Propeller & Powerplant Aircraft PDF

Summary

This document contains questions and answers about aircraft maintenance, including propeller and powerplant components. It covers various aspects of repair and alteration, categorized by different sections like appliance, airframe, and powerplant.

Full Transcript

Propeller & Powerplant Propeller & Powerplant (Aircraft) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger is an example of a. Powerplant Major Repair b. Powerplant Minor Alteration c. Powerplant Minor Repair Any maintenance op...

Propeller & Powerplant Propeller & Powerplant (Aircraft) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger is an example of a. Powerplant Major Repair b. Powerplant Minor Alteration c. Powerplant Minor Repair Any maintenance operation requiring of the cold and hot sections a. Powerplant major alterations b. Powerplant major repair c. Preventive maintenance Special repair to structural engine parts by welding, plating, metalizing or other methods is an example of ( Parts IS 5.5.5. 12) a. Powerplant major alterations b. Powerplant major repair c. Preventive maintenance Change to the Hub Design is? a. Powerplant minor repair b. Propeller Major Modification c. Propeller Major Repair Removal of accessories that are listed as required equipment on the aircraft or engine specifications is an example of a. Powerplant Major Modification b. Powerplant Major Repair c. Appliance Major Modification Conversions of any sort for the purpose of using fuel rating or grade other than listed in the engine specifications (Part IS 5.1.1.2 ) a. Airframe major alterations b. Powerplant major repair c. Powerplant major modification Installation of an accessory which is not approved for the engine is an example of a. Powerplant major modification/alteration b. Powerplant major repair c. A preventive maintenance Changes to the basic design of or the relocation of brackets or braces of the propeller control are considered ans. propeller minor repair Maintenance operation requiring disassembly of non-float type carburetor is classified as ans. powerplant major repair Special repair to structural engine part by weighing or other methods is considered as ans. powerplant major repair Installation of propeller de-icing is considered as ans. propeller major alteration Replacing a carburetor with the same type as specified by the manufacturer is considered as ans. powerplant major alteration Repair to deep dents, cut, scar, nicks, etc. on the propeller considered as ans. propeller major alteration Maintenance operation such as assembly and disassembly of ground adjustable propeller is considered ans. propeller minor repair Changes of engine cowling which do not effect engine cooling, such as revision to the mounting bracket attachment is considered ans. powerplant minor alteration Appliance Rewinding the field coil of an electrical accessories is an example of? a. Airframe Minor repair b. Appliance Major Repair c. Airframe Minor Alteration Replacement of an autopilot with parts manufactured with approved drawing is considered a. Appliance major repair b. Accessory major repair c. Component minor repair d. Airframe minor repair Calibration and repair of instruments is an example of (Part IS.5.1.12)? a. Appliance major alterations b. Appliance major repair c. Components major repair Modification of the basic design not made in accordance with the recommendations of the appliance manufacturer or in accordance with applicable airworthiness directives is considered as (Part IS 5.1.12) a.Appliance major repair b.Airframe major alterations c.Appliance major modification Change in the basic design made in accordance with the “ASSEC” of the air transportation approved recommendation of the “Landing gear shock strut” manufacturing or in accordance with ATO airworthiness directives are considered to be a. Appliance minor alteration b. Appliance major alteration c. Airframe major alteration Overhaul of pressure type carburetor mechanical accessories is considered as ans. appliance major repair Repair operation on hydraulic/pneumatic accessories, complete disassembly of complex hydraulic/ pneumatic power valves if repairable, per manufacturer’s instruction are classified as ans. appliance major alteration Any change to the basic design of navigational equipment approved under type certificate is classified as ans. an appliance major alteration Airframe The restoration of an engine mounts to a condition for safe operation after damage is classified as a. An airframe major repair b. A powerplant major repair c. A powerplant major alteration Strengthening or reinforcing the fuselage longeron. a. Airframe major alteration b. Airframe minor modification c. Airframe major repair Changes of the following type to a powerplant, or airframe when not listed in the specifications issued by the Air Transportation office in accordance with the manufacturer, are considered a. Powerplant major repair b. A powerplant major alteration c. Aircraft major alteration d. An airframe major alteration Modification to basic design of the exhaust system is considered a. Aircraft major alteration b. Airframe major alteration c. System major alteration d. Powerplant major alteration Changes to the basic design of the fuel or oil system is considered a. Airframe major modification b. A preventive maintenance c. Airframe minor modification Replacement of components or complete units such as landing gears with parts supplied by the original manufacturer or manufactured in accordance with approved drawings is considered a. Component minor repair b. Airframe minor repair c. Components major repair Repair made on the hydraulic/pneumatic system is considered a. An accessory minor repair b. A preventive maintenance c. An airframe major repair d. An airframe minor repair Changes made to structural elements for the purpose of improving the service life or reducing maintenance cost, but that the cumulative weight changes of all such maintenance work done since the aircraft was re-weight or the weight and balance data re-compared do not exceed two percent of the certificate empty weight on aircraft under 12,500 pounds gross weight is classified as a. Airframe minor repair b. Airframe major alterations c. Airframe minor alterations d. Aircraft major alterations Any repair to spare ribs, and surface involves ans. airframe minor repair techniques The installation or removal of equipment of equal or less weight and in the same location as the last listed as optional equipment in the aircraft specification is ans. an airframe minor alteration Preventive maintenance Replacing defective safety wiring or cotter pins is a. Progressive maintenance b. Airframe minor repair c. Routine maintenance d. Preventive maintenance A simple minor preservations and the replacement of small standard parts not involving complex assembly operations is classified as a. Airframe major repair b.Routine maintenance alteration c.Preventive maintenance d. Airframe minor repair Replacing defective safety wiring or cotter pins is a. Progressive maintenance b. Preventive maintenance c. Routine maintenance Replacing or cleaning spark plugs and setting of sparkplug gap clearance is considered as (Part IS 5.1.12) a.Preventive maintenance b.Powerplant major alterations c. Powerplant major repair Making simple fabric pitches not required rib stitching or removal of structural parts control surfaces is considered as ans. preventive maintenance Troubleshooting and repairing broken circuit in landing light wiring circuit is considered as. ans. preventive maintenance CFR The issuance of an Airworthiness Certificate is governed by a. 14 CFR Part 23 b. 14 CFR Part 21 c. 14 CFR Part 39 Which regulation provides the airworthiness standards for an airplane certificated in the normal category? a. 14 CFR Part 27 b. 14 CFR Part 25 c. 14 CFR Part 23 Which regulation provides information regarding instrument range markings for an airplane certificated in the normal category? a. 14 CFR Part 21 b. 14 CFR Part 25 c. 14 CFR Part 23 Each person performing an annual or 100-hour inspection shall use a checklist that contains at least those items in the appendix of a. 14CFR Part 43. b. 14CFR Part 65. c. AC 43.13-3. Where would find the recommended statement for recording the approval or disapproval of an aircraft after a 100 hour or annual inspection a.14 CFR Part 43 b.14 CFR Part 65 c. 14 CFR Part 91 What part of the Federal Aviation Regulations prescribes the requirements for issuing mechanic certificates and associated ratings and the general operating rules for the holders of these certificates and ratings? a. 14 CFR Part 43 b. 14 CFR Part 91 c. 14 CFR Part 65 Where would you find the operating conditions that make a 100-hour inspection mandatory? a.14 CFR Part 91 b.14 CFR Part 43 c.AC 43.13-2A Which of the FF Which of the following may a certificated airframe and powerplant mechanic perform on aircraft and approve for return to service? 1. A 100-hour inspection 2. An annual inspection, under specified circumstances 3. A progressive inspection, under specified circumstances a. 1,2 b. 1,3 c. 1,2,3 An aircraft owner was provided a list of discrepancies on an aircraft that was not approved for return to service after an annual inspection. Which of the following statements is/are true concerning who may correct the discrepancies? 1. Only a mechanic with an inspection authorization 2. An appropriately rated mechanic 3. Any certified repair station a. 2&3 b. 2 c. 1 What is /are the appropriate action (s) concerning minor repairs performed on a certificated aircraft? 1. FAA form 337’s must be completed 2. Entries must be made in the aircraft maintenance record. 3. The owner of the aircraft must submit a record of all minor repairs to the FAA at least annually. a. 2. b. 2 and 3. c. 1 and 2 (1) Propellers are NOT included in the Airworthiness Directive system. (2) A certificated powerplant mechanic may make a minor repair on an aluminum propeller and approve for return to serviceRegarding the above statements, a. Only No.2 is true b. Both No.1 and No.2 are true c. Neither No.1 nor No.2 is true (1) The Federal Aviation Regulations require approval after compliance with the data of a Supplemental Type Certificate (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft Regarding the above statements, a. Only No.2 is true b. Neither No.1 nor No.2 is true c. Only No.1 is true (1) Manufacturer’s data and FAA publications such as Airworthiness Directives, Type Certificate Data Sheets, and advisory circulars are all approved data (2) FAA publications such as Technical Standard Orders, Airworthiness Directives, Type Certificate Data Sheets, and Aircraft Specifications and Supplemental Type Certificates are all approved data Regarding the above statements, a. Both No.1 and No.2 are true b. Only No.1 is true c. Only No.2 is true The Air Transport Association of America (ATA) Specification No. 100 (1) establishes a standard for the presentation of technical data in maintenance manuals. (2) Divides the aircraft into numbered systems and simplify locating maintenance instructions. Regarding the above statements, a. Both No.1 and No.2 are true b. Neither No.1 nor No.2 is true c. Only No.1 is true (1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement. (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. Regarding the above statements, a. Both No.1 and No.2 are true b. Neither No.1 nor No.2 is true c. Only No.1 is true The action required by an AD may take what form? 1. Inspection 2. Part(s) replacement 3. Design modification 4. Change in operating procedure(s) 5. Overall change in the content, firm and disposition of the aircraft maintenance records. a. 1,2,3 and/or 4 b. 1,2,3 and/or 5 c. 1,2,3,4 and/or 5 Which of the following are sometimes used as authorization to deviate from an aircraft’s original type design? 1. FAA Form 337 2. Supplemental Type Certificate 3. Airworthiness Directives 4. Technical Standard Order a. 1,2,3 and 4 b. 1,2 and 4 c. 1,2 and 3 x(1) Certificated mechanics with an airframe rating may perform a minor repair to an airspeed indicator providing they have the necessary equipment available x(2) Certificated mechanics with a powerplant rating may perform a major repair to a propeller providing they have the necessary equipment available Regarding the above statements, a. Only No. 1 is true b. Neither No.1 nor No.2 is true c. Only No.2 is true Who has the authority to approve for return to service a propeller after a 100-hour inspection? 1. A mechanic with a powerplant rating 2. Any certificated repairman 3. A non-certificated mechanic working under the supervision of a certificated mechanic with airframe and powerplant ratings a. 1 b. 2 c. 1 and 3 Tab 7 Changes of the following type to a powerplant, or airframe when not listed in the specifications issued by the Air transport office in the accordance with the manufacturer a. A powerplant major alteration b. Powerplant major repair c. Aircraft major alteration Which of the following is not considered as power-plant major alteration? ans. disassembly of float type carburetor An example of powerplant major repairs ans. (cylinder removal/piston removal) or all of the above The replacement of a damaged engine mount with a new identical engine mount purchased from the aircraft manufacturer is considered a ans. minor repair The inspection of the main rotor transmission gearbox for obvious defects is included in what kind of inspection ans. major repair inspection The flight test of an aircraft which has undergone major repair is mandatory before it can be returned back to service likewise, this also required after ans. minor repairs as replacement of wing tips Which is not considered an airframe major alteration ans. strengthening or reinforcing the fuselage longeron Changes of the ff. type to a power-plant, or airframe when not listed in the specifications issued by the air transport office in accordance with the manufacturer, are considered ans. aircraft major alteration The replacement of fabric on fabric-covered parts such as wings, fuselages, stabilizers, or control surfaces is considered to be a ans. Major repair even though no other alteration or repair is performed The replacement of a damaged vertical stabilizer with a new identical stabilizer purchased from the aircraft manufacturer is considered a ans. Minor repair

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