P-3 Memory Items

Card Set Information

Author:
donconquistador
ID:
213142
Filename:
P-3 Memory Items
Updated:
2014-05-29 09:47:16
Tags:
EPs EP Memory
Folders:

Description:
EP Memory items. Updated to reflect MAY 2013 Change.
Show Answers:

Home > Flashcards > Print Preview

The flashcards below were created by user donconquistador on FreezingBlue Flashcards. What would you like to do?


  1. No. 1,2,3 or 4 engine STARTER CONTROL VALVE OPEN light on
    If light remains on or comes on after start, secure engine by pulling emergency shutdown handle
  2. FUS DUCT HOT light on
    • 1. On ground, secure ground air-conditioning and all engine and APU bleed air, and return to the line
    • 2. In flight, close all engine bleed and fuselage shutoff valves
  3. START VALVE light on
    1. Check overhead panel for individual engine start control valve open light
  4. NTS INOP light
    • 1. Continue holding out on feather button. (FE)
    • 2. Emergency shutdown handle -- Pull. (FE)
    • 3. Feather button -- Push. (FE)
  5. Fire of Unknown Origin
    • 1. Alert crew, activate fire bill -- Alerted. (CP,TC)
    • 2. Cabin exhaust fan -- OFF. (FE)
  6. Pressurization Loss
    • If cabin altitude exceeds 10,000 feet, the flight station SHALL:
    • 1. Don smoke masks.
    • 2. Alert Crew.
  7. Rapid Decompression
    • In the event of a scissor switch failure and loss of associated aircraft system functions, perform the following steps:
    • 1. Pressurization ground check switch -- TEST.(FE)
    • 2. Ground air-conditioning switch -- ON. (FE)
  8. Emergency Depressurization Procedure
    • 1. AUX VENT -- OPEN. (FE)
    • 2. OUTFLOW VALVE -- OPEN. (FE)
    • 3. EDCs -- DUMP. (FE)
    • 4. AUX VENT -- Close at 1-inch differential. (FE)
    • Without electrical power available:
    • 5. FREE-FALL CHUTE -- Open. (OBS)
  9. Emergency Descent
    • 1. Autopilot -- Disengaged. (P)
    • 2. Power levers -- FLIGHT IDLE. (P)
    • 3. Landing gear lever -- As required. (CP)
    • 4. Airspeed-- As required. (P)
    • 5. Pressurization -- As required. (FE)

    Note: Flight station shall verify obstacle clearance and altimeter setting.
  10. Ditching
    1. Alert crew time to impact -- Alerted. (CP)
  11. Brake Fire
    • 1. Request ground firefighting equipment. (CP)
    • 2. Stop the aircraft. (P)
  12. Engine Fire on the Ground
    • 1. Emergency chutdown handle -- Pull. (FE)
    • 2. HRD -- Discharged. (P, FE)
  13. Emergency Shutdown Procedure
    • 1. Emergency shutdown handle (on pilot command) -- Pull. (FE)
    • 2. HRD (fire only) -- Discharged. (P,FE)
  14. Shifting to Boost Off
    • 1. Disconnect the autopilot.
    • 2. Attempt to obtain a safe altitude.
    • 3. Set Condition V.
    •   W.If the trim tabs have been moved several degrees away from the normal trim position, the aircraft may react violently when shifting boost off.
    • 4. Trim tab setting -- Check for normal position.
    • If abnormal force is still present:
    • 5. Booster shift handle -- Pull.
    •   W - Be prepared to immediately return to boosted flight control if operation of the aircraft is diminished.
    •       - Avoid force on the affected controls while shifting to prevent a sudden change in control surface position when the boosters are turned on or off.
  15. Propeller Malfunctions
    • 1. If rpm at or above 115 percent -- Reduce airspeed (150 KIAS minimum) and perform Operation with a Pitchlocked Propeller procedure, paragraph 15.12.2. (P,FE)
    • 2. If rpm below 115 percent -- Smoothly advance affected power lever and increase TAS, noting engine indications. (P,FE)
  16. Propeller Fails to Feather
    • 1. Feather button -- In.
    •   W - If propeller feathered at step 1, ensure emergency shutdown wiper switch circuit breakers are set.
    • 2. PCO -- Press.
    • 3. Alternate bus (propellers 1 and 4) -- Select.
    • 4. PROP FEATHER circuit breakers -- Check in.
    • 5. Airspeed -- Decrease toward 150 KIAS.
    •   N: Subsequent airspeed selection should be based on aircraft gross weight and controllability.
    • If feather button light remains on:
    • 6. PROP FEATHER CONT circuit breaker -- Pull.
    •   N: If the propeller remains in an overspeed condition, refer to Operation with a Pitchlocked Propeller procedure, paragraph 15.12.2.
  17. Flight with a Cracked Front Windshield
    • 1. Turn off heat of affected panels.
    • 2. Helmets on, visors down. (P,CP,FE)
  18. Loss of All Airspeed Indication
    1. Check pitot heat -- ON. (FE)
  19. Out of Controlled Flight, Spiral and Spin Recovery
    • 1. Power levers -- FLIGHT IDLE. (P)
    • 2. Flight controls -- Neutralize. (P)
    • 3. Airspeed, AOA, turn needle -- Check. (P)
    •   N: A spiral is often mistaken for a spin. Anti-spin controls may not be effective in arresting a spiral and may aggravate the situation. The indications of a spiral are stalled AOA, pegged turn needle, and airspeed increasing. The indications of a spin are stalled AOA, pegged turn needle and stabilized airspeed.
    • If in a spin:
    • 4. Rudder -- Full opposite turn needle. (P)
    • As soon as yawing motion stops:
    • 5. Controls Neutralize. (P)
    • 6. Unusual attitude -- Recover. (P)
  20. Windshear Escape Procedure
    • 1. Max power -- Set. (P,FE)
    • 2. Pitch attitude -- 10° up. (P)
    •   W  Any attempt to recover loss of airspeed by decreasing pitch or allowing the aircraft nose to fall through is not recommended.
    • 3. Landing Gear -- UP. (P,CP)
    • 4. FLAPS -- Do not change until out of windshear. (P)
  21. Split Flap Procedures
    • 1. If uncontrollable, reset the flap handle to the previous position.
    • 2. If controllable, land with the flap handle in the selected position.

What would you like to do?

Home > Flashcards > Print Preview