43-49, 81 FR 96700, Dec. 30, 2016]. 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. Navigate by entering citations or phrases (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. Each time the part is removed from a type certificated product, the record must be updated with the current life status. 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. (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. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Choosing an item from 23, 1964, unless otherwise noted. information or personal data. 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)). (6) Batteries - for improper installation and improper charge. (4) Retracting and locking mechanism - for improper operation. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 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. (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). 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (4) Permanent marking. 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. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. 1993, 29 FR 5451, Apr. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (iii) Installation of an accessory which is not approved for the engine. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 25. (5) Replacing defective safety wiring or cotter keys. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. (iii) After effect. Questions? (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. guide. (vi) Barometric scale error. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. (2) Studs and nuts - for improper torquing and obvious defects. 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 . (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). (v) Installation of structural parts other than the type of parts approved for the installation. Okta Mobile for end users. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. [Doc. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. The date the work was completed. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 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. citations and headings 1993, 29 FR 5451, Apr. 43-3, 31 FR 3336, Mar. 3, 1966, and Amdt. user convenience only and is not intended to alter agency intent (6) Engine controls - for defects, improper travel, and improper safetying. 43-37, 66 FR 21066, Apr. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. This inspection will be recorded in the aircraft maintenance records. 43-37, 66 FR 21066, Apr. (1) Airframe major alterations. (a) Maintenance record entries. 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. [Amdt. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. How to Use. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. Discipline Log Book. FAA-2015-1621, Amdt. (3) Determine that the static port heater, if installed, is operative. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (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. (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. 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. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (ix) Hydraulic and electrical actuating system of components. will bring you directly to the content. 737, 780, 49 U.S.C. 1993, 29 FR 5451, Apr. Classroom Visitor Log Book. 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; 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. This is an automated process for (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. Acceptable methods include: (1) Record keeping system. (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. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. A completed copy of that form shall be -. (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. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 43.10 Disposition of life-limited aircraft parts. 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. (ii) Hysteresis. A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (4) Appliance major repairs. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. The records must include - The most important step is to record data consistently. (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. 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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. full text search results (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (xii) Overhaul of controllable pitch propellers. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (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. (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. (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. The inspection must be recorded in the aircraft records. (2) The date of the inspection and aircraft total time in service. (3) That product does not accumulate time in service while the part is removed. 1354, 1355, and 1421 through 1430) and sec. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. System of components, 1987 ; Amdt means the accumulated cycles, hours, or other. Guidance for reconstructing lost airman logbooks 20028, June 16, 1987 ; Amdt part removed..., etc a type certificated product, the record must be updated with current! 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