Term
| The maximum allowable registration error allowed is__ ft. of azimuth at ___, which can be estimated by using the open area of the LOS reticule, which is equivalent to ___________ at _______________. |
|
Definition
| The maximum allowable registration error allowed is 1 FOOT of azimuth at 90 FEET, which can be estimated by using the open area of the LOS reticule, which is equivalent to 1 FOOT AT 90 FEET. |
|
|
Term
| The internal boresight shall be performed as part of preflight procedures prior to _____________ or weapons using the MTADS |
|
Definition
| The internal boresight shall be performed as part of preflight procedures prior to using the MTADS |
|
|
Term
| Boresight aligns MTADS ____ to the ____ LOS and ____ to the ____ LOS. |
|
Definition
| Boresight aligns MTADS DTV to the LASER LOS and FLIR to the DTV LOS. |
|
|
Term
| Can the internal boresight be performed in flight? |
|
Definition
Can the internal boresight be performed in flight? YES, DUH
|
|
|
Term
| Manual Servo Drift Null may reduce TADS turret slew rates by up to ________ |
|
Definition
| Manual Servo Drift Null may reduce TADS turret slew rates by up to 50% |
|
|
Term
| During a TADS Drift Null, the aim point should remain within the NFOV DTV for |
|
Definition
| During a TADS Drift Null, the aim point should remain within the NFOV DTV for30 SECONDS |
|
|
Term
| During a TADS Electronic Unit failure the pilot is limited to ___ degrees in azimuth on the PNVS, and the message _________ will be displayed in the HAD. |
|
Definition
| During a TADS Electronic Unit failure the pilot is limited to +/- 75 DEGREES in azimuth on the PNVS, and the message PNVS DIRECT will be displayed in the HAD. |
|
|
Term
| Internal errors can develop in-flight due to temperature changes within the internal components of the TADS Thermal Drift. When confidence in the boresight is suspect, an internal boresight should be accomplished. Recommended every ______________________________________. |
|
Definition
| Internal errors can develop in-flight due to temperature changes within the internal components of the TADS Thermal Drift. When confidence in the boresight is suspect, an internal boresight should be accomplished. Recommended every 2 times in 2.5 flight hours |
|
|
Term
If the pilot selects TADS, either with the
NVS select switch or linking the TADS to
the FCR, while the CPG is sight select
TADS _______________________ |
|
Definition
| If the pilot selects TADS, either with the NVS select switch or linking the TADS to the FCR, while the CPG is sight select TADS, the CPG’s sight will default to HMD and weapons will be de-actioned. |
|
|
Term
| What three things will cause the LOS reticle on flight symbology to flash? |
|
Definition
What three things will cause the LOS reticle on flight symbology to flash?
1. LOS INVALID
2. SENSOR LIMITS
3. GUN FAIL & NOT FOLLOWING CREWMEMBER'S HEAD
|
|
|
Term
| During single DP operations, both crew stations share common symbology and imagery on their HMDs. If both crewmembers have NVS mode switch to NORM or FIXED, which symbology and imagery will be presented on the HMDs? |
|
Definition
| During single DP operations, both crew stations share common symbology and imagery on their HMDs. If both crewmembers have NVS mode switch to NORM or FIXED, which symbology and imagery will be presented on the HMDs? The symbology and imagery of the pilot will be displayed. "PLT FORMAT' displayed in HDU |
|
|
Term
| What do flashing IAT gates indicate? |
|
Definition
| What do flashing IAT gates indicate? IMPENDING BREAKLOCK |
|
|
Term
| If the IAT breaks lock and the LMC was turned on prior to activation the IAT, will the LMC be on after the IAT breaks lock? |
|
Definition
If the IAT breaks lock and the LMC was turned on prior to activation the IAT, will the LMC be on after the IAT breaks lock?
Yes, and LOS will continue to move at the last commanded slew rate |
|
|
Term
| TRUE/FALSE - No lead angle compensation is produced by the WP with the IHADSS as the selected LOS. |
|
Definition
TRUE - No lead angle compensation is produced by the WP with the IHADSS as the selected LOS.
|
|
|
Term
When the CPG is in HMD or NVS NORM mode, cueing is selected by _____________________________________________on the RH grip. |
|
Definition
When the CPG is in HMD or NVS NORM mode, cueing is selected by PRESSING THE SLAVE BUTTON on the RH grip. |
|
|
Term
| The PLT's HMD cueing will always remain on unless the PLT deselects cueing on the ____________ page CUEING button at R1. |
|
Definition
| The PLT's HMD cueing will always remain on unless the PLT deselects cueing on the WPN UTIL page CUEING button at R1. |
|
|
Term
| The maximum autonomous designation range for DTV Autotrack is ___ |
|
Definition
| The maximum autonomous designation range for DTV Autotrack is 6 KM |
|
|
Term
| The maximum autonomous designation range for DTV Manual track ___ |
|
Definition
| The maximum autonomous designation range for DTV Manual track 4 KM |
|
|
Term
| The maximum autonomous designation range for FLIR Autotrack is ____ |
|
Definition
The maximum autonomous designation range for FLIR Autotrack is 3.5 KM
|
|
|
Term
| The maximum autonomous designation range for FLIR Manual track___ |
|
Definition
The maximum autonomous designation range for FLIR Manual track 3 KM
|
|
|
Term
| What does the LRFD in the "Last" position do? |
|
Definition
| What does the LRFD in the "Last" position do? WP uses last laser return logic for solutions |
|
|
Term
| What is the maximum PRF laser frequency that may be entered? |
|
Definition
What is the maximum PRF laser frequency that may be entered? 1788
|
|
|
Term
| Squeezing the laser trigger to the second detent does what? |
|
Definition
| Squeezing the laser trigger to the second detent does what? Activates the laser transmitter for ranging and target designation. |
|
|
Term
| Can the BACKSCATTER inhibit be overridden by the trigger's second detent? |
|
Definition
Can the BACKSCATTER inhibit be overridden by the trigger's second detent? NO
|
|
|
Term
| List the seven laser related missile performance detractors: |
|
Definition
List the seven laser related missile performance detractors:
1. Backscatter
2. Underspill
3. Boresight error
4. Beam Divergence
5. Attenuation
6. Spot Jitter
7. Overspill
|
|
|
Term
| Backscatter is generally caused by ____ |
|
Definition
Backscatter is generally caused by a portion of the laser energy reflected off atmospheric particles in the laser path back toward the designator while the remainder of the laser energy penetrates towards the target. |
|
|
Term
| What are some techniques to overcome Backscatter? |
|
Definition
What are some techniques to overcome Backscatter?
Maintain true target in FOV; stop lasing, then redesignate; reposition; offset lasing; use remote designator; fire LOAL (2 second delay lase after launch); |
|
|
Term
| A solid asterisk is displayed in front of the range indicates |
|
Definition
| A solid asterisk is displayed in front of the range indicates receiving valid range data |
|
|
Term
| A flashing asterisk in the *XXXX message indicates a _____ |
|
Definition
A flashing asterisk in the *XXXX message indicates a multi-target condition is detected |
|
|
Term
| How many bursts of laser energy are fired when pulling the RH grip trigger to the first detent? |
|
Definition
How many bursts of laser energy are fired when pulling the RH grip trigger to the first detent? THREE BURSTS OF LASER ENERGY IN ONE SECOND
|
|
|
Term
[image]
WHAT DOES THIS SYMBOL INDICATE? |
|
Definition
|
|
