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MH-60R RDAF > MH-60R Emergency Procedures > Flashcards

MH-60R Emergency Procedures Flashcards

1
Q

The following should be performed for all emergencies..

A
  1. Maintain control of the aircraft
  2. Alert crew
  3. Determine the precise nature of the problem
  4. Complete the applicable emergency procedure or take action appropriate for the problem
  5. Determine landing criteria and land as required.
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2
Q

Land immediately

A

Execute a landing without delay.

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3
Q

Land as soon as possible

A

Execute a landing at the first site at which a safe landing can be made

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4
Q

Land as soon as practicable

A

Extended flight is not recommended. The landing site and duration of flight are at the discretion of the PIC.

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5
Q

Engine malfunction in flight

A

*1. Control Nr

WARNING: Flying with greater than 110% torque with one engine inoperative may result in unrecoverable decay of Nr in the event of a dual-engine failure

*2. CONTGCY PWR switch - On

*3. Single-engine conditions - Establish

*4. ENG ANTI-ICE switches - As required

WARNING: With engine anti-ice on, up to 18% torque available is lost. Torque may be reduced as much as 49% with improperly operating engine inlet anti-ice valves.

*5. External cargo/stores/fuel - Jettison/dump, as required

*6. Identify malfunction

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6
Q

Engine High-Side Failure in Flight

A

*1. Engine Malfunction in flight emergency procedure - Perform

Note

  • Ng does not pass through the EDECU and is a highly reliable signal.
  • Torque signal may be erratic or drop off for high side conditions driven by EDECU failure.

2. PCL (malfunctioning engine) - Retard to set:
a. Torque 10% below good engine, or
b. Matched Ng, or
c. Matched TGT.

  1. Land as soon as practicable.
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7
Q

Engine High-Side Failure on Deck

A

*1. PCLs - Idle

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8
Q

Engine Low-Side Failure

LEGEND:
(#1/#2) ENG SPEED LOW

OR

ENG SPEED LOW

A

*1. Engine Malfunction in Flight emergency procedure — Perform.

  1. PCL (malfunctioning engine) — Momentarily advance to LOCKOUT, then retard to set:
    a. Torque 10% below good engine, or
    b. Matched Ng, or
    c. Matched TGT.
  2. Land as soon as practicable.
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9
Q

Engine Torque or TGT Spiking/Fluctuations

A
  1. Engine Malfunction in Flight emergency procedure - Perform
    * If fuel contamination is suspected:*
  2. Land as soon as possible
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10
Q

Engine High-Speed Shaft Failure

A
  1. Engine Malfunction in Flight emergency procedure - Perform
  2. PCL (malfunctioning engine) - Off
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11
Q

Compressor stall

A
  1. Engine malfunction in flight emergency procedure - perform.
  2. PCL (malfunctioning engine) - IDLE.
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12
Q

Engine Malfunction During Hover/Takeoff

A
  1. Control Nr
  2. CONTGCY PWR switch - ON

If a suitable landing site exits or unable to transition to forward flight:

  1. Set level attitude, eliminate drift, cushion landing.

If able to transition to forward flight:

  1. Engine Malfunction in Flight emergency procedure - Perform
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13
Q

Abort Start

A

To abort start:

  1. PCL - OFF.
  2. ENGINE IGNITION - OFF.

If engine oil pressure is indicated:

  1. Starter - Engage.
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14
Q

Dual-Engine Failure

A

1. Autorotation - Establish.
2. Immediate Landing/Ditching emergency procedure - Perform.

If time and altitude permit:

3. Engine Air Restart emergency procedure - Perform.

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15
Q

Single-Engine Failure In Flight

A
  1. Engine Malfunction in Flight emergency procedure - Perform.
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16
Q

Engine Air Restart

A
  1. APU Emergency Start procedure - As required
  2. ENGINE IGNITION switch - NORM
  3. Fuel selector lever - DIR or XFD
  4. PCL - OFF
  5. Starter - Engage, motor engine.
  6. PCL - IDLE (TGT 80o or less, if time permits).
  7. PCL - Advance to FLY after starter dropout.

WARNING

If APU is unavailable, and a crossbleed start is necessary, maximum torque available will be reduced during start sequence. Depending on operating conditions, level flight may not be possible. Ensure AIR SOURCE ECS/START switch is placed to ENG for crossblead starts.

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17
Q

APU Emergency Start

A
  1. ECS - OFF
  2. AIR SOURCE ECS/START switch - APU
  3. FUEL PUMP switch - APU BOOST
  4. APU CTRL switch - ON
  5. APU GENERATOR SWITCH - ON
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18
Q

Unusual Vibrations On Deck

A

If ground resonance is encountered and a safe takeoff is possible:

1. Takeoff immediately
2. Unusual Vibrations In Flight emergency procedure - Perform

If ground resonance is not encountered, or a safe takeoff is not possible:

1. Collective - Lower
2. PCLs - OFF
3. Rotor brake - Apply as required

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19
Q

Hung Droop Stops

A

*1. Reengage rotor to greater than 75% Nr.

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20
Q

Low Rotor RPM Warning

A

*1. Control Nr.

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21
Q

Main Transmission Malfunction

LEGEND:

Cautions:

MAIN XMSN OIL HOT

MAIN XMSN PRESS HI

MAIN XMSN PRESS LOW

(#1/#2) ACCESSORY CHIP

MAIN XMSN CHIP

Advisories:

MAIN XMSN OIL HOT

MAIN XMSN PRESS HI

MAIN XMSN PRESS LOW

A

If failure is imminent:

1. Land immediately

If secondary indications are present:

2. Land as soon as possible

  1. APU Emergency Start Procedure - Perform.
  2. No. 1 and No. 2 GENERATOR switches - OFF, as required

If no secondary indications are present:

  1. Land as soon as practicable
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22
Q

LEGEND:

INT XMSN CHIP

TAIL XMSN CHIP

IN XMSN OIL HOT

TAIL XMSN OIL HOT

A

If failure is imminent:

1. Land immediately

If failure is not imminent:

2. Land as soon as possible

23
Q

(#1/#2) INPUT CHIP

A

1. Main Transmission Malfunction emergency procedure - Perform

If engine secondary indications are present:

  1. Engine Malfunction in Flight emergency procedure - Perform
  2. PCL (engine with affected input module) - IDLE
24
Q

Loss of Tail Rotor Drive Altitude & Airspeed Sufficient to Establish Autorotation

A

1. PAC call - “AUTO, AUTO, AUTO”

2. Autorotaation - Establish. Center tail rotor pedals.

3. Drive failure - Attempt to verify.

4. Immidiate Landing/Ditching emergency procedure - Perform.

5. PCLs - OFF when directed (Prior to the flare).

25
Q

Loss of Tail Rotor Drive Altitude and Airspeed Not Sufficient to establish Autorotation

A

1. PAC call - “HOVER, HOVER, HOVER”.

2. Collective - Lower.

3. PNAC - Hands on PCLs.

4. PCLs - OFF when directed (approximately 20 to 30 ft).

26
Q

Loss of Tail Rotor Control

A

1. Collective/airspeed - Adjust as required to control yaw

  1. If hydrolic malfunction is evident:
  • TAIL SERVO switch - BKUP.
  • BACKUP HYD PMP switch - Check ON.
  • Backup Hydrolic Pump Fails to Operate emergency procedure - Perform, as required.
  1. External cargo/stores/fuel - Jettison/dump, as required.
  2. Land as soon as practicable.
  3. APU Emergency Start Procedure - Perform prior to landing.
  4. PCLs - As required
27
Q

TAIL ROTOR QUADRANT

A

1. Check for tail rotor control.

If tail rotor control is not available:

2. Loss of Tail Rotor Control Emergency procedure - Perform.

If tail rotor control is available:

  1. Land as soon as practicable.
28
Q

HYD

A

1. Land immediately.

29
Q

1 HYD PUMP

AND

2 HYD PUMP

AND

1 + 2 HYD PUMP FAIL

AND

BACK UP PUMP ON

A

1. Restrict flight control movement.

2. Land as soon as possible.

30
Q

1 RSVR LOW

AND

1 HYD PUMP

AND

BACK UP PUMP ON

A

1. SERVO switch — 1ST OFF.

2. Land as soon as practicable.

If the BACK UP RSVR LOW caution also appears or the backup pump fails:

3. Land as soon as possible. Be prepared for loss of tail rotor control.

If the #2 PRI SERVO PRESS caution and/or HYD warning appears:

4. Land immediately.

31
Q

2 RSVR LOW

AND

2 HYD PUMP

AND

BACK UP PUMP ON

A

1. SERVO switch — 2ND OFF.

2. Land as soon as practicable.

If the BACK UP RSVR LOW caution also appears or backup pump fails:

3. Land as soon as possible. Be prepared for loss of the pilot assist servos

If the #1 PRI SERVO PRESS caution and/or HYD warning appears:

4. Land immediately.

32
Q

BOOST SERVO HARDOVER

A

1. PAC call — “BOOST, BOOST, BOOST”.

2. SAS/BOOST pushbutton — Off.

  1. Minimize flight control movements.
  2. Land as soon as practicable.
  3. Make a shallow approach to a hover, maximum 15 knots crosswind. Taxi no more than necessary.
33
Q

UTILITY HYD PUMP

UTILITY HYD PUMP HOT

UTILITY HYD RSVR LOW

A

1. Stop dome.

  1. UTILITY HYD PUMP switch — OFF.
  2. Raise/seat dome using AUX ELEC raise.
  3. Land as soon as practicable.
34
Q

AFCS DEGRADED

A

1. Safe altitude and airspeed — Establish (waveoff/Instrument Takeoff [ITO], as required).

  1. AFCS CONTROL panel — Check status (RADALT/BAR ALT hold).
  2. AKNL ADVSY pushbutton — Press.
  3. FAIL ADVISORY MODE RESET pushbutton — Press.

If #1/#2 EGI FAIL advisory appears:

  1. Single/Dual EGI Failure emergency procedure — Perform, as required.

If malfunction is not eliminated:

  1. CMPTR PWR/RESET pushbutton — Cycle, as required.

If malfunction is still not eliminated:

  1. Malfunctioning system — Off (if possible).
35
Q

STABILATOR

A

1. PAC call — “STAB, STAB, STAB”.

2. Cyclic — Arrest pitch rate.

3. Collective — Do not reduce.

4. STABILATOR MAN SLEW switch — Adjust to 0°.

When at a safe altitude and airspeed:

  1. Stabilator circuit breakers — Reset.
  • STAB PWR (COPILOT, NO. 1 DC PRIMARY BUS, RW 3, cb 7).
  • STAB SYS PWR (COPILOT OVHD, DC ESNTL BUS, RW 2, cb 4).
  • STAB CTRL (CENTER, NO. 1 AC PRIMARY BUS, RW 1, cb 10).
  • STAB IND (CENTER, AC ESSENTIAL BUS, RW 1, cb 6).
  • STAB CTRL (CENTER, AC ESSENTIAL BUS, RW 3, cb 7).
  1. STABILATOR AUTO CONTROL pushbutton switch — Press on once, as required.

If automatic control is not regained and manual mode is operable:

  1. STABILATOR MAN SLEW switch — Adjust as required. Do not exceed stabilator versus airspeed limits shown below.
  2. Fly at or below speed shown:
36
Q

Unusual Attitude Recovery

A

1. Level wings.

2. Nose on horizon.

3. Center ball.

4. Stop rate of climb/descent.

5. Control airspeed.

37
Q

Electrical Power Failure/Dual Generator Failure

A

1. Safe altitude and airspeed — Establish.

2. Stabilator — Check position, slew as required.

3. APU Emergency Start procedure — Perform.

4. CMPTR PWR/RESET, SAS 1, SAS 2, TRIM, AUTO PLT, STABILATOR AUTO CONTROL pushbuttons — On.

If ac electrical failure:

  1. NO. 1 and NO. 2 GENERATOR switches — RESET, then ON.

If dc electrical failure:

  1. Converter circuit breakers — Cycle.
  • NO. 1 CONVERTER POWER (CENTER, NO. 1 AC PRIMARY BUS, RW 1, cb 14).
  • NO. 2 CONVERTER POWER (CORNER, NO. 2 AC PRIMARY BUS, RW 2, cb 4).

If ac and/or dc electrical power is not restored:

  1. Land as soon as possible.
  2. Nonessential electrical equipment — Off.
38
Q

(#1/#2) FUEL FLTR BYPASS

OR

(#1/#2) FUEL PRESS

A

*1. Fuel selector lever (affected engine) — XFD (DIR if currently in XFD).

  1. Land as soon as practicable.

If affected engine indications are abnormal:

  1. Engine Malfunction in Flight procedure — Perform.
39
Q

1 FUEL FLTR BYPASS

AND
#2 FUEL FLTR BYPASS
OR
#1 FUEL PRESS
AND
#2 FUEL PRESS

A

1. Land as soon as possible.

2. APU Emergency Start procedure — Perform.

40
Q

Refueling Hose Jettison (HIFR)

A

1. T-handle — Pull (if applicable).

2. Hose status — Report.

If hose fails to break away:

3. Quickly disengage the nozzle and grounding wire, then cut the hoist cable.

41
Q

FIRE

A

1. Confirm fire.

2. Engine Malfunction in Flight emergency procedure — Perform.

3. PCL (affected engine) — OFF.

4. Engine T-handle (affected engine) — Pull.

5. FIRE EXTGH switch — MAIN (RESERVE if required or ac power is off).

If airborne and fire continues:

6. Land immediately.

If fire appears extinguished:

7. Land as soon as possible.

  1. Single-Engine Landing emergency procedure — Perform.
  2. Fire extinguisher — Discharge into engine compartment.
42
Q

Internal Engine Fire

A

1. Starter — Engage. Motor engine.

  1. Portable fire extinguisher — As required.
  2. Starter — Secure (once TGT decreases below 540 °C).
43
Q

APU FIRE

A

1. APU T-handle — Pull.

2. Confirm fire.

3. FIRE EXTGH switch — RESERVE (MAIN if required and available).

If airborne and fire continues:

4. Land immediately.

If fire appears extinguished:

5. Land as soon as possible.

If on ground:

6. Fire extinguisher — As required.

  1. FUEL PUMP switch — OFF.
  2. APU CTRL switch — OFF.
44
Q

Cockpit Fire/Cabin Fire

A

If source is known:

1. Affected power switches and circuit breakers — OFF/Pull.

2. Portable fire extinguisher — As required.

If fire continues or source is unknown:

3. Cabin/doors/vents/ECS — Close/OFF, as required.

4. Unnecessary electrical equipment and circuit breakers — OFF/Pull.

If fire continues:

5. Land as soon as possible.

  1. Stabilator — Manually slew to zero.
  2. NO. 1 and NO. 2 GENERATOR switches — OFF, as required.
  3. BATT switch — OFF, as required.

If fire is extinguished:

  1. Smoke and Fumes Elimination emergency procedure — Perform.
  2. Land as soon as practicable.
45
Q

Smoke and Fumes Elimination

A

1. Airspeed — Adjust, as required.

2. Doors/windows/vents — Open.

3. Aircraft — Yaw, as required.

46
Q

Immediate Landing/Ditching (Pilot)

A

1. Crew and passengers — Alert.

2. Shoulder harness — Locked.

3. APU Emergency Start Procedure - Perform, as required

4. External cargo/stores/fuel — Jettison/dump, as required.

5. Searchlight — As required.

6. Mayday/IFF — TRANSMIT/EMER

In the flare:

7. Windows — Jettison, as required.

After landing:

8. PCLs — OFF.

9. Rotor brake — On.

10. Copilot collective — Stow.

11. Pilot HCU — Stow.

After all violent motion stops:

12. Egress.

47
Q

Underwater Egress

A

1. Emergency Breathing Device — As required.

2. Cords — Disconnect.

3. Door/window — Open/jettison.

4. Place hand on known reference point.

5. Harness — Release.

6. Exit helicopter.

After egress:

7. Swim clear of helicopter and inflate LPU.

48
Q

Cargo Hook Emergency Release

A

1. Cyclic EMER REL — Press.

49
Q

Rescue Hoist Cable Cut

A

1. Emergency shear switch — SHEAR.

If unable:

2. Direct pilot to press cyclic EMER REL button.

50
Q

RAST Messenger Jettison

A

1. Cyclic EMER REL — Press.

51
Q

Dual-EGI Failure

A

1. Backup instruments — Scan, as required.

2. #1 and #2 EGI PWR switches — OFF, then ON.

  1. If IMC, transition to VMC.
  2. Mission display — Ensure dual in-flight alignment has commenced.

If IMC and neither EGI will align:

  1. Land as soon as possible.

If VMC and neither EGI will align:

  1. Land as soon as practicable.
52
Q

MTS Uncommanded Lasing

A

1. ACI MASTER ARM — SAFE.

2. LASER SELECT switch— SAFE.

If lasing continues:

3. FLIR bezel key > +FLIR OFF — Select.

  1. MTS circuit breakers — Pull.
  • FLIR (MISSION,115 VAC 3Ø AC SEC BUS, RW 1, cb 3).
  • FLIR (MISSION NO 2 DC PRI BUS, RW 4, cb 2).
53
Q

All Stores Jettison

A

1. ALL STORE JETT — Press.

  1. Verify store separation.

MH-60R RDAF (5 decks)

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