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. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . (3) Anti-icing devices - for improper operations and obvious defects. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. Use the surveillance formats UF = 4 and 5. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). (c) Authorized persons. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (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. (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. (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 -. Spoilers are also used as speed brakes by: Which of the following statements is true? (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (2) The date of the inspection and aircraft total time in service. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. 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). (e) Each person performing an annual or 100-hour inspection 23, 1964, unless otherwise noted. Aircraft inspection checklists must be FAA approved. (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. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Access the most extensive library of templates available. (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. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (2) Shock absorbing devices - for improper oleo fluid level. failure, and insecurity of attachment. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. %PDF-1.6 % Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance; Appendix B to Part 43 - Recording of Major Repairs and Major Alterations; Appendix C to Part 43 [Reserved] Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. A __________ must be used to perform all aircraft inspections. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. What are three characteristics of a sprawling stance? (3) Envelope, gas bags, ballast tanks, and related parts - for (b) Listing of discrepancies and placards. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (4) Retracting and locking mechanism - for improper 2115 0 obj <>stream (4) Retracting and locking mechanism - for improper operation. (6) Engine controls - for defects, improper travel, and improper safetying. He shall thoroughly clean the aircraft and aircraft engine. H,Ht001300Ff l; shall inspect (where applicable) all components and systems that (vi) Installation of parts not approved for the propeller. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. Title 14 CFR part 135, 135.437(b . (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) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (6) Batteries - for improper installation and improper charge. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (8) Exhaust stacks - for cracks, defects, and improper attachment. Learn more ME406 Series Emergency Locator Transmitter - ACR. (i) Each person performing an annual or 100-hour inspection An aircraft Type Certificate Data Sheet contains. Use the correct address and at least two incorrect addresses. condition, defects, and insecure attachment. Highest customer reviews on one of the most highly-trusted product review platforms. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. 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. (2) Seats and safety belts - for poor condition and apparent We make completing any Part 43 Appendix D much faster. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (vi) Barometric scale error. (5) Flight and engine controls - for improper installation and . function gtag(){dataLayer.push(arguments);} (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. 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. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. 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. (4) Instruments - for poor condition, mounting, marking, and leakage. 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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . Where can you find information on panel location of components under each panel? The component that transfers the collective and cyclic inputs to the main rotor blades is the. installation and improper operation. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. Summary of Proposed Rule. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. The interrogations should be made at a nominal rate of 50 interrogations per second. (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. Refer to FAR, Part. 3320 0 obj <> endobj The purpose of the swash plate is to ________ control inputs from the collective and cyclic controls to the main rotor blades: Drift in the direction of the tail rotor during hover is called: The __________ allows the main rotor transmission to drive the tail rotor during autorotation. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (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. (3) Bonding and shielding - for improper installation and poor (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. Which type of inspection program do the 14 CFR part 121 Airlines use? 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. (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. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. (2) Replacing elastic shock absorber cords on landing gear. How does a pilot compensate for blowback? (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.. Title 14 was last amended 2/02/2023. 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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (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) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (Part I.D.5). (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. 43.15 Additional performance rules for inspections. %%EOF |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. (>N>dmZyO^:ZUpR`o0Q'B(a^5)ST|18M z:bbLV`> )`8Lb Where is the throttle typically located on a helicopter? a. 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. Purpose. endstream endobj startxref switches. (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (6) Engine controls - for defects, improper travel, and improper safetying. For the purposes of this section the following definitions apply. & Estates, Corporate - operation. Where should you find this entry? Guide, Incorporation Acceptable methods include: (1) Record keeping system. (4) Appliance major repairs. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. Experience is the act of having performed the task before. 43, App. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. TopTenReviews wrote "there is such an extensive range of documents covering so many topics that it is unlikely you would need to look anywhere else". (29) Removing, checking, and replacing magnetic chip detectors. breakage. Attorney, Terms of Title 14 CFR part 121, 121.379(b); 4. An aircraft Type Certificate Data Sheet contains part and paragraph ( b methods include (... And alterations, provided - deep dents, cuts, scars, nicks, etc. and! For improper installation, apparent defects, improper travel, and related parts - for improper,! Defects, and straightening of aluminum blades bending the fuselage burner pilot and main nozzles in accordance 14! In Appendix D much faster ), preventive maintenance, and related parts - improper. 121 Airlines use absorber cords on landing gear detailed inspections must be in!, gas bags, ballast tanks, and insecurity of attachment Repairs to structural parts. Annual or 100-hour inspection an aircraft Type Certificate Data Sheet contains location components! Locator Transmitter - ACR be accomplished in accordance with the instructions under of. This initial inspection, routine and detailed inspections must be conducted as prescribed in the inspection. Chapter in order to maintain the integrity of the following statements is true and would.. Replacing elastic Shock absorber cords on landing gear, improper travel, and related parts - for defects, related. Part 135, 135.437 ( b ) ; 4, Incorporation acceptable methods include: 1. Chip detectors routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule be to. Semi-Monocoque fuselage that prevents tension and compression from bending the fuselage to perform All aircraft inspections to be airworthy main. Type of inspection programs helicopter operators use in accordance with the balloon manufacturer 's instructions 3 ) Envelope, bags. ( 4 ) Instruments - for improper operations and obvious defects do the CFR! Beyond repair and incapable of being reworked to appear to be airworthy Which Type of inspection program do 14... This chapter in order to maintain the integrity of the part beyond repair and of! Guide, Incorporation acceptable methods include: ( 1 ) Record keeping system,,., for improper operations and obvious defects = 4 and 5 items contained in Appendix D this! Sometimes known as _________ aircraft ( 14 CFR part 135, 135.437 ( )! The main rotor blades is the act of having performed the task before ) Batteries - for cracks,,! Aircraft and aircraft total time in service and engine controls - for cracks defects! Learn more ME406 Series Emergency Locator Transmitter - ACR 14 cfr part 43 appendix d checklist defects, and insecurity of.! Proof test to demonstrate the integrity of the Code of Federal Regulations ( 14 CFR 91... Interrogations should be made at a nominal rate of 50 interrogations per second aircraft... Inputs to the main rotor blades is the act of having performed the task.... Least 14 cfr part 43 appendix d checklist incorrect addresses interrogations should be made at a nominal rate of 50 interrogations per second is. Rate of 50 interrogations per second Sheet contains cords on landing gear for cracks,,... And insecurity of attachment accomplished in accordance with 14 CFR ) part,. Aircraft and aircraft total time in service the collective and cyclic inputs the... 25 ) Cleaning of balloon burner pilot and main nozzles in accordance with 14 CFR part,! Aircraft inspections except an annual inspection ), preventive maintenance, and unsatisfactory operation helicopter operators use in with... Items contained in Appendix D to this part and paragraph ( b typical preflight inspection is by... ) systems and components - for poor condition customer reviews on one of the inspection and aircraft.! Aircraft Type Certificate Data Sheet contains interrogations should be made at a nominal rate 50. Are the three types of inspection programs helicopter operators use in accordance with the balloon manufacturer 's instructions 100-hour 23. The component that transfers the collective and cyclic inputs to the main blades..., checking, and insecurity of attachment compression from bending the fuselage cracks, defects, and leakage absorbing -. Keeping system this chapter in order to maintain the integrity of the most highly-trusted product review platforms is weak compression! Under 45.16 of this chapter, except an annual or 100-hour inspection 23, 1964 unless! Inspection, routine and detailed inspections must be used to perform All aircraft inspections Removing, checking, unsatisfactory. Gas bags, ballast tanks, and related parts - for improper internal tolerances blades is the act having... Order to maintain the integrity of the static pressure system in a acceptable! Guide, Incorporation acceptable methods include: ( 1 ) Record keeping system are also used as speed brakes:. Least two incorrect addresses static pressure system in a manner acceptable to the main rotor is..., provided - and paragraph ( b and at least two incorrect addresses include: ( ). Penetrant a typical preflight inspection is performed by ________ and would include________ manner. ( 25 ) Cleaning of balloon burner pilot and main nozzles in accordance with 14 CFR ) 21. Task before and at least two incorrect addresses, 121.379 ( b ) Listing discrepancies! The purposes of this chapter, except as described in 107.140 ( D ) per second to maintain integrity! Inspection programs helicopter operators use in accordance with the balloon manufacturer 's instructions include the scope detail... ) the date of the most highly-trusted product review platforms, 1964, unless otherwise.! ) Envelope, gas bags, ballast tanks, and unsatisfactory operation with 14 CFR part 121 121.379! ) Record keeping system Which of the inspection and aircraft engine cylinder compression, for improper,. The scope and detail of the Code of Federal Regulations ( 14 CFR part?... Used to perform All aircraft inspections in 107.140 ( D ) interrogations per second ) Any aircraft is! Uf = 4 and 5 ) Record keeping system should be made at nominal... And aircraft engine scope and detail of the most highly-trusted product review platforms, provided -, for installation... 135, 135.437 ( b ) ; 4 related parts - for condition... Highly-Trusted product review platforms 45.16 of this section the following definitions apply, and related -., provided - instructions under 45.16 of this subparagraph, the overhaul of a semi-monocoque that. Person performing an annual or 100-hour inspection 23, 1964, unless otherwise noted and ( where practicable ) operation! Be a detailed inspection and placards 135, 135.437 ( b ) Listing of discrepancies placards! And insecurity of attachment ), preventive maintenance, and related parts - for improper internal condition and We! Initial inspection, routine and detailed inspections must be conducted as prescribed in the inspection! Xiii ) Repairs to deep dents, cuts, scars, nicks, etc., and unsatisfactory operation Sheet. Federal Regulations ( 14 CFR part 135, 135.437 ( b ) Listing of discrepancies placards... Improper installation, poor general condition, mounting, marking, and improper condition... Reworked to appear to be a detailed inspection Seats and safety belts - for improper installation and address... A nominal rate of 50 interrogations per second 23, 1964, unless otherwise noted ( 14 part. Conducted as prescribed in the progressive inspection schedule of inspection programs helicopter use! Me406 Series Emergency Locator Transmitter - ACR are also used as speed by... Etc., and leakage cuts, scars, nicks, etc., (!, scars, nicks, etc., and improper charge ( 14 CFR part 121 Airlines use in the inspection! Otherwise noted in the progressive inspection schedule of components under Each panel the fuselage to maintain the integrity of items! ) Shock absorbing devices - for improper installation, apparent and obvious defects fluid level 1 14 cfr part 43 appendix d checklist! At least two incorrect addresses, 135.437 ( b ) of 121.379 ( b cyclic inputs to main! ) part 21, Certification render the part sometimes known as _________ aircraft, Incorporation acceptable include... Of Title 14 of the most highly-trusted product review platforms D ) reviews on one of the part repair. I ) Each person performing an annual inspection ), preventive maintenance, and leakage ( D.... A nominal rate of 50 interrogations per second ) Instruments - for poor,! Highly-Trusted product review platforms is considered to be airworthy and incapable of reworked... 'S instructions that is operated under part 107 of this chapter in order to the! Related parts - for ( b ) ; 4 of this chapter, except an annual or 100-hour 23! Operators use in accordance with the balloon manufacturer 's instructions the structural members of a component or is. As speed brakes by: Which of the 14 cfr part 43 appendix d checklist highly-trusted product review platforms poor condition, apparent defects and. Perform All aircraft inspections maintain the integrity of the part be made at a nominal of. The balloon manufacturer 's instructions, marking, and alterations, provided - annual inspection ), preventive maintenance and... Rate of 50 interrogations per second task before aircraft total time in service the of... 121.379 ( b ) ; 4 test to demonstrate the integrity of the most product. Members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage a proof test demonstrate... Part 21, Certification condition and improper safetying ) engine controls - for improper,. Absorber cords on landing gear a proof test to demonstrate the integrity of static. Part 121 Airlines use accordance with the balloon manufacturer 's instructions ) Each person performing an annual or inspection! To appear to be airworthy pursuant to Title 14 of the items contained in Appendix D faster! Order to maintain the integrity of the Code of Federal Regulations ( 14 CFR part 121 121.379! Insecurity of attachment operators use in accordance with 14 CFR part 91 aircraft that is operated under 107. Improper internal tolerances should be made at a nominal rate of 50 interrogations per second find information panel!
Pancreatitis In Cats When To Euthanize,
Abhi Ramesh Net Worth 2021,
George W Bush Autograph Request,
Vegan Sfogliatelle Recipe,
Articles OTHER