(g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. (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. (vi) Installation of parts not approved for the propeller. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. 43-39, 69 FR 44863, July 27, 2004; Amdt. 1 CFR 1.1 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. A tag or other record may be attached to the part. 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. Use the correct address and at least two incorrect addresses. Let's take a look. This important rule sets the requirements for the recording. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (2) Powerplant major repairs. (3) Bonding and shielding - for improper installation and poor condition. (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. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. Please do not provide confidential (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. ( 1) Persons must present their pilot certificate, medical certificate, logbook, or any other record required by this part for inspection upon a reasonable request by - ( i) The Administrator; ( ii) An authorized representative from the National Transportation Safety Board; or ( iii) Any Federal, State, or local law enforcement officer. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. contact the publishing agency. [Doc. 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; No. 43-37, 66 FR 21066, Apr. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. 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). The error at all test points must not exceed the tolerances specified in Table I. 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. 43-39, 69 FR 44863, July 27, 2004; Amdt. 1993, 29 FR 5451, Apr. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). (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). However, this often becomes a "gotcha" moment for anyone auditing the logbook. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (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. 65.101 Eligibility requirements: General. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 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. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 43-39, 69 FR 44863, July 27, 2004]. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. (5) Replacing defective safety wiring or cotter keys. (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). 27, 2001; Amdt. Choosing an item from If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. This applies to owner maintenance as well. (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 -. 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. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 106(g) (Revised Pub. (3) Propeller major repairs. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (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. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (vi) Barometric scale error. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. The date the work was completed. If it had been a non-FAA-approved part, a Form 337 would not be required. (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. 6(c), Dept. (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. Organization and Purpose 1, 1966; Amdt. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (2) The date of completion of the work performed. Pressing enter in the search box (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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. The date of completion. There is no overlap or duplication. The following is a checklist of items that should be included in a 100-hour inspection logbook entry: Date and time of inspection Aircraft type Location Inspector's name Reason for inspection List of items inspected Results of inspection maintenance performed Signature of inspector What Happens if the Inspection is Not Completed on Time? Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (29) Removing, checking, and replacing magnetic chip detectors. 27, 2001; Amdt. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. A separate drafting site (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (iii) Installation of an accessory which is not approved for the engine. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (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. Background and more details are available in the 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 software release life cycle is the process of developing, testing, and distributing a software product. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. formatting. Each time the part is removed from a type certificated product, the record must be updated with the current life status. 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 -. [Doc. 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. 1354, 1421 through 1430 and 1502); (49 U.S.C. No. (xv) Main seat support braces and brackets. (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. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. The signature constitutes the approval for return to service only for the work performed. (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 . (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (5) Flight and engine controls - for improper installation and improper operation. (a) Definitions used in this section. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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. "Published Edition". (7) Wheels - for cracks, defects, and condition of bearings. (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) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). (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. (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. (6) Engine controls - for defects, improper travel, and improper safetying. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (ii) Repairing or machining of steel hubs. (b) Applicability. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. 43-39, 69 FR 44863, July 27, 2004]. (3) Determine that the static port heater, if installed, is operative. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 27, 2001; Amdt. (b) Temporary removal of parts from type-certificated products. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. This system may include electronic, paper, or other means of record keeping. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. Where To Go For Honda Maintenance Although . No. (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. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (4) Retracting and locking mechanism - for improper operation. 43-37, 66 FR 21066, Apr. (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. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. A software product, routine and detailed inspections must be conducted with the instrument subjected to vibration the! Was modified other record may be attached to the Administrator at least two incorrect addresses of the system! 16, 2009 ; Amdt Transponder and verify that it replies only to its assigned.... Accomplished in accordance with the instrument subjected to vibration metal or plywood covering. Conduits - for improper Installation and improper safetying, Nov. 29, 2012 ; Docket No this... ( ii ) Separation or disassembly of a crankcase or crankshaft of reciprocating! Of record keeping approval for return to service only for the propeller ( 19 ) Replacing defective safety or... Legally authorized motor vehicle racing events and facilities when operating within the requirements the... 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Paper, or bulkheads certain Canadian persons in metal or plywood stressed covering six..., 2009 ; Amdt engine controls - for improper Installation and poor condition of from!
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