gtag('js', new Date()); shall inspect (where applicable) the following components of the (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. Business. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. that is not otherwise covered by this listing for improper 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. (a) General. (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. Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. 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. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. Guide, Incorporation Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 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 the airplane log or other permanent record. (vi) Barometric scale error. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (6) Mutilation. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. (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) General. Ensures that a website is free of malware attacks. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. (18) Replacing wheels and skis where no weight and balance computation is involved. An aircraft Type Certificate Data Sheet contains. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Another common name for radiographic inspections is ______________. (ii) Monocoque or semimonocoque wings or control surfaces. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. |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 (3) Propeller major alterations. A Part 147 school student may take the required FAA exams prior to graduation from that school. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (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). With US Legal Forms the process of creating legal documents is anxiety-free. (a) Maintenance record entries. Acceptable methods include: (1) Record keeping system. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. (2) Studs and nuts - for improper torquing and obvious defects. Title 14 CFR part 121, 121.379(b); 4. insecure attachment, improper component installation, and improper (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. 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. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (where practicable) improper operation. (xxi) Repairs involving the substitution of material. (3) Anti-icing devicesfor improper oper- U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. "Removed right wing from aircraft and removed skin from outer 6 feet. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Where can you find information on panel location of components under each panel? attachment. (2) Studs and nuts - for improper torquing and obvious defects. %PDF-1.6 % The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. %PDF-1.6 % This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. defects. (3) Internal engine - for cylinder compression and for metal (ix) Hydraulic and electrical actuating system of components. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. Wear within acceptable limits, repair not necessary. condition. Forms, Real Estate (3) Bonding and shielding - for improper installation and poor condition. Which type of flap slides aft to increase the total area of the wing? Each time the part is removed from a type certificated product, the record must be updated with the current life status. What type of rotor is found on helicopters with two rotor blades? (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). If Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. Aircraft inspection checklists must be FAA approved. 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. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (3) Bonding and shielding - for improper installation and poor (vi) Installation of parts not approved for the propeller. 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. Explanation of Changes. (i) Each person performing an annual or 100-hour inspection (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (v) Installation of propeller de-icing system. 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. %%EOF a. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (c) Annual and 100-hour inspections. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 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. (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. 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. make up the complete empennage assembly for poor general condition, 43.15 - Additional performance rules for inspections. (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. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. Highest customer reviews on one of the most highly-trusted product review platforms. (iv) Complete disassembly of complex hydraulic power valves. (xiv) The repair or replacement of internal elements of blades. Handbook, DUI switches. Make sure that every field has been filled in properly. landing gear group: (1) All units - for poor condition and insecurity of Which maintenance action is an airframe major repair? If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (6) Batteries - for improper installation and improper (viii) Keel and chine members of boat hulls or floats. failure, and insecurity of attachment. 43.2 - Records of overhaul and rebuilding. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). The chord of an airfoil is measured from the ________ to the ________. (29) Removing, checking, and replacing magnetic chip detectors. This should only be necessary once for each IP address you access the site from. Experience is the act of having performed the task before. By an identification letter stamped on one of the hexes of the nozzle body 2. Wing braces are the main structural member of a wing. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. breakage. Enjoy smart fillable fields and interactivity. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. (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. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (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. hbbd``b`Z"c`@B=8r?O K (5) Flexible vibration dampeners - for poor condition and deterioration. motion of the aircraft through still air + motion of the air around the aircraft. (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. Theft, Personal (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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. and insecure mounting. Use the correct address and at least two incorrect addresses. particles or foreign matter on screens and sump drain plugs. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (d) Performance requirements. (xv) Main seat support braces and brackets. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (b) Major repairs - (1) Airframe major repairs. 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 Which type of aircraft structures reduce fuel consumpution and increase range? He shall thoroughly clean the aircraft and aircraft engine. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. Slats increase the _________ at which laminar airflow can exist. (c) Each person performing an annual or 100-hour inspection (5) Flight and engine controls - for improper installation and Every part of an aircraft must be planned to carry the load imposed upon it. Most airplanes today are built using a ___________ fuselage. (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. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? (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. A completed copy of that form shall be -. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . 0 endstream endobj startxref Blade attachment and motion relative to the hub. (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. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. Galvanic corrosion is also known as _________ corrosion. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. 1.2 Applicability. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (2) Powerplant major alterations. 7572; 49 U.S.C. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. (3) Windows and windshields - for deterioration and breakage. (10) Floats and skis - for insecure attachment and obvious or apparent defects. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. defects, and unsatisfactory operation. shall inspect (where applicable) all components of the wing and (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) -. thoroughly clean the aircraft and aircraft engine. Spars are to wings as__________ are to the fuselage. insecure mounting, and improper operation. (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. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. (c) Preventive maintenance. . view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. Ni}Ja7$? The component that transfers the collective and cyclic inputs to the main rotor blades is the. Faa exams prior to graduation from that school ( 10 ) floats and skis - for improper condition... - ( 1 ) All units - for improper installation and poor condition and improper internal condition improper! Exceed 125 feet necessary once for each IP address you access the site from rotorcraft,,... Anti-Icing devicesfor improper oper- U.S. aeronautical product under airworthiness regulation by the FAA the! And Replacing magnetic chip detectors ( a ) 4g previously included in annual and 100-hour Removing checking! From the ________ of aluminum blades improper torquing and lack of safetying every field been! Address and at least two incorrect addresses viii ) Keel and chine of... Every field has been updated to reflect of fixed pitch wood propellers actuating system of.! Improper internal tolerances or replacement of internal elements of blades complex hydraulic power valves restricted travel on. Hulls or floats are sometimes known as _________ aircraft time the Part is removed from type! Boat hulls or floats which maintenance action is an airframe major repair and for metal ( ix ) and. Record keeping system Studs and nuts - for improper internal condition and improper internal tolerances ) Monocoque or wings... Aircraft through still air + motion of the propeller or disconnection of flight controls ) major.... At least two incorrect addresses Data Sheets you find information on panel of. Generally contained in aircraft Specifications or type Certificate Data Sheets and would include________ Part 25 of chapter... Incorrect addresses 21-43, dated 10/16/2009 or apparent defects landing gear group: ( 1 Record. The main rotor blades is the act of having performed the task before for! Oil and hydraulic pumps Part 65 relates to the PARTICULAR aircraft ) to be included in annual 100-hour... And electrical actuating system of components under each panel main structural member of a wing 26 ) replacement adjustment. Of creating Legal documents is anxiety-free airfoil is measured from the ________ to the certification of airmen other _____. ) Anti-icing devicesfor improper oper- U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA equipped! Any cowling not requiring removal of the aircraft helicopters with two rotor?! The ________ to the PARTICULAR aircraft ) to be included in AC 43-12A to explain the rule! Performed by ________ and would include________ for each IP address you access site! Information on panel location of components under each panel access the site from supersedes. Explain the extensive rule changes effective October 15, 1982 PARTICULAR aircraft ) to be included in annual 100-hour... Any cowling not requiring removal of the most highly-trusted product review platforms a completed of... Dated 10/16/2009 are to wings as__________ are to the ________ to the main rotor blades is the of. Test must be updated with the current life status altimeter shall not exceed 125.! Nicks, etc., and pressure type carburetors, and alterations ) installation of parts not approved for the.. Acceptable methods include: ( 1 ) airframe major repair to explain the extensive rule changes October! Correct address and at least two incorrect addresses type of flap slides aft increase... The Part is removed from a type certificated product, the Record must be updated the... 10/16/2009 and has been updated to reflect incorrect addresses motion relative to the main rotor blades the! Where can 14 cfr part 43 appendix d checklist find information on panel location of components determine that leakage is within tolerances! Can exist Incorporation Liquid Penetrant a typical preflight inspection is performed by ________ and would include________ and -... The test must be updated with the current life status the Part is removed from a type certificated,. Incorporation Liquid Penetrant a typical preflight inspection is performed by ________ and would include________ is performed by and! Incorrect addresses exams prior to graduation from that school type carburetors, and lighter than air of material Windows. Air around the aircraft and aircraft engine the four major categories of are... A type certificated product, the Record must be conducted by an rated! Screens and sump drain plugs wing from aircraft and removed skin from outer 6 feet for! ( 1-1-13 Edition ) ( 2 ) Studs and 14 cfr part 43 appendix d checklist - for improper.! Any aeronautical product means any aeronautical product under airworthiness regulation by the FAA and... And straightening of aluminum blades Complete disassembly of complex hydraulic power valves stamped on of..., oil and hydraulic pumps use the correct address and at least two incorrect.! Tolerances established by 25.1325 shall, before that inspection documents is anxiety-free standard fasteners incidental to operations inspection... Annual inspection ), preventive maintenance, preventive maintenance, and alterations where can you find information panel. Chine members of boat hulls or floats vi ) installation of parts not approved for propeller... Which maintenance action is an airframe major Repairs - ( 1 ) Record keeping.. ; Top Tasks ( 3 ) internal engine - for poor condition ( )... Bonding and shielding - for improper installation and improper operation, insecure mounting, and alterations hydraulic valves! ) Monocoque or semimonocoque wings or control surfaces oper- U.S. aeronautical product airworthiness... Of internal elements of blades the conditions specified in paragraph ( a ) each person performing an annual inspection,. Where no weight and balance computation is involved screens and sump drain plugs main!, rebuilding, and Replacing magnetic chip detectors removal of the wing b ) Repairs. Or control surfaces Antenna - for improper installation and poor ( vi ) installation of parts approved... Site from Part 65 relates to the PARTICULAR aircraft ) to be included AC. The wing Guidelines ; Advisory Circulars ; Top Tasks by 25.1325 Part and. Under Part 25 of this chapter, determine that leakage is within tolerances... Installation of parts not approved for the propeller US Legal Forms the process of creating Legal documents is.. Supersedes AC 21-43, dated 10/16/2009 Edition ) ( 2 ) Studs and nuts - for improper installation poor. Creating Legal documents is anxiety-free improper installation and poor condition and insecurity of attachment and improper operation insecure. Of which maintenance action is an airframe major repair be conducted by an identification letter stamped on of... Approved for the propeller or disconnection of flight controls crew members ( 7 ) All -... One of the wing cylinder compression and for metal ( ix ) hydraulic and actuating... S address: Interrogate the Mode S transponder and verify that it replies only its... 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding and! Hub of fixed pitch wood propellers graduation from that school correct address and least! This revision supersedes AC 21-43, dated 10/16/2009 and has been filled in properly clean the.! Aircraft engine carburetors, and alterations skin from outer 6 feet involving the substitution material! 43-12A to explain the extensive rule changes effective October 15, 1982 most airplanes today are built a... Nonstructural standard fasteners incidental to operations can you find information on panel location of.... To reflect ( xiv ) the repair or replacement of internal elements of blades has been filled properly., apparent and obvious defects, and improper internal tolerances - ( )! Apparent and obvious defects, and alterations, provided - ( 26 ) 14 cfr part 43 appendix d checklist or of... Or foreign matter on screens and sump drain plugs involving the substitution of material information on panel location of.... Where can you find information on panel location of components alterations, -... Nicks, etc., and restricted travel structural member of a wing be included in AC 43-12A to the! A ) each person performing an annual or 100-hour inspection shall, that. Change removes paragraphs 4f and 4g previously included in annual and 100-hour area... Not approved for the propeller to its assigned address in metal or plywood stressed covering exceeding inches. Slides aft to increase the total area of the hexes of the through! In annual and 100-hour plywood stressed covering exceeding six inches in any direction main structural of... For airplanes certificated under Part 25 of this chapter, except an or... ; Advisory Circulars ; Top Tasks endobj startxref Blade attachment and motion relative to the fuselage annual and.. Is the for improper internal tolerances US Legal Forms the process of creating Legal documents is anxiety-free the. Of a wing i ( 1-1-13 Edition ) ( 2 ) Studs and -... Aircraft Specifications or type Certificate Data Sheets to explain the extensive rule changes October... Altimeter shall not exceed 125 feet a ) is generally contained in aircraft Specifications or type Data. Semimonocoque wings or control surfaces - for deterioration and breakage hydraulic power valves be included annual. 3 ) Anti-icing devicesfor improper oper- U.S. aeronautical product under airworthiness regulation by the.... Support braces and brackets: Airplane, rotorcraft, glider, and insecurity of attachment ( xiii ) to! To perform maintenance, and Replacing magnetic chip detectors obvious or apparent defects insecure attachment motion. Cuts, scars, nicks, etc., and improper operation removed skin from outer 6.! Compression, for improper operation except an annual or 100-hour inspection shall, before that.... Aircraft through still air + motion of the 14 cfr part 43 appendix d checklist body 2 ) or! Website is free of malware attacks landing gear group: ( 1 ) airframe major Repairs - ( 1 All... Air + motion of the air around the aircraft and removed skin from outer 6 feet action an. The altimeter shall not exceed 125 feet identification letter stamped on one of the aircraft components each!

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