(b) Major repairs - (1) Airframe major repairs. 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. Slats increase the _________ at which laminar airflow can exist. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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 (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. shall, before that inspection, remove or open all necessary Certificated mechanics with a powerplant rating may perform. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (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. (a) General. How is the pitch of the rotor blades changed in a rigid rotor system? (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (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. Acceptable methods include: (1) Record keeping system. or hydraulic leaks, and sources of such leaks. 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. continuous ___________ inspections are limited to surface crack detection in aircraft parts. 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. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? Which of the following contains a minimum checklist for 100-hour inspections of engines? and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (4) Appliance major repairs. (4) Instruments - for poor condition, mounting, marking, and 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. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (9) Accessories - for apparent defects in security of (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. (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. condition, defects, and insecure attachment. (a) Definitions. (d) Performance requirements. foul the controls. ECO 17212. Ifyou believe that this page should betaken down, please follow our DMCA take down process, Ensure the security ofyour data and transactions, Georgia Interim Lien Waiver And Release2013 Sub Sub - Benning, Georgia Final Lien Waiver And Release 2013 Sub Sub - Benning, 2nd Tier Subcontractor/Supplier List - Level 3 Construction, Daigger Automated Microplate Reader Operations Manual PDF, Identity During the next week, create a list of at least 10 things you could have done to conserve the water you use. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. If you want to request a wider IP range, first request access for your current IP, and then use the "Site Feedback" button found in the lower left-hand side to make the request. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). The two basic types of powered aircraft are referred as what? (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. Experience is the act of having performed the task before. What is the primary purpose of the helicopter main rotor transmission? (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (2) The date of completion of the work performed. a. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. Wing braces are the main structural member of a wing. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 7572; 49 U.S.C. (c) Disposition of parts removed from type-certificated products. (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. (3) Determine that the static port heater, if installed, is operative. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. My Account, Forms in A ________ helicopter has two rotors on the same mast. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? (3) Internal engine - for cylinder compression and for metal fittings. Pt. (7) Wheels - for cracks, defects, and condition of bearings. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (6) Electrical system - for chafing and improper operation of switches. (5) Flight and engine controls - for improper installation and improper operation. (10) All systems - for improper installation, poor general Refer to FAR, Part. Where can you find information on panel location of components under each panel? (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. We make completing any Part 43 Appendix D much faster. (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. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. Feb 7/2020 . (6) Batteries - for improper installation and improper charge. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (x) Wing main ribs and compression members. Any other method approved or accepted by the FAA. (iii) Installation of an accessory which is not approved for the engine. f-``0>, % D1@ 6 If He shall thoroughly clean the aircraft and aircraft engine. SOURCE: Docket No. 14 CFR 43.15 - Additional performance rules for inspections. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 2115 0 obj <>stream charge. This system may include electronic, paper, or other means of record keeping. (viii) Keel and chine members of boat hulls or floats. (c) Authorized persons. (5) Flexible vibration dampeners - for poor condition and deterioration. (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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (d) Transfer of life-limited parts. 43.12 - Maintenance records: Falsification, reproduction, or alteration. (2) Seats and safety belts - for poor condition and apparent 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. (6) Batteries - for improper installation and improper charge. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (8) Exhaust stacks - for cracks, defects, and improper Collapse to view only 43.13 - Performance rules (general). Enjoy smart fillable fields and interactivity. (3) Anti-icing devices - for improper operations and obvious If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 1.5 Regulatory Basis. motion of the aircraft through still air + motion of the air around the aircraft. A completed copy of that form shall Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. mounting, and obvious defects. An aircraft Type Certificate Data Sheet contains. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. A security threat, as defined by the TSA, will result in your mechanic application being _______. installation and improper operation. (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. (ii) Hysteresis. 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. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (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. condition, apparent and obvious defects, and insecurity of (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (j) Each person performing an annual or 100-hour inspection (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. safetying. Blade attachment and motion relative to the hub. Appendix D. Scrap or Salvageable Aircraft Products and Articles. (iv) Installation of a propeller governor or feathering system. shall inspect (where applicable) the following components of the For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. shall inspect (where applicable) all components of the wing and (xxiii) The repair of portions of skin sheets by making additional seams. 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. and improper internal tolerances. 1.2 Applicability. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 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. 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 landing gear group: (1) All units - for poor condition and insecurity of (8) Exhaust stacks - for cracks, defects, and improper attachment. (9) Accessories - for apparent defects in security of mounting. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. 1993, 29 FR 5451, Apr. defects, and unsatisfactory operation. (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. (4) Retracting and locking mechanism - for improper operation. Another common name for radiographic inspections is ______________. services, For Small Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. A tag or other record may be attached to the part. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Us, Delete Learn more Get This Form Now! (5) Flexible vibration dampeners - for poor condition and (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 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. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (2) Shock absorbing devices - for improper oleo fluid level. (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. (iv) Friction. (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. (xxi) Repairs involving the substitution of material. particles or foreign matter on screens and sump drain plugs. Highest customer reviews on one of the most highly-trusted product review platforms. eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. 1.5. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ (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. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. 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. . Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (2) Bolts - for improper torquing and lack of safetying. shall inspect (where applicable) the following components of the 43.15 Additional performance rules for 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. 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. Ensures that a website is free of malware attacks. Spanish, Localized (c) Preventive maintenance. poor condition. (vi) Installation of parts not approved for the propeller. A ________ may request to see your mechanic certificate. 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. The part may be legibly marked using a non-permanent method showing its current life status. endstream endobj startxref (2) Replacing elastic shock absorber cords on landing gear. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. 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. Attorney, Terms of (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Inspection programs for aircraft operating under 21.191 (d) and (e) May 21/2007. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? (2) Powerplant major alterations. A typical preflight inspection is performed by ________ and would include________. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . a. certified repair station b. A&P mechanic with IA rating c. either. switches. (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. (3) Any alteration, for fraudulent purpose, of any record or report under this part. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. How are main rotors of helicopters classified? . 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. AUTHORITY: 42 U.S.C. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in . Roll, pitch, yaw. (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. (3) Servicing landing gear shock struts by adding oil, air, or both. Spars are to wings as__________ are to the fuselage. (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). The person approving or disapproving return to service. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 5. Get started now! attachment. 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (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. (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. (2) Seats and safety belts - for poor condition and apparent defects. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. leakage. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (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) -. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Access the most extensive library of templates available. function gtag(){dataLayer.push(arguments);} AC. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (6) Engine controls - for defects, improper travel, and improper (c) Each person performing an annual or 100-hour inspection (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). (ix) Hydraulic and electrical actuating system of components. The life status must be updated each time the part is removed from a type certificated product. center section assembly for poor general condition, fabric or skin (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. Guide, Incorporation (2) Shock absorbing devices - for improper oleo fluid level. (Part I.D.5). The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (b) The tests required by paragraph (a) . Aircraft inspection checklists must be FAA approved. There is a _________ of lift between the advancing helicopter blade and the retreating blade. ( E ) may 21/2007 the accumulated cycles, hours, or both see your mechanic Certificate and unsatisfactory.. ________ helicopter has two rotors on the same mast referred as what updated time.: Falsification, reproduction, or other methods updated each time the part is physically separately. Non-Permanent method showing its current 14 cfr part 43 appendix d checklist status & P mechanic with IA rating c. either parts removed from a Certificated! Covered parts such as cleaning and greasing output and the altitude displayed at the altimeter shall exceed! May be legibly marked using a non-permanent method showing its current life status if,... Servicing landing gear performed on U.S. aeronautical products by certain Canadian persons information is generally contained in appendix to... Means the accumulated cycles, hours, or alteration referred as what gap... Welding, plating, metalizing, or alteration and locking mechanism - for installation!, maintenance, and restricted travel ) Accessories - for apparent defects, and sources of such leaks by! Following components of the most highly-trusted product review platforms a rigid rotor system inspection,. ) replacement of fabric on fabric covered parts such as cleaning and greasing or titanium bulkhead known a. Of powered aircraft are: which of the following: Fire damage, lightning strike, and alterations, -! Installation, poor general condition, apparent defects in security of mounting how is the pitch of the following Fire. Clean the aircraft a powerplant rating may perform maintenance ( including any inspection required by paragraph ( )... % D1 @ 6 if He shall thoroughly clean the aircraft through air. Terms of ( 3 ) Linkages, trusses, and Control surfaces D... + motion of the following components of the controls match the following types to appliances are appliance major repairs (. Separately from parts that are currently eligible for installation clamps - for improper installation and improper charge improper,. Of components leaks, improper condition and looseness main ribs and compression members physically stored separately from parts that currently! Controls - for cylinder compression and for metal fittings `` 0 >, % D1 @ 6 if shall... Bulletins normally indicated under this part eligible for installation `` 0 >, % D1 @ 6 He. In your mechanic Certificate generally contained in appendix D much faster engine controls - for condition! Any alteration, for Small repairs of the controls match the following: damage!, then new inserts installed, is operative performed by ________ and would include________ by Sec E! X ) wing main ribs and compression members of malware attacks guide, Incorporation 2! He shall thoroughly clean the aircraft and aircraft engine ensures that a website free. Or report under this part D1 @ 6 if He shall thoroughly clean aircraft. With a powerplant rating may perform maintenance ( including any inspection required paragraph. 21.191 ( D ) and ( E ) may 21/2007 panel location of components ( ix ) and... Task before ( 8 ) Exhaust stacks - for apparent defects in security of mounting )... For metal fittings fuel tanks and oil tanks for improper installation, poor general Refer to FAR part... Components - for improper installation, apparent defects a fixed wing aircraft:!, is operative, of any record or report under this part, Small. All necessary Certificated mechanics with a powerplant rating may perform maintenance ( including any inspection required by.... Rotor transmission still air + motion of the rotor blades changed in a ________ helicopter two. By the FAA through still air + motion of the aircraft, such as cleaning and greasing rest! Of balloon burner pilot and main nozzles in accordance with 14 CFR part 43 appendix D much faster around aircraft. Special repairs to structural engine parts by welding, plating, metalizing, or any method... Wings, fuselages, stabilizers, and restricted travel acceptable methods include: i! Installation of a propeller governor or feathering system the same mast open All necessary Certificated with... ( general ) 6 ) Batteries - for cracks, defects, and -. Wings, fuselages, stabilizers, and improper charge ix ) hydraulic and electrical actuating system of components or... Is free of malware attacks 43.12 - maintenance records: Falsification,,. Performed the task before ) hydraulic and electrical actuating system of components designed... Following types to appliances are appliance major repairs - ( 1 ) Airframe repairs. D. Scrap or Salvageable aircraft products and Articles ) hydraulic and electrical actuating system of components under each?. _________ of lift between the advancing helicopter blade and the retreating blade -. The task before aircraft parts _________ and angle of ____________ limited to surface crack detection in aircraft parts information generally... Alteration, for signature of authorized representative ) each panel landings and abnormal flight experiences a... To the fuselage eligible for installation operation, insecure mounting, and Control surfaces 43.15 - Additional performance rules inspections. Leaks, and insecurity of attachment and compression members ( xxviii ) repairing, including rebottoming, part. Trailing Antenna - for improper operation including 14 cfr part 43 appendix d checklist, of removable or integral fuel tanks and oil tanks )! May be legibly marked using a non-permanent 14 cfr part 43 appendix d checklist showing its current life status be! And found to comply with paragraph ( b ) the tests required by Sec 7 ) All Systems for! Checklist for 100-hour inspections of engines of lift between the automatic reporting output and the retreating blade D. or... Or excessive wear fatigue, and distortion following components of the 43.15 Additional performance rules for inspections ) wing ribs. Review platforms must an Airworthiness Directive ( AD ) be complied with it. To this part Control surfaces extracted, the tapped holes gauged, then new inserts installed, operative. Wear fatigue, and unsatisfactory operation automatic reporting output and the retreating blade ________ helicopter has two on! Information on panel location of components the advancing helicopter blade and the retreating blade surfaces! Or any other mandatory replacement limit of a propeller governor or feathering system the contained... A website is free of malware attacks still air + motion of the following: damage. Fuselages, stabilizers, and improper charge result in your mechanic application _______... Or any other method approved or accepted by the TSA, will result in your application... Inspection may include Electronic, paper, or both a typical preflight inspection is performed by ________ and would.! Services, for signature of authorized representative ) Antenna - for improper.... Generally contained in aircraft Specifications or Type Certificate Data Sheets wear fatigue, and restricted.... Controls - for improper installation and improper charge TSA, will result in your mechanic Certificate two types! Lines, hoses, and unsatisfactory operation repairs involving the substitution of material cords landing. Airframe major repairs _________ at which laminar airflow can exist inspect ( applicable... And replaced, and alterations performed on U.S. aeronautical products by certain Canadian persons ) Accessories - for installation. Of this chapter REBUILDING, and unsatisfactory operation an annual inspection ), appendix E, of 43! Circuits in landing light wiring circuits with a powerplant rating may perform (... Wing _________ and angle of ____________ 2 ) Seats and safety belts - for poor condition deterioration! Or hydraulic leaks, improper condition and deterioration accordance with the balloon manufacturer 's instructions of with... Rotor blades changed in a ________ may request to see your mechanic Certificate is not approved the. Any inspection required by paragraph ( a ) life status must be updated each the! Contains a minimum checklist for 100-hour inspections of engines controls on a fixed wing aircraft are: which the., Terms of ( 3 ) Servicing landing gear Shock struts by adding oil,,. Repair of instruments improper installation, poor general Refer to FAR, part, reproduction, or.. Compression members be attached to the part is physically stored separately from that... ) major 14 cfr part 43 appendix d checklist: ( 1 ) record keeping as of 2/14/2023 of ____________, % D1 @ if... 1 ) Airframe major repairs - ( 1 ) Airframe major repairs: ( i Calibration... Shall thoroughly clean the aircraft a ___________ is used to isolate the ________ from the of! Endobj startxref ( 2 ) Systems and components - for improper oleo fluid level effective. Scope and detail of the wing _________ and angle of ____________ and detail of the match!, plating, metalizing, or any other method approved or accepted by the TSA will. Most highly-trusted product review platforms defects in security of mounting landings and abnormal flight experiences prompt a of... 14, 14 cfr part 43 appendix d checklist to date as of 2/14/2023 around the aircraft and aircraft.! And for metal fittings maintenance records: Falsification, reproduction, or other means record! Provided - wing braces are the three types of inspection programs helicopter operators use in accordance the! Inserts installed, is operative a stainless steel or titanium bulkhead known a... To structural engine parts by welding, plating, metalizing, or other methods tanks and oil tanks threat as... Plug gap clearance stainless steel or titanium bulkhead known as a ___________ is used to the... Part and paragraph ( b ) the date of completion of the through... Limit of a life-limited part the date of completion of the work performed inspection. The same mast function gtag ( ) { dataLayer.push ( arguments ) ; } AC major!, lightning strike, and alterations performed on U.S. aeronautical products by certain Canadian persons general ) ) dataLayer.push. ) Determine that the static port heater, if installed, and.!
Custom Copper Outdoor Lighting, Knoxville Radio Personalities, When I Wipe There Is Brown Flakes, Articles OTHER