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AERONAUTICAL ENGINEERING MAINTENANCE MANAGEMENT MANUAL > SWE Questions > Flashcards

SWE Questions Flashcards

1
Q

M 13020.1G

A

AERONAUTICAL ENGINEERING MAINTENANCE MANAGEMENT MANUAL

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2
Q

It is the ______________ responsibility to ensure that maintenance is completed in an orderly and timely manner to meet the assigned mission requirements.

A

Commanding Officer’s

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3
Q

Three basic elements comprise the aeronautical maintenance system:_______ _______ ________.

A

a. management element,
b. technical element,
c. production element.

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4
Q

Standardized maintenance improves overall maintenance _________ _________ ________.

A

quality, capability, and reliability.

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5
Q

____________ ________ is the ability of a unit to maintain assigned equipment in serviceable condition and proper configuration

A

Maintenance capability

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6
Q

The overall maintenance philosophy determines both the ________ and________ level maintenance capabilities.

A

depot , organizational

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7
Q

___________________ must gauge their maintenance capability when planning to meet mission requirements

A

Engineering Officers

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8
Q

NMCS

A

is Not Mission Capable due to Supply.

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9
Q

NMCT

A

Not Mission Capable Total = NMCM + NMCS + NMCD (units).

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10
Q

NMCM

A

is Not Mission Capable due to Organizational-level Maintenance.

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11
Q

NMCD

A

(units) reflects the portion of Not Mission Capable Time due to Depot-Level Maintenance which is performed at a unit.

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12
Q

The ______________ is responsible for financial planning, preparation of budget requirements, and controlling expenditures within budget allocations.

A

Engineering Officer

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13
Q

Operating aviation units receive funds under ________.

A

AFC-30

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14
Q

________________ have final authority regarding the sub-allocation of funds to various departments.

A

Commanding Officers

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15
Q

All cannibalization actions shall be authorized by the _________________ or his/her designated representative

A

Engineering Officer

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16
Q

(PQDR)

A

PRODUCT QUALITY DEFICIENCY REPORT

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17
Q

All changes or modifications to aircraft must

be reviewed by the appropriate technical authority at _____ and approved via the ACCB process.

A

ALC

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18
Q

Urgent safety of flight materiel defects should be submitted in _________ format.

A

message

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19
Q

Prototype installations are authorized by the ____________.

A

Commandant (CG-41)

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20
Q

A trial installation is normally performed by the __________.

A

Prime Unit

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21
Q

Functional checks are divided into _____________, ___________, ______________.

A

A. ground checks,
B. flight verification checks,
C. test flights,

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22
Q

Visual inspection and functional checks performed on the ground

A

ground checks

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23
Q

Airborne functional checks, conducted during a scheduled operational or training mission, for components or systems whose failure would neither adversely affect flight safety nor seriously affect mission accomplishment.

A

flight verification checks

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24
Q

Airborne functional checks to establish if an airframe or equipment, when subjected to design environment, is operating properly.

A

test flights

25
Q

Any aircraft having undergone maintenance requiring a functional check or test flight must be ________________.

A

maintenance released

26
Q

The _______________ is authorized to maintenance release aircraft at their unit.

A

Engineering Officer

27
Q

A complete test flight is required:

A

(a) After extended aircraft storage
(b) After completion of major structural rework, including Programmed Depot Maintenance (PDM)
(c) As indicated by maintenance procedure cards or technical manuals
(d) Prior to delivery of aircraft to a PDM facility (see the Aeronautical Engineering Maintenance Management Process Guide, CGTO PG-85-00-110, Chapter 5)
(e) At the discretion of the Engineering Officer

28
Q

Partial test flights are required:

A

(a) As indicated by MPCs, maintenance instructions, or applicable T.O.s
(b) Flight control disassembly or replacement of any portion
of a flight control system (for example: elevators, rudders, ailerons, trim tabs, rotor head and blades, tail rotor gearbox and blades, control cables, bearings, fairleads, pulleys, rods, servo system, etc.)

29
Q

_______________________ should be assigned as a part of the flight crew when practical.

A

Quality Assurance Inspector

30
Q

Coast Guard _______________ are responsible for their unit’s programs and shall ensure that they are
in compliance with all federal, state, and local environmental laws and regulations.

A

Commanding Officers

31
Q

The ____________ is responsible for ALC shop space management and providing technical information and data to other ALC divisions, Headquarters, and other operating units.

A

Engineering Services Division (ESD)

32
Q

The purpose of providing a designated ___________ is to ensure a centralized point for technical responsiveness to field level maintenance management of a specific aircraft type or aviation life support equipment.

A

“Prime Unit”

33
Q

The _________ develops, reviews, and updates MPCs

and MTCs as necessary to ensure that all field level maintenance is accomplished with optimum efficiency.

A

Prime Unit

34
Q

Class _-level maintenance is also a part of the DoD “Intermediate Maintenance.” The work performed consists of the routine day-to-day upkeep required by shop facilities.

A

D

35
Q

Intermediate Maintenance

A

Class C-level

36
Q

All unit avionics shops are required to maintain an in-house capability for avionics repair at the Class _-level.

A

C

37
Q

are used to disseminate technical aeronautical information required for the operation and maintenance of USCG aircraft and support equipment.

A

Technical Orders (TO)

38
Q

PRECEDENCE OF DIRECTIVES.

A
  1. Asset Computerized Maintenance System (ACMS) 2. Coast Guard TOs
  2. Air Force TOs
  3. Navy TOs
  4. Army TOs
  5. Commercial Publications
39
Q

Use of electronic data (manuals) from the NATEC website shall be the _________ source for Coast Guard aviation maintenance functions.

A

primary

40
Q

When conflict of information exists, _____________ shall take precedence over CGTOs, which take precedence over other DoD publications.

A

ACMS MPCs

41
Q

generally require a physical change to an aircraft or a special, urgent, or repeated inspection requiring compliance within specified time limits.

A

Time Compliance Technical Orders (TCTO)

42
Q

Preflight Inspection

A

accomplished prior to the first flight of the day and remains effective for 24 hours

43
Q

Thruflight Inspection

A

accomplished as a turnaround inspection prior to takeoff on the second and each subsequent flight of the day

44
Q

Postflight Inspection

A

accomplished after the last flight of the flying period.

45
Q

_______________ are certain additional inspections, distinct in frequency from routine inspections, which are conditional upon operational environment, specific incidents, or other circumstances requiring inspections.

A

Special inspections

46
Q

Maintenance items may be delayed at the discretion

of the Commanding Officer or their designated representative as specified in the ACMS ____.

A

MDL

47
Q

Mandatory Special Requirements (MSR) shall _____ be extended.

A

not

48
Q

Completed MPCs will be retained for ___ days; then they may be discarded.

A

90

49
Q

Maintenance errors contribute to approximately ___ % of DoD and commercial aviation mishaps.

A

20

50
Q

MRM training is required _________ (every _ years)

A

biennially , 2

51
Q

_____ initial training is required before performing or authorizing maintenance on Coast Guard aircraft.

A

MRM

52
Q

The terms __ Condition, RFI, and serviceable are used interchangeably.

A

A

53
Q

The terms __ Condition, NON-RFI, and unserviceable are used interchangeably.

A

F

54
Q

If repair cannot be accomplished utilizing the district repair and calibration program, replacement, exchange, or repair may be requested via ___.

A

ALC

55
Q

ATC Mobile is the ______ Prime Unit.

A

ALSE

56
Q

Each salvage plan shall be updated ______.

A

annually

57
Q

__________ are marginally adequate for recovering HH-65/MH-65 helicopters.

A

Buoy tenders

58
Q

When removal of components is required, but disassembly of aircraft components is not involved, and semi-portable or bench-type equipment is required, the function is classified to the __ level.

A

D

59
Q

When removal of components is required and disassembly of aircraft components is involved or light installed job-shop type equipment is required, the function is classified to the __ level.

A

C

AERONAUTICAL ENGINEERING MAINTENANCE MANAGEMENT MANUAL (1 decks)

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