SY 1111 Avionics Abnormal Op Flashcards
WARNINGS (displayed boxed and blinking on HUD and MFD)
Alert pilot of a dangerous condition requiring immediate action
FIRE
Appears whenever either fire warning light illuminates
STALL
Appears when ldg gr is down and AOA is above 0.80, also by “GEAR UP STALL” settings
ALTITUDE
Appears whenever either the measured barometric altitude (MSL) or radar altitude (RALT) is lower than the minimum alt set on the UFCP ALT display
GEAR
Appears whenever the landing gear warning system is activated
CAUTIONS (displayed blinking on HUD and MFD)
Alert of an impending dangerous condition requiring attention, not necessarily immediate action
CAUTION
Appears whenever the MASTER CAUTION light illuminates
ENGINE
Appears when: RPM exceedence (latch event), Oil pressure high or low caution, Oil pressure high or low latch event, EGT overtemp (latch event), Loss of an engine sensor
FLAPS
Appears when KCAS approaches or exceeds the airspeed limit for the current flap setting
OVER-G
Appears when aircraft exceeds the current relevant maximum positive or negative G limit
Medium-G
slower modulated tone, G load within 1.00-0.50 G’s of G limit
High-G
higher modulated rate tone, G load within 0.50-0.20 G’s of G limit
G Exceedence
continuous tone, G load within 0.20 G’s of G limit
Over-G
clazon tone, current G greater than 100% of G limit
AVIONICS
avionics failure occurs, listed in the PFL
BINGO
fuel quantity reaches amount set on UFCP SET display
ADVISORIES (only displayed on HUD)
inform the pilot of certain normal or notable conditions, events, and actions
Indications: MASTER CAUTION, LEFT (or right) GENERATOR light, flashing CAUTION on HUD and UFCP
GENERATOR FAILURE In Flight (Good Crossover)
Indications: Flashing CAUTION on HUD and MFD, all AOA indexer lights illuminated, MASTER CAUTION lights, LEFT GENERATOR light, LEFT FUEL PRESS light, loss of left AC powered instruments
LEFT GEN FAIL In Flight (No AC Crossover)
Indications: Loss of HUD and UFCP, b/u display on MFD, MASTER CAUTION light, RIGHT GENERATOR, RIGHT FUEL PRESS and ENG ANTI-ICE ON lights, loss of right AC powered instruments
RIGHT GEN FAIL In Flight (No AC Crossover)
Indications: Blank UFCP, Illumination of MASTER CAUTION and XMFR RECT OUT lights
Dual Transformer Rectifier Unit Failure
Indications: Yaw and moderate rudder roll or chattering rudder pedals, possible AVIONICS alert on MFD/HUD
Stability Augmentor Malfunction
