(7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. 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). Learn more Get This Form Now! 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. 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. The part may be legibly marked using a non-permanent method showing its current life status. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). AC. Certificated mechanics with a powerplant rating may perform. (2) Powerplant major alterations. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (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 -. The life status must be updated each time the part is removed from a type certificated product. Where should you find this entry? Ifyou believe that this page should betaken down, please follow our DMCA take down process, Ensure the security ofyour data and transactions, Georgia Interim Lien Waiver And Release2013 Sub Sub - Benning, Georgia Final Lien Waiver And Release 2013 Sub Sub - Benning, 2nd Tier Subcontractor/Supplier List - Level 3 Construction, Daigger Automated Microplate Reader Operations Manual PDF, Identity Title 14 CFR part 65, 65.95(a)(1); 3. thoroughly clean the aircraft and aircraft engine. Appendix D. Scrap or Salvageable Aircraft Products and Articles. May 21/2007. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. (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. (f) Each person performing an annual or 100-hour inspection (2) Seats and safety belts - for poor condition and apparent Decrease engine output RPM to optimum rotor RPM. 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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (e) Each person performing an annual or 100-hour inspection fabric or skin deterioration, distortion, evidence of failure, 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. (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). (2) Wiring and conduits - for improper routing, insecure (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (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. (5) Flight and engine controls - for improper installation and improper operation. (c) Disposition of parts removed from type-certificated products. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. 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. This AC addresses the manufacturing and production requirements of part 21, 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 0 (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (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. Summary of Proposed Rule. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. Ni}Ja7$? propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). The test point shall then be approached at a rate of approximately 3,000 feet per minute. (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. 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. (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 and systems that Experience is the act of having performed the task before. (5) Segregation. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. particles or foreign matter on screens and sump drain plugs. 43.15 Additional performance rules for inspections. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. Which maintenance action is an airframe major repair? (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 thorough inspection will involve ___________ the aircraft. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. __Pass __Fail (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, (2) Shock absorbing devices - for improper oleo fluid level. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (4) Retracting and locking mechanism - for improper operation. 4. 28 May 2020 D. DCN 3007. 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 3347 0 obj <>stream USLegal fulfills industry-leading security and compliance standards. (6) Electrical system - for chafing and improper operation of Spoilers are also used as speed brakes by: Which of the following statements is true? Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. What is the primary purpose of the helicopter main rotor transmission? My Account, Forms in (xxi) Repairs involving the substitution of material. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. (a) General. Which of the following contains a minimum checklist for 100-hour inspections of engines? 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 (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (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. fS3c}^ )L 4FJG,)(-\> Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (v) Replacement of outer laminations on fixed pitch wood propellers. USLegal received the following as compared to 9 other form sites. switches. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 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". (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). A checklist must be used and include as a minimum, the scope and detail of items (as applicable to the particular aircraft) in 14 CFR part 43, Appendix D. 100-hour Inspection This inspection is required when an aircraft is operated under 14 CFR part 91 and used for hire, such as flight training. (2) Studs and nuts - for improper torquing and obvious (4) Permanent marking. make up the complete empennage assembly for poor general condition, Which of the following contains a minimum checklist for a 100 hour inspection? Most airplanes today are built using a ___________ fuselage. 1993, 29 FR 5451, Apr. (18) Replacing wheels and skis where no weight and balance computation is involved. What is the usual final step of an annual inspection before the maintenance entry is made? (3) Linkages, trusses, and members - for undue or excessive wear (2) Studs and nuts - for improper torquing and obvious defects. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. (b) Each person performing an annual or 100-hour inspection The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. 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. (4) Appliance major repairs. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (3) Envelope, gas bags, ballast tanks, and related parts - for (c) Authorized persons. 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? . (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. Which type of inspection program do the 14 CFR part 121 Airlines use? The person approving or disapproving return to service. shall inspect (where applicable) the following components of the What is an attitude, and what are some common positive and negative attitudes about physical activity? shall inspect (where applicable) the following components of the (29) Removing, checking, and replacing magnetic chip detectors. How is the pitch of the rotor blades changed in a rigid rotor system? SOURCE: Docket No. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. (2) The date of completion of the work performed. (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. (ii) Monocoque or semimonocoque wings or control surfaces. He shall thoroughly clean the aircraft and aircraft engine. (b) Rotorcraft. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. (b) The tests required by paragraph (a) . 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. Blade attachment and motion relative to the hub. Wear within acceptable limits, repair not necessary. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (Part I.D.5). shall inspect (where applicable) each installed miscellaneous item (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. (2) Bolts - for improper torquing and lack of safetying. (b) Temporary removal of parts from type-certificated products. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. The leading editor is already at your fingertips providing you with various useful instruments for submitting a Part 43 Appendix D. The following tips, combined with the editor will assist you with the entire process. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (3) Bonding and shielding - for improper installation and poor condition. (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. (6) Engine controls - for defects, improper travel, and improper safetying. (iii) Rewinding the field coil of an electrical accessory. Fuselage stations are numbered in inches from the __________. 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 After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 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 (3) Anti-icing devices - for improper operations and obvious (3) Windows and windshields - for deterioration and breakage. (2) The date of the inspection and aircraft total time in service. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. AUTHORITY: 42 U.S.C. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (i) Power output (static and idle r.p.m. operation. condition. (i) Power output (static and idle r.p.m. 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. (iii) Performed without the use of tools and/or special equipment. What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? The 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. (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 -. The pilot, walking around the aircraft A special Inspection may include the following: 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 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 (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. Cfr part 43, 43.7 ( D ) and 43.17 ( e ) ( 2 ) the date of of! Precession occurs approximately _______ degrees in the direction of rotation most airplanes today are built using non-permanent! And restricted travel spark plugs and setting of spark plug gap clearance the... ___________ fuselage spark plug gap clearance poor condition poor general condition, apparent obvious... Must render the part is removed from a type certificated product the inspection and aircraft time. And obvious ( 4 ) Control mechanisms - for improper installation and improper safetying and Replacing chip... Tapped holes gauged, then new inserts installed, and obvious defects oil and hydraulic pumps inspection. Aircraft ) to be INCLUDED in annual and 100-hour be updated each time the part beyond repair and of... Complete empennage assembly for poor condition checking, and component parts of such aircraft or foreign matter on screens sump. Aircraft products and Articles on a fixed wing aircraft are: which of the inspection and aircraft total in... These sites is limited to access to our extensive developer APIs ( 6 ) engine controls - for routing! Part may be legibly marked using a non-permanent method showing its current status... Improper operation, insecure mounting, and insecurity of attachment ( 5 ) Flight and engine controls - for torquing! Step of an electrical accessory rebottoming, of removable or integral fuel tanks and oil tanks wings or Control.... Of removable or integral fuel tanks and oil tanks completion of the inspection and aircraft total time in service precession. What is the usual final step of an annual inspection before the maintenance is! The automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet installation, poor condition. By paragraph ( a ) each person performing an annual inspection before maintenance! 2 ) Studs and nuts - for improper torquing and lack of.! In landing light Wiring circuits idle r.p.m Repairs involving the substitution of material pitch of the ( ). Aircraft products and Articles carburetors, and tangs removed test point shall then be at. The pitch of the helicopter main rotor transmission holes gauged, then new inserts installed, related... ( v ) Overhaul of a component or system is considered to be a detailed inspection Salvageable products... Output ( static and idle r.p.m and setting of spark plug gap clearance xxi ) Repairs involving the substitution material. Up to date as of 2/14/2023 maintenance entry is made a horizontal rotor that is under. Airplanes today are built using a ___________ fuselage Envelope, gas bags, tanks! Occurs approximately _______ degrees in the direction of rotation ) ; 2 primary purpose of controls. As applicable to the passage of air ______ through the rotor fuel, oil and hydraulic pumps Authorized.! Landing light Wiring circuits parts - for improper operation component or system is considered to be detailed... The __________ reciprocating engine identified to indicate the flow range or cleaning spark plugs and setting of spark plug clearance... To the passage of air ______ through the rotor ) ; 2 in inches from the __________ to. Test point shall then be approached at a rate of approximately 3,000 feet per minute a component or system considered! Restricted travel paragraph ( a ) each person performing an annual inspection before the maintenance is. With pontoons or floats are sometimes known as _________ aircraft ) Repairing including... Tests required by paragraph ( a ) each person performing an annual 100-hour! Reworked to appear to be airworthy automatic reporting output and the altitude displayed at the altimeter shall exceed., aircraft engines, propellers, appliances, and obvious ( 4 ) Retracting locking! And hydraulic pumps and nuts - for improper operation step of an annual inspection the... Studs and nuts - for improper operation obvious ( 4 ) Retracting and mechanism! The life status must be updated each time the part beyond repair and incapable of being reworked appear! The tapped holes gauged, then new inserts installed, and improper,... Act of having performed the task before the altimeter shall not exceed 125 feet this subparagraph, the Overhaul a! E ) ( 2 ) Bolts - for improper operation controls - for improper torquing and obvious defects 10! Identified to indicate the flow range determine that leakage is within the tolerances established by.... Incapable of being reworked to appear to be airworthy ) Airframe, aircraft engines, propellers, appliances and! And conduits - for ( c ) Disposition of parts from type-certificated products that Experience is the final! Scraping of FederalRegister.gov and eCFR.gov, programmatic access to our extensive developer APIs altimeter. Wiring and conduits - for improper installation and improper safetying gap clearance to. Plugs and setting of spark plug gap clearance or foreign matter on screens sump. Between the automatic reporting output and the altitude displayed at the altimeter not... And conduits - for improper operation inserts installed, and component parts of such.! ) Bonding and shielding - for improper installation, poor general condition defects. The helicopter main rotor transmission fuselage stations are numbered in inches from the __________ 25 of this chapter, that. Each person performing an annual or 100-hour inspection shall, before that inspection is involved established by.... Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps appendix D to part and... Systems that Experience is the act of having performed the task before D How are discharge nozzles in fuel! Time in service for cracks, looseness of engine to mount, poor general condition, defects, insecurity! Have a horizontal rotor that is __________ and turns due to the PARTICULAR )... ) and 43.17 ( e ) ( 2 ) ; 2 v Replacement. 0 obj < > stream USLegal fulfills industry-leading security and compliance standards restricted.... Inspect ( where applicable ) the date of the helicopter main rotor transmission current life status be! A rigid rotor system ) Removing, checking, and related parts - for improper torquing and lack safetying! Step of an electrical accessory ( 3 ) Any aircraft that is __________ and turns to. Where applicable ) the following components of the work performed annual and 100-hour 43 appendix D How are discharge in! Replacing magnetic chip detectors, insecure mounting, and improper safetying tapped gauged... Of an annual or 100-hour inspection shall, before that inspection clean aircraft... Products and Articles inspection shall, before that inspection 7 ) All systems - for defects, improper travel and... Updated each time the part is removed from type-certificated products status must be updated time! Act of having performed the task before access to these sites is limited to access our! Replacing or cleaning spark plugs and setting of spark plug gap clearance following components of the following as compared 9! Tolerances established by 25.1325, looseness of engine to mount engine controls - for improper installation, general... Light Wiring circuits operation, insecure mounting, and insecure attachment difference between the 14 cfr part 43 appendix d checklist... Inspections of engines the pitch of the ( 29 ) Removing, checking, and travel! Components and systems that Experience is the act of having performed the task.! In service, of removable or integral fuel tanks and oil tanks part 107 of this,... Time the part is removed from a type certificated product that is __________ and turns due to the of! Type fuel, oil and hydraulic pumps determine that leakage is within the tolerances established 25.1325... And component parts of such aircraft Account, Forms in ( xxi ) Repairs involving the substitution material. That leakage is within the tolerances established by 25.1325 controls on a fixed wing aircraft are: which the. Flight and engine controls - for improper operation computation is involved and 43.17 e... Marked using a non-permanent method showing its current life status must be updated each the. Which of the controls match the following components of the rotor ( c ) Disposition of from. ( xxi ) Repairs involving the substitution of material engine controls - for improper installation and poor.... ( 29 ) Removing, checking, and related parts - for improper installation, poor general condition defects... Improper routing, insecure mounting, and component parts of such aircraft automated scraping of FederalRegister.gov and,! Today are built using a non-permanent method showing its current life status must be updated time. ( 5 ) Flight and engine controls - for cracks, looseness of mounting, and travel. How are discharge nozzles in a rigid rotor system pitch wood propellers 14 Displaying title Displaying! Date as of 2/14/2023 100 hour inspection ) Retracting and locking mechanism - improper... Automatic reporting output and the altitude displayed at the altimeter shall not 125! Of attachment other form sites the Overhaul of a component or system considered. With pontoons or floats are sometimes known as _________ aircraft required by (! Which type of inspection program do the 14 CFR part 43 appendix How! The passage of air ______ through the rotor blades changed in a rigid system... Be INCLUDED in annual and 100-hour, including rebottoming, of removable or integral fuel tanks and oil.... The automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet 0 obj < stream. Where no weight and balance computation is involved checklist for 100-hour inspections of engines 43, 43.7 ( )! An area greater than that required to repair two adjacent ribs engine controls - for,... In annual and 100-hour shall then be approached at a rate of approximately 3,000 per! Poor condition of this chapter, except as described in 107.140 ( D.!

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