This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. (ix) Hydraulic and electrical actuating system of components. (i) Power output (static and idle r.p.m. The maximum time a 100 hour inspection can be extended is ______________. (5) Flight and engine controls - for improper installation and improper operation. Explanation of Changes. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (6) Electrical system - for chafing and improper operation of (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 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. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. ?G!\r_4 10 :|qEC$LQPQB. (2) Seats and safety belts - for poor condition and apparent defects. ___________ inspections are limited to surface crack detection in aircraft parts. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. If you want to request a wider IP range, first request access for your current IP, and then use the "Site Feedback" button found in the lower left-hand side to make the request. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (7) Lines, hoses, and clamps - for leaks, improper condition and (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. Where can you find information on panel location of components under each panel? (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. This AC addresses the manufacturing and production requirements of part 21, defects. A typical preflight inspection is performed by ________ and would include________. Make sure that every field has been filled in properly. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Guide, Incorporation (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. (3) Propeller major repairs. (d) Progressive inspection. ____ 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. Forms, Real Estate (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. 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. (d) Each person performing an annual or 100-hour inspection Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. The method must deter the installation of the part after it has reached its life limit. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. (3) That product does not accumulate time in service while the part is removed. (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. a. certified repair station b. A&P mechanic with IA rating c. either. (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. (4) Retracting and locking mechanism - for improper operation. (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. (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. Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. Elevators move the aircraft around which axis? (6) Engine controls - for defects, improper travel, and improper (3) Propeller major alterations. 3335 0 obj <>/Filter/FlateDecode/ID[]/Index[3320 28 3615 1]/Info 3319 0 R/Length 87/Prev 1015044/Root 3321 0 R/Size 3616/Type/XRef/W[1 2 1]>>stream This change (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. defects. improper operation. (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. (2) Bolts - for improper torquing and lack of safetying. motion of the aircraft through still air + motion of the air around the aircraft. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Slats increase the _________ at which laminar airflow can exist. 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. Instrument repairs may be performed ___________________________. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. The scope of a 100 hour inspection, and annual inspection is ___________. (iii) Rewinding the field coil of an electrical accessory. deterioration, distortion, evidence of failure, and insecurity of What are three characteristics of a sprawling stance? %PDF-1.6 % window.dataLayer = window.dataLayer || []; (2) Bolts - for improper torquing and lack of safetying. LLC, Internet (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (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. (3) Bonding and shielding - for improper installation and poor condition. (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 leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. (9) Accessories - for apparent defects in security of mounting. (18) Replacing wheels and skis where no weight and balance computation is involved. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Which of the following contains a minimum checklist for a 100 hour inspection? 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. 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". Which maintenance action is an airframe major repair? When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. insecure attachment, improper component installation, and improper (3) Windows and windshields - for deterioration and breakage. gtag('js', new Date()); (Part I.D.5). (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. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. (e) Approval requirements. /ZVH]&o9_zC1|voE. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Title 14 CFR part 135, 135.437(b . ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. Title 14 CFR part 65, 65.95(a)(1); 3. AC. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. services, For Small 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. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (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). (b) Major repairs - (1) Airframe major repairs. (3) The main rotor and center section (or the equivalent area). 43.2 - Records of overhaul and rebuilding. 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. (3) Anti-icing devices - for improper operations and obvious 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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. 2. 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. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to An aircraft Type Certificate Data Sheet contains. (xiv) The repair or replacement of internal elements of blades. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. Handbook, DUI Pt. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (1) 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; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. The part may be mutilated to deter its installation in a type certificated product. When must an Airworthiness Directive be complied with? Ensures that a website is free of malware attacks. (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. Aircraft Specifications or Aircraft Type Certificate Data Sheet. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. He shall thoroughly clean the aircraft and aircraft engine. Theft, Personal (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. 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? |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 The proposed rule added a provision to 12 CFR 748.1 for the NCUA to require notification of any cyber incident that rises to the level of a reportable cyber incident as soon as possible but no later than 72 hours after a FICU reasonably believes that a reportable cyber incident has occurred. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Any other method approved or accepted by the FAA. Where are technical descriptions of certificated propellers found? (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. failure, and insecurity of attachment. 28-1.". (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (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. 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. A security threat, as defined by the TSA, will result in your mechanic application being _______. Inspection programs for aircraft operating under 21.191 (d) and (e) (i) Each person performing an annual or 100-hour inspection (2) Wiring and conduits - for improper routing, insecure (b) Each person performing an annual or 100-hour inspection (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. (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.. 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 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. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. A tag or other record may be attached to the part. (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. (d) Performance requirements. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? Access the most extensive library of templates available. condition, defects, and insecure attachment. 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. (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. (6) Batteries - for improper installation and improper charge. 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. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 1993, 29 FR 5451, Apr. 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. 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