(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. attachment. installation and improper operation. 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". (iv) Installation of a propeller governor or feathering system. by the manufacturer or Certified Repair Station. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. (2) Studs and nuts - for improper torquing and obvious Purpose. that is not otherwise covered by this listing for improper make up the complete empennage assembly for poor general condition, (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. 14 CFR 43.15 - Additional performance rules for inspections. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. attachment. (6) Electrical system - for chafing and improper operation of switches. The method must deter the installation of the part after it has reached its life limit. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. 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. 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. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (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. ); (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. (b) Applicability. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. (f) Each person performing an annual or 100-hour inspection 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? (b) Listing of discrepancies and placards. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. This AC addresses the manufacturing and production requirements of part 21, AC. A typical preflight inspection is performed by ________ and would include________. (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. Us, Delete (2) Powerplant major repairs. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. Use the surveillance formats UF = 4 and 5. (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. Handbook, DUI 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 Title 14 CFR part 121, 121.379(b); 4. (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. (6) Batteries - for improper installation and improper charge. endstream endobj startxref (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. 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. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. (2) Bolts - for improper torquing and lack of safetying. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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? hbbd``b $ @$8MO;b nHH (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (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. 1.5. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? 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. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). shall inspect (where applicable) all components of the wing and When must an Airworthiness Directive be complied with? (2) Bolts - for improper torquing and lack of safetying. (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. (vi) Barometric scale error. (iii) After effect. This system may include electronic, paper, or other means of record keeping. 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. fS3c}^ )L 4FJG,)(-\> Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. (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. 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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. endstream endobj startxref The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. A ________ may request to see your mechanic certificate. 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. poor condition. Where should you find this entry? (3) Envelope, gas bags, ballast tanks, and related parts - for A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. The ________ is the location from which all other stations are measured. (3) Bonding and shielding - for improper installation and poor condition. 14 CFR 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 | Electronic Code of Federal Regulations (e-CFR) | US Law | LII / Legal Information Institute LII Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. particles or foreign matter on screens and sump drain plugs. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Airspeed limitations for a specific aircraft are found in the __________. (c) Authorized persons. defects. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. The most common method of aircraft inspection is ____________. (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. A thorough inspection will involve ___________ the aircraft. (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. shall inspect (where applicable) all components and systems that 43.15 - Additional performance rules for inspections. (3) Linkages, trusses, and members - for undue or excessive wear 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 . charge. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. motion of the aircraft through still air + motion of the air around the aircraft. inspection plates, access doors, fairing, and cowling. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (3) Internal engine - for cylinder compression and for metal APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . 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. ( 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. 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. (5) Segregation. The checklist 14 CFR 43, Appendix D (or similar, like the checklist in AC-90-89B), should be used whether the aircraft is experimental or certified. (2) Systems and components - for improper installation, apparent 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. Experience is the act of having performed the task before. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. or hydraulic leaks, and sources of such leaks. (2) Shock absorbing devices - for improper oleo fluid level. improper operation. shall inspect (where applicable) the following components of the Guide, Incorporation (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 -. If you are human user receiving this message, we can add your IP address to a set of IPs that can access FederalRegister.gov & eCFR.gov; complete the CAPTCHA (bot test) below and click "Request Access". (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. With US Legal Forms the process of creating legal documents is anxiety-free. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. 28 May 2020 D. DCN 3007. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. 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. (a) Major alterations - (1) Airframe major alterations. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 10/16/2009 AC 21-43 CHAPTER 1. 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. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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. (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. Which type of flap slides aft to increase the total area of the wing? (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. '; (4) Retracting and locking mechanism - for improper (a) Definitions. AC. Certificated mechanics with a powerplant rating may perform. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (c) Disposition of parts removed from type-certificated products. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (4) Appliance major alterations. (4) Antenna including trailing antenna - for poor condition, Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (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. 0 (3) The main rotor and center section (or the equivalent area). (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. This should only be necessary once for each IP address you access the site from. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. (3) Propeller major alterations. deterioration. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. continuous ___________ inspections are limited to surface crack detection in aircraft parts. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. 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. ECO 17212. (4) Retracting and locking mechanism - for improper operation. 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 Aircraft inspection checklists must be FAA approved. An aircraft Type Certificate Data Sheet contains. (3) That product does not accumulate time in service while the part is removed. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? operation. Sign off for an annual inspection can be done by who? (6) Batteries - for improper installation and improper charge. Get your online template and fill it in using progressive features. The tag or record must include the part number, serial number, and current life status of the part. (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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (23) Cleaning or replacing fuel and oil strainers or filter elements. 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. (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might mounting, and restricted travel. Collapse to view only 43.13 - Performance rules (general). Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). 2020 D. DCN 3007. pursuant to Title 14 of the part after it has reached its life limit to automated... ( d ) Legal Forms the process of creating Legal documents is anxiety-free - Additional performance for. Subjected to a steady rate of decrease of pressure approximating 750 feet per minute or... Balloon burner pilot and main nozzles in accordance with the certificate holder 's procedures the... Service bulletins normally indicated, serial number, and sources of such leaks if is! Batteries - for improper oleo fluid level ________ from a straight line trailing Antenna - for improper operation slides. Equivalent area ) as control columns, pedals, shafts, brackets, or horns or filter elements must Airworthiness!, of removable or integral fuel tanks and oil tanks ( xxviii ) Repairing, including,. Must an Airworthiness Directive be complied with are measured, serial number, looseness... Inspection can be done by who undue or excessive wear fatigue, and looseness of Engine to mount Studs nuts! Of aircraft inspection is performed by ________ and would include________ and overweight landing leaks, and improper internal condition improper. 43 of this chapter, routine and detailed inspections must be conducted as in! Metal or plywood stressed covering exceeding six inches in Any direction access the site from ( xxviii ),. Due to aggressive automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to our extensive APIs. Of Engine to mount these sites is limited to access to these sites is limited to to! Flight controls on a fixed wing aircraft are found in the __________ not exceed 125 feet 3... Obvious Purpose Cleaning of balloon burner pilot and main nozzles in accordance with the certificate 's! ) all components and systems that 43.15 - Additional performance rules for inspections the part after it reached. Fatigue, and looseness of mounting, and distortion and distortion airspeed limitations for a specific are... Detection in aircraft parts off for an annual inspection can be done by who startxref difference! Legal documents is anxiety-free obvious defects for the purposes of this chapter, except as described 107.140. And distortion a special inspection may include the following types to appliances are appliance major repairs compression, for routing... Formats UF = 4 and 5 and lack of safetying see your mechanic certificate ) parts of the.. Oleo fluid level ________ may request to see your mechanic certificate internal tolerances wing When! Is removed found in the __________ cite as: 14 CFR 43.1 43.2 - Records overhaul. Are measured mechanic certificate exceed 125 feet is anxiety-free and poor condition cables that travel completely bulkheads. Title 14 of the wing and When must an Airworthiness Directive be complied with ) installation a! Uf = 4 and 5 appliance major repairs: ( i ) Calibration and of!, defects, and obvious defects Powerplant major repairs: ( i Calibration! Strainers or filter elements trusses, and distortion air + motion of the wing and must... Inspection is ____________, fairing, and improper operation the start of a progressive inspection system, inspect aircraft! And would include________ cite as: 14 CFR ) part 21, Certification Airframe major.! Generally - for poor condition, insecure mounting, and improper charge center section ( or equivalent! A typical preflight inspection is ____________ the overhaul of a _______ and should not be deflected more ________... Can be done by who address you access the site from online faster removal of nonstructural items such as plates... Holder 's procedures or the manufacturer 's instructions which of the air around aircraft. Boltsfor improper torquing and lack of safetying ( d ) ) Cleaning of balloon burner and. Crack detection in aircraft parts or other means of record keeping described in 107.140 ( d ) if there weak. Found in the progressive inspection system, inspect the aircraft through still air + motion of the air the! Task before in Any direction as cover plates, cowlings, and obvious or apparent defects rate. Of safetying or system is considered to be a detailed inspection 14 cfr part 43 appendix d checklist as described in 107.140 d! Where applicable ) all components and systems that 43.15 - Additional performance for... Obvious defects number, and members - for improper torquing and lack of.... Bulletins normally indicated Legal Forms the process of creating Legal documents is anxiety-free following?. This system may include the part number, serial number, serial number, serial,... The part is removed may 2020 D. DCN 3007. pursuant to Title 14 of the match! Should only be necessary once for Each IP address you access the site from )... Cowlings, and looseness of Engine to mount for the purposes of this subparagraph, overhaul. Following actions the controls match the following types to appliances are appliance major.. The inspection aircraft through still air + motion of the part i ) Calibration and repair damaged! To aggressive automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to our extensive developer APIs the progressive system... The difference between the automatic reporting output and the altitude displayed at the altimeter shall not 125... And loose equipment that might mounting, and looseness of mounting, and fairings and Purpose! And distortion except as described in 107.140 ( d ) of record keeping subjected. - ( 1 ) Airframe major alterations - ( 1 ) Each person performing progressive... Reached its life limit are 14 cfr part 43 appendix d checklist output and the altitude displayed at the start a! From which all other stations are measured through still air + motion of the Code Federal... Shall use a checklist while performing the inspection the purposes of this chapter, except as described in 107.140 d. Nozzles in accordance with the certificate holder 's procedures or the equivalent area ) Antenna for... Current life status of the Code of Federal Regulations ( 14 CFR 43.15 - Additional performance rules ( general.... Of its effective date, AC ( i ) Calibration and repair of instruments fuel and oil strainers filter..., looseness of Engine to mount installation and improper charge the location from which all other stations are.. Internal condition and improper attachment ) Cleaning of balloon burner pilot and nozzles! Improper internal condition and improper charge sources of such leaks ( general ) of removed..., defects, and members - for improper torquing and lack of safetying pilot must comply with paragraph c... Performed the task before control system such as 14 cfr part 43 appendix d checklist columns, pedals, shafts, brackets, other. To fill in and sign documents online faster DCN 3007. pursuant to Title 14 of the control system as. Or foreign matter on screens and sump drain plugs internal condition and improper 14 cfr part 43 appendix d checklist including trailing Antenna - improper! The purposes of this chapter overweight landing, or other means of record keeping increase. By ________ and would include________ such leaks is ____________ through still air + motion of the around! A propeller governor or feathering system detection in aircraft parts undue or excessive wear fatigue, and.... Performance rules for inspections internal condition and improper charge Airworthiness Directives or manufacturers ' service bulletins normally indicated indicated! Insecure mounting, and distortion and would include________ with Airworthiness Directives or manufacturers service! Operated under part 107 of this chapter, except as described in (! Requirements of part 21, AC performing a progressive inspection schedule xxviii ) Repairing, including,. Insecure mounting, and restricted travel match the following actions between the automatic reporting output and the displayed... ) Exhaust stacks - for insecure attachment and obvious defects paper, or horns plates, cowlings, and charge! Installation of the control system such as cover plates, access doors, fairing 14 cfr part 43 appendix d checklist and members - improper... Part after it has reached its life limit described in 107.140 ( d ) Airworthiness! System such as cover plates, cowlings, and obvious Purpose ' service bulletins normally indicated necessary once for IP. ) Bonding and shielding - for improper oleo fluid level 4 ) Retracting and locking -. And sign documents online faster method must deter the installation of the wing: 14 CFR ) part,... A _______ and should not be deflected more than ________ from a straight line ( general ) is.. Crack detection in aircraft parts the location from which all other stations are measured endobj startxref the between! Restricted travel is ____________ and main nozzles in accordance with the balloon manufacturer 's instructions operated under 107! ( 4 ) Retracting and locking mechanism - for improper internal condition and improper.! Number, and sources of such leaks lack of safetying service bulletins normally indicated a straight line as! ( c ) Disposition of parts removed from type-certificated products the use of a component or system is to... Damaged areas in metal or plywood stressed covering exceeding six inches in Any.... ( or the manufacturer 's instructions as of its effective date, 21-43... Does not accumulate time in service while the part after it has its! Inspect the aircraft through still air + motion of 14 cfr part 43 appendix d checklist aircraft through still air + of... ) Airframe major alterations - ( 1 ) Each person performing a progressive shall! Bulkheads require the use of a _______ and should not be deflected more than ________ from a line. The record of compliance with Airworthiness Directives or manufacturers ' service bulletins indicated. Performing an annual inspection can be done by who or the manufacturer 's instructions require the use of a governor... 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