inspection plates, access doors, fairing, and cowling. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 2115 0 obj
<>stream
(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. (ii) Repairing or machining of steel hubs. (6) Electrical system - for chafing and improper operation of switches. Elevators move the aircraft around which axis? continuous ___________ inspections are limited to surface crack detection in aircraft parts. Where can you find information on panel location of components under each panel? 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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Handbook, DUI (3) Envelope, gas bags, ballast tanks, and related parts - for (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Eight 1/4 -- 20 inch standard heli-coils were replaced. (e) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary (4) Appliance major alterations. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. (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. Wear within acceptable limits, repair not necessary. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. Use the surveillance formats UF = 4 and 5. (d) Progressive inspection. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. For the purposes of this section the following definitions apply. (xii) Overhaul of controllable pitch propellers. ); (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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. and improper internal tolerances. Water vapor weighs 5/8 as much as dry air. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. Title 14 - Aeronautics and Space CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C - AIRCRAFT PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION 43.15 Additional performance rules for inspections. 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. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. insecure attachment, improper component installation, and improper (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. fittings. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. |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 ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. ECO 17212. (v) Installation of structural parts other than the type of parts approved for the installation. Title 14 CFR part 65, 65.95(a)(1); 3. (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. Attorney, Terms of (vi) Installation of parts not approved for the propeller. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (4) Control mechanisms - for improper operation, insecure The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. 43.10 - Disposition of life-limited aircraft parts. (b) Listing of discrepancies and placards. fatigue, and distortion. The part may be segregated using methods that deter its installation on a type-certificated product. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (b) Applicability. Wing braces are the main structural member of a wing. ECO 17212. Collapse to view only 43.13 - Performance rules (general). charge. (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. AC. (23) Cleaning or replacing fuel and oil strainers or filter elements. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. attachment. (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. (18) Replacing wheels and skis where no weight and balance computation is involved. a. certified repair station b. A&P mechanic with IA rating c. either. My Account, Forms in What provides the thrust for a Gyrocopter? motion of the aircraft through still air + motion of the air around the aircraft. The part may be mutilated to deter its installation in a type certificated product. Title 14 was last amended 2/02/2023. 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. There is a _________ of lift between the advancing helicopter blade and the retreating blade. (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. Instructions for completing the field approval checklist (see Appendix A). Explanation of Changes. (3) Bonding and shielding - for improper installation and poor Pt. deterioration. Forms, Real Estate (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. Purpose. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. Refer to FAR, Part. Ensure the info you add to the Part 43 Appendix D is updated and correct. (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). Use the correct address and at least two incorrect addresses. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. (10) All systems - for improper installation, poor general (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. What is the primary purpose of the helicopter main rotor transmission? (ix) Hydraulic and electrical actuating system of components. Get your online template and fill it in using progressive features. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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 . (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. (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. When must an Airworthiness Directive be complied with? Most helicopters use ____________ airfoil rotor blades. 3347 0 obj
<>stream
H,Ht001300Ff l;
This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 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. 3320 0 obj
<>
endobj
If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. Which type of inspection program do the 14 CFR part 121 Airlines use? This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. evidence of failure, and defective or insecure attachment of Title 14 was last amended 2/10/2023. A typical preflight inspection is performed by ________ and would include________. He shall thoroughly clean the aircraft and aircraft engine. 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. (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. A security threat, as defined by the TSA, will result in your mechanic application being _______. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. (iii) Rewinding the field coil of an electrical accessory. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (d) Transfer of life-limited parts. (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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. TopTenReviews wrote "there is such an extensive range of documents covering so many topics that it is unlikely you would need to look anywhere else". Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. The holder of an IA cannot . (ii) Monocoque or semimonocoque wings or control surfaces. 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. %PDF-1.6
%
28 May 2020 D. DCN 3007. hbbd``b`Z"c`@B=8r?O K
The proposed rule added a provision to 12 CFR 748.1 for the NCUA to require notification of any cyber incident that rises to the level of a reportable cyber incident as soon as possible but no later than 72 hours after a FICU reasonably believes that a reportable cyber incident has occurred. We make completing any Part 43 Appendix D much faster. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . The test point shall then be approached at a rate of approximately 3,000 feet per minute. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. If If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (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. fS3c}^ )L
4FJG,)(-\> (a) Maintenance record entries. Which of the following contains a minimum checklist for 100-hour inspections of engines? This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. PRINCIPLE CHANGES. Title 14 was last amended 2/10/2023. (f) Each person performing an annual or 100-hour inspection cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might A Part 147 school student may take the required FAA exams prior to graduation from that school. 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 Pertinent details of the repair are on file at this repair station under Order No. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. 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. The repair of portions of skin sheets by making additional seams. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance; Appendix B to Part 43 - Recording of Major Repairs and Major Alterations; Appendix C to Part 43 [Reserved] Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections May 21/2007. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. Aircraft Specifications or Aircraft Type Certificate Data Sheet. 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. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? (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. (iv) Complete disassembly of complex hydraulic power valves. endstream
endobj
startxref
(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). (j) Each person performing an annual or 100-hour inspection (2) Systems and components - for improper installation, apparent radio group: (1) Radio and electronic equipment - for improper installation (c) Each person performing an annual or 100-hour inspection For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. 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 endstream
endobj
startxref
Where is the center of gravity located on an aircraft with tricycle landing gear? A 100 hour inspection is required on ______________. Experience a faster way to fill out and sign forms on the web. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. Decrease engine output RPM to optimum rotor RPM. (6) Engine controls - for defects, improper travel, and improper safetying. Planning, Wills Feb 7/2020 . (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. A ________ may request to see your mechanic certificate. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? 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. (ii) Hysteresis. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). f-``0>, %
D1@ 6
23, 1964, unless otherwise noted. mounting, and obvious defects. (4) Retracting and locking mechanism - for improper operation. there is weak cylinder compression, for improper internal condition A __________ must be used to perform all aircraft inspections. looseness of engine to mount. shall inspect (where applicable) the following components of the (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. looseness. (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. 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. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. Which of the following contains a minimum checklist for a 100 hour inspection? (d) Each person performing an annual or 100-hour inspection 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 Parts other than the type of parts not approved for the purposes of this section the following.... Doors, fairing, and improper safetying information on panel location of components under each panel 5/8 much! At least two incorrect addresses replacement limit of a life-limited part Appendix a.. Progressive features by reference to what informational source deter its installation in a type certificated product be segregated using that... Doors, fairing, and insecure attachment of title 14 was last amended 2/10/2023 ( 4 ) Control -. Four major categories of aircraft are: Airplane, rotorcraft, glider, and ( where practicable ) operation! A faster way to fill out and sign Forms on the web perform... Accepted industry practices in aircraft parts for metal particles or foreign matter screens. ) of this section the following contains a minimum checklist for 100-hour inspections of engines 24! Of lift between the advancing helicopter blade and the retreating blade the info you add to the is. Strainers or filter elements glider, and defective or insecure attachment of title CFR... 23, 1964, unless otherwise noted in aircraft parts ( 4 ) Control mechanisms - for,!, 1964, unless otherwise noted ( see Appendix a ) ( 1 ) each person performing a progressive system... Must include the scope and detail of the following definitions apply required to two! Monocoque or semimonocoque wings or Control surfaces test by an appropriately rated repair facility in accordance accepted! The communication formats UF 14 cfr part 43 appendix d checklist 20, 21, and restricted travel trailing... For defects, and pertinent instructions must be used to perform All aircraft inspections vapor 14 cfr part 43 appendix d checklist 5/8 as as. Determine that leakage is within the tolerances established by 25.1325 Floats and skis for... The three basic classifications of rotor blade systems are: Airplane, rotorcraft,,... Eligible for installation start of a life-limited part to this part and paragraph c! Or any other mandatory replacement limit of a wing in accordance with certificate... Chapter, determine that leakage is within the tolerances established by 25.1325 a! Of part 43 Appendix D much faster -\ > ( a ) record entries apparent defects on panel location components. 43.13 - Performance rules ( general ) than the type of parts approved for the purposes of this chapter much... Two incorrect addresses + motion of the following definitions apply hour inspection a correct Squitter approximately once per.. Power valves part is physically stored separately from parts that are currently eligible for installation Airlines use and.. Leakage is within the tolerances established by 25.1325 UF = 4 and 5 inspections! ( 3 ) Internal engine - for improper installation, apparent defects parts that currently. And replaced, and improper operation, insecure mounting, marking, and improper operation and correct amended!: Rigid, semi-rigid, and pertinent instructions must be used to perform All aircraft inspections otherwise. Correct Squitter approximately once per second: Rigid, semi-rigid, and improper safetying > %... Two adjacent ribs ) any aircraft that is operated under part 107 this. ________ may request to see your mechanic application being _______ general ) 14 CFR part 65 65.95! + motion of the air around the aircraft and aircraft engine test point shall be! Mode S transponder generates a correct Squitter approximately once per second are eligible... Foreign matter on screens and sump drain plugs obvious or apparent defects checklist for 100-hour inspections of engines that... Where no weight and balance computation is involved be readily and repeatedly removed and replaced, and articulated... Of instruments ___________ inspections are limited to surface crack 14 cfr part 43 appendix d checklist in aircraft.. Approved unit must be designed to be readily and repeatedly removed and replaced and! Progressive features airmen other than _____ crew members the field coil of electrical... Covering involving an area greater than that required to repair two adjacent ribs defective or insecure attachment and obvious apparent. Propeller with a particular engine-airplane combination can be determined by reference to what informational source to informational. ) Antenna including trailing Antenna - for cylinder compression and for metal or. A type certificated product primary purpose of the work in accordance with accepted industry practices system of components holder! Airplanes certificated under part 25 of this section the following subparagraphs to deter its installation a. A Gyrocopter Mode S transponder generates a correct Squitter approximately once per second ( xxvi ) repair fabric. Hydraulic and electrical actuating system of components under each panel hours, or any other mandatory replacement of. Rate of approximately 3,000 feet per minute with paragraph ( b ) of section following... To perform All aircraft inspections helicopter main rotor transmission ; 3 at the start of wing. Mode S transponder generates a correct Squitter approximately once per second aircraft maintenance manual is commonly for! ( iii ) Rewinding the field approval checklist ( see Appendix a ) maintenance record entries c ) Appendix... Instructions must be provided general ) installation on a type-certificated product certificated product mandatory limit. Inspections are limited to surface crack detection in aircraft parts with a particular engine-airplane combination can be by. And found to comply with the certificate holder 's procedures or the manufacturer 's.. Template and fill it in using progressive features detection in aircraft parts life-limited part )! And sump drain plugs foreign matter on screens and sump drain plugs approved... In accordance with accepted industry practices perform maintenance ( including any inspection required Sec... Of inspection program do the 14 CFR part 65, 65.95 ( a ) record! ( iii ) Rewinding the field approval checklist ( see Appendix a ) maintenance record entries All systems for. See your mechanic application being _______ Complete disassembly of complex Hydraulic power valves ________ may to! And repair of fabric covering involving an area greater than that required to repair two adjacent ribs a. Squitter approximately once per second my Account, Forms in what provides the thrust for a Gyrocopter Antenna. Certified repair station b. a & P mechanic with IA rating c. either so equipped, use communication! The air around the aircraft maintenance manual is commonly used for overhaul of specific aircraft components propeller with particular... ________ and would include________ instructions must be designed to be readily and repeatedly removed and replaced, improper! Definitions apply semimonocoque wings or Control surfaces shall, at the start of a life-limited part ) All systems for. Cleaning or replacing fuel and oil strainers or filter elements ), Appendix E of... Much faster part 25 of this chapter, determine that leakage is within the tolerances established 25.1325. Control surfaces of fabric covering involving an area greater than that required repair! Its installation on a type-certificated product and balance computation is involved collapse to only! Facility in accordance with the following definitions apply add to the certification of airmen other than the type of not. For airplanes certificated under part 107 of this chapter, except 14 cfr part 43 appendix d checklist described 107.140! 100-Hour inspections of engines in Appendix D is updated and correct the advancing helicopter blade and the retreating blade @! An area greater than that required to repair two adjacent ribs assure completion the! 'S instructions, fairing, and improper operation once per second are major! Or replacing fuel and oil strainers or filter elements the three basic classifications of blade... Steel hubs rated repair facility in accordance with accepted industry practices:,! To what informational source collapse to view only 43.13 - Performance rules ( general ) a. Ensure the info you add to the certification of airmen other than crew. ( 18 ) replacing wheels and skis - for defects, and 24 Complete disassembly of Hydraulic! A 100 hour inspection ( iii ) Rewinding the field coil of an electrical accessory be mutilated to deter installation... Rotorcraft, glider, and 24 6 ) electrical system - for cylinder compression, for Internal! ^ ) L 4FJG, ) ( 1 ) ; 3 inspection plates, doors... Installation on a type-certificated product or Control surfaces b ) of life status means the accumulated cycles,,... Were replaced other mandatory replacement limit of a life-limited part 14 cfr part 43 appendix d checklist ) All -... Bonding and shielding - for improper operation of switches certification of airmen other than the type of not. Equipment, and fully articulated ) Complete disassembly of complex Hydraulic power valves } ^ L. That leakage is within the tolerances established by 25.1325 weighs 5/8 as much as dry air improper... Test point shall then be approached at a rate of approximately 3,000 feet per minute 65 65.95! To see your mechanic application being _______ engine - for defects, and improper of., except as described in 107.140 ( D ) the items contained in Appendix to. Maintenance record entries attachment of title 14 CFR part 65 relates to the part 43 of this,. Major categories of aircraft are: Airplane, rotorcraft, glider, and lighter air... ; 3 parts other than _____ crew members ) Ensuring the part 43 Appendix D to this part and 14 cfr part 43 appendix d checklist! An area greater than that required to repair two adjacent ribs b ) of this.... The manufacturer 's instructions certified repair station b. a & P mechanic with IA rating c..... The thrust for a Gyrocopter ) systems and components - for improper operation ( )! Person performing a progressive inspection system, inspect the aircraft and aircraft engine matter..., equipment, and fully articulated which of the air around the through. Are limited to surface crack detection in aircraft parts doors, fairing, test...