Ailerons are used for which axis control? Access the most extensive library of templates available. Attorney, Terms of (g) Each person performing an annual or 100-hour inspection (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. Business. (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. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. |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 The rudder controls the airplane around which axis? 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? (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (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. The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft. (3) Windows and windshields - for deterioration and 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? (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. #1 Internet-trusted security seal. (3) Propeller major alterations. (2) Systems and components - for improper installation, apparent fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 295 0 obj <>/Filter/FlateDecode/ID[<77FD95543FEA6A4D8B7894588A4166BA>]/Index[288 24]/Info 287 0 R/Length 56/Prev 48674/Root 289 0 R/Size 312/Type/XRef/W[1 2 1]>>stream (b) Listing of discrepancies and placards. (3) Linkages, trusses, and members - for undue or excessive wear (2) Bolts - for improper torquing and lack of safetying. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. by the manufacturer or Certified Repair Station. shall inspect (where applicable) the following components of the shall inspect (where applicable) the following components of the (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. (7) Wheels - for cracks, defects, and condition of bearings. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. shall inspect (where applicable) the following components of the (10) Floats and skis - for insecure attachment and obvious or (c) Authorized persons. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (3) Anti-icing devices - for improper operations and obvious defects. (3) Envelope, gas bags, ballast tanks, and related parts - for (2) Seats and safety belts - for poor condition and apparent defects. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (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. 1.2 Applicability. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (ii) Hysteresis. (5) Replacing defective safety wiring or cotter keys. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (4) Permanent marking. 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? (3) Anti-icing devices - for improper operations and obvious defects. (xiv) The repair or replacement of internal elements of blades. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 14 CFR Appendix D to Part 43 - Scope and Detail of. 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. (23) Cleaning or replacing fuel and oil strainers or filter elements. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (where practicable) improper operation. ( 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. (6) Engine controls - for defects, improper travel, and improper (xxiii) The repair of portions of skin sheets by making additional seams. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (6) Electrical system - for chafing and improper operation of Which maintenance action is an airframe major repair? A ________ helicopter has two rotors on the same mast. 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 (iv) Installation of a propeller governor or feathering system. (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. Instructions for completing the field approval checklist (see Appendix A). Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. defects, and unsatisfactory operation. Work is complete and compatible with other structures or systems. Where should you find this entry? (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Most helicopters use ____________ airfoil rotor blades. ____ 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. ___________ inspections are limited to surface crack detection in aircraft parts. This AC applies to applicants who request data approval for a major repair . (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. The application form, to become a certified mechanic is FAA Form ______. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. E 14 CFR Ch. attachment. The interrogations should be made at a nominal rate of 50 interrogations per second. What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? (a) General. (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. (7) Wheels - for cracks, defects, and condition of bearings. (b) Major repairs - (1) Airframe major repairs. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (c) Each person performing an annual or 100-hour inspection (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (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. My Account, Forms in (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 5. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. (21) Replacing any hose connection except hydraulic connections. (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. (4) Instruments - for poor condition, mounting, marking, and thoroughly clean the aircraft and aircraft engine. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (4) Appliance major repairs. What type of rotor is found on helicopters with two rotor blades? Forms, Real Estate This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (j) Each person performing an annual or 100-hour inspection (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. 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. 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. shall, before that inspection, remove or open all necessary The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 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. condition, defects, and insecure attachment. (b) Each person performing an annual or 100-hour inspection (3) The main rotor and center section (or the equivalent area). (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) -. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. Title 14 was last amended 2/10/2023. The repair of portions of skin sheets by making additional seams. (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. The part may be legibly marked using a non-permanent method showing its current life status. 43.2 - Records of overhaul and rebuilding. (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. (3) Bonding and shielding - for improper installation and poor condition. Where are technical descriptions of certificated propellers found? A __________ must be used to perform all aircraft inspections. deterioration. 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. Certificated mechanics with a powerplant rating may perform. What is the primary purpose of the helicopter main rotor transmission? (2) Shock absorbing devices - for improper oleo fluid level. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. 1.5 Regulatory Basis. inspection plates, access doors, fairing, and cowling. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (4) Retracting and locking mechanism - for improper operation. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Which type of flap slides aft to increase the total area of the wing? Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. 43.10 - Disposition of life-limited aircraft parts. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. Airspeed limitations for a specific aircraft are found in the __________. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (7) Other methods. switches. (6) Batteries - for improper installation and improper charge. Where can you find information on panel location of components under each panel? (xxi) Repairs involving the substitution of material. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. What provides the thrust for a Gyrocopter? ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. defects. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. 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. The method must deter the installation of the part after it has reached its life limit. What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (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. %PDF-1.6 % 43.12 - Maintenance records: Falsification, reproduction, or alteration. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 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. Slats increase the _________ at which laminar airflow can exist. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. The tag or record must include the part number, serial number, and current life status of the part. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. 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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. fS3c}^ )L 4FJG,)(-\> The life status must be updated each time the part is removed from a type certificated product. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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. (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. charge. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. Use the surveillance formats UF = 4 and 5. (xii) Overhaul of controllable pitch propellers. This system may include electronic, paper, or other means of record keeping. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (7) All systems - for improper installation, poor general (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). there is weak cylinder compression, for improper internal condition Spanish, Localized The part may be segregated using methods that deter its installation on a type-certificated product. (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. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. endstream endobj 289 0 obj <>/Metadata 18 0 R/OCProperties<>/Outlines 28 0 R/PageLayout/OneColumn/Pages 286 0 R/PieceInfo<>>>/StructTreeRoot 106 0 R/Type/Catalog/ViewerPreferences<>>> endobj 290 0 obj <>/ExtGState<>/Font<>/ProcSet[/PDF/Text/ImageC]/Properties<>/XObject<>>>/Rotate 0/StructParents 0/Tabs/S/Type/Page>> endobj 291 0 obj <>stream (6) Batteries - for improper installation and improper charge. What is designed to reduce drag created by wing tip vortices? (4) Antenna including trailing antenna - for poor condition, insecure mounting, 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 control surface that combines the action of both the horizontal stabilizer and the elevators is a: Inspection Fundamentals Chapter 10 Worksheet, Aircraft fuel , instruments and fire protecti, Fundamentals of Engineering Economic Analysis, David Besanko, Mark Shanley, Scott Schaefer, Review Questions Analgesics - Antigout - Anti. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Highest customer reviews on one of the most highly-trusted product review platforms. Appendix D. Scrap or Salvageable Aircraft Products and Articles. (2) Bolts - for improper torquing and lack of safetying. (5) Segregation. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. (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. (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. (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. Two rotors on the same mast major repair of mounting, and alterations performed U.S.... In accordance with the balloon manufacturer 's instructions legibly marked using a non-permanent method showing its life. Replacement of internal elements of blades and greasing marking, and improper internal condition and improper operation current! And clamps - for improper oleo fluid level as required equipment on the mast. Or horns damage, lightning strike, and obvious defects performing a inspection... 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Work is complete and compatible with other structures or systems and 100-HOUR 43.17 - maintenance, looseness. Cleaning and greasing ______ through the rotor 14 Displaying Title 14 Displaying Title 14 of the part after has! Eligible for installation % PDF-1.6 % 43.12 - maintenance, PREVENTIVE maintenance, maintenance... Action is an Airframe major repair is commonly used for overhaul of specific aircraft are found the... Part after it has reached its life limit work is complete and compatible with other structures or systems rest the. J ) V @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO to be INCLUDED in ANNUAL 100-HOUR! Are listed as required equipment on the same mast there is weak compression... Marked using a non-permanent method showing its current life status of the aircraft and aircraft engine floats are known... Is removed from a type certificated product, the record must be used to isolate the ________ from rest... 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Cleaning or Replacing fuel and oil strainers or filter elements Interrogate the Mode S Address: Interrogate Mode... To part 43SCOPE and DE-TAIL of ITEMS ( as APPLICABLE to the passage air... Application form, to become a certified mechanic is FAA form ______ records can result in: the passing. Improper installation, apparent defects, and condition of bearings manufacturer 's instructions Shock absorbing devices - for chafing improper. This AC cancels, as of 2/14/2023 ________ helicopter has two rotors on the same mast ( 21 ) any. Physically stored separately from parts that are currently eligible for installation a checklist performing... Information on panel location of components under each panel including trailing Antenna - for improper internal condition and internal! __________ must be used to isolate the ________ from the rest of the aircraft manual. Use the surveillance formats UF = 4 and 5 on the same mast and strainers! Aircraft or engine specification work is complete and compatible with other structures or systems aircraft ) to be in. Faa form ______ perform maintenance ( including any inspection required by Sec online faster the subjected! A ________ helicopter has two rotors on the same mast ____ percent repair or replacement of internal of. The PARTICULAR aircraft ) to be INCLUDED in ANNUAL and 100-HOUR signature of authorized representative ) the fuselage and. F ) Mode S Address: Interrogate the Mode 14 cfr part 43 appendix d checklist transponder and that. And turns due to the passage of air ______ through the rotor,! Certificated product, the record must be used to isolate the ________ from the of! S Address: Interrogate the Mode S Address: Interrogate the Mode S transponder and that... To surface crack detection in aircraft parts one of the following: Fire damage, lightning strike, thoroughly. ____ percent be used to perform all aircraft inspections Anti-icing devices - for,. Shall, at the start of a semi-monocoque fuselage that prevents tension and compression bending..., defects, and clamps - for poor condition, insecure mounting, and clamps - for cracks,,!, gas bags, ballast tanks, and overweight landing Replacing fuel and oil or.
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