TM 1-1520-238-109-20 Change 9Section II. MISSION EQUIPMENT9.16 MISSION EQUIPMENT FAILURES ANDMALFUNCTIONS.Emergency operation of mission equipment is con-tained in this section, insofar as its use affects safety offlight.9.16.1 Wing Stores Jettison.CAUTIONDo not jettison Hellfire missile if hang-fire is in progress (i.e. missile is still ig-nited).a. Armament Wing Stores.1. Airspeed–120KIASmaximum.2. SelectedSTORESJETTswitches–Activate.OR3. STJETT–Press.b. External Fuel Wing Stores.1. Airspeed–100KIASmaximum.2. SelectedSTORESJETTswitches–Activate.OR3. STJETT–Press.9.16.2 ENCU Malfunction.1. ENCU switch – OFF.2. ECS panel – STBY FAN if desired.3. Emergency crew station ventilator door –Open if desired.9.16.3 PNVS/IHADSS Failure.WARNINGIf night or simulated night NOE, reac-tion to the following malfunctions mustbe immediate. Exit the NOE environ-ment immediately.NOTEDuringrollingmaneuvers,a phenomenaknown as AC coupling may degrade thePNVS imagery. Generally, this image deg-radation will worsen as the bank angle isincreased. To reduce the adverse affectsof AC coupling, the pilot should reduce theamount of sky visible within the PNVS fieldof view by viewing the terrain below thehorizon.a. PNVS Failure.PilotNVSselectswitch–TADS.Switch over to TADSWFOV. FLIR image should occur in about 3 seconds.TADS slew rates are noticeably slower in azimuth thanPNVS. Some gain and level adjustment is usually nec-essary for optimum image.NOTEIn the event of a GEN-1 failure, the auto-matic power transfer to GEN-2 will resultin gray-scale selection in the HDU onsome aircraft. Should this condition occur,resetting the VID SEL switch to TADS willrestore normal video.b. IHADSS/HDU Failure.WARNINGIn the event of IHADSS failure with gunselected, the gun will be commandedto the fixed forward position. Once inthis position, the gun can still be firedwithout having to re–action the gun.Pilot1. Establishvisualflight.2. VDU control switch – PLT.3. ACQ SEL – NVS FXD.ORCPG1. CPG SIGHT SEL switch – NVS.2. PLT/GND ORIDE switch – ORIDE.3. NVS select switch – PNVS or TADS.4. CPG assume helicopter control.9.16.4 Dual IHADSS/HDU Failure.Pilot1. Establishvisualflight.2. VDUcontrol switch – PLT.3. ACQ SEL – NVS FXD.ORCPG1. Establishvisualflight.2. CPG assume helicopter control.
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