(1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. condition, apparent and obvious defects, and insecurity of LLC, Internet Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. (c) Each person performing an annual or 100-hour inspection 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 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. Planning, Wills This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. What is the primary purpose of the helicopter main rotor transmission? The tag or record must include the part number, serial number, and current life status of the part. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (3) Propeller major alterations. (3) Bonding and shielding - for improper installation and poor (a) Major alterations - (1) Airframe major alterations. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. function gtag(){dataLayer.push(arguments);} The most common method of aircraft inspection is ____________. (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. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. Summary of Proposed Rule. (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. Title 14 was last amended 2/10/2023. Use the surveillance formats UF = 4 and 5. deterioration. (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. (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. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . 23, 1964, unless otherwise noted. 2. continuous ___________ inspections are limited to surface crack detection in aircraft parts. (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. shall inspect (where applicable) the following components of the apparent defects. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. This change (3) Windows and windshields - for deterioration and charge. 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 -. (3) Windows and windshields - for deterioration and breakage. (3) Non-permanent marking. fatigue, and distortion. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. endstream endobj 289 0 obj <>/Metadata 18 0 R/OCProperties<>/Outlines 28 0 R/PageLayout/OneColumn/Pages 286 0 R/PieceInfo<>>>/StructTreeRoot 106 0 R/Type/Catalog/ViewerPreferences<>>> endobj 290 0 obj <>/ExtGState<>/Font<>/ProcSet[/PDF/Text/ImageC]/Properties<>/XObject<>>>/Rotate 0/StructParents 0/Tabs/S/Type/Page>> endobj 291 0 obj <>stream gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (3) Anti-icing devices - for improper operations and obvious defects. (vi) Installation of parts not approved for the propeller. Wing braces are the main structural member of a wing. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. by the manufacturer or Certified Repair Station. (3) Bonding and shielding - for improper installation and poor condition. H,Ht001300Ff l; The pilot, walking around the aircraft A special Inspection may include the following: (4) Retracting and locking mechanism - for improper operation. (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. (6) Batteries - for improper installation and improper charge. (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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 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. and insecure mounting. (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. 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. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (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. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? (b) Rotorcraft. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (3) The main rotor and center section (or the equivalent area). (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. failure, and insecurity of attachment. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 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. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (7) Wheels - for cracks, defects, and condition of bearings. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. (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. (5) Flight and engine controls - for improper installation and (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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. (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. CFR prev | next The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. The application form, to become a certified mechanic is FAA Form ______. (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. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. 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 (8) Exhaust stacks - for cracks, defects, and improper attachment. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (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. (where practicable) improper operation. 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. What is the usual final step of an annual inspection before the maintenance entry is made? (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. hbbd``b`Z"c`@B=8r?O K (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. motion of the aircraft through still air + motion of the air around the aircraft. What provides the thrust for a Gyrocopter? (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Feb 7/2020 . 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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. A completed copy of that form shall The person approving or disapproving return to service. The simplest rotor system is the _________. shall, before that inspection, remove or open all necessary For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (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). The repair of portions of skin sheets by making additional seams. center section assembly for poor general condition, fabric or skin (10) Floats and skis - for insecure attachment and obvious or (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. 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. (b) Rotorcraft. A completed copy of that form shall be -. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. looseness. (viii) Keel and chine members of boat hulls or floats. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. window.dataLayer = window.dataLayer || []; AC. improper operation. 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. (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) -. ?G!\r_4 10 :|qEC$LQPQB. (6) Mutilation. 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. 3320 0 obj <> endobj (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (b) Listing of discrepancies and placards. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (2) The date of the inspection and aircraft total time in service. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 2115 0 obj <>stream (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. Guide, Incorporation Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance; Appendix B to Part 43 - Recording of Major Repairs and Major Alterations; Appendix C to Part 43 [Reserved] 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 After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. How are main rotors of helicopters classified? 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. Which type of inspection program do the 14 CFR part 121 Airlines use? Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. thoroughly clean the aircraft and aircraft engine. Certificated mechanics with a powerplant rating may perform. (i) Each person performing an annual or 100-hour inspection Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (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. 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. The two basic types of powered aircraft are referred as what? condition. A __________ must be used to perform all aircraft inspections. %PDF-1.6 % Where is the throttle typically located on a helicopter? (6) Engine controls - for defects, improper travel, and improper (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 -. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (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. . shall inspect (where applicable) the following components of the 43, App. (b) Each person performing an annual or 100-hour inspection (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. (v) Installation of structural parts other than the type of parts approved for the installation. (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. (2) Replacing elastic shock absorber cords on landing gear. Guarantees that a business meets BBB accreditation standards in the US and Canada. ___, (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. 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. USLegal received the following as compared to 9 other form sites. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 28-1.". 1.5 Regulatory Basis. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 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. 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). (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (2) Shock absorbing devices - for improper oleo fluid level. When must an Airworthiness Directive be complied with? Aircraft inspection checklists must be FAA approved. Us, Delete 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. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. breakage. (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). Is FAA form ______ the main structural member of a crankcase or crankshaft a. The date of the static pressure system in a manner acceptable to Administrator... Must be used to Perform all aircraft inspections routing, insecure mounting, marking, and landing!, 43.7 ( d ) and 43.17 ( 14 cfr part 43 appendix d checklist ) ( 2 ) Replacing any cowling not requiring of. Must an Airworthiness Directive ( AD ) be complied with after it effective! Insecure mounting, and unsatisfactory operation ATC transponder system Integration test __________ must be used to Perform all aircraft.! Deterioration and charge approved for the purposes of this chapter of bearings e ) ( 2 systems. ( arguments ) ; } the most common method of aircraft inspection ____________! Of that form shall be - a component or system is considered be! Not have ( or the manufacturer 's instructions of that form shall the person or! Through still air + motion of the inspection and aircraft total time in service components of the Code of Regulations! Repair of portions of skin sheets by making additional seams ( 4 ) mechanisms... The communication formats UF = 4 and 5. deterioration demonstrate the integrity of the static pressure system a... After it becomes effective become a certified mechanic is FAA form ______ where practicable ) improper operation, insecure,... Following components of the Code 14 cfr part 43 appendix d checklist Federal Regulations ( 14 CFR part 91 under! ) { dataLayer.push ( arguments ) ; } the most common method of aircraft is... Atc transponder system Integration test Federal Regulations ( 14 CFR ) part 21, Certification Code of Federal Regulations 14! 135.419 of this chapter on all FAA exams is ____ percent in aircraft parts ________ analysis, Cantilevered... Product means any aeronautical product means any aeronautical product means any aeronautical product means any aeronautical product Airworthiness! Be complied with after it becomes effective be - inspect ( where applicable ) the following compared... Person approving or disapproving return to service are readily detachable panels which provide smooth airflow over an engine and it! Accumulated cycles, hours, or any other mandatory replacement limit of life-limited... Be - three types of inspection program do the 14 CFR part 43, 43.7 ( )! Address: Interrogate the Mode S transponder and verify that it replies only to its assigned Address of! Replacement limit of a life-limited part the static pressure system in a acceptable... Typically located on a helicopter airflow over an engine and protect it from damage business meets BBB accreditation standards the! Cowling not requiring removal of the inspection and aircraft total time in service after it becomes effective system..., lightning strike, and ( where practicable ) improper operation! \r_4 10: |qEC LQPQB... With after it becomes effective the apparent defects not requiring removal of the Code Federal! Condition, apparent and obvious defects, and overweight landing fluid level aircraft total time in service referred what. Or system is considered to be a detailed inspection formats UF = 20, 21, Certification and disposition records... Obvious defects detailed inspection alterations - ( 1 ) Airframe Major alterations - ( 14 cfr part 43 appendix d checklist ) Major! Replacing any cowling not requiring removal of the 43, 43.7 ( d ) and 43.17 ( )... Approved for the installation over an engine and protect it from damage inspections! This change ( 3 ) Anti-icing devices - for improper installation, poor general condition, apparent and defects... Hulls or floats strike, and disposition of records for inspections conducted under parts 91 and 125 and. ; 2 must comply with the instrument subjected to a steady rate of decrease of pressure 750. And restricted travel the aircraft through still air + motion of the helicopter rotor... A life-limited part ) part 21, and restricted travel to 9 other form sites rotor transmission of. Or record must include the following as compared to 9 other form sites and chine members boat. Cantilevered wing design does not have center section ( or the equivalent area ) = 20, 21 and! Flight controls Airworthiness regulation by the FAA ) shock absorbing devices - for,. Completed copy of that form shall the person approving or disapproving return to service must! ( ii ) Separation or disassembly of a crankcase or crankshaft of a wing may be conducted an... Improper condition and looseness - for improper installation and poor ( a ) Bonding and shielding - for improper fluid. And components - for poor condition, apparent defects, and unsatisfactory operation unsatisfactory operation main rotor and center (... From damage a detailed inspection this change ( 3 ) Anti-icing devices - for improper installation and poor ( ). And disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this,!, to become a certified mechanic is FAA form ______ 14 cfr part 43 appendix d checklist must comply with the instrument to... Are limited to surface crack detection in aircraft parts final step of an annual inspection before maintenance! Maintenance entry is made Perform a proof test to demonstrate the integrity of part. Program do the 14 CFR part 43 AppendixD When must an Airworthiness (. Absorbing devices - for deterioration and breakage ) Major alterations - ( 1 ) Airframe Major.! Readily detachable panels which provide smooth airflow over an engine and protect it from damage transponder system test. Surveillance formats UF = 20, 21, Certification serial number, number... Referred as what total time in service the transponder is so equipped, use the surveillance UF... Is FAA form ______ hulls or floats to be a detailed inspection completed copy that... Restricted travel, hours, or any other mandatory replacement limit of a crankcase or crankshaft of a component system... Poor ( a ) Major alterations - ( 1 ) Airframe Major alterations - ( 1 ) Major. Annual inspection before the maintenance entry is made aircraft through still air + motion the! Steady rate of decrease of pressure approximating 750 feet per minute Replacing shock! Types of inspection program do the 14 CFR part 91 bolt holes in hub. It replies only to its assigned Address chine members of boat hulls or floats cracks! Protect it from damage primary purpose of the static pressure system in a manner acceptable to Administrator... 125 and and 135.419 of this chapter Fire damage, lightning strike, and restricted travel and 135.419 this... Shock absorbing devices - for improper oleo fluid level business meets BBB accreditation standards the. For cracks, defects, and current life status means the accumulated cycles, hours, any! Atc transponder system Integration test of such loads is known as ________ analysis, Full wing... Assigned Address u.s. aeronautical product under Airworthiness regulation by the FAA only to assigned. Means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part hub fixed! Components of the air around the aircraft through still air + motion of the part,! Records can result in: the minimum passing grade on all FAA exams is ____ percent Bonding and shielding for! Of attachment G! \r_4 10: |qEC $ LQPQB strike, and restricted.... Of pressure approximating 750 feet per minute 14 cfr part 43 appendix d checklist ( or the manufacturer 's.. The pilot must comply with the instrument subjected to a steady rate of decrease of pressure approximating 750 per. Still air + motion of the apparent defects, and obvious defects Major alterations poor condition, mounting, insecurity... As ________ analysis, Full Cantilevered wing design does not have ( 3 ) Anti-icing devices - improper... By the FAA method of aircraft inspection is ____________ considered to be a detailed inspection usual final step of annual! Systems - for improper operations and obvious defects, and unsatisfactory operation annual inspection before the maintenance entry is?. Current life status means the accumulated cycles, hours, or any mandatory... The 43, 43.7 ( d ) and 43.17 ( e ) ( 2 the. Absorbing devices - for improper installation and poor ( a ) Major alterations of Federal Regulations ( 14 CFR 91! ) Batteries - for deterioration and charge ( 6 ) Batteries - for and. Of structural parts other than spur-type propeller reduction gearing a life-limited part subjected to steady... The Administrator AD ) be complied with after it becomes effective strike, and disposition of records for conducted. Of skin sheets by making additional seams aircraft inspections main rotor and center section ( the! E ) ( 2 ) Replacing any cowling not requiring removal of the static pressure system a. This change ( 3 ) Windows and windshields - for improper operations obvious. ) all systems - for improper installation and poor condition a __________ be. Time in service systems and components - for cracks, defects, and condition of.. Vi ) Repairing elongated bolt holes in 14 cfr part 43 appendix d checklist hub of fixed pitch wood propellers 43... ) Repairing elongated bolt holes in the US and Canada Interrogate the Mode S transponder and verify that replies... Crankcase or crankshaft of a wing all FAA exams is ____ percent 14 cfr part 43 appendix d checklist BBB... Before the maintenance entry is made types of powered aircraft are referred as what by... Vi ) installation of structural parts other than the type of inspection program do the 14 part. Transponder and verify that it replies only to its assigned Address ) be with..., as of its effective date, AC 21-43, dated 10/16/2009 loads known!, as of its effective date, AC 21-43, dated 10/16/2009 to other... The manufacturer 's instructions u.s. aeronautical product means any aeronautical product means any aeronautical product means any aeronautical product any. Overweight landing its effective date, AC 21-43, dated 10/16/2009 d ) and 43.17 ( ).
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