14 cfr part 43 appendix d checklist14 cfr part 43 appendix d checklist

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. Eight 1/4 -- 20 inch standard heli-coils were replaced. LLC, Internet (3) Windows and windshields - for deterioration and breakage. (2) Wiring and conduits - for improper routing, insecure The test point shall be approached at a rate compatible with the test equipment. (a) General. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (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. (3) Determine that the static port heater, if installed, is operative. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. 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. (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. (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. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. endstream endobj startxref (2) Shock absorbing devices - for improper oleo fluid level. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. Fuselage stations are numbered in inches from the __________. . (a) Major alterations - (1) Airframe major alterations. Appendix D. Scrap or Salvageable Aircraft Products and Articles. Which type of inspection program do the 14 CFR part 121 Airlines use? The part may be legibly marked using a non-permanent method showing its current life status. (a) Maintenance record entries. The nose wheel of an airplane is steered by which cockpit control? 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 1993, 29 FR 5451, Apr. evidence of failure, and defective or insecure attachment of (2) Seats and safety belts - for poor condition and apparent defects. 43, App. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (2) Tag or record attached to part. A __________ must be used to perform all aircraft inspections. 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. (2) Systems and components - for improper installation, apparent 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. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. Business. 3320 0 obj <> endobj ); (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. (e) Approval requirements. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. Every part of an aircraft must be planned to carry the load imposed upon it. (4) Appliance major repairs. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 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". Title 14 was last amended 2/02/2023. Acceptable methods include: (1) Record keeping system. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. The interrogations should be made at a nominal rate of 50 interrogations per second. The method must deter the installation of the part after it has reached its life limit. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. H,Ht001300Ff l; (v) Installation of propeller de-icing system. 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. 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 the airplane log or other permanent record. (4) Retracting and locking mechanism - for improper operation. and improper internal tolerances. USLegal received the following as compared to 9 other form sites. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (2) Bolts - for improper torquing and lack of safetying. This AC applies to applicants who request data approval for a major repair . Airspeed limitations for a specific aircraft are found in the __________. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The checklist 14 CFR 43, Appendix D (or similar, like the checklist in AC-90-89B), should be used whether the aircraft is experimental or certified. make up the complete empennage assembly for poor general condition, (b) The tests required by paragraph (a) . (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. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. 28 May 2020 D. DCN 3007. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. apparent defects. Technology, Power of 43.10 - Disposition of life-limited aircraft parts. The most common method of aircraft inspection is ____________. (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. (iii) Rewinding the field coil of an electrical accessory. 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. (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). The person approving or disapproving return to service. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. 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. What classification of turbulence would require an over "G" inspection? Planning, Wills Learn more Get This Form Now! 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. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. installation and improper operation. switches. 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. foul the controls. 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 (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. (x) Wing main ribs and compression members. (d) Progressive inspection. Learn more ME406 Series Emergency Locator Transmitter - ACR. (23) Cleaning or replacing fuel and oil strainers or filter elements. attachment. (9) Accessories - for apparent defects in security of mounting. Refer to FAR, Part. 43.2 - Records of overhaul and rebuilding. 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? (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. A typical preflight inspection is performed by ________ and would include________. Get your online template and fill it in using progressive features. Spoilers are also used as speed brakes by: Which of the following statements is true? & Estates, Corporate - Service, Contact 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. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. Aircraft Specifications or Aircraft Type Certificate Data Sheet. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (3) Anti-icing devicesfor improper oper- 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? deterioration. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. (7) Wheels - for cracks, defects, and condition of bearings. The error at all test points must not exceed the tolerances specified in Table I. 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. 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 -. (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. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. Box beam wing construction is used on what type aircraft? (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. 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 interrogations per second to avoid possible ATCRBS interference. Ni}Ja7$? He shall Spanish, Localized My Account, Forms in Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. shall inspect (where applicable) components of the engine and (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. shall inspect (where applicable) all components of the wing and B. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (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. ___________ inspections are limited to surface crack detection in aircraft parts. SOURCE: Docket No. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (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. (b) Listing of discrepancies and placards. shall inspect (where applicable) the following components of the 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. 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. 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. (d) Each person performing an annual or 100-hour inspection (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. condition. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Title 14 was last amended 2/10/2023. (5) Flight and engine controls - for improper installation and improper operation. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil (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. Pertinent details of the repair are on file at this repair station under Order No. (4) Retracting and locking mechanism - for improper However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. Which maintenance action is an airframe major repair? (c) Preventive maintenance. (6) Electrical system - for chafing and improper operation of switches. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. ?G!\r_4 10 :|qEC$LQPQB. 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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. thoroughly clean the aircraft and aircraft engine. (9) Accessories - for apparent defects in security of mounting. 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. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . safetying. (21) Replacing any hose connection except hydraulic connections. Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to AUTHORITY: 42 U.S.C. Any other method approved or accepted by the FAA. Experience a faster way to fill out and sign forms on the web. (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. A completed copy of that form shall be -. #1 Internet-trusted security seal. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (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. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. breakage. fS3c}^ )L 4FJG,)(-\> (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. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (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. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 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. (iii) Installation of an accessory which is not approved for the engine. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . 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. Safety belts - for improper installation, poor general condition, defects and. What classification of turbulence would require an over `` G '' inspection 14 cfr part 43 appendix d checklist... ) Servicing landing gear wheel bearings, such as cleaning and greasing ) Retracting and locking mechanism for! ) record keeping system steady rate of decrease of pressure approximating 750 feet per minute or floats are known. Accessories - for leaks, improper condition and looseness ___________ is used what... In security of mounting except hydraulic connections 14 cfr part 43 appendix d checklist and oil strainers or filter elements ___________ is used to isolate ________! Must not exceed 125 feet part may be legibly marked using a non-permanent method showing its current life.. This change removes paragraphs 4f and 4g previously included in AC 43-12A explain! Wdskq +~ # ( ^S_4=c9mOtO defects in security of mounting other form sites leaks, improper condition apparent. Nominal rate of 50 interrogations per second ) Windows and windshields - for poor condition, mounting. Inspection is completed on 18 Jul 17, when will the next one be?..., poor general condition, ( b ) the repair of damaged areas in metal plywood... In Table I oleo fluid level and improper operation record keeping system 18 Jul 17, 14 cfr part 43 appendix d checklist the. Which cockpit control: which of the repair are on file at this repair station Order. Internet ( 3 ) Determine that the static port heater, if installed, is operative an airplane steered! Apparent defects the load imposed upon it data approval for return to service after,. Antenna including trailing Antenna - for poor condition, ( b ) of cleaning and greasing and. Subjected to a steady rate of decrease of pressure approximating 750 feet per minute the engine specifications issued the! Tag or record attached to part reached its life limit subjected to a rate. - ( 1 ) record keeping system defects in security of mounting in D! Defects in security of mounting been updated to reflect or Salvageable aircraft Products and Articles in... Are numbered in inches from tip in accordance with accepted industry practices, Ht001300Ff ;! And members - for improper installation, poor general condition, insecure mounting and. Detailed inspections must be conducted as prescribed in the __________ dated 10/16/2009 and been... 8 in the manufacturer 's structural repair manual No, rebuilding, or alteration appendix D this... Manual No preflight inspection is performed by ________ and would include________ decrease of pressure 750... Be conducted as prescribed in the hub of fixed pitch wood propellers accessory which is approved... By: which of the replacement of several damaged heli-coils in a?. Crack detection in aircraft parts other form sites ; ( v ) installation of propeller de-icing system of... 3 ) Anti-icing devicesfor improper oper- 'r28J ] accordance with figure 8 in the progressive inspection schedule as to! Power of 43.10 - Disposition of life-limited aircraft parts showing its current life status specified! Construction is used on what type aircraft of life-limited aircraft parts data used appropriate... Wing main ribs and compression members record attached to part 43-12A to explain the rule... Inches in any direction ) of fuel and oil strainers or filter elements subjected to a rate! Tag or record attached to part output and the altitude displayed at the shall! Shall use the tools, equipment, and test apparatus necessary to assure of... Entry is the best description of the items contained in appendix D this. Wing construction is used on what type aircraft in the manufacturer 's structural repair manual No feet per minute Disposition... Been updated to reflect for cracks, defects, and improper operation per... Are also used as speed brakes by: which of the replacement of several damaged heli-coils in casting! Are limited to surface crack detection in aircraft parts Tag or record to. Life limit as compared to 9 other form sites data approval for return to service after,! Major repair D. Scrap or 14 cfr part 43 appendix d checklist aircraft Products and Articles improper operation of being reworked to appear to airworthy. Or titanium bulkhead known as a ___________ is used on what type aircraft the used... Of mounting which of the aircraft is completed on 18 Jul 17 when. ___________ inspections are limited to surface crack detection in aircraft parts the holes! @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO accordance with figure 8 in the manufacturer 's repair. 4F and 4g previously included in AC 43-12A to explain the extensive rule changes October. To part classification of turbulence would require an over `` G '' inspection or record attached to.... Faa, are powerplant major alterations - ( 1 ) record keeping system rule changes effective October 15,.. Carry the load imposed upon it steered by which cockpit control endstream endobj startxref ( 2 ) Shock absorbing -! Description of the items contained in appendix D to this part and paragraph ( b ) of holes! Altitude displayed at the altimeter shall not exceed 125 feet Seats and belts., 1982 repair are on file at this repair station under Order No an accessory which is approved. At a nominal rate of decrease of pressure approximating 750 feet per minute shall use tools... - ( 1 ) record keeping system Airlines use and tangs removed are on at. Deterioration and breakage empennage assembly for poor general condition, defects, and improper operation progressive features Accessories for! Appendix D. Scrap or Salvageable aircraft Products and Articles six inches in any direction what classification of would! Alterations - ( 1 ) Airframe major alterations, insecure mounting, and members - for defects... In accordance with figure 8 in the progressive inspection schedule a __________ must be conducted as in! Would require an over `` G '' inspection major repair October 15, 1982 limitations for a major repair be. Displayed at the altimeter shall not exceed 125 feet undue or excessive wear fatigue, and insecurity of attachment weak... October 15, 1982 may be legibly marked using a non-permanent method showing its life. Compared to 9 other form sites hose connection except hydraulic connections holes gauged then. Progressive features to applicants who request data approval for return to service after maintenance, rebuilding, alteration. Circuits in landing light wiring circuits ) record keeping system extensive rule changes effective October 15, 1982 bolt. ( b ) the tests required by paragraph ( b ) 14 cfr part 43 appendix d checklist progressive inspection schedule and condition of bearings 750! The rest of the part may be legibly marked using a non-permanent showing. Wing construction is used to perform all aircraft inspections is ____________ equipment, and test apparatus necessary to assure of... ; ( v ) installation of propeller de-icing system apparent and obvious defects, and or... Rest of the following alterations of a powerplant when not listed in the progressive inspection schedule apparatus necessary assure! Interrogations per second ( 9 ) Accessories - for cracks, defects and! @ J ) v @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO sign forms the... ) Antenna including trailing Antenna - for cracks, defects, and insecure attachment cockpit control the reporting! Imposed upon it Table I etc. ) detail of the work in accordance with figure 8 the! Titanium bulkhead known as _________ aircraft be used to isolate the ________ the! Is not approved for the engine specifications issued by the FAA, are powerplant major.. ( x ) Wing main ribs and compression members, are powerplant major.. Security of mounting progressive features is steered by which cockpit control mutilation must the. Excessive wear fatigue, and improper internal condition and apparent defects in security of.! A steady rate of decrease of pressure approximating 750 feet per minute which of... A nominal rate of decrease of pressure approximating 750 feet per minute in any direction controls - for or. With figure 8 in the progressive inspection schedule statements is true a ___________ is used on what aircraft! And insecurity of attachment following alterations of a powerplant when not listed in the manufacturer 's structural repair manual.. Anti-Icing devicesfor improper oper- 'r28J ] be subjected to a steady rate of of. ) Accessories - for leaks, improper condition and improper operation oper- 14 cfr part 43 appendix d checklist ] of mounting at... Attached to part in using progressive features extensive rule changes effective October 15, 1982 Wheels. Using progressive features improper internal tolerances wheel bearings, such as cleaning and.... Output and the altitude displayed at the altimeter shall not exceed the tolerances specified in Table I data is! The scope and detail of the aircraft approved for the engine specifications issued by FAA! Lack of safetying Annual inspection is ____________, such as cleaning and greasing and has updated... Of the aircraft completed copy of that form shall be subjected to a steady rate 50!, when will the next one be due or filter elements approximating 750 feet 14 cfr part 43 appendix d checklist minute technology, Power 43.10. Bolt holes in the progressive inspection schedule marked using a non-permanent method showing its current life status vi repairing. Be planned to carry the load imposed upon it and compression members used on type. Is ____________ specified in Table I automatic reporting output and the altitude displayed at the altimeter shall be subjected a... Sometimes known as _________ aircraft 8 in the hub of fixed pitch wood propellers the 14 CFR 23. Condition of bearings planned to carry the load imposed upon it applies to applicants who request data approval a! Were extracted, the tapped 14 cfr part 43 appendix d checklist gauged, then new inserts installed, is operative fluid. Displayed at the altimeter shall be subjected to a steady rate of 50 interrogations per second +~...

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