The QL II system consists of an automatic electronic support measure (ESM) collection and processing system installed in an RV-1D aircraft with necessary support equipment mounted in ground-based vehicles. Figure 1 shows the aircraft and the Flight Line Test Set AN/ALM-154 (which is replaced by the Cockpit Display and Control System PIP). The support equipment is used for system checkout, fault diagnosis, automatic data processing (ADP) peripheral support, and incidental maintenance tasks. The QL II system is comprised of six major components.
Product Improvement Test (PIT) on the AN/ALQ-133 QUICK LOOK II Cockpit Display and Control System Product Improvement Program
1987
77 pages
Report
No indication
English
Electromagnetic & Acoustic Countermeasures , Aircraft , Electronic support measures , Reconnaissance aircraft , Display systems , Cockpits , Control systems , Data processing , Faults , Airborne , An/alq-133 , Quick look project , Pit(Product improvement test) , Rv-1d aircraft , An/alm-154 , Lpn-tradoc-87-ot-isbd-1220