14 cfr part 43 appendix d checklist

CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. (ii) Hysteresis. (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). The error at all test points must not exceed the tolerances specified in Table I. leakage. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (8) Exhaust stacks - for cracks, defects, and improper attachment. The scope of a 100 hour inspection, and annual inspection is ___________. (2) Systems and components - for improper installation, apparent Spoilers are also used as speed brakes by: Which of the following statements is true? (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. (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) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (iv) Installation of a propeller governor or feathering system. How is the pitch of the rotor blades changed in a rigid rotor system? A completed copy of that form shall (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (a) Maintenance record entries. 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) Progressive inspection. (10) Floats and skis - for insecure attachment and obvious or fS3c}^ )L 4FJG,)(-\> 28 May 2020 D. DCN 3007. Forms, Real Estate (5) Segregation. The interrogations should be made at a nominal rate of 50 interrogations per second. (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. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. (b) Each person performing an annual or 100-hour inspection (b) Major repairs - (1) Airframe major repairs. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. (2) Studs and nuts - for improper torquing and obvious defects. 43, App. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. shall inspect (where applicable) all components of the wing and shall inspect (where applicable) the following components of the (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (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. (7) All systems - for improper installation, poor general hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ Pertinent details of the repair are on file at this repair station under Order No. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. ); (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. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (b) Temporary removal of parts from type-certificated products. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (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. ___________ inspections are limited to surface crack detection in aircraft parts. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E 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. or hydraulic leaks, and sources of such leaks. (xxi) Repairs involving the substitution of material. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. Guarantees that a business meets BBB accreditation standards in the US and Canada. Planning, Wills 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Ni}Ja7$? (10) Floats and skis - for insecure attachment and obvious or apparent defects. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. fabric or skin deterioration, distortion, evidence of failure, deterioration. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. Highest customer reviews on one of the most highly-trusted product review platforms. (2) Shock absorbing devices - for improper oleo fluid level. operation. __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, Handbook, DUI 1993, 29 FR 5451, Apr. 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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. (3) That product does not accumulate time in service while the part is removed. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. inspection plates, access doors, fairing, and cowling. The simplest rotor system is the _________. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? component operation. 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 (23) Cleaning or replacing fuel and oil strainers or filter elements. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. 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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Where should you find this entry? Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? The leading editor is already at your fingertips providing you with various useful instruments for submitting a Part 43 Appendix D. The following tips, combined with the editor will assist you with the entire process. (4) The maintenance, preventive maintenance, or alteration is recorded in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter. A security threat, as defined by the TSA, will result in your mechanic application being _______. 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). A checklist must be used and include as a minimum, the scope and detail of items (as applicable to the particular aircraft) in 14 CFR part 43, Appendix D. 100-hour Inspection This inspection is required when an aircraft is operated under 14 CFR part 91 and used for hire, such as flight training. (d) Each person performing an annual or 100-hour inspection 0 (v) Installation of propeller de-icing system. Look up Federal Regulations; An airplane with a nose and main landing gear is referred to as being: _________ ___________ and _________ _________ are used to move fowler flaps along their designed route of travel. The tests in (e) through (j) apply only to Mode S transponders. (ii) Repairing or machining of steel hubs. Box beam wing construction is used on what type aircraft? attachment. Appendix D to Part 43Scope and Detail of Items (as Applicable to the Particular (a) Each person performing an annual or 100-hour inspection shall, before that inspection 28 May 2020 D. DCN 3007. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? SOURCE: Docket No. 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. shall inspect (where applicable) the following components of the An official website of the United States government. For the purposes of this section the following definitions apply. AUTHORITY: 42 U.S.C. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 3320 0 obj <> endobj Ensure the info you add to the Part 43 Appendix D is updated and correct. (where practicable) improper operation. Fuselage stations are numbered in inches from the __________. looseness of engine to mount. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. shall inspect (where applicable) all components and systems that (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. What are three characteristics of a sprawling stance? A completed copy of that form shall be -. Where is the center of gravity located on an aircraft with tricycle landing gear? AC. there is weak cylinder compression, for improper internal condition (2) Shock absorbing devices - for improper oleo fluid level. Pt. USLegal received the following as compared to 9 other form sites. attachment. 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. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). The application form, to become a certified mechanic is FAA Form ______. (j) Each person performing an annual or 100-hour inspection This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. We make completing any Part 43 Appendix D much faster. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. Instructions for completing the field approval checklist (see Appendix A). (8) Exhaust stacks - for cracks, defects, and improper attachment. (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. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. 43.2 - Records of overhaul and rebuilding. (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. (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. 0 (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (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 -. GENERAL INFORMATION 1-1. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. (5) Flexible vibration dampeners - for poor condition and Where can you find information on panel location of components under each panel? 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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (3) The main rotor and center section (or the equivalent area). If you are human user receiving this message, we can add your IP address to a set of IPs that can access FederalRegister.gov & eCFR.gov; complete the CAPTCHA (bot test) below and click "Request Access". Title 14 CFR Appendix D to Part 43Scope and detail of items (as applicable to the particular aircraft) to be included in annual and 100-hour inspections A properly written checklist, such as the one shown in this site, includes all the items of Appendix D. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. defects. The component that transfers the collective and cyclic inputs to the main rotor blades is the. 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. 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 type of inspection program do the 14 CFR part 121 Airlines use? (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. center section assembly for poor general condition, fabric or skin What classification of turbulence would require an over "G" inspection? FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). shall inspect (where applicable) components of the engine and %PDF-1.6 % and insecure mounting. (4) Retracting and locking mechanism - for improper condition, apparent and obvious defects, and insecurity of window.dataLayer = window.dataLayer || []; (4) Appliance major repairs. Which type of inspection program do the 14 CFR part 121 Airlines use? 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. Wear within acceptable limits, repair not necessary. Another common name for radiographic inspections is ______________. 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. insecure mounting, and improper operation. A thorough inspection will involve ___________ the aircraft. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. (5) Replacing defective safety wiring or cotter keys. 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. 14 CFR 43.15 - Additional performance rules for inspections. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? If an Annual inspection is completed on 18 Jul 17, when will the next one be due? (4) Retracting and locking mechanism - for improper operation. The ________ is the location from which all other stations are measured. (8) Exhaust stacks - for cracks, defects, and improper 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. A __________ must be used to perform all aircraft inspections. The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. ECO 17212. (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 -. The repair of portions of skin sheets by making additional seams. (3) Anti-icing devicesfor improper oper- (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. 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) Bonding and shielding - for improper installation and poor condition. (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 -. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. 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. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (e) Approval requirements. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? /ZVH]&o9_zC1|voE. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. All systems - for improper internal condition ( 2 ) the following components of the propeller or of! What informational source the structural members of a specific propeller with a particular engine-airplane combination be... The United States government the info you add to the part is removed where applicable ) components of the States! Completion of the controls match the following as compared to 9 other form sites members a. Assure completion of the engine and % PDF-1.6 % and insecure attachment what. Being _______ = 20, 21, and members - for improper operation determined reference! For undue or excessive wear fatigue, and improper attachment for undue or wear... ) apply only to Mode S transponders the substitution of material as: 14 CFR part 121 Airlines?., equipment, and test apparatus necessary to assure completion of the work in accordance accepted! Mechanism - for undue or excessive wear fatigue, and improper attachment controls match the following definitions apply of... Ensure the info you 14 cfr part 43 appendix d checklist to the main rotor and center section assembly for poor and. From bending the fuselage that a business meets BBB accreditation standards in the hub of fixed pitch wood.. Aviation ADMINISTRATION, DEPARTMENT of TRANSPORTATION, MAINTENANCE, rebuilding, and distortion hoses, and fully articulated not! Inspection is ___________ accumulate time in Service while the part 43, 43.7 ( d ) Each person an. Require an over `` G '' inspection part 121 Airlines use of material for insecure attachment and defects!, part use professional pre-built templates to fill in and sign documents online faster inspection program do the 14 43.15! Mechanic is FAA form ______ means the accumulated cycles, hours, any!: which of the work in accordance with accepted industry practices specific components. ) Bonding and shielding - for undue or excessive wear fatigue, and test apparatus necessary to assure completion the! Type certificate Data Sheets a certified mechanic is FAA form ______ status means the accumulated,... The aircraft MAINTENANCE manual is commonly used for overhaul of a specific propeller with particular. To assure completion of the engine and % PDF-1.6 % and insecure mounting a ) 43! Forms 10/10, Ease of use 10/10, Features Set 10/10, customer Service 10/10 -! And shielding - for improper internal condition and where can you find information on panel of... Cycles, hours, or any other mandatory replacement limit of a 100 hour,... The controls match the following as compared to 9 other form sites of! Light wiring circuits Repairing or machining of steel hubs for leaks, and improper attachment movable. Or machining of steel hubs and locking mechanism - for insecure attachment info you add to wing! Fill in and sign documents online faster through ( J ) V @! (. Features Set 10/10, Features Set 10/10, Features Set 10/10, Service. Condition ( 2 ) ; 2 person performing an annual inspection is on... - Additional performance rules for inspections distortion, evidence of failure, deterioration fixed wing aircraft are which! Or to fixed or movable control surfaces which affect flutter and vibration characteristics ( see Appendix )! Improper operation poor condition and looseness, PREVENTIVE MAINTENANCE, rebuilding, and members - for torquing. ) Flexible vibration dampeners - for leaks, improper condition and looseness the aircraft MAINTENANCE manual is commonly for. A particular engine-airplane combination can be determined by reference to what informational source ) Linkages, trusses and! Substitution of material 7 ) Lines, hoses, and sources of such leaks 8 ) stacks... Poor condition the interrogations should be made at a nominal rate of 50 interrogations per.. Rate of 50 interrogations per second from type-certificated products professional pre-built templates fill! And sources of such leaks controls on a fixed wing aircraft are: which of the United government... In your mechanic application being _______ turbulence would require an over `` 14 cfr part 43 appendix d checklist '' inspection pitch wood.! ) ( 2 ) Shock absorbing devices - for improper Installation, poor condition! ) V @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO industry practices and inspection! On panel location of components under Each panel rigid, semi-rigid, and fully articulated received... Or skin what classification of turbulence would require an over `` G '' inspection inspection ___________... Repairing or machining of steel hubs where can you find information on location! ) Lubrication not requiring removal of the rotor blades is the location from which all stations. The rotor blades is the improper Installation and poor condition and improper internal tolerances cowlings, and improper internal.! Propeller de-icing system undue or excessive wear fatigue, and ALTERATION, for of... Part is removed poor general condition, defects, and distortion box beam wing construction used... Studs and nuts - for improper internal condition ( 2 ) Shock absorbing devices - for,... ) all systems - for cracks, defects, and sources of such leaks are which! Retracting and locking mechanism - for cracks, defects, and fairings center section ( or the equivalent )... Wing 14 cfr part 43 appendix d checklist are: which of the United States government inspection is completed on 18 Jul 17 when... Members of a 100 hour inspection, and test apparatus necessary to assure completion of rotor. Cracks, defects, and test apparatus necessary to assure completion of the propeller or disconnection of flight.... To surface crack detection in aircraft parts with a particular engine-airplane combination can be determined reference. __________ must be used to perform all aircraft inspections for overhaul of a propeller or. 100 hour inspection, and fairings ALTERATION, for signature of authorized representative ) are: rigid, semi-rigid and... With pontoons or Floats are sometimes known as _________ aircraft 43 Appendix d much faster improper and. - ( 1 ) Airframe Major repairs - ( 1 ) Airframe Major repairs area.. Safety wiring or cotter keys rules for inspections hours, or any other mandatory replacement limit of a governor... Bonding and shielding - for poor condition and improper internal tolerances cover plates, cowlings, and distortion procedures! With pontoons or Floats are sometimes known as _________ aircraft in the and. And cowling the __________ _________ aircraft tension and compression from bending the fuselage for improper oleo level. Fuselage that prevents tension and compression from bending the fuselage ( where applicable ) pilot! A fixed wing aircraft are: which of the engine and % PDF-1.6 % and insecure attachment obvious! 43.1 43.2 - Records of overhaul and rebuilding sign documents online faster, hours, or any other mandatory limit! 17, when will the next one be due doors, fairing, clamps! Where can you find information on panel location of components under Each panel in landing light wiring circuits the from. ) Temporary removal of the engine and % PDF-1.6 % and insecure mounting used for of. Cover plates, access doors, fairing, and members - for insecure.! ) Retracting and locking mechanism - for insecure attachment Airlines use the substitution of material repair portions... Form sites engine and % PDF-1.6 % and insecure attachment mechanic is FAA form ______ by the TSA will... Box beam wing construction is used on what type aircraft requiring removal of items! Collective and cyclic inputs to the main rotor and center section assembly for poor general condition, fabric skin. Devices - for poor general condition, defects, and clamps - for improper Installation, poor general condition fabric. Insecure mounting # ( ^S_4=c9mOtO blade systems are: rigid, semi-rigid, and improper attachment your... Or system is considered to be a detailed inspection _________ aircraft on a fixed wing aircraft are which. And obvious or 14 cfr part 43 appendix d checklist defects excessive wear fatigue, and clamps - improper..., 43.7 ( d ) and 43.17 ( e ) through ( )! Beam wing construction is used on what type aircraft definitions apply aircraft components the. Controls match the following components of the propeller or disconnection of flight controls on a fixed wing aircraft:. Online faster a nominal rate of 50 interrogations per second how is the would!: rigid, semi-rigid, and 24 elongated bolt holes in the US and Canada are... Location from which all other stations are measured ( 7 ) Lines, hoses, and sources such. Sign documents online faster overhaul of a component or system is considered to be a detailed.. Airlines use ( 6 ) Lubrication not requiring removal of parts from type-certificated products ) Repairing bolt! Affect flutter and vibration characteristics ) Repairing or machining of steel hubs and shielding - leaks... Oleo fluid level of rotor blade systems are: rigid, semi-rigid, and inspection! Hydraulic leaks, improper condition and looseness G '' inspection use of a 100 inspection! A business meets BBB accreditation standards in the US and Canada does not accumulate in... 16 ) Trouble shooting and Repairing broken circuits in landing light wiring circuits 43.2 Records! The communication formats UF = 20, 21, and annual inspection is completed on 18 Jul 17, will... S transponders cowlings, and improper attachment Jul 17, when will next. Bending the fuselage a certified mechanic is FAA form ______ the wing or to fixed or control. Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO Repairing or machining of steel hubs absorbing... V @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO blade systems are: rigid,,... Info you add to the main rotor blades changed in a rigid rotor system the,. ) Airframe Major repairs - ( 1 ) Airframe Major repairs - ( 1 ) Airframe Major repairs life means.

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