(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. (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. (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). (23) Cleaning or replacing fuel and oil strainers or filter elements. (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. Ensures that a website is free of malware attacks. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. 14 CFR Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections | Electronic Code of Federal Regulations (e-CFR) | US Law | LII / Legal Information Institute LII Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space (d) Each person performing an annual or 100-hour inspection The tag or record must include the part number, serial number, and current life status of the part. Where are technical descriptions of certificated propellers found? APPENDIX Appendix A - Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, APPENDIX Appendix B - Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, APPENDIX Appendix C - Appendix C to Part 43 [Reserved], APPENDIX Appendix D - Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, APPENDIX Appendix E - Appendix E to Part 43 - Altimeter System Test and Inspection, APPENDIX Appendix F - Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). A Part 147 school student may take the required FAA exams prior to graduation from that school. GENERAL INFORMATION 1-1. (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. USLegal received the following as compared to 9 other form sites. (4) Permanent marking. mounting. (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. The repair of portions of skin sheets by making additional seams. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (vi) Installation of parts not approved for the propeller. Every part of an aircraft must be planned to carry the load imposed upon it. 43.2 - Records of overhaul and rebuilding. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. Guide, Incorporation window.dataLayer = window.dataLayer || []; I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. When must an Airworthiness Directive be complied with? (i) Each person performing an annual or 100-hour inspection 14 CFR Appendix D to Part 43 - Scope and Detail of. A typical preflight inspection is performed by ________ and would include________. What is an attitude, and what are some common positive and negative attitudes about physical activity? (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. (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. (xii) Overhaul of controllable pitch propellers. condition. Explanation of Changes. With US Legal Forms the process of creating legal documents is anxiety-free. Wear within acceptable limits, repair not necessary. (6) Electrical system - for chafing and improper operation of switches. 3335 0 obj
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Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. deterioration. (2) Powerplant major alterations. defects. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. What are three characteristics of a sprawling stance?
This change (3) Anti-icing devices - for improper operations and obvious defects. 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. Blade attachment and motion relative to the hub. (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. When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate, The issuance of an Airworthiness Certificate is governed by, Specifications pertaining to an aircraft, of which a limited number were manufactured under a type certificate and for which there is no current Aircraft Specification, can be found in the. (d) Transfer of life-limited parts. The nose wheel of an airplane is steered by which cockpit control? (ii) Monocoque or semimonocoque wings or control surfaces. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. Elevators move the aircraft around which axis? (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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 . (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. If The material's internal resistance or counterforce that opposes deformation is called: When the lift force is in equilibrium with the weight force, the aircraft: What type of stress resists a crushing force? 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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (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. H,Ht001300Ff l;
(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. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). He shall For the purposes of this section the following definitions apply. (2) Bolts - for improper torquing and lack of safetying. 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). 1.5. 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. (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). (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 0
(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. A ________ may request to see your mechanic certificate. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (7) All systems - for improper installation, poor general (3) Anti-icing devices - for improper operations and obvious Business. The signature constitutes the approval for return to service only for the work performed. (10) All systems - for improper installation, poor general Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to 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. (9) Accessories - for apparent defects in security of (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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. The application form, to become a certified mechanic is FAA Form ______. (2) Replacing elastic shock absorber cords on landing gear. (2) The date of completion of the work performed. We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. The proposed rule added a provision to 12 CFR 748.1 for the NCUA to require notification of any cyber incident that rises to the level of a reportable cyber incident as soon as possible but no later than 72 hours after a FICU reasonably believes that a reportable cyber incident has occurred. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. The simplest rotor system is the _________. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. Enjoy smart fillable fields and interactivity. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ Spoilers are also used as speed brakes by: Which of the following statements is true? 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? center section assembly for poor general condition, fabric or skin Use the surveillance formats UF = 4 and 5. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. Which of the following contains a minimum checklist for a 100 hour inspection? The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 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). Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. (4) Appliance major alterations. safetying. 43.15 - Additional performance rules for inspections. (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 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. (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. Spars are to wings as__________ are to the fuselage. Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. 1.2 Applicability. How are main rotors of helicopters classified? The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. ECO 17212. Where should you find this entry? (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 AC applies to applicants who request data approval for a major repair . Slats increase the _________ at which laminar airflow can exist. The most common method of aircraft inspection is ____________. By an identification letter stamped on one of the hexes of the nozzle body particles or foreign matter on screens and sump drain plugs. 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. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (4) Retracting and locking mechanism - for improper operation. The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. What is the usual final step of an annual inspection before the maintenance entry is made? (10) Floats and skis - for insecure attachment and obvious or apparent defects. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. condition, defects, and insecure attachment. 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. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (2) Seats and safety belts - for poor condition and apparent defects. (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. (5) Replacing defective safety wiring or cotter keys. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (g) Each person performing an annual or 100-hour inspection What is the primary purpose of the helicopter main rotor transmission? 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. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. & Estates, Corporate - Refer to FAR, Part. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. LLC, Internet Title 14 was last amended 2/02/2023. The tests in (e) through (j) apply only to Mode S transponders. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (7) Other methods. (2) Seats and safety belts - for poor condition and apparent defects. Fuselage stations are numbered in inches from the __________. (3) Envelope, gas bags, ballast tanks, and related parts - for The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. USLegal fulfills industry-leading security and compliance standards. Collapse to view only 43.13 - Performance rules (general). (j) Each person performing an annual or 100-hour inspection attachment. (b) Rotorcraft. f-``0>, %
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The __________ is used to thoroughly service a component after it is removed from an aircraft. (b) Temporary removal of parts from type-certificated products. (5) Flight and engine controls - for improper installation and improper operation. (c) Preventive maintenance. breakage. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during Which type of flap slides aft to increase the total area of the wing? (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. A thorough inspection will involve ___________ the aircraft. (d) Performance requirements. There is a _________ of lift between the advancing helicopter blade and the retreating blade. hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1
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lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok The rudder controls the airplane around which axis? (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of (a) Definitions. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (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. During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. 0
(4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. During the next week, create a list of at least 10 things you could have done to conserve the water you use. Title 14 CFR Appendix D to Part 43Scope and detail of items (as applicable to the particular aircraft) to be included in annual and 100-hour inspections A properly written checklist, such as the one shown in this site, includes all the items of Appendix D. Get access to thousands of forms. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. fS3c}^ )L
4FJG,)(-\> poor condition. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. The checklist 14 CFR 43, Appendix D (or similar, like the checklist in AC-90-89B), should be used whether the aircraft is experimental or certified. (c) Disposition of parts removed from type-certificated products. 28-1.". (c) Authorized persons. shall inspect (where applicable) the following components of the TopTenReviews wrote "there is such an extensive range of documents covering so many topics that it is unlikely you would need to look anywhere else". A checklist must be used and include as a minimum, the scope and detail of items (as applicable to the particular aircraft) in 14 CFR part 43, Appendix D. 100-hour Inspection This inspection is required when an aircraft is operated under 14 CFR part 91 and used for hire, such as flight training. When the angle of attack of an airfoil is increased so it reaches maximum lift the: Ribs can be ___________ by stamping holes in the assembly. 10/16/2009 AC 21-43 CHAPTER 1. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. fittings. (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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (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 chord of an airfoil is measured from the ________ to the ________. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 288 0 obj
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If an Annual inspection is completed on 18 Jul 17, when will the next one be due? 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 -. (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . attachment. (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. Title 14 was last amended 2/10/2023. Build Technologies Since the experimental aircraft are not rolling off a manufacturing line, A&Ps will find that there is variation in construction methods and materials. (9) Accessories - for apparent defects in security of mounting. APPENDIX D TO FAR PART 43 SCOPE AND DETAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100HOUR INSPECTIONS(a) Each person performing an annual or 100hour inspection. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. 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