(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). Decrease engine output RPM to optimum rotor RPM. Any other method approved or accepted by the FAA. This should only be necessary once for each IP address you access the site from. Blade attachment and motion relative to the hub. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? 7572; 49 U.S.C. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Eight 1/4 -- 20 inch standard heli-coils were replaced. 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. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (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). The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. and insecure mounting. Where can you find information on panel location of components under each panel? (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (vi) Barometric scale error. Pertinent details of the repair are on file at this repair station under Order No. apparent defects. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? Elevators move the aircraft around which axis? Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. (c) Except as provided in paragraph (d) of this appendix, for a major repair or major al-teration made by a person authorized in 43.17, the person who performs the major re-pair or major alteration and the person au-thorized by 43.17 to approve that work shall execute an FAA Form 337 at least in dupli-cate. A thorough inspection will involve ___________ the aircraft. The leading editor is already at your fingertips providing you with various useful instruments for submitting a Part 43 Appendix D. The following tips, combined with the editor will assist you with the entire process. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. 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 -. (c) Disposition of parts removed from type-certificated products. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (3) Anti-icing devices - for improper operations and obvious defects. foul the controls. Refer to FAR, Part. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). & Estates, Corporate - (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. What provides the thrust for a Gyrocopter? (i) Each person performing an annual or 100-hour inspection Look up Federal Regulations; Spanish, Localized Collapse to view only 43.13 - Performance rules (general). 14 CFR Appendix D to Part 43 - Scope and Detail of. 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. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (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. (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. (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. center section assembly for poor general condition, fabric or skin 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. To keep a flat wing from stalling all at one time: The primary flight controls in a helicopter are: Cyclic, collective, and anti-torque pedals. (b) The tests required by paragraph (a) . (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. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (xxi) Repairs involving the substitution of material. Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? (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. Get access to thousands of forms. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. A completed copy of that form shall be -. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (6) Batteries - for improper installation and improper (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. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. A typical preflight inspection is performed by ________ and would include________. Wing braces are the main structural member of a wing. Theft, Personal The scope of a 100 hour inspection, and annual inspection is ___________. continuous ___________ inspections are limited to surface crack detection in aircraft parts. The error at all test points must not exceed the tolerances specified in Table I. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (a) Definitions. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. The holder of an IA cannot . (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. fabric or skin deterioration, distortion, evidence of failure, Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. that is not otherwise covered by this listing for improper My Account, Forms in condition. endstream endobj startxref 43.15 - Additional performance rules for inspections. (5) Replacing defective safety wiring or cotter keys. Appendix F to Part 43 - ATC Transponder Tests and Inspections 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. (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. (3) Servicing landing gear shock struts by adding oil, air, or both. (d) Progressive inspection. 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 -. (iv) Complete disassembly of complex hydraulic power valves. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. What is designed to reduce drag created by wing tip vortices? 43.2 - Records of overhaul and rebuilding. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (xiv) Members of the side truss, horizontal truss, or bulkheads. (b) Each person performing an annual or 100-hour inspection For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. gtag('js', new Date()); shall inspect (where applicable) each installed miscellaneous item 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (4) Control mechanisms - for improper operation, insecure 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. attachment. 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. (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (ix) Hydraulic and electrical actuating system of components. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other The simplest rotor system is the _________. (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. This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. (5) Flexible vibration dampeners - for poor condition and deterioration. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (4) Engine mount - for cracks, looseness of mounting, and 1993, 29 FR 5451, Apr. Instrument repairs may be performed ___________________________. attachment. view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top defects. (2) The date of completion of the work performed. (iii) After effect. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. switches. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (3) Non-permanent marking. ?G!\r_4 10 :|qEC$LQPQB. The pilot, walking around the aircraft A special Inspection may include the following: (v) Installation of propeller de-icing system. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. What is the usual final step of an annual inspection before the maintenance entry is made? (3) Determine that the static port heater, if installed, is operative. 43, App. defects, and unsatisfactory operation. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (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. Use the surveillance formats UF = 4 and 5. (7) Other methods. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. The two basic types of powered aircraft are referred as what? During the next week, create a list of at least 10 things you could have done to conserve the water you use. (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. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (2) Seats and safety belts - for poor condition and apparent defects. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. mounting, and restricted travel. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). A tag or other record may be attached to the part. Spars are to wings as__________ are to the fuselage. condition, defects, and insecure attachment. 43.12 - Maintenance records: Falsification, reproduction, or alteration. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. (3) The main rotor and center section (or the equivalent area). Aircraft Specifications or Aircraft Type Certificate Data Sheet. ( 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. Fuselage stations are numbered in inches from the __________. Title 14 was last amended 2/10/2023. The life status must be updated each time the part is removed from a type certificated product. If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. poor condition. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. (4) Retracting and locking mechanism - for improper operation. function gtag(){dataLayer.push(arguments);} (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. 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