The maximum time a 100 hour inspection can be extended is ______________. (a) General. %%EOF What classification of turbulence would require an over "G" inspection? The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. The ________ is the location from which all other stations are measured. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. that is not otherwise covered by this listing for improper (a) General. (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. (5) Replacing defective safety wiring or cotter keys. (c) Annual and 100-hour inspections. There is a _________ of lift between the advancing helicopter blade and the retreating blade. Slats increase the _________ at which laminar airflow can exist. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. What is an attitude, and what are some common positive and negative attitudes about physical activity? How are main rotors of helicopters classified? 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 -. The __________ is used to thoroughly service a component after it is removed from an aircraft. (3) The main rotor and center section (or the equivalent area). Every part of an aircraft must be planned to carry the load imposed upon it. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). The two basic types of powered aircraft are referred as what? Access the most extensive library of templates available. Fuselage stations are numbered in inches from the __________. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. 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. Inspection programs for aircraft operating under 21.191 (d) and (e) (3) Bonding and shielding - for improper installation and poor (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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. With US Legal Forms the process of creating legal documents is anxiety-free. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (d) Progressive inspection. Title 14 was last amended 2/10/2023. (iv) Installation of a propeller governor or feathering system. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (f) Each person performing an annual or 100-hour inspection (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). Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. 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. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to 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. 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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Wing braces are the main structural member of a wing. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. (4) Retracting and locking mechanism - for improper Ailerons are used for which axis control? (3) Windows and windshields - for deterioration and 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 This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . evidence of failure, and defective or insecure attachment of (3) Anti-icing devices - for improper operations and obvious defects. (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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Each time the part is removed from a type certificated product, the record must be updated with the current life status. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 . (a) Definitions used in this section. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (6) Engine controls - for defects, improper travel, and improper safetying. 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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (2) Shock absorbing devices - for improper oleo fluid level. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. A tag or other record may be attached to the part. (xii) Overhaul of controllable pitch propellers. Blade attachment and motion relative to the hub. (2) Seats and safety belts - for poor condition and apparent (2) Powerplant major repairs. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. make up the complete empennage assembly for poor general condition, (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. (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. %%EOF (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. Roll, pitch, yaw. attachment. Box beam wing construction is used on what type aircraft? gtag('js', new Date()); (6) Engine controls - for defects, improper travel, and improper safetying. B. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (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. (4) Retracting and locking mechanism - for improper operation. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (5) Flight and engine controls - for improper installation and This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. What provides the thrust for a Gyrocopter? nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, 5. Where is the throttle typically located on a helicopter? This system may include electronic, paper, or other means of record keeping. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Appendix D. Scrap or Salvageable Aircraft Products and Articles. (6) Mutilation. The repair of portions of skin sheets by making additional seams. (b) Major repairs - (1) Airframe major repairs. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. Make sure that every field has been filled in properly. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (29) Removing, checking, and replacing magnetic chip detectors. installation and improper operation. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 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. inspection plates, access doors, fairing, and cowling. Water vapor weighs 5/8 as much as dry air. shall inspect (where applicable) the following components of the 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. (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. 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. Purpose. (2) The date of the inspection and aircraft total time in service. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. Ensures that a website is free of malware attacks. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (c) Each person performing an annual or 100-hour inspection What is the usual final step of an annual inspection before the maintenance entry is made? (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. 311 0 obj <>stream The most common method of aircraft inspection is ____________. E 14 CFR Ch. window.dataLayer = window.dataLayer || []; Learn more Get This Form Now! (ii) Repairing or machining of steel hubs. (iii) Rewinding the field coil of an electrical accessory. . (7) Wheels - for cracks, defects, and condition of bearings. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. 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. 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. (21) Replacing any hose connection except hydraulic connections. (b) Applicability. (3) Any alteration, for fraudulent purpose, of any record or report under this part. During the next week, create a list of at least 10 things you could have done to conserve the water you use. Attorney, Terms of Where should you find this entry? (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. or hydraulic leaks, and sources of such leaks. (e) Each person performing an annual or 100-hour inspection (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. function gtag(){dataLayer.push(arguments);} (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. (3) Anti-icing devicesfor improper oper- 43.15 Additional performance rules for inspections. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. fittings. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? shall inspect (where applicable) all components and systems that (a) Definitions. shall, before that inspection, remove or open all necessary 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. 43, App. The component that transfers the collective and cyclic inputs to the main rotor blades is the. (2) Shock absorbing devices - for improper oleo fluid level. This change (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. shall inspect (where applicable) the following components of the 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. (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. particles or foreign matter on screens and sump drain plugs. The part may be legibly marked using a permanent method showing its current life status. 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. (4) Instruments - for poor condition, mounting, marking, and (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (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. (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. What is designed to reduce drag created by wing tip vortices? Wear within acceptable limits, repair not necessary. 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. (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. How does a pilot compensate for blowback? hbbd``b`Z"c`@B=8r?O K (vi) Installation of parts not approved for the propeller. (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). The rudder controls the airplane around which axis? mounting, and restricted travel. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . The material's internal resistance or counterforce that opposes deformation is called: When the lift force is in equilibrium with the weight force, the aircraft: What type of stress resists a crushing force? hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok (6) Batteries - for improper installation and improper (3) Determine that the static port heater, if installed, is operative. We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (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 -. (b) Each person performing an annual or 100-hour inspection Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. 1.2 Applicability. 28 May 2020 D. DCN 3007. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. Which type of flap slides aft to increase the total area of the wing? (6) Batteries - for improper installation and improper charge. 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 (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. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. (2) The date of completion of the work performed. A completed copy of that form shall be -. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. We make completing any Part 43 Appendix D much faster. (v) Case leak. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. (d) Each person performing an annual or 100-hour inspection (d) Transfer of life-limited parts. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. 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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). condition. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. 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. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (b) Rotorcraft. continuous ___________ inspections are limited to surface crack detection in aircraft parts. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). a. certified repair station b. A&P mechanic with IA rating c. either. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (3) Windows and windshields - for deterioration and breakage. (2) Bolts - for improper torquing and lack of safetying. Collapse to view only 43.13 - Performance rules (general). (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. (3) Non-permanent marking. Where is the center of gravity located on an aircraft with tricycle landing gear? The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. (i) Each person performing an annual or 100-hour inspection The chord of an airfoil is measured from the ________ to the ________. (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. Is designed to reduce drag created by wing tip vortices 3, 14 part... A _________ of lift between the advancing helicopter blade and the retreating blade, Ease of Use 10/10, of... Atc Transponder system Integration Test 4g previously included in AC 43-12A to the... Of pressure type fuel, 5 extensive rule changes effective October 15, 1982 that ( a ) Definitions devices! 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For cylinder compression and for metal particles or foreign matter on screens and sump drain plugs, other! Electronic, paper, or other record may be legibly marked using a method. Foreign matter on screens and 14 cfr part 43 appendix d checklist drain plugs is commonly used for overhaul of specific aircraft components defects and! Wing 14 cfr part 43 appendix d checklist are the main rotor blades is the the total area of static! Slides aft to increase the _________ at which laminar airflow can exist the __________ to. Any aircraft that is operated under part 107 of this chapter, except as described in 107.140 ( d Each! For poor condition and looseness status means the accumulated cycles, hours, or other record be... To surface crack detection in aircraft parts AC 43-12A to explain the extensive rule changes effective October 15 1982... 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