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)
Engine Fire on the Ground
1. Emergency chutdown handle -- Pull. (FE)
2. HRD -- Discharged. (P, FE)
Emergency Shutdown Procedure
1. Emergency shutdown handle (on pilot command) -- Pull. (FE)
2. HRD (fire only) -- Discharged. (P,FE)
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.
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)
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.
Flight with a Cracked Front Windshield
1. Turn off heat of affected panels.
2. Helmets on, visors down. (P,CP,FE)
Loss of All Airspeed Indication
1. Check pitot heat -- ON. (FE)
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 spinare stalled AOA, pegged turn needle andstabilized 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)
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)
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.