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Flashcards in Chapter 9 - Emergency Procedures Deck (54)
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31

Engine Fire In Flight

WARNING
Attempt to visually confirm fire before engine shutdown or discharging extinguishing agent.
1. ________________________.
2. __________________— ___.
3. _____________ — ________.
4. _____________ — _______________.
5. _____________________.

 

1. Establish single engine airspeed.
2. ENG POWER CONT lever (affected engine) — OFF.
3. ENG EMER OFF handle — Pull.
4. FIRE EXTGH switch — MAIN/RESERVE as required.
5. LAND AS SOON AS POSSIBLE.

32

 

Electrical Fire In Flight

 

1. ___________ — ______

2. __________________.

 

 

1. BATT and GENERATORS switches — OFF.
2. LAND AS SOON AS POSSIBLE.                  

33

 

FUEL 1 BYPASS and FUEL 2 BYPASS Cautions Appear

 

1. ______________________

 

 

1. LAND AS SOON AS POSSIBLE

34

 

FUEL 1 PRESS LOW or FUEL 2 PRESS LOW Caution Appears

If the caution appears and the situation is critical:
1. ___________________________--_________.
2. ____________________ — ________.
3. ______________________________.
4. _____________________________.

 

If the caution appears and the situation is critical:


1. ENG FUEL SYS selector on affected engine — XFD.
2. FUEL BOOST PUMP switch on side being used — ON.
3. LAND AS SOON AS POSSIBLE.
4. EMER ENG SHUTDOWN after landing.

35

 

FUEL 1 PRESS LOW and FUEL 2 PRESS LOW Cautions Appear

 

1. ____________________________.
2. ____________________________.

 

 

 

1. LAND AS SOON AS POSSIBLE.
2. EMER ENG SHUTDOWN after landing.

36

 

GEN 1 FAIL and GEN 2 FAIL (No. 1 & No. 2 CONV and AC REF BUS DEGRAD) Cautions Appear.

1. Airspeed — Adjust (80 KIAS or less).
2. GENERATORS NO. 1 and NO. 2 switches — RESET; then ON.
If electrical power is not restored:
3. GENERATORS NO. 1 and NO. 2 switches — OFF.
4. MCUs and ECS — OFF prior to EMER APU START.
5. ______________________.
6. LAND AS SOON AS PRACTICABLE.
7. If APU GEN ON advisory light extinguishes, ensure MCUs and ECS — OFF prior to resetting the APU generator.

 

 

 

5. EMER APU START.

37

 

 

HYD PUMP 1 FAIL and HYD PUMP 2 FAIL Cautions Appear

_______________________. Restrict
control movement to moderate rates.

 

 

LAND AS SOON AS POSSIBLE. Restrict
control movement to moderate rates.

38

 

HYD PUMP 1 FAIL or HYD PUMP 2 FAIL Caution Appears and BACK UP PUMP ON Advisory Does Not Appear

1. ________ — _______ to a comfortable airspeed.
2. __________________ — ______.
If BACKUP PUMP ON advisory still does not appear:
3. ___________ — ________ (________).
4. _________________________.

 

1. Airspeed — Adjust to a comfortable airspeed.
2. BACKUP HYD PUMP switch — ON.
If BACKUP PUMP ON advisory still does not appear:
3. FPS and SAS/BOOST switchesPress off
(switch lights off, for HYD PUMP 2 FAIL caution)
.
4. LAND AS SOON AS POSSIBLE.

39

 

PRI SERVO 1 FAIL or PRI SERVO 2 FAIL Caution Appears.

1. ___________ — Check centered.
2. __________________________

__________________________.
3. _________________________.

 

 

1. SERVO OFF switch — Check centered.
2. If the caution appears with the SERVO OFF
switch centered, move the SERVO OFF
switch to turn off the malfunctioning servo.

3. LAND AS SOON AS POSSIBLE.

40

 

RSVR 1 LOW and HYD PUMP 1 Cautions Appear With BACK UP PUMP ON Advisory Appearing.
1. LAND AS SOON AS PRACTICABLE.
If the BACK UP RSVR LOW caution also appears:
2. _____________ — ________.
WARNING
If PRI SERVO 2 FAIL caution appears, establish landing attitude, minimize control inputs, and begin a descent.
3. _____________________.

 


2. SERVO OFF switch — 1ST STG.
 

3. LAND AS SOON AS POSSIBLE.

41

 

RSVR 2 LOW and HYD PUMP 2 FAIL Cautions Appear With BACK UP PUMP ON Advisory Appearing.

1. AUTO FLIGHT CONTROL panel CPTR 1 and/or CPTR 2 switches (if illuminated) — Press to reset FCC.
2. LAND AS SOON AS PRACTICABLE.
If BACK UP RSVR LOW caution also appears:
3. ____________ — _________. 

WARNING
If PRI SERVO 1 FAIL caution appears, establish landing attitude, minimize control inputs, and begin a descent.
4. ____________________.

 

 

3. SERVO OFF switch — 2ND STG.

4. LAND AS SOON AS POSSIBLE.

42

 

Collective Boost Servo Hardover/Power Piston Failure.

1. ______________ — ____.
2. FPS switch — Off.
3. LAND AS SOON AS PRACTICABLE.

 

 

1. SAS/BOOST switchOff.
2. FPS switch — Off.
3. LAND AS SOON AS PRACTICABLE.

43

 

BOOST SERVO OFF Caution Appears.

1. __________ — ____.
2. FPS switch — Off.
3. LAND AS SOON AS PRACTICABLE

 

 

1. SAS/BOOST switch — Off.
2. FPS switch — Off.
3. LAND AS SOON AS PRACTICABLE

44

 

Emergency Landing In Wooded Areas — Power Off

 

1. __________. Decelerate helicopter to stop all forward speed at treetop level.
2. _________________ to maximum before main rotor contacts tree branches.

 

 

1. AUTOROTATE Decelerate helicopter to stop all forward speed at treetop level.
2. Collective adjust to maximum before main rotor contacts tree branches.

45

 

Ditching — Power Off

1. ________________.
2. Cockpit doors jettison and cabin doors open prior to entering water.
3. Apply full collective to decay rotor rpm as helicopter settles.
4. Position cyclic in direction of roll.
5. Exit when main rotor has stopped.

 

 

 

1. AUTOROTATE

46

 

FLIGHT CONTROL/MAIN-ROTOR SYSTEM MALFUNCTIONS.

WARNING
Danger exists that the main rotor system
could collapse or separate from the
helicopter after landing. Exit when main
rotor has stopped.
1. __________________.
2. __________________.
3. _______ — ________.

 

 

1. LAND AS SOON AS POSSIBLE.
2. EMER ENG(S) SHUTDOWN after landing.
3. Rotor Brake — As required.

47

 

ROTOR BRAKE ON Advisory Appears in Flight.

1. Rotor brake handle — Check in detent and gage pressure at zero.
2. Check for secondary indications of brake pad dragging (smoke, smell, noise, etc.).
If secondary indications present:
3. ___________________________.
If no secondary indications present:
4. LAND AS SOON AS PRACTICABLE.

 

 

 

 

3. LAND AS SOON AS POSSIBLE.
 

48

 

STABILATOR MALFUNCTION — AUTO MODE FAILURE.

1. _____________________ to arrest or prevent nose down pitch rate.
2. ____________________________________________________.
If automatic control is not regained:
3. Manually slew stabilator — Adjust to 0° for flight above 40 KIAS or full down when airspeed is below 40 KIAS. The preferred method of manually slewing the stabilator up is to use the cyclic mounted stabilator slew-up switch.
4. LAND AS SOON AS PRACTICABLE.
If manual control is not possible, the airspeed limit indication will show the adjusted airspeed limit with a red arc.
5. Airspeed indicator — Check and fly at or
below red arc shown on the indicator.
6. LAND AS SOON AS PRACTICABLE.

 

 

1. Cyclic mounted stabilator slew-up switch —
Adjust if necessary
to arrest or prevent nose
down pitch rate.
2. AUTO CONTROL RESET switch — Press
ON once after establishing a comfortable airspeed.

.

49

 

UNCOMMANDED NOSE DOWN/UP PITCH ATTITUDE CHANGE

If an uncommanded nose down pitch attitude occurs:
1. ___________ — _________________.
2. __________ — __________________.
3. _______________ —________ to arrest nose down pitch rate.

4. MAN SLEW switch — Adjust to 0° at airspeeds above 40 KIAS and full down at
airspeeds below 40 KIAS.
5. LAND AS SOON AS PRACTICABLE.
If an uncommanded nose up pitch attitude occurs:
1. _______ — ________________.
2. _________ — ______________.
3. MAN SLEW switch — Adjust to 0° at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.
4. LAND AS SOON AS PRACTICABLE.

 

1. Cyclic — Adjust as required.
2. Collective — Maintain or increase.
3. Cyclic mounted stabilator slew-up switch — Adjust as required to arrest nose down pitch rate.

If an uncommanded nose up pitch attitude occurs:

1. Cyclic — Adjust as required.
2. Collective — Reduce as required.

50

 

 

STAB UNLOCKED Caution Appears.

In flight — ___________________.

 

 

 

In flight — LAND AS SOON AS POSSIBLE.

51

 

 

INTEGRATED AVIONICS SYSTEM MALFUNCTIONS

The following component failures will result in — ________________

 

 

 

The following component failures will result in — LAND AS SOON AS POSSIBLE

52

 

FLT DIR FAIL, FD COUPLE FAIL Cautions Appear

1. ___________________________________________________.
2. FAILURE RESET CPTR 1 and/or CPTR 2 — Press to clear flight director cautions.
3. Check AFCS and FCC status page. Clear BITE codes if necessary.
4. Reengage affected mode when able.
5. Fly affected axis manually if not restored.

 

 

 

1. Check FD/DCP to verify which flight director modes are functioning.
 

53

 

M/R DE-ICE FAULT, M/R DE-ICE FAIL, or T/R DE-ICE FAIL Caution Appears

1. Icing conditions — Exit.
2. BLADE DEICE POWER switch — OFF, when out of icing conditions. If vibrations increase:
3. ________________________.

 

 

 

3. LAND AS SOON AS POSSIBLE.

54

 

Loss of NO. 1 or NO. 2 Generator During Blade Deice Operation

Pilot not on the controls:
1. ___________.
2. ____________ — ______________.

 

 

Pilot not on the controls:
1. EMER APU START.
2. BLADE DE-ICE POWER switch — OFF
then ON.