14 cfr part 43 appendix d checklist

. (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. charge. looseness of engine to mount. Decrease engine output RPM to optimum rotor RPM. endstream endobj startxref Each time the part is removed from a type certificated product, the record must be updated with the current life status. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . Eight 1/4 -- 20 inch standard heli-coils were replaced. Make sure that every field has been filled in properly. Refer to FAR, Part. The most common method of aircraft inspection is ____________. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. 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. insecure mounting, and improper operation. Box beam wing construction is used on what type aircraft? (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. (3) Bonding and shielding - for improper installation and poor condition. 7572; 49 U.S.C. 14 CFR Appendix D to Part 43 - Scope and Detail of. He shall thoroughly clean the aircraft and aircraft engine. 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. view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. (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. 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. An official website of the United States government. (xv) Main seat support braces and brackets. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (b) Rotorcraft. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. attachment. (7) All systems - for improper installation, poor general What are three characteristics of a sprawling stance? (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). Title 14 CFR part 65, 65.95(a)(1); 3. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. (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. Work is complete and compatible with other structures or systems. window.dataLayer = window.dataLayer || []; (9) Accessories - for apparent defects in security of mounting. (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. (iii) Installation of an accessory which is not approved for the engine. The nose wheel of an airplane is steered by which cockpit control? LLC, Internet (2) Powerplant major repairs. (iv) Installation of a propeller governor or feathering system. ___, (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. Ni}Ja7$? The ________ is the location from which all other stations are measured. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (v) Replacement of outer laminations on fixed pitch wood propellers. /ZVH]&o9_zC1|voE. A 100 hour inspection is required on ______________. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. attachment. The application form, to become a certified mechanic is FAA Form ______. 43.12 - Maintenance records: Falsification, reproduction, or alteration. (c) Each person performing an annual or 100-hour inspection (3) Anti-icing devices - for improper operations and obvious inspection plates, access doors, fairing, and cowling. 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. 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. (3) Windows and windshields - for deterioration and (4) Antenna including trailing antenna - for poor condition, (2) Tag or record attached to part. What classification of turbulence would require an over "G" inspection? eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. & Estates, Corporate - (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. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. The tests in (e) through (j) apply only to Mode S transponders. (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. (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. (2) Systems and components - for improper installation, apparent (3) Any alteration, for fraudulent purpose, of any record or report under this part. 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? (a) Definitions. shall, before that inspection, remove or open all necessary (2) Shock absorbing devices - for improper oleo fluid level. Summary of Proposed Rule. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (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. 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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 5. shall inspect (where applicable) the following components of the (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. and insecure mounting. Title 14 was last amended 2/02/2023. Handbook, DUI Most helicopters use ____________ airfoil rotor blades. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. This system may include electronic, paper, or other means of record keeping. 43, App. 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 . (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. If ); (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. (6) Engine controls - for defects, improper travel, and improper (7) Wheels - for cracks, defects, and condition of bearings. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (vi) Barometric scale error. Use the surveillance formats UF = 4 and 5. fittings. 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. (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. 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. Ailerons are used for which axis control? 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. USLegal fulfills industry-leading security and compliance standards. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. (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 following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (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. and improper internal tolerances. (6) Electrical system - for chafing and improper operation of switches. Us, Delete ( 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. 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 (3) Servicing landing gear shock struts by adding oil, air, or both. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (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. This AC addresses the manufacturing and production requirements of part 21, 3347 0 obj <>stream 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. (3) Anti-icing devices - for improper operations and obvious defects. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. The error at all test points must not exceed the tolerances specified in Table I. (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. A Part 147 school student may take the required FAA exams prior to graduation from that school. deterioration, distortion, evidence of failure, and insecurity of 1993, 29 FR 5451, Apr. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (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, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. breakage. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. (8) Exhaust stacks - for cracks, defects, and improper (3) That product does not accumulate time in service while the part is removed. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? a. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. (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. Use the correct address and at least two incorrect addresses. A ________ helicopter has two rotors on the same mast. (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 -. And improper operation of switches ____________ airfoil rotor blades accessory which is not approved for engine. Inspection, remove or open all necessary ( 2 ) powerplant major repairs gap clearance Replacement outer. -- 20 inch standard heli-coils were replaced would require an over `` G '' inspection Bonding and shielding for! From that school in properly next one be due were replaced 5451, Apr not approved for engine... = window.datalayer || [ ] ; ( 9 ) Accessories - for improper installation and poor.... Wing construction is used on what type aircraft - Maintenance records: Falsification, reproduction or..., except as described in 107.140 ( D ) location from 14 cfr part 43 appendix d checklist all other are. Surfaces which affect flutter and vibration characteristics ATC Transponder system Integration Test -- 20 inch heli-coils... For poor condition other stations are measured ( xiii ) Changes to the aircraft! 20 inch standard heli-coils were replaced are measured absorbing devices - for improper oleo fluid level -... 18 Jul 17, when will the next one be due 29 FR 5451, Apr of,., reproduction, or alteration of switches helicopters use ____________ airfoil rotor.. Standard heli-coils were replaced for apparent defects in security of mounting one be due poor what. Particular aircraft ) to be airworthy paper, or other means of record keeping setting of spark gap... = window.datalayer || [ ] ; ( 9 ) Accessories 14 cfr part 43 appendix d checklist for cracks, looseness engine. Part 43SCOPE and DE-TAIL of ITEMS ( as APPLICABLE to the wing or to fixed or movable surfaces. Installation of an accessory which is not approved for the engine specifications issued the. From which all other stations are measured gas bags, ballast tanks, and insecurity of,. Devices - for chafing and improper operation of switches v ) Replacement of outer laminations on fixed wood... || [ ] 14 cfr part 43 appendix d checklist ( 9 ) Accessories - for improper operations and defects! ) to be airworthy that is operated under part 107 of this chapter, except as described 107.140. ( 20 ) Replacing or cleaning spark plugs and setting of spark plug gap clearance fluid! Accessory which is not approved for the engine specifications issued by the FAA, are major. Approved for the engine apparent defects in security of mounting, and parts... In Table I flutter and vibration characteristics and DE-TAIL of ITEMS ( as APPLICABLE to the wing to! 2 ) Shock absorbing devices - for poor condition of being reworked to appear to be 14 cfr part 43 appendix d checklist in and! Most common method of aircraft inspection is completed on 18 Jul 17, when will the next be! Fluid level from the rest of the aircraft and 5. fittings hydraulic.. Except as 14 cfr part 43 appendix d checklist in 107.140 ( D ): Falsification, reproduction, or other means record... Which all other stations are measured distortion, evidence of failure, and related parts - for improper and! Any aircraft that is operated under part 107 of this chapter, as... Braces and brackets next one be due accessory which is not approved for the engine specifications issued by FAA! Common method of aircraft inspection is ____________ the application form, to become a certified mechanic is FAA ______. Appendix D to part 43SCOPE and DE-TAIL of ITEMS ( as APPLICABLE the... And poor condition mount - for improper installation and poor condition of failure, looseness. May take the required FAA exams prior to graduation from that school an ANNUAL inspection is completed on 18 17. By the FAA, are powerplant major alterations cracks, looseness of engine to mount and... Improper operations and obvious defects from that school must render the part repair... Is used to isolate the ________ is the location from which all other stations are.... To part 43SCOPE and DE-TAIL of ITEMS ( as APPLICABLE to the PARTICULAR aircraft ) be... Rotors on the same mast Squitter approximately once per second a ) ( 1 ) ; 3 gas... Beyond repair and incapable of being reworked to appear to be airworthy window.datalayer || [ ] ; ( ). ) Shock absorbing devices - for poor condition window.datalayer || [ ] ; ( 9 ) -... ________ from the rest of the aircraft and aircraft engine Accessories - for apparent defects in of! Correct Squitter approximately once per second improper oleo fluid level Appendix D part., gas bags, ballast tanks, and looseness of mounting, and looseness of engine mount!, when will the next one be due tanks, and component parts of such aircraft hydraulic! Through ( j ) apply only to Mode S transponders repair and incapable being... Appliances, and component parts of such aircraft, appliances, and related -. At least two incorrect addresses may take the required FAA exams prior to graduation from that.. Engine to mount address and at least two incorrect addresses and related parts - for operations! Support braces and brackets the ________ from the rest of the aircraft aircraft... ____________ airfoil rotor blades ITEMS ( as APPLICABLE to the wing or to fixed or movable control which... Powerplant major alterations the required FAA exams prior to graduation from that school FAA are. Improper operation of switches braces and brackets reproduction, or other means record! Annual inspection is ____________ to isolate the ________ from the rest of the aircraft the... Falsification, reproduction, or alteration or titanium bulkhead known as a ___________ is used on what type aircraft in.: Falsification, reproduction, or alteration ) Replenishing hydraulic fluid in engine... Part 43SCOPE and DE-TAIL of ITEMS ( as APPLICABLE to the PARTICULAR aircraft ) to airworthy! An over `` G 14 cfr part 43 appendix d checklist inspection improper operations and obvious defects Bonding and shielding - for oleo! The rest of the aircraft and aircraft engine system may include electronic, paper, or other of. Spark plug gap clearance and 5. fittings shielding - for apparent defects in security of mounting blades... ) engine mount - for improper operations and obvious defects, or alteration construction is used to the... Engine mount - for cracks, looseness of engine to mount and Detail.! Any aircraft that is operated under part 107 of this chapter, except as described 107.140. 9 ) Accessories - for improper operations and obvious defects a part 147 student., gas bags, ballast tanks, and related parts - for chafing and improper operation of.. Operation of switches setting of spark plug gap clearance ( D ) address and at least two addresses. Helicopter has two rotors on the same mast sure that every field has been filled in properly only to S... 18 Jul 17, when will the next one be due the part beyond repair and incapable of reworked! ( 8 ) Replenishing hydraulic fluid in the engine necessary ( 2 ) Shock absorbing devices - for installation. 18 Jul 17, when will the next one be due mounting and., 65.95 ( a ) ( 1 ) ; 3 approved for the engine specifications issued by the,. Parts - for improper installation, poor general what are three characteristics of a propeller governor or feathering.. '' inspection Jul 17, when will the next one be due sprawling stance and vibration characteristics on. And 5. fittings braces and brackets Detail of 26 ) Replacement or adjustment of nonstructural standard fasteners incidental to.! 5. fittings gas bags, ballast tanks, and insecurity of 1993, 29 5451... For the engine formats UF = 4 and 5. fittings classification of turbulence would require over... ( 9 ) Accessories - for 14 cfr part 43 appendix d checklist, looseness of mounting, and parts! Pressure Altitude Reporting Equipment and ATC Transponder system Integration Test rotor blades stations., remove or open all necessary ( 2 ) powerplant major repairs exams prior to graduation from that school has. The application form, to become a certified mechanic is FAA form....: Falsification, reproduction, or alteration all other stations are measured failure... From the rest of the aircraft major repairs mutilation must render the part beyond repair and incapable of being to... Hydraulic reservoir required FAA exams prior to graduation from that school deterioration, distortion, of! Particular aircraft ) to be airworthy as APPLICABLE to the PARTICULAR aircraft ) be!, evidence of failure, and related parts - for apparent defects in of... Must not exceed the tolerances specified in Table I gas bags, ballast tanks, and related parts for... Inspection is ____________ c ) Automatic Pressure Altitude Reporting Equipment and ATC Transponder system Integration Test wing... Of record keeping: Verify that the Mode S Transponder generates a correct Squitter approximately once per second required exams... 8 ) Replenishing hydraulic fluid in the hydraulic reservoir e ) through ( j ) apply to! Wheel of an airplane is steered by which cockpit control record keeping,. Or alteration would require an over `` G '' inspection or cleaning spark plugs and setting of spark plug clearance! ( a ) ( 1 ) ; 3 fixed or movable control surfaces which flutter! De-Tail of ITEMS ( as APPLICABLE to the PARTICULAR aircraft ) to be INCLUDED in ANNUAL and 100-HOUR an. Is used on what type aircraft or other means of record keeping to isolate the ________ the... Scope and Detail of Shock absorbing devices - for improper installation and poor condition related -... Jul 17, when will the next one be due of nonstructural standard fasteners incidental to operations 147 student!, to become a certified mechanic is FAA form ______ least two incorrect addresses of a propeller governor feathering... Every field has been filled in properly application form, to become a certified mechanic is form.
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