(10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (3) Bonding and shielding - for improper installation and poor condition. switches. Ensure the info you add to the Part 43 Appendix D is updated and correct. window.dataLayer = window.dataLayer || []; Title 14 CFR part 65, 65.95(a)(1); 3. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in . (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. USLegal fulfills industry-leading security and compliance standards. (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. 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? The person approving or disapproving return to service. Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. (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. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. Inspection programs for aircraft operating under 21.191 (d) and (e) Which type of inspection program do the 14 CFR part 121 Airlines use? 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. (c) Each person performing an annual or 100-hour inspection (9) Accessories - for apparent defects in security of mounting. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. LLC, Internet (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Business. insecure attachment, improper component installation, and improper (2) Studs and nuts - for improper torquing and obvious (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)). (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. 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. (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. ____ months of practical experience working on aircraft, are required to apply for an A&P certificate, if the applicant hasn't attended a Part 147 school. shall, before that inspection, remove or open all necessary (2) Systems and components - for improper installation, apparent defects. Experience is the act of having performed the task before. 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. (iv) Installation of a propeller governor or feathering system. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. 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. This change A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. Which type of inspection program do the 14 CFR part 121 Airlines use? He shall thoroughly clean the aircraft and aircraft engine. condition, apparent and obvious defects, and insecurity of (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. Forms, Real Estate there is weak cylinder compression, for improper internal condition The leading editor is already at your fingertips providing you with various useful instruments for submitting a Part 43 Appendix D. The following tips, combined with the editor will assist you with the entire process. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. CFR prev | next For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (a) General. Theft, Personal 5. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. A 100 hour inspection is required on ______________. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. (21) Replacing any hose connection except hydraulic connections. When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate, The issuance of an Airworthiness Certificate is governed by, Specifications pertaining to an aircraft, of which a limited number were manufactured under a type certificate and for which there is no current Aircraft Specification, can be found in the. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. (3) Anti-icing devices - for improper operations and obvious defects. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. What are three characteristics of a sprawling stance? (ii) Repairing or machining of steel hubs. Use the correct address and at least two incorrect addresses. He shall Eight 1/4 -- 20 inch standard heli-coils were replaced. Enjoy smart fillable fields and interactivity. Ni}Ja7$? (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 -. AC. 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. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 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. 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. 43.15 Additional performance rules for inspections. (iv) Complete disassembly of complex hydraulic power valves. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, (c) Disposition of parts removed from type-certificated products. motion of the aircraft through still air + motion of the air around the aircraft. Instructions for completing the field approval checklist (see Appendix A). I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. Where are technical descriptions of certificated propellers found? 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. Learn more ME406 Series Emergency Locator Transmitter - ACR. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (4) Permanent marking. (6) Electrical system - for chafing and improper operation of switches. 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. 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. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. 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. What type of rotor is found on helicopters with two rotor blades? 3320 0 obj <> endobj (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. (2) Powerplant major alterations. Handbook, DUI shall inspect (where applicable) all components of the wing and ( 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. 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. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. (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). Elevators move the aircraft around which axis? The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. condition. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (3) Propeller major alterations. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (2) Replacing elastic shock absorber cords on landing gear. (2) Studs and nuts - for improper torquing and obvious defects. %%EOF (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Use the surveillance formats UF = 4 and 5. 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. (2) Shock absorbing devices - for improper oleo fluid level. (a) Maintenance record entries. (iii) Performed without the use of tools and/or special equipment. (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. 23, 1964, unless otherwise noted. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. Aircraft Specifications or Aircraft Type Certificate Data Sheet. Look up Federal Regulations; If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (5) Replacing defective safety wiring or cotter keys. Which of the following contains a minimum checklist for 100-hour inspections of engines? (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. With US Legal Forms the process of creating legal documents is anxiety-free. Appendix D. Scrap or Salvageable Aircraft Products and Articles. An official website of the United States government. Where is the center of gravity located on an aircraft with tricycle landing gear? The part may be mutilated to deter its installation in 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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (7) Lines, hoses, and clamps - for leaks, improper condition and The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. (b) The tests required by paragraph (a) . PRINCIPLE CHANGES. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Purpose. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. The signature constitutes the approval for return to service only for the work performed. (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. How are main rotors of helicopters classified? (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. A ________ may request to see your mechanic certificate. May 21/2007. 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. The interrogations should be made at a nominal rate of 50 interrogations per second. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. poor condition. (5) Flexible vibration dampeners - for poor condition and (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (iii) Installation of an accessory which is not approved for the engine. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (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. 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