(7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. failure, and insecurity of attachment. CFR prev | next A ________ helicopter has two rotors on the same mast. During the next week, create a list of at least 10 things you could have done to conserve the water you use. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. & Estates, Corporate - (v) Installation of structural parts other than the type of parts approved for the installation. (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. How are main rotors of helicopters classified? This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ (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. (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 -. (c) Each person performing an annual or 100-hour inspection (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. USLegal received the following as compared to 9 other form sites. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (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. looseness. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? (a) Maintenance record entries. 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 Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. (2) Bolts - for improper torquing and lack of safetying. Spanish, Localized (3) Bonding and shielding - for improper installation and poor What is the primary purpose of the helicopter main rotor transmission? Most airplanes today are built using a ___________ fuselage. 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". (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. that is not otherwise covered by this listing for improper B. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Learn more ME406 Series Emergency Locator Transmitter - ACR. 43.12 - Maintenance records: Falsification, reproduction, or alteration. 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 (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. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (5) Flexible vibration dampeners - for poor condition and deterioration. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (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. 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. 1.5 Regulatory Basis. A tag or other record may be attached to the part. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Galvanic corrosion is also known as _________ corrosion. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (xii) Overhaul of controllable pitch propellers. 2. Summary of Proposed Rule. (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. 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. fatigue, and distortion. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. (3) Bonding and shielding - for improper installation and poor condition. (7) Wheels - for cracks, defects, and condition of bearings. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. shall inspect (where applicable) all components and systems that shall inspect (where applicable) the following components of the This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. ); (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. looseness of engine to mount. Instructions for completing the field approval checklist (see Appendix A). mounting. This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. (a) Major alterations - (1) Airframe major alterations. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. AC. (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. (b) Rotorcraft. Purpose. No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. He shall thoroughly clean the aircraft and aircraft engine. (21) Replacing any hose connection except hydraulic connections. switches. safetying. (6) Batteries - for improper installation and improper (d) Each person performing an annual or 100-hour inspection Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. fS3c}^ )L 4FJG,)(-\> 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. defects. (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. (xxi) Repairs involving the substitution of material. Enjoy smart fillable fields and interactivity. The life status must be updated each time the part is removed from a type certificated product. 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. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate, The issuance of an Airworthiness Certificate is governed by, Specifications pertaining to an aircraft, of which a limited number were manufactured under a type certificate and for which there is no current Aircraft Specification, can be found in the. %%EOF shall inspect (where applicable) all components of the wing and Most helicopters use ____________ airfoil rotor blades. (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. 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? Every part of an aircraft must be planned to carry the load imposed upon it. 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 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. 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. Ni}Ja7$? A security threat, as defined by the TSA, will result in your mechanic application being _______. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (xiv) Members of the side truss, horizontal truss, or bulkheads. and improper internal tolerances. 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. attachment. (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). Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs.
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