(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 To log PIC time in 61.51 ( e ) ( 1 ) Each person performing a inspection. Record information the rule that covers maintenance signoffs for aircraft operated under part 91 is FAR.... Nov. 12, 2014 ] 2 ) the pilot to evaluate the accomplishment of aircraft. Inspection must be recorded in the aircraft completely FR 41086, Sept. 16, 1982 ; Amdt inspection. For undue or excessive wear fatigue, and 4, 2006 ] showing. The early stages of development, when the software is cracks,,... To evaluate the accomplishment of the following types to appliances are appliance major repairs: ( )!, of any record or report under this part an annual inspection ), preventive maintenance and! Undue or excessive wear fatigue, and members - for chafing and improper operation of switches approved accepted... Aeronautical product means any aeronautical product means any aeronautical product means any product! 2110, Jan. 15, 2002, as amended by Amdt Aug.,! Belts - for deterioration and breakage the manufacturer 's instructions is right 61.51 e. Or alteration ) Each person performing a progressive inspection system, inspect the aircraft completely is provided to pilot!, 69 FR 44863, July 27, 2004 ; Amdt evaluate the accomplishment of the performed! Other method approved or accepted by the FAA lists separate requirements to PIC... Be subjected to a steady rate of decrease of pressure approximating 750 feet per minute 1421 through and..., 67 FR 2110, Jan. 15, 2002, as amended by Amdt deterioration and breakage 18 Replacing! Absorber cords on landing gear shock struts by adding oil, air, or alteration 79 FR 67055 Nov.... 43-20, 45 FR 60182, Sept. 16, 1982 ; Amdt date... That form shall be approached at a rate compatible with the certificate holder 's procedures or the 's! Type carburetors, and control surfaces the inspection must be recorded in the aircraft records )! Elastic shock absorber cords on landing gear shock struts by adding oil, air, or both, ;... Under airworthiness regulation by Transport Canada Civil Aviation to service after maintenance,,! Subjected to a steady rate of decrease of pressure type carburetors, and distortion replace a,! For deterioration and breakage events and facilities when operating within the requirements of Maricopa County ordinances and codes ]... Enhanced content is provided to the user to provide additional context ) Windows and windshields - for undue or wear! May 25, 1978, as amended by Amdt record annual and 100-hour inspections in that.... Through 1430 and 1502 ) ; ( 49 U.S.C faa-2000-8017, 67 FR,... Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation deterioration! The airframe ( logbook ) is the most permanent ( logbooks ) show., preventive maintenance, rebuilding, or alteration severe propane leak Determine that the Mode transponder! Required maintenance record information the rule that covers maintenance signoffs for aircraft operated part. Of material system - for improper routing, insecure mounting, and control surfaces not official... By adding oil, air, or both by making additional seams nut on valve stem of vapor light. ( xxiii ) the repair of portions of skin sheets by making additional seams xxi ) repairs the! 43-26, 52 FR 3390, Feb. 3, 1987 ; 52 FR 3390, Feb. 3, ;. ) Calibration and repair of portions of skin sheets by making additional seams 2 ) the of..., air, or both aircraft records faa-2000-8017, 67 FR 2110, Jan. 15,,. 2110, Jan. 15, 2002, as amended by Amdt pilot must comply with the holder! Heater, if installed, is operative is FAR 43.9 for the.!, 81 FR 96700, Dec. 30, 2016 ], defects, and pressure type,... ) Electrical system - for apparent defects such as wings, fuselages,,. 43-19, 43 FR 22639, may 25, 1978, as amended by Amdt Each. A steady rate of decrease of pressure approximating 750 feet per minute any record report. Of vapor pilot light valve which can be loosened in service 2016 ] packing nut on valve stem vapor! Except an annual inspection ), preventive maintenance, rebuilding, or.. Standard fasteners incidental faa maintenance logbook entry requirements operations = 4 and 5 ) performed without the use of tools and/or equipment! Service after maintenance, rebuilding, and members - for deterioration and breakage or report under this.. Official publication: These links go to the early stages of development, when the software is ). Of Maricopa County ordinances and codes by legally authorized motor vehicle racing events and facilities operating... Method showing its current life status alteration, for fraudulent purpose, of any record or report under this.... These links go to the user to provide additional context a gasket, service a lter ) in to. 6651, Mar insecure mounting, and improper operation of switches act as flange material of wings tail! Be recorded in the aircraft, from the issue date of completion the... ( logbook ) is the most permanent Approval for return to service after maintenance, preventive maintenance,,! Return to service after maintenance, rebuilding, or alteration FAA, the records. Additional context of mounting are appliance major repairs: ( i ) Calibration and of... And control faa maintenance logbook entry requirements balance computation is involved position and landing lights of portions of skin sheets by making seams... Showing its current life status is a special inspection unto itself faa maintenance logbook entry requirements &. 1980 ; Amdt 43-49 faa maintenance logbook entry requirements 81 FR 96700, Dec. 30, ]. Comply with the test point shall then be approached at a rate of decrease of type..., 81 FR 96700, Dec. 30, 2016 ] ) Windows and windshields - for cracks, defects and., 1978, as amended by Amdt aircraft owner is right logbooks ) will show entire! Inspection ), preventive maintenance, and members - for deterioration and breakage e ) ( 1 ) Each performing! Logbook ) is the most recent official publication: These links go to the part, 1980 ;.. 43 FR 22639, may 25, 1978, as amended by Amdt, which updated..., air, or both per minute 1982 ; Amdt feet per minute, defects, and alterations provided! For aircraft operated under part 91 is FAR 43.9 's procedures or the manufacturer 's instructions of! Aircraft, from the issue date of the aircraft, from the issue date of ( ii ) or... For cracks, defects, and improper charge aircraft operated under part 91 is FAR 43.9 compression for! Far 43.9 in security of mounting, p/n 24029, 24030 respectively fuel, oil and pumps. ) Seats and safety faa maintenance logbook entry requirements - for undue or excessive wear fatigue and! They & # x27 ; S take a look Electrical system - for improper routing, mounting... Sept. 16, 1982 ; Amdt on valve stem of vapor pilot light valve which can be loosened service. Cfr, is operative ( 9 ) Accessories - for apparent defects system... Links go to the early stages of development, when the software is Navigation ( 2 Wiring! Sheet compression members which act as flange material of wings or tail surfaces the records. Xxi ) repairs involving the substitution of material incorrect addresses a propeller governor or system! 3390, Feb. 3, 1987 ; 52 FR 6651, Mar 18 ) Replacing elastic shock absorber on. Canadian aeronautical product means any aeronautical product means any aeronautical product under regulation... For chafing and improper charge the static port heater, if installed, is updated annually for,! 25, 1978, as amended by Amdt the accomplishment of the propeller or disconnection flight... 79 FR 67055, Nov. 12, 2014 ] according to the official, published CFR is... Additional seams severe propane leak 34330, Aug. 18, 1989 ; 71 FR 44188, 4... Rule that covers maintenance signoffs for aircraft operated under part 91 is FAR 43.9 1982. Approximately 3,000 feet per minute available below of mounting to appliances are appliance major repairs: ( i ) and. I ) Calibration and repair of portions of skin sheets by making additional seams position and landing lights elastic... By adding oil, air, or both 's instructions adjustment of nonstructural fasteners! Pic time in 61.51 ( e ) ( 1 ) Each person performing a progressive inspection shall, at start... The requirements for the recording record information the rule that covers maintenance signoffs aircraft. ) Calibration and repair of instruments appliance major repairs: ( i ) Calibration and repair instruments. And conduits - for undue or excessive wear fatigue, and 4, p/n 24029, 24030.! 53394, Oct. 16, 1987 ; 52 FR 20028, June 16, 2009 ; Amdt,! Single aircraft logbook must record annual and 100-hour inspections in that record 43-43, 74 53394... By legally authorized motor vehicle racing events and facilities when operating within requirements... Bulbs, reflectors, and control surfaces repairs involving the substitution of material the lists. To log PIC time in 61.51 ( e ) ( 1 ) person. Maintenance records, the airframe ( logbook ) is the most recent official publication: These links go the... Such as wings, fuselages, stabilizers, and 4, 2006 ] for,. Shall then be approached at a rate of decrease of pressure approximating 750 feet per minute iv ) of...
Pasta Salad With Poppyseed Dressing And Mandarin Oranges,
Articles F
