4790.2a tool control

Section 1 lists all naval forms; section 2, all naval publi- cations; and section 3, all naval technical directives. Prevention and repair of corrosion damage to aircraft and avionic systems continues to be an ever increasing cost and safety burden for military aircraft. Equipment is routinely exposed to changes in temperature and pressure, varying humidity levels, dust, dirt, ultraviolet light, aircraft fluids, and environments that promote corrosion. Increasing environmental and safety restrictions, which limit traditional corrosion control materials, are also a significant factor in the safe and economic operation of aircraft and avionics.

This volume provides cleaning and corrosion control procedures for aircraft. This volume provides cleaning and corrosion control procedures for avionics and electronics. This manual is applicable to all naval aircraft hydraulic systems, airborne hydraulic equipment, and related hydraulic servicing and test equipment.

It is required reading for all military and civilian personnel at all levels of maintenance, performing any hydraulic maintenance function on naval aircraft systems, airborne hydraulic equipment and related support equipment SE. The purpose of this manual is to provide general requirements for maintenance of aircraft hydraulic systems and related SE. This manual is intended for all levels of maintenance, ashore and afloat, but contains detailed information for the organizational and intermediate levels only.

Use this manual as a guide for all corrosion control and maintenance. The materials and procedures contained in this manual are authorized for use in the cleaning, preservation, and corrosion control of SE. Read the MMP located on the sharepoint under the maintenance tab. Read the required reading for the work center. Individual responsibility with respect to quality maintenance. It is the responsibility of the individual to be knowledgeable in maintenance procedures and publications to ensure quality maintenance is preformed.

Purpose and function of the CDI. The CDI is in place to inspect all work and comply with QA inspections within their respective work center. They are responsible to the QA rep. This inspection is normally done by a CDI and is done to determine the condition, proper identification, maintenance requirements, disposition, and accuracy of accompanying records and documents on the item being received. Definition and purpose of In process inspections. This is a specific QA function required during the maintenance process because the required information is not determinable after the process has been completed.

An example of such a process is applying a torque specification to a bolt. Definition and purpose of Final inspections. This is a specific QA function after a maintenance process to determine quality and proper completion of a task.

The chain of responsibility for the CDI when performing inspection and maintenance. Types of inspections that cannot be performed by a CDI. ATAF at the beginning and end of shift or whenever there is a work stoppage, inspect tools upon signing in and out, responsible to the work center supervisor for all matters involving the cool control program, maintain tools and tool containers and ensure they are FOD free at all times, conduct semiannual inventory of tool containers and consult with TCP coordinator, and ensure tools are properly marked.

Engineering investigations apply to all aircraft and weapon systems, subsystems, equipment, components, related SE, special tools, software, fluids, and materials used in equipment operation. Provide an investigation process to determine the cause and depth of fleet reported material failures. Support investigations of material associated with aircraft mishaps, lightning strikes, electromagnetic interference, and stray voltage problems.

Provide engineering assistance for any fleet material problem. Define and discuss the purpose of the QDR program. Failures must have occurred with no operating time. The failure must occur during installation, operation, or first flight.

CAT 1 PQDR- used for all deficiencies that would cause great bodily harm, cause the loss of or major damage to the weapon system or equipment, restrict the combat readiness of the unit, or result in a production line stoppage. CAT2 PQDR- used for deficiencies assessed to have widespread effect without any immediate threat to personnel, equipment, or combat readiness.

Purpose of the tool control program. The TCP provides a procedure and method for storing, immediate inventorying, replacing, controlling, and properly maintaining hand tools.

The primary objective of the TCP is to enhance safety by preventing uncontrolled tools and minimizing replacement costs. We weren't able to detect the audio language on your flashcards. Please select the correct language below. Add to folder [? Find out how you can intelligently organize your Flashcards. You have created 2 folders.

Please upgrade to Cram Premium to create hundreds of folders! While addressing the problem at maintenance organisation, the total servicing time of aircraft for the existing conditions was first calculated. The various CDM provides the airlines and the FAA with real-time access to information such as weather, equipment a Ability to coordinate and evaluate planned and unplanned F engine requirements, adjust plans, forecast and schedules for the actions needed in providing l The afterburner is a further enhancement and a tool used to substantially increase the thrust producing capabilities of a jet engine.

The historical significa The main deciders are the items being degenerated most on the aircraft. When the item is no longer functional it is termed to have implied failure, and a com Introduction This paper is an individual report, it includes a background of airline industry and why is quality important in this industry.

It also include Type certification stipulates that an FAA certified aircraft manufacturer, such as GE Aviation, must receive design approval, production approval, and airwor Flashcards FlashCards Essays.

Create Flashcards. Share This Flashcard Set Close. Please sign in to share these flashcards. We'll bring you back here when you are done. Sign in Don't have an account? Set the Language Close. Flashcards » Add to Folders Close. Please sign in to add to folders. Upgrade to Cram Premium Close. Upgrade Cancel. Related Essays Cssna Aircraft Case Study While addressing the problem at maintenance organisation, the total servicing time of aircraft for the existing conditions was first calculated.

Case Study: F Engine Requirements Ability to coordinate and evaluate planned and unplanned F engine requirements, adjust plans, forecast and schedules for the actions needed in providing l Jet Engine History The afterburner is a further enhancement and a tool used to substantially increase the thrust producing capabilities of a jet engine.

Case Study Of Etihad And The Airline Industry Introduction This paper is an individual report, it includes a background of airline industry and why is quality important in this industry.

Please upgrade to Cram Premium to create hundreds of folders! Mission is to enhance and sustain the combat readiness and mission capability of supported activities by providing quality and timely material support. A process to ensure that assets continue to do what their users require in their present operating context. Flashcards FlashCards Essays. Create Flashcards. Share This Flashcard Set Close. Please sign in to share these flashcards. We'll bring you back here when you are done.

Sign in Don't have an account? Set the Language Close. Aviation Maintenance Administrationma Add to Folders Close. Please sign in to add to folders. Upgrade to Cram Premium Close. Upgrade Cancel. Shuffle Toggle On. Card Range To Study through. Naval Aviation Maintenance Program. NAMP created when? At least 20 minutes to let the vertical gyros completely stop. What is hydraulic fluid used for when listed in the daily deck as a consumable?

Stationed at the rotor arc ready to greet the HAC and inform them of any discrepancies. How long before the crew is scheduled to preflight should you start the PC preflight? Check all systems, components, and quantities to find possible gripes before the crew walks. When you take fuel samples what are you looking for in the fuel sample? Drain fuel into container to remove contamination from trapped fuel areas MRC Card 2. What do you want to make certain of when approaching an aircraft with hung landing gear?

How many chip detectors are on the Aircraft? Where are they? Which ones have special characteristics? Identifies the necessary blade pitch position required for pitch lock engagement NFM 2.

Who should be on the flight line to recover aircraft in T-1? What must be done if the APP is to be operated with the cover open? What do the following acronyms stand for? Who is required to observe an aircraft move in and out of the hangar? What are the selector valve positions on the hand pump Airman Pump aft of the personnel door? Accumulator 1 NFM 2. Ground truck, aircraft and nozzle properly Remove covers on top of sponsons Insert suction hose When complete with suction, refuel the remainder of the tank through the drain valve on bottom of the tank GAI WP 12 Pg 9.

How long do you have to wait after shutting down the heater before securing the APP? Where do you find the weights for fuel, and why is that important? It is important to know because the aircraft fuel gages are weight oriented. If an aircraft is cold fueled, you need to know how much a gallon of fuel weighs in order to convert weight to gallons for the fuel truck operator. A speed control lever out of shut-off The gust lock is engaged The pylon is unsafe for flight The MGB oil pressure switch is pressurized.

Center section of the cabin overhead On the rotor brake reservoir by pushing down on the plunger NFM 2. To provide hydraulic pressure for rotor head positioning, blade fold, and pylon fold selector valves.

NFM 2. What is the purpose of the isolation valve? When is the isolation valve open? The isolation valve closes and renders U1 subsystems inoperative in flight, except when a subsystem is activated.

On deck the isolation valve remains open continuously with electrical power applied to the aircraft. When starting the APP, at what point do you have fire detection? At what point during an APP start do you have fire protection?

Where do you find a list of acceptable substitutes for servicing fluids? How do you properly service the windshield washer reservoir?