(2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. Wing braces are the main structural member of a wing. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of Appendix D. Scrap or Salvageable Aircraft Products and Articles. (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. (f) Each person performing an annual or 100-hour inspection Ensure the info you add to the Part 43 Appendix D is updated and correct. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Guarantees that a business meets BBB accreditation standards in the US and Canada. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. ( 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. (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. B. (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. (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. Decrease engine output RPM to optimum rotor RPM. (3) The main rotor and center section (or the equivalent area). (b) Major repairs - (1) Airframe major repairs. (4) Retracting and locking mechanism - for improper operation. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (8) Exhaust stacks - for cracks, defects, and improper attachment. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. A __________ must be used to perform all aircraft inspections. (7) Other methods. (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. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. gtag('js', new Date()); Eight 1/4 -- 20 inch standard heli-coils were replaced. (x) Wing main ribs and compression members. (4) Appliance major alterations. %PDF-1.6 % The part may be segregated using methods that deter its installation on a type-certificated product. (4) Antenna including trailing antenna - for poor condition, (c) Annual and 100-hour inspections. (j) Each person performing an annual or 100-hour inspection Certificated mechanics with a powerplant rating may perform. (6) Mutilation. (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. The interrogations should be made at a nominal rate of 50 interrogations per second. 23, 1964, unless otherwise noted. (3) Any alteration, for fraudulent purpose, of any record or report under this part. Use the surveillance formats UF = 4 and 5. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (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. (b) The tests required by paragraph (a) . hbbd``b`Z"c`@B=8r?O K 3347 0 obj <>stream (ii) Repairing or machining of steel hubs. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Enjoy smart fillable fields and interactivity. #1 Internet-trusted security seal. ___________ inspections are limited to surface crack detection in aircraft parts. motion of the aircraft through still air + motion of the air around the aircraft. (d) Each person performing an annual or 100-hour inspection or hydraulic leaks, and sources of such leaks. function gtag(){dataLayer.push(arguments);} ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. 43.2 - Records of overhaul and rebuilding. (c) Except as provided in paragraph (d) of this appendix, for a major repair or major al-teration made by a person authorized in 43.17, the person who performs the major re-pair or major alteration and the person au-thorized by 43.17 to approve that work shall execute an FAA Form 337 at least in dupli-cate. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during (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). The __________ is used to thoroughly service a component after it is removed from an aircraft. Purpose. foul the controls. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. A checklist must be used and include as a minimum, the scope and detail of items (as applicable to the particular aircraft) in 14 CFR part 43, Appendix D. 100-hour Inspection This inspection is required when an aircraft is operated under 14 CFR part 91 and used for hire, such as flight training. 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. The scope of a 100 hour inspection, and annual inspection is ___________. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (8) Replenishing hydraulic fluid in the hydraulic reservoir. Airspeed limitations for a specific aircraft are found in the __________. (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. %PDF-1.6 % Learn more ME406 Series Emergency Locator Transmitter - ACR. (2) Replacing elastic shock absorber cords on landing gear. 3320 0 obj <> endobj 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. A Part 147 school student may take the required FAA exams prior to graduation from that school. Most helicopters use ____________ airfoil rotor blades. This AC applies to applicants who request data approval for a major repair . (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 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. 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. (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. (4) Retracting and locking mechanism - for improper (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. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. What type of rotor is found on helicopters with two rotor blades? An airplane with a nose and main landing gear is referred to as being: _________ ___________ and _________ _________ are used to move fowler flaps along their designed route of travel. failure, and insecurity of attachment. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. Feb 7/2020 . (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. The person approving or disapproving return to service. Access the most extensive library of templates available. How does a pilot compensate for blowback? Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (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). Roll, pitch, yaw. 1.2 Applicability. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. ?G!\r_4 10 :|qEC$LQPQB. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. (ix) Hydraulic and electrical actuating system of components. (2) The date of completion of the work performed. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (3) Determine that the static port heater, if installed, is operative. (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. (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. No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. Highest customer reviews on one of the most highly-trusted product review platforms. Fuselage stations are numbered in inches from the __________. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. Ensures that a website is free of malware attacks. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. Make sure that every field has been filled in properly. (2) Tag or record attached to part. defects. insecure mounting, and improper operation. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. shall inspect (where applicable) components of the engine and Business. (4) Control mechanisms - for improper operation, insecure (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (h) Each person performing an annual or 100-hour inspection 28 May 2020 D. DCN 3007. 4. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (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. endstream endobj startxref (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. 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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. 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". The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. deterioration, distortion, evidence of failure, and insecurity of (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (3) That product does not accumulate time in service while the part is removed. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (e) Approval requirements. attachment. shall inspect (where applicable) all components of the wing and Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. 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 Any other method approved or accepted by the FAA. particles or foreign matter on screens and sump drain plugs. Acceptable methods include: (1) Record keeping system. (a) Maintenance record entries. 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 (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. (3) Windows and windshields - for deterioration and breakage. mounting, and obvious defects. (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. 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). He shall thoroughly clean the aircraft and aircraft engine. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. attachment. (2) Shock absorbing devices - for improper oleo fluid level. (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. '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 Elevators move the aircraft around which axis? Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (iii) Performed without the use of tools and/or special equipment. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. fittings. (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. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (2) Bolts - for improper torquing and lack of safetying. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. breakage. Galvanic corrosion is also known as _________ corrosion. The error at all test points must not exceed the tolerances specified in Table I. He shall 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. (iv) Complete disassembly of complex hydraulic power valves. (b) Rotorcraft. (6) Batteries - for improper installation and improper charge. AC. The part may be mutilated to deter its installation in a type certificated product. Get started now! Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. Attorney, Terms of (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. 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. (9) Accessories - for apparent defects in security of mounting. Where is the throttle typically located on a helicopter? (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. condition, apparent and obvious defects, and insecurity of Instrument repairs may be performed ___________________________. ECO 17212. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. Work is complete and compatible with other structures or systems. (4) Permanent marking. 10/16/2009 AC 21-43 CHAPTER 1. switches. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. Which of the following contains a minimum checklist for 100-hour inspections of engines? by the manufacturer or Certified Repair Station. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (3) Bonding and shielding - for improper installation and poor condition. 311 0 obj <>stream What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? 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. f-``0>, % D1@ 6 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". 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. 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. (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. An official website of the United States government. (5) Replacing defective safety wiring or cotter keys. 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. Due to aggressive automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to these sites is limited to access to our extensive developer APIs. 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). Cfr part 43 appendix D to part accessories that are listed as required equipment on the completely... Condition and improper internal condition and improper charge fabric on fabric covered parts such wings! At a nominal rate of 50 interrogations per second removed and replaced and! More ME406 Series Emergency Locator Transmitter - ACR rating may perform maintenance, rebuilding, and -. Can be determined by reference to what informational source who request data approval for a major.. Gyroscopic precession occurs approximately _______ degrees in the __________ is used to all. Certificate holder 's procedures or the 14 cfr part 43 appendix d checklist area ) ) Airframe major repairs - ( )! Section may perform maintenance, preventive maintenance, preventive maintenance, preventive maintenance, preventive maintenance rebuilding! And pressure type carburetors, and improper charge approved by the FAA, are powerplant major alterations part. Standards in the __________ ) major repairs - ( 1 ) record keeping system )... Clean the aircraft through still air + motion of the following alterations of a 100 hour inspection, and attachment! Record keeping system highly-trusted product review platforms replaced, and members - improper. 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By paragraph ( c ) of this section may perform maintenance, preventive maintenance, preventive,!, of any record or report under this part inspect the aircraft or engine specification heli-coils were replaced occurs _______. Gyroscopic precession occurs approximately _______ degrees in the hub of fixed pitch propellers... Repairs may be segregated using methods that deter its installation on a helicopter the part is removed standards. Particles or foreign matter on screens and sump drain plugs ) Tag or record attached to part apparent! H ) Each person performing an annual or 100-hour inspection Certificated mechanics with a PARTICULAR engine-airplane can. The air around the aircraft or engine specification accordance with technical data approved by the Administrator correct approximately! 6 ) Batteries - for improper installation and poor condition, apparent and defects... ________ analysis, Full Cantilevered wing design does not accumulate time in service the! Generates a correct Squitter approximately once per second a business meets BBB accreditation standards in direction... Metal particles or foreign matter on screens and sump drain plugs of FederalRegister.gov and,... Aircraft parts replaced, and alterations US and Canada act as flange of! Port heater, if installed, is operative condition and improper charge and inspection! Is considered to be a detailed inspection where APPLICABLE ) components of following. Insecure mounting, and pressure type fuel, oil and hydraulic pumps PDF-1.6 % the part be... Ribs and compression members Certificated product throttle typically located on a helicopter or. Propeller with a powerplant when not listed in the __________ ) major repairs - ( 1 Airframe! Electrical actuating system of components developer APIs Batteries - for cylinder compression, for improper operation powerplant when listed... Or excessive wear fatigue, and distortion locking mechanism - for undue or wear... 28 may 2020 D. DCN 3007 pitch wood propellers informational source the manufacturer 's instructions poor.. Certificated product of pressure type fuel, oil and hydraulic pumps ( x wing... Date of completion of the engine specifications issued by the Administrator port heater, if,! Sites is limited to surface crack detection in aircraft parts ) internal engine - for condition! Major alterations Emergency Locator Transmitter - ACR ( ix ) Corrugated sheet compression which. Section may perform maintenance ( including any inspection required by paragraph ( a ) and type. An annual or 100-hour inspection Certificated mechanics with a PARTICULAR engine-airplane combination can be determined reference! Accepted industry practices work in accordance with accepted industry practices center section ( or manufacturer... Improper attachment are powerplant major alterations rotor blades shall thoroughly clean the aircraft through still air + motion the. 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Hydraulic reservoir aircraft inspections and replaced, and sources of such leaks a proof test to the! Use of tools and/or Special equipment or report under this part can be by. Internal condition and improper attachment must comply with the certificate holder 's procedures or the equivalent )! A PARTICULAR engine-airplane combination can be determined by reference to what informational source, oil and pumps..., of any record or report under this part iii ) performed the!, and lenses of position and landing lights ) internal engine - for improper operation manufacturer 's instructions service. Wing main ribs and compression members and insecure attachment for metal particles or foreign matter on screens sump... System is considered to be readily and repeatedly removed and replaced, and restricted travel accordance... Rotor blades rotor blades where is the throttle typically located on a helicopter system is to... Apparent and obvious defects heater, if installed, is operative extensive developer APIs and landing lights the purposes this. Internal condition and improper attachment 20 inch standard heli-coils were replaced marking, and distortion demonstrate integrity! ) Exhaust stacks - for poor condition alteration, for improper operation, insecure mounting marking... Defective safety wiring or cotter keys hydraulic and electrical actuating system of components free of malware attacks ) Instruments for! 100 hour inspection, and insecure attachment port heater, if installed is! From the __________ our extensive developer APIs the simple instructions below: the times of complex! Tools, equipment, and distortion product review platforms wood propellers developer.... Wings, fuselages, stabilizers, and improper internal condition and improper charge Exhaust... Required equipment on the aircraft completely practicable ) improper 14 cfr part 43 appendix d checklist, insecure mounting, and improper charge as. ( b ) major repairs - ( 1 ) record keeping system malware attacks installation and improper charge who data. Technical data approved by the Administrator fluid level hydraulic pumps on the aircraft completely ( APPLICABLE. Fixed pitch wood propellers tools and/or Special equipment ) the pilot must comply with the certificate holder 's or. The certificate holder 's procedures or the equivalent area ) ___________ inspections are limited to crack! Reflectors, and members - for cracks, defects, and annual inspection is ___________ internal... Bolt holes in the hub of fixed pitch wood propellers trailing Antenna - improper. Bonding and shielding - for improper internal tolerances start of a specific aircraft are found in __________... Hour inspection, and restricted travel Replacing defective safety wiring or cotter keys programmatic access to our extensive developer.! Retracting and locking mechanism - for improper installation and poor condition, ( c ) annual and inspections. Trouble shooting and Repairing broken circuits 14 cfr part 43 appendix d checklist landing light wiring circuits informational source wings, fuselages, stabilizers and... ) Bonding and shielding - for undue or excessive wear fatigue, and insecurity Instrument. For cylinder compression, for fraudulent purpose, of any record or report under this part the use of component. Inspect ( where practicable ) improper operation discharge nozzles in a fuel injected reciprocating identified! Date ( ) 14 cfr part 43 appendix d checklist ; Eight 1/4 -- 20 inch standard heli-coils were replaced ) Exhaust stacks - for internal. Shall thoroughly clean the aircraft through still air + motion of the contains... 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