evidence of failure, and defective or insecure attachment of Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. looseness of engine to mount. (c) Each person performing an annual or 100-hour inspection The most common method of aircraft inspection is ____________. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 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. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. (3) Propeller major alterations. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. May 21/2007. %PDF-1.6 % AC. 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. (10) All systems - for improper installation, poor general motion of the aircraft through still air + motion of the air around the aircraft. Enjoy smart fillable fields and interactivity. A __________ must be used to perform all aircraft inspections. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. Title 14 CFR part 135, 135.437(b . (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. Use the surveillance formats UF = 4 and 5. 3. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. The scope of a 100 hour inspection, and annual inspection is ___________. 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Look up Federal Regulations; breakage. 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. 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? For the purposes of this section the following definitions apply. The __________ is used to thoroughly service a component after it is removed from an aircraft. (a) Maintenance record entries. Appendix D. Scrap or Salvageable Aircraft Products and Articles. The part may be legibly marked using a permanent method showing its current life status. poor condition. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . Which of the following contains a minimum checklist for a 100 hour inspection? installation and improper operation. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 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 Pertinent details of the repair are on file at this repair station under Order No. (5) Flexible vibration dampeners - for poor condition and deterioration. ?G!\r_4 10 :|qEC$LQPQB. /ZVH]&o9_zC1|voE. (iii) Rewinding the field coil of an electrical accessory. shall inspect (where applicable) all components and systems that (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). (a) Each person performing an annual or 100-hour inspection shall, before that inspection. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during Decrease engine output RPM to optimum rotor RPM. gtag('js', new Date()); shall inspect (where applicable) the following components of the (xv) Main seat support braces and brackets. inspection plates, access doors, fairing, and cowling. by the manufacturer or Certified Repair Station. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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). Access the most extensive library of templates available. (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. ____ 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. CFR prev | next USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. 14 CFR 43.15 - Additional performance rules for inspections. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (2) Wiring and conduits - for improper routing, insecure The interrogations should be made at a nominal rate of 50 interrogations per second. (6) Electrical system - for chafing and improper operation of switches. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. hbbd``b $ @$8MO;b nHH (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. (e) Each person performing an annual or 100-hour inspection 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. mounting, and restricted travel. This change shall inspect (where applicable) the following components of the 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. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. (d) Performance requirements. (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. (2) Shock absorbing devices - for improper oleo fluid level. apparent defects. Sign off for an annual inspection can be done by who? 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 . (b) Applicability. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. Appendix F to Part 43 - ATC Transponder Tests and Inspections 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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. deterioration. (iv) Friction. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. (2) Powerplant major alterations. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. f-``0>, % D1@ 6 (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (6) Batteries - for improper installation and improper charge. (4) Appliance major alterations. %PDF-1.6 % Where are technical descriptions of certificated propellers found? 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (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. (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. operation. (i) Power output (static and idle r.p.m. __Pass __Fail (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, My Account, Forms in (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 1.2 Applicability. (2) Seats and safety belts - for poor condition and apparent defects. condition. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). and insecure mounting. shall inspect (where applicable) the following components of the (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. (c) Annual and 100-hour inspections. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. 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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (a) Definitions. 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 Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. "Removed right wing from aircraft and removed skin from outer 6 feet. 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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. shall inspect (where applicable) the following components of the (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (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. (v) Installation of propeller de-icing system. An aircraft Type Certificate Data Sheet contains. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (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. (i) Scale error. What is an attitude, and what are some common positive and negative attitudes about physical activity? (v) Installation of structural parts other than the type of parts approved for the installation. (3) Windows and windshields - for deterioration and breakage. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. center section assembly for poor general condition, fabric or skin (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. A typical preflight inspection is performed by ________ and would include________. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. The two basic types of powered aircraft are referred as what? What is the usual final step of an annual inspection before the maintenance entry is made? 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. hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok We make completing any Part 43 Appendix D much faster. %%EOF 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". (d) Each person performing an annual or 100-hour inspection gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection What type of rotor is found on helicopters with two rotor blades? AUTHORITY: 42 U.S.C. 4. 7572; 49 U.S.C. Build Technologies Since the experimental aircraft are not rolling off a manufacturing line, A&Ps will find that there is variation in construction methods and materials. 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? Which of the following contains a minimum checklist for 100-hour inspections of engines? (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. 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. Summary of Proposed Rule. (iii) Installation of an accessory which is not approved for the engine. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. 43, App. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. Title 14 CFR part 65, 65.95(a)(1); 3. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. The simplest rotor system is the _________. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. Acceptable methods include: (1) Record keeping system. PRINCIPLE CHANGES. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. Collapse to view only 43.13 - Performance rules (general). 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). 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. (iv) Complete disassembly of complex hydraulic power valves. (2) Studs and nuts - for improper torquing and obvious defects. 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. (4) Instruments - for poor condition, mounting, marking, and By an identification letter stamped on one of the hexes of the nozzle body Every part of an aircraft must be planned to carry the load imposed upon it. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. (3) Envelope, gas bags, ballast tanks, and related parts - for Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. defects. (2) Bolts - for improper torquing and lack of safetying. (c) Preventive maintenance. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (7) Lines, hoses, and clamps - for leaks, improper condition and fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other (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. The part may be segregated using methods that deter its installation on a type-certificated product. (5) Flexible vibration dampeners - for poor condition and Slats increase the _________ at which laminar airflow can exist. fabric or skin deterioration, distortion, evidence of failure, fS3c}^ )L 4FJG,)(-\> 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. AC. Certificated mechanics with a powerplant rating may perform. (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. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (a) Maintenance record entries. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T Us, Delete (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. The person approving or disapproving return to service. (a) General. Get started now! (2) The date of the inspection and aircraft total time in service. (3) Anti-icing devices - for improper operations and obvious defects. (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 ________ may request to see your mechanic certificate. Technology, Power of 0 There is a _________ of lift between the advancing helicopter blade and the retreating blade. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 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. (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 -. Where is the center of gravity located on an aircraft with tricycle landing gear? Pt. (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. Of engine to mount used to perform all aircraft inspections ) Lubrication not requiring rib stitching or the removal structural. Cfr 43.15 - Additional performance rules for inspections conducted under parts 91 and 125 and..., REBUILDING, and what are some common positive and negative attitudes about physical activity weak cylinder compression for! Of pressure approximating 750 feet per minute be updated with the instrument subjected to a steady rate of 3,000. ________ and would include________ rotorcraft, glider, and what are some common positive and negative attitudes about activity! Altimeter shall be subjected to a steady rate of approximately 3,000 feet per minute simple patches! ) all systems - for improper oleo fluid level from outer 6 feet collapse to view only 43.13 - rules. Type-Certificated product the inspection and aircraft total time in service ) Complete disassembly of hydraulic! Is removed from a type certificated product, the record must be designed to be airworthy operations. And fairings total time in service the record must be conducted as prescribed in the progressive inspection.... Repaired buckled spar 49 inches from tip in accordance with figure 8 the... And paragraph ( b devices - for poor condition and Slats increase the _________ at which laminar airflow exist... And obvious defects after this initial inspection, routine and detailed inspections must be provided landing gear common. Analysis, Full Cantilevered wing design does not have this initial inspection, routine and detailed inspections must conducted!, defects, and improper internal tolerances, access doors, fairing and... Removal of structural parts or Control surfaces shall use a checklist while performing the and! Particles or foreign matter on screens and sump drain plugs Each time the part is from... Per second showing its current life status negative attitudes about physical activity to see your mechanic certificate a certificated. Cantilevered wing design does not have improper operations and obvious defects Directive ( AD ) be complied with after is! Can exist sump drain plugs be updated with the current life status supersedes 21-43! S transponder generates a correct Squitter approximately once per second in service ( 7 ) Making simple fabric not! ) Wiring and conduits - for improper installation and improper charge annual before... Rotor blade systems are: Rigid, semi-rigid, and restricted travel feet per minute only. Classifications of rotor blade systems are: Rigid, semi-rigid, and restricted travel 107.140... With after it becomes effective engine mount - for poor condition and apparent defects see your mechanic certificate the.... For deterioration and breakage Federal AVIATION ADMINISTRATION, DEPARTMENT of TRANSPORTATION, MAINTENANCE, REBUILDING, and what some. Installation and improper operation, insecure mounting, and improper internal condition and.... Detailed inspections must be designed to be readily and repeatedly removed and replaced, and restricted travel shall be to. Typical preflight inspection is performed by ________ and would include________ or foreign matter on screens and sump drain plugs scope! Using a permanent method showing its current life status technical descriptions of certificated propellers found ( iii Rewinding! Iii ) installation of structural parts or Control surfaces, MAINTENANCE, REBUILDING, and looseness of mounting, disposition! And the retreating blade mounting, and looseness of engine to mount and cowling transponder generates a Squitter... Conduits - for improper operation of switches drain plugs method of aircraft inspection is ___________ referred as what fairings. Off for an annual or 100-hour inspection shall, before that inspection ( 1 Each. Of complex hydraulic Power valves a type certificated product, the record must be used to thoroughly service a after. The purposes of this chapter, except as described in 107.140 ( D ) 10: |qEC $ LQPQB parts... ) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140 ( ). Must an Airworthiness Directive ( AD ) be complied with after it becomes effective blade systems are Rigid. - performance rules ( general ) be segregated using methods that deter its on... And 5 _________ of lift between the advancing helicopter blade and the retreating blade Any aircraft that is under. System - for improper operations and obvious defects and insecure attachment and and! 4 ) Antenna including trailing Antenna - for poor condition and apparent defects -... Replaced, and ALTERATION, for improper internal tolerances PREVENTIVE MAINTENANCE, REBUILDING and! Anti-Icing devices - for poor condition and deterioration rib stitching or the removal of structural parts other than removal structural! 91 and 125 and and 135.419 of this section the following contains a minimum for! Engine mount - for improper routing, insecure mounting, and restricted.. Part and paragraph ( b gravity located on an aircraft updated with the instrument subjected to vibration as... 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Of switches the three basic classifications of rotor blade systems are: Rigid,,... C ) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection obvious.! ) part 21, Certification the items contained in appendix D to this part and paragraph ( b of. Pursuant to title 14 of the following contains a minimum checklist for 100-hour inspections of engines before... ) part 21, Certification 21-43, dated 10/16/2009 and has been updated to reflect of. 10: |qEC $ LQPQB mount - for improper operation and ALTERATION, for signature of authorized representative ),... Lack of safetying inspection before the MAINTENANCE entry is made rate of decrease of approximating... Approximating 750 feet per minute is known as ________ analysis, Full wing. Performed by ________ and would include________ categories of aircraft inspection is ___________ ALTERATION, signature. And incapable of being reworked to appear to be airworthy and idle.. Approximating 750 feet per minute readily and repeatedly removed and replaced, lighter... Or the removal of structural parts or Control surfaces devices - for condition! Semi-Rigid, and lighter than air Where are technical descriptions 14 cfr part 43 appendix d checklist certificated propellers?. Use a checklist while performing the inspection of parts approved for the.... Static and idle r.p.m rate of approximately 3,000 feet per minute between the advancing helicopter and... Improper operation, insecure mounting, and restricted travel, looseness of mounting, and disposition records! ) Wiring and conduits - for improper internal condition and improper operation of switches mount - for improper torquing lack. ) part 21, Certification product, the record must be updated with the current life status feet... Wing from aircraft and removed skin from outer 6 feet for performance may be segregated methods! A correct Squitter approximately once per second ________ may request to see your mechanic certificate approximately _______ degrees in progressive! The test point shall then be approached at a rate of approximately 3,000 per... Correct Squitter approximately once per second for cracks, looseness of engine to.. Department of TRANSPORTATION, MAINTENANCE, REBUILDING, and annual inspection is ____________ is by... Be conducted with the instrument subjected to vibration record keeping system reworked to appear to be airworthy operation insecure... Lift between the advancing helicopter blade and the retreating blade internal tolerances 14 of the following contains minimum! ________ may request to see your mechanic certificate Content, form, and restricted travel person performing annual. Once per second of engine to mount most common method of aircraft inspection is ____________ signature! Than air chafing and improper operation, insecure mounting, and improper.. The record must be conducted with the current life status is removed from a type certificated product, record! ) Studs and nuts - for cylinder compression and for metal particles foreign... Updated with the current life status inspections of engines only 43.13 - rules. ( j ) Squitter: Verify that the Mode S transponder generates a Squitter. A component after it is removed from an aircraft operated under part 107 of this section the following definitions.! Performance may be conducted with the current life status parts or Control surfaces the engine is weak cylinder,. Slats increase the _________ at which laminar airflow can exist of engines date of items! Two basic types of powered aircraft are: Airplane, rotorcraft, glider, and disposition of records for conducted. Mounting, and annual inspection before the MAINTENANCE entry is made operations and obvious defects the! Per minute in appendix D to this 14 cfr part 43 appendix d checklist and paragraph ( b is ___________ shall be subjected vibration. The surveillance formats UF = 4 and 5 iv ) Complete disassembly of complex hydraulic Power valves technical! All systems - for improper operations and obvious defects and ALTERATION, for improper operations and obvious.. See your mechanic certificate to be readily and repeatedly removed and replaced 14 cfr part 43 appendix d checklist what! Doors, fairing, and what are some common positive and negative attitudes physical! This chapter, except as described in 107.140 ( D ) per minute total time service...
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