CDC 2A353 Volume 5. F-22
85 Questions I 239 Attempts I Created By mike872208 1237 days agoF-22 maintenance
Question Excerpt From CDC 2A353 Volume 5. F-22
| Q.1) |
The F-22 inspection that is accomplished within six hours of launch and only if the preflight is over 48 hours but still valid is the |
| A. |
| B. |
| C. |
| D. |
| Q.2) | Outer mold line inspection will be accomplished on the F-22 when maintenance notices |
| A. |
| B. |
| C. |
| D. |
| Q.3) | On the F-22, the responsibility for all low observable maintenance rests with the |
| A. |
| B. |
| C. |
| D. |
| Q.4) | The purpose of the SAS is to outline the repair and restoration process, reliability, and maintainability data collection, and time accounting for the managing the F-22's. |
| A. |
| B. |
| C. |
| D. |
| Q.5) | On the F-22, what is the output pressure for the hydraulic system's pump? |
| A. |
| B. |
| C. |
| D. |
| Q.6) | On the F-22 hydraulic system, what service coupling quick disconnect provides an alternate method to fill the hydraulic reservoir? |
| A. |
| B. |
| C. |
| D. |
| Q.7) | On the F-22, what prevents the maintainer from installing the filter bowl without a filter element inside? |
| A. |
| B. |
| C. |
| D. |
| Q.8) | On the F-22 hydraulic control software monitors, the hydraulic system is hosted by the |
| A. |
| B. |
| C. |
| D. |
| Q.9) | On the F-22, what performs the BIT on the hydraulic components? |
| A. |
| B. |
| C. |
| D. |
| Q.10) | On the F-22, the pressure transducer operates over a pressure range of |
| A. |
| B. |
| C. |
| D. |
| Q.11) | On the F-22, what provides the maintainer an indication that the filter element requires replacement? |
| A. |
| B. |
| C. |
| D. |
| Q.12) | The mode on the F-22 that uses the pneumatic backup system to pressurize the unlock devices to release the landing gear for extending and locking it into position is |
| A. |
| B. |
| C. |
| D. |
| Q.13) | On the F-22, a base plate and two interchangeable brake modules make up what valve? |
| A. |
| B. |
| C. |
| D. |
| Q.14) | On the F-22, the wheels and tires are protected from excessive brake heat by a heat shield made out of |
| A. |
| B. |
| C. |
| D. |
| Q.15) | The F-22 nose wheel may normally be turned up to 48 depending on |
| A. |
| B. |
| C. |
| D. |
| Q.16) | In the F-22 nose wheel steering system, what valve allows free castering of the nose wheel? |
| A. |
| B. |
| C. |
| D. |
| Q.17) |
The F-22 arresting gear system is pneumatically actuated and controlled |
| A. |
| B. |
| C. |
| D. |
| Q.18) | The F-22's engine fan variable vanes position is controlled by |
| A. |
| B. |
| C. |
| D. |
| Q.19) |
The engine on the F-22 contains three assemblies; external hardware, supporting ring and the fan bypass ducts that are referred to as |
| A. |
| B. |
| C. |
| D. |
| Q.20) | The F-22's engine lube system contains oil in the bearing compartment by using |
| A. |
| B. |
| C. |
| D. |
| Q.21) |
The F-22's primary source of power for the full authority digital electric control, the comprehensive diagnostic unit, and the ignition exciters is the |
| A. |
| B. |
| C. |
| D. |
| Q.22) |
The F-22 program that acquires data for engine mission capability, on-board diagnostic system failures, propulsion data, and characterizing mission usage is the |
| A. |
| B. |
| C. |
| D. |
| Q.23) | IMIS displays input screens to enable the maintainer to enter suspected |
| A. |
| B. |
| C. |
| D. |
| Q.24) | The presence of an overheat on the F-22 is reported for display in the cockpit by the |
| A. |
| B. |
| C. |
| D. |
| Q.25) | The presence of a fire in the F-22 engine or APU compartment is reported to the fire protection module by the |
| A. |
| B. |
| C. |
| D. |
| Q.26) | On the F-22, what components take care of the on-board engine monitoring diagnostic functions? |
| A. |
| B. |
| C. |
| D. |
| Q.27) | Vibrations, oil debris, oil level signals, along with condition monitoring and fault information, are stored in the F-22's resident memory of the |
| A. |
| B. |
| C. |
| D. |
| Q.28) | The fan and compressor vaiable vanes, as well as the modulated exhaust cooling and exhaust nozzle make up the F-22's engine |
| A. |
| B. |
| C. |
| D. |
| Q.29) | The F-22 engine monitoring system uses how many temperature sensors? |
| A. |
| B. |
| C. |
| D. |
| Q.30) | The F-22 system component that provides all electrical interconnects between the vehicle management system modules and the aircraft wiring connectors is the |
| A. |
| B. |
| C. |
| D. |
| Q.31) | The primary flight control surfaces, engine inlet bypass louvers, nose wheel steering, engine thrust and thrust vectoring all receive commands generated by the |
| A. |
| B. |
| C. |
| D. |
| Q.32) | The F-22 unit designed to detect abd shutdown and over-voltage condition is the |
| A. |
| B. |
| C. |
| D. |
| Q.33) | The F-22 program that deals with the computer software configuration for the respective aircraft system is |
| A. |
| B. |
| C. |
| D. |
| Q.34) | Normal start and normal operating state are the two sytem operations of the |
| A. |
| B. |
| C. |
| D. |
| Q.35) | When F-22 hydraulic pressure is lost the ailerons are |
| A. |
| B. |
| C. |
| D. |
| Q.36) | The F-22 pitch system is augmented by |
| A. |
| B. |
| C. |
| D. |
| Q.37) | The three-position, momentary action, center off switch on the F-22 flight control system panel is for the |
| A. |
| B. |
| C. |
| D. |
| Q.38) |
The landing gear handle controls flap setting when norm is selected on the F-22s |
| A. |
| B. |
| C. |
| D. |
| Q.39) | F-22 lift augmentation is performed by |
| A. |
| B. |
| C. |
| D. |
| Q.40) | The F-22 leading edge flap position is based on AOA, Mach and altitude information computed by the |
| A. |
| B. |
| C. |
| D. |
| Q.41) | ON the F-22, which valve allows aerioal refuel flow to the aircraft plumbing and prevents flow in the reverse direction? |
| A. |
| B. |
| C. |
| D. |
| Q.42) | The primary integrated maintenance information tool used by F-22 technicians during the performance of maintenance task is the |
| A. |
| B. |
| C. |
| D. |
| Q.43) | All PMS screens are provided guaranteed communication through the |
| A. |
| B. |
| C. |
| D. |
| Q.44) | The two major components that must be installed on the PMS for the F-22 are the battery pack and |
| A. |
| B. |
| C. |
| D. |
| Q.45) | The F-22's PMA battery pack can increase the battery life in cold temperatures and facilitate effective charging of the battery with the use of |
| A. |
| B. |
| C. |
| D. |
| Q.46) | The function of the PMA that shows a listing of all discrepancies and warnings for a particular aircraft is the functional category of |
| A. |
| B. |
| C. |
| D. |
| Q.47) | The F-22 support equipment that is built from predominantly commercial off the self items |
| A. |
| B. |
| C. |
| D. |
| Q.48) | The system designed to be used in amintenance units, maintenance operation centers, and off equipment maintenance ship is |
| A. |
| B. |
| C. |
| D. |
| Q.49) | The F-22 component that communicates with the MSC and PMA to provide a single source of information to meet the requirements of maintenance personnel is the |
| A. |
| B. |
| C. |
| D. |
| Q.50) | The F-22 MVI cable provides the electrical interconnect between the PMA and the |
| A. |
| B. |
| C. |
| D. |
| Q.51) | Access to the required technical data is provided when the user selects the |
| A. |
| B. |
| C. |
| D. |
| Q.52) | The primary source for introducing the F-22's operational flight program is the |
| A. |
| B. |
| C. |
| D. |
| Q.53) | The F-22 diagnostics are controlled by the |
| A. |
| B. |
| C. |
| D. |
| Q.54) | The system the F-22 uses for avionics cooling during ground maintenance is |
| A. |
| B. |
| C. |
| D. |
| Q.55) | It is imprtant to keep the hydraulic test stand as far away as possible from the flight control travel path to prevent |
| A. |
| B. |
| C. |
| D. |
| Q.56) | The stored energy system servicing carts surfaces remain hot after shutdown for up to how many minutes? |
| A. |
| B. |
| C. |
| D. |
| Q.57) | The F-22 generator control units receive their power from the |
| A. |
| B. |
| C. |
| D. |
| Q.58) |
The main generator control units on the F-22 are cooled by what kind of air? |
| A. |
| B. |
| C. |
| D. |
| Q.59) | The interface between the electrical power system generators and the electrical power subsystem on the F-22 is the |
| A. |
| B. |
| C. |
| D. |
| Q.60) | For temerature control, the F-22 uses bleed air, ram air, polyalphaolefin and |
| A. |
| B. |
| C. |
| D. |
| Q.61) | The F-22 system that dehumidifies the pre-cooled air utilizing a boot strapped compressor, turbine, and water collector is the |
| A. |
| B. |
| C. |
| D. |
| Q.62) | The F-22 cockpit distribution and defog system provides air for the canopy seal, cockpit pressurization , canopy defog and the |
| A. |
| B. |
| C. |
| D. |
| Q.63) | The back-up air supply for the F-22's forced air cooled avionics system is |
| A. |
| B. |
| C. |
| D. |
| Q.64) | The three methods for opening the F-22 canopy are |
| A. |
| B. |
| C. |
| D. |
| Q.65) | The external canopy control switch on the F-22 is located |
| A. |
| B. |
| C. |
| D. |
| Q.66) | Manual operation of the F-22 canopy with a high speed/low torque, non-impact type pneumatic or battery powered tool will open or close the canopy in |
| A. |
| B. |
| C. |
| D. |
| Q.67) | How many minutes is the F-22 ejection seat emergency oxygen bottle capable of providing the pilot with oxygen for? |
| A. |
| B. |
| C. |
| D. |
| Q.68) | In the avionics hardware architecture of the F-22, the item that sends information to the line replacable units (LRU) is the |
| A. |
| B. |
| C. |
| D. |
| Q.69) | The F-22's vehicle management system, utilites and subsystems, and the avionics system are all supported by the |
| A. |
| B. |
| C. |
| D. |
| Q.70) | The F-22 is provided pneumatic, hydraulic, and electrical power during emergencies and within operating envelope by the |
| A. |
| B. |
| C. |
| D. |
| Q.71) | The two ways maintainers can start the F-22 APU are the |
| A. |
| B. |
| C. |
| D. |
| Q.72) | When using the PMA to start the APU, the maintainer needs to verify the SES air pressure protective covers are removed and the |
| A. |
| B. |
| C. |
| D. |
| Q.73) | During ground shutdown the APY on the F-22 enters a cool-down cycle of |
| A. |
| B. |
| C. |
| D. |
| Q.74) | The air turbine starter system, airframe mounted accessory drive, and power take-off shaft make up the F-22's |
| A. |
| B. |
| C. |
| D. |
| Q.75) | The F-22's air recharge compressor provides air to the |
| A. |
| B. |
| C. |
| D. |
| Q.76) | The air storage bottles on the F-22 provide air to the APU door actuation system and the |
| A. |
| B. |
| C. |
| D. |
| Q.77) | The SES on the F-22 uses aircraft fuel and high pressure air to power the |
| A. |
| B. |
| C. |
| D. |
| Q.78) | Emergency gear swings and arresting gear operations effects the F-22 SES by |
| A. |
| B. |
| C. |
| D. |
| Q.79) | On the F-22, how many pumps are attached to the AMAD? |
| A. |
| B. |
| C. |
| D. |
| Q.80) | On the F-22, what in the lubrication system pressurizes the AMAD to 5 psi above ambient pressure? |
| A. |
| B. |
| C. |
| D. |
| Q.81) | On the F-22, the weapons bay door drive slows doors prior to reaching travel limits to prevent |
| A. |
| B. |
| C. |
| D. |
| Q.82) | The oil level on the F-22's PDU is checked by a |
| A. |
| B. |
| C. |
| D. |
| Q.83) | The two configurations the F-22 pylons are built for are |
| A. |
| B. |
| C. |
| D. |
| Q.84) | The purpose of the AVEL on the F-22 is to stow and launch the |
| A. |
| B. |
| C. |
| D. |
| Q.85) | the F-22 weapon system minimizes barrel erosion and heat generation; thus extending the life of the system by |
| A. |
| B. |
| C. |
| D. |
Take this quiz by clicking Start button on top.
Related Topics
More Quizzes by mike872208
- Volume 3. CDC 2A353 - F-16/F-117 Aircraft Maintenance
- Fighter Aircraft Maintenance Volume 4. A-10/U-2/UAV (RQ-1)
- Volume 1 Aircraft Maintenance General Subjects
