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Table  2-14-2   Master Caution/Advisory Panel Capsules  714A
SECTION  XV.  SERVICING, PARKING, AND MOORING

TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual
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TM  1-1520-240-10 2-14-12            Table  2-14-2   Master Caution/Advisory Panel Capsules  714A   (Continued) WORD SEGMENT EXPLANATION PWR STEER Steering control has been disabled due to system malfunction or steering limits have been exceeded. RECT 2 Transformer-rectifier has failed or the generator output is interrupted. GEN 1 No. 1 generator is inoperative or the generator switch is at OFF. GEN 2 No. 2 generator is inoperative or the generator switch is at OFF. HYD 1 No. 1 flight control hydraulic system pressure us below 1,800 psi. CD JAM Counter measures jammer failed. UTIL HYD SYS Utility hydraulic system pressure is below 1,800 psi. HYD 2 No. 2 flight control hydraulic system pressure is below 1,800 psi. AFCS 1 The No. 1 AFCS is off, failed, or DASH is reprogramming. CM INOP Counter measures inoperative. DUAL HOOK FAULT The forward and/or aft hook circuit has an electrical fault and the hook(s) shall not be re- leased electrically. AFCS 2 The No. 2 AFCS is off, failed, or DASH is reprogramming. APU ON The APU is up to speed and can be used. EXT PWR The light comes on whenever external popwer is conencted to the bus. FWD HOOK OPEN The forward cargo hook has been opened either electrically or manually. PARK BRK ON Parking brake is on. MID HOOK OPEN The midcargo hook has been opened, either hydraulically, pneumatically, or manually. AFT HOOK OPEN The aft cargo hook has been opened either electrically or manually.







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