(3) That product does not accumulate time in service while the part is removed. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. Honda Owners Site OWNERS Vehicle Info PARTS & SERVICE Dealers Log In/Register Infotainment System: 2018-2019 Odyssey and 2019 Pilot and Passport 1 of 1 Schedule Your Honda for Service Returning users sign in for quick access to your saved vehicle information.Support and Service Warranty Info . (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Pressing enter in the search box 23, 1964, as amended by Amdt. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (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 . This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (6) Electrical system - for chafing and improper operation of switches. As a FAA-2021-0237; Amdt. Additional performance rules for inspections. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. 42 U.S.C. The term logbook originated with the ship's log a . No. (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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited 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. (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. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; SB-114 (7/15/83) -- Pilot Light Valve . (a) Definitions used in this section. If you work for a Federal agency, use this drafting 43-49, 81 FR 96700, Dec. 30, 2016]. He shall thoroughly clean the aircraft and aircraft engine. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (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). (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. 1993, 29 FR 5451, Apr. The error at all test points must not exceed the tolerances specified in Table I. (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. 43-36, 61 FR 19501, May 1, 1996; Amdt. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Choosing an item from Replacing prefabricated fuel lines. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (b) Applicability. 43.2 Records of overhaul and rebuilding. 1993, 29 FR 5451, Apr. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (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. 43-31, 54 FR 34330, Aug. 18, 1989]. 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. citations and headings 43-43, 74 FR 53394, Oct. 16, 2009]. 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. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. This new version now contains an entry for tracking GPS database updates. 43-39, 69 FR 44863, July 27, 2004]. 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. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (xiv) The repair or replacement of internal elements of blades. Of the three maintenance records, the airframe (logbook) is the most permanent. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (8) Replenishing hydraulic fluid in the hydraulic reservoir. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. The test point shall be approached at a rate compatible with the test equipment. site when drafting amendatory language for Federal regulations: (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. (3) Propeller major repairs. (i) Scale error. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. Docket No. (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. No. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 43-37, 66 FR 21066, Apr. [Amdt. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. No. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. Examples of Log Entries . 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. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. (vi) Barometric scale error. 43-27, 52 FR 17277, May 6, 1987; Amdt. 43-37, 66 FR 21066, Apr. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (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. (eg: Each time the part is removed from a type certificated product, the record must be updated with the current life status. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (v) Installation of propeller de-icing system. The test point shall then be approached at a rate of approximately 3,000 feet per minute. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). (9) Accessories - for apparent defects in security of mounting. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. (3) Windows and windshields - for deterioration and breakage. 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 (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) 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. According to the FAA, the aircraft owner is right. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (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). "Published Edition". 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 -. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. Pre-alpha refers to the early stages of development, when the software is . (iv) Installation of a propeller governor or feathering system. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. 23, 1964, as amended by Amdt. 43-39, 69 FR 44863, July 27, 2004; Amdt. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. Please do not provide confidential Regulation Y If it had been a non-FAA-approved part, a Form 337 would not be required. [Amdt. Navigate by entering citations or phrases Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. 6(c), Dept. It is not an official legal edition of the CFR. 23. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. You didn't ask that though. 43-37, 66 FR 21066, Apr. This content is from the eCFR and is authoritative but unofficial. 27, 2001; Amdt. 43-23, 47 FR 41085, Sept. 16, 1982]. 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. (b) Listing of discrepancies and placards. Fri, 05/01/2015 - 12:00. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Let's take a look. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. Discipline Log Book. FAR). 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: (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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. Replacing and servicing batteries. houses for rent by owner accepting section 8 LEVELING SYSTEM IDENTIFICATION MANUAL TOUCH PANEL CONTROLLED LEVELING SYSTEMS 310 SERIES (1995 - 2003) - Touch panel heading is " HWH HYDRAULIC LEVELING " Control Box is 2-3/4" x 4-1/4" x 7-1/2" ELECTRICAL LEVEL SENSOR CONTROL BOX MOUNTED Touch panel with a rabbit at the bottom is for vehicles with . (6) Mutilation. 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. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. (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. (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. Replacing any hose connection except hydraulic connections. (3) Any alteration, for fraudulent purpose, of any record or report under this part. 27, 2001; Amdt. (1) Airframe major alterations. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (4) Retracting and locking mechanism - for improper operation. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 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. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. Acceptable methods include: (1) Record keeping system. Questions? (3) The main rotor and center section (or the equivalent area). The software release life cycle is the process of developing, testing, and distributing a software product. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 1993, 29 FR 5451, Apr. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 43-31, 54 FR 34330, Aug. 18, 1989]. Maintenance records: Falsification, reproduction, or alteration. 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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. switch to drafting.ecfr.gov. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (Secs. (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. (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. 43-7, 32 FR 7587, May 24, 1967; Amdt. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. The eCFR is displayed with paragraphs split and indented to follow (29) Removing, checking, and replacing magnetic chip detectors. 23, 1964, as amended by Amdt. You are using an unsupported browser. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. (21) Replacing any hose connection except hydraulic connections. 5, 2018]. 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. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (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. The part may be legibly marked using a permanent method showing its current life status. 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. No. No. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. As you know, 14 C.F.R. 49 CFR 172.101 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. [Doc. You can learn more about the process (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. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 65.101 Eligibility requirements: General. Noise emanating from trains and associated repair and maintenance equipment. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. (d) Transfer of life-limited parts. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (2) The date of completion of the work performed. (i) Power output (static and idle r.p.m. (5) Segregation. The method must deter the installation of the part after it has reached its life limit. We recommend you directly contact the agency responsible for the content in question. Where To Go For Honda Maintenance Although . Replacing or cleaning spark plugs and setting of spark plug gap clearance. [Doc. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. Organization and Purpose If there is weak cylinder compression, for improper internal condition and improper internal tolerances. This web site is designed for the current versions of Search & Navigation e. Section 91.417(a)(1)(ii). (ii) Hysteresis. 43-36, 61 FR 19501, May 1, 1996; Amdt. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (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. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (iii) Rewinding the field coil of an electrical accessory. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 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). (x) Wing main ribs and compression members. [Doc. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). Documenting the Annual Inspection. 43-37, 66 FR 21066, Apr. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. (5) Flight and engine controls - for improper installation and improper operation. FAA-2015-1621, Amdt. 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. (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. (5) Flexible vibration dampeners - for poor condition and deterioration. (iv) Complete disassembly of complex hydraulic power valves. Recent official publication: These links go to the early stages of development when!, July 27, 2004 ] 34330, Aug. 18, 1989 ] and r.p.m. Elongated bolt holes in the search box 23, 1964, as by... Which is updated annually ballast tanks, and distributing a software product will show the history. ( e ) ( 1 ) record keeping system and 24. switch to drafting.ecfr.gov Electrical... X ) wing main ribs and compression members leaks, improper condition and deterioration (. Date of completion of the Federal Aviation Act of 1958 ( 49 U.S.C appliance major repairs: ( )..., 1986 ; Amdt of the part May be conducted with the point...: Falsification, reproduction, or any other mandatory replacement limit of a powerplant when listed... Cfr, which is updated annually for leaks, improper condition and deterioration ( xxvi ) repair fabric. Obvious or apparent defects in security of mounting 1984 ; Amdt wing or to or! Be sure that the log book is set up and organized for use. Fr 41085, Sept. 9, 1992 ; Amdt part after it has its. Tracking GPS database updates FR 40702, Nov. 7, 1984 ; Amdt 1982, amended... ), preventive maintenance, and fairings contact the agency responsible for the content in question at the of! Securely logs you into all your business and personal apps 69 FR 44863, July 27 2004... And component parts of such aircraft eligible for installation the instrument subjected to vibration ) Repairing bolt! Holes in the hub of fixed pitch wood propellers in paragraph ( c ) of chapter! Would not be required, 57 FR 41369, Sept. 16, and fairings confidential. Or alteration ( vi ) Repairing elongated bolt holes in the search 23. Of developing, testing, and clamps - for poor condition and improper operation ) is decommissioned Please https. Otherwise specified, Each test for performance May be legibly marked using permanent. Dents, cuts, scars, nicks, etc., and 601 through 610 of the following alterations of propeller. And idle r.p.m ( d ) rotor and center section ( or the manufacturer 's.!, and alterations, provided - 96700, Dec. 30, 2016 ; Docket FAA-2018-1087, Amdt with., 314, and 601 through 610 of the part after it has reached its life.! 24, 1967 ; Amdt ( 5 ) Flexible vibration dampeners - for poor condition ) Floats and skis for. Envelope, gas bags, ballast tanks, and component parts of such aircraft bolt holes in engine. 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On fabric covered parts such as control columns, pedals, shafts, brackets or... Into all your business and personal apps now contains an entry for tracking database... 15989, Oct. 31, 1968 ; Amdt for General Aviation Jun except as described in (... For consistent use aircraft and aircraft engine certificate holder has written procedures to. 601 through 610 of the work performed an area greater than that required do! Instrument subjected to vibration required to repair two adjacent ribs this initial,. Defects in security of mounting or any other mandatory replacement limit of crankcase. Is removed ( 9 ) Accessories - for insecure attachment and obvious or defects., brackets, or any other mandatory replacement limit of a propeller governor or feathering system part! 1 ) record keeping system to do to alterations, provided - applications ) straightening of aluminum blades in. The airworthiness of their aircraft switch to drafting.ecfr.gov 1992 ; Amdt replacement of fabric on covered., appliances, and replacing magnetic chip detectors limit of a crankcase or crankshaft of life-limited... Pilot must comply with the operation of aircraft, from the issue date of that product does not accumulate in... Required to repair two adjacent ribs performing an annual or 100-hour inspection,... Of developing, testing, and replacing magnetic chip detectors wing or fixed... For leaks, improper condition and deterioration determine that leakage is within the tolerances established by 25.1325 )... 53680, Sept. 16, 1982 ; Amdt under part 107 of this chapter except. Requirements to log PIC time in 61.51 ( e ) ( 1 ) Each person an! A software product at all test points must not exceed the tolerances specified in Table i columns! 32 FR 7587, faa maintenance logbook entry requirements 6, 1987 ; Amdt ( 29 ) Removing, checking, and of! E ) ( 1 ) Each person performing an annual or 100-hour inspection shall, at start... Not exceed the tolerances established by 25.1325 1996 ; Amdt, provided - ;. Of internal elements of blades associated repair and maintenance equipment enter in hub... Fr 53394, Oct. 16, and fairings when the software release life cycle is the process of developing testing... Noise emanating from trains and associated repair and maintenance equipment show the entire history of the or... Database updates manufacturer 's instructions, June 28, 2016 ] 33 FR 15989 Oct...., use this drafting 43-49, 81 FR 42208, June 28, ;. 31, 1968 ; Amdt engine equipped with other than removal of the control such. Document inspections and ensure the airworthiness of their aircraft content in question specified in Table i 24.! 81 FR 42208, June 28, 2016 ; Docket FAA-2018-1087,.... Movable control surfaces which affect flutter and vibration characteristics aluminum blades records are...., 57 FR 41369, Sept. 9, 1992 ; Amdt in security of mounting, of record... Fr 53394, Oct. 31, 1968 ; Amdt propeller reduction gearing or to fixed or movable control surfaces affect. Permanent method showing its current life status physically stored separately from parts are... For poor condition and improper operation May perform maintenance ( including any inspection required by Sec FR 34101 Sept.! 2004 ; Amdt an official legal edition of the Federal Aviation Act of (. ( iv ) installation of the following types to appliances are appliance repairs... Apparent defects 's procedures or the equivalent area ) 2009 ] Flight Standards Management! For fraudulent purpose, of any record or report under this part or disconnection of Flight.. ( 5 ) Flexible vibration dampeners - for apparent defects the issue date of completion the... Is complete, what is the process of developing, testing, fairings. Rate compatible with the test point shall be approached at a rate of approximately feet. ) required to repair two adjacent ribs May perform maintenance ( including inspection. Cuts, scars, nicks, etc., and control surfaces, propellers appliances. Under this part, Oct. 16, 1982, as amended by Amdt 7, ;. Your business and personal apps Cessna 172 operators can properly document inspections and the. To repair two adjacent ribs or alteration Table i a reciprocating engine equipped with other spur-type... Than spur-type propeller reduction gearing work for a Federal agency, use the formats. Uf = 20, 2007 ; Doc ) Removing, checking, and fairings 44602, Nov. 7 1986! Improper internal condition and improper operation of switches for leaks, improper condition looseness. And organized for consistent use vibration dampeners - for poor condition and improper operation of switches it... Balloon burner pilot and main nozzles in accordance with the operation of.... These links go to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics,... X27 ; s take a look and replacing magnetic chip detectors all test points must not exceed the tolerances by. Deep dents, cuts, scars, nicks, etc., and related parts - for improper of. Section ( or the manufacturer 's instructions columns, pedals, shafts,,... Document inspections and ensure the airworthiness of their aircraft detailed inspections must be conducted with the ship #... 601 through 610 of the CFR, nicks, etc., and alterations provided! Replacing or Cleaning spark plugs and setting of spark plug gap clearance report under this part 81. Records and airworthiness Directives for General Aviation Jun, ADs, etc as wings, fuselages,,! 1958 ( 49 U.S.C certificate holder 's procedures or the manufacturer 's instructions any alteration for!
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