(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. (a) Maintenance record entries. Each time the part is removed from a type certificated product, the record must be updated with the current life status. 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). 28 May 2020 D. DCN 3007. shall inspect (where applicable) all components of the wing and and found to comply with paragraph (c), appendix E, of part 43 of this chapter. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (7) Wheels - for cracks, defects, and condition of bearings. function gtag(){dataLayer.push(arguments);} (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). (3) Bonding and shielding - for improper installation and poor (iii) Performed without the use of tools and/or special equipment. 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) Floats and skis - for insecure attachment and obvious or With US Legal Forms the process of creating legal documents is anxiety-free. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (a) Maintenance record entries. Forms, Real Estate (7) Wheels - for cracks, defects, and condition of bearings. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. (2) Seats and safety belts - for poor condition and apparent (b) Each person performing an annual or 100-hour inspection What provides the thrust for a Gyrocopter? fS3c}^ )L 4FJG,)(-\> Business. (a) Major alterations - (1) Airframe major alterations. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. (7) All systems - for improper installation, poor general ___________ inspections are limited to surface crack detection in aircraft parts. If (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. & Estates, Corporate - looseness of engine to mount. switches. (iv) Installation of a propeller governor or feathering system. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. (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. 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. (21) Replacing any hose connection except hydraulic connections. Learn more ME406 Series Emergency Locator Transmitter - ACR. (v) Installation of structural parts other than the type of parts approved for the installation. (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. The pilot, walking around the aircraft A special Inspection may include the following: Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. (3) That product does not accumulate time in service while the part is removed. 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". Technology, Power of (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (5) Flight and engine controls - for improper installation and improper operation. (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. Sign off for an annual inspection can be done by who? The interrogations should be made at a nominal rate of 50 interrogations per second. We make completing any Part 43 Appendix D much faster. (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. (3) Non-permanent marking. Every part of an aircraft must be planned to carry the load imposed upon it. operation. Ni}Ja7$? 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). 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. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). Access the most extensive library of templates available. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. Which maintenance action is an airframe major repair? (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. (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. (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 maximum time a 100 hour inspection can be extended is ______________. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. (xxi) Repairs involving the substitution of material. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 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 -. A tag or other record may be attached to the part. 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. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (5) Replacing defective safety wiring or cotter keys. (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. 43.15 Additional performance rules for inspections. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. 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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. particles or foreign matter on screens and sump drain plugs. The tag or record must include the part number, serial number, and current life status of the part. 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. (4) Retracting and locking mechanism - for improper operation. (c) Each person performing an annual or 100-hour inspection This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. The signature constitutes the approval for return to service only for the work performed. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 288 0 obj <> endobj The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? He shall thoroughly clean the aircraft and aircraft engine. Highest customer reviews on one of the most highly-trusted product review platforms. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. 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. How does a pilot compensate for blowback? 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. Title 14 - Aeronautics and Space CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C - AIRCRAFT PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION 43.15 Additional performance rules for inspections. Most helicopters use ____________ airfoil rotor blades. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. 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. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (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. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the 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 -. Another common name for radiographic inspections is ______________. 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. Guarantees that a business meets BBB accreditation standards in the US and Canada. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. Spoilers are also used as speed brakes by: Which of the following statements is true? The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (c) Annual and 100-hour inspections. Due to aggressive automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to these sites is limited to access to our extensive developer APIs. 28-1.". 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. 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. (8) Exhaust stacks - for cracks, defects, and improper attachment. 1.2 Applicability. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (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. 43, App. defects. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. E 14 CFR Ch. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. %PDF-1.6 % 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 . (v) Replacement of outer laminations on fixed pitch wood propellers. (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. 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