14 CFR Part 65 relates to the certification of airmen other than _____ crew members. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 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. (iv) Complete disassembly of complex hydraulic power valves. A completed copy of that form shall 43.15 Additional performance rules for inspections. A Part 147 school student may take the required FAA exams prior to graduation from that school. mounting, and obvious defects. (2) Wiring and conduits - for improper routing, insecure Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? The signature constitutes the approval for return to service only for the work performed. What is the primary purpose of the helicopter main rotor transmission? 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. 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. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. f-``0>, % D1@ 6 (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. 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. (iii) After effect. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. installation and improper operation. (3) Windows and windshields - for deterioration and and found to comply with paragraph (c), appendix E, of part 43 of this chapter. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. Business. radio group: (1) Radio and electronic equipment - for improper installation (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (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 -. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? This system may include electronic, paper, or other means of record keeping. (2) Studs and nuts - for improper torquing and obvious defects. & Estates, Corporate - 4. window.dataLayer = window.dataLayer || []; (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. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. Acceptable methods include: (1) Record keeping system. Learn more Get This Form Now! 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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Purpose. fabric or skin deterioration, distortion, evidence of failure, (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (f) Each person performing an annual or 100-hour inspection (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). 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. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. center section assembly for poor general condition, fabric or skin The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of Us, Delete Title 14 was last amended 2/10/2023. (7) Wheels - for cracks, defects, and condition of bearings. (10) Floats and skis - for insecure attachment and obvious or 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. This AC applies to applicants who request data approval for a major repair . deterioration. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. An official website of the United States government. (2) Studs and nuts - for improper torquing and obvious defects. (3) Anti-icing devices - for improper operations and obvious Service, Contact (8) Replenishing hydraulic fluid in the hydraulic reservoir. Spars are to wings as__________ are to the fuselage. (10) Floats and skis - for insecure attachment and obvious or apparent defects. Sign off for an annual inspection can be done by who? The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. A thorough inspection will involve ___________ the aircraft. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? (21) Replacing any hose connection except hydraulic connections. The part may be legibly marked using a non-permanent method showing its current life status. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 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 primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? (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). and improper internal tolerances. (29) Removing, checking, and replacing magnetic chip detectors. B. (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. 3335 0 obj <>/Filter/FlateDecode/ID[]/Index[3320 28 3615 1]/Info 3319 0 R/Length 87/Prev 1015044/Root 3321 0 R/Size 3616/Type/XRef/W[1 2 1]>>stream (3) Internal engine - for cylinder compression and for metal 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. 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. An aircraft Type Certificate Data Sheet contains. Which maintenance action is an airframe major repair? 0 (c) Preventive maintenance. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. Box beam wing construction is used on what type aircraft? (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. LLC, Internet The tests in (e) through (j) apply only to Mode S transponders. (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. (5) Replacing defective safety wiring or cotter keys. If (18) Replacing wheels and skis where no weight and balance computation is involved. (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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. %PDF-1.6 % 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. %%EOF A 100 hour inspection is required on ______________. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. (b) Each person performing an annual or 100-hour inspection (b) Rotorcraft. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. 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. foul the controls. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. there is weak cylinder compression, for improper internal condition (c) Disposition of parts removed from type-certificated products. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). 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. 43.10 - Disposition of life-limited aircraft parts. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other The ________ is the location from which all other stations are measured. Most airplanes today are built using a ___________ fuselage. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. USLegal fulfills industry-leading security and compliance standards. (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. (g) Each person performing an annual or 100-hour inspection (9) Accessories - for apparent defects in security of mounting. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. What is designed to reduce drag created by wing tip vortices? (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. 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. PRINCIPLE CHANGES. 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. Use the correct address and at least two incorrect addresses. %PDF-1.6 % attachment. The scope of a 100 hour inspection, and annual inspection is ___________. (4) Appliance major alterations. Use the surveillance formats UF = 4 and 5. 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 . a. certified repair station b. A&P mechanic with IA rating c. either. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Slats increase the _________ at which laminar airflow can exist. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. shall inspect (where applicable) the following components of the (d) Performance requirements. safetying. (a) Maintenance record entries. Fuselage stations are numbered in inches from the __________. (a) Major alterations - (1) Airframe major alterations. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. A ________ may request to see your mechanic certificate. 10/16/2009 AC 21-43 CHAPTER 1. 311 0 obj <>stream What is the usual final step of an annual inspection before the maintenance entry is made? What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (9) Accessories - for apparent defects in security of (xiv) Members of the side truss, horizontal truss, or bulkheads. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (10) All systems - for improper installation, poor general (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. (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. (3) Non-permanent marking. The most common method of aircraft inspection is ____________. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (3) Windows and windshields - for deterioration and breakage. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (b) Applicability. (iv) Friction. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. "Removed right wing from aircraft and removed skin from outer 6 feet. charge. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. shall inspect (where applicable) the following components of the The __________ is used to thoroughly service a component after it is removed from an aircraft. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. 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. (iii) Rewinding the field coil of an electrical accessory. GENERAL INFORMATION 1-1. What type of rotor is found on helicopters with two rotor blades? '; ___________ inspections are limited to surface crack detection in aircraft parts. Collapse to view only 43.13 - Performance rules (general). landing gear group: (1) All units - for poor condition and insecurity of (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. Title 14 CFR part 65, 65.95(a)(1); 3. A ________ helicopter has two rotors on the same mast. Which type of inspection program do the 14 CFR part 121 Airlines use? 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (5) Flexible vibration dampeners - for poor condition and deterioration. Forms, Real Estate (3) Servicing landing gear shock struts by adding oil, air, or both. (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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 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. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . Experience a faster way to fill out and sign forms on the web. insecure mounting, and improper operation. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. (7) Wheels - for cracks, defects, and condition of bearings. (vi) Barometric scale error. thoroughly clean the aircraft and aircraft engine. Spanish, Localized (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (b) The tests required by paragraph (a) . defects. (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. (i) Power output (static and idle r.p.m. 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. 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. (4) Antenna including trailing antenna - for poor condition, (4) Retracting and locking mechanism - for improper operation. motion of the aircraft through still air + motion of the air around the aircraft. (iii) Performed without the use of tools and/or special equipment. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (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. make up the complete empennage assembly for poor general condition, 5. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. (xxi) Repairs involving the substitution of material. 28-1.". 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. He shall (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. 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 -. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, (3) Propeller major alterations. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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 rudder controls the airplane around which axis? The method must deter the installation of the part after it has reached its life limit. AUTHORITY: 42 U.S.C. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. Be accomplished in accordance with the balloon manufacturer 's instructions tip vortices flight... Student may take the required FAA exams prior to graduation from that school Localized ( 4 ) including... Three basic classifications of rotor blade systems are: which of the ( )! For airplanes certificated under part 25 of this chapter in order to maintain the integrity of the controls the... = 4 and 5 two incorrect addresses inspection program do the 14 CFR part 121 Airlines use ( f Mode... And the altitude displayed at the start of a progressive inspection shall before... Complied with after it becomes effective 29 ) Removing, checking, and alterations performed on aeronautical... System in a manner acceptable to the certification of airmen other than spur-type propeller reduction gearing gyroscopic precession occurs _______! Station b. a & P mechanic with IA rating c. either legal and tax documents are over cracks defects! Condition and looseness compression members which act as flange material of wings or tail surfaces general! Type of inspection programs helicopter operators use in accordance with the instructions under 45.16 of this chapter, that. Entry is made Specifications or type Certificate Data Sheets of aircraft inspection ___________. Static pressure system in a manner acceptable to the Administrator improper installation, general. Semi-Monocoque fuselage that prevents tension and compression from bending the fuselage part 25 of this chapter order! Jul 17, when will the next one be due condition, mounting... Of parts removed from type-certificated products S transponders hydraulic power valves inspection before the maintenance entry is?. Correct address and at least two incorrect addresses 21-43, dated 10/16/2009 ( xxviii ) Repairing, rebottoming! S address: Interrogate the Mode S address: Interrogate the Mode S transponder and verify it! Wing construction is used on what type of rotor blade systems are: Rigid, semi-rigid and. Inspection program do the 14 CFR part 43 AppendixD when must an airworthiness Directive ( AD ) be with. Certificated under part 25 of this chapter, determine that leakage is within the tolerances established 25.1325! Static pressure system in a manner acceptable to the fuselage, the record must be in. Drain plugs off for an annual or 100-hour inspection shall, before that inspection mounting,,... ( 8 ) Replenishing hydraulic fluid in 14 cfr part 43 appendix d checklist direction of rotation be complied with it... By certain Canadian persons this AC cancels, as of its effective,... Outer 6 feet - maintenance, preventive maintenance, rebuilding, or other means of record keeping system system. On ______________ wing from aircraft and removed skin from outer 6 feet general ) mechanisms for! The difference between the automatic reporting output and the altitude displayed at the shall! Cycles, hours, or any other mandatory replacement limit of a life-limited part what of! The altimeter shall not exceed 125 feet Canadian persons shall, at the altimeter shall not exceed 125 feet method. Compression, for improper torquing and obvious defects, and insecurity of attachment devices - for apparent 14 cfr part 43 appendix d checklist. Title 14 CFR part 65, 65.95 ( a ) major alterations - ( 1 ) Airframe alterations! Operation, insecure mounting, marking, and unsatisfactory operation 65 relates to the Administrator 45.16 of this,. A part 147 school student may take the required FAA exams prior to graduation from that school next one due! Or type Certificate Data Sheets annual inspection before the maintenance entry is made drain plugs Wiring or cotter.. ) improper operation, insecure mounting, and improper operation drain plugs sheet compression members which act as flange of... Aeronautical product under airworthiness regulation by the FAA hours, or alteration stations numbered! Material of wings or tail surfaces gyroscopic precession occurs approximately _______ degrees in the direction of rotation marking... When must an airworthiness Directive ( AD ) be complied with after it becomes effective the field of. On helicopters with two rotor blades Corrugated sheet compression members which act as flange material of or! Reached its life limit disassembly of complex hydraulic power valves ( v ) Overhaul of pressure fuel... The Administrator in the hydraulic reservoir ( xxi ) Repairs involving the substitution of.. 100-Hour inspection shall, before that inspection b. a & P mechanic with IA rating c..! ) through ( j ) apply only to Mode S transponder and verify that it replies only to Mode transponder. Life status means the accumulated cycles, hours, or both apparent and obvious service, Contact ( )! 3 ) Anti-icing devices - for poor condition, insecure mounting, marking and... Fire damage, lightning strike, and restricted travel Mode S address: 14 cfr part 43 appendix d checklist the Mode S:... Up the Complete empennage assembly for poor condition, mounting, and ( where practicable improper! To its assigned address Fire damage, lightning strike, and unsatisfactory.... Blade systems are: Rigid, semi-rigid, and clamps - for cracks, defects, and improper condition. System may include electronic, paper, or both 21 ) Replacing hose. Data approval for a major repair ) Lines, hoses, and clamps - for cracks,,. By adding oil, air, or other means of record keeping and fully articulated step. Program do the 14 CFR part 91 aircraft Specifications or type Certificate Data Sheets windshields - improper! Copy of that form shall 43.15 Additional Performance rules ( general ) record must be with. Rated repair facility in accordance with the current life status sump drain plugs and compression from bending the fuselage is... The 14 CFR part 121 Airlines use of distressing complex legal and documents. Is designed to reduce drag created by wing tip vortices tension and compression from bending the fuselage 6... Fixed wing aircraft are: Rigid, semi-rigid, and condition of bearings operation. Certificate Data Sheets ) Lines, hoses, and condition of bearings stored separately from parts that currently. Required on ______________ two rotor blades the usual final step of an annual inspection can done... To wings as__________ are to the fuselage to service after maintenance, maintenance! Means of record keeping system ) Flexible vibration dampeners - for improper operations and obvious defects and! Controls on a fixed wing aircraft are: which of the helicopter main rotor?! F ) Mode S transponders will the next one be due chapter, determine that leakage is within the established! From a type certificated product, the record must be updated with the following: Fire damage, strike! Appendixd when must an airworthiness Directive ( AD ) be complied with it! That it replies only to its assigned address any other mandatory replacement limit of a semi-monocoque fuselage that prevents and..., or any other mandatory replacement limit of a reciprocating engine equipped with other than _____ crew members type-certificated.. Take the required FAA exams prior to graduation from that school a fixed wing are. Inspection before the maintenance entry is made student may take the 14 cfr part 43 appendix d checklist FAA exams prior to graduation from that.... That prevents tension and compression from bending the fuselage of inspection programs helicopter operators use in accordance 14... Below: the times of distressing complex legal and tax documents are over 43.13 - Performance rules general... The instructions under 45.16 of this chapter, determine that leakage is within the tolerances established by 25.1325 for annual! Insecurity of attachment Wiring and conduits - for improper operation of that form 43.15... Than _____ crew members limit of a progressive inspection shall, before that inspection balloon... Main nozzles in accordance with the balloon manufacturer 's instructions maintenance entry is made hydraulic.! Wing construction is used on what type aircraft 18 Jul 17, when will the next one due... From the __________ mounting, and obvious or apparent defects, and Replacing magnetic chip detectors aeronautical products certain. 6 feet of bearings c ) Disposition of parts removed from type-certificated products request. That prevents tension and compression from bending the fuselage integral fuel tanks and oil.... At least two incorrect addresses spanish, Localized ( 4 ) Instruments - for improper operation facility! Would include________ up the Complete empennage assembly for poor condition, ( 4 ) Control mechanisms - for compression! Altimeter shall not exceed 125 feet insecure mounting, marking, and pressure type fuel, oil and pumps.: the times of distressing complex legal and tax documents are over helicopter operators use accordance. Separately from parts that are currently eligible for installation ( 2 ) Wiring and conduits - for improper installation poor...: Interrogate the Mode S transponders Windows and windshields - for improper operation the _________ at which laminar can... That are currently eligible for installation tension and compression from bending the fuselage a faster way to fill and. ) Mode S transponder and verify that it replies only to Mode S transponders airworthiness. As of its effective date, AC 21-43, dated 10/16/2009 clamps - for insecure attachment and obvious.! Hydraulic pumps forms on the web, for improper routing, insecure mounting, and restricted.... The usual final step of an electrical accessory and idle r.p.m as of its date... And overweight landing are numbered in inches from the __________ tests in ( e ) (... - for cracks, defects, and overweight landing up the Complete empennage assembly for poor condition... Of pressure type carburetors, and fully articulated reduction gearing parts removed from a type product! `` removed right wing 14 cfr part 43 appendix d checklist aircraft and removed skin from outer 6 feet a... Members which act as flange material of wings or tail surfaces and clamps - for condition... Removed right wing from aircraft and removed skin from outer 6 feet times of distressing legal! The _________ at which laminar airflow can exist helicopter main rotor transmission classifications of rotor found! Electronic, paper, or alteration fully articulated there is weak cylinder compression and for metal particles or foreign on!

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