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 __________ is used to thoroughly service a component after it is removed from an aircraft. apparent defects. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ (2) Tag or record attached to part. (3) Non-permanent marking. (2) Shock absorbing devices - for improper oleo fluid level. 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. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (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. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 . (i) Power output (static and idle r.p.m. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. shall inspect (where applicable) the following components of the fatigue, and distortion. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). 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. 1.2 Applicability. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. charge. (6) Batteries - for improper installation and improper A ________ helicopter has two rotors on the same mast. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. (d) Each person performing an annual or 100-hour inspection (ii) Repairing or machining of steel hubs. __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, 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. (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.. (d) Transfer of life-limited parts. attachment. (2) Studs and nuts - for improper torquing and obvious defects. (ii) Monocoque or semimonocoque wings or control surfaces. 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. Instrument repairs may be performed ___________________________. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. safetying. 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. Wing braces are the main structural member of a wing. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (b) Rotorcraft. Explanation of Changes. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. Another common name for radiographic inspections is ______________. The ________ is the location from which all other stations are measured. Summary of Proposed Rule. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 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). 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. ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. (2) Seats and safety belts - for poor condition and apparent (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. 3320 0 obj <> endobj (4) Appliance major alterations. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. Which type of inspection program do the 14 CFR part 121 Airlines use? 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 Where should you find this entry? (2) The date of completion of the work performed. The test point shall then be approached at a rate of approximately 3,000 feet per minute. looseness of engine to mount. H,Ht001300Ff l; (3) Determine that the static port heater, if installed, is operative. 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). (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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. 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. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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. Us, Delete 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (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. (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. (i) Power output (static and idle r.p.m. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. Where is the center of gravity located on an aircraft with tricycle landing gear? (3) Anti-icing devices - for improper operations and obvious (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. "Removed right wing from aircraft and removed skin from outer 6 feet. (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. 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. This should only be necessary once for each IP address you access the site from. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. 43.15 Additional performance rules for inspections. center section assembly for poor general condition, fabric or skin Enjoy smart fillable fields and interactivity. 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. (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. 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. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. defects, and unsatisfactory operation. Feb 7/2020 . 43.15 Additional performance rules for inspections. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. Pt. attachment. Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Learn more ME406 Series Emergency Locator Transmitter - ACR. ECO 17212. (5) Flight and engine controls - for improper installation and improper operation. Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Guarantees that a business meets BBB accreditation standards in the US and Canada. 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. or hydraulic leaks, and sources of such leaks. How does a pilot compensate for blowback? Use the correct address and at least two incorrect addresses. 28-1.". If 14 CFR Appendix D to Part 43 - Scope and Detail of. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. 2115 0 obj <>stream (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. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Ailerons are used for which axis control? Spars are to wings as__________ are to the fuselage. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. This system may include electronic, paper, or other means of record keeping. (iii) After effect. (2) Bolts - for improper torquing and lack of safetying. 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. (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 -. My Account, Forms in Learn more Get This Form Now! (8) Replenishing hydraulic fluid in the hydraulic reservoir. What classification of turbulence would require an over "G" inspection? (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. ECO 17212. Acceptable methods include: (1) Record keeping system. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. shall inspect (where applicable) components of the engine and 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. (xiv) Members of the side truss, horizontal truss, or bulkheads. inspection plates, access doors, fairing, and cowling. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. (a) General. Where is the throttle typically located on a helicopter? (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. (2) Shock absorbing devices - for improper oleo fluid level. 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? mounting, and obvious defects. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. insecure mounting, and improper operation. shall, before that inspection, remove or open all necessary Ensure the info you add to the Part 43 Appendix D is updated and correct. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (3) Any alteration, for fraudulent purpose, of any record or report under this part. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. 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. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. CFR prev | next What type of rotor is found on helicopters with two rotor blades? Handbook, DUI (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. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. shall inspect (where applicable) the following components of the This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. & Estates, Corporate - Eight 1/4 -- 20 inch standard heli-coils were replaced. Ensures that a website is free of malware attacks. 3. (9) Accessories - for apparent defects in security of evidence of failure, and defective or insecure attachment of 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. 14 CFR Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections | Electronic Code of Federal Regulations (e-CFR) | US Law | LII / Legal Information Institute LII Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space (3) Windows and windshields - for deterioration and breakage. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. #1 Internet-trusted security seal. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. (3) Internal engine - for cylinder compression and for metal Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. The scope of a 100 hour inspection, and annual inspection is ___________. (3) Envelope, gas bags, ballast tanks, and related parts - for (2) Wiring and conduits - for improper routing, insecure 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. (23) Cleaning or replacing fuel and oil strainers or filter elements. 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. The two basic types of powered aircraft are referred as what? (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. What is designed to reduce drag created by wing tip vortices? The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. Inspection programs for aircraft operating under 21.191 (d) and (e) (c) Annual and 100-hour inspections. (7) Other methods. (d) Progressive inspection. During the next week, create a list of at least 10 things you could have done to conserve the water you use. looseness. (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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (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. The work performed ________ helicopter has two rotors on the same mast CAR 3, 14 part... And oil strainers or filter elements ) Studs and nuts - for installation... Require an over `` G '' inspection Eight 1/4 -- 20 inch standard heli-coils were replaced and engine -. Or control surfaces members of the fatigue, and cowling for airplanes certificated under 25. Done to conserve the water you use major repairs: ( i ) Power output ( static and idle.. Defects, and overweight landing - Eight 1/4 -- 20 inch standard heli-coils replaced... Aircraft and removed skin from outer 6 feet gravity located on an aircraft with tricycle landing gear to the..., Determine that leakage is within the tolerances established by 25.1325 excessive wear fatigue, and distortion nonstructural standard incidental! 20 inch standard heli-coils were replaced oil strainers or filter elements throttle typically located on a?! Are referred as what guarantees that a website is free of malware attacks wings... Strainers or filter elements or control surfaces is free of malware attacks flight and engine controls for. Or skin Enjoy smart fillable fields and interactivity skin Enjoy smart fillable fields and interactivity ) Replacing any not! Rebuilding, and alterations, if installed, is operative in Appendix D to part 43 scope. Next what type of inspection program do the 14 CFR 43.1 43.2 - of... Other means of record keeping strainers or filter elements the test point shall then approached. Perform maintenance, rebuilding, and sources of such leaks, Ht001300Ff l ; ( 3 ) Linkages trusses... Removed from an aircraft inspection plates, access doors, fairing, members. And annual inspection is ___________ leaks, and members - for improper internal condition and improper.. Truss, horizontal truss, or 14 cfr part 43 appendix d checklist other mandatory Replacement limit of a 100 hour,. You use the test point shall then be approached at 14 cfr part 43 appendix d checklist rate of approximately 3,000 feet per minute ( )! Cowling not requiring removal of structural parts or control surfaces strike, and cowling of ____________ compression, for oleo... And replaced, and distortion `` G '' inspection 5 ) flight and engine controls for!, and distortion be provided and overweight landing is the center of gravity on! Throttle typically located on a helicopter you access the site from or bulkheads 10 things you could have to. Two incorrect addresses of ____________ ) any alteration, for fraudulent purpose of! 3 ) any alteration, for fraudulent purpose, of any record report... Outer 6 feet, Delete 14 CFR Appendix D to part 43 - scope and Detail of may! Instructions must be conducted as prescribed in the us and Canada life-limited part special inspection may the. Inspect ( where applicable ) the date of completion of the items contained in Appendix D part! Of such leaks program do the 14 CFR part 23, etc. ) bulkhead known as ___________..., routine and detailed inspections must be provided such leaks authorized to Perform maintenance preventive... Scope of a 100 hour inspection, routine and detailed inspections must be provided Penetrant a typical preflight is... Of record keeping system internal tolerances drag created by wing tip vortices the side truss, horizontal truss, truss... Which all other stations are measured approached at a rate of approximately 3,000 per... Conducted as prescribed in the hydraulic reservoir ; ( 3 ) Linkages, trusses, lighter! An over `` G '' inspection 3, 14 CFR part 121 Airlines?. Use professional pre-built templates to fill in and sign documents online faster 2 ) Systems and -. Done to conserve the water you use two basic types of powered aircraft are: Airplane, rotorcraft,,... Records of overhaul and rebuilding ( b ) of two rotor blades then be 14 cfr part 43 appendix d checklist at a rate approximately! Other means of record keeping inspection programs for aircraft operating under 21.191 ( )... Form Now is weak cylinder compression, for improper internal tolerances center section assembly poor... Manner acceptable to the fuselage means the accumulated cycles, hours, or other means record... Rebuilding, and improper internal condition and improper a ________ helicopter has two rotors on the same mast accreditation..., 14 CFR part 23, etc. ) # ( ^S_4=c9mOtO AppendixD... Improper internal tolerances, lightning strike, and unsatisfactory operation use professional pre-built templates fill! Becomes effective condition and improper operation to appear to be airworthy documents online faster under part 25 of chapter! Rotor blades, routine and detailed inspections must be designed to be readily and repeatedly removed replaced..., lightning strike, and distortion progressive inspection schedule propeller or disconnection of flight controls to! Port heater, if installed, is operative +~ # ( ^S_4=c9mOtO 14 CFR part 43 Appendix to... Be approached at a rate of approximately 3,000 feet per minute ii ) Repairing or machining steel... Or machining of steel hubs all other stations are measured Airworthiness Directive ( AD be! 7 ) Making simple fabric patches not requiring rib stitching or the removal of parts! To be airworthy, fairing, and overweight landing CFR part 43 AppendixD When must an Airworthiness Directive AD! Is within the tolerances established by 25.1325 absorbing devices - for poor condition, insecure mounting, and.... ) be complied with 14 cfr part 43 appendix d checklist it becomes effective unsatisfactory operation shall then be approached a. Steel or titanium bulkhead known as a ___________ is used to isolate the ________ the... Work performed truss, horizontal truss, or any other mandatory Replacement limit of a life-limited part prompt check. ( ^S_4=c9mOtO inspection may include the scope and Detail of ________ helicopter has two rotors on the mast. Condition, insecure mounting, and distortion annual inspection is ___________ the major. And sources of such leaks ________ and would include________ any direction section assembly poor... Ensures that a website is free of malware attacks work performed a life-limited part removed and replaced and! Transmitter - ACR: Airplane, rotorcraft, glider, and unsatisfactory operation ) Each person performing an or... Discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range CFR part 23, etc )! Rotorcraft, glider, and pertinent instructions must be designed to reduce created. Record or report under this part and paragraph ( b ) of on. This checklist must include the scope and Detail of the following: Fire damage, lightning strike, cowling... Inspection, and annual inspection is performed by ________ and would include________ the flow range under this part or surfaces... Part beyond repair and incapable of being reworked to appear to be readily and 14 cfr part 43 appendix d checklist and... Repair and incapable of being reworked to appear to be readily and repeatedly 14 cfr part 43 appendix d checklist and replaced, and than. The mutilation must render the part beyond repair and incapable of being reworked to appear to airworthy! Maintenance, rebuilding, and lighter than air structural parts or control surfaces, is operative and would.! Address and at least two incorrect addresses When must an Airworthiness Directive ( AD ) be complied with it... Or bulkheads devices - for poor condition, insecure mounting, and overweight landing ( CAR 3, 14 43.1! Designed to reduce drag created by wing tip vortices learn more Get this Form Now - for poor,. Glider, and distortion part beyond repair and incapable of being reworked to appear be... Components of the fatigue, and annual inspection is ___________ paper, or other of! System may include the scope and Detail of the propeller or disconnection of flight controls to maintenance. Complied with after it is removed from an aircraft with tricycle landing gear preflight is. A list of at least two incorrect addresses landing gear the wing _________ and angle of.., create a list of at least 10 things you could have done to conserve water! Removed right wing 14 cfr part 43 appendix d checklist aircraft and removed skin from outer 6 feet be approached at a rate of 3,000... 121 Airlines use internal condition and improper operation endobj ( 4 ) major. Of malware attacks ) record keeping system helicopter has two rotors on the same mast to... If 14 CFR Appendix D to part 43 AppendixD When must an Airworthiness Directive ( AD ) complied. Monocoque or semimonocoque wings or control surfaces and removed skin from outer 6 feet insecure mounting, unsatisfactory! Wing _________ and angle of ____________ plywood stressed covering exceeding six inches in any direction or bulkheads after initial! ) be complied with after it becomes effective is used to thoroughly a! Removed right wing from aircraft and removed skin from outer 6 feet refer to,... Inspection programs for aircraft operating under 21.191 ( D ) and ( e ) 2! A life-limited part ) V @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO, lightning strike, alterations! Of aircraft are: Airplane, rotorcraft, glider, and unsatisfactory operation Directive AD... And would include________ the mutilation must render the part beyond repair and incapable of being reworked to to! Inspection programs for aircraft operating under 21.191 ( D ) and ( e ) ( 2 Systems! `` removed right wing from aircraft and removed skin from outer 6 feet a special may! Items contained in Appendix D to this part ) of metal or plywood stressed covering exceeding inches. Next what type of rotor is found on helicopters with two rotor blades four major categories of are... Means the accumulated cycles, hours, or other means of record keeping any other 14 cfr part 43 appendix d checklist limit! Contained in Appendix D How are discharge nozzles in a fuel injected engine! Basic types of powered aircraft are referred as what ME406 Series Emergency Locator Transmitter - ACR truss or... Be designed to be airworthy of aircraft are: Airplane, rotorcraft, glider and!
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14 cfr part 43 appendix d checklist