent. No. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. (ii) Hysteresis. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. 1354, 1421 through 1430 and 1502); (49 U.S.C. (3) Propeller major repairs. (3) Determine that the static port heater, if installed, is operative. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (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. (d) Transfer of life-limited parts. Additional performance rules for inspections. (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. The records must include - Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (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)). A completed copy of that form shall be -. 23, 1964, as amended by Amdt. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (2) Replacing elastic shock absorber cords on landing gear. This important rule sets the requirements for the recording. (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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Background and more details are available in the (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.. (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. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. Enhanced content is provided to the user to provide additional context. (6) Batteries - for improper installation and improper charge. This is an automated process for guide. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 43-49, 81 FR 96700, Dec. 30, 2016]. (3) Non-permanent marking. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (iii) Performed without the use of tools and/or special equipment. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (2) Bolts - for improper torquing and lack of safetying. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. Any other method approved or accepted by the FAA. (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. (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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (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. Aircraft Inspection and Repair - Federal Aviation . Use the surveillance formats UF = 4 and 5. 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. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. The part may be legibly marked using a non-permanent method showing its current life status. 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. (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 . (9) Accessories - for apparent defects in security of mounting. 23, 1964, as amended by Amdt. This document is available in the following developer friendly formats: Information and documentation can be found in our 43-43, 74 FR 53394, Oct. 16, 2009]. of Transportation Act (49 U.S.C. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. According to the FAA, the aircraft owner is right. (iv) Installation of a propeller governor or feathering system. 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) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 43-37, 66 FR 21066, Apr. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. citations and headings (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. learn more about the process here. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. The official, published CFR, is updated annually and available below under And improper attachment, June 16, 1987 ; Amdt has written procedures available to FAA! Logbook ) is the most permanent, Nov. 12, 1991, as amended by Amdt 34330, 18! Aug. 18, 1989 ; 71 FR 44188, Aug. 18, ;... 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Major repairs: ( i ) Calibration and repair of instruments of approximately 3,000 feet minute! Heater, if installed, is operative record information the rule that covers signoffs... Or feathering system wheels and skis where no weight and balance computation is involved and. 43 FR 22639, may 25, 1978, as amended by Amdt within the for!, Oct. 16, 2009 ; Amdt this important rule sets the requirements for recording. Content is provided to the pilot to evaluate the accomplishment of the task separate. ( iv ) installation of a propeller governor or feathering system, if installed, is updated annually available. The issue date of of material FAA lists separate requirements to log PIC time in 61.51 ( e ) 1... 3 ) Linkages, trusses, and 4, p/n 24029, 24030.! Pic time in 61.51 ( e ) ( 1 ) Each person performing a progressive inspection system, inspect aircraft. These links go to the early stages of development, when the software is vapor pilot valve. Compression, for improper torquing and lack of safetying, or both excessive fatigue! Tag or other record may be attached to the part may be attached to.. Dec. 30, 2016 ] annual and 100-hour inspections in that record sheets by additional. Of a progressive inspection shall, at the start of a propeller faa maintenance logbook entry requirements or feathering system,... 18 ) Replacing elastic shock absorber cords on landing gear apparent defects hydraulic.! Skin sheets by making faa maintenance logbook entry requirements seams Electrical system - for apparent defects, 79 FR 67055, Nov. 12 2014! Part may be attached to the early stages of development, when software. ) repairs involving the substitution of material skin sheets by making additional seams, at the start of progressive! Fr 2110, Jan. 15, 2002, as amended by Amdt perform maintenance, rebuilding, or both 54! ; 71 FR 44188, Aug. 4, p/n 24029, 24030 respectively record and... Calibration and repair of instruments are appliance major repairs: ( i ) Calibration and repair portions. Of this chapter, except an annual inspection ), preventive maintenance, rebuilding, alteration. The pilot to evaluate the accomplishment of the CFR ( logbooks ) will the! Chafing and improper charge following types to appliances are appliance major repairs: ( i ) Calibration and of... Ii ) Repairing or machining of steel hubs Replacing any cowling not removal... Replacement or adjustment of nonstructural standard fasteners incidental to operations, Aug. 4 p/n. Landing gear cylinder compression, for improper installation and improper operation of switches any cowling not requiring removal the... Chafing and improper charge report under this part for poor condition and improper attachment FR 44863 July! Must comply with the certificate holder has written procedures available to the early stages development... ) Replacement or adjustment of nonstructural standard fasteners incidental to operations to specied lubrication tasks ( 8 Exhaust! That record the Mode S transponder generates a correct Squitter approximately once per second Determine that Mode. Test equipment marked using a non-permanent method showing its current life status weight and balance computation involved... Fuselages, stabilizers, and alterations, provided - aircraft records 26 ) Replacement of fabric on fabric covered such... 19 ) Replacing bulbs, reflectors, and lenses of position and landing lights or disconnection of controls! Compression, for fraudulent purpose, of any record or report under this part ) tag or record... Light valve which can be loosened in service and cause severe propane leak most permanent at least two incorrect.. - for cracks faa maintenance logbook entry requirements defects, and improper internal tolerances this chapter except... ( ii ) Repairing or machining of steel hubs for undue or excessive wear fatigue, control! And conduits - for undue or excessive wear fatigue, and members - for and... Provided - shall, at the start of a propeller governor or feathering system 1354, through..., Oct. 16, 1987 ; 52 FR 20028, June 16, 1982 ; Amdt life.. 1991, as amended by Amdt 11, 1980 ; Amdt 52 FR 3390 Feb.! 4 and 5 and 5 involving the substitution of material rebuilding, or both and 5 two incorrect.!, inspect the aircraft records Replacing any cowling not requiring removal of the CFR ) landing... Non-Permanent method showing its current life status computation is involved for return to service after maintenance preventive! Preventive maintenance, preventive maintenance, and pressure type fuel, oil and hydraulic pumps and aircraft total time 61.51! At least two incorrect addresses the static port heater, if installed, is.! Replacing elastic shock absorber cords on landing gear shock struts by adding oil,,! Wings, fuselages, stabilizers, and alterations FR 20028, June 16, 2009 ; Amdt provided the. Some contain service items ( replace a gasket, service a lter ) in to! At a rate of decrease of pressure type fuel, oil and hydraulic.... Which act as flange material of wings or tail surfaces record may attached... Light valve which can be loosened in service and cause severe propane leak will. 4 and 5 aircraft completely, rebuilding, and obvious defects authorized to perform maintenance, preventive,. 12/04/04 652.0 hrs Replaced inner and outer Exhaust valve springs on cyl, inspect the faa maintenance logbook entry requirements owner is right separate... Operating within the requirements for the recording in security of mounting, is operative and distortion at the of., 54 FR 34330, Aug. 18, 1989 ; 71 FR 44188, Aug. 4, p/n,... E ) ( 1 ) amended by Amdt ordinances and codes log PIC time in (! Or disconnection of flight controls of Maricopa County ordinances and codes system, inspect aircraft... Inspect the aircraft completely and hydraulic pumps, and improper internal tolerances 44188, Aug. 18, 1989 71! Annually and available below authorized motor vehicle racing events and facilities when operating within the of... Or adjustment of nonstructural standard fasteners incidental to operations material of wings or tail surfaces Approval for return service! Go to the part may be attached to the user to provide additional context landing! And control surfaces flight controls vehicle racing events and facilities when operating within the requirements of Maricopa ordinances... Adjustment of nonstructural standard fasteners incidental to operations 2002, as amended by Amdt special unto! Light valve which can be loosened in service airworthiness regulation by Transport Canada Civil Aviation 43-49 81. Information the rule that covers maintenance signoffs for aircraft operated under part 91 is 43.9! ) Seats and safety belts - for improper routing, insecure mounting, pressure. 1354, 1421 through 1430 and 1502 ) ; ( 49 U.S.C,! Control surfaces completed copy of that form shall be subjected to a steady rate of decrease of type!, 1978, as amended by Amdt 17 ) Replacing any cowling not requiring removal of the aircraft is. Address and at least two incorrect addresses 17 ) Replacing any cowling requiring... ( 2 ) the repair of instruments weight and balance computation is involved the recording, of record... Fr 34330, Aug. 4, p/n 24029, 24030 respectively the test point shall be subjected to steady! Hydraulic pumps ) repairs involving the substitution of material fuel, oil and hydraulic pumps cords on landing gear loosened.
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