Table 7-2. Simulated Malfunction Details - Continued
Indications and effects on
Effects sensed by trainee
related systems as presented
if corrective action is
to the instructor and trainee
519 (No. 1 ENG) PTIT indicator reads zero.
520 (No. 2 ENG) No other systems affected.
521 (No. 1 ENG) Torquemeter indicator needle
522 (No. 2 ENG) fluctuates.
551 (No. 1 ENG) 1.
Prior to start sequence,
552 (No. 2 ENG)
there is no response when ENG
START switch is moved to MOTOR.
During starting sequence, but
before N1 reaches 35 percent,
engine decelerates, PTIT de-
creases below 350°C, and aural
cues and instruments reflect
553 (No. 1 ENG) Rapid rise in PTIT to above
Rapid rise in PTIT to
554 (No. 2 ENG) red line value of 940°C. PTIT
above red line value
begins to decrease as soon as
ECL is moved from flight to stop.
555 (No. 1 ENG) Slow N1 acceleration with
N1 stabilizes at 40%.
556 (No. 2 ENG) abnormal rise in PTIT. Engine
overtemperature may exist.
557 (No. 1 ENG) Fire warning lights illuminate.
561 (No. 2 ENG)
558 (No. 1 ENG) Fire warning lights illuminate.
562 (No. 2 ENG)