____ 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. (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. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (2) Studs and nuts - for improper torquing and obvious defects. (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. (7) All systems - for improper installation, poor general This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. 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. (a) General. Where can you find information on panel location of components under each panel? pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . (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. (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. deterioration, distortion, evidence of failure, and insecurity of (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. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. Where is the center of gravity located on an aircraft with tricycle landing gear? For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. a. certified repair station b. A&P mechanic with IA rating c. either. (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. He shall thoroughly clean the aircraft and aircraft engine. 'r28J].@J)V@!Y(c,4
WDskq +~#(^S_4=c9mOtO? The simplest rotor system is the _________. 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. Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? (2) Powerplant major alterations. (4) Permanent marking. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. When must an Airworthiness Directive be complied with? Where are technical descriptions of certificated propellers found? (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. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . AC. "Removed right wing from aircraft and removed skin from outer 6 feet. (3) Anti-icing devices - for improper operations and obvious defects. (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. (4) Engine mount - for cracks, looseness of mounting, and (4) The maintenance, preventive maintenance, or alteration is recorded in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter. (iv) Installation of a propeller governor or feathering system. center section assembly for poor general condition, fabric or skin (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. A __________ must be used to perform all aircraft inspections. (3) Servicing landing gear shock struts by adding oil, air, or both. (5) Flight and engine controls - for improper installation and improper operation. (iii) Rewinding the field coil of an electrical accessory. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (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.. He shall thoroughly clean the aircraft and aircraft engine. shall inspect (where applicable) all components of the wing and (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . Purpose. Inspection programs for aircraft operating under 21.191 (d) and (e) Ifyou believe that this page should betaken down, please follow our DMCA take down process, Ensure the security ofyour data and transactions, Georgia Interim Lien Waiver And Release2013 Sub Sub - Benning, Georgia Final Lien Waiver And Release 2013 Sub Sub - Benning, 2nd Tier Subcontractor/Supplier List - Level 3 Construction, Daigger Automated Microplate Reader Operations Manual PDF, Identity Pertinent details of the repair are on file at this repair station under Order No. The holder of an IA cannot . (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. AUTHORITY: 42 U.S.C. Which type of inspection program do the 14 CFR part 121 Airlines use? shall inspect (where applicable) the following components of the (3) Anti-icing devicesfor improper oper- (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. (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. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. 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. 43.15 - Additional performance rules for inspections. 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. 3. Spars are to wings as__________ are to the fuselage. Handbook, DUI (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. condition, defects, and insecure attachment. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. foul the controls. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. 43.2 - Records of overhaul and rebuilding. 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? The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. The method must deter the installation of the part after it has reached its life limit. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. ?G!\r_4 10 :|qEC$LQPQB. thoroughly clean the aircraft and aircraft engine. ( 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. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. What is an attitude, and what are some common positive and negative attitudes about physical activity? f-``0>, %
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and insecure mounting. (8) Exhaust stacks - for cracks, defects, and improper attachment. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (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) Non-permanent marking. 0
E 14 CFR Ch. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (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. (29) Removing, checking, and replacing magnetic chip detectors. 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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (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. 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. defects. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (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. %PDF-1.6
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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. Which of the following contains a minimum checklist for a 100 hour inspection? (xxiii) The repair of portions of skin sheets by making additional seams. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (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) -. Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. ECO 17212. A typical preflight inspection is performed by ________ and would include________. particles or foreign matter on screens and sump drain plugs. (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. fatigue, and distortion. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T Title 14 CFR part 135, 135.437(b . We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. (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. Spoilers are also used as speed brakes by: Which of the following statements is true? A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. LLC, Internet 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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (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). (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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Us, Delete The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? (7) Wheels - for cracks, defects, and condition of bearings. |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 USLegal fulfills industry-leading security and compliance standards. 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. Explanation of Changes. AC. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. Wing braces are the main structural member of a wing. (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. 43.12 - Maintenance records: Falsification, reproduction, or alteration. Get access to thousands of forms. Appendix D. Scrap or Salvageable Aircraft Products and Articles. 2115 0 obj
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safetying. (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) The main rotor and center section (or the equivalent area). This system may include electronic, paper, or other means of record keeping. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). 1993, 29 FR 5451, Apr. (2) Wiring and conduits - for improper routing, insecure Ensures that a website is free of malware attacks. The repair of portions of skin sheets by making additional seams. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . Every part of an aircraft must be planned to carry the load imposed upon it. hbbd``b`Z"c`@B=8r?O K
A tag or other record may be attached to the part. 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. 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. endstream
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(4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Title 14 CFR part 65, 65.95(a)(1); 3. Ailerons are used for which axis control? (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Aircraft inspection checklists must be FAA approved. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. insecure mounting, and improper operation. The checklist 14 CFR 43, Appendix D (or similar, like the checklist in AC-90-89B), should be used whether the aircraft is experimental or certified. mounting, and obvious defects. (3) Bonding and shielding - for improper installation and poor Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (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. He shall The interrogations should be made at a nominal rate of 50 interrogations per second. CFR prev | next The tests in (e) through (j) apply only to Mode S transponders. (6) Engine controls - for defects, improper travel, and improper An aircraft Type Certificate Data Sheet contains. Most helicopters use ____________ airfoil rotor blades. (f) Each person performing an annual or 100-hour inspection gtag('js', new Date()); (2) The date of completion of the work performed. APPENDIX D TO FAR PART 43 SCOPE AND DETAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100HOUR INSPECTIONS(a) Each person performing an annual or 100hour inspection. 295 0 obj
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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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. Collapse to view only 43.13 - Performance rules (general). hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ (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) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. component operation. 1.2 Applicability. %PDF-1.6
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