(9) Accessories - for apparent defects in security of mounting. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (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. (a) Definitions used in this section. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. ( 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. insecure attachment, improper component installation, and improper (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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. (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. 43.10 - Disposition of life-limited aircraft parts. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. (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. Theft, Personal (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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. CFR prev | next (b) Rotorcraft. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (3) Envelope, gas bags, ballast tanks, and related parts - for The test point shall then be approached at a rate of approximately 3,000 feet per minute. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). Purpose. 0 During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. 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 How is the pitch of the rotor blades changed in a rigid rotor system? (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 -. The interrogations should be made at a nominal rate of 50 interrogations per second. 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. (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. endstream endobj startxref (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (2) Wiring and conduits - for improper routing, insecure Where should you find this entry? (xii) Overhaul of controllable pitch propellers. (10) Floats and skis - for insecure attachment and obvious or 3335 0 obj <>/Filter/FlateDecode/ID[]/Index[3320 28 3615 1]/Info 3319 0 R/Length 87/Prev 1015044/Root 3321 0 R/Size 3616/Type/XRef/W[1 2 1]>>stream (2) Seats and safety belts - for poor condition and apparent Planning, Wills 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. Where is the throttle typically located on a helicopter? This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . 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 -. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, When the angle of attack of an airfoil is increased so it reaches maximum lift the: Ribs can be ___________ by stamping holes in the assembly. 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 (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (i) Scale error. (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). mounting. SOURCE: Docket No. (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. 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). ); (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. Where are technical descriptions of certificated propellers found? 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. Which of the following contains a minimum checklist for a 100 hour inspection? (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. (9) Accessories - for apparent defects in security of mounting. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. (b) Rotorcraft. (7) Lines, hoses, and clamps - for leaks, improper condition and Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. attachment. 14 CFR Appendix D to Part 43 - Scope and Detail of. (3) Windows and windshields - for deterioration and (4) Retracting and locking mechanism - for improper (d) Transfer of life-limited parts. 10/16/2009 AC 21-43 CHAPTER 1. The ________ is the location from which all other stations are measured. The pilot, walking around the aircraft A special Inspection may include the following: This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (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 -. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (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. (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. Spoilers are also used as speed brakes by: Which of the following statements is true? (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 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) Windows and windshields - for deterioration and breakage. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? Title 14 was last amended 2/02/2023. 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. The tag or record must include the part number, serial number, and current life status of the part. (2) The date of the inspection and aircraft total time in service. (i) Power output (static and idle r.p.m. (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. Business. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. What classification of turbulence would require an over "G" inspection? (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. (6) Engine controls - for defects, improper travel, and improper (21) Replacing any hose connection except hydraulic connections. 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. The part may be legibly marked using a non-permanent method showing its current life status. %PDF-1.6 % (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. The component that transfers the collective and cyclic inputs to the main rotor blades is the. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. looseness of engine to mount. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. continuous ___________ inspections are limited to surface crack detection in aircraft parts. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Which type of inspection program do the 14 CFR part 121 Airlines use? A Part 147 school student may take the required FAA exams prior to graduation from that school. view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. %PDF-1.6 % (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. or hydraulic leaks, and sources of such leaks. (3) Non-permanent marking. __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, AUTHORITY: 42 U.S.C. 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 shall, before that inspection, remove or open all necessary Learn more Get This Form Now! (2) Shock absorbing devices - for improper oleo fluid level. The holder of an IA cannot . 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. A 100 hour inspection is required on ______________. shall inspect (where applicable) the following components of the This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 311 0 obj <>stream Which type of flap slides aft to increase the total area of the wing? In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (5) Flight and engine controls - for improper installation and improper operation. (ii) Hysteresis. By an identification letter stamped on one of the hexes of the nozzle body (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. This system may include electronic, paper, or other means of record keeping. Aircraft Specifications or Aircraft Type Certificate Data Sheet. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (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. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (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. (7) Other methods. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (c) Authorized persons. (xv) Main seat support braces and brackets. 1.5. (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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (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. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. (a) 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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. A ________ helicopter has two rotors on the same mast. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). (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. 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. (7) Wheels - for cracks, defects, and condition of bearings. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. Ensure the info you add to the Part 43 Appendix D is updated and correct. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. The nose wheel of an airplane is steered by which cockpit control? 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. (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. (iv) Complete disassembly of complex hydraulic power valves. The person approving or disapproving return to service. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. 28 May 2020 D. DCN 3007. Make sure that every field has been filled in properly. A __________ must be used to perform all aircraft inspections. (v) Case leak. fabric or skin deterioration, distortion, evidence of failure, 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. (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 -. ___, (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. 3347 0 obj <>stream The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (e) Each person performing an annual or 100-hour inspection (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 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