Table 2–1. Master Failure Symptom Index (cont)

TM 1–1520–238–T–2 Change 4 2–55 Table 2–1. Master Failure Symptom Index (cont) Failure Symptom MOC Reference CYCLIC STICK DOES NOT TRAVEL FULL FORWARD AND AFT TO THE RESPECTIVE STOP (PILOT CYCLIC STICK: FORCE TRIM SWITCH SET TO OFF) TM 1–1520–238–T–7 FLIGHT CONTROL SYSTEM CYCLIC STICK DOES NOT TRAVEL FULL LEFT AND RIGHT TO RESPECTIVE STOPS (PILOT CYCLIC STICK: FORCE TRIM SWITCH SET TO OFF) TM 1–1520–238–T–7 FLIGHT CONTROL SYSTEM DASE COMPUTER NO–GO AFT AVIONICS BAY APPEARS ON HOD TM 1–1520–238–T–7 DASE DASE ENGAGE PANEL NO–GO PLT COMPARTMENT APPEARS ON HOD TM 1–1520–238–T–7 DASE DASE MRTU – LT BUS NO–GO AFT AVIONICS BAY APPEARS ON HOD (ACZ) TM 9–1230–476–20–2 MULTIPLEX SUBSYSTEM DASE MRTU – RT BUS NO–GO AFT AVIONICS BAY APPEARS ON HOD (ACZ) TM 9–1230–476–20–2 MULTIPLEX SUBSYSTEM DASE MRTU NO–GO AFT AVIONICS BAY APPEARS ON HOD (SEC BUS DETACHED) (ACY) TM 9–1230–476–20–2 MULTIPLEX SUBSYSTEM DASE MRTU NO–GO AFT AVIONICS BAY APPEARS ON HOD (PRI BUS DETACHED) (ACY) TM 9–1230–476–20–2 MULTIPLEX SUBSYSTEM DASE MRTU NO–GO AFT AVIONICS BAY APPEARS ON HOD TM 9–1230–476–20–2 MULTIPLEX SUBSYSTEM DATA DISPLAYED FOR WAYPOINT 3 (DISPLAY LINES 1 AND 2 OF FLIGHT PLAN DICTIONARY PAGE 2) IS NOT THE SAME AS HOME (CDU: VAB NEXT TO DISPLAYED NUMBER 3 PRESSED) TM 11–1520–238–23–2 DOPPLER NAVIGATION SYSTEM (DNS) AN/ASN–137 DATA ENTRY KEYBOARD AND CPG FIRE CONTROL PANEL NO–GO APPEARS ON HOD TM 9–1230–476–20–2 MULTIPLEX SUBSYSTEM DATA ENTRY KEYBOARD EDGE–LIGHTS DO NOT LIGHT (CPG INTR LT PANEL: L CSL AND R CSL CONTROLS SET AT DESIRED LEVEL) TM 9–1230–476–20–2 MULTIPLEX SUBSYSTEM