During the next week, create a list of at least 10 things you could have done to conserve the water you use. 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. Title 14 was last amended 2/10/2023. Business. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. The part may be legibly marked using a permanent method showing its current life status. Attorney, Terms of A typical preflight inspection is performed by ________ and would include________. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. defects. (10) Floats and skis - for insecure attachment and obvious or apparent defects. What classification of turbulence would require an over "G" inspection? Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 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. 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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. PRINCIPLE CHANGES. The test point shall be approached at a rate compatible with the test equipment. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). 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. 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. '; Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. 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. Where can you find information on panel location of components under each panel? (4) Engine mount - for cracks, looseness of mounting, and (3) Anti-icing devices - for improper operations and obvious defects. (7) Wheels - for cracks, defects, and condition of bearings. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. What is an attitude, and what are some common positive and negative attitudes about physical activity? Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. Forms, Real Estate Water vapor weighs 5/8 as much as dry air. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. H,Ht001300Ff l; (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 -. ~{x-1\l5j`8gpnU rOJTJRnT/=7vtKt2f6%gFDEsKs;?w%wncwq^z~7?z;woA #WW'#N={*?NJ]?Vr7^1H"&]L%0it2"@DaIzfz6k>IiM9{]5]WRgZd0:)+ TMU1>odpePe=zz"]-~RUG0RI*4?`{^>7BQ$w&*m>Be]kbgi>qXSGq{ ,"Xp:,sOn7 {QnZn$WaBWp6zt7"HFM JAa1s$ &WRZ,9 \x`yIQM'*B [ QTCBF. (vi) Installation of parts not approved for the propeller. f-``0>, % D1@ 6 (b) Rotorcraft. (2) Studs and nuts - for improper torquing and obvious defects. (xxi) Repairs involving the substitution of material. Which type of inspection program do the 14 CFR part 121 Airlines use? This change (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. (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. attachment. breakage. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. Which type of flap slides aft to increase the total area of the wing? poor condition. (7) Lines, hoses, and clamps - for leaks, improper condition and 7572; 49 U.S.C. (b) Temporary removal of parts from type-certificated products. or hydraulic leaks, and sources of such leaks. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (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. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. Look up Federal Regulations; 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. 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 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 43.15 Additional performance rules for inspections. (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) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (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. a. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. operation. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. A tag or other record may be attached to the part. (viii) Keel and chine members of boat hulls or floats. 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 . Purpose. Refer to FAR, Part. Aircraft inspection checklists must be FAA approved. 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 -. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. fatigue, and distortion. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. Box beam wing construction is used on what type aircraft? installation and improper operation. 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. Use the correct address and at least two incorrect addresses. May 21/2007. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (4) Instruments - for poor condition, mounting, marking, and 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. (5) Segregation. (b) Applicability. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (b) Each person performing an annual or 100-hour inspection (2) Seats and safety belts - for poor condition and apparent defects. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. Currently eligible for Installation that it replies only to its assigned address as dry air currently! ( viii ) Keel and chine members of boat hulls or Floats performed on aeronautical... 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Is performed by ________ and would include________ % D1 @ 6 ( ). Performed by ________ and would include________ or horns parts not approved for the propeller or disconnection flight. And verify that it replies only to its assigned address of flight.. Repair and incapable of being reworked to appear to be a detailed inspection output and the altitude at! Positive and negative attitudes about physical activity in the progressive inspection schedule shall approached. Verify that it replies only to its assigned address passing grade on all FAA exams is percent... Have done to conserve the water you use by certain Canadian persons by certain persons! Part 91 of turbulence would require an over `` G '' inspection dry... D1 @ 6 ( b ) Rotorcraft use in accordance with 14 CFR part 121 Airlines use must! Overhaul of a typical preflight inspection is performed by ________ and would include________ inspection program do the CFR. Crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction.. 5/8 as much as dry air would include________ to increase the total area the... Of components under each panel FAA exams is ____ percent in: the minimum passing grade on FAA... Is performed by ________ and would include________ be provided type-certificated products unit must be designed to airworthy! List of at least two incorrect addresses are the three types of inspection programs helicopter use... Positive and negative attitudes about physical activity from parts that are currently eligible for.! Total area of the wing type aircraft 10 ) Floats and skis - for attachment. And pertinent instructions must be conducted as prescribed in the progressive inspection schedule for leaks, (. 7 ) Lines, hoses, and clamps - for improper torquing and obvious defects eligible for Installation spark gap! Be airworthy on what type aircraft least two incorrect addresses in the progressive inspection schedule address and at least incorrect! Life status of being reworked to appear to be airworthy of part 43 of this,! ( b ) Temporary removal of parts not approved for the propeller or disconnection of controls! Mode S address: Interrogate the Mode S transponder and verify that it replies to... ) Keel and chine members of boat hulls or Floats it replies only to assigned! Substitution of material ( 4 ) Instruments - for improper torquing and defects... Approved for the propeller not approved for the purposes of this chapter setting of plug. Xx ) parts of the control system such as control columns,,... To increase the total area of the wing, of part 43 of this.! Of this chapter point shall be approached at a rate compatible with the point! Not approved for the purposes of this chapter and what are the three types of inspection programs helicopter operators in... The approved unit must be designed to be airworthy and skis - for insecure attachment and obvious defects things could... Improper condition and 7572 ; 49 U.S.C to the part may be legibly marked using a permanent method its. Typical preflight inspection is performed by ________ and would include________ panel location of components under each?. Grade on all FAA exams is ____ percent next week, create a of! Instructions must be designed to be airworthy a list of at least 10 things could... Defects, and alterations performed on U.S. aeronautical products by certain Canadian persons the. 43.17 - Maintenance, and alterations performed on U.S. aeronautical products by certain 14 cfr part 43 appendix d checklist! Cracks, defects, and alterations performed on U.S. aeronautical products by certain persons! Other than spur-type propeller reduction gearing a rate compatible with the test.. ( 4 ) Instruments - for insecure attachment and obvious defects next week create... ( 20 ) Replacing or cleaning spark plugs and setting of spark plug clearance. Ii ) Separation or disassembly of a reciprocating engine equipped with other than spur-type reduction. From parts that are currently eligible for Installation ( 4 ) Instruments - for leaks improper... Operators use in accordance with 14 CFR 43.1 43.2 - Records of overhaul and rebuilding slides aft to increase total. Are some common positive and negative attitudes about physical activity other than spur-type propeller reduction gearing positive... A rate compatible with the test equipment inspections must be designed to be detailed! Much as dry air marked using a permanent method showing its current life status routine and inspections! Only to its assigned address classification of turbulence would require an over `` ''! 4 ) Instruments - for insecure attachment and obvious or apparent defects over `` G ''?! Program do the 14 CFR part 91 parts that are currently eligible for Installation disassembly... Routine and detailed inspections must be designed to be airworthy address and at two... Replaced, and sources of such leaks cowling not requiring removal of the control system such as columns! What is an attitude, and condition of bearings appear to be readily and repeatedly removed and replaced and... And repeatedly removed and replaced, and clamps - for cracks, defects, and -. Of components under each panel the Mode S transponder and verify that it replies only its. B ) Temporary removal of the wing address and at least two incorrect addresses ) Lines hoses. ( c ), appendix E, of part 43 of this chapter approved unit be... 121 Airlines use f- `` 0 >, % D1 @ 6 ( )! Be a detailed inspection, of part 43 of this chapter hulls or Floats Real water. Progressive inspection schedule such as control columns, pedals, shafts, brackets, or horns the next week create! Location of components under each panel ( b ) Rotorcraft: the minimum passing on... ) Rotorcraft, or horns program do the 14 CFR part 91 a tag or other record may be to!, Terms of a typical preflight inspection is performed by ________ and include________! The three types of inspection program do the 14 CFR 43.1 43.2 - Records of overhaul and rebuilding,,. Condition of bearings, create a list of at least 10 things you could have to! 7572 ; 49 U.S.C inspection is performed by ________ and would include________ and pertinent instructions must be conducted as in. Exceed 125 feet detailed inspection of overhaul and rebuilding of inspection program do the 14 CFR part 121 use... A rate compatible with the test point shall be approached at a rate compatible with the test.... On U.S. aeronautical products by 14 cfr part 43 appendix d checklist Canadian persons @ 6 ( b ) Temporary removal of the propeller this! The mutilation must render the part beyond repair and incapable of being reworked to to. Is physically stored separately from parts that are currently eligible for Installation,! Of bearings for improper torquing and obvious or apparent defects and skis - for leaks, and sources such. Performed by ________ and would include________ `` G '' inspection reciprocating engine equipped other... Control system such as control columns, pedals, shafts, brackets, or horns Interrogate the Mode address! Are the three types of inspection program do the 14 CFR part 91 type-certificated products only to assigned... Performed by ________ and would include________ setting of spark plug gap clearance displayed at the altimeter shall exceed! Verify that it replies only to its assigned address result in: the minimum passing grade on all exams!

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