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Page Title: b. TM 1–1520–238–T–2, Master Failure Symptom Index
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Section  I. GENERAL INFORMATION
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TM-1-1520-238-T-2 Army Model AH-64 Helicopter (NSN 1520-01-106-9519) (EIC: RHA) Master Failure Symptom Index Manual
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h.   TM 1–1520–238–T–8, Aviation Unit and Intermediate Troubleshooting Manual

TM 1–1520–238–T–2 1–3 1–6. FUNCTION OF EACH VOLUME OF THE MANUAL (cont) 1–6 b.   TM 1–1520–238–T–2, Master Failure Symptom Index. TM 1–1520–238–T–2 lists all integrated troubleshooting failure symptoms in alphabetical order. Each failure symptom refers you to the appropriate MOC in another volume. Additional troubleshooting information can be found by using the display symbology data found in chapter 1. You can refer to this volume for all types of failures, i.e., audio/visual, loss of power, short or open exists, etc. c.   TM 1–1520–238–T–3, Multiplex (MUX) Read Codes. TM 1–1520–238–T–3 contains Multiplex (MUX) Read Code interpretations by system. You are directed to go to this volume from MOCs in subsystem volumes. You can use this volume as an aid to interpret MUX read codes and locate faults. You are directed to the appropriate volume, to remove or replace a failed LRU or to a failure symptom within this volume. d.   TM 1–1520–238–T–4, Aviation Unit and Intermediate Troubleshooting Manual. TM 1–1520–238–T–4 contains system location and description, theory of operation, electrical component location and configuration (ECLC) index, power up/power down procedures, MOCs, wiring interconnect diagrams, and fault isolation procedures (FIPs). The following systems are covered in this volume: · Airframe. · Landing Gear. · Power Plants. · Rotors. · Drive. e.   TM 1–1520–238–T–5, Aviation Unit and Intermediate Troubleshooting Manual. TM 1–1520–238–T–5 contains system location and description, theory of operation, ECLC index, power up/power down procedures, MOCs, wiring interconnect diagrams, and FIPs. The following systems are covered in this volume: · Hydraulic and Pneumatic. · Instruments. f.   TM 1–1520–238–T–6, Aviation Unit and Intermediate Troubleshooting Manual. TM 1–1520–238–T–6 contains subsystem location and description, theory of operation, ECLC index, power up/power down procedures, MOCs, wiring interconnect diagrams, FIPs and FD/LS NO–GO FIPs. The following system is covered in this volume: · Electrical. g.   TM 1–1520–238–T–7, Aviation Unit and Intermediate Troubleshooting Manual. TM 1–1520–238–T–7 contains system location and description, theory of operation, ECLC index, power up/power down procedures, MOCs, wiring interconnect diagrams, FIPs and FD/LS NO–GO FIPs. The following systems are covered in this volume: · Fuel. · Flight Control.

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