NAMP Flashcards

Question

MALS

Answer 1

Marine Air Logístics Squadron

Answer 2

The functional organization within the OMA responsible for workload control

Answer 3

Mission Essential Subsystem Matrix

Answer 4

Naval Aviation Logistics Command Management Information System

Answer 5

Organizational Level Maintenance Activity

Answer 6

Naval Aviation Maintenance Discrepancy Reporting Program

Answer 7

Naval Aviation Maintenance Program

Answer 8

Naval Aviation Technical Data Engineering Services

Answer 9

Naval Flight Record Subsystem

Answer 10

Non combat expenditure allowance

Answer 11

Not Mission Capable

Answer 12

Naval Oil Analysis Program

Answer 13

Optimized Organizational Maintenance Activity

Answer 14

Partially Mission Capable

Answer 15

Planned Maintenance Interval

Answer 16

Quality Assurance

Answer 17

Ready Basic Aircraft Capable of flight in vmc/imc Fcf complete

Answer 18

Safe For Flight The material condition of an aircraft which permits it to be launched, flown and landed safely. And ensures the aircrew at a minimum has the operable equipment for safe flight

Answer 19

Technical Directive A document to provide technical info necessary to properly and systematically inspect or alter the config of aircraft systems or equipment.

Answer 20

Aviation Machinist Mate Engines, transmission, rotor system 110

Answer 21

Aviation Electrician Mate AFCS, Electrical, Wiring, Instrumentation 220

Answer 22

Aviation Structural Mechanic Flight Controls, Hydraulica, Airframes, ECS 120

Answer 23

Aviation Ordinanceman Ordinance, torps, hellfire, cads, cmds 230

Answer 24

Aviation Electronics Technician Mission Systems, Radios, Avionics, secure comms 210

Answer 25

Aviation Maintenance Administrationman

Answer 26

Aviation Survival Equipmentman 13A

Answer 27

Naval Aircrewman

Answer 28

05C/D - Supply/tool 12C - Corrosion 13A - PR’s 020 - Maintenance Control 040 - Quality Assurance 140 - Phase 310 - Line

Answer 29

Collateral Duty Inspector E4 and above Requires completion of apprentice/journeyman

Answer 30

Collateral Duty Quality Assurance Representative E5 and above Qualified to inspect components critical to Safety of Flight

Answer 31

E7 and above (with select set LPO’s) Requires a board for selected individuals Requires completion of wing PQS

Answer 32

Conducted between flights to ensure the integrity of flight to verify proper servicing and to detect degradation Valid for a period of 24 hours from time completed, provided no flight and no other maintenance servicing occurs during this period Does not require sampling Not required between repetitive flight evolutions interspersed with ground periods Turnarounds are more restrictive than daily

Answer 33

Conducted to inspect to a greater depth than turnaround Valid for 72 hours from completion date and time, provided no flight occurs or maintenance action other than servicing has been performed Aircraft may be flown for 24 hours without another daily. The 24 hours cannot exceed the 72 hours unless the expiration occurs during a mission. Turnarounds are not included in daily and must be executed separately CO’s pay authorize PIC to conduct inspection and sign for it while operating away from home without qualified maintenance personnel for periods not exceeding 72 hours

Answer 34

A scheduled inspection with a prescribed interval other than daily or phase Day: +- 3 day tolerance 7,28,56,112,182,224,365,546 day (Don’t plan 365 or 546 at sea) Hours : +- 10% of hours 30,60,525,1000 Additional 10,100 arrestments 5000 rds fired

Answer 35

Conditional maintenance as a result of specific over-limit condition or a result of circumstances or events Engine water wash, post terf, hard landing, post hide, engine over temp, chip lights

Answer 36

An inspection performed at the time a reporting custodian accepts a newly assigned aircraft, from any source including an offsite depot facility

Answer 37

A general inspection of a specific area of aircraft at a scheduled interval. For leaks, frayed cables, cracks, corrosion, or physical damage.

Answer 38

Phase cycle is 800 hours 200 hours between each phase +-10% window

Answer 39

3 Days Corrosion, flight control cables, landing gear, pas cables, #1 LDS, APU, IGB/TGB oil, tail rotor torque

Answer 40

3 days Tail bumper, nose vibes, flight controls, #2 LDS, exhausts, ECS, tail drive shaft, sono system

Answer 41

4 days Corrosion, flight control cables, landing gear, pas cables, #1 LDS, APU, IGB/TGB oil, tail rotor torque

Answer 42

Tail bumper, nose vibe, flight controls, #2 LDS, exhaust, ECS, tail drive shaft, sono, flight controls, MLG fluid change, MRH disassembly, MR damper sys drain

Answer 43

An operational evolution where an aircraft is refueled while the engines are operating

Answer 44

Where the crew is changed while the engine is operating For hot seats, a new aircraft inspection and acceptance record is required. Block 8 - hot seat Block 10 - off coming PIC Block 11 - on coming PIC