CAR-M From Subpart A to E (1) PDF

CAR-M TEST-04 1.MTCS a)No component may be fitted unless it is in a satisfactory condition, has been appropriately released to service on a CA Form 1 b) a+marked in accordance with CAR 21 Subpart Q c) otherwise specified in CAR 21, CAR 145 or CAR-M Section A, Subpart F d)all. 2. Prior to install...

CAR-M TEST-04 1.MTCS a)No component may be fitted unless it is in a satisfactory condition, has been appropriately released to service on a CA Form 1 b) a+marked in accordance with CAR 21 Subpart Q c) otherwise specified in CAR 21, CAR 145 or CAR-M Section A, Subpart F d)all. 2. Prior to installation of a component on an aircraft _________ shall ensure that the particular component is eligible for fitment. a)organisationb)personc)bothd)only a is correct 3.MTICS a) Standard parts shall only be fitted to an aircraft or a component b) Material being either raw material or consumable material shall only be used on an aircraft or a component c) certifying staff of approved maintenance organisation should perform checks and verifications to ensure a component is in a satisfactory condition, d) organisations shall perform checks and verifications to ensure a component is in a satisfactory condition 4.Purpose of CAFORM-1 a) to release components after manufacture b)a+to release maintenance work carried out on such components under the approval of a DGCA c)to allow components removed from one aircraft/component to be fitted to another aircraft/ component. d)all 5. Document equivalent to a CA Form 1 may a)release document issued by an organisation under the terms of a bilateral agreement signed by DGCA -b)EASA Form ONE c) FAA Form 8130-3 d)all +Any other form acceptable to DGCA. 6.MTCS a) Consumable material is any material which is only used once, such as lubricants, cements, compounds, paints, chemicals dyes and sealants etc. b) Raw material is any material that requires further work to make it into a component part of the aircraft such as metals, plastics, wood, fabric etc. c) When using raw or consumable material on an aircraft or component near, or adjacent to, , it should be ensured that the CDCCL has not been compromised d)all 7.MTCS a) maintenance of acomponent while installed or temporarily removed from a Light aircraft not used in commercial air transport and performed in accordance with component maintenance data. b) except for: 1. overhaul of components other than engines and propellers, and; 2. overhaul of engines and propellers for aircraft other than CS-VLA,CS-22 and LSA. c)Component maintenance performed in option a is noteligible for the issuance of a CA Form 1 and shall be subject to the aircraft release requirements 8.MTCS”Service life components” a)Installed service life limited components shall not exceed the approved service life limit b)The approved service life is expressed in calendar time, flight hours, landings or cycles. c) a+At the end the approved service life, the component must be removed from the aircraft for maintenance, or for disposal in the case of components with a certified life limit d)all 9.Unserviceable component 1. expiry of the service life limit as defined in the maintenance program; 2. non-compliance with the applicable airworthiness directives and other continued airworthiness requirement mandated by DGCA; 3. absence of the necessary information to determine the airworthiness status or eligibility for installation; 4. no evidence of defects or malfunctions; 5. involvement in an incident or accident likely to affect its serviceability. a),2,4,5b)1,3c)1,2,3,4,5d)1,2,3,5, 10. “Unsalvageable” 1) components with non-repairable defects, whether visible or not to the nakedeye; 2) components that meet design specifications 3) components subjected to unacceptable modification or rework that is irreversible; 4) certified life-limited parts that have reached or exceeded their certified life limits, or have missing or incomplete records; 5) components that cannot be returned to airworthy condition due to exposure to extreme forces, heat or adverse environment; 6) components for which conformity with an applicable airworthiness directive is traceable a)1,2,6b)3,4,5c)1,3,4,5d)1,2,3,4,5,6 11.MTCS”Mutliation of component” a) grinding,burning,removal of a major lug or other integral feature,permanent distortion of parts is seldom effective b) identification by tag or markings,drilling small holes,sawing in two pieces is best way to mutilate and successfully method c)both are correct d)none is correct 12.In case of car-m organisation for fabrication a)dgca approval is requirement b)agreement with dgca is required c)a+approval BR TC,STC.CAR-21 organisation also required d)all 13. The maintenance organisation manual and its amendments shall be approved by a)DGCAb)local officec)DGCA Regional Office.d)dgca hdqtr 14.MTICS’’Storage facility in case of subpart-f organisation” a) clean, wellventilated b)a+ maintained at an even dry temperature c) Manufacturer’s storage recommendations should be followed d)manufactures instruction is been published in recommendations given by manufacture 15. Segregation means a) storing unserviceable components in a separate secured location from serviceable components b) as in a) and from unsalvageable components c) storing serviceable components in a separate secured location from unserviceable components d) as in c) and from unsalvageable components 16. Limited certifying staff authorisation is issued to a) Aircraft commander b) As in a) and on the basis of the flight crew licence held c) Aircraft Maintenance Engineer d) as in c) and on the basis AME licence held 17. MTICS “Nominated persons” a)practical experience and expertise in the application of aviation safety standards and safe maintenance practices; b)comprehensive knowledge of CAR M & maintenance organisation manual; c) five years aviation experience of which at least three years should be practical maintenance experience d)all is correct except c) instead of five years experience requirement is 3 yrs 18. a) Boroscoping and other techniques such as delamination coin tapping are non-destructive inspections rather than non-destructive testing b) thermography and shearography, should be carried out in accordance with the particular equipment manufacturers’ recommendations c) The referenced standards, methods, training and procedures should be specifiedin the maintenance organisation manual d)all 19.MTCS a)A certificate should not be issued for any component when it is known that the component is unserviceable b)except in the case of a component undergoing aseries of maintenance processes at several approved maintenance organisations c)In such a case clear statement of limitation should be endorsed in block 12. d)all 20. The primary objectives of the organisational review a)to maintain org. Approval continuedb) to ensure that it can deliver a safe product c)b+ approved maintenance organisation remains in compliance with therequirements. d)all 21.MTICS ‘Endangers flight safety’ a) any instance where safe operation could not be assured or which could lead to an unsafe conditionbut b)a+ significant cracking, deformation, corrosion or failure of primary structure, any evidence of burning, electrical arcing, significant hydraulic fluid or fuel leakage c) any emergency system or total system failure. d)An airworthiness directive overdue for compliance is not considered a hazard to flight safety.” 22. “Pilot-owner” hold a valid pilot licence or equivalent b)own the aircraft, either as sole or joint owner c) one of the natural persons on the registration form; or a member of a non-profit recreational legal entity, d)all+ The scope of the limited Pilot-owner maintenance shall be specified in the aircraft maintenance programme. 23.Controlled envoirnment a) continuously managed during the previous 12 months by a unique continuing airworthiness management organisation b) maintained forthe previous 12 months by maintenance organisations c)a+by CAMO d)b+by CAMO 24. When DGCA carries out the airworthiness review and/or issues the airworthiness review certificate itself, the owner or operator shall provide DGCA a) the documentation required by DGCA; and b) suitable accommodation at the appropriate location for its personnel; c)when necessary, the support of personnel appropriately d)all 25.MTCS a) It is acceptable to anticipate the extension of the airworthiness review certificate by a maximum of 30 days without a loss of continuity b) It is acceptable to anticipate the airworthiness review certificate by a maximum of 90 days without a loss of continuity c)both d)only a is correct 26.MTCS a) “Generic” maintenance programme: it is a maintenance programme developed to cover a group of similar types of aircraft. b) “Base line” and “generic” maintenance programmes are not applicable to a particular aircraft registration mark c) A copy of any airworthiness review certificate issued or extended for an aircraft shall be sent to State of Registry within 10 days d)allA copy of any airworthiness review certificate issued or extended for an aircraft shall be sent to State of Registry within 10 days 27.MTICS a) “3 years of appropriate maintenance experience” means 3 years working in an aircraft maintenance environment on at least some of the aircraft type systems b) “3 years of appropriate maintenance experience” means 3 years total maintenance exp. c) A pilot owner should only issue a certificate of release to service for maintenance performed by the pilot owner d) The scope of the limited Pilot-owner maintenance shall be specified in the aircraft maintenance programme 28. Data for modification and repair approved by 1. DGCA 2. As in 1 + CAR 21 / EASA 21 / FAR 21 Production org 3. Both 1 & 2 4. Only 2 is correct 29. CRS to be entered in continuing airworthiness record 1. As soon as Practicable 2. As in 1 + but in no event within 72 hours 3.As in 1 + but in no event more than 30 days 4. As in 3+ after the date of completion of maintenance 30. Authorized Release Document 1. CA Form 1 2. As in 1 + E A S A Form 1 3. FA A 8 130-3 4. All of the above 31. Current states of AD Preserved for 1. 2 years 2. 12 month 3. 24 months 4. Either 1 or 3 33. MOM is approved by 1. DGCA 2. DGCA Local Office 3. DGCA Regional Office 4. Either 2 or 3 34. MTCS 1. Subpart- f approval includes fabrication of parts2. Maint. Org. under CAR-M Subpart F cannot Fabricate parts 3. 1 + Provided they are used within own facilities 4. 3 + as identified in MOE 35. Personnel carrying out specialized tasks shall hold 1. Certificate of compliance 2. Certificate of competency 3. Certificate of course completion 4. Only 1 is correct 36. MTCS 1. Limited certifying staff authorization ( LCA)is issued to a/c commander by the organization 2. 1 + issued to personnel holding ATPL /CPL /FEL 3. 2 + not issued to when a/c is operating away from supported location 4. All of the above 37. CA Form 1 shall not be issued for 1. Components maintained by A rated organization 2. Component maintained by B rated organization 3. Component maintained in a light a/c not used commercial transport 4. All the above 38. Approval of AMO is issued for 1. One year 2.Up to one year 3. Max period of one year 4.Any of the above 39. MTCS 1. Installed service life shall exceed the approved service life 2. Installed service life shall not exceed the approved service life 3. Installed service life shall have no relation with approved service life 40. Components considered unserviceable 1. Expiry of certified life limit2. 1 + non- compliance with Ads 3. 2 + evidence of defects or malfunctions4. None 43. Environmental limitation given in 1. M O E 2. C AME 3. Work card 4. Maintenance Data 44. Defects that would not hazard the flight safety shall be rectified 1. As soon as practicable 2. But in no case with 72 hours 3. But in no event than 30 days 4. Both 1 &2 45.When aircraft operating away from a supported location the organization may issue a limited certifying staff authorization to the a)aircraft commander b)as in a and on the basis of the flight crew licence c)As in b and organization ensures that sufficient practical training has been carried out to ensure that such person can accomplish the task to the required standardd)None Q46. where an aircraft is grounded at a location other than the main base where no appropriate certifying staff is available, the maintenance organisation contracted to provide maintenance support may issue a one-off certification authorization to a)One of its employees holding type qualifications on aircraft of similar technology, construction and systems b)any person with not less than 3 years maintenance experience and holding a valid ICAO aircraft maintenance licence rated for the aircraft type c)Either a or b and in such case report to DGCA within 7 days d)None Q47. Defects that would not hazard the flight safety shall be rectified 1. As soon as practicable 2. But in no case with 72 hours 3. But in no event than 30 days 4. Both 1 &2 48. Component certificate release to service document is a)CA form 10b)CA form 2c)CA form 1d)CA form 3 49. According to CAR M, approved maintenance organisation shall retain a copy of all maintenance records and any associated maintenance data for a)3 yearb)2 yearc)1 yeard)None Q50. According to CAR M ,an ORGINIZATION approval shall be issued for a maximum period of a)1 yrb)2yrc)3yrd)5 yr