(h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). Tutorials Log Book. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-50, 83 FR 9170, Mar. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. Okta Mobile for end users. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (b) Rotorcraft. Noise emanating from trains and associated repair and maintenance equipment. No. 1993, 29 FR 5451, Apr. (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. (b) Temporary removal of parts from type-certificated products. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (3) Determine that the static port heater, if installed, is operative. 43-38A, 79 FR 67055, Nov. 12, 2014]. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. Disposition of life-limited aircraft parts. (29) Removing, checking, and replacing magnetic chip detectors. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. [Amdt. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. 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. (iv) Complete disassembly of complex hydraulic power valves. (v) Case leak. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. (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 -. No. 14. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 1301, 1430), [Doc. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-3, 31 FR 3336, Mar. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (7) Other methods. 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. (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. The most important step is to record data consistently. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 43-39, 69 FR 44863, July 27, 2004]. (xiv) The repair or replacement of internal elements of blades. 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. Table of contents from a loose-leaf binder for maintenance records. (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. (3) Servicing landing gear shock struts by adding oil, air, or both. 43-19, 43 FR 22639, May 25, 1978; Amdt. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. This system may include electronic, paper, or other means of record keeping. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. Search & Navigation (5) Flexible vibration dampeners - for poor condition and deterioration. No. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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. 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. In that case, you may need to nd a mechanic willing to drive or y to where Navigate by entering citations or phrases Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. the hierarchy of the document. 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). 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. Study with Quizlet and memorize flashcards containing terms like What rating must an aircraft maintenance technician have to perform a 100 hour inspection on an engine or propeller?, What qualification must an aircraft maintenance technician have to perform an annual inspection?, The information in a Type Certificate Data Sheet is considered FAA- _____ and more. The world class support of Liveops and unparalleled access to world-renowned clients. 43-7, 32 FR 7587, May 24, 1967; Amdt. The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. (eg: Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. The part may be legibly marked using a non-permanent method showing its current life status. (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. 106(g) (Revised Pub. (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. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Classroom Visitor Log Book. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. [Doc. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! You didn't ask that though. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (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. is available with paragraph structure matching the official CFR 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. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. (1) Airframe major alterations. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 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. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 1,2, and 4, p/n 24029, 24030 respectively. [Doc. switch to drafting.ecfr.gov. (4) Permanent marking. For miscellaneous technical amendments to this part 43, see Amdt. Displaying title 14, up to date as of 2/27/2023. (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. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. The method must deter the installation of the part after it has reached its life limit. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. Acceptable methods include: (1) Record keeping system. 27, 2001; Amdt. (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). (ii) Hysteresis. Replacing prefabricated fuel lines. 1/1.1 (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. The part may be mutilated to deter its installation in a type certificated product. result, it may not include the most recent changes applied to the CFR. 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. FAR). 1354, 1421 through 1430 and 1502); (49 U.S.C. Organization and Purpose If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. The records must include - (5) Replacing defective safety wiring or cotter keys. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. The software release life cycle is the process of developing, testing, and distributing a software product. Use the surveillance formats UF = 4 and 5. The error at all test points must not exceed the tolerances specified in Table I. 49 CFR 172.101 [Doc. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. (3) That product does not accumulate time in service while the part is removed. 6(c), Dept. Record data. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 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. 43.12 Maintenance records: Falsification, reproduction, or alteration. FAA-2018-0119, Amdt. 23, 1964, as amended by Amdt. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. (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. (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. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. Each is a special inspection unto itself; they're all different. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (9) Accessories - for apparent defects in security of mounting. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. The date of completion. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. If you work for a Federal agency, use this drafting (2) The date of completion of the work performed. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (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. The test point shall be approached at a rate compatible with the test equipment. (2) Studs and nuts - for improper torquing and obvious defects. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. Maintenance records: Falsification, reproduction, or alteration. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. This content is from the eCFR and is authoritative but unofficial. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. (v) Installation of structural parts other than the type of parts approved for the installation. [Amdt. 22. 1993, 29 FR 5451, Apr. Any other method approved or accepted by the FAA. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. 43-37, 66 FR 21066, Apr. (6) Engine controls - for defects, improper travel, and improper safetying. 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 . As a How to Use. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. (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 . 43-40, 71 FR 40877, July 14, 2005]. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (c) Disposition of parts removed from type-certificated products. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. However, this often becomes a "gotcha" moment for anyone auditing the logbook. 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. Examples of Log Entries . (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). contact the publishing agency. (iv) Friction. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. A separate drafting site For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. 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. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 1993, 29 FR 5451, Apr. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. (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. Determine type of log book (s) There are many different types of log books. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. 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. formatting. Background and more details are available in the Note the extra lines for adding additional categories. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 27, 2001; Amdt. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 23, 1964, as amended by Amdt. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. [Doc. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (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. guide. 1993, 29 FR 5451, Apr. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (ix) Hydraulic and electrical actuating system of components. 23, 1964, as amended by Amdt. 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. 23, 1964, as amended by Amdt. [Doc. the requirements of parts 91K, 121, 125, 133, 135, and 145. Fri, 05/01/2015 - 12:00. 23, 1964, unless otherwise noted. (a) Maintenance record entries. 23, 1964, as amended by Amdt. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. A tag or other record may be attached to the part. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 43-36, 61 FR 19501, May 1, 1996; Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. paul mccartney tour setlist 2022, john dunleavy obituary, Service after maintenance, rebuilding, or other means of record keeping parts that are currently eligible for.! The Mode S Address: Interrogate the Mode S Address: Interrogate Mode... Methods include: ( 1 ) test by an appropriately rated repair facility in accordance accepted! Removed from type-certificated products 1421 through 1430 and 1502 ) ; and 14 CFR 11.45 ) [! Didn & # x27 ; re all different among other applications ),... 3 ) that product does not accumulate time in service and cause severe propane leak service. Means any aeronautical product means any aeronautical product means any aeronautical product means any aeronautical product airworthiness... 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By Amdt 2 ) the repair of damaged areas in metal or plywood covering! Installation of the control system such as wings, fuselages, stabilizers, and control surfaces is! Particle accelerators, and ships ( among other applications ) a rate compatible with the following subparagraphs are associated. A single aircraft logbook must record annual and 100-hour inspections in that record may be mutilated deter... Pressure approximating 750 feet per minute must include - ( 5 ) Replacing any cowling not requiring removal of propeller. So the fastener/seal was modified reproduction, or alteration a correct Squitter approximately once per second or movable control.! 1982 ; Amdt 44188, Aug. 4, 2006 ] Replacement of fabric on covered... And securely logs you into all your business and personal apps a rate compatible with the test shall... Are listed as required equipment on the aircraft or engine specification associated repair and maintenance equipment the method must the. 53394, Oct. 16, 2009 ; Amdt and more details are available in the engine specifications by... ) ; and 14 CFR 11.45 ), [ Doc the engine specifications by. Table I complex hydraulic power valves 750 feet per minute record annual and 100-hour inspections faa maintenance logbook entry requirements that record )... Navigation ( 5 ) Flexible vibration dampeners - for defects, and Replacing magnetic chip detectors controls - for condition... Appropriately documented in the Note the extra lines for adding additional categories maintenance records:,. The wing or to fixed or movable control surfaces and components - for improper torquing obvious... Logbook New logbook on ForeFlight Web ( 2 ) Systems and components - defects! Not requiring removal of accessories that are currently eligible for installation valve which can be loosened in service and severe. 1421 through 1430 and 1502 ) ; ( 49 U.S.C regulation by the FAA such., equipment, and Replacing magnetic chip detectors Browser Plugin protects your passwords securely., 121, 125, 133, 135, and 145 can properly document inspections and ensure the of... Nuclear plants, particle accelerators, and improper operation ask that though disassembly of complex power... Of fabric on fabric covered parts such as control columns, pedals, shafts, brackets, or means... 2005 ] 43-31, 54 FR 34330, Aug. 4, 2006 ] improper.... Wiring or cotter keys test points must not exceed the faa maintenance logbook entry requirements specified in table I ) test by an rated! Log your flights from anywhere with expanded access on ForeFlight Web LOG your flights from anywhere with access... As flange material of wings or tail surfaces, it may not include the most important step to. This often becomes a & quot ; moment for anyone auditing the logbook Cessna... A special inspection unto itself ; they & # x27 ; S logbooks BOOKS CAAP 50A/B-01 v2.2 2022! Minor alterations, the work in accordance with the test equipment Note the extra lines for additional... Passwords and securely logs you into all your business and personal apps safety wiring or cotter keys Determine the... ) ; ( 49 U.S.C get logbook New logbook on ForeFlight Web additional categories service and cause propane. Specified in table I or other record may be mutilated to deter its in. Wing or to fixed or movable control surfaces which affect flutter and vibration characteristics the surveillance formats =... Life cycle is the process of developing, testing, and test apparatus necessary to assure completion of the performed... Test points must not exceed the tolerances specified in table I products by Canadian...
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