Decrease engine output RPM to optimum rotor RPM. (2) Bolts - for improper torquing and lack of safetying. Which of the following contains a minimum checklist for a 100 hour inspection? 2115 0 obj <>stream 14 CFR 43.15 - Additional performance rules for inspections. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. component operation. . (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (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. Aircraft Specifications or Aircraft Type Certificate Data Sheet. SOURCE: Docket No. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (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). 4. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. (6) Mutilation. (3) Anti-icing devicesfor improper oper- Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (3) Anti-icing devices - for improper operations and obvious defects. (5) Flexible vibration dampeners - for poor condition and deterioration. insecure attachment, improper component installation, and improper (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Aircraft inspection checklists must be FAA approved. 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 interrogations per second to avoid possible ATCRBS interference. The most common method of aircraft inspection is ____________. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. shall inspect (where applicable) the following components of the . (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (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. (3) Linkages, trusses, and members - for undue or excessive wear The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. operation. Business. 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. An aircraft Type Certificate Data Sheet contains. condition, apparent and obvious defects, and insecurity of (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 7572; 49 U.S.C. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (2) The date of the inspection and aircraft total time in service. (2) Studs and nuts - for improper torquing and obvious Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 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 -. (b) Rotorcraft. that is not otherwise covered by this listing for improper (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. shall inspect (where applicable) all components and systems that (e) Approval requirements. (2) Seats and safety belts - for poor condition and apparent defects. (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. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (a) Definitions used in this section. If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. (a) Maintenance record entries. (7) Wheels - for cracks, defects, and condition of bearings. 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? The part may be mutilated to deter its installation in a type certificated product. (ix) Hydraulic and electrical actuating system of components. 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. (6) Electrical system - for chafing and improper operation of switches. 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? 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. (5) Flight and engine controls - for improper installation and (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. attachment. Where is the throttle typically located on a helicopter? gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection 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 Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. He shall Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. (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. (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. (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 -. 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. Inspection programs for aircraft operating under 21.191 (d) and (e) (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. The maximum time a 100 hour inspection can be extended is ______________. Ailerons are used for which axis control? 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. There is a _________ of lift between the advancing helicopter blade and the retreating blade. (iii) Installation of an accessory which is not approved for the engine. AC. 14 CFR Appendix D to Part 43 - Scope and Detail of. #1 Internet-trusted security seal. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (3) The main rotor and center section (or the equivalent area). 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