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Page Title: Table 7-2. Simulated Malfunction Details (cont)
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Table 7-2. Simulated Malfunction Details (cont)
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TM-55-6930-212-10 Pyrometer and Thermocouple Tester Field Type N-3A Manual
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Table 7-2. Simulated Malfunction Details (cont)

TM 55-6930-212-10 Table 7-2.  Simulated Malfunction Details - Continued Method of Indications and effects on Effects sensed by trainee introduction related systems as presented if corrective action is Malfunction by instructor to the instructor and trainee not taken Center section 364 Center section instrument lights Restricted cockpit/instru- instrument lights are inoperative. ment visibility. Circuit breaker 401-455 CB related system is inoperative. CB related system is failures inoperative. Gas producer (N1) 501 (No. 1 ENG)   Gas producer indicator reads zero. None tachometer indica- 502 (No. 2 ENG)   No effects on other systems. tor Engine oil 505 (No. 1 ENG)   Engine oil pressure indicator None pressure indicator 507 (No. 2 ENG)   slowly decreases to zero.  No effects on other systems. Engine oil 506 (No. 1 ENG)   Engine oil pressure indicator None pressure indicator 508 (No. 2 ENG)   reads abnormally low (30 psi). Low No effects on other systems. Engine oil 509 (No. 1 ENG)   Engine oil temperature indicator None temperature 512 (No. 2 ENG)   does not move and does not indicator freezes respond to changed conditions. Engine oil 510 (No. 1 ENG)   Engine oil temperature indicator None temperature 513 (No. 2 ENG)   reads -700C and does not respond indicator minimum to changed conditions. No effects on other systems. Engine oil 511 (No. 1 ENG)   Engine oil temperature indicator None temperature 514 (No. 2 ENG)   reads ±1500C and does not re- indicator maximum spond to changed conditions. No effects on other systems. Rotor tachometer 517 (Pilot) Small fluctuations for 5-10 None fluctuates/fail 518 (Copilot) seconds, then rotor tachometer indicator reads zero. 7-13

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