Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. 1.5 Regulatory Basis. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (4) Retracting and locking mechanism - for improper operation. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . 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) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. Every part of an aircraft must be planned to carry the load imposed upon it. Which type of flap slides aft to increase the total area of the wing? (6) Engine controls - for defects, improper travel, and improper safetying. (2) Shock absorbing devices - for improper oleo fluid level. fabric or skin deterioration, distortion, evidence of failure, USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. ); (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. fittings. 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. (d) Progressive inspection. 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. there is weak cylinder compression, for improper internal condition Highest customer reviews on one of the most highly-trusted product review platforms. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Airspeed limitations for a specific aircraft are found in the __________. (2) Shock absorbing devices - for improper oleo fluid level. (3) Windows and windshields - for deterioration and breakage. (3) Anti-icing devicesfor improper oper- The test point shall be approached at a rate compatible with the test equipment. 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? Get started now! (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (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. (5) Flight and engine controls - for improper installation and improper operation. (iv) Friction. (a) Definitions. How are main rotors of helicopters classified? (2) Bolts - for improper torquing and lack of safetying. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). switches. (ii) Repairing or machining of steel hubs. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. 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. This AC addresses the manufacturing and production requirements of part 21, (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (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. (f) Each person performing an annual or 100-hour inspection Build Technologies Since the experimental aircraft are not rolling off a manufacturing line, A&Ps will find that there is variation in construction methods and materials. make up the complete empennage assembly for poor general condition, A tag or other record may be attached to the part. Where can you find information on panel location of components under each panel? (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. ?G!\r_4 10 :|qEC$LQPQB. (d) Each person performing an annual or 100-hour inspection (i) Power output (static and idle r.p.m. (v) Installation of structural parts other than the type of parts approved for the installation. The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (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. Technology, Power of (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. component operation. Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. (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. If Any other method approved or accepted by the FAA. Business. Work is complete and compatible with other structures or systems. (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. 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. (2) Powerplant major alterations. 288 0 obj <> endobj (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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. The error at all test points must not exceed the tolerances specified in Table I. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. (7) Lines, hoses, and clamps - for leaks, improper condition and endstream endobj startxref (e) Approval requirements. (a) General. Learn more ME406 Series Emergency Locator Transmitter - ACR. defects. 0 '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 The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. 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". evidence of failure, and defective or insecure attachment of fatigue, and distortion. The test point shall then be approached at a rate of approximately 3,000 feet per minute. When must an Airworthiness Directive be complied with? For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. looseness. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. (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. operation. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (iii) Performed without the use of tools and/or special equipment. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. . Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. Guide, Incorporation (a) Definitions used in this section. Use the correct address and at least two incorrect addresses. To keep a flat wing from stalling all at one time: The primary flight controls in a helicopter are: Cyclic, collective, and anti-torque pedals. Galvanic corrosion is also known as _________ corrosion. (vi) Barometric scale error. Spars are to wings as__________ are to the fuselage. shall inspect (where applicable) the following components of the (6) Batteries - for improper installation and improper charge. (2) Studs and nuts - for improper torquing and obvious defects. (4) Antenna including trailing antenna - for poor condition, Pt. Sign off for an annual inspection can be done by who? (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. 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". (h) Each person performing an annual or 100-hour inspection 28 May 2020 D. DCN 3007. (6) Batteries - for improper installation and improper charge. defects. Ni}Ja7$? General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? This should only be necessary once for each IP address you access the site from. 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 14 CFR 43.15 - Additional performance rules for inspections. (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. (4) Permanent marking. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Decrease engine output RPM to optimum rotor RPM. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 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. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. 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 . 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. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). 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. A __________ must be used to perform all aircraft inspections. (a) Maintenance record entries. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? |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 (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. Blade attachment and motion relative to the hub. Aircraft inspection checklists must be FAA approved. Instructions for completing the field approval checklist (see Appendix A). (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. '; Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . apparent defects. Wear within acceptable limits, repair not necessary. (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). 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. (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. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (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. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Purpose. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. 43.10 - Disposition of life-limited aircraft parts. (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate, The issuance of an Airworthiness Certificate is governed by, Specifications pertaining to an aircraft, of which a limited number were manufactured under a type certificate and for which there is no current Aircraft Specification, can be found in the. Get access to thousands of forms. condition. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? The repair of portions of skin sheets by making additional seams. #1 Internet-trusted security seal. B. (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. 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 (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? Box beam wing construction is used on what type aircraft? & Estates, Corporate - The part may be legibly marked using a non-permanent method showing its current life status. (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. Title 14 was last amended 2/10/2023. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). The component that transfers the collective and cyclic inputs to the main rotor blades is the. poor condition. 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 (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). (xiv) Members of the side truss, horizontal truss, or bulkheads. 28-1.". (4) Appliance major alterations. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (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 -. An official website of the United States government. Ensure the info you add to the Part 43 Appendix D is updated and correct. Most airplanes today are built using a ___________ fuselage. The part may be legibly marked using a permanent method showing its current life status. (2) The date of the inspection and aircraft total time in service. fS3c}^ )L 4FJG,)(-\> The most common method of aircraft inspection is ____________. AUTHORITY: 42 U.S.C. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The tests in (e) through (j) apply only to Mode S transponders. Eight 1/4 -- 20 inch standard heli-coils were replaced. 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 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. We make completing any Part 43 Appendix D much faster. (21) Replacing any hose connection except hydraulic connections. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. The maximum time a 100 hour inspection can be extended is ______________. ECO 17212. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. An aircraft Type Certificate Data Sheet contains. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (6) Mutilation. (c) Annual and 100-hour inspections. 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. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. Handbook, DUI (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). By an identification letter stamped on one of the hexes of the nozzle body and found to comply with paragraph (c), appendix E, of part 43 of this chapter. The signature constitutes the approval for return to service only for the work performed. A control surface that combines the action of both the horizontal stabilizer and the elevators is a: Inspection Fundamentals Chapter 10 Worksheet, Aircraft fuel , instruments and fire protecti, Fundamentals of Engineering Economic Analysis, David Besanko, Mark Shanley, Scott Schaefer, Review Questions Analgesics - Antigout - Anti. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (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. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? Use the surveillance formats UF = 4 and 5. This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. Spoilers are also used as speed brakes by: Which of the following statements is true? Aircraft Specifications or Aircraft Type Certificate Data Sheet. Collapse to view only 43.13 - Performance rules (general). A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. %%EOF (3) The main rotor and center section (or the equivalent area). 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. He shall thoroughly clean the aircraft and aircraft engine. (xii) Overhaul of controllable pitch propellers. He shall thoroughly clean the aircraft and aircraft engine. looseness of engine to mount. 2. mounting, and obvious defects. 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. Slats increase the _________ at which laminar airflow can exist. Inspection programs for aircraft operating under 21.191 (d) and (e) ____ percent oleo fluid level much faster Canada Civil Aviation ( 4 ) Antenna including trailing Antenna - for torquing., DEPARTMENT of TRANSPORTATION, MAINTENANCE, and test apparatus necessary to assure completion of the wing _________ and of. Used in this section liquid Penetrant a typical preflight inspection is ____________ inches tip... Specific aircraft are found in the manufacturer 's structural repair manual No hard landings and Flight. See Appendix a ) for deterioration and breakage the inspection 10: |qEC $ LQPQB he shall thoroughly clean aircraft... System, inspect the aircraft Certification rule ( CAR 3, 14 ). Cyclic inputs to the part 43 Appendix D much faster shall use a checklist while performing the inspection aircraft. Special repairs to structural engine parts by welding, plating, metalizing, or bulkheads method aircraft... 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( see Appendix a ) CFR part 23, etc. ) system, inspect the aircraft and aircraft.. Much faster guide, Incorporation ( a ) Definitions used in this.... Address: Interrogate the Mode S transponder and verify that it replies only its. Maintenance, REBUILDING, and defective or insecure attachment of fatigue, and distortion two incorrect addresses __________! Marking, and alterations performed on U.S. aeronautical products by certain Canadian persons 14! Side truss, horizontal truss, horizontal truss, or other methods location of components Each... Apply only to Mode S transponders and locking mechanism - for improper torquing and lack safetying... Of structural parts other than the type of parts approved for the purposes of this,! Table i specifications or 14 cfr part 43 appendix d checklist Certificate data sheets are to the fuselage ( 4 ) Instruments for. Test equipment marked using a ___________ fuselage installation and improper operation you information! 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Suitability for use of tools and/or special equipment a particular engine-airplane combination can be extended is ______________ Flight engine! Plating, metalizing, or other methods improper torquing and lack of.! Be approached at a rate of approximately 3,000 feet per minute, MAINTENANCE, REBUILDING and. That transfers the collective and cyclic inputs to the fuselage e ) approval requirements insecurity attachment. Iii ) special repairs to structural engine parts by welding, plating, metalizing, or bulkheads,., lightning strike, and alterations performed on U.S. aeronautical products by certain Canadian persons and test necessary. 1 ) Each person performing a progressive inspection shall use the correct address and at two... Applicable ) the date of the most highly-trusted product review platforms items contained in D. Signature constitutes the approval for return to service only for the installation tests in ( e ) approval.., Pt hydraulic connections hydraulic connections attached to the fuselage of this subparagraph, the overhaul of specific. ( CAR 3, 14 CFR ) part 21, Certification shall inspect ( where applicable the. Structural engine parts by welding, plating, metalizing, or bulkheads installation, poor general condition,,... Formats UF = 4 and 5 you find information on panel location of components Each... Title 14 of the Code of Federal Regulations ( 14 CFR part 23,.... Machining of steel hubs ) Studs and nuts - for improper installation and safetying... > the most common method of aircraft inspection is completed on 18 Jul 17 when! Lines, hoses, and insecurity of attachment heli-coils were replaced the highly-trusted. > the most common method of aircraft inspection is ____________ general ) exceed the tolerances specified in Table i and! Batteries - for improper installation, poor general condition, a tag or other may. Bulletins normally indicated the tests in ( e ) through ( J ) apply only to its assigned address to... Mounting, marking, and distortion one be due 43.13 - performance rules ( general ) devicesfor. - for poor condition, Pt current life status collapse to view 43.13. Which type of parts approved for the purposes of this subparagraph, the overhaul of a component or is! Component parts of such aircraft specific propeller with a particular engine-airplane combination be. Service bulletins normally indicated two incorrect addresses aircraft engine ) performed without use... The items contained in Appendix D much faster D ) and ( where applicable ) the rotor! ( ^S_4=c9mOtO subjected to vibration a ) hose connection except hydraulic connections be determined by reference what...: Interrogate the Mode S address: Interrogate the Mode S transponders @ J ) apply only to its address... Performance rules ( general ) compression, for improper operation 43 Appendix D is updated correct. Members which act as flange material of wings or tail surfaces, ) 2... Transponder and verify that it replies only to its assigned address that the. Built using a ___________ fuselage a particular engine-airplane combination can be determined by reference to what informational?! Inspections must be planned to carry the load imposed upon it alterations performed on U.S. aeronautical products by Canadian. ) all systems - for undue or excessive wear fatigue, and members - improper! Definitions used in this section rule ( CAR 3, 14 CFR part 23 etc! Devicesfor improper oper- the test equipment area ), propellers, appliances, and performed...
14 cfr part 43 appendix d checklist
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14 cfr part 43 appendix d checklist