Caution Warning Panel Flashcards

1
Q

HDY IGE
(horn with increased load factor)
pressure < 30 bars

A

land normally
keep heading
lock collective and shut down

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2
Q

HDY OGE
(horn with increased load factor)
pressure < 30 bars

A

reduce collective airspeed to 40-60 kts (50-70 mph)
disengage collective hydraulic pressure switch
flat approach with run on landing at walking speed ASAP
lock collective and shut down

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3
Q

GEN
(batt approx 50 min/day or 20 min/night
DC power supply failure or over voltage detected

note: with electrical circuit failure check fuse

A
check DC voltage gauge 
check GEN pushbutton ON
reset GEN 
- if unsuccessful, shed Gen circuits
continue flight - monitor voltage (min 22 volts)
land asapl

5000’ max if boost pumps off

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4
Q

HORN

horn sounds when (4)

A

check horn pushbutton ON
horn sounds:

with HDY caution light when HDY Pressure drop < 30 bar
when N2 between 250-360 (continuous)
when Nr > 410 (intermittent)
when testing cw/l panel with rotor >350 Nr

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5
Q

DOORS

A
reduce airspeed to 120 kts 
visually check doors
if open or unable to check, land or 
continue flight at reduced speed
maintain low slink rate and flat landing approach
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6
Q

ENG CHIP

A

land ASAP

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7
Q

TGB CHIP

A

land ASAPL

avoid prolonged hovering

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8
Q

MGB CHIP

A

reduce engine power
monitor MGBP and MGBT lights

if MGBP light ON - reduce power - land ASAP
if MGBT light is ON -
press CWP Test to check MGBP light
if light does not illuminate - land ASAP
if light illuminates - land and check MGB oil level
if normal - fly to nearest base

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9
Q

MGB P

min gb pressure

A

reduce power - land ASAP

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10
Q

MGB T

max gb temp

A

press CWP Test Switch to check MGBP light
if light does not illuminate - land ASAP
if light illuminates - land and check MGB oil level
if normal - fly to nearest base

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11
Q

BATT (yellow)
battery isolated from DC network
no longer charging

for batt only DAY ops
battery, fuel pumps, vhf, radio/nav

A

check battery pushbutton ON continue flight, monitor voltage

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12
Q
BATT T (red)
max batt temp
A

switch battery OFF

land ASAP

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13
Q

PITOT

A

check pushbutton ON

monitor IAS

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14
Q

BLEED V
illuminates (BV open) when Ng < 93%
extinguishes (BV closed) when Ng > 97%

A

FLAG ON: BV remains closed with Ng < 93%
- possible surge or flameout
FLAG OFF: BV remains open with Ng > 97%
- increases fuel consumption & may limit power available
avoid fast power changes - land ASAPL

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15
Q

ENG P

A

reduce power

check Engine Oil Pressure Gauge
if LOW or ZERO read Torquemeter
if Tq very low shut down engine 
if Tq correct land immediately 
if EOP and TQ correct - land ASAP
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16
Q

Low Engine Oil Pressure on Guage

A

test EOP light in C/W Panel
if light does not illuminate:
check Tq reading
if Tq reading too low - shut down & autorotate
if Tq reading correct - land ASAP
if light illuminates
check Tq reading
if Tq reading too low - land ASAP
if Tq reading correct - land ASAPL
monitor ENG P light

17
Q

Engine Oil Temp High on Gauge - Low Speed/Hover

temp > 110C

A

land, shutdown, check cooler fan operation
if landing impossible, increase speed to 80 kts
temp should reduce - if not land ASAP

18
Q

Engine Oil Temp High on Gauge - in flight

(temp > 110C) has

A

reduce speed to 80 kts

temp should reduce - if not land ASAP

19
Q
Fuel Filter
 (clogging - impending bypass)
A

reduce power
if light goes out - continue flight at reduced power
if light stays on - land ASAP

20
Q

Fuel Pressure Gauge

LOW or ZERO

A

check fuel filter warning light

if fuel filter light OFF - continue flight (gauge failure)

if fuel filter light ON - reduce power
if light stays on - land ASAP
if light goes out - continue flight at reduced power

21
Q

Fuel

A

quantity < 60 L
B2 - 18 min at MCP

avoid large changes in attitude

22
Q

Fuel P
fuel pressure lower than 2 bar
on either or both pumps.

A

check fuel pressure gauge

if pressure normal, continue flight
1 pump failure
if pressure zero, continue flight below 5000”
(2 pump failure)

23
Q

Airframe Fuel Filter

A

check fuel pressure gauge

if pressure normal, continue flight

if pressure decreases, continue flight less than 5000 ft

24
Q

Low Inlet Pressure Annunciator

light with unexplained increase in T4
dirty/blocked filter, BV failure, poor turbine
t/o with light on prohibited

A

ENG ALT Air Switch - OPEN
if light extinguishes continue flight
service prior to next flight
if light stays on, monitor eng instruments
if pwr required can be achieved, continue flight, service prior to next flight
if pwr required cannot be achieved, land ASAP - service filter and do power check