NAVAL AVIATOR CRM TRAINING
WARNING FATIGUE & ATTENTION CONTROL - SIMULATION MODULE 4
PHASE 1 - ROUTINE ALERT SPAM
01:21:31Z
ZULU TIME
MASTER
CAUTION
MASTER
WARNING
ADVISORY PANEL
GEN 2 DEGRADE
Generator 2 Degraded
HYD FLICKER
Hydraulic Pressure Fluctuation
BLEED AIR
Bleed Air Overpressure
ECS FAULT
Environmental Control Fault
ENG 1 FIRE
Engine 1 Fire Detected
ATTENTION CONTROL LEVEL
FOCUSED / ATTENTIVE100%
FCS
HAB
AUT
REF
MRF
PILOT RESPONSE LOG
RST #10.41s
RST #20.38s
RST #30.34s
RST #40.29s
REFLEX0.17s
2020151510105555101015152020280300320340310KTS150020002500300035002500FTNAVHDGALTPITCH 0.5°  BANK 0.0°
MISSION STATUS
CRUISE / APPROACH PREP
ALT 2500 FT
HUMAN FACTORS ANALYSIS
01 Stimulus-Response HabituationPHASE 1

Repeated low-priority alerts create a conditioned reflex: alert fires, pilot resets, no consequence follows. Over 4-6 exposures, the reset action migrates from prefrontal cortex (deliberate) to basal ganglia (automatic).

02 Attention Control DepletionCOGNITIVE LOAD

Each interrupt costs attentional resource. Vigilance decrement research (Mackworth, 1948) shows sustained attention degrading after 20-30 min; repeated false alarms accelerate the curve to under 10 min.

03 Cry Wolf EffectAUTOMATION BIAS

Dixon & Wickens (2006): when alarm false-alarm rate exceeds 40%, operators begin treating all alarms as false. Reaction time decreases BUT appraisal drops to near-zero - speed is not safety.

04 Motor-Reflex DominanceNEUROMOTOR

The reset sequence (see alert, reach, press) becomes a learned motor program. Under high workload or fatigue, the motor program fires before the frontal lobe appraises the stimulus content.

05 Critical Phase VulnerabilityPHASE 2

Short final (< 500 ft AGL) is the highest-workload segment. Attentional tunneling is already active. Any novel alert must break through a heavily loaded attention bottleneck.

06 Reflexive OverridePHASE 3

0.17s reset is physiologically impossible as a deliberate response (minimum deliberate RT: ~250ms). The action was purely procedural memory. The pilot did not read "ENG 1 FIRE" before pressing reset.

07 Consequence CascadeSYSTEMIC

Fire handle not pulled. Engine continues to burn. At < 300 ft AGL, insufficient altitude for ejection. Outcome: loss of aircraft and crew. Root cause: alert system design, not pilot error alone.

08 CRM / Design MitigationMITIGATION

Countermeasures: (1) tiered alarm architecture with forced-read for Warnings. (2) Distinct audio encoding by criticality. (3) Copilot challenge protocol for all red-level events. (4) MFOQA alarm logging.

0:00PHASE 1: ROUTINE SPAMPHASE 2: FINALPHASE 3: FAILURE0:42
T+00.0s
SIMULATION TIME