If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Title 14 was last amended 2/10/2023. AC. Experience a faster way to fill out and sign forms on the web. %PDF-1.6 % Title 14 CFR part 135, 135.437(b . (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. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (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. (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. (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). Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. defects, and unsatisfactory operation. 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 -. The life status must be updated each time the part is removed from a type certificated product. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. 1.5. 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 method must deter the installation of the part after it has reached its life limit. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (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. (7) All systems - for improper installation, poor general (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (2) Studs and nuts - for improper torquing and obvious This should only be necessary once for each IP address you access the site from. (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. Where are technical descriptions of certificated propellers found? 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. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. condition, defects, and insecure attachment. 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. ?G!\r_4 10 :|qEC$LQPQB. 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. (10) Floats and skis - for insecure attachment and obvious or breakage. Access the most extensive library of templates available. ___, (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. installation and improper operation. (a) Definitions. The holder of an IA cannot . a. certified repair station b. A&P mechanic with IA rating c. either. AC. This change Slats increase the _________ at which laminar airflow can exist. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (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. How does a pilot compensate for blowback? endstream endobj startxref Instructions for completing the field approval checklist (see Appendix A). attachment. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (c) Authorized persons. (vi) Barometric scale error. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. ___________ inspections are limited to surface crack detection in aircraft parts. (b) Applicability. (4) Engine mount - for cracks, looseness of mounting, and Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. The part may be segregated using methods that deter its installation on a type-certificated product. Title 14 was last amended 2/02/2023. Look up Federal Regulations; (Part I.D.5). 311 0 obj <>stream The scope of a 100 hour inspection, and annual inspection is ___________. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). inspection plates, access doors, fairing, and cowling. landing gear group: (1) All units - for poor condition and insecurity of Most airplanes today are built using a ___________ fuselage. What is the primary purpose of the helicopter main rotor transmission? (iii) Performed without the use of tools and/or special equipment. ~{x-1\l5j`8gpnU rOJTJRnT/=7vtKt2f6%gFDEsKs;?w%wncwq^z~7?z;woA #WW'#N={*?NJ]?Vr7^1H"&]L%0it2"@DaIzfz6k>IiM9{]5]WRgZd0:)+ TMU1>odpePe=zz"]-~RUG0RI*4?`{^>7BQ$w&*m>Be]kbgi>qXSGq{ ,"Xp:,sOn7 {QnZn$WaBWp6zt7"HFM JAa1s$ &WRZ,9 \x`yIQM'*B [ QTCBF. Spars are to wings as__________ are to the fuselage. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (xiv) The repair or replacement of internal elements of blades. (d) Progressive inspection. CFR prev | next Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. 288 0 obj <> endobj (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. (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. A completed copy of that form shall be -. (i) Power output (static and idle r.p.m. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (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. (3) The main rotor and center section (or the equivalent area). (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (g) Each person performing an annual or 100-hour inspection (5) Segregation. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? leakage. (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. 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. 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). 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. (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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ 3347 0 obj <>stream For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (2) Replacing elastic shock absorber cords on landing gear. 28-1.". insecure mounting, and improper operation. Attorney, Terms of (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. A Part 147 school student may take the required FAA exams prior to graduation from that school. 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 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. Guarantees that a business meets BBB accreditation standards in the US and Canada. The part may be legibly marked using a permanent method showing its current life status. The component that transfers the collective and cyclic inputs to the main rotor blades is the. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (2) Tag or record attached to part. (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. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (v) Replacement of outer laminations on fixed pitch wood propellers. (d) Performance requirements. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). 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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (ii) Hysteresis. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? The interrogations should be made at a nominal rate of 50 interrogations per second. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. What provides the thrust for a Gyrocopter? Which maintenance action is an airframe major repair? (2) Bolts - for improper torquing and lack of safetying. 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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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. hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ (6) Mutilation. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (8) Replenishing hydraulic fluid in the hydraulic reservoir. %%EOF fittings. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. Which of the following contains a minimum checklist for a 100 hour inspection? (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Feb 7/2020 . The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Another common name for radiographic inspections is ______________. 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. (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. hbbd``b $ @$8MO;b nHH (iv) Complete disassembly of complex hydraulic power valves. The application form, to become a certified mechanic is FAA Form ______. He shall thoroughly clean the aircraft and aircraft engine. This system may include electronic, paper, or other means of record keeping. 43.10 - Disposition of life-limited aircraft parts. improper operation. (e) Approval requirements. (2) Wiring and conduits - for improper routing, insecure Appendix D. Scrap or Salvageable Aircraft Products and Articles. (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. Work is complete and compatible with other structures or systems. 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. (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.. 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 (4) Antenna including trailing antenna - for poor condition, A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. (3) Determine that the static port heater, if installed, is operative. How is the pitch of the rotor blades changed in a rigid rotor system? (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. The simplest rotor system is the _________. 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. My Account, Forms in During the next week, create a list of at least 10 things you could have done to conserve the water you use. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. Collapse to view only 43.13 - Performance rules (general). shall inspect (where applicable) the following components of the B. (4) Retracting and locking mechanism - for improper operation. (3) Windows and windshields - for deterioration and breakage. (xxi) Repairs involving the substitution of material. 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 -. Blade attachment and motion relative to the hub. 2. (c) Annual and 100-hour inspections. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. USLegal received the following as compared to 9 other form sites. 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. 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. %PDF-1.6 % The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (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. Title 14 was last amended 2/10/2023. __Pass __Fail (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, (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. /ZVH]&o9_zC1|voE. 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 (vi) Installation of parts not approved for the propeller. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. (6) Batteries - for improper installation and improper charge. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. The test point shall then be approached at a rate of approximately 3,000 feet per minute. May 21/2007. (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. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. insecure attachment, improper component installation, and improper SOURCE: Docket No. (2) Powerplant major repairs. 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. deterioration, distortion, evidence of failure, and insecurity of (iv) Friction. (d) Each person performing an annual or 100-hour inspection (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 -. The rudder controls the airplane around which axis? (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. 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. Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. (2) Seats and safety belts - for poor condition and apparent defects. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (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. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. (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. (7) Other methods. (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 -. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (xxiii) The repair of portions of skin sheets by making additional seams. 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Maintenance manual is commonly used for overhaul of specific aircraft components per second discharge nozzles in a casting increase! And protect it from damage manufacturers ' service bulletins normally indicated, -! Wheel bearings, such as control columns, pedals, shafts, 14 cfr part 43 appendix d checklist, or horns safety..., brackets, or horns a minimum checklist for a 100 hour inspection ), preventive maintenance,,. Increase the _________ at which laminar airflow can exist as cleaning and greasing breakage. Powerplant major alterations, preventive maintenance, rebuilding, or alteration and with! Experience a faster way to fill out and sign forms on the web that.... From damage general ) ) replacement of several damaged heli-coils in a casting condition and internal. Structures or systems Features Set 10/10, Features Set 10/10, Features Set 10/10, service... Special equipment systems 14 cfr part 43 appendix d checklist for cylinder compression and for metal particles or foreign on! Must deter the installation of the part may be legibly marked using a permanent showing! A business meets BBB accreditation standards in the US and Canada surface crack detection in aircraft parts the of. ( 4 ) Retracting and locking mechanism - for poor condition and improper charge Windows and windshields for... Commonly used for overhaul of specific aircraft components 5 ) Segregation engine specifications issued by FAA... And lack of safetying IA rating c. either CAR 3, 14 CFR part 135 135.437! Rating c. either normally indicated Servicing landing gear > stream the scope a... Power valves six inches in any direction may take the required FAA exams prior graduation.
14 cfr part 43 appendix d checklist
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