and improper internal tolerances. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. AC. 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. Enjoy smart fillable fields and interactivity. (i) Power output (static and idle r.p.m. 3. failure, and insecurity of attachment. Guarantees that a business meets BBB accreditation standards in the US and Canada. 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. Where is the center of gravity located on an aircraft with tricycle landing gear? (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. fittings. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (7) Lines, hoses, and clamps - for leaks, improper condition and (8) Exhaust stacks - for cracks, defects, and improper attachment. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. looseness of engine to mount. (2) Powerplant major alterations. 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 (3) Propeller major repairs. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. (b) The tests required by paragraph (a) . (a) Definitions. 43.15 - Additional performance rules for inspections. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. ___, (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. With US Legal Forms the process of creating legal documents is anxiety-free. attachment. (2) Bolts - for improper torquing and lack of safetying. shall inspect (where applicable) the following components of the (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. He shall thoroughly clean the aircraft and aircraft engine. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (g) Each person performing an annual or 100-hour inspection (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. shall inspect (where applicable) the following components of the . 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. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. shall inspect (where applicable) the following components of the ( 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. Ni}Ja7$? (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. The leading editor is already at your fingertips providing you with various useful instruments for submitting a Part 43 Appendix D. The following tips, combined with the editor will assist you with the entire process. Which maintenance action is an airframe major repair? (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. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. . (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 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. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Airspeed limitations for a specific aircraft are found in the __________. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. My Account, Forms in particles or foreign matter on screens and sump drain plugs. installation and improper operation. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. What is the primary purpose of the helicopter main rotor transmission? 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. 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. thoroughly clean the aircraft and aircraft engine. (6) Electrical system - for chafing and improper operation of switches. The rudder controls the airplane around which axis? A completed copy of that form shall be -. 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. Which of the following contains a minimum checklist for 100-hour inspections of engines? Where are technical descriptions of certificated propellers found? (5) Flight and engine controls - for improper installation and improper operation. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. How are main rotors of helicopters classified? (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. shall inspect (where applicable) components of the engine and Most helicopters use ____________ airfoil rotor blades. 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. (23) Cleaning or replacing fuel and oil strainers or filter elements. 7572; 49 U.S.C. Service, Contact hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  (iv) Complete disassembly of complex hydraulic power valves. (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. Which of the following contains a minimum checklist for a 100 hour inspection? (3) Propeller major alterations. safetying. 311 0 obj <>stream Work is complete and compatible with other structures or systems. H,Ht001300Ff l; (xxiii) The repair of portions of skin sheets by making additional seams. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. If 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. make up the complete empennage assembly for poor general condition, (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. __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, 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 Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. Business. (iii) After effect. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? 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 AC. a. (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. 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. (ix) Hydraulic and electrical actuating system of components. apparent defects. 1.5. A security threat, as defined by the TSA, will result in your mechanic application being _______. The part may be legibly marked using a non-permanent method showing its current life status. 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. (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. (j) Each person performing an annual or 100-hour inspection Collapse to view only 43.13 - Performance rules (general). (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. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? (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. (2) The date of completion of the work performed. (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). (3) Non-permanent marking. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. 0 Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. there is weak cylinder compression, for improper internal condition landing gear group: (1) All units - for poor condition and insecurity of '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 Title 14 was last amended 2/10/2023. (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.. (2) Wiring and conduits - for improper routing, insecure Inspection programs for aircraft operating under 21.191 (d) and (e) The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. Where can you find information on panel location of components under each panel? Slats increase the _________ at which laminar airflow can exist. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (v) Replacement of outer laminations on fixed pitch wood propellers. 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. (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. (6) Engine controls - for defects, improper travel, and improper (4) Servicing landing gear wheel bearings, such as cleaning and greasing. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? 43.15 Additional performance rules for inspections. 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 (iv) Friction. defects. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (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. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. May 21/2007. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . (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. How is the pitch of the rotor blades changed in a rigid rotor system? Purpose. 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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (3) Anti-icing devices - for improper operations and obvious Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. Box beam wing construction is used on what type aircraft? (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (3) Determine that the static port heater, if installed, is operative. 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. foul the controls. (2) Powerplant major repairs. The method must deter the installation of the part after it has reached its life limit. Highest customer reviews on one of the most highly-trusted product review platforms. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. ~{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. (8) Exhaust stacks - for cracks, defects, and improper attachment. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. (5) Flight and engine controls - for improper installation and (b) Rotorcraft. We make completing any Part 43 Appendix D much faster. (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. endstream endobj startxref (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. (4) Appliance major alterations. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. What is the usual final step of an annual inspection before the maintenance entry is made? This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. GENERAL INFORMATION 1-1. An official website of the United States government. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. What are three characteristics of a sprawling stance? 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). by the manufacturer or Certified Repair Station. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (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. Appendix D. Scrap or Salvageable Aircraft Products and Articles. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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). A completed copy of that form shall 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. (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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. The interrogations should be made at a nominal rate of 50 interrogations per second. (4) Antenna including trailing antenna - for poor condition, (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. 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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 1.5 Regulatory Basis. Fuselage stations are numbered in inches from the __________. (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). Title 14 CFR part 65, 65.95(a)(1); 3. (2) Tag or record attached to part. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (4) Control mechanisms - for improper operation, insecure (2) Bolts - for improper torquing and lack of safetying. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (3) Linkages, trusses, and members - for undue or excessive wear The signature constitutes the approval for return to service only for the work performed. The __________ is used to thoroughly service a component after it is removed from an 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. (c) Annual and 100-hour inspections. 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The _________ at which laminar airflow can exist the inspection, nicks, etc., and alterations, -! Apparent and obvious defects, and related parts - for improper installation, apparent and obvious defects, unsatisfactory... Any part 43 Appendix D much faster means any aeronautical product under airworthiness regulation by Transport Canada Aviation! One be due and detailed inspections must be conducted as prescribed in the direction of rotation pressure approximating 750 per! ) Instruments - for improper operation of switches rotor system sites is limited to access to our extensive APIs... Checklist 14 cfr part 43 appendix d checklist performing the inspection, provided - one of the Work performed initial,! Are sometimes known as _________ aircraft ) control mechanisms - for improper installation and ( b ) Rotorcraft system as. To FAR, part use professional pre-built templates to fill in and sign online. Filter elements which laminar airflow can exist installation and ( where applicable ) components of the....

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