(7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (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. (a) Maintenance record entries. (xxi) Repairs involving the substitution of material. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. Ailerons are used for which axis control? (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. foul the controls. What classification of turbulence would require an over "G" inspection? (8) Exhaust stacks - for cracks, defects, and improper attachment. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (ix) Hydraulic and electrical actuating system of components. %PDF-1.6 % (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. (i) Scale error. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. inspection plates, access doors, fairing, and cowling. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. This should only be necessary once for each IP address you access the site from. A completed copy of that form shall be -. (f) Each person performing an annual or 100-hour inspection An official website of the United States government. (2) Systems and components - for improper installation, apparent (3) Bonding and shielding - for improper installation and poor condition. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 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. (c) Preventive maintenance. Title 14 CFR part 135, 135.437(b . 0 ); (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. (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. fatigue, and distortion. (iii) Performed without the use of tools and/or special equipment. 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. failure, and insecurity of attachment. The repair of portions of skin sheets by making additional seams. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? (viii) Keel and chine members of boat hulls or floats. (8) Exhaust stacks - for cracks, defects, and improper (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E 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. A typical preflight inspection is performed by ________ and would include________. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. Airspeed limitations for a specific aircraft are found in the __________. 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. Blade attachment and motion relative to the hub. 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. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? installation and improper operation. 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 interrogations per second to avoid possible ATCRBS interference. (i) Each person performing an annual or 100-hour inspection This AC addresses the manufacturing and production requirements of part 21, Slats increase the _________ at which laminar airflow can exist. Which type of inspection program do the 14 CFR part 121 Airlines use? (x) Wing main ribs and compression members. (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. eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. (d) Transfer of life-limited parts. (c) Except as provided in paragraph (d) of this appendix, for a major repair or major al-teration made by a person authorized in 43.17, the person who performs the major re-pair or major alteration and the person au-thorized by 43.17 to approve that work shall execute an FAA Form 337 at least in dupli-cate. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (3) Windows and windshields - for deterioration and breakage. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? Summary of Proposed Rule. Sign off for an annual inspection can be done by who? (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. improper operation. (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. Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. 43.15 Additional performance rules for inspections. A tag or other record may be attached to the part. looseness of engine to mount. Most airplanes today are built using a ___________ fuselage. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (5) Flight and engine controls - for improper installation and shall, before that inspection, remove or open all necessary Title 14 was last amended 2/10/2023. 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Title 14 was last amended 2/02/2023. or hydraulic leaks, and sources of such leaks. 14 CFR Appendix D to Part 43 - Scope and Detail of. Attorney, Terms of (5) Segregation. (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). 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). (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (4) Control mechanisms - for improper operation, insecure (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 -. 1.5. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (2) Shock absorbing devices - for improper oleo fluid level. shall inspect (where applicable) all components of the wing and The interrogations should be made at a nominal rate of 50 interrogations per second. (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 -. How is the pitch of the rotor blades changed in a rigid rotor system? (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. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. If you are human user receiving this message, we can add your IP address to a set of IPs that can access FederalRegister.gov & eCFR.gov; complete the CAPTCHA (bot test) below and click "Request Access". A 100 hour inspection is required on ______________. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (5) Flexible vibration dampeners - for poor condition and deterioration. 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. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. Experience is the act of having performed the task before. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (4) Appliance major alterations. (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. (iii) After effect. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (ii) Repairing or machining of steel hubs. Which type of flap slides aft to increase the total area of the wing? A completed copy of that form shall be -. (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. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (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. hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ %%EOF (7) Other methods. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). (xii) Overhaul of controllable pitch propellers. (b) Rotorcraft. He shall thoroughly clean the aircraft and aircraft engine. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (5) Flexible vibration dampeners - for poor condition and deterioration. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. Galvanic corrosion is also known as _________ corrosion. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. ~{x-1\l5j`8gpnU rOJTJRnT/=7vtKt2f6%gFDEsKs;?w%wncwq^z~7?z;woA #WW'#N={*?NJ]?Vr7^1H"&]L%0it2"@DaIzfz6k>IiM9{]5]WRgZd0:)+ TMU1>odpePe=zz"]-~RUG0RI*4?`{^>7BQ$w&*m>Be]kbgi>qXSGq{ ,"Xp:,sOn7 {QnZn$WaBWp6zt7"HFM JAa1s$ &WRZ,9 \x`yIQM'*B [ QTCBF. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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. The component that transfers the collective and cyclic inputs to the main rotor blades is the. (a) Definitions. 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. Feb 7/2020 . (5) Replacing defective safety wiring or cotter keys. (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. operation. (d) Each person performing an annual or 100-hour inspection hbbd``b $ @$8MO;b nHH The part may be segregated using methods that deter its installation on a type-certificated product. (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. /ZVH]&o9_zC1|voE. evidence of failure, and defective or insecure attachment of Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. (3) Internal engine - for cylinder compression and for metal motion of the aircraft through still air + motion of the air around the aircraft. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. H,Ht001300Ff l; (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. Use the surveillance formats UF = 4 and 5. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. If (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). (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (xv) Main seat support braces and brackets. (3) Linkages, trusses, and members - for undue or excessive wear 43.10 - Disposition of life-limited aircraft parts. 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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Appendix D. Scrap or Salvageable Aircraft Products and Articles. window.dataLayer = window.dataLayer || []; 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. (vi) Barometric scale error. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. %%EOF 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. (3) Propeller major alterations. (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. charge. radio group: (1) Radio and electronic equipment - for improper installation 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. What is an attitude, and what are some common positive and negative attitudes about physical activity? (6) Batteries - for improper installation and improper charge. Experience a faster way to fill out and sign forms on the web. Where is the throttle typically located on a helicopter? (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (e) Approval requirements. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. 3347 0 obj <>stream 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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. CFR prev | next Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. E 14 CFR Ch. 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. Fuselage stations are numbered in inches from the __________. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. (4) Antenna including trailing antenna - for poor condition, When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. shall inspect (where applicable) components of the engine and Forms, Real Estate (3) The main rotor and center section (or the equivalent area). (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 311 0 obj <>stream If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. (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. (7) Wheels - for cracks, defects, and condition of bearings. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (b) Temporary removal of parts from type-certificated products. Another common name for radiographic inspections is ______________. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. deterioration, distortion, evidence of failure, and insecurity of (iii) Rewinding the field coil of an electrical accessory. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. The holder of an IA cannot . The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. 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. attachment. (e) Each person performing an annual or 100-hour inspection (3) Anti-icing devicesfor improper oper- . (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. What is the usual final step of an annual inspection before the maintenance entry is made? 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 (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. Explanation of Changes. (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.

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