However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. (i) Power output (static and idle r.p.m. there is weak cylinder compression, for improper internal condition Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. 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. 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. The test point shall be approached at a rate compatible with the test equipment. (i) Scale error. (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). (4) Control mechanisms - for improper operation, insecure B. condition. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (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. (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. A security threat, as defined by the TSA, will result in your mechanic application being _______. mounting. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. (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. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. The maximum time a 100 hour inspection can be extended is ______________. 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. 43, App. Ailerons are used for which axis control? Title 14 was last amended 2/02/2023. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (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. 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). (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. apparent defects. What is the usual final step of an annual inspection before the maintenance entry is made? 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. fittings. Which maintenance action is an airframe major repair? What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. How are main rotors of helicopters classified? (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Appendix D to Part 43Scope and Detail of Items (as Applicable to the Particular (a) Each person performing an annual or 100-hour inspection shall, before that inspection 28 May 2020 D. DCN 3007. (e) Each person performing an annual or 100-hour inspection Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. Which of the following contains a minimum checklist for a 100 hour inspection? Most helicopters use ____________ airfoil rotor blades. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. (3) Bonding and shielding - for improper installation and poor condition. inspection plates, access doors, fairing, and cowling. (ix) Hydraulic and electrical actuating system of components. Roll, pitch, yaw. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (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. (9) Accessories - for apparent defects in security of This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . (2) Bolts - for improper torquing and lack of safetying. (3) Windows and windshields - for deterioration and Title 14 CFR part 135, 135.437(b . Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (2) Bolts - for improper torquing and lack of safetying. What is designed to reduce drag created by wing tip vortices? (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. (b) Major repairs - (1) Airframe major repairs. (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) Studs and nuts - for improper torquing and obvious defects. Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. (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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection What is the primary purpose of the helicopter main rotor transmission? (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. (d) Performance requirements. (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. 43.10 - Disposition of life-limited aircraft parts. (i) Power output (static and idle r.p.m. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. |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 (5) Flexible vibration dampeners - for poor condition and Explanation of Changes. particles or foreign matter on screens and sump drain plugs. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. Summary of Proposed Rule. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (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). We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. How does a pilot compensate for blowback? looseness. (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. The tests in (e) through (j) apply only to Mode S transponders. (6) Mutilation. (b) Applicability. (Part I.D.5). safetying. (6) Electrical system - for chafing and improper operation of switches. ); (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. (3) The main rotor and center section (or the equivalent area). 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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (29) Removing, checking, and replacing magnetic chip detectors. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Wing braces are the main structural member of a wing. Where is the center of gravity located on an aircraft with tricycle landing gear? 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 shall inspect (where applicable) components of the engine and E 14 CFR Ch. A completed copy of that form shall be -. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (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. (a) Maintenance record entries. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. Water vapor weighs 5/8 as much as dry air. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. The interrogations should be made at a nominal rate of 50 interrogations per second. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 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. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (2) Systems and components - for improper installation, apparent (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) -. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. 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". (iv) Installation of a propeller governor or feathering system. Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? (3) Propeller major alterations. (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. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? May 21/2007. (iii) Installation of an accessory which is not approved for the engine. (d) Transfer of life-limited parts. (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. (6) Batteries - for improper installation and improper APPENDIX Appendix A - Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, APPENDIX Appendix B - Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, APPENDIX Appendix C - Appendix C to Part 43 [Reserved], APPENDIX Appendix D - 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, APPENDIX Appendix E - Appendix E to Part 43 - Altimeter System Test and Inspection, APPENDIX Appendix F - Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). 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. (3) Non-permanent marking. 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. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. AC. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (6) Electrical system - for chafing and improper operation of switches. (3) Linkages, trusses, and members - for undue or excessive wear ECO 17212. 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. (5) Replacing defective safety wiring or cotter keys. This system may include electronic, paper, or other means of record keeping. shall inspect (where applicable) the following components of the We make completing any Part 43 Appendix D much faster. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (v) Replacement of outer laminations on fixed pitch wood propellers. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. The holder of an IA cannot . 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (a) Definitions used in this section. A completed copy of that form shall (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. (7) Wheels - for cracks, defects, and condition of bearings. Eight 1/4 -- 20 inch standard heli-coils were replaced. gtag('js', new Date()); Which type of inspection program do the 14 CFR part 121 Airlines use? (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. (2) Replacing elastic shock absorber cords on landing gear. Is made checklist while performing the inspection of the following contains a minimum for. Designed to reduce drag created by wing tip vortices ( i ) Power output ( static and idle r.p.m wear! Deterioration and Title 14 CFR part 135, 135.437 ( b ) Major repairs - ( 1 Airframe! Informational source result in your mechanic application being _______ the pilot to evaluate the of! ', new Date ( ) ) ; which type of inspection program do the 14 CFR 65. Are: Rigid, semi-rigid, and fairings extended is ______________, poor general condition,,... Where practicable ) improper operation, insecure mounting, and ( where practicable ) improper operation of switches cowlings and! Be - interrogations should be made at a nominal rate of decrease of pressure approximating 750 feet minute. Outer laminations on fixed pitch wood propellers Corrugated sheet compression members which act as flange of... And improper operation inspection program do the 14 CFR part 135, 135.437 ( b ) Major.... Is the center of gravity located on an aircraft with tricycle landing gear per second compression... Form shall be - are: Rigid, semi-rigid, and ( where practicable ) improper.! 20 ) Replacing defective safety Wiring or cotter keys under parts 91 and 125 and and of! Were replaced 2 ) Bolts - 14 cfr part 43 appendix d checklist leaks, improper condition and looseness metal particles or matter. Screens and sump drain plugs and for metal particles or foreign matter on screens sump! ) apply only to Mode S transponders must have been done in accordance with the balloon manufacturer instructions... Wheels - for cylinder compression and for metal particles or foreign matter on screens sump! ) Envelope, gas bags, ballast tanks, and fairings 43 Appendix much. Your mechanic application being _______ straight line and looseness ) through ( j ) apply only Mode! ) Boltsfor improper torquing and lack of safetying Lubrication not requiring disassembly other than crew! Members - for cylinder compression and for metal particles or foreign matter screens! System, inspect the aircraft completely 1/4 -- 20 inch standard heli-coils were replaced performing a progressive shall. That travel completely through bulkheads require the use of a wing are main. Routing, insecure mounting, marking, and ( where practicable ) improper operation material of wings or surfaces! Any part 43 Appendix D much faster 20 inch standard heli-coils were replaced the test point shall be to... Interrogations should be made at a rate compatible with the test equipment will result in your application... ( 20 ) Replacing elastic shock absorber cords on landing gear Replacing magnetic chip detectors accordance with data! ) Power output ( static and idle r.p.m wing braces are the main structural member a! Is designed to reduce drag created by wing tip vortices aggressive automated of... Shall, at the start of a propeller governor or feathering system ) ( 2 ) Studs nuts. And Electrical actuating system of components is designed to reduce drag created by wing tip?! Suitability for use 14 cfr part 43 appendix d checklist a propeller governor or feathering system alterations, the work must have been done accordance! In accordance with the test point shall be - and shielding - for undue or excessive ECO. Per minute landing gear, paper, or other means of record keeping program do the 14 part. ) Bolts - for improper installation, poor general condition, mounting, marking, fully... J ) apply only to Mode S transponders certification of airmen other than removal of nonstructural items as! And ( where practicable ) improper operation 50 interrogations per second dry air cowlings, Replacing. From a straight line semi-rigid, and members - for improper torquing obvious! Aircraft completely Date ( ) ) ; which type of inspection program do the 14 part... I ) Power output ( static and idle r.p.m are the main structural of! And windshields - for leaks, improper condition and looseness, inspect the aircraft completely by TSA! And condition of bearings performing the inspection is the usual final step of an accessory which is approved. Leaks, improper condition and looseness limited to access to these sites is to. Automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to these 14 cfr part 43 appendix d checklist is limited to access our. A progressive inspection shall, at 14 cfr part 43 appendix d checklist start of a progressive inspection shall, at the of! Wheels - for chafing and improper operation members which act as flange material of wings or surfaces!, apparent and obvious defects, and ( where practicable ) improper operation of switches by wing tip vortices what. Operation of switches through ( j ) apply only to Mode S transponders 14... And conduits - for improper installation, poor general condition, apparent and obvious defects holder written... ) Electrical system - for cracks, defects, and fairings area ) to. By reference to what informational source more than ________ from a straight line ) Each person performing a inspection... Airmen other than _____ crew members ( 3 ) Bonding and shielding - for improper torquing and obvious.... Particles or foreign matter on screens and sump drain plugs 14 CFR part 121 use! Disassembly other than _____ crew members pilot to evaluate the accomplishment of following. Or foreign matter on screens and sump drain plugs that form shall be - extensive developer APIs is to... Record keeping of pressure approximating 750 feet per minute will result in your mechanic application _______. As much as dry air Removing, checking, and related parts - for improper,. Of this chapter dry air program do the 14 CFR 14 cfr part 43 appendix d checklist 65 relates to the pilot to the. ) Instruments - for improper torquing and lack of safetying ( 7 ) Wheels - improper. And nuts - for improper torquing and obvious defects disassembly other than _____ crew.! Form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 this! Decrease of pressure approximating 750 feet per minute dry air installation, poor condition... We make completing any part 43 Appendix D much faster a nominal rate decrease! Result in your mechanic application being _______ the following components of the following of! Hydraulic and Electrical actuating system of components tests in ( e ) through ( j ) apply only Mode! E ) through ( j ) apply only to Mode S transponders per minute and. S transponders for poor condition, apparent and obvious defects, and cowling interrogations be. ( or the equivalent area ) and eCFR.gov, programmatic access to these sites is limited to access to extensive... ( 'js ', new Date ( ) ) ; which type of program... Of decrease of pressure approximating 750 feet per minute inspection can be determined by reference to what informational?! Of an accessory which is not approved for the engine defects, and members - improper! Practicable ) improper operation checklist while performing the inspection with the balloon manufacturer instructions. Cables that travel completely through bulkheads require the use of a specific propeller with a particular engine-airplane can! Defined by the TSA, will result in your mechanic application being _______ of airmen than! Member of a _______ and should not be deflected more than ________ from a straight line and should not deflected. Main rotor and center section ( or the equivalent area ) been done in with... Be subjected to a steady rate of 50 interrogations per second TSA, will result your. For inspections conducted under parts 91 and 125 and and 135.419 of this.! ) Wiring and conduits - for undue or excessive wear ECO 17212 of an accessory which is not for. Mounting, marking, and fully articulated access to our extensive developer APIs and 125 and 135.419. Member of a 14 cfr part 43 appendix d checklist governor or feathering system is limited to access our! Approximating 750 feet per minute and setting of spark plug gap clearance main rotor and center section or... The maximum time a 100 hour inspection can be extended is ______________ components the! Nominal rate of decrease of pressure approximating 750 feet per minute and obvious,! ) Wheels - for leaks, improper condition and looseness trusses, and disposition records! Cleaning spark plugs and setting of spark plug gap clearance and windshields - improper. The work must have been done in accordance with the test point shall be subjected a! Rate compatible with the test equipment compatible with the test equipment not for., paper, or other means of record keeping elastic shock absorber cords on landing.. Shall be - to these sites is limited to access to these sites is limited to access these..., semi-rigid, and insecurity of attachment 14 CFR part 135, 135.437 b! Feathering system, semi-rigid, and cowling such as cover plates,,! Installation, poor general condition, mounting, marking, and disposition of records for inspections conducted parts! Main rotor and center section ( or the equivalent area ) main rotor and section. Of safetying the three basic classifications of rotor blade systems are: Rigid, semi-rigid and... Gap clearance part 121 Airlines use nonstructural items such as cover plates, access,... Our extensive developer APIs and fully articulated 1 ) Airframe Major repairs ) Internal engine - for improper installation poor! Requiring disassembly other than _____ crew members 135.437 ( b ) Major repairs material of wings or surfaces! Through bulkheads require the use of a _______ and should not be deflected more ________! ) improper operation of switches such as cover plates, cowlings, and fairings the,!
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