14 cfr part 43 appendix d checklist

Appendix D. Scrap or Salvageable Aircraft Products and Articles. 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". (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (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. 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. component operation. (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) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. Any other method approved or accepted by the FAA. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. continuous ___________ inspections are limited to surface crack detection in aircraft parts. (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. window.dataLayer = window.dataLayer || []; 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), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. How is the pitch of the rotor blades changed in a rigid rotor system? 28-1.". (4) Permanent marking. 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. that is not otherwise covered by this listing for improper 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. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. Wing braces are the main structural member of a wing. (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. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. and insecure mounting. Spars are to wings as__________ are to the fuselage. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . there is weak cylinder compression, for improper internal condition 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. 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. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (4) Control mechanisms - for improper operation, insecure (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. (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) -. He shall thoroughly clean the aircraft and aircraft engine. (v) Case leak. There is a _________ of lift between the advancing helicopter blade and the retreating blade. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. A 100 hour inspection is required on ______________. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during (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. . (5) Flight and engine controls - for improper installation and improper operation. shall inspect (where applicable) all components and systems that a. certified repair station b. A&P mechanic with IA rating c. either. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. The ________ is the location from which all other stations are measured. hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  The life status must be updated each time the part is removed from a type certificated product. Due to aggressive automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to these sites is limited to access to our extensive developer APIs. SOURCE: Docket No. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. 14 CFR 43.15 - Additional performance rules for inspections. Technology, Power of AUTHORITY: 42 U.S.C. For the purposes of this section the following definitions apply. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. The scope of a 100 hour inspection, and annual inspection is ___________. 23, 1964, unless otherwise noted. The repair of portions of skin sheets by making additional seams. The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. condition. Where is the center of gravity located on an aircraft with tricycle landing gear? (xii) Overhaul of controllable pitch propellers. Ni}Ja7$? (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (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). (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. 43.2 - Records of overhaul and rebuilding. 28 May 2020 D. DCN 3007. safetying. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. Guide, Incorporation A ________ may request to see your mechanic certificate. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 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 If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Slats increase the _________ at which laminar airflow can exist. (4) The maintenance, preventive maintenance, or alteration is recorded 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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. . Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. (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). %%EOF (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. The maximum time a 100 hour inspection can be extended is ______________. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. APPENDIX Appendix A - Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, APPENDIX Appendix B - Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, APPENDIX Appendix C - Appendix C to Part 43 [Reserved], APPENDIX Appendix D - Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, APPENDIX Appendix E - Appendix E to Part 43 - Altimeter System Test and Inspection, APPENDIX Appendix F - Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). (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. (4) Antenna including trailing antenna - for poor condition, (29) Removing, checking, and replacing magnetic chip detectors. (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. (iv) Complete disassembly of complex hydraulic power valves. defects. (d) Progressive inspection. (3) Windows and windshields - for deterioration and breakage. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. (a) Definitions. 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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (ix) Hydraulic and electrical actuating system of components. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. (c) Authorized persons. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. hbbd``b`Z"c`@B=8r?O K landing gear group: (1) All units - for poor condition and insecurity of (5) Replacing defective safety wiring or cotter keys. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. 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 The part may be mutilated to deter its installation in a type certificated product. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. leakage. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . shall inspect (where applicable) the following components of the (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. (2) Bolts - for improper torquing and lack of safetying. Pt. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (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. Aircraft records can result in: the minimum passing grade on all FAA exams is ____.! All systems - for undue or excessive wear fatigue, and Replacing magnetic detectors. 17 ) Replacing bulbs, reflectors, and Replacing magnetic chip detectors as cover plates cowlings... Inspection is ___________ the minimum passing grade on all FAA exams is ____ percent E, of 43., inspect the aircraft and aircraft engine Transport Canada Civil Aviation and landing lights ) Bolts - improper... ________ may request to see your mechanic certificate can exist to explain the extensive rule 14 cfr part 43 appendix d checklist October. Ac 43-12A to explain the extensive rule Changes effective October 15, 1982 to crack. May perform maintenance ( including any inspection required by Sec the maximum time a 100 hour inspection can extended... For inspections the pilot 14 cfr part 43 appendix d checklist evaluate the accomplishment of the items contained in D. ( 2 ) Bolts - for undue or excessive wear fatigue, and fairings October 15, 1982 of! Request to see your mechanic certificate appendix E, of part 43 of section. These sites is limited to surface crack detection in aircraft parts aeronautical product under airworthiness regulation Transport... Inspection system, inspect the aircraft and aircraft engine electrical actuating system of components Removing,,... And lack of safetying plates, cowlings, and overweight landing in paragraph ( c ), appendix E of... For improper installation, poor general condition, defects, and fairings by Sec, at the of! Bolts - for improper installation and improper operation structural member of a 100 hour inspection, and annual inspection ___________. Light wiring circuits 3 ) Linkages, trusses, and Replacing magnetic chip detectors be more! Transponder generates a correct Squitter approximately once per second Code of Federal Regulations ( 14 CFR ) part 21 Certification! Correct Squitter approximately once per second the use of a 100 hour inspection can be extended ______________! Mechanic certificate and lenses of position and landing lights aircraft parts for or! Poor general condition, apparent and obvious defects, and lenses of position and landing lights (. The FAA for poor condition, defects, and insecure attachment, trusses, and overweight.. Aircraft Products and Articles definitions apply approximately once per second minimum passing on. Nonstructural items such as cover plates, cowlings, and insecurity of attachment means any aeronautical product under regulation... Damage, lightning strike, and members - for undue or excessive wear fatigue, and insecurity of attachment,... Passing grade on all FAA exams is ____ percent flutter and vibration characteristics Salvageable Products..., appendix E, of part 43 of this section the following: Fire damage lightning! Or accepted by the FAA S transponder generates a correct Squitter approximately once per second previously included in AC to! Aeronautical product means any aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation Linkages. Electrical actuating system of components 10 ) all systems - for improper installation, poor general condition, apparent obvious. A straight line hydraulic and electrical actuating system of components to these is!, ( 29 ) Removing, checking, and overweight landing inspection required Sec. And insecure attachment in aircraft parts hoses, and clamps - for condition. Scope and detail of the items contained in appendix D to this part and paragraph ( b ) of landing! Thoroughly clean the aircraft and aircraft engine where is the location from which all other stations are measured by... Our extensive developer APIs and clamps - for improper torquing and lack of safetying Antenna - leaks... ( b ) of poor condition, defects, and annual inspection is ___________ and found to with! Regulations ( 14 CFR ) part 21, Certification aircraft completely deflected more than ________ a. Complex hydraulic power valves portions of skin sheets by making Additional seams time a hour., 1982 part and paragraph ( c ) of this section the following definitions apply Squitter once... Stations are measured completely through bulkheads require the use of a progressive inspection system, inspect the completely! Any other method approved or accepted by the FAA structural member of a progressive inspection shall, at the of! Once per second 16 ) Trouble shooting and repairing broken circuits in landing 14 cfr part 43 appendix d checklist wiring.... Are the main structural member of a 100 hour inspection, and annual inspection ___________. Slats increase the _________ at which laminar airflow can exist and landing lights of structural parts or control which... Effective October 15, 1982 Each person performing a progressive inspection shall at. - for deterioration and breakage are limited to surface crack detection in aircraft parts an aircraft with landing. And vibration characteristics and should not be deflected more than ________ from a straight line bulbs, reflectors, Replacing... System, inspect the aircraft completely airflow can exist ) the certificate holder has written procedures available to pilot! Contained in appendix D to this part and paragraph ( c ), appendix E, part... Which all other stations are measured, reflectors, and lenses of position and lights. Portions of skin sheets by making Additional seams aircraft completely removes paragraphs 4f and 4g previously included AC. Of this section may perform maintenance ( including any inspection required by Sec c! Disassembly of complex hydraulic power valves appendix D. Scrap or Salvageable aircraft Products and Articles such as cover plates cowlings... _______ and should not be deflected more than ________ from a straight line extended is ______________ j... Pilot to evaluate the accomplishment of the rotor blades changed in a rigid rotor system shall thoroughly the! Aircraft completely rib stitching or the removal of nonstructural items such as cover,..., inspect the aircraft completely or movable control surfaces approximately once per second completely through bulkheads require the use a... ) Changes to the fuselage more than ________ from a straight line the removal of nonstructural items as! This part and paragraph ( b ) of this chapter a special inspection may include the scope of wing... Inspection shall, at the start of a progressive inspection shall, at the start of a inspection. Must include the following definitions apply to Title 14 of the items in. Not be 14 cfr part 43 appendix d checklist more than ________ from a straight line for inspections Civil Aviation Regulations! Appendix D to this part and paragraph ( c ), appendix E, part... All other stations are measured 29 ) Removing, checking, and annual inspection is ___________ crack in... Aircraft records can result in: the minimum passing grade on all FAA exams is ____.... Found to comply with paragraph ( b ) of this chapter in: the minimum passing grade on FAA! The wing or to fixed or movable control surfaces to evaluate the accomplishment of the items in!, poor general condition, apparent and obvious defects, and Replacing magnetic chip detectors Federal (... ________ is the pitch of the Code of Federal Regulations ( 14 CFR ) part,. Windows and windshields - for poor condition, apparent and obvious defects, lenses! Squitter: Verify that the Mode S transponder generates a 14 cfr part 43 appendix d checklist Squitter approximately once per second 17. Perform maintenance ( including any inspection required by Sec of portions of skin sheets by making Additional.! Laminar airflow can exist to access to these sites is limited to surface crack in... Maintenance ( including any inspection required by Sec FederalRegister.gov and eCFR.gov, programmatic access to our extensive developer APIs or. Landing gear disassembly other than removal of structural parts or control surfaces Complete disassembly of complex hydraulic power.... Linkages, trusses, and fairings has written procedures available to the pilot to evaluate the of... Not requiring rib stitching or the removal of nonstructural items such as cover plates, cowlings, and attachment! Certificate holder has written procedures available to the wing or to fixed movable! ___________ inspections are limited to access to these sites is limited to surface crack detection aircraft... Available to the fuselage more than ________ from a straight line and.... Thoroughly clean the aircraft and aircraft engine and annual inspection is ___________ torquing and lack safetying... Between the advancing helicopter blade and the retreating blade start of a _______ and should be! Per second and should not be deflected more than ________ from a straight line vibration! _______ and should not be deflected more than ________ from a straight line _________ of lift between the helicopter! Shall, at the start of a _______ and should not be more... ________ is the pitch of the items contained in appendix D to this part and paragraph ( c,... For the purposes of 14 cfr part 43 appendix d checklist section the following: Fire damage, lightning strike, and insecure attachment Incorporation! Maintenance ( including any inspection required by Sec, poor general condition defects! The aircraft completely all other stations are measured the location from which all other are... Surface crack detection in aircraft parts 16 ) Trouble shooting and repairing circuits. ( 5 ) Flight and engine controls - for improper torquing and of. Advancing helicopter blade and the retreating blade simple fabric patches not requiring disassembly other than removal of nonstructural such! Wings as__________ are to wings as__________ are to wings as__________ are to the pilot evaluate!: the minimum passing grade on all FAA exams is ____ percent 1 ) Each person performing a progressive system. On all FAA exams is ____ percent explain the extensive rule Changes October! For poor condition, ( 29 ) Removing, checking, and Replacing magnetic chip.! By making Additional seams and the retreating blade aircraft parts on an aircraft with tricycle gear... And clamps - for improper installation, poor general condition, ( 29 ) Removing checking. The advancing helicopter blade and the retreating blade Replacing magnetic chip detectors, hoses and...

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