SY 1111 Avionics Abnormal Op Flashcards

1
Q

WARNINGS (displayed boxed and blinking on HUD and MFD)

A

Alert pilot of a dangerous condition requiring immediate action

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2
Q

FIRE

A

Appears whenever either fire warning light illuminates

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3
Q

STALL

A

Appears when ldg gr is down and AOA is above 0.80, also by “GEAR UP STALL” settings

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4
Q

ALTITUDE

A

Appears whenever either the measured barometric altitude (MSL) or radar altitude (RALT) is lower than the minimum alt set on the UFCP ALT display

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5
Q

GEAR

A

Appears whenever the landing gear warning system is activated

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6
Q

CAUTIONS (displayed blinking on HUD and MFD)

A

Alert of an impending dangerous condition requiring attention, not necessarily immediate action

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7
Q

CAUTION

A

Appears whenever the MASTER CAUTION light illuminates

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8
Q

ENGINE

A

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

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9
Q

FLAPS

A

Appears when KCAS approaches or exceeds the airspeed limit for the current flap setting

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10
Q

OVER-G

A

Appears when aircraft exceeds the current relevant maximum positive or negative G limit

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11
Q

Medium-G

A

slower modulated tone, G load within 1.00-0.50 G’s of G limit

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12
Q

High-G

A

higher modulated rate tone, G load within 0.50-0.20 G’s of G limit

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13
Q

G Exceedence

A

continuous tone, G load within 0.20 G’s of G limit

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14
Q

Over-G

A

clazon tone, current G greater than 100% of G limit

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15
Q

AVIONICS

A

avionics failure occurs, listed in the PFL

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16
Q

BINGO

A

fuel quantity reaches amount set on UFCP SET display

17
Q

ADVISORIES (only displayed on HUD)

A

inform the pilot of certain normal or notable conditions, events, and actions

18
Q

Indications: MASTER CAUTION, LEFT (or right) GENERATOR light, flashing CAUTION on HUD and UFCP

A

GENERATOR FAILURE In Flight (Good Crossover)

19
Q

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

A

LEFT GEN FAIL In Flight (No AC Crossover)

20
Q

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

A

RIGHT GEN FAIL In Flight (No AC Crossover)

21
Q

Indications: Blank UFCP, Illumination of MASTER CAUTION and XMFR RECT OUT lights

A

Dual Transformer Rectifier Unit Failure

22
Q

Indications: Yaw and moderate rudder roll or chattering rudder pedals, possible AVIONICS alert on MFD/HUD

A

Stability Augmentor Malfunction