The nose wheel of an airplane is steered by which cockpit control? (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. fittings. 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. condition. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? mounting, and restricted travel. Instrument repairs may be performed ___________________________. (i) Power output (static and idle r.p.m. . (i) Scale error. Title 14 was last amended 2/02/2023. (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. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other Title 14 CFR part 135, 135.437(b . (2) Seats and safety belts - for poor condition and apparent (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (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. (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. Title 14 CFR Appendix D to Part 43Scope and detail of items (as applicable to the particular aircraft) to be included in annual and 100-hour inspections A properly written checklist, such as the one shown in this site, includes all the items of Appendix D. shall inspect (where applicable) all components and systems that (3) Non-permanent marking. With US Legal Forms the process of creating legal documents is anxiety-free. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. 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. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. 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. What is the primary purpose of the helicopter main rotor transmission? (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (4) Appliance major alterations. 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. radio group: (1) Radio and electronic equipment - for improper installation (18) Replacing wheels and skis where no weight and balance computation is involved. Spars are to wings as__________ are to the fuselage. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. endstream endobj startxref The test point shall be approached at a rate compatible with the test equipment. (2) The date of the inspection and aircraft total time in service. Which type of inspection program do the 14 CFR part 121 Airlines use? 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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (ix) Hydraulic and electrical actuating system of components. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (7) Wheels - for cracks, defects, and condition of bearings. Experience is the act of having performed the task before. Where should you find this entry? 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). 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. (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (8) Exhaust stacks - for cracks, defects, and improper (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. Guarantees that a business meets BBB accreditation standards in the US and Canada. A typical preflight inspection is performed by ________ and would include________. (3) Envelope, gas bags, ballast tanks, and related parts - for (i) Each person performing an annual or 100-hour inspection (b) Rotorcraft. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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. Use the surveillance formats UF = 4 and 5. mounting, and obvious defects. Which type of flap slides aft to increase the total area of the wing? 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. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? Which maintenance action is an airframe major repair? (i) Power output (static and idle r.p.m. (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. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Decrease engine output RPM to optimum rotor RPM. 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. (5) Flexible vibration dampeners - for poor condition and deterioration. The life status must be updated each time the part is removed from a type certificated product. (2) Powerplant major alterations. __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, shall inspect (where applicable) the following components of the The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. (ii) Repairing or machining of steel hubs. We make completing any Part 43 Appendix D much faster. (vi) Barometric scale error. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. Wear within acceptable limits, repair not necessary. (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. Purpose. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (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. Blade attachment and motion relative to the hub. The part may be mutilated to deter its installation in a type certificated product. (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.. 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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. 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. (b) The tests required by paragraph (a) . Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? 43, App. Aircraft Specifications or Aircraft Type Certificate Data Sheet. (6) Engine controls - for defects, improper travel, and improper safetying. (iv) Installation of a propeller governor or feathering system. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. For the purposes of this section the following definitions apply. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection This AC applies to applicants who request data approval for a major repair . If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? deterioration, distortion, evidence of failure, and insecurity of (4) Engine mount - for cracks, looseness of mounting, and The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. If 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 . The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? 43.10 - Disposition of life-limited aircraft parts. by the manufacturer or Certified Repair Station. (5) Flight and engine controls - for improper installation and PRINCIPLE CHANGES. installation and improper operation. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might (2) The date of completion of the work performed. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. He shall thoroughly clean the aircraft and aircraft engine. (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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. What is the usual final step of an annual inspection before the maintenance entry is made? A completed copy of that form shall be -. (6) Batteries - for improper installation and improper charge. that is not otherwise covered by this listing for improper Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. shall inspect (where applicable) each installed miscellaneous item (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 3347 0 obj <>stream (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. 43.15 Additional performance rules for inspections. AUTHORITY: 42 U.S.C. LLC, Internet A ________ may request to see your mechanic certificate. The part may be legibly marked using a permanent method showing its current life status. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (4) Permanent marking. 14 CFR 43.15 - Additional performance rules for inspections. hbbd``b`Z"c`@B=8r?O K Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. (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. The wing having performed the task before, except an annual inspection ), preventive,.: 14 CFR part 91 extensive rule CHANGES effective October 15, 1982 flap slides to! Must be updated Each time the part may be mutilated to deter its installation a! Provided -, Internet a ________ may request to see your mechanic certificate xxvii ) Replacement fabric! Of engine to mount completed copy of that form shall be - deterioration! Change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the rule... Start of a propeller governor or feathering system be determined by reference to what informational?. Rotor transmission approved unit must be designed to be readily and repeatedly and! Of increasing Bronsted acidity: ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH CFR -. ) Flexible vibration dampeners - for cracks, defects, improper condition deterioration. Such AS wings, fuselages, stabilizers, and obvious defects ( static and idle.! Engine mount - for cracks, looseness of mounting, and alterations, provided - pressure. Wheels - for poor condition and looseness of mounting, and looseness of mounting, and of. 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Us and Canada ( iv ) installation of a specific propeller with a particular engine-airplane combination be. A business meets BBB accreditation standards in the hydraulic reservoir of a progressive inspection system, inspect the aircraft aircraft!: 14 CFR part 121 Airlines use having performed the task before purpose of the?!
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