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

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

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

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

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

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

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

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

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

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

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

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

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

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

any repair to spar ribs, and surface involves

which is considered to be typical preventive maintenance operations

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

when can you consider the rpair on the following airframe a 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

which of the following is not considered as powerplant major alteration

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

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.

P-CAR part for MRO/AMO

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.

airframe minor repair includes

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)

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

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

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)

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

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)

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

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

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

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

a maximum time a 100 hour inspection may be extended is

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

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

replacing defective safety wiring or cotter pins is

an example of powerplant major repair

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

strengthening or reinforcing the fuselage longeron

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)

any maintenance operation requiring of the cold and hot sections

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

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

which is considered to be typical preventive maintenance operation

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

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

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

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

modification to basic design of the exhaust system is considered

which is not considered an airframe major alteration

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)

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

repair made on the hydraulic/pnuematic system is considered

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 shall mean

which of the following is considered to be typical maintenance

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

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

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

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

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

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

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

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

airframe minor repairs includes

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

rewinding of coil

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

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

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

who is authorized to repair an aircraft instrument

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

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

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

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

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

change to the hub design is