Airlaw and Airworthiness Reviewer Sheet PDF

Summary

This document provides information on aircraft maintenance and inspection procedures. It covers various aspects, including electrical equipment, component replacements, and operating conditions.

Full Transcript

AIRLAW AND AIRWORTHINESS REVIEWER SHEET c. Compliance with an applicable AD is mandatory and must be recorded in the AIRFRAME INSPECTION maintenance r...

AIRLAW AND AIRWORTHINESS REVIEWER SHEET c. Compliance with an applicable AD is mandatory and must be recorded in the AIRFRAME INSPECTION maintenance records 8. Where would you find the operating conditions 1. When overhauling electrical equipment, all that make a 100-hour inspection mandatory? necessary information should be obtained from a. 14 CFR Part 91 a. The aircraft maintenance manual b. 14 CFR Part 43 b. Maintenance instructions published by the c. AC 43.13-2A aircraft and/or equipment manufacturer 9. Which statement is correct regarding an aircraft c. Illustrated parts manual for the aircraft that is found to be unairworthy after an annual 2. Which statement is correct when an aircraft has inspection, due to an item requiring a major not been approved for return to service after an repair (assuming approved to accomplish the annual inspection because of several items repair)? requiring minor repair? a. An appropriately approved mechanic may a. Only the person who performed the annual accomplish the repair, and an IA may inspection may approve the aircraft for return approve the aircraft for return to service to service b. An appropriately rated mechanic or repair b. An appropriately rated mechanic may station may repair the defect and approve the repair the defects and approve the aircraft aircraft for return to service for return to service c. Only the person who performed the annual c. An appropriately rated mechanic may repair inspection may approve the aircraft for return the defects, but an IA must approve the to service, after the major repair aircraft for return to service 10. Large airplane and turbine-powered multiengine 3. An aircraft may be flown beyond the 100-hour airplanes operated under Federal Aviation inspection requirement to reach a place where Regulation Part 91, General Operating and Flight the inspection can be accomplished, provided it Rules, must be inspected a. Does not exceed 10 flight hours a. In accordance with an inspection program b. Has a special flight permit authorized under Federal Aviation c. Does not exceed 15 flight hours Regulation Part 91, Subpart E. 4. Radio equipment installations made in accordance b. In accordance with a continuous with Supplemental Type Certificate data require airworthiness maintenance program (camo approval for return to service program) authorized under Federal Aviation a. By a field approval from the FAA Regulation Part 91, Subpart E b. By an airframe and powerplant mechanic c. In accordance with the progressive inspection c. By the holder of an inspection requirements of Federal Aviation Regulation authorization Section 91.409 (d) 5. For an individual (not a repair station) to conduct 11. The maximum time a 100-hour inspection may be a complete 100-hour inspection on an aircraft and extended is approve it for return to service requires a a. 10 hours mechanic certificates with b. 10 hours with a special flight permit a. An airframe rating only c. 12 hours with a special flight permit b. Airframe and powerplant rating 12. An aircraft that is due an annual inspection may c. Airframe and powerplant ratings with an be flown inspection authorization a. If a special permit has been issued for the 6. Where would you find the recommended aircraft statement for recording the approval or b. For the purpose of performing maintenance disapproval for return to service of an aircraft c. For a period of time not to exceed 10 hours after a 100-hour or annual inspection a. 14 CFR Part 65 MAINTENANCE FORMS AND RECORDS b. 14 CFR Part 43 c. 14 CFR Part 91 1. For aircraft operated under part 91, which of the 7. Which statement about Airworthiness Directives following records must be retained for at least (AD’s) is true one year, or until the work is repeated or a. AD’s are information alert bulletins issued by superseded? the airframe, powerplant or component a. Records of time since overhaul of items manufacturer requiring overhaul on a time specified basis b. Compliance with an AD is not mandatory unless the aircraft affected is for hire b. Records of maintenance, alterations, 7. Which is an appliance major repair? preventive maintenance, 100-hour, annual a. Overhaul of a hydraulic pressure pump and progressive inspections b. Repairs to a propeller governor or its control c. Records of the current inspection status of the c. Troubleshooting and repairing broken circuits aircraft, including time since last required in landing light circus inspections 8. When approving for return to service after a 2. Which of the following may a certificated maintenance or alteration, the approving person airframe and powerplant mechanic perform on must enter in the maintenance record of the aircraft and approve for return to service? aircraft 1. A 100-hour inspection a. The date the maintenance or alteration was 2. An annual inspection, under specified begun, description (or reference to acceptable circumstances data) of work performed, the name of the 3. A progressive inspection, under specified person performing the work (if someone circumstances else), signature and certificate number a. 1,2 b. A description ( or reference of acceptable b. 1,3 data) of work performed, date of completion, c. 1,2,3 the name of the person performing the work 3. If work performed on an aircraft has been done (if someone else), signature and certificate satisfactorily, the signature of an authorized number person on the maintenance records for c. A description (or reference of acceptable maintenance or alterations performed constitutes data) of work performed, date of a. Approval of the aircraft for return to service completion, the name of the person b. Approval for return to service only for the performing the work (if someone else) , work performed signature, certificate number and kind of c. Verification that the maintenance or certificate held alterations were performed referencing 9. Who is responsible for upkeep of the work approved maintenance data required maintenance record of an aircraft? 4. Which aircraft record entry is the best description a. The maintaining repair station or authorized of the replacement of several damaged heli-coils inspector in a casting? b. The maintaining certified aircraft mechanic a. Eight ¼--20 inch standard heli-coils were c. The aircraft owner replaced. The damaged inserts were 10. Which is statement is true regarding the extracted , the tapped holes gaged, then requirements for maintenance record format? new inserts installed, and tangs removed a. Any format that provides record continuity b. Eight ¼--20 inch standard heli-coils were and includes the required information may installed in place of damaged ones be used c. Eight ¼--20 inch standard heli-coil inserts b. The format provided by the manufacturer of were repaired by replacing the damaged the aircraft must be retained inserts with a lock-type insert, after the c. Any desired change from manufacturer tapped holes were checked for corrosions provided format requires approval from the 5. What is the means by which the FAA notifies Federal Aviation Administration aircraft owners and other interested persons of 11. Where should you find this entry? unsafe conditions and prescribes the condition ‘Removed right wing from aircraft and remove under which the product may continue to be skin from outer 6 feet. Repaired buckled spar 49 operated? inches and in figure 8 in the manufacturer’s a. Airworthiness Directives structural repair manual No. 28-1.’ b. Aviation Maintenance Alerts a. Aircraft engine maintenance record c. Aviation Safety Data b. Aircraft minor repair and alteration 6. Which maintenance record entry best describes c. FAA Form 337 the action taken for a.125-inch deep dent in a 12. When a 100-hour inspection is completed, if straight section of 1/2 –inch aluminum alloy separate maintenance records for the airframe, tubing? powerplant(s), and propeller(s) are maintained, a. Dented section removed and replaces with where is the entry for the inspection recorded? identical new tubing flared to 45° a. In each record b. Dent within acceptable limits, repair not b. In the airframe record only necessary c. In any one of the records c. Dented section removed and replaced with identical new tubing flared to 37° 13. When work is performed on an aircraft that a. Two; one copy for the aircraft owner and necessitates the use of FAA Form 337, who should one copy for the FAA prepare the form? b. Two; one coy for the FAA and one copy for the a. The person who performs or supervises the permanent records of the repairing agency or work individuals b. The person who approves for return to c. Three; one copy for the aircraft owner, one service copy for the FAA, and one copy for the c. The aircraft owner or operator permanent records of the repairing agency or 14. A certificated mechanic without an inspection individual authorization who signs the appropriate block on 20. An aircraft owner was provided a list of FAA Form 337 is doing what? discrepancies on an aircraft that was not a. Certifying that he work was done in approved for return to service after an annual accordance with the requirements of 14CFR inspection. Which of the following statements Part 43 is/are true concerning who may correct the b. Approving the work for return to service discrepancies? c. Certifying the maintenance information used 1. Only a mechanic with an inspection as FAA-approved data authorization 15. For the aircraft operated under part 91, what 2. An appropriately rated mechanic difference is there, if any, between the record 3. Any certified repair station entry requirements for maintenance (e.g., repair a. 2&3 or alteration) and the record entry requirements b. 2 for inspections (beyond the description of the c. 1 work performed and the type and extent of 21. Which aircraft record entry best describes repair inspection? of a dent in a tubular steel structure dented at a a. There is no difference cluster? b. Aircraft total time is required to be included a. Removed and replaced the damaged member only in the maintenance entry b. Welded a reinforcing plate over the dented c. Aircraft total time is required to be area included only in the inspection entry c. Filled the damaged area with a molten metal 16. What is the status of data used as a basis of an dressed to the original contour approving major repairs or alternations for 22. During an annual inspection, if a defect is found returning to service? which makes the aircraft unairworthy, the person a. Data must be least FAA-acceptable when it is disapproving must used for that purpose. a. Void the aircraft’s airworthiness certificate b. Data must be FAA-approved prior to its use b. Submit a malfunction defect report for that purpose. c. Provide a written notice of the defect to the c. Data may be FAA-approved after its used for owner that purpose. 23. When a discrepancy list is provided to an aircraft 17. Where is the record of compliance with owner or operator after an inspection, it says in Airworthiness Directives or manufacturer’s effect that service bulletins normally indicated? a. The item inspected is unairworthy a. FAA form 337 b. Except for these discrepancies, the item b. Aircraft maintenance record inspected is airworthy c. Flight manual c. The item inspected may or may not be 18. If more spaces is needed for a work description airworthy depending on the discrepancies entered o FAA Form 337, what information should found be included on the attached sheet (s), in addition 24. For aircraft operated under part 91, when is to the rest of the work description? aircraft total time is required to be recorded in a. Make, model, and serial number of the aircraft maintenance records? aircraft a. After satisfactorily completing maintenance, b. Aircraft nationality and registration mark, preventive maintenance, rebuilding and and the date the work was accomplished alteration (excluding inspection) c. Name, date, and office designator of the FAA b. After satisfactorily completing inspections inspector from the supervising district office c. After satisfactorily completing airframe, 19. After making a certain repair to an aircraft engine component, or propeller maintenance that is to be returned to service, an FAA Form 337 25. For aircraft operated under part 91, which of the is prepared. How many copies are required and following records must be retained and what is the disposition of the completed forms? transferred with the aircraft when it is sold? a. Records of maintenance, alterations, a. Changes to the wing or to fixed or movable preventive maintenance, 100-hour, annual control surfaces which affect flutter and and progressive inspections vibration characteristics. b. Records of inspections performed in b. Rewinding the field coil of an electrical accordance with 14 CFR part 43, Appendix D accessory. c. Records of the current status of applicable c. The repair of portions of skin sheets by AD’s, and date and time when recurring making additional seams. AD’s are next due 32. Which maintenance record entry best describes 26. Which statement is true regarding the use of FAA the action taken for a control cable showing Form 337? approximately 20 percent wear on several of the a. FAA Form 337 is unauthorized for use with individual outer wires at a fairlead? both U.S. and foreign registered aircraft a. Wear within acceptable limits, repair not b. FAA Form 337 is authorized for use with U.S. necessary. registered aircraft, and foreign registered b. Removed and replaced the control cable and aircraft when located in the United States re-rigged the system. c. FAA Form 337 is not authorized for use c. Cable repositioned, worn area moved away with other U.S. registered aircraft from fairlead. 27. An FAA form 337 is used to record and document 33. Who is responsible for making the entry in the a. Preventive and unscheduled maintenance and maintenance records after an annual, 100 hour, special inspections. or progressive inspection? b. Major and minor repairs, and major and a. The owner or operator of the aircraft. minor alterations. b. The person approving or disapproving for c. Major repairs and major alterations. return so service. 28. What is /are the appropriate action (s) c. The designee or inspector representing the concerning minor repairs performed on a FAA Administrator. certificated aircraft? 34. An aircraft was not approved for return to service 1. FAA form 337’s must be completed after an annual inspection and the owner wanted 2. Entries must be made in the aircraft to fly the aircraft to another maintenance base. maintenance record. Which statement is correct? 3. The owner of the aircraft must submit a a. The owner must obtain a special flight record of all minor repairs to the FAA at least permit. annualy. b. The aircraft may be flown without restriction a. 2. up to 10 hours to reach another maintenance b. 2 and 3. base. c. 1 and 2. c. The aircraft becomes a restricted category 29. A person installing a product , part, or appliance type until it is approved for return to service. on a type certificated product must make certain 35. In order to reconstruct lost or destroyed aircraft that the item’s records document what type of maintenance records, what is it necessary to statement? establish? a. The product, part, or materials meets FAA a. Dates of all maintenance, preventive airworthiness standards. maintenance and alterations. b. A product produced by an owner or operator b. Dates and/ or times of all 100-hour, annual, does not need a statement. or progressive inspections. c. The product or material was not produced c. Total time-in-service of the airframe. under an FAA production approval. 36. Each person performing an annual or 100-hour 30. After a mechanic holding an airframe an inspection shall use a checklist that contains at powerplant rating completes a 100-hour least those items in the appendix of inspection, what action is required before the a. 14CFR Part 43. aircraft is returned to service? b. 14CFR Part 65. a. Make the proper entries in the aircraft’s c. AC 43.13-3. maintenance record. b. An operational check of all systems. MAINTENANCE PUBLICATIONS c. A mechanic with an inspection authorization 1. (1) Propellers are NOT included in the must approve the inspection. Airworthiness Directive system. 31. Which maintenance action is an airframe major (2) A certificated powerplant mechanic may make repair? a minor repair on an aluminum propeller and approve for return to service Regarding the above statements, c. Aircraft Specifications or Type Certificate a. Only No.2 is true Data Sheets b. Both No.1 and No.2 are true 9. Aviation Maintenance Alerts (formerly General c. Neither No.1 nor No.2 is true Aviation Airworthiness Alerts) 2. (1) The Federal Aviation Regulations require a. Provide mandatory procedure to prevent or approval after compliance with the data of a correct serious aircraft problems Supplemental Type Certificate b. Provide information about aircraft (2) An installation of an item manufactured in problems and suggested corrective actions accordance with the Technical Standard Order c. Provide temporary emergency procedures system requires no further approval for until Airworthiness Directives can be issued installation in a particular aircraft 10. What is the maintenance recording responsibility Regarding the above statements, of the person who complies with an a. Only No.2 is true Airworthiness Directive? b. Neither No.1 nor No.2 is true a. Advise the aircraft owner/operator of the c. Only No.1 is true work performed 3. Type Certificate Data Sheets are issued for which b. Make an entry in the maintenance record of the following products? of that equipment a. Aircraft, engines and propellers c. Advise the FAA district of office of the work b. Aircraft, engines and appliance performed, by submitting an FAA Form 337 c. Aircraft, engines, propellers and appliance 11. Primary responsibility for compliance with 4. Where are technical descriptions of certificated Airworthiness Directives lies with the propellers found? a. Aircraft owner or operator a. Applicable Airworthiness Directives b. Certificated mechanic holding an Inspection b. Aircraft Specifications Authorization who conducts appropriate c. Propeller Type Certificate Data Sheet inspections 5. (1) Manufacturer’s data and FAA publications c. Certificated mechanic who maintains the such as Airworthiness Directives, Type Certificate aircraft Data Sheets, and advisory circulars are all 12. A Technical Standard Order (TSO) is issued by approved data whom? (2) FAA publications such as Technical Standard a. The Aircraft industry Orders, Airworthiness Directives, Type Certificate b. Part manufacturers Data Sheets, and Aircraft Specifications and c. The Administrator Supplemental Type Certificates are all approved 13. Check trust bearing nuts for tightness on new or data newly overhauled engines at the first 50-hour Regarding the above statements, inspection following installation. Subsequent a. Both No.1 and No.2 are true inspections on thrust bearing nuts will be made at b. Only No.1 is true each third 50-hour inspection. c. Only No.2 is true From the above statement, at what intervals 6. The following is a table of airspeed limits as given should you check the thrust bearing nut for in an FAA-issued aircraft specification: tightness? Normal-exceed speed 293 knots Maximum a. 150 hours landing gear operation speed 174 knots b. 200 hours Maximum flap extended speed 139 knots c. 250 hours The high end of the white arc on the airspeed 14. A complete detailed inspection and adjustment of instrument would be at the valve mechanism will be made at the first 25 a. 260 knots hours after the engine has been placed in service. b. 293 knots Subsequent inspections of the valve mechanism c. 139 knots will be made each 50-hour period. 7. Which regulation provides the airworthiness From the above statement, at what intervals will standards for an airplane certificated in the valve mechanism inspections be performed? normal category? a. 100 hours a. 14 CFR Part 27 b. 50 hours b. 14 CFR Part 25 c. 125 hours c. 14 CFR Part 23 15. How long are AD compliance records required to 8. Placards required on an aircraft are specified in be kept? a. AC 43. 13-1B a. Until the work is repeated or superseded by b. The Federal Aviation Regulations under which other work the aircraft was type certificated b. For one year after the work is performed, or b. Neither No.1 nor No.2 is true until the work is repeated or superseded by c. Only No.1 is true other work 22. What is the maximum penalty for cheating or c. They shall be retained, and then other unauthorized conduct when taking an FAA transferred with the aircraft when it is mechanic test? solid a. Ineligibility to receive any certificate or 16. What does the Type Certificate Data designation rating for one year code ‘2 PCSM’ mean? b. Ineligibility to receive any certificate or a. Two place (number of seats), closed, sea, rating for one year, and suspension or monoplane. revocation of any certificate held b. Two wing(biplane), primary category, c. Ineligibility to receive any certificate or semimonocoque (airframe) rating for one year, and suspension of any c. Neither of the other two choices. certificate held 17. Suitability for the use of a specific propeller with 23. Which regulation provides information regarding a particular engine-airplane combination can be instrument range markings for an airplane determined by reference to what informational certificated in the normal category? source? a. 14 CFR Part 21 a. Propeller Specifications or Propeller Type b. 14 CFR Part 25 Certificate Data Sheet c. 14 CFR Part 23 b. Aircraft Specifications or Aircraft Type 24. What information is generally contained in Certificate Data Sheet. Aircraft Specifications or Type Certificate Data c. Alphabetical Index of Current Propeller Type Sheets? Certificate Data Sheets, Specifications and a. Empty weight of the aircraft Listings. b. Useful load of aircraft 18. An aircraft Type Certificate Data Sheet contains. c. Control surface movements a. Maximum fuel grade to be used. 25. The action required by an AD may take what b. Control surface adjustment points. form? c. Location of the datum. 1. Inspection 19. The Air Transport Association of America (ATA) 2. Part(s) replacement Specification No. 100 (1) establishes a standard 3. Design modification for the presentation of technical data in 4. Change in operating procedure(s) maintenance manuals. 5. Overall change in the content, firm and (2) Divides the aircraft into numbered systems disposition of the aircraft maintenance and simplify locating maintenance instructions. records. Regarding the above statements, a. 1,2,3 and/or 4 a. Both No.1 and No.2 are true b. 1,2,3 and/or 5 b. Neither No.1 nor No.2 is true c. 1,2,3,4 and/or 5 c. Only No.1 is true 26. Airworthiness Directives are issued primarily to 20. Which of the following includes all the regulatory a. Provide information about malfunction or definitions of ‘maintenance’? defect trends a. Overhaul, repair, parts replacement, and b. Present recommended maintenance preservation, and preventive maintenance procedures for correcting potentially b. Overhaul, repair, parts replacement, hazardous defects preservation, inspection, and preventive c. Correct an unsafe condition maintenance 27. Specifications pertaining to an aircraft model c. Overhaul, repair, parts replacement, manufactured under a type certificate, of which inspection, and preservation less than 50 are shown on the FAA Aircraft 21. (1) A Supplemental Type Certificate may be issued Registry, can be found in the to more than one applicant for the same design a. Aircraft listing change, providing each applicant shows b. Summary of Discontinued Aircraft compliance with the applicable airworthiness Specifications requirement. c. FAA Statistical Handbook of Civil Aircraft (2) An installation of an item manufactured in Specifications accordance with the Technical Standard Order 28. The following words are an example of what kind system requires no further appr6oval for of statement in an AD? ‘Required within the next installation in a particular aircraft. 25 hours time-in-service after the effective date Regarding the above statements, of this AD, unless already accomplished a. Both No.1 and No.2 are true a. Amendment b. Compliance (2) Divides the aircraft into numbered systems c. Applicability and subsystems in order to simplify locating 29. Under the Federal Aviation Regulations, an maintenance instructions Aviation maintenance technician is required to Regarding the above statements, perform maintenance on an aircraft so that it a. Both No.1 and No. 2 are correct a. Always meets its original type design b. Neither No.1 nor No.2 is correct b. Is at least equal to its original or properly c. Only No. 1 is correct altered condition 37. Which of the following are sometimes used as c. Exceeds minimum standards with regard to authorization to deviate from an aircraft’s aerodynamic function, structural strength, original type design? resistance to vibration, and other qualities 1. FAA Form 337 affecting airworthiness 2. Supplemental Type Certificate 30. When is a mechanic responsible for checking AD 3. Airworthiness Directives compliance? 4. Technical Standard Order a. Never, the owner or operator is solely a. 1,2,3 and 4 responsible b. 1,2 and 4 b. When performing an inspection required c. 1,2 and 3 under part 91, 125, or 135 38. When an airworthy (at the time of sale) aircraft c. Anytime an aircraft or portion thereof is is sold, the Airworthiness Certificate returned to service a. becomes invalid until the aircraft is 31. When information is generally contained in reinspected and approved for return to Aircraft Specifications or Type Certificate Data service Sheets? b. is voided and a new Certificate is issued upon a. Empty weight of the aircraft application by the new certificate is issued b. Useful load of aircraft upon application by the new owner c. Control surface movements c. is transferred with the aircraft 32. The issuance of an Airworthiness Certificate is governed by MECHANIC PRIVILEGES AND LIMITATIONS a. 14 CFR Part 23 1. All of the following are consequences of human b. 14 CFR Part 21 error, except c. 14 CFR Part 39 a. Mental stressor 33. An aircraft mechanic is privileged to perform b. Catastrophic major alterations on U.S. certificated aircraft; c. Personal injury however, the work must be done in accordance 2. An airworthiness Directive requires that a with FAA-approved technical data before the propeller be altered. Certificated mechanics could aircraft can be returned to service. Which is NOT a. Perform and approve the work for return to approved data? service if it is a minor alteration a. Airworthiness Directives b. Not perform the work because it is an b. AC 43. 13-2A alteration c. Supplemental Type Certificates c. Not perform the work because they are not 34. Technical information about older aircraft allowed to perform and approve for return to models, of which no more than 50 remain in service, repairs or alterations to propellers service, can be found in the 3. When we think of aviation safety in a a. Aircraft listing contemporary way, human error is b. Summary of Deleted and Discontinued a. The starting point Aircraft Specifications b. The ending point c. Index of Antique Aircraft c. The intervention point 35. Where are technical descriptions of certificated 4. (1) Certificated mechanics with an airframe propellers found? rating may perform a minor repair to an airspeed a. Applicable Airworthiness Directives indicator providing they have the necessary b. Aircraft specifications equipment available c. Propeller type Certificate Data Sheets (2) Certificated mechanics with a powerplant 36. The Air Transport Association of America (ATA) rating may perform a major repair to a propeller Specification No. 100 providing they have the necessary equipment (1) Establishes a standard for the representation available of technical data in maintenance manuals Regarding the above statements, a. Only No. 1 is true b. Neither No.1 nor No.2 is true 3. A non-certificated mechanic working under the c. Only No.2 is true supervision of a certificated mechanic with 5. A certificated mechanic shall not exercise the airframe and powerplant ratings privileges of the certificate and rating unless, a. 1 within the preceding 24 months, the b. 2 Administrator has found that the certificate c. 1 and 3 holder is able to do the work or the certificate 11. A certificated mechanic with a powerplant rating holder has may perform the a. Served as a mechanic under the certificate a. Annual inspection required by the Federal and rating for at least 18 months Aviation regulations on a powerplant or any b. Served as a mechanic under the certificate component thereof and approve and return and rating for at least 12 months the same to service c. Served as a mechanic under the certificate b. 100-hour inspection required by the Federal and rating for at least 6 months Aviation Regulations on a powerplant or 6. A repair, as performed on an airframe, shall mean any component thereof and approve and a. The upkeep and preservation of the airframe return the same to service including the component parts thereof c. 100-hour inspection requires by the Federal b. The restoration of the airframe to a Aviation Regulations on an airframe, condition for safe operation after damage powerplant or any other component of the or deterioration aircraft thereof and approve and return the c. Simple or minor preservation operations and same to service the replacement of small standard parts not 12. Under Title 14 of the Code of Federal Regulations, involving complex assembly operations what is the maximum penalty for falsification, 7. FAA certificated mechanics may alteration, or fraudulent reproduction of a. Approve for return to service a major repair certificates, logbooks, reports and records? for which they are rated a. Ineligibility to receive any certificate or b. Supervise and approve a 100-hour inspection rating for one year c. Approve for return to service a minor b. Imprisonment for one year and a $5,000.00 alteration they have performed appropriate fine to the rating(s) they hold c. Suspension or revocation of any certificate 8. The 100-hour inspection required by Federal held Aviation Regulations for certain aircraft being 13. Which is classified as a major repair? operated for hire may be performed by a. The splicing of skin sheets a. Persons working under the supervision of an b. Installation of new engine mounts obtained appropriately rated mechanic for return to from the aircraft manufacturer service c. Any repair of damaged stressed metal skin b. Appropriately rated mechanics only if they 14. What is the normal duration a mechanic have an inspection authorization certificate with airframe and/or powerplant c. Appropriately rated mechanics and ratings? approved by them for return to service a. Until the holder is relieved of duties for 9. Which of the following statements is true for a which the holder was employed and certificated and appropriately rated mechanic certificated regarding repairs and alterations? b. Until surrendered, suspended, or revoked a. He/she may perform an airframe major c. Until 24 months after the holder has last repair or major alteration, but cannot exercised the privileges of the certificate approve work for return to service 15. Who is responsible for determining that materials b. He/she may perform airframe minor repairs used in aircraft maintenance and repair are of the and minor alterations and approve the work proper type and conform to the appropriate for return to service, but cannot perform an standards? airframe major repair or major alteration a. The installing person or agency c. He/she may perform airframe major repair or b. The owner or operator of the aircraft major alteration and approve the work, but c. The manufacturer of the aircraft not the entire aircraft, for return to service 16. Many areas of aviation have shifted their focus 10. Who has the authority to approve for return to from eliminating error to service a propeller after a 100-hour inspection? a. Preventing and managing error 1. A mechanic with a powerplant rating b. Identifying and mitigating error 2. Any certificated repairman c. Reducing and containing error 17. Why a mechanic applicant is issued a temporary b. 100-hour and/or annual inspections required certificate after successful completion of the by the Federal Aviation Regulations on required tests? powerplants, propellers or any components a. To allow for review of his/her application thereof and may release the same to service and supplementary documents c. 100-hour inspections required by the b. So that a background check/investigation may Federal Aviation Regulations on be completed powerplants, propellers, or any c. Both of the other two choices components thereof, and may release the 18. certificated mechanics, under their general same to service certificate privileges, may 26. Instrument repairs may be performed a. perform minor repairs to instruments a. By the instrument manufacturer only b. perform 100-hour inspection of b. By an FAA-approved instrument repair instruments station c. perform minor alterations to instruments c. On airframe instruments by mechanics with 19. the replacement of a damaged engine mount with an airframe rating a new identical engine mount purchased from the 27. The “SHEL” model is another human factors tool. aircraft manufacturer is considered a The goal is to determine not only what the a. major or minor repair, depending upon the problem is, but also complexity of the installation a. Where and why it exists b. major repair b. How we prevent the problem c. minor repair c. How many factors contribute to the error 20. How long does the holder of a certificate issued 28. What is the maximum duration of a temporary under 14 CFR part 65 have to notify the FAA after airman certificate? any change in permanent mailing address? a. 60 days a. 30 days b. 90 days b. 60 days c. 120 days c. 90 days 29. What part of the Federal Aviation Regulations 21. According to Dr. James Reason, there are two prescribes the requirements for issuing mechanic types of human failure which can occur. They are: certificates and associated ratings and the a. Active and latent general operating rules for the holders of these b. Mental and physical certificates and ratings? c. Proper and improper a. 14 CFR Part 43 22. Which of these publications contains standards b. 14 CFR Part 91 for protrusion of bolts, studs, and screws through c. 14 CFR Part 65 self-locking nuts? 30. How is a quality system assured? a. AC 43. 13-1B a. By an independent organization b. AC 43. 13-2 b. By a dependent organization c. Aircraft Specifications or Type Certificated c. By an internal reporting and auditing Data Sheets system 23. The three types of human error are 31. The positive aspects of human factor issues are a. Omission, commission and extraneous referred to as the b. Active, latent and stressor a. Magnificent seven c. Mental, situational and physiological b. Dirty Dozen 24. The replacement of fabric on fabric-covered parts c. MEDA such as wings, fuselages, stabilizers or control 32. When may an otherwise qualified mechanic who does surfaces is considered to be a not read, write, speak and understand the English language be eligible to apply for a mechanic certificate? a. Minor repair unless the new cover is different a. When a special authorization has been granted by in any way from the original cover the Administrator b. Minor repair unless the underlying structure b. When employed outside the United States by a is altered or repaired U.S. air carrier c. Major repair even though no other c. When employed outside the United States alteration or repair is performed 33. A person working under the supervision of a 25. Certificated mechanics with a powerplant rating certificated mechanic with an airframe and may perform powerplant rating is not authorized to perform a. Any inspection required by the Federal a. Repair of a wing brace strut by welding Aviation Regulations on a powerplant or b. A 100-hour inspection propeller or any component thereof, and may c. Repair of an engine mount by riveting release the same to service PCAR 11. Which of the ff. Is a portion of the required permanent maintenance record entry a 100 hour 1. Calibration and repair of instruments is an example inspection of (Part IS.5.1.12)? a. The date of the inspection and aircraft time in a. Appliance major alterations service b. Appliance major repair b. The name of the owner of the aircraft c. Components major repair c. A brief description of the extent of the inspection 2. The alteration of an aircraft or aeronautical product 12. Replacing or cleaning spark plugs and setting of in conformity with an approved standard sparkplug gap clearance is considered as (Part IS a. Replacement 5.1.12) b. Alteration a. Preventive maintenance c. Modification b. Powerplant major alterations 3. Changes to the basic design of the fuel or oil system c. Powerplant major repair is considered 13. Where would find the recommended statement for a. Airframe major modification recording the approval or disapproval of an aircraft b. A preventive maintenance after a 100 hour or annual inspection c. Airframe minor modification a. 14 CFR Part 43 4. Changes of the following type to a powerplant, or b. 14 CFR Part 65 airframe when not listed in the specifications issued c. 14 CFR Part 91 by the Air transport office in the accordance with the 14. Disassembly of a crankcase or crankshaft of a manufacturer reciprocating engine equipped with an integral a. A powerplant major alteration supercharger is an example (Part IS.5.1.12) b. Powerplant major repair a. Powerplant major repair c. Aircraft major alteration b. Powerplant minor repair 5. In accordance with the table of sanction under c. Preventive maintenance PCAR’s Part 1, the penalty for “falsification of 15. Any repair to spars ribs, and surface involves records or reports” a. Airframe minor repair techniques a. Lawsuit b. An AD or CAM 18 b. Revocation c. The inspection and approved by the ATO c. Suspension 16. Which is considered to be typical preventive 6. Simple or minor preservation operations and the maintenance operations replacement of small standards parts not involving a. Piston removal complex assembly operation is known as b. Overhauling Instruments a. Powerplant/airframe minor repair c. Removal, installation and repair of landing b. Preventive maintenance gear tires c. Appliance major repair 17. What does it mean when it is said that a component 7. Installation of an accessory which is not approved conforms with the technical standard order for the engine is an example of a. It does not require an STC when used in a. Powerplant major modification/alteration alteration b. Powerplant major repair b. It does not require AD when used in major repair c. A preventive maintenance c. It can be used in my certified aircraft 8. Who may perform inspection of the aircraft if it is 18. When can you consider the repair on the following away from the station where inspection is normally airframe, a major repair conducted a. The repair of damaged areas in the plywood a. A certified repair station stressed covering (6) inches b. An appropriate licensed mechanic b. The repair of damaged areas in the stressed c. All of the above covering at least (10) inches 9. Who is responsible for ensuring that all aircraft c. The repair of a control surface ribs of a maintenance records are kept up to date convenient type a. CAAP 19. Modification of the basic design not made in b. Inspector accordance with the recommendations of the c. Licensed mechanic/owner appliance manufacturer or in accordance with 10. When major repair alteration results in any change applicable airworthiness directives is considered as in the aircraft operating limitations or data (Part IS 5.1.12) contained in approved airplane flight a. Appliance major repair a. The form and manner prescribed by the CAAP b. Airframe major alterations b. Aircraft maintenance manual c. Appliance major modification c. Aircraft operating and maintenance manual 20. Which of the following is not considered as a. The registered operator powerplant major alteration b. The maintenance crew chief a. Disassembly of float type carburetor c. An appropriate licensed aircraft mechanic b. Replacement of cylinder 29. A special flight permit may be issued for an aircraft c. Removal of piston that may not currently meet applicable 21. In order to reconstruct lost/destroyed aircraft airworthiness requirements but is capable of safe maintenance records, what is necessary to establish? flight for the purposes of ( PCAR 5.4.1. 11.4) a. Total service of the airframe a. Not to exceed 10 hrs TBO b. Total service of the powerplant b. Not more than 10 hrs of TBO c. Service on the whole aircraft c. All of the above 22. No person, entity other than the authority may 30. Change to the basic design made in accordance with disapprove an aircraft, airframe, aircraft engine, the assec of the air transportation approved propeller appliance, or component part for return to recommendations of the landing gear shock strut service after it has gone under maintenance, a. Airframe major alteration preventive maintenance, rebuilding or modification b. Appliance minor alteration except as provided in the ff. c. Appliance major alteration a. Manufacturer’s manual 31. A document signed by an authorized representative b. Propeller manual of an Approved Maintenance Organization (AMO) in c. All of the above respect with an inspection, repair or modification on 23. P-CAR part for MRO/AMO a complete aircraft, engine or propeller after it has a. Airframe major repair received a maintenance performed (Part is 5.1. 12) b. Routine maintenance alteration a. Maintenance Release c. PCAR Part 6 b. Airworthiness certificate 24. Airframe, powerplant or appliance which has c. Return to service undergone maintenance, minor repair or minor 32. Any repair to spars ribs, and surface involves alteration may approve and returned to the service a. Airframe minor repair techniques except by one of the ff. b. An AD or CAM 18 a. An appropriate licensed aircraft mechanic c. The inspection and approved by the ATO b. An appropriate licensed Pilot 33. When can an aircraft be operated with a 100 hour c. An air transport office aircraft inspection inspection overdue 25. Airframe minor repair includes a. Only when the aircraft is operated under a a. Box beams continuous airworthiness program b. Wing or tall surface brace and struts b. If necessary to reach a place at which the c. Wing and control surface fairings inspection can be done 26. Each person performing a major repair or major c. If aircraft is equipped with an hour meter modification shall forward a copy of that form to the 34. The restoration of an engine mounts to a good Authority in accordance with Authority instructions condition for safe operation after the damage is within 48 hours after aeronautical product is classified as approved for return to service (part IS 5.7.1.1) a. An airframe major repair a. 48 hours b. A powerplant major repair b. 72 hours c. A powerplant major alteration c. 144 hours 35. Special repair to structural engine parts by welding, 27. Large airplanes and turbine powered multi engine plating, metalizing or other methods is an example airplanes operated under federal aviation of ( Parts IS 5.5.5. 12) a. In accordance with the continuous airworthiness a. Powerplant major alterations maintenance program ( camp program ) authorized b. Powerplant major repair under federal aviation regulation part 91. Subpart E c. Preventive maintenance b. In accordance with the inspection program 36. In accordance with the table of sanction under authorized under federal aviation regulation part PCAR’s part of the penalty for “Failure to complete 91, subpart E and sign maintenance release” is c. In accordance with the progressive inspection a. 15 to 30 days suspension requirements of federal aviation regulation part b. An airframe minor repair 91.409 c. Group Responsibility 28. A permanent record of every maintenance ( not 37. A maximum time a 100 hour inspection may be including preventive maintenance ) Repair of extended is building or alternations on any airframe, a. 5 hrs powerplant, propeller, or appliance shall be b. 10 hrs maintained by c. 2 hrs 38. Require owner shall retain maintenance and AFCAR inspection records for minimum periods of a. 100 days 1. Replacement of an autopilot with parts b. 60 days manufactured with approved drawing is c. 90 days considered 39. Replacement of components or complete units such a. Appliance major repair as landing gears which parts supplied by the original b. Accessory major repair manufacturer or manufactured in accordance with c. Component minor repair approved drawing is considered d. Airframe minor repair a. Component minor repair 2. Replacing any cowling not requiring removal of b. Airframe minor repair the propeller or any disconnecting of flight c. Components major repair control is considered 40. Replacing defective safety wiring or cotter pins is a. Airframe maintenance repair a. Progressive maintenance b. Component minor repair b. Preventive maintenance c. Preventive maintenance c. Routine maintenance d. Airframe minor repair 41. An example of powerplant major repairs 3. Which statement about Airworthiness Directives a. Cylinder removal (AD’s) is true? b. Piston removal a. Compliance with an applicable AD is c. All of the above mandatory and must be recorded in the 42. Where would you find the operating conditions that maintenance record make 100 hour inspection mandatory b. AD’s are information alert bullets issued by a. 14 CFR Part43 the airframe, powerplant, or component b. AC 43.13-2A manufacturer c. 14 CFR Part 91 c. Compliance with an AD is not mandatory 43. Strengthening or reinforcing the fuselage longeron unless the aircraft is affected is for hire a. Airframe minor modification 4. The installation or removal of equipment of equal b. Airframe major alteration or less weight and in the same location as the last c. Airframe major repair listed as optional equipment in the aircraft 44. Conversions of any sort for the purpose of using fuel specifications is rating or grade other than listed in the engine a. An appliance major repair specifications (Part IS 5.1.1.2 ) b. An airframe minor alteration a. Airframe major alterations c. An airframe major alteration b. Powerplant major repair d. An airframe minor repair c. Powerplant major modification 5. Modification to basic design of the exhaust 45. Any maintenance operation requiring of the cold and system is considered hot sections a. Aircraft major alteration a. Powerplant major alterations b. Airframe major alteration b. Powerplant major repair c. System major alteration c. Preventive maintenance d. Powerplant major alteration 46. Special repairs to structural engine parts by welding, 6. Which is not considered an airframe major plating, metalizing or other methods is an example alteration? of (Part IS 5.1.1.12) a. Installation of any system affecting the a. Powerplant major alterations structural airworthiness or control of the b. Powerplant major repair aircraft c. Preventive maintenance b. Modification of the wing 47. In accordance with table of sanction under PCAR’S c. Strengthening or reinforcing the fuselage part 1, the penalty for “Improperly releasing an longeron aircraft to service” is d. A change to the basic design of the hydraulic a. 15 to 30 days suspension system b. 30 to 60 days suspension 7. Which statement is correct regarding an aircraft c. 10 to 20 days suspension that is found to be not airworthy after an annual 48. Which is considered to be typical preventive inspection, due to an item requiring a major maintenance operations (Part IS 5.1.12) repair (assuming approved data is issued to a. Removal installation repair of landing gears accomplish the repair)? b. Changing landing gear cowling a. An appropriately approved mechanic or repair c. Changing piston pin station may repair the defect and approve the aircraft for return to service b. An appropriately rated mechanic may 13. Airframe shall mean accomplish the repair and an IA may a. Any and all kinds of booms, landing gear, approve the aircraft for return to service empennages, fairing or control of fuselage, c. Only the person who performed the animal booms empennages, nacelles, fairing, inspection may approve the aircraft for return cowlings, control surfaces to service after the major repair b. Any kind all kinds contrivance, hull, cowlings, 8. An aircraft that is required by section 91.409 to landing gear, or control of whatever have a 100 hour inspection may be flown beyond description appertaining thereto, but not the inspection requirement including powerplant and electrical a. If necessary to reach a place at which the c. Any and all kinds of fuselage, booms, cowling, inspection can be accomplished, but a special landing gear, or control of whatever permit is necessary description appertaining thereto but not b. If necessary to reach a place at which the including powerplant and electrical inspection can be accomplished, but not to d. None of the above exceed 15 flight hours 14. Which of the following is considered to be c. If necessary to reach a place at which the typical maintenance? inspection can be accomplished, but not to a. Removal, Installation and repair of landing exceed 10 flight hours gear tires d. If necessary to reach a place at which the b. Removal, Installation of cylinders inspection can be accomplished, but not to c. Repairing dents, cuts, and small cracks on exceed 5 flight hours wooden propeller 9. The repair station or manufacturer may use a d. Grinding of valves and removing carbon maintenance release of its own design provided 15. No aircraft which has undergone any major repair the release includes the following alteration shall be returned to service unless such a. Make of aircraft, model, serial number, aircraft has thereafter been test flown by a nationality and registration person holding at least: b. Ake of aircraft, identification and registration a. A commercial pilot license with instrument mark, nationality rating c. Make of aircraft, type, model, serial number, b. A private pilot licensed nationality and identification mark c. A commercial pilot license d. Make of aircraft, identification mark, type d. An airline transport pilot license and serial number 16. Any restoration or maintenance work done on an 10. An aircraft that is due an annual inspection may airframe to place it back to a condition for safe be flown operation after damage or deterioration shall a. For the purpose of performing maintenance mean: b. If special permit has been issued for the a. An alteration aircraft b. A major maintenance c. For a period of time not to exceed 10 hours c. A repair d. For the purpose of obtaining permit d. A modification 11. Repair made on the hydraulic/pneumatic system 17. It means that the supervising mechanic is considered personally maintain such observation of the a. An accessory minor repair working being performed as is necessary to b. A preventive maintenance insure that the work being performed properly, c. An airframe major repair and the supervising mechanic is readily available d. An airframe minor repair for consultation with the person performing 12. Changes made to structural elements for the work. purpose of improving the service life or reducing a. Supervising aircraft mechanic maintenance cost, but that the cumulative weight b. Mechanic aide changes of all such maintenance work done since c. Under supervision the aircraft was re-weight or the weight and d. Direct supervision balance data re-compared do not exceed two 18. Which statement is correct when an aircraft has percent of the certificate empty weight on not been approved for return to service after an aircraft under 12,500 pounds gross weight is annual inspection because of several items classified as requiring minor repair? a. Airframe minor repair a. Only the person who performed the annual b. Airframe major alterations inspection may approve the aircraft for return c. Airframe minor alterations to service d. Aircraft major alterations b. An appropriately rated mechanic may 26. Changes of the following type to a powerplant, or repair the defects and approve the aircraft airframe when not listed in the specifications for return to service issued by the Air Transportation office in c. An appropriately rated mechanic may repair accordance with the manufacturer, are the defects, but an IA must approve the considered aircraft for return to service a. Powerplant major repair 19. The procedure recommended in making a scarf b. A powerplant major alteration for a spar splice is c. Aircraft major alteration a. A block plane d. An airframe major alteration b. A jointer 27. No airframe, powerplant or appliance which has c. A wood rasp undergone maintenance, minor repair or minor d. Kiln dried alteration may be approved and returned to the 20. The maximum time a 100-hour inspection may be service except by one of the following extended is a. The Chief of Aircraft Airworthiness Inspection a. 10 hours with a special flight permit b. An Air Transportation Office Aircraft b. 12 hours with a special flight permit Inspection c. 15 hours with a special flight permit c. An appropriate licensed aircraft mechanic d. 10 hours d. An appropriate license pilot 21. When overhauling electrical equipment, all 28. Where would you find the recommended necessary information should be obtained from statement for recording the approval or a. Maintenance instructions published by the disapproval for return to service of an aircraft aircraft or equipment manufacturer after a 100-hour annual inspection? b. The aircraft maintenance manual a. 14 CFR Part 43 c. Illustrated parts manual for the aircraft b. 14 CFR Part 65 22. Radio equipment installation made in accordance c. 14 CFR Part 91 with the Supplemental Type Certificate data d. 14 CFR Part 25 require approval for return to Service 29. Airframe minor repairs includes a. By field approval of the FAA a. Box beams b. By the holder of an inspection b. Wing or tail surface brace-struts authorization c. Main seat support brace and brackets c. By an airframe and powerplant mechanic d. Wing and control surface fairings d. By an pilot 30. When can you consider the repair on the following 23. For an individual (not a repair station) to conduct airframe, a major repair a. The repair of the leading edge of the wing and a complete 100 hour inspection on an aircraft and control surface between two adjacent wing and approve it for return to service requires a control surface ribs mechanic certificate with an b. The repair of a control surface ribs of a convenient a. Airframe rating only type b. Airframe and powerplant ratings with an c. The repair of damaged areas in the stressed inspection authorization covering exceeding at least (10) inches in any c. Powerplant rating only direction d. Airframe and powerplant ratings d. The repair damaged areas in the plywood 24. Who is authorized among the following to perform stressed covering exceeding (6) inches in any maintenance Preventive maintenance, repair or direction alteration on civil aircraft of the Philippine registry 31. Changes to the basic design of the fuel or oil a. Licensed pilot who owns and operates the aircraft system is considered that is not used in an air carrier service a. Airframe major modification b. A licensed aircraft mechanic or a person working b. A preventive maintenance under the supervision of the licensed mechanic c. Airframe major alteration c. An appropriate rated repair station d. Airframe minor modification d. All of the above 32. A permanent record of every maintenance (not 25. A simple minor preservations and the including preventive maintenance) repair of replacement of small standard parts not involving building or alteration of any airframe, complex assembly operations is classified as powerplant, propeller or appliances shall be a. Airframe major repair maintained by b. Routine maintenance alteration a. The registered operator c. Preventive maintenance b. The maintenance crew chief d. Airframe minor repair c. An appropriate licensed aircraft mechanic d. The pilot mechanic 33. Replacing defective safety wiring or cotter pins is 41. Replacement of components or complete units a. Progressive maintenance such as landing gears with parts supplied by the b. Airframe minor repair original manufacturer or manufactured in c. Routine maintenance accordance with approved drawings is considered d. Preventive maintenance a. Component minor repair 34. Where would you find the operating conditions b. Airframe minor repair that make a 100 hour inspection mandatory? c. Components major repair a. 14 CFR Part 91 42. When an aircraft be operated with a 100-hour b. 14 CFR Part 43 inspection overdue? c. AC 43.13-2A a. If necessary to reach a place at which the 35. Large airplanes and turbine powered multiengine inspection can be done airplanes operated under Federal Aviation b. Only when the aircraft is operated under a Regulation Part 91, General Operating and Flight continuous airworthiness program Rules, must be inspected c. If aircraft is equipped with an hour meter a. In accordance with an inspection program 43. A maximum time a 100-hour inspection may be authorized under Federal Aviation extended is Regulation Part 91, Subpart E a. 10 hr b. In accordance with a continuous b. 2 hr airworthiness maintenance program (camp c. 15 hr program) authorized under Federal Aviation 44. Which of the following is a portion of the Regulation Part 91, Subpart E required permanent maintenance record entry c. In accordance with the progressive inspection after 100-hour inspection? requirements of Federal Aviation Regulation a. The name of the owner of the aircraft Part 91.409 b. The date of the inspection and aircraft time 36. Any repair to spars, ribs, and surface involves in service a. An AD or CAM 18 c. A brief description of the extent of the b. Airframe minor repair techniques inspection c. The inspection and approved by the ATO 45. Change in the basic design made in accordance 37. What does it mean it is said that a component with the “ASSEC” of the air transportation conforms with a technical standard order? approved recommendation of the “Landing gear a. It does not require AD when used in a major shock strut” manufacturing or in accordance with repair ATO airworthiness directives are considered to be b. It can be used on my certified aircraft a. Appliance minor alteration c. It does not require an STC when used in an b. Appliance major alteration alteration c. Airframe major alteration 38. The restoration of an engine mounts to a condition for safe operation after damage is Familiarize the following classified as Choices: True or False a. An airframe major repair b. A powerplant major repair Answer: TRUE c. A powerplant major alteration 39. Strengthening or reinforcing the fuselage Answer: Part 5 longeron. Answer: Maintenance Release a. Airframe major alteration b. Airframe minor modification Answer: Special Flight Permit c. Airframe major repair 1st question with choices: a. 2 yrs b. 3yrs c. 5 yrs 40. When a major repair alteration results in any change in the aircraft operating limitations or Answer: c. 5 yrs data contained in approved airplane flight manual appropriate amendments to the aircraft operating 2nd question following the 1st Q have also these choices: a. limitations shall be made in 2yrs b. 3 yrs c. 5yrs a. The form and manner prescribed by the Answer: b. 3 yrs CAAP b. Aircraft maintenance manual Note: choose c. A and B are both correct or all of the c. Aircraft operating and maintenance manual above, because the entire question that having this choices are the correct answers 1. Removal of accessories that are listed as required 8. The owner of an aircraft or, in the case of a equipment on the aircraft or engine specifications leased aircraft, the lessee, shall be responsible for is an example of maintaining the aircraft in an airworthy condition a. Powerplant Major Modification a. All maintenance, overhaul, modifications and b. Powerplant Major Repair repairs which affect airworthiness are c. Appliance Major Modification performed as prescribed by the State of 2. A certification confirming that the maintenance Registry work to which it relates has been complied wit in b. Authorized maintenance personnel make accordance with the applicable standards of appropriate entries in the aircraft airworthiness using approved data maintenance records certifying that the a. Service Manual aircraft is airworthy b. Maintenance Release c. A maintenance release is completed to the c. Aircraft Tags certify that the maintenance work performed 3. Separation or disassembly of a crankcase or has been completed satisfactorily and in crankshaft of a reciprocating engine equipped accordance with the prescribed method with an integral supercharger is an example of d. All of the above a. Powerplant Major Repair 9. The Contracting State which approved the b. Powerplant Minor Alteration original type certificate and any subsequent c. Powerplant Minor Repair supplemental type certificates for an aircraft, or 4. Who is authorized to repair an aircraft which approved the design of an aeronautical instrument? product or appliance a. Aircraft Avionics a. State of Registry b. Certified repair station of the instrument b. State of Design c. Mechanic c. State of Manufacturer 5. Who is responsible for maintaining aircraft from 10. The AMO shall relieve the person performing unworthy condition? maintenance functions from all duties for 24 a. Licensed Aircraft Maintenance/Mechanic consecutive hour during any b. Pilot in Command a. 5 Days c. CAAP/Authority b. 3 Consecutive days 6. The restoration of an aircraft/aeronautical c. 7 Consecutive days product by using methods, techniques, and 11. Which part of Philippine Civil aviation Regulation practices acceptable to the Authority, when it has prescribe the requirements for certification of an been disassembled, cleaned, inspected as aircraft and aeronautical components or permitted, repaired as necessary, reassembled, continuing airworthiness? and tested to the same tolerances and limits as a a. PCAR Part 2 (Personnel Licensing) new item, using either new parts or used parts b. PCAR Part 8 (Operations) that conform to new part tolerances and limits c. PCAR Part 5 (Airworthiness) a. Overhaul 12. Change to the Hub Design is? b. Repair a. Powerplant minor repair c. Rebuild b. Propeller Major Modification 7. Who is responsible for ensuring that all c. Propeller Major Repair maintenance required to be carried out in the 13. Rewinding the field coil of an electrical hangar plus any defect rectification carried out accessories is an example of? during base maintenance, is carried out to a. Airframe Minor repair specified design and quality standards? b. Appliance Major Repair a. Pilot c. Airframe Minor Alteration b. Line Maintenance Manager c. Owner

Use Quizgecko on...
Browser
Browser