(16) Trouble shooting and repairing broken circuits in landing light wiring circuits. deterioration, distortion, evidence of failure, and insecurity of (18) Replacing wheels and skis where no weight and balance computation is involved. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (2) Tag or record attached to part. (3) Windows and windshields - for deterioration and (5) Flight and engine controls - for improper installation and What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? (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. (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. (3) Servicing landing gear shock struts by adding oil, air, or both. Use the surveillance formats UF = 4 and 5. looseness of engine to mount. An official website of the United States government. (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. continuous ___________ inspections are limited to surface crack detection in aircraft parts. (3) Propeller major alterations. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (2) The date of completion of the work performed. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. Ensures that a website is free of malware attacks. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (4) Appliance major alterations. (e) Each person performing an annual or 100-hour inspection 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. 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. (4) Retracting and locking mechanism - for improper operation. Which maintenance action is an airframe major repair? mounting. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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). condition. (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. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. The maximum time a 100 hour inspection can be extended is ______________. 43.15 Additional performance rules for inspections. a. The two basic types of powered aircraft are referred as what? Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. 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? 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. (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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. ECO 17212. (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. (b) Rotorcraft. (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. 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. What provides the thrust for a Gyrocopter? 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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. If (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 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). (6) Batteries - for improper installation and improper (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (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. (7) All systems - for improper installation, poor general a. certified repair station b. A&P mechanic with IA rating c. either. attachment. (ii) Hysteresis. 3320 0 obj <> endobj Spoilers are also used as speed brakes by: Which of the following statements is true? (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). make up the complete empennage assembly for poor general condition, function gtag(){dataLayer.push(arguments);} Another common name for radiographic inspections is ______________. USLegal fulfills industry-leading security and compliance standards. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. This AC addresses the manufacturing and production requirements of part 21, (where practicable) improper operation. 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. 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. Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. #1 Internet-trusted security seal. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. (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. 5. Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? (vi) Barometric scale error. (d) Performance requirements. (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. 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. (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. (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. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. or hydraulic leaks, and sources of such leaks. 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. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. installation and improper operation. 288 0 obj <> endobj 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. The part may be mutilated to deter its installation in a type certificated product. Feb 7/2020 . breakage. The life status must be updated each time the part is removed from a type certificated product. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. ?G!\r_4 10 :|qEC$LQPQB. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . 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. A ________ helicopter has two rotors on the same mast. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. Collapse to view only 43.13 - Performance rules (general). pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . /ZVH]&o9_zC1|voE. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . 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. (29) Removing, checking, and replacing magnetic chip detectors. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. What is the usual final step of an annual inspection before the maintenance entry is made? 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. 28-1.". (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? The application form, to become a certified mechanic is FAA Form ______. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of 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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (8) Exhaust stacks - for cracks, defects, and improper (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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Where should you find this entry? Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. By an identification letter stamped on one of the hexes of the nozzle body Purpose. (6) Mutilation. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (2) Shock absorbing devices - for improper oleo fluid level. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. evidence of failure, and defective or insecure attachment of (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. 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 -. PRINCIPLE CHANGES. Sign off for an annual inspection can be done by who? (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 -. May 21/2007. 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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (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. (2) Seats and safety belts - for poor condition and apparent defects. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. How does a pilot compensate for blowback? defects. The scope of a 100 hour inspection, and annual inspection is ___________. (6) Electrical system - for chafing and improper operation of switches. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . (5) Flight and engine controls - for improper installation and improper operation. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. shall inspect (where applicable) the following components of the What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? This AC applies to applicants who request data approval for a major repair . (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (d) Each person performing an annual or 100-hour inspection Attorney, Terms of Water vapor weighs 5/8 as much as dry air. (6) Engine controls - for defects, improper travel, and improper safetying. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 2115 0 obj <>stream (iii) After effect. improper operation. (9) Accessories - for apparent defects in security of A completed copy of that form shall be -. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 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