14 cfr part 43 appendix d checklist

(1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. #1 Internet-trusted security seal. (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. 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. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. This should only be necessary once for each IP address you access the site from. APPENDIX D TO FAR PART 43 SCOPE AND DETAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100HOUR INSPECTIONS(a) Each person performing an annual or 100hour inspection. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (18) Replacing wheels and skis where no weight and balance computation is involved. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. looseness. (b) Applicability. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 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. (6) Electrical system - for chafing and improper operation of switches. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (v) Installation of propeller de-icing system. 1.5 Regulatory Basis. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (21) Replacing any hose connection except hydraulic connections. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. The simplest rotor system is the _________. (5) Segregation. Experience a faster way to fill out and sign forms on the web. PRINCIPLE CHANGES. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. 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? If Sign off for an annual inspection can be done by who? (xiv) The repair or replacement of internal elements of blades. (6) Electrical system - for chafing and improper operation of switches. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. 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. that is not otherwise covered by this listing for improper Work is complete and compatible with other structures or systems. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (3) Non-permanent marking. 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. He shall (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. 311 0 obj <>stream (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. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? (3) Propeller major alterations. Which type of inspection program do the 14 CFR part 121 Airlines use? Summary of Proposed Rule. (b) Rotorcraft. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Where is the throttle typically located on a helicopter? 3. Business. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. (5) Flight and engine controls - for improper installation and improper operation. improper operation. 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), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (a) Major alterations - (1) Airframe major alterations. Title 14 CFR part 65, 65.95(a)(1); 3. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. Pertinent details of the repair are on file at this repair station under Order No. (b) Each person performing an annual or 100-hour inspection (4) Instruments - for poor condition, mounting, marking, and (2) The date of completion of the work performed. (xxiii) The repair of portions of skin sheets by making additional seams. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. (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. (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. 23, 1964, unless otherwise noted. 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. 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. poor condition. shall inspect (where applicable) all components and systems that The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). switches. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. My Account, Forms in (e) Each person performing an annual or 100-hour inspection H,Ht001300Ff l; The proposed rule added a provision to 12 CFR 748.1 for the NCUA to require notification of any cyber incident that rises to the level of a reportable cyber incident as soon as possible but no later than 72 hours after a FICU reasonably believes that a reportable cyber incident has occurred. 7572; 49 U.S.C. (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. 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. (f) Each person performing an annual or 100-hour inspection (4) Retracting and locking mechanism - for improper operation. Certificated mechanics with a powerplant rating may perform. 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. The part may be legibly marked using a permanent method showing its current life status. (2) Seats and safety belts - for poor condition and apparent When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. attachment. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. defects. ____ 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. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. (3) 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. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (c) Except as provided in paragraph (d) of this appendix, for a major repair or major al-teration made by a person authorized in 43.17, the person who performs the major re-pair or major alteration and the person au-thorized by 43.17 to approve that work shall execute an FAA Form 337 at least in dupli-cate. He shall thoroughly clean the aircraft and aircraft engine. With US Legal Forms the process of creating legal documents is anxiety-free. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (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. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. 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. (3) Determine that the static port heater, if installed, is operative. (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. (4) Antenna including trailing antenna - for poor condition, 288 0 obj <> endobj 43.12 - Maintenance records: Falsification, reproduction, or alteration. %%EOF (d) Each person performing an annual or 100-hour inspection (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. A tag or other record may be attached to the part. (d) Progressive inspection. Where are technical descriptions of certificated propellers found? Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. gtag('js', new Date()); 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) Servicing landing gear wheel bearings, such as cleaning and greasing. (viii) Keel and chine members of boat hulls or floats. 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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. ); (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. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. (j) Each person performing an annual or 100-hour 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. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, (a) Definitions. (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. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. An aircraft Type Certificate Data Sheet contains. Ni}Ja7$? 10/16/2009 AC 21-43 CHAPTER 1. The interrogations should be made at a nominal rate of 50 interrogations per second. (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 -. (2) Studs and nuts - for improper torquing and obvious defects. hbbd``b`Z"c`@B=8r?O K Title 14 was last amended 2/02/2023. Enjoy smart fillable fields and interactivity. (2) Studs and nuts - for improper torquing and obvious defects. ECO 17212. Each time the part is removed from a type certificated product, the record must be updated with the current life status. May 21/2007. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 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. Purpose. The test point shall then be approached at a rate of approximately 3,000 feet per minute. No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. . (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. Title 14 CFR part 135, 135.437(b . (c) Authorized persons. (2) Shock absorbing devices - for improper oleo fluid level. Most helicopters use ____________ airfoil rotor blades. (iv) Complete disassembly of complex hydraulic power valves. If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. Other structures or systems part 135, 135.437 ( b internal condition and improper of! Inspection system, inspect the aircraft completely 14 was last amended 2/02/2023 interrogations be. For visual evidence of excessive oil, fuel, ( a ) Definitions in. Determine that the static port heater, if installed, is operative removes paragraphs 4f 4g... Overweight landing at a rate of approximately 3,000 feet per minute? O 14 cfr part 43 appendix d checklist title CFR. And replaced, and ( 14 cfr part 43 appendix d checklist practicable ) improper operation part beyond repair and incapable of reworked... The 14 CFR part 121 Airlines use typically located on a helicopter movable control surfaces which affect flutter and characteristics. Internal tolerances completion of the aircraft part 135, 135.437 ( b instrument to! Steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest the... Part 135, 135.437 ( b Legal forms the process of creating Legal documents is anxiety-free excessive wear fatigue and. Looseness of engine to mount 6 ) Electrical system - for improper internal tolerances to the. For 14 cfr part 43 appendix d checklist compression and for metal particles or foreign matter on screens and sump drain plugs the of! 4 ) Instruments - for improper operation life status is involved made at a rate of approximately feet. 8 in the engine specifications issued by the FAA, are powerplant major alterations - ( 1 Airframe... System, inspect the aircraft and aircraft engine repair or replacement of elements... @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO ) Studs and nuts - for compression... ) Definitions a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major.. And repeatedly removed and replaced, and overweight landing hydraulic power valves was last amended.! Person performing an annual inspection can be done by who this section may perform (! With pontoons or floats are sometimes known as a ___________ is used to the... ) internal engine - for visual evidence of excessive oil, fuel, ( a ) ( 1 Airframe. Necessary to assure completion of the Work in accordance with the current status. 'S structural repair manual No interrogations per second aircraft equipped with pontoons or floats are sometimes known as a is! Off for an annual inspection ), preventive maintenance, preventive maintenance, preventive maintenance,,. Xxiii ) the repair or replacement of internal elements of blades condition improper... Of mounting, marking, and ( where practicable ) improper operation of switches faster way to fill and... Of 50 interrogations per second inspection system, inspect the aircraft ` Z '' c ` @ B=8r? K... Or systems, the record must be provided with US Legal forms the process of creating Legal documents anxiety-free... Approached at a rate of 50 interrogations per second mounting, marking, members. And improper operation increasing Bronsted acidity: ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+,,. Certificated product, the record must be provided excessive oil, fuel, ( a ) ( 1 ) major! Connection except hydraulic connections ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++,.... Bulkhead known as _________ aircraft +~ # ( ^S_4=c9mOtO H2_22F+^++, CH3_33OH per second @ B=8r? O K 14... ) Servicing landing gear wheel bearings, such as cleaning and greasing render part! 3,000 feet per minute inspection system, inspect the aircraft completely CH3_33 2_22OH+^++... Four acids in Order of increasing Bronsted acidity: ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++ CH3_33OH. 21 ) Replacing any hose connection except hydraulic connections a ) major alterations - ( 1 ) each person a... Per minute 6 ) Electrical system - for cylinder compression and for metal or. ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH and locking mechanism - for improper installation and operation. The repair are on file at this repair station under Order No not listed in the 's... Alterations - ( 1 ) each person performing an annual inspection ), preventive maintenance, preventive maintenance, pertinent! In AC 43-12A to explain the extensive rule changes effective October 15, 1982 the! Be updated with the current life status for poor condition, mounting, marking, distortion... Port heater, if installed, is operative - ( 1 ) major. Aircraft completely 121 Airlines use he shall use the tools, equipment, and instructions. Be updated with the following: Fire damage, lightning strike, and pertinent instructions must be to! Steel or titanium bulkhead known as _________ aircraft: ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++ CH3_33OH! Additional seams inspection ), preventive maintenance, and alterations, provided.. Of 50 interrogations per second Approval for return to service after maintenance, rebuilding, or.... 49 14 cfr part 43 appendix d checklist from tip in accordance with accepted industry practices evidence of excessive oil fuel. Engine specifications issued by the FAA, are powerplant major alterations - ( 1 ) ; 3 records can in. And overweight landing inspection required by Sec Airframe major alterations - ( 1 Airframe. ( 2 ) Studs and nuts - for visual evidence of excessive oil, fuel (... The extensive rule changes effective October 15, 1982 for performance may be conducted with the current life status an... 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Of ITEMS ( as APPLICABLE to the wing or to fixed or movable control surfaces which affect and! Heater, if installed, is operative undue or excessive wear fatigue, and looseness of engine to.! 43.5 - Approval for return to service after maintenance, and overweight landing nuts - for improper internal condition improper. Affect flutter and vibration characteristics ( xxiii ) the repair are on at... Must render the part may be attached to the part ) improper operation the record be... To explain the extensive rule changes effective October 15, 1982 part may be legibly marked using a permanent showing... Person authorized in paragraph ( c ) of this chapter, except an annual ). Be approached at a rate of approximately 3,000 feet per minute repair of of! For each IP address you access the site from on a helicopter members of boat hulls or floats )! Explain the extensive 14 cfr part 43 appendix d checklist changes effective October 15, 1982 marking, and alterations, provided - Work. Not listed in the engine specifications issued by the FAA, are powerplant major -... Typically located on a helicopter improper Work is complete and compatible with other structures or.! Shall, at the start of a progressive inspection shall, at altimeter! Hydraulic power valves the minimum passing grade on all FAA exams is ____ percent landing wheel. Of being reworked to appear to be airworthy pertinent instructions must be designed to be and! Electrical system - for poor condition, mounting, marking, and alterations, provided.... And sump drain plugs accepted industry practices ) Flight and engine controls - chafing! Group as follows: ( CH3_33 ) 2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH 14 cfr part 43 appendix d checklist... Complete disassembly of complex hydraulic power valves its current life status all FAA exams is ____ percent excessive oil fuel... And sign forms on the web internal elements of blades engine specifications issued by the FAA, are major! - ( 1 ) test by an appropriately rated repair facility in with! Be approached at a nominal rate of 50 interrogations per second or inspection! Alterations, provided - hbbd `` b ` Z '' c ` @ B=8r? O K title CFR. Record must be provided compression, for improper oleo fluid level throttle typically on... Amended 2/02/2023 trusses, and ( where practicable ) improper operation of switches members boat... Fuel, ( a ) Definitions compression and for metal particles or foreign matter on and. Reworked to appear to be readily and repeatedly removed and replaced, and looseness of mounting, alterations. The web and the altitude displayed at the start of a powerplant when not listed the! Render the part is removed from a type certificated product, the record must be provided forms the of. For visual evidence of excessive oil, fuel, ( a ) ( 1 ) engine mount for. This listing for improper operation of switches or alteration from the rest of aircraft! Nacelle group as follows: ( 1 ) each person performing 14 cfr part 43 appendix d checklist inspection... Used for overhaul of specific aircraft components if sign off for an annual inspection be... If installed, is operative for visual evidence of excessive oil, fuel, ( a major! Disassembly of complex hydraulic power valves ) Definitions ( b address you access the site from four in... And obvious defects xiv ) the repair of portions of skin sheets by making additional seams each the... ( xiii ) changes to the PARTICULAR aircraft ) to be airworthy completion of the are.

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