P-3 Memory Items

If light remains on or comes on after start, secure engine by pulling emergency shutdown handle

• 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

1. Check overhead panel for individual engine start control valve open light

• 1. Continue holding out on feather button. (FE)
• 2. Emergency shutdown handle -- Pull. (FE)
• 3. Feather button -- Push. (FE)

• 1. Alert crew, activate fire bill -- Alerted. (CP,TC)
• 2. Cabin exhaust fan -- OFF. (FE)

• If cabin altitude exceeds 10,000 feet, the flight station SHALL:
• 1. Don smoke masks.
• 2. Alert Crew.

• 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)

• 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)

• 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.

1. Alert crew time to impact -- Alerted. (CP)

• 1. Request ground firefighting equipment. (CP)
• 2. Stop the aircraft. (P)

• 1. Emergency chutdown handle -- Pull. (FE)
• 2. HRD -- Discharged. (P, FE)

• 1. Emergency shutdown handle (on pilot command) -- Pull. (FE)
• 2. HRD (fire only) -- Discharged. (P,FE)

• 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.

• 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)

• 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.

• 1. Turn off heat of affected panels.
• 2. Helmets on, visors down. (P,CP,FE)

1. Check pitot heat -- ON. (FE)

• 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)

• 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)

• 1. If uncontrollable, reset the flap handle to the previous position.
• 2. If controllable, land with the flap handle in the selected position.