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Page Title: HARS FAIL (ACY) HARS TEST STAT (ACZ)
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PITCH A–B MISTRACK (ACY) PITCH ACTR MISTRK (ACZ)
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TM-1-1520-238-T-3 Army Model AH-64 Helicopter (NSN 1520-01-106-9519) (EIC: RHA) Multiplex Read Codes Manual
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COLL ACT FAIL (ACY) CLTV ACTR STAT (ACZ)

TM 1–1520–238–T–3 Change 4 3–21 3–90    SIGNAL NAME: HARS FAIL (ACY) HARS TEST STAT (ACZ) MEMORY LOCATION:    002106 MEMORY DATA BIT(S): 6 (BINARY) CONDITION: (None) SIGNAL FUNCTION: Indicates capability of HARS to supply data to DASEC. REMARKS:   From DASEC to FCC. PASS: If fifth digit displayed on HOD is 0 or 1, go to paragraph 3–91. FAIL:    Location of fault: refer to Chapter 6, paragraph 6–9. 3–91    SIGNAL NAME: AIR DATA FAIL (ACY) ADS TEST STAT (ACZ) MEMORY LOCATION:    002106 MEMORY DATA BIT(S): 7 (BINARY) CONDITION: (None) SIGNAL FUNCTION: Indicates capability of air data system (ADS) to function properly and to supply data to DASEC. REMARKS:   From DASEC to FCC. PASS: If fifth digit displayed on HOD is 0, go to paragraph 3–92. FAIL:    Location of fault: refer to Chapter 2, paragraph 2–3. 3–92    SIGNAL NAME: LONG ACT FAIL (ACY) LONG ACTR STAT (ACZ) MEMORY LOCATION:    002106 MEMORY DATA BIT(S): 10 (BINARY) CONDITION: (None) SIGNAL FUNCTION: Indicates capability of longitudinal (pitch) servoactuator to respond correctly to DASEC commands. REMARKS:   From DASEC to FCC. PASS: If fourth digit displayed on HOD is 0, 2, 4, or 6, go to paragraph 3–93. FAIL:    Location of fault: longitudinal (pitch) servoactuator, wiring from longitudinal (pitch) servoactuator to DASEC. Troubleshoot wiring to isolate fault (TM 1–1520–238–T–7). 3–93    SIGNAL NAME: LAT ACT FAIL (ACY) LAT ACTR STAT (ACZ) MEMORY LOCATION:    002106 MEMORY DATA BIT(S): 11 (BINARY) CONDITION: (None) SIGNAL FUNCTION: Indicates capability of lateral (roll) servoactuator to respond correctly to DASEC commands. REMARKS:   From DASEC to FCC. PASS: If third digit displayed on HOD is 0, 1, 2, or 3, go to paragraph 3–94. FAIL:    Location of fault: lateral (roll) servoactuator, wiring from lateral (roll) servoactuator to DASEC. Troubleshoot wiring to isolate fault (TM 1–1520–238–T–7). 3–94    SIGNAL NAME: DIR ACT FAIL (ACY) DIR ACTR STAT (ACZ) MEMORY DATA BIT(S): 002106 MEMORY LOCATION:    12 (BINARY) CONDITION: (None) SIGNAL FUNCTION: Indicates capability of tail rotor actuator to respond correctly to DASEC commands. REMARKS:   From DASEC to FCC. PASS: If third digit displayed on HOD is 0 or 1, go to paragraph 3–95. FAIL:    Location of fault: tail rotor actuator, wiring from tail rotor actuator to DASEC. Troubleshoot wiring to isolate fault (TM 1–1520–238–T–7).

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