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  • 問題数 80 • 4/1/2024

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    問題一覧

  • 1

    large airplanes and turbine powered multi engine airplanes operated under federal aviation

    in accordance with the inspection program authorized under federal aviation regulation part 91, subpart E

  • 2

    the procedure recommended in making a scarf for a spar splice is

    a jointer

  • 3

    what does it mean when it is said that a component conforms with the technical standard order

    it does not require an STC when used in alteration

  • 4

    in accordance with the table of sanction under PCAR’s part of the penalty for failure to complete and sign maintenance release is

    15-30 days suspension

  • 5

    which is not considered an airframe major alteration

    strengthening or reinforcing the fuselage longeron

  • 6

    the restoration of an aircraft/ aeronautical product by using methods, techniques and practices acceptable to the authority, when it hase been disassembled, cleaned, inspected as permitted, repaired as necessary, reassembled and tested to the same tolerances and limits as a new item, using either new parts or used parts the conform to new part tolerances and limits

    rebuild

  • 7

    the owner of an aircraft or, in case of a leased aircraft, the lessee shall be responsible for maintaining the aircraft in an airworthy condition

    all of the above

  • 8

    in order to reconstract lost/destroyed aircraft maintenance records, what is necessary to establish

    total service of the airframe

  • 9

    each person performing a major repair or major modification shall forward a copy of that form to the authority in accordance with authority instructions within _ hours after aeronautical product is approved for return to service ( part IS 5.7.1.1)

    48 hours

  • 10

    the repair station or manufacturer may use a maintenance release of its own design provided the release includes the following

    make of aircraft, model, serial number, nationality and registration

  • 11

    which is considered to be typical preventive maintenance operations

    removal, installation and repair of landing gear tires

  • 12

    a maximum time a 100 hour inspection may be extended is

    10 hours

  • 13

    repair made on the hydraulic/pnuematic system is considered

    an airframe minor repair

  • 14

    which is considered to be typical preventive maintenance operation

    removal installation repair of landing gear

  • 15

    changes to the basic design of the fuel or oil system is considered

    airframe major modification

  • 16

    a special flight permit may be issued for an aircraft that may not currently meet applicable airworthiness requirements but is capable of safe flight for the purpose of ( PCAR 5.4.1.11.4)

    all of the above

  • 17

    any restoration or maintenance work done on an airfram to place it back to a condition for safe operation after damage of deterioration shall mean

    a repair

  • 18

    a certification confirming the maintenance work to which it relates has been complied within accordance with the applicable standards of airworthiness using approved data

    maintenance release

  • 19

    a document signed by an authorized representative of an approved maintenance organization (AMO) in respect with an inspection, repair or modification on a complete aircraft, engine or propeller after it has received a maintenance performed (Part IS 5.1.12)

    return to service

  • 20

    special repair to structural engine parts by welding, plating, metalizing or other methods is an example of (part IS 5.5.5.12)

    powerplant major repair

  • 21

    where would you find the recommended statement for recording the approval or disapproval of an aircraft after a 100 hour or annual inspection

    14 CFR Part 43

  • 22

    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

    appliance minor alteration

  • 23

    in accordance with the table of sanction under PCAR’s part 1, the penalty for improperly releasing an aircraft to service is

    30-60days suspension

  • 24

    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 nad 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

    airframe minor alteration

  • 25

    the AMO shall relive the person perfoming maintenance functions from all duties for 24 consecutive hour during any

    7 consecutive days

  • 26

    an example of powerplant major repair

    all of the above

  • 27

    who is responsible for ensuring that all aircraft maintenance records are kept up to date

    licensed mechanic/owner

  • 28

    replacing defective safety wiring or cotter pins is

    preventive maintenance

  • 29

    which statement about airworthiness directives (AD’s) is true

    compliance with an applicable AD is mandatory and must be recorded in the maintenance record

  • 30

    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

    appliance major modification

  • 31

    installation of an accessory which is not approved for the engine is an example of

    powerplant major modification/alteration

  • 32

    when major repair alteration results in any change in the aircraft operating limitations or data contained in approved airplane flight

    the form and manner prescribed by the CAAP

  • 33

    a permanent record of every maintenance (not including preventive maintenance) repair of building or alterations on any airframe, powerplant, propeller or appliance shall be maintained by

    the registered operator

  • 34

    no airframe, powerplant or appliance which has undergone maintenance, minor repair or minor alteration may be approved and returned to the service except by one the following

    an appropriate licensed aircraft mechanic

  • 35

    no person, entity other than the authority may disapprove an aircraft, airframe, aircraft engine, propeller appliance or component part for return to service after it has gone under maintenance, preventive maintenance, rebuilding or modification except as provided in the ff.

    all of the above

  • 36

    airframe minor repair includes

    wing and control surface fairings

  • 37

    when can you consider the rpair on the following airframe a major repair

    the repair of damaged areas in the plywood stressed covering (6) inches

  • 38

    rewinding of coil

    minor repair

  • 39

    any repair to spar ribs, and surface involves

    airframe minor repair techniques

  • 40

    reweight of gen av aircraft 5yrs, reweight of commercial aircraft every 3 yrs

    edi wow

  • 41

    airframe,powerplant or appliance which has undergone maintenance, minor repair or minor alteration may approve and returned to the service except by one of the ff.

    an appropriate licensed aircraft mechanic

  • 42

    P-CAR part for MRO/AMO

    PCAR part 6

  • 43

    who may perform inspection of the aircraft if it is away from the station where inspection is normally conducted

    all of the above

  • 44

    require owner shall retain maintenance and inspection records for minimum periods of

    90 days

  • 45

    any maintenance operation requiring of the cold and hot sections

    powerplant major repair

  • 46

    replacing any cowling not requiring removal of the propeller or any disconnecting of flight control is considered

    preventive maintenance

  • 47

    calibration and repair of instruments is an example of (Part IS.5.1.12)

    appliance major repair

  • 48

    strengthening or reinforcing the fuselage longeron

    airframe major repair

  • 49

    replacing or cleaning spark plugs and setting of sparkplug gup clearance is considered as (Part IS 5.1.12)

    preventive maintenance

  • 50

    modification to basic design of the exhaust system is considered

    airframe major alteration

  • 51

    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

    aircraft major alteration

  • 52

    simple or minor preservation operations and the replacement of small standards parts not involving complex assembly operation is known as

    preventive maintenance

  • 53

    which statement is correct regarding an aircraft tha is found to be not airworthy after an annual inspection, due to an item requiring a major repair (assuming approved data is issued to accomplish the repair)

    an appropriately rated mechanic may accomplish the repair and IA may approve the aircraft for return to service

  • 54

    it means that supervising mechanic personally maintain such observation of the working being performed as is necessary to insue that the work being perfomred properly, and the supervising mechanic is readily available for consultation with the person performing work

    direct supervision

  • 55

    which of the following is considered to be typical maintenance

    repairing dents, cuts and small cracks on wooden propeller

  • 56

    change to basic desing made in accordance with the assec of the air transportation approved recommendations of the landing gear shock strut

    appliance minor alteration

  • 57

    when can an aircraft be operated with a 100 hour inspection overdue

    if necessary to reach a place at which the inspection can be done

  • 58

    airframe minor repairs includes

    wing and control surface fairings

  • 59

    no aircraft which has underegone any major repair alteration shall be retunred to service unless such aircraft has thereafter been test flown by a person holding at least

    a private pilot license

  • 60

    removal of accessories that are listed as required equipment on the aircraft or engine specifications is an example of

    powerplant major modifciation

  • 61

    who is authorized to repair an aircraft instrument

    certified repair station of the instrument

  • 62

    converstion 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)

    powerplant major modification

  • 63

    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

    aircrafr major alteration

  • 64

    in accordance with the table of sanction under PCAR’s Part 1, the penalty for falsification of records or reports

    revocation

  • 65

    who is authorized among the following to perform maintenance, preventive maintenance, repair or alteration on civil aircraft of the philippine registry

    all of the above

  • 66

    a simple minor preservations and the replacement of small standard part not involving complex assembly operations is classified as

    preventive maintenance

  • 67

    the restoration of an engine mounts to a good condition for safe operation after the damage is classified as

    an airframe major repair

  • 68

    replacement of an autopilot with parts manufactured with approved drawing is considered

    appliance major repair

  • 69

    the alteration of an aircraft or aeronautical product in conformity with an approved standard

    modification

  • 70

    the contracting state which approved the orignial type certificate and any subsequent supplemental type certificates for an aircraft, or which approved the design of an aeronautical product or appliance

    state of design

  • 71

    replacement of components or complete units such as landing gears which parts supplied by the original manufacturer or manufactured in accordance with approve drawing considered

    airframe minor repair

  • 72

    airframe shall mean

    any and all kinds of booms, landing gear, empennages, fairing or control of fuselage, booms empennages, nacelles, fairing, cowlings and control surfaces

  • 73

    the installation or removal of equipment of equal or less weight and in the same location as the last listed optional equipment in the aircraft specification is

    an airframe minor alteration

  • 74

    special repairs to structural engine parts by welding, plating, metalizing or other methods is an example of

    powerplant major repair

  • 75

    disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger is an example (Part IS 5.1.12)

    powerplant major repair

  • 76

    which of the ff. is a portion of the required permanent maintenance record entry a 100 hour inspection

    the date of the inspection and aircraft time in service

  • 77

    which of the following is not considered as powerplant major alteration

    disassembly of float type carburetor

  • 78

    change to the hub design is

    propeller major modification

  • 79

    who is responsible for ensuring that all maintenance required to be carried out in the hangar plus any defect rectification carried out during base maintenance, is carried out to specified design and quality standards

    line maintenance manager

  • 80

    where would you find the operating conditions that make a 100 hour inspection mandatory

    14 CFR Part 91