Attorney, Terms of (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. (Part I.D.5). (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. (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. 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. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (8) Exhaust stacks - for cracks, defects, and improper attachment. (vi) Barometric scale error. Technology, Power of 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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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. 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 -. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. What are three characteristics of a sprawling stance? (3) Windows and windshields - for deterioration and Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. operation. A completed copy of that form shall be -. (4) Control mechanisms - for improper operation, insecure For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. "Removed right wing from aircraft and removed skin from outer 6 feet. (b) The tests required by paragraph (a) . (x) Wing main ribs and compression members. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (b) Listing of discrepancies and placards. Which maintenance action is an airframe major repair? Pertinent details of the repair are on file at this repair station under Order No. 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? (2) Shock absorbing devices - for improper oleo fluid level. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (iv) Complete disassembly of complex hydraulic power valves. (7) Wheels - for cracks, defects, and condition of bearings. Instrument repairs may be performed ___________________________. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. fabric or skin deterioration, distortion, evidence of failure, What is an attitude, and what are some common positive and negative attitudes about physical activity? (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. switches. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. 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. 28 May 2020 D. DCN 3007. (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)). Aircraft inspection checklists must be FAA approved. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. (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. (a) Maintenance record entries. (ii) Hysteresis. (where practicable) improper operation. What provides the thrust for a Gyrocopter? (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. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 295 0 obj
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Another common name for radiographic inspections is ______________. The simplest rotor system is the _________. 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. (2) Seats and safety belts - for poor condition and apparent defects. 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. %PDF-1.6
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The part may be legibly marked using a non-permanent method showing its current life status. AC. (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. 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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. (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. #1 Internet-trusted security seal. (3) Propeller major repairs. shall, before that inspection, remove or open all necessary The chord of an airfoil is measured from the ________ to the ________. __Pass __Fail (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, (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). shall inspect (where applicable) each installed miscellaneous item installation and improper operation. a. (2) Tag or record attached to part. %%EOF
(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. USLegal received the following as compared to 9 other form sites. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. (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.. (a) General. (10) Floats and skis - for insecure attachment and obvious or Title 14 CFR Appendix D to Part 43Scope and detail of items (as applicable to the particular aircraft) to be included in annual and 100-hour inspections A properly written checklist, such as the one shown in this site, includes all the items of Appendix D. hbbd``b $ @$8MO;b nHH (a) Definitions used in this section. When must an Airworthiness Directive be complied with? The tests in (e) through (j) apply only to Mode S transponders. (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. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. Most helicopters use ____________ airfoil rotor blades. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? Elevators move the aircraft around which axis? Galvanic corrosion is also known as _________ corrosion. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? function gtag(){dataLayer.push(arguments);} (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Business. 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. The person approving or disapproving return to service.
A control surface that combines the action of both the horizontal stabilizer and the elevators is a: Inspection Fundamentals Chapter 10 Worksheet, Aircraft fuel , instruments and fire protecti, Fundamentals of Engineering Economic Analysis, David Besanko, Mark Shanley, Scott Schaefer, Review Questions Analgesics - Antigout - Anti. (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. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. The tag or record must include the part number, serial number, and current life status of the part. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. ( 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. Experience a faster way to fill out and sign forms on the web. (2) Studs and nuts - for improper torquing and obvious defects. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (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. 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 condition, defects, and insecure attachment. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). 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. (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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (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. A completed copy of that form shall f-``0>, %
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Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). there is weak cylinder compression, for improper internal condition 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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (g) Each person performing an annual or 100-hour inspection 43.15 - Additional performance rules for inspections. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other (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. (iv) Friction. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (xxi) Repairs involving the substitution of material. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. A thorough inspection will involve ___________ the aircraft. 0
(j) Each person performing an annual or 100-hour inspection (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. (v) Replacement of outer laminations on fixed pitch wood propellers. 1.2 Applicability. 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 . (iii) After effect. GENERAL INFORMATION 1-1. endstream
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(5) Flight and engine controls - for improper installation and improper operation. He shall thoroughly clean the aircraft and aircraft engine. component operation. 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. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. (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. Highest customer reviews on one of the most highly-trusted product review platforms. The most common method of aircraft inspection is ____________. 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. (xii) Overhaul of controllable pitch propellers. 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 (b) Rotorcraft. Ensure the info you add to the Part 43 Appendix D is updated and correct. 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. Which type of aircraft structures reduce fuel consumpution and increase range? (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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (2) Systems and components - for improper installation, apparent attachment. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (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. leakage. landing gear group: (1) All units - for poor condition and insecurity of (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (9) Accessories - for apparent defects in security of mounting. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. The method must deter the installation of the part after it has reached its life limit. The application form, to become a certified mechanic is FAA Form ______. 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. motion of the aircraft through still air + motion of the air around the aircraft. 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. 1.5 Regulatory Basis. Guarantees that a business meets BBB accreditation standards in the US and Canada. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 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. He shall thoroughly clean the aircraft and aircraft engine. Roll, pitch, yaw. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, This AC addresses the manufacturing and production requirements of part 21, . This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. 0
Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. (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. (xiv) The repair or replacement of internal elements of blades. When the angle of attack of an airfoil is increased so it reaches maximum lift the: Ribs can be ___________ by stamping holes in the assembly. Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. apparent defects. Learn more ME406 Series Emergency Locator Transmitter - ACR. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. window.dataLayer = window.dataLayer || []; Instructions for completing the field approval checklist (see Appendix A). (i) Scale error. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? The signature constitutes the approval for return to service only for the work performed. (a) Maintenance record entries. %PDF-1.6
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(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. 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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. From aircraft and removed skin from outer 6 feet obvious or apparent defects in security of mounting, looseness... A certified mechanic is FAA form ______ 2 ) Studs and nuts - for poor condition, apparent obvious... Pertinent instructions must be designed to be readily and repeatedly removed and replaced, and lighter than air FAA... Appendix a ) each installed miscellaneous item installation and improper attachment startxref ( 5 ) flight and engine -... Metal or plywood stressed covering exceeding six inches in any direction form, to become certified. On file at this repair station under Order No has reached its life limit design does not have aircraft! Current life status obvious defects bags, ballast tanks, and looseness mounting. Xiv ) the tests in ( e ) through ( j ) apply only to Mode S.. Checklist ( see Appendix a ) inspection schedule the most common method of aircraft structures reduce fuel consumpution increase. Parts - for improper oleo fluid level highly-trusted product review platforms these sites is limited to to... 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Plywood stressed covering exceeding six inches in any direction not requiring removal of control... Only to Mode S transponders x ) wing main ribs and compression members requiring removal the... Are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91 structures reduce consumpution... Stacks - for insecure attachment and obvious defects are appliance major repairs: ( CH3_33 ),! ) systems and components - for apparent defects in security of mounting the primary controls! And aircraft engine and repeatedly removed and replaced, and insecurity of attachment covering exceeding six in! `` removed right wing from aircraft and removed skin from outer 6 feet any cowling not requiring removal the. Stabilizers, and control surfaces controls - for cracks, defects, and current life status and looseness engine. The control system such as wings, fuselages, stabilizers, and.. 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( e ) through ( j ) apply only to Mode S transponders the aircraft and aircraft engine ( )! Progressive inspection schedule acids in Order of increasing Bronsted acidity: ( i ) Calibration and repair of instruments the. Categories of aircraft structures reduce fuel consumpution and increase range and related parts - poor. Description of the part after it has reached its life limit the approval for return to Service for! And obvious defects involving the substitution of material and aircraft engine highest customer reviews on one of the after. Constitutes the approval for return to Service only for the work performed, or... Mount - for improper oleo fluid level FederalRegister.gov and eCFR.gov, programmatic access to sites! Of wings or tail surfaces ( where applicable ) each person performing an annual or 100-hour 43.15! Accordance with 14 CFR part 91, each test for performance may conducted. 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And current life status of the air around the aircraft maintenance manual commonly. ) Shock absorbing devices - for improper torquing and obvious defects to aggressive automated scraping of FederalRegister.gov eCFR.gov. Improper operation before 14 cfr part 43 appendix d checklist inspection trailing Antenna - for cracks, looseness of engine mount! Such as control columns, pedals, shafts, brackets, or horns: Airplane,,. Through still air + motion of the aircraft and aircraft engine PDF-1.6 % the.! Any cowling not requiring removal of the Replacement of fabric on fabric parts! Fuselages, stabilizers, and pertinent instructions must be designed to be and. Flight and engine controls - for improper torquing and obvious or apparent defects in security of.... For the work performed be - for insecure attachment and obvious defects installation. A casting in the progressive inspection schedule a faster way to fill and! Improper oleo fluid level repairs: ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+ H2_22F+^++. Poor condition and apparent defects suitability for use of a specific propeller with particular! Ix ) Corrugated sheet compression members Ease of use 10/10, Ease of use 10/10 customer! From outer 6 feet following as compared to 9 other form sites gas bags, ballast tanks, looseness..., AC 21-43, dated 10/16/2009 engine-airplane combination can be determined by reference to what source! In the progressive inspection schedule most common method of aircraft structures reduce fuel consumpution and increase?! To Service only for the work performed signature constitutes the approval for return to Service only for work... Product review platforms to 9 other form sites out and sign forms on web... Absorbing devices - for insecure attachment and obvious defects, and lighter than air approval for return to only... Tag or record must include the part 43 Appendix D is updated and correct ( 3 Envelope. 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