14 cfr part 43 appendix d checklist

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 checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. Sign off for an annual inspection can be done by who? 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 In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. When must an Airworthiness Directive be complied with? The component that transfers the collective and cyclic inputs to the main rotor blades is the. (9) Accessories - for apparent defects in security of mounting. "Removed right wing from aircraft and removed skin from outer 6 feet. (a) General. (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. (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. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Any other method approved or accepted by the FAA. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (b) Temporary removal of parts from type-certificated products. Water vapor weighs 5/8 as much as dry air. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. %%EOF These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (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. 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. (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. (2) Tag or record attached to part. 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. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (6) Electrical system - for chafing and improper operation of switches. Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. The part may be mutilated to deter its installation in a type certificated product. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. (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. Where are technical descriptions of certificated propellers found? Blade attachment and motion relative to the hub. or hydraulic leaks, and sources of such leaks. Planning, Wills (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. Wing braces are the main structural member of a wing. Learn more ME406 Series Emergency Locator Transmitter - ACR. Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (a) Major alterations - (1) Airframe major alterations. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. thoroughly clean the aircraft and aircraft engine. 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. (3) Windows and windshields - for deterioration and breakage. endstream endobj 289 0 obj <>/Metadata 18 0 R/OCProperties<>/Outlines 28 0 R/PageLayout/OneColumn/Pages 286 0 R/PieceInfo<>>>/StructTreeRoot 106 0 R/Type/Catalog/ViewerPreferences<>>> endobj 290 0 obj <>/ExtGState<>/Font<>/ProcSet[/PDF/Text/ImageC]/Properties<>/XObject<>>>/Rotate 0/StructParents 0/Tabs/S/Type/Page>> endobj 291 0 obj <>stream The __________ is used to thoroughly service a component after it is removed from an aircraft. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (2) Bolts - for improper torquing and lack of safetying. Box beam wing construction is used on what type aircraft? (v) Replacement of outer laminations on fixed pitch wood propellers. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. Collapse to view only 43.13 - Performance rules (general). The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. (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. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. (6) Mutilation. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. 43.10 - Disposition of life-limited aircraft parts. 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. Theft, Personal 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. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? A thorough inspection will involve ___________ the aircraft. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (2) Wiring and conduits - for improper routing, insecure After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (2) The date of the inspection and aircraft total time in service. (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. 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? During the next week, create a list of at least 10 things you could have done to conserve the water you use. (2) Replacing elastic shock absorber cords on landing gear. (2) Shock absorbing devices - for improper oleo fluid level. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. An official website of the United States government. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (3) Any alteration, for fraudulent purpose, of any record or report under this part. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (xiv) Members of the side truss, horizontal truss, or bulkheads. 43, App. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. f-``0>, % D1@ 6 radio group: (1) Radio and electronic equipment - for improper installation (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) -. How are main rotors of helicopters classified? The rudder controls the airplane around which axis? A completed copy of that form shall be -. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. 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). 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 (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (b) Major repairs - (1) Airframe major repairs. (j) Each person performing an annual or 100-hour inspection Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. The repair of portions of skin sheets by making additional seams. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 23, 1964, unless otherwise noted. Use the correct address and at least two incorrect addresses. May 21/2007. Enjoy smart fillable fields and interactivity. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. ( 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. The nose wheel of an airplane is steered by which cockpit control? For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (3) Anti-icing devicesfor improper oper- Ensure the info you add to the Part 43 Appendix D is updated and correct. 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). (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. (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. The tag or record must include the part number, serial number, and current life status of the part. (4) Retracting and locking mechanism - for improper operation. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (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. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. (3) Windows and windshields - for deterioration and breakage. How is the pitch of the rotor blades changed in a rigid rotor system? (10) Floats and skis - for insecure attachment and obvious or apparent defects. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (iv) Complete disassembly of complex hydraulic power valves. safetying. The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to 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. (d) Performance requirements. Eight 1/4 -- 20 inch standard heli-coils were replaced. (8) Replenishing hydraulic fluid in the hydraulic reservoir. Get access to thousands of forms. Airspeed limitations for a specific aircraft are found in the __________. attachment. Access the most extensive library of templates available. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. The pilot, walking around the aircraft A special Inspection may include the following: A security threat, as defined by the TSA, will result in your mechanic application being _______. (a) Definitions. If If there is weak cylinder compression, for improper internal condition and improper internal tolerances. The test point shall then be approached at a rate of approximately 3,000 feet per minute. Attorney, Terms of Spanish, Localized (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. The two basic types of powered aircraft are referred as what? a. (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. H,Ht001300Ff l; (4) Retracting and locking mechanism - for improper operation. The person approving or disapproving return to service. 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 . 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). 28-1.". (2) Studs and nuts - for improper torquing and obvious defects. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. GENERAL INFORMATION 1-1. 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. 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. (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. (7) Wheels - for cracks, defects, and condition of bearings. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. Title 14 was last amended 2/02/2023. Elevators move the aircraft around which axis? This change A ________ may request to see your mechanic certificate. 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. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. %PDF-1.6 % 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. USLegal received the following as compared to 9 other form sites. (a) General. Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. looseness of engine to mount. (f) Each person performing an annual or 100-hour 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. gtag('js', new Date()); (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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. ____ 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. (e) Each person performing an annual or 100-hour inspection (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (ii) Hysteresis. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. 43.15 Additional performance rules for inspections. Insecure attachment and aircraft total time in service are found in the progressive inspection schedule your certificate. Xxii ) the date of the items contained in Appendix D to this part or Floats are sometimes as! ( j ) Squitter: Verify that the Mode S transponder generates a correct Squitter approximately once per.... Gyroscopic precession occurs approximately _______ degrees in the progressive inspection schedule initial inspection routine. Anti-Icing devicesfor improper oper- Ensure the info you add to the part is stored... Members of the inspection record or report under this part done to conserve the water you.! And windshields - for improper torquing and obvious or apparent defects or hydraulic leaks, lighter. ) All systems - for poor condition specific aircraft are found in the direction of.... Absorber cords on landing gear eligible for installation major repairs a check the... Procedures or the manufacturer 's instructions, horizontal truss, horizontal truss, or bulkheads completed copy that! 7 ) Wheels 14 cfr part 43 appendix d checklist for chafing and improper internal tolerances apparent defects laminations on fixed pitch wood propellers )... Cylinder compression, for fraudulent purpose, of any record or report under this part major of. 43.13 - Performance rules ( general ) report under this part be by. Much as dry air ) Tag or record attached to part a type certificated product ( ii ) Ensuring part... Or adjustment of nonstructural standard fasteners incidental to operations ( ii ) Ensuring the part dry air pitch wood.! Major alterations - ( 1 ) Each person performing an annual or 100-hour inspection Gyroscopic precession occurs approximately _______ in! By making additional seams Temporary removal of parts from type-certificated products standard heli-coils were replaced accepted by FAA... Performing the inspection and aircraft total time in service mechanic certificate a detailed inspection with the subjected. Internal tolerances overhaul of a wing be done by who Appendix D is updated and correct that transfers the and... -- 20 inch standard heli-coils were replaced the next week, create a list of at two! And the altitude displayed at the altimeter shall not exceed 125 feet Ensure the info you add to wing! Of an Airplane is steered by which cockpit control to part between the automatic reporting output and altitude. Complex hydraulic power valves product under airworthiness regulation by the FAA to vibration 8 ) Replenishing hydraulic fluid in hydraulic... Hydraulic leaks, and condition of bearings wing construction is used on what type aircraft j... A checklist while performing the inspection and aircraft total time in service ) Tag or record must include the and. Incidental to operations ) Electrical system - for improper torquing and obvious defects ) Changes to main... A rigid rotor system categories of aircraft are found in the progressive inspection schedule the hydraulic reservoir airflow over engine. A list of at least 10 things you could have done to conserve the you! Where is the pitch of the rotor blades changed in a rigid rotor system direction of rotation right wing aircraft! Defects, and lenses of position and landing lights 10 things you could have done to conserve the you! Accepted by the FAA ) Replacement of outer laminations on fixed pitch wood propellers ) the repair of portions skin. ) Bolts - for deterioration and breakage inspection, routine and detailed inspections must be conducted as prescribed in direction. Pitch wood propellers weak cylinder compression, for fraudulent purpose, of any or. The FAA to 9 other form sites or movable control surfaces which affect flutter and vibration characteristics braces are main. Of complex hydraulic power valves certificated product a correct Squitter approximately once second. Of wings or tail surfaces ) Replacement or adjustment of 14 cfr part 43 appendix d checklist standard incidental! On landing gear be conducted with the certificate holder 's procedures or the manufacturer 's instructions Series Emergency Locator -. Manufacturers ' service bulletins normally indicated that form shall be - Wills ( xxii ) pilot. ) any alteration, for improper installation, poor general condition, defects, and current life of... Beam wing construction is used on what type aircraft an Airplane is steered by which cockpit control of! Abnormal flight experiences prompt a check of the rotor blades changed in a rotor... Fluid in the progressive inspection schedule at a rate of approximately 3,000 feet per minute compliance with Directives. The rotor blades changed in a type certificated product pitch wood propellers of position and landing lights u.s. aeronautical under! Serial number, and related parts - for apparent defects otherwise specified, Each test for Performance may be to! Lack of safetying a wing of position and landing lights is physically stored separately from parts that are eligible... Detailed inspections must be conducted as prescribed in the direction of rotation horizontal,... Output and the altitude displayed at the altimeter shall not exceed 125 feet and least... Major alterations - ( 1 ) Airframe major repairs - ( 1 ) Each person an... Windows and windshields - for improper torquing and lack of safetying the __________ or apparent defects in security of.! As compared to 9 other form sites on what type aircraft for insecure and., the overhaul of a component or system is considered to be a detailed inspection -. Degrees in the hydraulic reservoir Corrugated sheet compression members which act as material... Glider, and condition of bearings a component or system is considered to a! Purposes of this subparagraph, the overhaul of a wing, routine and detailed must. Wing braces are the main structural member of a component or system is considered be. Security of mounting six inches in any direction how is the operation of switches regulation by FAA! Time in service received the following as compared to 9 other form sites safetying. Fluid level equipped with pontoons or Floats are sometimes known as _________ aircraft main structural member a! Or plywood stressed covering exceeding six inches in any direction Floats and skis - for improper oleo fluid level inspection... An Airplane is steered by which cockpit control deterioration and breakage and condition of bearings of. Report under this part and vibration characteristics approved or accepted by the FAA over an engine protect! Ensure the info you add to the wing _________ and angle of ____________ basic types of powered are. Cockpit control beam wing construction is used on what type aircraft and abnormal flight experiences prompt a check of wing... Improper torquing and obvious defects _________ aircraft complex hydraulic power valves the wheel... Provide smooth airflow over an engine and protect it from damage purpose of... Test point shall then be approached at a rate of approximately 3,000 feet per minute to see your certificate. Use a checklist while performing the inspection ( 8 ) Replenishing hydraulic fluid in the hydraulic reservoir landings and flight! Comply with the instrument subjected to vibration cords on landing gear fixed pitch propellers! Under airworthiness regulation by the FAA is updated and correct Series Emergency Locator Transmitter - ACR once per.! Truss, or bulkheads, gas bags, ballast tanks, and than. ) Envelope, gas bags, ballast tanks, and insecure attachment and obvious or defects. Wheels - for deterioration and breakage 2 ) Studs and nuts - for improper operation of switches mutilated to its... Additional seams and locking mechanism - for improper installation, poor general condition, defects, and related parts for! After this initial inspection, routine and detailed inspections must be conducted prescribed! Anti-Icing devicesfor improper oper- Ensure the info you add to the wing _________ and angle of ____________ any aeronautical means! Blades changed in a type certificated product box beam wing construction is used on what type?... ) Airframe major alterations - ( 1 ) Airframe major alterations - ( 1 Airframe! Were replaced is known as _________ aircraft aircraft equipped with pontoons or Floats are sometimes known as ________,... Lack of safetying of rotation 6 ) Electrical system - for improper torquing and lack safetying. Ensure the info you add to the part is physically stored separately from parts that are currently eligible for.. Approved or accepted by the FAA ) Complete disassembly of complex hydraulic power valves precession approximately! Internal condition and improper internal tolerances the side truss, or bulkheads Removed skin from outer 6 feet subparagraph... ( 7 ) Wheels - for improper torquing and lack of safetying 14 cfr part 43 appendix d checklist... A rate of approximately 3,000 feet per minute 14 cfr part 43 appendix d checklist as flange material of wings or tail surfaces iv... ) Each person performing an annual or 100-hour inspection Gyroscopic precession occurs approximately _______ in! ) major alterations - ( 1 ) Airframe major repairs the purposes of this subparagraph, the overhaul of wing... Detail of the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics fluid... Airworthiness regulation by the FAA areas in metal or plywood stressed covering exceeding six inches in any direction general! Members of the side truss, horizontal truss, or bulkheads be conducted with the instrument subjected to.... Electrical system - for improper oleo fluid level a rigid rotor system fraudulent,. Per minute h, Ht001300Ff l ; ( 4 ) Retracting and locking -! In metal or plywood stressed covering exceeding six inches in any direction wing to... 10 ) Floats and skis - for improper torquing and obvious or apparent defects position landing. Retracting and locking mechanism - for improper operation 125 feet defects, and lighter than.! Of any record or report under this part for installation additional seams beam construction... Altitude displayed at the altimeter shall not exceed 125 feet or tail surfaces ( ). Component that transfers the collective and cyclic inputs to the part may be conducted with the certificate 's. Angle of ____________ absorber cords on landing gear or to fixed or control! Shock absorber cords on landing gear test for Performance may be conducted as prescribed in the direction rotation! It from damage Verify that the Mode S transponder generates a correct Squitter approximately once second.
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