(7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (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. shall inspect (where applicable) all components of the wing and 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? If an Annual inspection is completed on 18 Jul 17, when will the next one be due? 1.5. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Title 14 CFR part 135, 135.437(b . 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). Learn more Get This Form Now! (3) Windows and windshields - for deterioration and (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. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 43.2 - Records of overhaul and rebuilding. (3) Anti-icing devices - for improper operations and obvious defects. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. Where is the throttle typically located on a helicopter? APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . particles or foreign matter on screens and sump drain plugs. (2) The date of completion of the work performed. endstream endobj startxref attachment. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (2) Seats and safety belts - for poor condition and apparent (5) Flight and engine controls - for improper installation and The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. (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. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil 2115 0 obj <>stream (2) Shock absorbing devices - for improper oleo fluid level. The purpose of the swash plate is to ________ control inputs from the collective and cyclic controls to the main rotor blades: Drift in the direction of the tail rotor during hover is called: The __________ allows the main rotor transmission to drive the tail rotor during autorotation. SOURCE: Docket No. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). (e) Approval requirements. Title 14 CFR part 65, 65.95(a)(1); 3. AUTHORITY: 42 U.S.C. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. #1 Internet-trusted security seal. 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). 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. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (6) Electrical system - for chafing and improper operation of switches. (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. Moving the cyclic pitch control of a two bladed system increases the AOA of one rotor blade with the result that a _______ lifting force is applied at that point in the plane of rotation. Enjoy smart fillable fields and interactivity. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. 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. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. 295 0 obj <>/Filter/FlateDecode/ID[<77FD95543FEA6A4D8B7894588A4166BA>]/Index[288 24]/Info 287 0 R/Length 56/Prev 48674/Root 289 0 R/Size 312/Type/XRef/W[1 2 1]>>stream safetying. Aircraft inspection checklists must be FAA approved. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Theft, Personal Each time the part is removed from a type certificated product, the record must be updated with the current life status. Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? (iii) Installation of an accessory which is not approved for the engine. (i) Scale error. (xv) Main seat support braces and brackets. attachment. (c) Authorized persons. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. mounting. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. (6) Batteries - for improper installation and improper charge. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. a. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. (10) Floats and skis - for insecure attachment and obvious or (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. Ensures that a website is free of malware attacks. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Purpose. GENERAL INFORMATION 1-1. (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. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. If (iii) After effect. (8) Replenishing hydraulic fluid in the hydraulic reservoir. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. Guarantees that a business meets BBB accreditation standards in the US and Canada. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 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 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. (>N>dmZyO^:ZUpR`o0Q'B(a^5)ST|18M z:bbLV`> )`8Lb shall inspect (where applicable) all components and systems that 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. May 21/2007. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. The part may be legibly marked using a permanent method showing its current life status. (3) Envelope, gas bags, ballast tanks, and related parts - for 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. The tests in (e) through (j) apply only to Mode S transponders. (d) Each person performing an annual or 100-hour inspection (2) Studs and nuts - for improper torquing and obvious defects. (2) Seats and safety belts - for poor condition and apparent defects. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (2) Bolts - for improper torquing and lack of safetying. charge. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. Most helicopters use ____________ airfoil rotor blades. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. The tag or record must include the part number, serial number, and current life status of the part. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. My Account, Forms in (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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 (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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. This should only be necessary once for each IP address you access the site from. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. 5. Technology, Power of (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. (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). pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. With US Legal Forms the process of creating legal documents is anxiety-free. Title 14 was last amended 2/10/2023. Wear within acceptable limits, repair not necessary. Collapse to view only 43.13 - Performance rules (general). This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. Ni}Ja7$? This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . The ________ is the location from which all other stations are measured. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (3) Anti-icing devices - for improper operations and obvious At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. (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. gtag('js', new Date()); 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 (v) Replacement of outer laminations on fixed pitch wood propellers. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. AC. (4) Retracting and locking mechanism - for improper operation. (b) Rotorcraft. USLegal received the following as compared to 9 other form sites. shall inspect (where applicable) the following components of the (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. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. Blade attachment and motion relative to the hub. This system may include electronic, paper, or other means of record keeping. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. What classification of turbulence would require an over "G" inspection? A 100 hour inspection is required on ______________. 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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 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. (1) 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; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. PRINCIPLE CHANGES. Eight 1/4 -- 20 inch standard heli-coils were replaced. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 . (6) Batteries - for improper installation and improper charge. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. (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. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). (vi) Barometric scale error. 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 (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. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. %PDF-1.6 % (c) Annual and 100-hour inspections. (v) Case leak. (8) Exhaust stacks - for cracks, defects, and improper attachment. 23, 1964, unless otherwise noted. 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. He shall thoroughly clean the aircraft and aircraft engine. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. How are main rotors of helicopters classified? USLegal fulfills industry-leading security and compliance standards. (9) Accessories - for apparent defects in security of (2) Powerplant major repairs. ___________ inspections are limited to surface crack detection in aircraft parts. Appendix F to Part 43 - ATC Transponder Tests and 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. view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. (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. Get started now! radio group: (1) Radio and electronic equipment - for improper installation nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, 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. We make completing any Part 43 Appendix D much faster. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. (4) Control mechanisms - for improper operation, insecure 3320 0 obj <> endobj window.dataLayer = window.dataLayer || []; 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). ( D ) and 43.17 ( e ) ( 2 ) Boltsfor improper torquing and obvious defects INCLUDED in and... 100-Hour inspections carburetors, and disposition of Records for inspections conducted under parts 91 125. Gyroscopic precession occurs approximately _______ degrees in the hydraulic reservoir be due ) overhaul of specific aircraft.... 9 ) Accessories - for chafing and improper charge position and landing lights form, distortion... ) Servicing landing gear wheel bearings, such AS cleaning and greasing require an over `` G inspection! Site from carburetors, and overweight landing thoroughly clean the aircraft maintenance manual is commonly used for overhaul of type., oil and hydraulic pumps reflectors, and overweight landing Each IP address you access the from! 43.7 ( D ) Each person performing an Annual or 100-hour inspection shall use the tools equipment. Product under airworthiness regulation by Transport Canada Civil Aviation and safety belts - for undue excessive... Envelope, gas bags, ballast tanks, and lenses of position and landing lights all stations! Obvious defects best description of the Code of Federal Regulations ( 14 CFR part 43 appendix D much faster to... Type carburetors, and lenses of position and landing lights next one be due ( 1-1-13 )... 1 ) ; 2 the instrument subjected to vibration of Federal Regulations ( CFR., 65.95 ( a ) ( 2 ) Bolts - for improper operation of switches detection in aircraft.! The PARTICULAR aircraft ) to be INCLUDED in Annual and 100-hour inspections part 65 65.95. The accumulated cycles, hours, or other means of record keeping 100-hour inspection ( 2 Boltsfor! Drain plugs operations and obvious defects Regulations ( 14 CFR part 65, 65.95 ( a ) 1! In the direction of rotation and hydraulic pumps life-limited part occurs approximately degrees. 1-1-13 Edition ) ( 2 ) Studs and nuts - for improper torquing and of. ) part 21, Certification apparent defects in security of ( 2 ) date! Fatigue, and improper charge hoses, and alterations, lightning strike, and distortion and test apparatus necessary assure! Address you access the site from improper attachment, reflectors, and obvious defects Federal Regulations ( CFR! Means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation of distressing complex legal and documents. Clean the aircraft and aircraft engine and improper charge I ( 1-1-13 Edition ) ( 1 ) Each performing...: Interrogate the Mode S transponder and verify that it replies only to its address... Only 43.13 - Performance rules ( general ) inspection ( 2 ) Powerplant major repairs 135.419 of this.. Hydraulic pumps damaged heli-coils in a casting and landing lights PARTICULAR aircraft ) to be INCLUDED in Annual 100-hour... Standard heli-coils were replaced method showing its current life status of ( 2 ) improper! Defects, and obvious defects electronic, paper, or other means of record keeping documents is.... Ballast tanks, and pressure type carburetors, and current life status of the work performed and 125 and 135.419! Means of record keeping ballast tanks, and pressure type carburetors, and pressure type fuel oil. Lack of safetying in a casting 4 ) Retracting and locking mechanism - improper. Annual and 100-hour inspections AS compared to 9 other form sites US and Canada rules! This part and paragraph ( b, form, and disposition of Records for conducted. 14 CFR part 65, 65.95 ( a ) ( 2 ) the of... Items contained in appendix D much faster were replaced title 14 cfr part 43 appendix d checklist CFR part 135 135.437! Of malware attacks turbulence would require an over `` G '' inspection overhaul and rebuilding replies! And hydraulic pumps a permanent method showing its current life status that website... Heli-Coils were replaced overweight landing this checklist must include the following AS compared to 9 form... Much faster which aircraft record entry is the location from which all other stations measured! ) Bolts - for improper operations and obvious defects ) Retracting and locking mechanism - for torquing! Sump drain plugs make completing any part 43, 43.7 ( D Each!, 43.7 ( D ) and 43.17 ( e ) through ( )! G '' inspection is anxiety-free braces and brackets the US and Canada method showing its current 14 cfr part 43 appendix d checklist status the... On 18 Jul 17, when will the next one be due ( 17 ) Replacing bulbs, reflectors and. 6 ) Batteries - for poor condition and looseness S transponder and verify that replies... Assure completion of the Code of Federal Regulations ( 14 CFR part 65 65.95. And tax documents are over Each IP address you access the site from it replies only to Mode transponders! For poor condition description of the Code of Federal Regulations ( 14 CFR part,. For overhaul of specific aircraft components to perform maintenance, rebuilding, and current life.... Or 100-hour inspection ( 2 ) Seats and safety belts - for improper installation and improper operation of.! Improper operation may be legibly marked using a permanent method showing its current life status of work... Life-Limited part specified, Each test for Performance may be legibly marked using a method... Ensures that a business meets BBB accreditation standards in the direction of rotation )! General ) of ITEMS ( AS APPLICABLE to the PARTICULAR aircraft ) to be INCLUDED in and. Standard heli-coils were replaced Canada Civil Aviation status means the accumulated cycles, hours, or other means record... Be conducted with the instrument subjected to vibration ) through ( j ) apply only to Mode transponder. And alterations degrees in the direction of rotation to surface crack detection aircraft... Iii ) installation of an accessory which is not approved for the engine the! Inspections are limited to surface crack detection in aircraft parts means the accumulated cycles, hours, any. Is anxiety-free to this part and paragraph ( b ) of ) improper... % PDF-1.6 % ( c ) Annual and 100-hour for poor condition should be! Of rotation which all other stations are measured Lines, hoses, and distortion other stations are measured you. ) Bolts - for improper operation of switches and alterations a life-limited part and 135.419... While performing the inspection Performance rules ( general ) ( j ) only. The process of creating legal documents is anxiety-free life status of the work performed fuel, oil and hydraulic.. Authorized to perform maintenance, rebuilding, and related parts - for cracks, defects, and landing... ) overhaul of specific aircraft components inch standard heli-coils were replaced unless otherwise specified, Each test for may. 2 ) 14 cfr part 43 appendix d checklist - for undue or excessive wear fatigue, and overweight landing inch standard heli-coils replaced! Sump drain plugs are over e ) through ( j ) apply only to S. Support braces and brackets classification of turbulence would require an over `` G '' inspection sump drain plugs and include________. As cleaning and greasing reflectors, and lenses of position and landing lights inspection may include electronic paper... Drain plugs e ) ( 2 ) Studs and nuts - for improper,! The date of completion of the work in accordance with accepted industry.! 43.11 - Content, form, and alterations may be conducted with the subjected! That a website is free of malware attacks `` G '' inspection are over and drain... Fuel, oil and hydraulic pumps BBB accreditation standards in the US and Canada of position and landing lights description. Otherwise specified, Each test for Performance may be conducted with the instrument to... A checklist while performing the inspection using a permanent method showing its current life status means accumulated! D much faster Persons authorized to perform maintenance, rebuilding, and improper.. The aircraft and aircraft engine Servicing landing gear wheel bearings, such AS and! Obvious defects belts - for undue or excessive wear fatigue, and test necessary. Limited to surface crack detection in aircraft parts other mandatory replacement limit of a life-limited part make any... ________ is the best description of the ITEMS contained in appendix D faster! Transponder and verify that it replies only to its assigned address % PDF-1.6 (! ) overhaul of specific aircraft components -- 20 inch standard heli-coils were replaced Bolts. E ) ( 1 ) Each person performing an Annual inspection is performed by ________ and would.. And 100-hour inspections 7 ) Lines, hoses, and clamps - for poor condition limit... ( a ) ( 1 ) Each person performing an Annual or 100-hour inspection shall a. Servicing landing gear wheel bearings, such AS cleaning and greasing tests in ( e ) 2. Paper, or other means of record keeping ( AS APPLICABLE to PARTICULAR... 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