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E-2C NATOPS > EPs and Warnings > Flashcards

EPs and Warnings Flashcards

1
Q

State the boldface for Fail to Feather Procedure.

A
  1. Power lever (operating engine) - As Required
  2. Configuration - Gear Up, Flaps 10 deg, Max Rudder 20 deg.
  3. Airspeed - As Required
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2
Q

State the warning associated with the Fail to Feather EP.

A

Warning:

Flaps set greater than 10 deg will adversely impact single engine rate of climb and/or directional control.

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3
Q

State the boldface for Smoke or Fumes from Air-Conditioning System.

A
  1. Personnel AIR COND switch - OFF

2. Don Oxygen - 100%

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4
Q

State the boldface for Fire, Smoke, or Fumes.

A
  1. Don Oxygen - 100%
  2. Isolate affected equipment.
    * If source cannot be immediately isolated:
  3. GEN switches - OFF
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5
Q

State six WARNINGS embedded within the boldface procedures for Fire, Smoke, or Fumes.

A

WARNING:
1. Circuit Breakers should be reset in flight only if associated equipment is essential to the safety of flight and then reset only once.

  1. At any time a fire is uncontrollable the crew should bailout or ditch.
  2. Selecting both Generators OFF and placing the EMER GCU switch to OFF will isolate all electrical busses in the aircraft. IN extremis, this may be the only way to gain control of a severe electrical fire.
  3. Smoke elimination procedure may have to be executed during an uncontrollable fire to execute bailout.
  4. During Electrical arcing or fire, KAPTON wiring/Teflon coating may generate toxic fumes (colorless, odorless) causing irritation to nose and throat. Excessive inhalation of these fumes may result in heart palpitations and death within 4-6 hours.
  5. The generators should not be turned ON or OFF in the presence of fuel fumes or fuel vapors.
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6
Q

State the boldface for Smoke or Fume Elimination Procedure.

A
  1. PERSONNEL AIR COND switch - ON

2. SIDE WINDOW DEFOG - MAX

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7
Q

State five WARNINGS embedded within the boldface procedures for

A

WARNINGS:
1. Complete Fire, Smoke, or Fumes procedure before initiating this procedure.

  1. Should fire re-ignite execute the Fire, Smoke, or Fumes procedure.
  2. During electrical arcing or fire, KAPTON wiring/Teflon coating may generate toxic fumes (colorless, odorless) causing irritation to nose and throat. Excessive inhalation of these fumes may result in heart palpitations and death within 4-6 hours.
  3. If smoke or fumes intensify refer to Smoke or Fumes from Air-Conditioning System procedure.
  4. The cockpit door should not be opened. When smoke/fumes originate outside the cockpit, keeping the door closed with the air-conditioning on and the side window defog max will keep positive pressure inside the cockpit.
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8
Q

State the WARNING associated with the rudder stop release handle.

A

WARNING:

1. The Operator shall not attempt to hold release handle if q-feel speed is being cycled.

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9
Q

State the boldface for Explosive Decompression.

A
  1. Don Oxygen - As Required.
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10
Q

State the Note associated with Explosive Decompression EP.

A

NOTE:

1. If explosive decompression occurs above 10,000 feet, don Oxygen masks 100%.

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11
Q

State the boldface for Bailout.

A
  1. Inform crew
  2. Don oxygen/Emergency oxygen - As Required
  3. depressurize cabin.
  4. MEH - Jettison.
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12
Q

State three WARNINGS embedded within the boldface procedures for Bailout.

A

WARNING:
1. Above 20,000ft or if smoke is present, failure to don 100% oxygen and connect to emergency supply will result in hypoxia or smoke inhalation during egress.

  1. Prior to jettisoning door, ensure that the cabin pressure is within 2,000 ft of aircraft altitude. Time to depressurize is 10 seconds at 20,000 feet and 15 seconds at 35,000 ft when using both the RAM AIR VALVE and the CABIN PRESS DUMP switch. Failure to reduce cabin pressure will prevent retraction of door pins.
  2. Ensure FEC is clear of personnel prior to jettison. Emergency jettison handle must be pulled up approximately 40 deg and left up until door is jettisoned. returning handle to the stowed position will reseat pins.
  3. With hatches open, negative pressure may prevent jettisoning of the main entrance hatch.
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13
Q

State the procedures for parachute descent.

A
  1. (C)heck condition of main canopy and full riser separation immediately following opening shock of canopy.
  2. (R)emove oxygen mask and disconnect from emergency oxygen supply hose.
  3. (I)nflate LPFC.
  4. (R)elease life raft.
  5. (O)ptions.
  6. (K)och fittings, prepare for landing.
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14
Q

State the procedures for Ditching Checklist Before Impact.

A
  1. LDG GEAR - UP
  2. Flaps - As Required
  3. Ditching Hatches - OPEN/REMOVE
  4. MAX RUDDER - As Required
  5. Harness - LOCKED
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15
Q

State the procedures for Ditching Checklist after Impact.

A
  1. Don SEBD bottle - As Desired
  2. Service Lead - DISCONNECT
  3. Upper Koch Fittings - DISCONNECT
  4. Reference Point - SELECT
  5. Lower Koch Fittings - DISCONNECT
  6. Abandon Aircraft
  7. Swing clear of aircraft and inflate LPU
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16
Q

State three WARNINGS embedded within the boldface procedures for Ditching.

A

WARNING:
1. With one engine feathered and the other windmilling, normal and emergency electrical flap operation can be restored by placing the feathered engine’s condition lever to run and it’s T-Handle in. Do not return a T-Handle to the in position if that engine was secured for a fire.

  1. This will produce a rush of air forward to the cockpit and out through the copilot’s ditching hatch. Use force against the CIC ditching hatch to prevent possible head injury.
  2. Ensure the cockpit ditching hatches are completely aft and locked in position. Failure to do so may result in ditching hatches slamming closed upon impact, thus prohibiting the pilot/copilot from safely egressing the aircraft.
17
Q

State six WARNINGS embedded within Ditching after impact checklist.

A

WARNING:
1. If oxygen is necessary up to the time of impact, remove oxygen mask from helmet immediately after impact.

  1. The upper Koch fittings should be released first, followed by the lower Koch fittings. This procedure will preclude “hanging-up” inside the aircraft if the aircraft comes to rest inverted. The lower strap may be used as an initial reference point.
  2. UWARS will not release the crewmember from the seat. If ditching in seawater, UWARS will fire, however, it will only release the main canopy. Therefore, the upper Koch fittings must be released.
  3. If connected to the emergency oxygen hose it must be detached in order to egress the aircraft.
  4. If SEBD use is required during egress from a submerged aircraft, aircrew shall maintain regular breathing during the ascent.
  5. To prevent the possibility of lung damage and/or arterial gas embolism during a rapid ascent, aircrew shall maintain steady exhalation. Consider delaying inflation of the LPU to prevent any overly rapid ascent.

E-2C NATOPS (6 decks)

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