Study The 407

Front 1

RED Caution Lights Illuminated

Back 1

Requires Immediate Action which if not correctly followed could result in personal injury or loss of life

Front 2

Land as Soon as Possible

Back 2

Land without delay at nearest suitable area that will ensure a safe approach and landing

Front 3

Land as Soon as Practical

Back 3

Practical landing site and duration of flight at discreation of pilot. Flight beyond nearest approved landing area is not recommended

Front 4

FADEC Failure

In Flight
1. Indications
2. Corrective Actions

Back 4

1. FADEC Fail light on Overspeed may occure in 2-7 seconds
2. Throttle- match Benzel to Ng indication, maintain Nr/Np with collective and throttle press FADEC mode SW- once to mute audio. Land as soon as Practical.

Front 5

Battery Hot
Light Only
1. Indications
2. Corrective Actions

Back 5

1. Battery hot light illuminated ( Batt over 71deg C)
2. Battery switch; off if battery relay light illuminates : Gen. SW- off
Land as soon as possible- Reduce Electrical Load

Front 6

Engine Overspeed
No Lights Illuminated
1. Indications
2. Corrective Actions

Back 6

1. Increase In; Nr, Np Ng and TRQ
2. Throttle- Retard control Np/Ng with collective and throttle FADEC Mode SW- Manual Nr- Control W- Collective and Throttle
If uncontrollable- shut down Engine and autorotate.

Front 7

Engine Failure
Hovering
1. Indications
2. Corrective Actions

Back 7

1. Left Yaw Engine out and RPM light Engine out audio- Ng down 55% Nr down 95%
2. Maintain Heading and Att. collective control rate of decent cushion landing, land and shut down ACFT.

Front 8

Smoke and Fumes
1. Indications
2. Corrective Actions

Back 8

1. Smoke and or fumes
2. Initiate Descent
Air Cond/Blo.SW- off
Heater SW- off
All Vents- open
All windows- open
Identify source???
Isolate Source I.P
Land as soon as Practical

Front 9

Engine Fire
Inflight
1. Indications
2. Corrective Actions

Back 9

1. Smoke- Fumes- Fire
2. Verify
Enter Autorotation
Throttle- Closed
Fuel Valve SW- Off
Fuel boost/xfer SW- Off
Battery SW- Off

Front 10

RPM with Audio- Low
1. Indications
2. Corrective Actions

Back 10

1. RPM Light and Audio RPMK down 95% Nr
2. Reduce collective check throttle in "Fly"

Front 11

XMSN Oil Press
1. Indication
2. Corrective Actions

Back 11

1. XMSN Oil Press Light Illuminates
2. Reduce power verify oil pressure with gauge
Land as soon as Possible

Front 12

XMSN Oil Temp
1. Indications
2. Corrective Actions

Back 12

1. XMSN Oil Temp Light is ON
2. Reduce power verify with gauge
Land as soon as Possible

Front 13

FADEC FAIL during Start
1. Indications
2. Corrective actions

Back 13

1. FADEC fail light is ON. FADEC has Detected Malfunction.
2. Throttle- Closed
Starter- engaged to reduce MGT down 150deg
Maintain action required prior to next flight.

Front 14

Engine Underspeed: No lights Illuminated
1. Indications
2. Corrective actions

Back 14

1. Decrease in : Ng, Np,
Torque and possibly Nr.
2. Collective- maintain Nr. Throttle- Verify in Fly position benzel with Ng Indicated
FADEC mode SW- Manual
Nr- Maintain with collective and throttle land as soon as practical

Front 15

Engine Fire During Start
1. Indications
2. Procedures

Back 15

1. Smoke, Fumes, Fire
2. Throttle- Closed
Fuel Valve SW- Off
Gen SW- Off
Battery SW- Off
Rotor Brake- Engage
Exit Helicopter
Fight Fire

Front 16

Engine Failure in Flight
1. Indications
2. Corrective Actions

Back 16

1. Left Yaw- Engine out and RPM light
Verify engine inst. indicate power loss
Engine out audio- on down 55% Ng
2. Collective - maintain Nr 85107
Cyclic- Control airspeed
60-KTS- Min rate of descent
80 KTS- Max Glide Dist.
Flare- Lose airspeed and rate of descent

Front 17

RPM No Audio- High
1. Indications
2. Corrective Actions

Back 17

1. RPM Light Illuminates Verify Nr above 107%
2. Increase collective
Reduce severty of maneuver

Front 18

Drive Shaft Failure
1. Indications
2. Corrective Actions

Back 18

1. Left Yaw Rapid Nr Decrease Rapid Np Increase. Low RPM Audio RPM light- ON
Maintain heading and altitude control Nr with collective autorotate-60-80 KTS.
Do not shut engine down to maintain T/R Effectiveness

Front 19

Engine Hot Start
1. Indications
2. Corrective Actions

Back 19

1. Excessive MGT.
Visible smoke or fire
2. Throttle- Closed
Fuel Valve SW- Closed
Starter-Engage
Motor until MGT decreases to 150 Deg C
Wait until Ng reaches "0" before attempting restart

Front 20

Engine Comp Stall
1. Indications
2. Corrective Actions

Back 20

1. Engine popping sound
erattic MGT, Ng or Np.
Torque oscillations
2. Reduce Power
Engine Anti-ice- ON
Part. Sep SW- On
Heater SW- On
Severity of stalls will sictate if Engine should be shut down

Front 21

Tail Rotor Failure
Loss of Thrust
1. Indications
2. Corrective Actions

Back 21

1. Yaw to the Right
Nose tuck or roll off ACFT Body
2. Hover: Close throttle and autorotate
Inflight: Reduce throttle
airspeed: 55KTS to maintain FLT. To landing slide on landing use collective to reduce forward speed.

Front 22

Tail Rotor Failure
Loss of Control
1. Indications
2. Corrective Actions

Back 22

1. Lack of Directional response
Stuck Petals
2. TRQ, Nr and Airspeed- control to control Yaw.
-Pull pedal stop, emergency release. Hover- land
In flight- control Yaw with power and airspeed- slide on
If right Yaw becomes excessive, Close throttle and autorotate.

Front 23

Yellow Caution Lights Illuminated

Back 23

Requires an operating procedure which if not strictly observed could result in damage to or destruction of equipment

Front 24

FADEC Fault
1. Indications
2. Corrective Actions

Back 24

1. FADEC Fault Light- on
Engine Automatic limiting circuits not functional
2. Remain in Auto Mode
Land as soon as practical and maintain action required prior to next flight

Front 25

FADEC Degraded Inflight
1. Indication
2. Corrective Actions

Back 25

FADEC Degraded Light-on
ECU operation degraded may result in reduced max power capability
2. Remain in "Auto" Mode. Fly smoothly and non aggressivly. Land as soon as practical
-may need to use fuel valve SW to shut down engine
MX required prior to FLT

Front 26

Battery RLY
1. Indication
2. Corrective Actions

Back 26

1. Battery Rly light on relay has failed in "ON" position with battery SW off- Batt still connected to DC Buss
2. If Batt not illuminated Gen SW- Off
If conditions permit land as soon as possible

Front 27

FADEC Manual
1. Indications
2. Corrective Actions

Back 27

1. FADEC Manual Light -ON
Auto Relight Light- On
No auto governing avail
2. Fly smoothly and non aggressively maintain Nr with collective and throttle
Land as soon as practical

Front 28

FADEC Degraded
Engine shut Down
1. Indication
2. Corrective Actions

Back 28

1. FADEC Degraded Light- ON
FADEC detected a fault either currrent or from previous flight
2. Throttle- to idle if light extinguishes: Fault from previous FLT: MX required prior to next flight

Front 29

Pedal Stop
1. indication
2. Corrective Action

Back 29

1. Pedal stop light- On
Failure of system
2. Airspeed max=60 KTS VNE

Front 30

Cyclic Centering
1. Indication
2. Corrective Action

Back 30

1. Cyclic Ctr Light-On
Cyclic Not centered
2. Repositon Cyclic until light extinguishes
Disreguard during T.O.

Front 31

Hydraulic System
1. Indications
2. Corrective Actions

Back 31

1. Hyd system light- On
Increased force required to move flight controls, feedback forces may be felt
2. Airspeed reduce to 70-100 Hyd sys C/B- Pull out if Hyd Pwr not restored push back in and turn Hyd system switch off. Land as soon as practical

Front 32

Check Instr
1. Indications
2. Corrective Actions

Back 32

1. Check instr light- On
Flashing LCT Trend ARC indicates impending TRQ, Ng or MGT exceedance
2. Reduce Engine power inst. check button- press to read exceedance

Front 33

Gen Fail
1. Indications
2. Corrective Actions

Back 33

1. Gen Fail Light-On
Amp Gauge Reads- "0"
Voltmeter Read Approx-24V
2. Gen Field and Gen Reset C/B's Check-"IN"
Gen SW. "Reset" then "GEN" on.
If power is not restored general W off and land as soon as Practical * Battery will provide approx. 20 min-ft.

Front 34

Fuel Valve
1. Indication
2. Corrective Action

Back 34

1. Fuel Valve Light- On
Fuel Valve position differs from SW indication or C/B is pulled
2. Check fuel valve C/B -In
Land as soon as Practical
If On GND- cycle Fuel valve Switch

Front 35

"l" or "R" Fuel XFR
1. Indication
2. Corrective Actions

Back 35

L or R Fuel XFR light- On
1 pump failed- LASA pract.
Both pumps failed- ususable
fuel may be up to 135 LBS stuck in Fwd Cell
2. Land as soon as practical

Front 36

Fuel Filter
1.Indication
2. Corrective Actions

Back 36

1. Fuel filter light On filter impending bypass
2. Land as soon as practical MX required prior to next flight

Front 37

Fuel Low
1. Indication
2. Corrective Actions

Back 37

1. Fuel Low Light is On
100 +/- 10 LBS of fuel left in AFT tank
2. Verify fuel quantity land as soon as practical
20 min of fuel APPROX

Front 38

R or L Fuel Boost
1. Indication
2. Corrective Actions

Back 38

1. R or L Fuel Boost Light ON Boost Pump(s) have failed
2. Descend below 8000' HP Jet A
Descend below 4000' HP Jet B
If both pumps fail land as soon as Practical

Front 39

Cyclic Cam Jam
1. Indications
2. Corrective Actions

Back 39

1. High force and Aft Control forces less than 151 LBS. Normal forces in lat cyclic, pedal and collective
2. Maintain normal pitch attitudes. DO NOT TURN HYD. OFF.
Land as soon as Practical

Front 40

Engine Chip
1. Indication
2. Corrective action

Back 40

1. Engine chip light is -ON
Particles in Engine Oil
2. Land as soon as Possible

Front 41

XMSN Chip
1. Indication
2. Corrective action

Back 41

1. XMSN Chip Light is -ON
Particles in XMSN Oil
2. Land as soon as Possible

Front 42

T/R Chip
1. Indication
2. Corrective Action

Back 42

1. T/R Chip Light- ON
Particles in T/R G/B oil
2. Land as soon as Possible

Front 43

Litter Door
1. Indication
2. Corrective Actions

Back 43

1. Litter Door Light- On
Litter Door Not Secure
2. Close and latch priot to Flight.
In Flight: Land as soon as Practical

Front 44

Baggage Door
1. Indication
2. Corrective Actions

Back 44

1. Baggage Door Light-ON
Baggage door not secured
2. Close and latch prior to flight. In Flight: Land as soon as Practical

Front 45

Heater Overtemp
1. Indication
2. Corrective Action

Back 45

1. Heater Overtemp Light is ON
1 of 3 probes detected an overtemperature
2. Heater SW- Off

Front 46

Float Arm
1. Indication
2. Corrective Actions

Back 46

1. Float Arm Light- On
Float Arm SW - ON
Float "Armed"
2. Normal for T/O and Landing
Float arm SW-Off
If light remains on- floatsC/B- Pull and land as soon as practical

Front 47

Float Test
1. Indication
2. Corrective Action

Back 47

1. Float Test Light on System in Test Mode
2. None

Front 48

Start
1. Indication
2. Corrective Action

Back 48

1. Start relay in start mode
If start SW not engaged and amp guage reads "0" - start relay has malfunctioned- ACFT is running on Battery Power.
2. Start C/B- out
Reduce Electrical Load
Land as soon as Practical

Front 49

Restart Fault
1. Indication
2. Corrective Actions

Back 49

1. Restart fault illuminated FADEC ECU detected fault which will not allow engine to be started in auto mode.
2. Remain in auto mode. Plan landing accordingly
MX required prior to next flight.