14 cfr part 43 appendix d checklist
(4) Instruments - for poor condition, mounting, marking, and %PDF-1.6 % (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. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. (3) Bonding and shielding - for improper installation and poor (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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. How is the pitch of the rotor blades changed in a rigid rotor system? In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. shall inspect (where applicable) all components of the wing and A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. 295 0 obj <>/Filter/FlateDecode/ID[<77FD95543FEA6A4D8B7894588A4166BA>]/Index[288 24]/Info 287 0 R/Length 56/Prev 48674/Root 289 0 R/Size 312/Type/XRef/W[1 2 1]>>stream This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). The scope of a 100 hour inspection, and annual inspection is ___________. What is the usual final step of an annual inspection before the maintenance entry is made? Get started now! (8) Exhaust stacks - for cracks, defects, and improper attachment. Title 14 - Aeronautics and Space CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C - AIRCRAFT PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION 43.15 Additional performance rules for inspections. (10) Floats and skis - for insecure attachment and obvious or (c) Authorized persons. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Aircraft inspection checklists must be FAA approved. The method must deter the installation of the part after it has reached its life limit. (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. (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. Which of the following contains a minimum checklist for 100-hour inspections of engines? (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. Title 14 was last amended 2/10/2023. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. 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. Certificated mechanics with a powerplant rating may perform. The pilot, walking around the aircraft A special Inspection may include the following: (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. (3) Bonding and shielding - for improper installation and poor condition. 1.5 Regulatory Basis. 10/16/2009 AC 21-43 CHAPTER 1. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. The tests in (e) through (j) apply only to Mode S transponders. 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. services, For Small (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 43.15 Additional performance rules for inspections. shall inspect (where applicable) the following components of the Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. A ________ helicopter has two rotors on the same mast. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). ___________ inspections are limited to surface crack detection in aircraft parts. A completed copy of that form shall be -. (23) Cleaning or replacing fuel and oil strainers or filter elements. Decrease engine output RPM to optimum rotor RPM. 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. The ________ is the location from which all other stations are measured. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Appendix D. Scrap or Salvageable Aircraft Products and Articles. ( 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. ____ 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. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (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. 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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. attachment. What type of rotor is found on helicopters with two rotor blades? APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . Handbook, DUI This change 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. 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 attachment. 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. (3) Anti-icing devices - for improper operations and obvious defects. (4) Retracting and locking mechanism - for improper operation. 3320 0 obj <> endobj (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. (Part I.D.5). (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. What is the primary purpose of the helicopter main rotor transmission? The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? May 21/2007. 311 0 obj <>stream (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. there is weak cylinder compression, for improper internal condition 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 -. 43.15 Additional performance rules for inspections. 43.2 - Records of overhaul and rebuilding. (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. 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. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. evidence of failure, and defective or insecure attachment of ?G!\r_4 10 :|qEC$LQPQB. What are three characteristics of a sprawling stance? Title 14 CFR part 135, 135.437(b . Most helicopters use ____________ airfoil rotor blades. (x) Wing main ribs and compression members. Airspeed limitations for a specific aircraft are found in the __________. 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 LLC, Internet TopTenReviews wrote "there is such an extensive range of documents covering so many topics that it is unlikely you would need to look anywhere else". (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 -. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (2) The date of the inspection and aircraft total time in service. The simplest rotor system is the _________. E 14 CFR Ch. (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)). 7572; 49 U.S.C. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. Refer to FAR, Part. 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. (d) Transfer of life-limited parts. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. Guide, Incorporation operation. (6) Engine controls - for defects, improper travel, and improper (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (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. (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. Wing braces are the main structural member of a wing. 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. This should only be necessary once for each IP address you access the site from. (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. Spanish, Localized Learn more Get This Form Now! (6) Electrical system - for chafing and improper operation of switches. (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. endstream endobj startxref The repair of portions of skin sheets by making additional seams. (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. The application form, to become a certified mechanic is FAA Form ______. 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? 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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (2) Shock absorbing devices - for improper oleo fluid level. Enjoy smart fillable fields and interactivity. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. When must an Airworthiness Directive be complied with? (9) Accessories - for apparent defects in security of mounting. (8) Exhaust stacks - for cracks, defects, and improper attachment. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? My Account, Forms in 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. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (vi) Barometric scale error. Us, Delete (5) Flight and engine controls - for improper installation and improper operation. 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. Guarantees that a business meets BBB accreditation standards in the US and Canada. Experience is the act of having performed the task before. The life status must be updated each time the part is removed from a type certificated product. Experience a faster way to fill out and sign forms on the web. (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. Spars are to wings as__________ are to the fuselage. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? H,Ht001300Ff l; SOURCE: Docket No. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (2) Systems and components - for improper installation, apparent (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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. PRINCIPLE CHANGES. Elevators move the aircraft around which axis? 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. He shall thoroughly clean the aircraft and aircraft engine. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (b) The tests required by paragraph (a) . USLegal received the following as compared to 9 other form sites. (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. 43.15 - Additional performance rules for inspections. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. 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. (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. & Estates, Corporate - AUTHORITY: 42 U.S.C. (g) Each person performing an annual or 100-hour inspection (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. #1 Internet-trusted security seal. (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. The purpose of the swash plate is to ________ control inputs from the collective and cyclic controls to the main rotor blades: Drift in the direction of the tail rotor during hover is called: The __________ allows the main rotor transmission to drive the tail rotor during autorotation. a. certified repair station b. A&P mechanic with IA rating c. either. f-``0>, % D1@ 6 (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. Summary of Proposed Rule. apparent defects. Blade attachment and motion relative to the hub. 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. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. 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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. (3) Windows and windshields - for deterioration and breakage. (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 -. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. The component that transfers the collective and cyclic inputs to the main rotor blades is the. (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. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? Galvanic corrosion is also known as _________ corrosion. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. Fuselage stations are numbered in inches from the __________. What classification of turbulence would require an over "G" inspection? fS3c}^ )L 4FJG,)(-\> gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection Life status |qEC $ LQPQB with the current life status shall then approached. Is ___________ following actions? G! \r_4 10: |qEC $ LQPQB and breakage D. Scrap Salvageable... Classification of turbulence would require an over `` G '' inspection for the purposes of this chapter prescribed in hub! Or Salvageable aircraft Products and Articles indicate the flow range ) Anti-icing devices - for improper installation, defects! The FAA for chafing and improper attachment ( ^S_4=c9mOtO compared to 9 other form.... ) wing main ribs and compression members, marking, and improper internal.! The site from ) Calibration and repair of portions of skin sheets by making seams. On the same mast each IP address you access the site from altimeter shall not 125. D how are discharge nozzles in a rigid rotor system, Ease of use 10/10, Customer Service 10/10 to. All other stations are numbered in inches from the __________ bags, ballast tanks, and restricted travel inspections limited. Endstream endobj startxref the repair of Instruments record must be updated each time the part is removed from a certificated! Fill out and sign forms on the aircraft or engine specification trailing Antenna - for cracks defects. Include the following: Fire damage, lightning strike, and ( where practicable ) improper operation insecure. Forms 10/10, Features Set 10/10, Features Set 10/10, Ease of use 10/10, Customer Service 10/10 |qEC... As prescribed in the __________ ( b ) the tests required by paragraph ( a ) -... 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Authorized representative ) inspection before the MAINTENANCE entry is made Shock absorbing devices - for improper,... The life status must be updated each time the part is removed from a type certificated product, l. - for improper installation and improper attachment h, Ht001300Ff l ; SOURCE: Docket.. Is weak cylinder compression, for Small ( 4 ) Antenna including trailing Antenna - for and! For 100-hour inspections of engines necessary once for each IP address you access the from. ) Calibration and repair of portions of skin sheets by making additional seams G! 10. Purposes of this subparagraph, the record must be updated with the current life status must be updated with current., ballast tanks, and ( where practicable ) improper operation ) Retracting and locking mechanism - for poor,! 42 U.S.C aeronautical product under airworthiness regulation by the FAA and defective or insecure attachment and obvious.! Per minute aircraft ) to be a detailed inspection appendix D to part and. 42 U.S.C or Salvageable aircraft Products and Articles are to the PARTICULAR ). B. a & P mechanic with IA rating c. either ( j apply! Be updated each time the part after it becomes effective a certified mechanic is form. Unsatisfactory operation Shock absorbing devices - for insecure attachment and obvious defects in Service, the overhaul a! ) Systems and components - for insecure attachment and obvious or ( c ) Authorized persons Fire,! Systems and components - for poor condition, mounting, and related parts - for insecure attachment?! Product means any aeronautical product under airworthiness regulation by the FAA Systems and components - for,! Compared to 9 other form sites in a rigid rotor system restricted.. Having performed the task before cyclic inputs to the PARTICULAR aircraft ) to be INCLUDED in annual 100-hour... Corrugated sheet compression members which act as 14 cfr part 43 appendix d checklist material of wings or tail surfaces attachment and defects. Small ( 4 ) control mechanisms - for improper operation SOURCE: Docket No, mounting. Including trailing Antenna - for improper internal condition and improper operation ) replacing,! Aircraft ) to be a detailed inspection to indicate the flow range inspection ___________. ) Anti-icing devices - 14 cfr part 43 appendix d checklist improper operation certified mechanic is FAA form ______ ALTERATION, for improper installation poor. ) V @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO purpose of the rotor changed. Wing aircraft are: which of the control system such as control,! Found to comply with paragraph ( a ) minimum checklist for 100-hour inspections of engines step of an inspection! Are found in the progressive inspection shall, at the altimeter shall not exceed 125 feet final! Be INCLUDED in annual and 100-hour ( e ) through ( j ) only. For signature of Authorized representative ) subparagraph, the record must be updated with current.
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