Ranger Danger Red Pages

Throttle - close

FUEL VALVE switch - off

BAT switch - off

Rotor Brake - engage and allow rotors to stop

Helicopter - open or jettison doors and egress

Starter switch - engage and hold until TOT < 810

Throttle - close

Fuel valve switch - Off

IGN ENG CB - out

Shutdown - complete

Bat switch - off

GPU - off

Starter switch - release

GPU - off

Helicopter - complete emergency shutdown

Helicopter - establish autorotation

Throttle - close

Fuel valve switch - off

Helicopter - complete autorotative landing

Helicopter - start descent

Blower A/C switch - off

Vents and windows - open

Helicopter - land asap, complete emergency shutdown

Gen switch - off

BAT switch - off

If: fire, smoke/fumes persist:

A. Vents and windows - open

Helicopter - land as soon as possible, complete emergency shutdown

Pedals - maintain direction

Cyclic - eliminate drift

Collective - cushion landing

Helicopter - establish autorotation

If engine fails to automatically relight:

Throttle - close

Helicopter - complete autorotative landing

If time permits:

Passengers/crew - alert

Radio - transmit mayday

Engine - attempt restart in flight procedure

Collective - increase to control Nr

Throttle - reduce to maintain 97-100% N2

Helicopter - land asap

If unable to maintain powered flight:

Throttle - close

Helicopter - establish autorotation and complete autorotative landing.

Collective - decrease to control Nr

Throttle - full

Gov rpm switch - increase to maximum

Blower A/C switch - A/C off

If unable to maintain powered flight:

Helicopter - establish autorotation and complete autorotative landing

Else if powered flight can be maintained:

Helicopter - land asap

Helicopter - establish autorotation

Throttle - maintain 97-100% N2

Helicopter - complete autorotative landing

1. Helicopter………………………….. Reduce collective to control yaw
2. If: Yaw is uncontrollable:
a. Helicopter…………….………….. Establish autorotation
b. Throttle…………….…………….. Close for landing

c. Helicopter……………………….. Complete autorotative landing
3. Else if: Yaw is controllable:
a. Helicopter………………………... Resume restricted powered flight
Position to suitable landing area
Enter and complete autorotative landing

b. Throttle Close for landing
Note: For a zero groundspeed landing, use a steep flare as close to the ground as possible and use later than normal collective check before cushioning the landing.

Cyclic……………………………….. Eliminate drift

2. Collective…………………………... Lower slowly, accepting rotation on touchdown

1. Throttle……………………………... Idle

2. Cyclic……………………………….. Eliminate drift

3. Collective…………………………... Cushion landing

1. Helicopter………………………….. Maintain controllable airspeed above 60 KIAS

2. FOD check…………………………. Complete

3. Torque Reaction Check…………. Complete

4. Approach…………………………... Shallow to normal

5. Landing…………………………….. Use procedure for pedals locked at hover

1. HYDRAULIC SYSTEM switch… OFF

2. Helicopter………………………… Land as soon as possible

1. Helicopter………………………….. Gradually reduce airspeed (61 to69 KIAS)

2. HYDRAULIC SYSTEM switch…... Confirm ON

3. HYD BOOST circuit breaker……. OUT

4. If: Hydraulic pressure is not regained:

a. HYD BOOST circuit breaker….. IN

b. HYDRAULIC SYSTEM switch… OFF

c. Helicopter………………………... Land as soon as practical

Minimize flight control movements

d. Approach………………………… Shallow to normal
Terminate in a run-on landing

e. Landing…………………………... A run-on landing at 10 KIAS to 15KIAS is recommended

Note: With the skis installed, maximum run-on ground speed is 10 knots.

1. Helicopter…………………………… Establish autorotation

2. Doors………………………………... Open and locked

3. Cyclic………………………………... Reduce groundspeed to 0 beforetouchdown

Maintain level attitude

4. Collective……………………………. Minimize rate of decent as rotorcraftsettles into the water

5. Helicopter…………………………… Allow rotors to stop and egress

1. Crew and passengers……………... Alert/Brief

2. Helicopter…………………………… Establish low hover and jettisondoors

Crew and passengers egress

Taxi downwind well clear of crew andpassengers

3. Throttle……………………………… Close

4. Cyclic………………...……………… Maintain level attitude

5. Collective……………………………. Minimize rate of decent as rotorcraftsettles into the water

6. Helicopter…………………………… Allow rotors to stop and egress

1. Altimeter..… Check for sufficient altitude

2. Collective…………. Maintain 90% to 107% NR

3. Helicopter………………… Reduce airspeed to 52 KIAS to 69KIAS for existing conditions

4. Throttle……………………………… Close

5. ENG ANTI-ICE switch…………….. OFF

6. HEATER switch……………………. OFF

7. GEN switch…………………………. OFF

8. Engine………………. Proceed with normal start

9. If: Engine idles normally:

a. Throttle………………. Open slowly to FULL

b. TOT……………………………….. Monitor

c. Helicopter…………. Land as soon as possible

Else if: No relight, completeshutdown:

a. FUEL VALVE switch…………….. OFF

b. BAT switch……………………….. OFF

c. Helicopter… Complete autorotative landing

1. Helicopter……….. Establish autorotation

2. Throttle…………………………….. Idle

3. If: Time and altitude permit:

a. Throttle……………………………. Open

If: NR and N2 rise together:

(1) Limited powered flight may bepossible

(2) Helicopter………... Land as soon as possible

Else if: Unable to maintain poweredflight:

a. Helicopter…………. Establish autorotation

Follow engine failure in flightprocedure

1. Collective…………………………... Reduce

2. ENG ANTI-ICE switch……………. Reposition

3. HEAT VENT switch………………. Reposition

4. BLOWER A/C switch…………….. A/C OFF

5. If: Problem continues:

a. Helicopter…….. Land as soon as possible

Be prepared for an engine failure at any time

Else if: Problem stops:

a. Helicopter………. Land as soon as practical

Be prepared for possible reoccurrence

1. Engine oil pressure and temperature……. Check gauge

If: Engine oil temperature exceeds 107°C:

2. Power……………………….. Reduce

If: Engine oil temperature remains out of limits:

3. Helicopter……... Land as soon as possible

Else if: Engine oil temperature within limits oris fluctuating:

a. Helicopter…………. Land as soon as practical

1. Engine oil pressure and temperature…….Check gauge

If: Engine oil pressure below 50 psi or above130 psi:

2. Power…………………………….. Reduce

If: Engine oil pressure remains out of limits:

3. Helicopter……... Land as soon as possible

Else if: Engine oil pressure within limits or isfluctuating:

a. Helicopter……………. Land as soon as practical

1. Power………………….. Reduce
Monitor gauge

2. If: TRANS OIL TEMP caution light remains on:

a. Helicopter…….. Land as soon as possible

Else if: TRANS OIL TEMP cautionlight goes out:

a. Helicopter…............. Land as soon as practical

1. Power……………………………….. Reduce

Monitor gauge

2. Helicopter……….. Land as soon as possible

1. Fuel pressure………………… Check

2. If: No indication of fuel pressure (dual pump failure):

a. Helicopter…. Land as soon as possible

A dual pump failure can cause the loss of head pressure to the engine-driven fuel pump and result in power loss

Else if: With indication of fuel pressure (single pump failure):

a. Altitude………Descend below 6,000 feet HP

b. Helicopter…………Land as soon as practical

1. Helicopter………………. Land as soon as possible

Be prepared for an engine failure at any time

1. Helicopter...... land as soon as practical

1. Loadmeter…………………………... Check

2. GEN FIELD and GEN RESET… cbsCheck IN

3. GEN switch…………………………. RESET then ON

4. If: GEN FAIL caution light remainsON:

a. GEN switch……………………….. OFF

b. Load shed……………All unnecessary electrics

Required systems ON

c. Altitude………. Reduce to below 6000 feet HP

d. Helicopter……… Land as soon as practical

Consider remaining battery power

1. CHIP FAULT caution light switch.. Press then release

2. If: CHIP and CHIP FAULT caution lights do not extinguish:

a. Helicopter………… Land as soon as possible

Else if: CHIP and CHIP FAULT cautions lights extinguish:

a. Helicopter…………….. Flight can be continued

b. Clock……………………………….. Start

T/R CHIP or TRANS CHIP
c. If: Second CHIP caution light on the same component illuminates within30 minutes:

(1) Helicopter…………. Land as soon as possible

d. If: Third CHIP caution light on the same component illuminates:

(1) Helicopter…………………………. Land as soon as possible

ENGINE CHIP

e. If: Second ENGINE CHIP caution light illuminates within 50 aircraft hoursof the first ENGINE CHIP illumination:

(1) CHIP FAULT caution light switch. Press then release

If: ENGINE CHIP and CHIP FAULT lights do not extinguish:

(2) Helicopter…………. Land as soon as possible

Else if: ENGINE CHIP and CHIP FAULT caution lights extinguish:

(1) Helicopter…………. Land as soon as practical

If: Third or fourth ENGINE CHIP caution light illuminates within 50 aircrafthours of the first ENGINE CHIP illumination:

(2) Helicopter…………. Land as soon as possible

1. Helicopter………………………….. Fly clear of icing conditions

2. ENG ANTI-ICE switch…………….. ON

3. PITOT HEAT switch………………. ON

4. TOT………………………. Maintain within limits

5. If: Icing condition persists:

a. Helicopter…………… Land as soon as possible

1. Loss of Transponder Function ..... Considered

1. Function (FUNC)… ............................... SYS

2. GPS Status (8 or 9 keys)……….30 DIFF or 30 POS

3. Loss of ADS-B Function .......... Considered

Note:The NO 1090ES TX annunciation may illuminate as the unit powers on and begins to receive input from external systems, including acquiring the SBAS position