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(1) HC-130J > Emergency Procedures+ > Flashcards

Emergency Procedures+ Flashcards

1
Q

ENGINE FIRE SHUTDOWN

A
  1. Power Lever (affected engine) - FLT IDLE
  2. FIRE Handle (affected engine) - PULL
  3. Agent (affected engine) - Discharge, as required
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2
Q

APU FIRE

A
  1. APU Fire handle - PULL
  2. AGENT - Discharge, as required
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3
Q

ABORTED TAKE OFF

A
  1. State - “ABORT, ___”
  2. Power Levers (All) - FLT IDLE
  3. Maximum Braking - As required
    ————————————————
  4. Nosewheel steering - As Required
  5. Power Levers (all) - GND Idle
  6. State - All Four/Inboards/Outboards
  7. Power Levers - MAX REV
  8. ACAWS Crew Action - Accomplish
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4
Q

INADVERTENT IMC

A
  1. Announce - “Inadvertent IMC”
  2. Transition - Establish Instrument Scan
  3. Maneuver - As required
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5
Q

FIRE/SMOKE/FUMES ELIMINATION

A
  1. OXYGEN - ON, 100%

If at any time during the execution of this checklist the fire, smoke, or fumes decrease in intensity, stop and ascertain what systems are affected and isolate the component(s) (if able) and restore aircraft power

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6
Q

RAPID DECOMPRESSION

A
  1. OXYGEN - ON, 100%
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7
Q

Windshear Recognition

A

o +/- 20 KCAS
o +/- 500 fpm Alt Changes
o +/- 6* Pitch Attitude Changes
o +/- 1.5 dot G/S Deviation
o Unusually steep/shallow pitch attitudes
o Unusually high/low Pwr Settings

Recommended:
o Use 50% Flaps for LDG

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8
Q

Windshear Recovery

A
  1. T/O Power and Level Wings
  2. Pitch to 15* Nose up to
  3. Maintain 10 kts > Stall Caret
  4. PM Calls RA, A/S, Sink Rate
  5. Do not change config until out of alert and stable
  6. Do not use G/A F/D – Does not optimize Perf
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9
Q

Abort Start With FIRE handle When:

A
  1. Engine Fire
  2. Engine MGT High
  3. Start Valve Open
  4. MGT rapidly approaches/exceeds 807* C
  5. Visible fluid leak/smoke or flames
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10
Q

FIRE Handle Secures:

A

HBOFFA
H: HYDRAULIC
B: BLEED AIR
O: OIL
F: FUEL
F: FEATHERS PROP
A: ARMS/ROUTES FIRE EXT AGENT

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11
Q

Go-Around

A
  1. Announce Go-Around
  2. Go-Around Button - Press
  3. Power Levers - set TAKEOFF as req
  4. Pitch - Follow FD
  5. Flaps - Check/Set 50%
  6. Gear - Up
  7. Rudder Trim - As Req
  8. Flaps - Up (Passing FUSS)
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12
Q

Three Engine Go-Around

A
  1. Announce Go- Around
  2. Go-Around Button - Press
  3. Power Levers - set TAKEOFF as req
  4. Bank - 2-5* into operating engines
  5. Pitch - Follow FD
  6. Flaps - Check/Set 50%
  7. Gear - Up
  8. Rudder Trim - As Req
  9. Flaps - Up (Passing FUSS)
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13
Q

Four Engine Flameout

A
  1. Pitch Attitude - Adjust for airspeed control (NG between 15-28%)
  2. Power Levers (all) - FLT IDLE
  3. Fuel X Feed Switches - Close
  4. Inboard (No. 2 and No. 3) ENGINE START switches - STOP, START, release
  5. Outboard (No. 1 and No. 4) ENGINE START switches - STOP, START, release
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14
Q

Loss of Normal Brake Pressure

A
  1. AUX PUMP switch - ON
  2. BRAKES - EMER
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15
Q

Engine Surge Identification

A

Characterized by several ACAWS in succession
- ENG 1 (2, 3, or 4) MGT HI (W)
- ENG 1 (2, 3, or 4) MGT HI (C)
- HOT START 1 (2, 3, or 4) (C)
- ENG 1 (2, 3, or 4) FAIL (C)
- ENG 1 (2, 3, or 4) A/I VLV FAIL (C)
- ENG 1 (2, 3, or 4) FLAMEOUT (C)

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16
Q

Clear Air Icing Procedure

A

Ice Protection Panel
1. ENG Switch - Off (at or above FL210) or AUTO (below FL210)
2. WING/EMP - AUTO (Verify DE-ICE Selected)

When ICE DETED (A) or LEVEL 2 ICE (A) or crew detects indication of clear air icing
3. Autothrottle - Disengaged
4. Power Levers (all) - Immediately retard approx two knob widths, no lower than FLT IDLE
5. WING/EMP switch - ON (Verify DE-ICE selected)
6. After WING/EMP A/I has been ON approx 5 seconds - ENG Switch - ON

After NG stablized (approx 15 seconds)
7. Power Levers (all) - Slowly advance, as requried, while monitoring MGT
8. If at or above FL210 and conditions permit descend below FL210 and maintain cruise airspeed

After 6 minutes since ICE DETECTED (A) or LVL 2 ICE (A) has cleared:
ICE PROTECTION panel, in this order:
9. ENG switch - OFF (at or above FL210)
10. WING/EMP switch - AUTO

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17
Q

Engine Surge Recovery

A
  1. Autothrottle - Disengage
  2. Power Levers (all) - Immediately retard approx two knob widths, no lower than FLT IDLE
  3. Power Lever (affected engine) - retard to FLT Idle

After NG has stabilized on nonaffected engines (approx 15 sceonds)
4. Power Levers (nonaffected engines) - Slowly advance as required while monitoring MGT
5. Descend below FL210, if conditions permit

If affected engine has decresaed to <100 HP and is not responsive to power lever movement:
6. FIRE handle - Pull
7. ENGINE START Switch - Stop
8. Airstart - As required
9. Land as soon as practicable

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18
Q

Engine Failure Above Refusal Speed

A
  1. Takeoff - continue
  2. Directional Control - Maintain
  3. Rotate - to target pitch attitude
  4. Speed - capture VOBS
  5. Bank Angle - 2 to 5 degrees into operating engine
  6. Rudder Trim - Set, as required
  7. GEAR - Up
  8. Flaps - Up
  9. Power Levers - Max Cont
  10. ACAWS Crew Action - Accomplish
  11. Climb Speed - Maintain
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19
Q

ACAWS Logic

A

The aural alert and the MASTER WARNING and MASTER CAUTION lights for some ACAWS alerts are inhibited for takeoff between 70 to 140 kt or 0 to 400 ft AGL. Aural alerts remain active during touch and go landings unless airspeed decreases to ≤60 KIAS on the runway with the power levers below FLT IDLE.

20
Q

Place ENGINE START switch to STOP for:

A
  1. Flameout (C)
  2. No Lightoff (A)
  3. Stagnated Start (A)
  4. No NG within 10 seconds
  5. No oil px within 15 seconds of NG or ENG 1/2/3/4 NO OIL PRESS (c)
  6. No oil px within 15 second of NP rotation or GBOX 1/2/3/4 NO OIL PRESS (C)
  7. Torching
21
Q

Hydraulic System Leak

A
  1. Hydraulic Engine Pump Switches (affected system) - Off
  2. Suction Boost Pump Switches (affected engine) - Off
  3. Reservoir Fluid Level - Check

— continue checklist in red book

22
Q

Drift Down Procedures

A

1) Engine failure.
2) Set maximum continuous power (decelerate).
3) At drift down speed descend at DD speed to the lower service ceiling (3/2ENG SVC).
4) At the service ceiling accelerate to cruise speed.

23
Q

Basic Assumptions for Landing Distance

A

o 1 Second allowance for distance traveled during transition from TD to taxi attitude
o Maximum anti-skid braking and power selection upon reaching taxi attitude

24
Q

Land Immediately

A

Land without delay; primary consideration is to assure survival of occupants

25
Q

Land as soon as possible

A

Land at the nearest site which a safe landing can be made

26
Q

Land as soon as practicable

A

Extended flight is not recommended. Landing site and duration of flight at discretion of pilot in command.

27
Q

Wing Fire

A
  1. X Feed Switches (all) - Close
  2. Hyd Engine Pumps switches (affected wing) - Off
  3. Suction Boost Pump switches (affected wing) - Off
  4. ISO Valve (affected wing) - Close
  5. NAC SOV Valves (engines or affected wing) - Close
  6. Aircraft - Sideslip to keep fire away from fuselage
  7. Land - As soon as possible
28
Q

FADEC AUTOFEATHER

A

With power levers FLT IDLE or above:
1) loss of prop control (high power and NP below 73%)
2) high power setting, low HP (less than 74% of command HP) and decelerating NG (>500 RPM per sec)
3) Low power setting, low NG (<69%)

29
Q

Confirm gear down and lock

A

Ball nut on upper bumper stop

Drag pins in shelf bracket

30
Q

Check, Check, STAR, GO

A

Normal checklist
Emergency checklist
Systems
Trim
Airspeed (vmca, gear, flaps)
Reversing (inboard/outboard only)
Go-Around procedure

31
Q

Turbulence/Thunderstorm Penetration

A
  1. Crew and Passengers - Briefed
  2. Seatbelts/Harness - Fastened
  3. Airspeed - 65 KIAS above power off stall, no more than 181 KIAS (VRA on V Speeds Pg in MC IDX)
  4. Aircraft Attitude- Maintain wings level. Do not attempt to hold exact altitude.
  5. Aircraft Lighting - Set
  6. Engine Power - Establish. Establish engine power for desired airspeed. Disengage AT.
  7. AFCS - Engage, as required.
32
Q

Ditching

A
  1. Configuration - 7° nose high, Flaps 100%, gear up, Vs+10
  2. Winds less than 30kts, land parallel and on top of major swell
  3. Winds greater than 30kts - Land on the upwind (back) side of the swell
33
Q

Electrical Failures Categories (3)

A

1) Loss of one or more of primary power sources

2) Faults on the main bus or distribution system

3) Faults within equipment items

34
Q

Order of Precedence Correcting Landing Gear Malfunctions

A

1) Overriding the Landing Gear Selector Valve
2) Main Landing Gear Manual Extension
3) Nose Landing Gear Emergency Extension
4) Nose Landing Gear Emergency Extension after Complete Loss of Hydraulic Pressure (Utility or Auxiliary)
5) Main Landing Gear Extension after Normal and Emergency System Failure

35
Q

Main Landing Gear Tiedown Required When:

A

Broken shelf bracket or drag pin not engaged in the shelf bracket

36
Q

Controllability Check

A

Purpose: determine minimum safe airspeed for approach and landing

Conduct if suspected damange to flight control surfaces

1) Preliminary Inspection - Accomplish
2) Climb - 10,000 ft AGL, if able
3) Fuel - Dump, as required
4) Approach Checklist - Accomplish
5) Autopilot - Disengage (Can use AT)
6) Aircraft - Configure for landing
7) Approach Airspeed/Landing configuration - Determine
- slow in 5kt increments until desired speed or control problem encountered
- Evaluate controls in turns and landing approaches
- Control problems indicated by excessive rolling, yawing, and/or pitching

If aircraft control problems encountered:
8) Airspeed - increase minimum 5kts (until touchdown)

If no problem encountered:
9) Aircraft - Land at normal landing speed

37
Q

Fuel Dumping

A

Above 5k, >3NM offshore, not in circular pattern, don’t transmit on HF or MSS radar (“5-3-OH”)

1) ATC - notify (adjust gross weight)
2) Quantity - Set, as desired
3) X Feed switches - Close
4) Dump Switches- Open
5) X Ship switch - Close (if L or R dump valve fails to open, open x ship)
6) Transfer Switches - From
7) Fuel Qty Indicators - Monitor

When fuel dumping complete:
8) Transfer switches - Off
9) Dump Switches - Close
10) L/R Dump VLV Open ACAWS - Verify
11) Perf WGT FOB - Correct to new load (PERF INIT WEIGHT)
12) Fuel Manifold - Clear (wing low attitude and slight side slip)

38
Q

Hot Brakes

A

1) Move aircraft clear of active runway
2) Do not taxi into confined/congested areas
3) Be prepared for wheel fires after aircraft is stopped
4) Request fire department crash crew to make inspection of brakes and tires
5) Determine danger zone, comply with crew actions

“Clear, Avoid, Aware, Call, Crew Action”

39
Q

Rapid Descent (Full Flaps)

A

Used if structural damage is known or suspected unless configuration may induce further damage.

1) Power Levers - FLT IDLE
2) Landing Configuration, 100% Flaps
3) Descend at 145KIAS

40
Q

Rapid Decent at VD (clean)

A

Used if there’s no indications of structural damage. When flying in excess of VH, avoid moderate and severe turbulence.

1) FLT IDLE
2) Clean configuration

41
Q

STALL (Voice)

A

1) Power Levers - Takeoff, as necessary
2) Pitch Attitude - Adjust (lower nose as altitude allows)
3) Maintain 5-10 kt above stall warning speed until clear of obstacles

Gouge: relax, max, level, speed

42
Q

Handling Emergencies Guidance

A
  1. Stabilize the Aircraft
  2. Analyze the Situation
  3. Take Coordianted Corrective Action
  4. Monitor the Situation
43
Q

ESS DC BUS OVERLOAD (A) ACAWS during APU start

A

No maintenance action is required unless the ACAWS message is coupled with a Tranformer Rectifier (TR) failure and/or another bus fail ACAWS message.

(2-A-26)

44
Q

Pusher Test Fail

A

A 5-minute cool-down period is required between stick pusher activations to prevent damage to the stick pusher activator.
(2-A-51)

2 failed tests = NO GO

45
Q

Nuisance PROP 1(2, 3, or 4) LO PITCH STOP FAIL (W) ACAWS

A

To identify the nuisance ACAWS, prior to departure, place power levers to FLT IDLE for greater than 30 seconds. This check remains valid until the power levers are moved into the ground range
(2-A-65)

(1) HC-130J (15 decks)

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