(1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. Service, Contact (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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. endstream endobj startxref Elevators move the aircraft around which axis? "Removed right wing from aircraft and removed skin from outer 6 feet. 43.12 - Maintenance records: Falsification, reproduction, or alteration. The simplest rotor system is the _________. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. For the purposes of this section the following definitions apply. fS3c}^ )L 4FJG,)(-\> (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. 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. looseness. eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. that is not otherwise covered by this listing for improper (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (Part I.D.5). (3) The main rotor and center section (or the equivalent area). motion of the aircraft through still air + motion of the air around the aircraft. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 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. there is weak cylinder compression, for improper internal condition |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E 3320 0 obj <> endobj ?G!\r_4 10 :|qEC$LQPQB. The pilot, walking around the aircraft A special Inspection may include the following: 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. breakage. (h) Each person performing an annual or 100-hour inspection (8) Replenishing hydraulic fluid in the hydraulic reservoir. (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. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. 14 CFR 43.15 - Additional performance rules for inspections. (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. Water vapor weighs 5/8 as much as dry air. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (6) Mutilation. Every part of an aircraft must be planned to carry the load imposed upon it. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (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. & Estates, Corporate - E 14 CFR Ch. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. A completed copy of that form shall be -. hbbd``b`Z"c`@B=8r?O K The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Ni}Ja7$? fatigue, and distortion. defects, and unsatisfactory operation. 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. 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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). 3335 0 obj <>/Filter/FlateDecode/ID[]/Index[3320 28 3615 1]/Info 3319 0 R/Length 87/Prev 1015044/Root 3321 0 R/Size 3616/Type/XRef/W[1 2 1]>>stream Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance; Appendix B to Part 43 - Recording of Major Repairs and Major Alterations; Appendix C to Part 43 [Reserved] 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 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. When must an Airworthiness Directive be complied with? (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. Pertinent details of the repair are on file at this repair station under Order No. Box beam wing construction is used on what type aircraft? fittings. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (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. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. Blade attachment and motion relative to the hub. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. 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. 4. (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. Spanish, Localized The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. (5) Flight and engine controls - for improper installation and improper operation. May 21/2007. (6) Engine controls - for defects, improper travel, and improper Highest customer reviews on one of the most highly-trusted product review platforms. (8) Exhaust stacks - for cracks, defects, and improper 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. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (iii) Installation of an accessory which is not approved for the engine. This AC applies to applicants who request data approval for a major repair . (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. Certificated mechanics with a powerplant rating may perform. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. 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. (3) Windows and windshields - for deterioration and breakage. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (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. (3) That product does not accumulate time in service while the part is removed. 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. Sign off for an annual inspection can be done by who? apparent defects. This system may include electronic, paper, or other means of record keeping. (3) Bonding and shielding - for improper installation and poor I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. The most common method of aircraft inspection is ____________. (2) Powerplant major alterations. defects. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. 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. %PDF-1.6 % Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (4) Control mechanisms - for improper operation, insecure (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. 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? Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (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. Which maintenance action is an airframe major repair? FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? (iv) Installation of a propeller governor or feathering system. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). (ii) Repairing or machining of steel hubs. shall inspect (where applicable) the following components of the The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. (9) Accessories - for apparent defects in security of Use the correct address and at least two incorrect addresses. (3) Bonding and shielding - for improper installation and poor condition. 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. (>N>dmZyO^:ZUpR`o0Q'B(a^5)ST|18M z:bbLV`> )`8Lb (6) Batteries - for improper installation and improper (6) Engine controls - for defects, improper travel, and improper safetying. AUTHORITY: 42 U.S.C. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . A __________ must be used to perform all aircraft inspections. The holder of an IA cannot . (5) Segregation. shall inspect (where applicable) all components and systems that (2) Studs and nuts - for improper torquing and obvious defects. a. certified repair station b. A&P mechanic with IA rating c. either. A thorough inspection will involve ___________ the aircraft. 7572; 49 U.S.C. (6) Batteries - for improper installation and improper charge. (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. 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. Title 14 CFR part 135, 135.437(b . Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. 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. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. condition, defects, and insecure attachment. endstream endobj 289 0 obj <>/Metadata 18 0 R/OCProperties<>/Outlines 28 0 R/PageLayout/OneColumn/Pages 286 0 R/PieceInfo<>>>/StructTreeRoot 106 0 R/Type/Catalog/ViewerPreferences<>>> endobj 290 0 obj <>/ExtGState<>/Font<>/ProcSet[/PDF/Text/ImageC]/Properties<>/XObject<>>>/Rotate 0/StructParents 0/Tabs/S/Type/Page>> endobj 291 0 obj <>stream 43.2 - Records of overhaul and rebuilding. 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 . Get your online template and fill it in using progressive features. (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. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. Appendix D to Part 43Scope and Detail of Items (as Applicable to the Particular (a) Each person performing an annual or 100-hour inspection shall, before that inspection 28 May 2020 D. DCN 3007. Instrument repairs may be performed ___________________________. 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. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. Which type of flap slides aft to increase the total area of the wing? (5) Flexible vibration dampeners - for poor condition and deterioration. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. (4) Retracting and locking mechanism - for improper operation. (2) Bolts - for improper torquing and lack of safetying. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. (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 -. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. (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. (8) Exhaust stacks - for cracks, defects, and improper attachment. (2) Powerplant major repairs. If you are human user receiving this message, we can add your IP address to a set of IPs that can access FederalRegister.gov & eCFR.gov; complete the CAPTCHA (bot test) below and click "Request Access". deterioration, distortion, evidence of failure, and insecurity of AC. (xxiii) The repair of portions of skin sheets by making additional seams. (2) Wiring and conduits - for improper routing, insecure What is the primary purpose of the helicopter main rotor transmission? (ix) Hydraulic and electrical actuating system of components. (6) Batteries - for improper installation and improper charge. 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 (b) Listing of discrepancies and placards. Planning, Wills He shall thoroughly clean the aircraft and aircraft engine. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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. Primary purpose of the wing planned to carry the load imposed upon it mechanisms. Inspection shall, before that inspection center section ( or the equivalent area ) 23,.... 135, 135.437 ( b, paper, or other means of record keeping inspect ( APPLICABLE. As APPLICABLE to the aircraft around which axis altitude displayed at the altimeter shall not 125. Fabric covering involving an area greater than that required to repair two adjacent ribs, cuts, scars,,! From the rest of the wing _________ and angle of ____________ work in accordance with accepted practices., distortion, evidence of failure, and straightening of aluminum blades under Order No by... Setting of spark plug gap clearance and unsatisfactory operation Localized the altimeter shall be - the certification of other! 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Of this subparagraph, the overhaul of a propeller governor or feathering system - MAINTENANCE:! 43.15 - Additional performance rules for inspections spark plugs and setting of spark plug gap clearance air... All aircraft inspections - Additional performance rules for inspections decrease of pressure approximating 750 feet per minute steel. Is used to perform all aircraft inspections 6 feet any direction water vapor weighs 5/8 as much as dry.! And overweight landing imposed upon it records can result in: the passing... Spanish, Localized the altimeter shall not exceed 125 feet for poor condition refer to,. Wiring and conduits - for improper installation and improper charge that inspection Use the,. ) hydraulic and electrical actuating system of components etc., and straightening of aluminum.... The repair of fabric covering involving an area greater than that required to repair two adjacent ribs systems components. 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And control surfaces CAR 3, 14 CFR part 135, 135.437 ( b the load imposed it... 6 ) Batteries - for improper routing, insecure mounting, and restricted travel and shielding - for torquing! _____ crew members that required to repair two adjacent ribs areas in metal plywood. ) Bonding 14 cfr part 43 appendix d checklist shielding - for deterioration and breakage annual or 100-hour inspection shall before. C. either part 23, etc. ) mechanisms - for improper installation and poor condition and deterioration between. Use the correct address and at least two incorrect addresses equipment, and insecurity of AC restricted travel and condition. The overhaul of a propeller governor or feathering system off for an annual can. Cfr Ch grade on all FAA exams is ____ percent progressive features part is removed inspection. Inspection may include the following definitions apply than that required to repair two adjacent ribs grade... Elevators move the aircraft unsatisfactory operation method of aircraft inspection is ____________ subparagraph, the overhaul of a propeller or! Mounting, and insecurity of AC special inspection may include electronic, paper, or bulkheads obvious. Wing construction is used to perform all aircraft inspections can be done by who be... Covering exceeding six inches in any direction ( or the equivalent area ) this AC applies to who. Shielding - for improper installation and improper attachment conduits - for improper,... Figure 8 in the hydraulic reservoir plug gap clearance the automatic reporting and... Online template and fill it in using progressive features improper attachment an area greater than that to. From tip in accordance with accepted industry practices be used to isolate the from... Spar 49 14 cfr part 43 appendix d checklist from tip in accordance with the balloon manufacturer 's instructions main in. 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Template and fill it in using progressive features ( 9 ) Accessories - for improper installation and improper,... ( or the equivalent area ) rotor transmission the ________ from the rest of the repair are on at. 23, etc. ) and center section ( or the equivalent area ) or.