TM 55-1520-240-TADVANCED FLIGHT CONTROLS SYSTEM (Continued)SYMPTOMTASKNO. 1 YAW ILCA DOES NOT EXTEND OR RETRACT WHENPEDALS ARE MOVED11-3.3NO. 1 YAW ILCA HAS ENGAGE TRANSIENT11-3.3NO. 2 AFCS AC CIRCUIT BREAKER WILL NOT STAY CLOSED11-3.3NO. 2 AFCS COMPUTER BITE INDICATES 85 OR 8611-3.3NO. 2 AFCS COMPUTER BITE INDICATES 8911-3.3NO. 2 AFCS COMPUTER BITE SWITCH DOES NOT LIGHTAND COUNTER DOES NOT STEP WHEN BITE SWITCH ISPRESSED AND RELEASED11-3.3NO. 2 AFCS HEADING SELECT MOVE RESPONSE WEAK ORINOPERATIVE11-3.3SYMPTOMTASKNO. 2 AFCS OFF (WITHOUT 74) OR AFCS 2 (WITH 74 ) CAP-SULE DOES NOT GO OUT WHEN SYSTEM SELECTED11-3.3NO. 2 AFCS OFF (WITHOUT 74) OR AFCS 2 (WITH 74 ) CAP-SULE IS OUT WITH SYSTEM SELECTED OFF11-3.3NO. 2 AFCS PITCH ATTITUDE/AIR SPEED HOLD WEAK ORINOPERATIVE11-3.3NO. 2 AFCS YAW STABILITY ERRATIC/OSCILLATORY11-3.3NO. 2 PITCH ILCA HAS ENGAGE TRANSIENT11-3.3NO. 2 ROLL ILCA DOES NOT EXTEND OR RETRACT WITHLATERAL STICK MOTION11-3.3SYMPTOMTASKNO. 2 ROLL ILCA DOES NOT MOVE WHEN PILOT'S OR CO-PILOT'S PITCH AND ROLL TRIM SWITCH MOVED RIGHT ORLEFT11-3.3NO. 2 ROLL ILCA HAS ENGAGE TRANSIENT11-3.3NO. 2 YAW ILCA DOES NOT EXTEND OR RETRACT WHENPEDALS ARE MOVED11-3.3NO. 2 YAW ILCA HAS ENGAGE TRANSIENT11-3.3PITCH AND ROLL CONTROL STICK DOES NOT MOVE FOR-WARD OR AFT WHEN PILOT'S OR COPILOT'S PITCH ANDROLL TRIM SWITCH IS MOVED FORWARD AND AFT11-3.3RADAR ALTITUDE HOLD INOPERATIVE OR RESPONSE ER-RATIC (BAROMETRIC ALTITUDE HOLD OKAY)11-3.3RADAR OR BARO ALT ENGAGED CAPTIONS DO NOT COMEON WHEN PRESSED11-3.3Change 23 11-2.3/(11-2.4 blank)
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