attachment. 43.12 - Maintenance records: Falsification, reproduction, or alteration. Decrease engine output RPM to optimum rotor RPM. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Ni}Ja7$? (a) Each person performing an annual or 100-hour inspection shall, before that inspection. hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok A thorough inspection will involve ___________ the aircraft. (8) Exhaust stacks - for cracks, defects, and improper attachment. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (h) Each person performing an annual or 100-hour inspection endstream endobj startxref (ii) Hysteresis. (i) Power output (static and idle r.p.m. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. (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. 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. (5) Segregation. What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. shall inspect (where applicable) the following components of the and improper internal tolerances. (a) Maintenance record entries. 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. 28 May 2020 D. DCN 3007. (5) Flight and engine controls - for improper installation and Where should you find this entry? (c) Authorized persons. Guide, Incorporation Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. An airplane with a nose and main landing gear is referred to as being: _________ ___________ and _________ _________ are used to move fowler flaps along their designed route of travel. (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. The error at all test points must not exceed the tolerances specified in Table I. (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. (v) Case leak. The __________ is used to thoroughly service a component after it is removed from an aircraft. What type of rotor is found on helicopters with two rotor blades? (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (d) Each person performing an annual or 100-hour inspection We make completing any Part 43 Appendix D much faster. Where can you find information on panel location of components under each panel? APPENDIX Appendix A - Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, APPENDIX Appendix B - Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, APPENDIX Appendix C - Appendix C to Part 43 [Reserved], APPENDIX Appendix D - 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, APPENDIX Appendix E - Appendix E to Part 43 - Altimeter System Test and Inspection, APPENDIX Appendix F - Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. Appendix D. Scrap or Salvageable Aircraft Products and Articles. & Estates, Corporate - (4) Appliance major alterations. Feb 7/2020 . (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. Any other method approved or accepted by the FAA. Water vapor weighs 5/8 as much as dry air. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. looseness of engine to mount. This change 43.15 Additional performance rules for inspections. Title 14 was last amended 2/02/2023. (3) Anti-icing devicesfor improper oper- (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 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. Which type of inspection program do the 14 CFR part 121 Airlines use? 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. 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. (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. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. (6) Electrical system - for chafing and improper operation of (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. 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. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 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 -. 1.2 Applicability. "Removed right wing from aircraft and removed skin from outer 6 feet. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (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. (6) Engine controls - for defects, improper travel, and improper safetying. (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. (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) Powerplant major repairs. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. During the next week, create a list of at least 10 things you could have done to conserve the water you use. To keep a flat wing from stalling all at one time: The primary flight controls in a helicopter are: Cyclic, collective, and anti-torque pedals. Spanish, Localized 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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. SOURCE: Docket No. (d) Performance requirements. (2) Shock absorbing devices - for improper oleo fluid level. mounting, and obvious defects. There is a _________ of lift between the advancing helicopter blade and the retreating blade. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E attachment. Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T (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 -. Attorney, Terms of fatigue, and distortion. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (a) Definitions. The person approving or disapproving return to service. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). (d) Transfer of life-limited parts. The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. 3347 0 obj <>stream (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. A 100 hour inspection is required on ______________. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. and insecure mounting. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 1993, 29 FR 5451, Apr. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . An aircraft Type Certificate Data Sheet contains. Learn more ME406 Series Emergency Locator Transmitter - ACR. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. /ZVH]&o9_zC1|voE. For the purposes of this section the following definitions apply. (7) Wheels - for cracks, defects, and condition of bearings. A completed copy of that form shall FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (2) Systems and components - for improper installation, apparent 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. (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. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. 0 Follow the simple instructions below: The times of distressing complex legal and tax documents are over. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (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. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (2) The date of completion of the work performed. 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 the airplane log or other permanent record. Galvanic corrosion is also known as _________ corrosion. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. defects. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. charge. (23) Cleaning or replacing fuel and oil strainers or filter elements. (2) The date of the inspection and aircraft total time in service. 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 (v) Installation of structural parts other than the type of parts approved for the installation. (a) General. (2) Studs and nuts - for improper torquing and obvious defects. (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. 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. 3320 0 obj <> endobj '; (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. A ________ helicopter has two rotors on the same mast. improper operation. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (10) All systems - for improper installation, poor general After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. (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. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. (6) Engine controls - for defects, improper travel, and improper (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. shall inspect (where applicable) the following components of the (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, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. Get your online template and fill it in using progressive features. 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