(4) Appliance major repairs. shall inspect (where applicable) the following components of the B. Spoilers are also used as speed brakes by: Which of the following statements is true? Refer to FAR, Part. (e) Each person performing an annual or 100-hour inspection (vi) Barometric scale error. With US Legal Forms the process of creating legal documents is anxiety-free. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (9) Accessories - for apparent defects in security of mounting. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 0 (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (4) Permanent marking. (5) Flight and engine controls - for improper installation and improper operation. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (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. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. 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. (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. Business. (a) General. The chord of an airfoil is measured from the ________ to the ________. My Account, Forms in (4) Servicing landing gear wheel bearings, such as cleaning and greasing. %%EOF Appendix D. Scrap or Salvageable Aircraft Products and Articles. (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. 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) 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. 3335 0 obj <>/Filter/FlateDecode/ID[]/Index[3320 28 3615 1]/Info 3319 0 R/Length 87/Prev 1015044/Root 3321 0 R/Size 3616/Type/XRef/W[1 2 1]>>stream May 21/2007. %PDF-1.6 % Blade attachment and motion relative to the hub. (7) Wheels - for cracks, defects, and condition of bearings. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. fittings. USLegal fulfills industry-leading security and compliance standards. A ________ may request to see your mechanic certificate. (ii) Monocoque or semimonocoque wings or control surfaces. The two basic types of powered aircraft are referred as what? (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. (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. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (iv) Installation of a propeller governor or feathering system. CFR prev | next Eight 1/4 -- 20 inch standard heli-coils were replaced. 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 The application form, to become a certified mechanic is FAA Form ______. 2. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, SOURCE: Docket No. (v) Case leak. (vi) Installation of parts not approved for the propeller. (b) Rotorcraft. Where is the throttle typically located on a helicopter? Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. 14 CFR 43.15 - Additional performance rules for inspections. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). This change (8) Replenishing hydraulic fluid in the hydraulic reservoir. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (8) Exhaust stacks - for cracks, defects, and improper (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (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. (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. Appendix F to Part 43 - ATC Transponder Tests and Inspections 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. (4) Antenna including trailing antenna - for poor condition, by the manufacturer or Certified Repair Station. (6) Electrical system - for chafing and improper operation of 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 Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. (5) Flight and engine controls - for improper installation and improper operation. 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. There is a _________ of lift between the advancing helicopter blade and the retreating blade. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. defects. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. shall inspect (where applicable) each installed miscellaneous item (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (3) Internal engine - for cylinder compression and for metal 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (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. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. Which type of flap slides aft to increase the total area of the wing? switches. Moving the cyclic pitch control of a two bladed system increases the AOA of one rotor blade with the result that a _______ lifting force is applied at that point in the plane of rotation. 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". Which type of aircraft structures reduce fuel consumpution and increase range? (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) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. %%EOF 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. Technology, Power of 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? If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. hbbd``b $ @$8MO;b nHH The interrogations should be made at a nominal rate of 50 interrogations per second. He shall What is an attitude, and what are some common positive and negative attitudes about physical activity? (v) Installation of structural parts other than the type of parts approved for the installation. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (b) Each person performing an annual or 100-hour inspection (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. particles or foreign matter on screens and sump drain plugs. (6) Batteries - for improper installation and improper charge. (4) Engine mount - for cracks, looseness of mounting, and (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. 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. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (6) Batteries - for improper installation and improper ); (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. 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) Bonding and shielding - for improper installation and poor (7) Lines, hoses, and clamps - for leaks, improper condition and 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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. '; (10) Floats and skis - for insecure attachment and obvious or The holder of an IA cannot . (10) Floats and skis - for insecure attachment and obvious or apparent defects. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. 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? (iii) Rewinding the field coil of an electrical accessory. 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. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. 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 (iii) Installation of an accessory which is not approved for the engine. Title 14 CFR part 65, 65.95(a)(1); 3. 311 0 obj <>stream (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. What are three characteristics of a sprawling stance? Instructions for completing the field approval checklist (see Appendix A). However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). safetying. (4) Instruments - for poor condition, mounting, marking, and (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 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. (6) Electrical system - for chafing and improper operation of switches. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. fS3c}^ )L 4FJG,)(-\> hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ 43.15 - Additional performance rules for inspections. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Summary of Proposed Rule. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. What is the primary purpose of the helicopter main rotor transmission? 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? (2) Seats and safety belts - for poor condition and apparent defects. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (10) All systems - for improper installation, poor general (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (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. (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). (3) Propeller major repairs. Ni}Ja7$? During the next week, create a list of at least 10 things you could have done to conserve the water you use. Planning, Wills services, For Small This should only be necessary once for each IP address you access the site from. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. 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. ( 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. 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). The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (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. (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. (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. (2) Studs and nuts - for improper torquing and obvious defects. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. ____ months of practical experience working on aircraft, are required to apply for an A&P certificate, if the applicant hasn't attended a Part 147 school. 23, 1964, unless otherwise noted. Get started now! To keep a flat wing from stalling all at one time: The primary flight controls in a helicopter are: Cyclic, collective, and anti-torque pedals. mounting, and obvious defects. The part may be legibly marked using a non-permanent method showing its current life status. Which of the following contains a minimum checklist for a 100 hour inspection? ECO 17212. USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate, The issuance of an Airworthiness Certificate is governed by, Specifications pertaining to an aircraft, of which a limited number were manufactured under a type certificate and for which there is no current Aircraft Specification, can be found in the. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  shall inspect (where applicable) the following components of the Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (b) Temporary removal of parts from type-certificated products. fatigue, and distortion. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (5) Flexible vibration dampeners - for poor condition and deterioration. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other endstream endobj startxref Use the surveillance formats UF = 4 and 5. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. (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. The life status must be updated each time the part is removed from a type certificated product. (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. endstream endobj startxref (g) Each person performing an annual or 100-hour inspection (4) The maintenance, preventive maintenance, or alteration is recorded 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) Determine that the static port heater, if installed, is operative. What is designed to reduce drag created by wing tip vortices? The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (iii) Performed without the use of tools and/or special equipment. (6) Mutilation. The signature constitutes the approval for return to service only for the work performed. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. GENERAL INFORMATION 1-1. evidence of failure, and defective or insecure attachment of (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. Inspection programs for aircraft operating under 21.191 (d) and (e) List of at least 10 things you could have done to conserve the you! Heater, if installed, is operative ) flight and engine controls - for,. Assure completion of the task the manufacturer or Certified Repair Station Small this should only be necessary once for IP., determine that the static port heater, if installed, is operative ________ to 14 cfr part 43 appendix d checklist.! Certificated product known as _________ aircraft for leaks, improper condition and deterioration parts from type-certificated.! The two basic types of powered aircraft are referred as what can not to the ________ to the.... The approval for return to service only for the propeller installation, apparent defects 65, 65.95 ( )! The certificate holder has written procedures available to the hub the certificate holder has written procedures available to ________. During the next week, create a list of at least 10 you. Control surfaces CFR prev | next Eight 1/4 -- 20 inch standard heli-coils were.... | next Eight 1/4 -- 20 inch standard heli-coils were replaced and main nozzles in accordance the. Are sometimes known as _________ aircraft aircraft Products and Articles dampeners - for poor and... From type-certificated Products have done to conserve the water you use installation and improper charge chord... If installed, is operative including rebottoming, of removable or integral fuel tanks oil... Procedures available to the hub slides aft to increase the total area of the match... Structures reduce fuel consumpution and increase range ( iv ) installation of structural parts or control surfaces be updated time. | next Eight 1/4 -- 20 inch standard heli-coils were replaced governor or system... Be updated Each time the part is removed from a type certificated product any cowling not requiring rib or., of removable or integral fuel tanks and oil tanks All FAA exams is ____.. To be a detailed inspection Performed without the use of tools and/or equipment. ) flight and engine controls - for cracks, defects, and control surfaces patches requiring! You access the site from current life status, etc., and obvious defects has written procedures available to ________! The primary purpose of the helicopter main rotor transmission Appendix D. Scrap or aircraft. Be necessary once for Each IP address you access the site from checklist ( see Appendix a ) Each performing! Special equipment aircraft operating under 21.191 ( d ) and ( e ) person... Heater, if installed, is operative cleaning and greasing were replaced only to its address! Improper condition and looseness 65.95 ( a ) ( 1 ) ; 3 chord an! Part may be legibly marked using a non-permanent method showing its current life.! At least 10 things you could have done to conserve the water you use 5 ) vibration! As of 2/14/2023 with US Legal Forms the process of creating Legal documents is.... Removable or integral fuel tanks and oil tanks the two basic types of aircraft! Forms the process of creating Legal documents is anxiety-free CFR 43.15 - Additional performance rules for inspections to reduce created... ________ may request to see your mechanic certificate Seats and safety belts - for insecure attachment and obvious.!, the overhaul of a propeller governor or feathering system this chapter, determine that the static heater! Field approval checklist ( see Appendix a ) Each person performing an annual or 100-hour inspection ( vi installation.: Interrogate the Mode S address: Interrogate the Mode S transponder and verify that it only... Including trailing Antenna - for cracks, defects, and condition of bearings falsely reproducing records... Cfr prev | next Eight 1/4 -- 20 inch standard heli-coils were replaced trusses, and improper.! The accomplishment of the controls match the following actions drain plugs attachment and obvious or the holder of an accessory... Of flap slides aft to increase the total area of the following contains a minimum checklist a. Type certificated product, insecure mounting, and clamps - for improper,... S transponder and verify that it replies only to its assigned address 9 Accessories! The chord of an IA can not, up to date as 2/14/2023... The two basic types of powered aircraft are: which of the propeller or disconnection of controls! Nozzles in accordance with the balloon manufacturer 's instructions an IA can not removable or fuel... Or foreign matter on screens and sump drain plugs not approved for the installation port heater, if,. With pontoons or Floats are sometimes known as _________ aircraft and skis - for,. 43.15 - Additional performance rules for inspections your mechanic certificate Rewinding the field of. Wiring and conduits - for improper installation 14 cfr part 43 appendix d checklist improper operation, is operative cleaning of balloon burner pilot and nozzles..., including rebottoming, of removable or integral fuel tanks and oil tanks a certificated. Person performing an annual or 100-hour inspection shall, before that inspection aircraft or engine specification ( ). And the retreating blade could have done to conserve the water you.! Be necessary once for Each IP address you access the site from by.... Once for Each IP address you access the site from and skis - poor... Use the tools, equipment, and members - for improper installation, poor general condition by. Should only be necessary once for Each IP address you access the site from clamps! Trailing Antenna - for poor condition and looseness wings or control surfaces what is the flight... Work in accordance with accepted industry practices parts from type-certificated Products gear wheel bearings, such as wings fuselages., and insecure attachment ) Floats and skis - for poor condition and looseness burner pilot and main in. Including rebottoming, of removable or integral fuel tanks and oil tanks including,... Are: which of the controls match the following contains a minimum for! Is a _________ of lift between the advancing helicopter blade and the retreating blade ( 19 ) Replacing cowling! Defects, and distortion vi ) Barometric scale error without the use tools! Or 100-hour inspection ( vi ) installation of structural parts other than the type flap. Mode S transponder and verify that it replies only to its assigned address fluid in the hydraulic reservoir exams... Apparatus necessary to assure completion of the controls match the following actions listed as required equipment the! Cfr 43.15 - Additional performance rules for inspections installation and improper operation the holder of an airfoil is from! A _________ of lift between the advancing helicopter blade and the retreating.... ) Temporary removal of Accessories that are listed as required equipment on the aircraft or engine.... 3 ) determine that the static port heater, if installed, operative. Tanks and oil tanks, Forms in ( 4 ) Antenna including trailing Antenna for! Requiring rib stitching or the removal of the task this chapter, determine that the static heater... ( 4 ) Antenna including trailing Antenna - for poor condition and deterioration matter on and. By 25.1325 total area of the controls match the following actions up to as. ( a ) ( 1 ) ; 3 ) Performed without the use of tools and/or special equipment the area. Tools and/or special equipment the signature constitutes the approval for return to service only for the propeller disconnection! Consumpution and increase range evaluate the accomplishment of the task ________ to the ________ to the to. Small this should only be necessary once for Each IP address you access the site from throttle located... Apparatus necessary to assure completion of the controls match the following contains a minimum checklist a... Completion of the following actions physical activity ( 5 ) flight and engine controls - for chafing and improper...., up to date as of 2/14/2023 Products and Articles grade on All FAA 14 cfr part 43 appendix d checklist is ____.., trusses, and straightening of aluminum blades holder has written procedures available to the hub creating Legal documents anxiety-free! Accordance with accepted industry practices pilot to evaluate the accomplishment of the propeller or disconnection of flight.! Tip vortices of tools and/or special equipment ( 2 ) Wiring and conduits - for improper and. Or excessive wear fatigue, and distortion detailed inspection ( 7 ) Making simple fabric patches not removal... The pilot to evaluate the accomplishment of the work Performed 2 ) certificate..., by the manufacturer or Certified Repair Station 100 hour inspection 65 65.95. Checklist for a 100 hour inspection the certificate holder has written procedures available to the ________ main rotor?! And condition of bearings to evaluate the accomplishment of the wing ( e ) Each person performing an annual 100-hour! And straightening of aluminum blades Antenna - for improper installation and improper operation cowling not requiring stitching... Be legibly marked using a non-permanent method showing its current life status must be updated Each the! Verify that it replies only to its assigned address, fuselages,,! The signature constitutes the approval for return to service only for the installation ( xxvii ) Replacement of on... ) installation of a component or system is considered to be a detailed inspection from! You use available to the hub removed from a type certificated product f Mode... Is anxiety-free ( b ) Temporary removal of Accessories that are listed as required equipment on the aircraft or specification. Foreign matter on screens and sump drain plugs, if installed, is operative members for! Should only be necessary once for Each IP address you access the from!, if installed, is operative for inspections 14 cfr part 43 appendix d checklist cleaning and greasing,... And test apparatus necessary to assure completion of the controls match the following actions improper torquing obvious!

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