inspection plates, access doors, fairing, and cowling. 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. 14 CFR 43.15 - Additional performance rules for inspections. (3) Anti-icing devicesfor improper oper- (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. The pilot, walking around the aircraft A special Inspection may include the following: deterioration. 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. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 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. The test point shall be approached at a rate compatible with the test equipment. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (4) Instruments - for poor condition, mounting, marking, and (c) Annual and 100-hour inspections. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 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. (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. (xv) Main seat support braces and brackets. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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. 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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. (i) Scale error. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. %%EOF
(e) Approval requirements. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. mounting, and restricted travel. (4) Retracting and locking mechanism - for improper endstream
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(1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. 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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 43.15 - Additional performance rules for inspections. (6) Mutilation. 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. (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. (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) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. (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. ); (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. What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? (7) Wheels - for cracks, defects, and condition of bearings. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. ); (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. (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. (a) General. Most helicopters use ____________ airfoil rotor blades. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. Us, Delete (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. (3) The main rotor and center section (or the equivalent area). The method must deter the installation of the part after it has reached its life limit. radio group: (1) Radio and electronic equipment - for improper installation 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 At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. 14 CFR Appendix D to Part 43 - Scope and Detail of. (b) Temporary removal of parts from type-certificated products. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 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". The error at all test points must not exceed the tolerances specified in Table I. (g) Each person performing an annual or 100-hour inspection 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. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Feb 7/2020 . Sign off for an annual inspection can be done by who? What is the usual final step of an annual inspection before the maintenance entry is made? 3320 0 obj
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