It is safe to use the crossover valve after loss of fluid from either hydraulic system, provided pressure can be ________ and ________ in the affected system with the appropriate hydraulic pressure and aux pump switches on. When the LH system is affected, set the inboard spoiler switch to cut-off. When the RH system is affected set the CIPS generator switch to EMER and turn the rudder power switch to OFF

It is safe to use the crossover valve after loss of fluid from either hydraulic system, provided pressure can be ________ and ________ in the affected...

A creeping stabilizer is a stabilizer that does not remain in a ________ and may be caused by partial loss of the stabilizer jackscrew braking. Trim position should be monitored at all times and the _________ should be held as required to maintain trim position. Under this condition, the airplane should be ________ as soon as practicable

A creeping stabilizer is a stabilizer that does not remain in a ________ and may be caused by partial loss of the stabilizer jackscrew braking. Trim position...

If inadvertent or incorrect stabilizer trimming occurs during flight, the runaway is most apt to be caused by an electrical malfunction and can best be stopped by setting the tab trim cutout switch to CUTOUT. If the trim wheel continues to rotate after the stab trim switch is set to CUTOUT, the aircrew should _______________________

If inadvertent or incorrect stabilizer trimming occurs during flight, the runaway is most apt to be caused by an electrical malfunction and can best be...

If the engine fire cannot be controlled, immediately increase airspeed to the max allowable indicated airspeed or mach number and initiate a________________ if conditions permit. Descending allows increased acceleration to max speed with resultant decrease in ________. This helps keep the fire away from the wing until the fire is extinguished or controlled.

If the engine fire cannot be controlled, immediately increase airspeed to the max allowable indicated airspeed or mach number and initiate a________________...

If the engine seizes or if the fire warning light remains on, the copilot will pull the ________ upon direction of the pilot. The engine should be visually checked for evidence of fire. While a crew member is scanning the engine from the cargo compartment, maintain _______ with the pilot.

If the engine seizes or if the fire warning light remains on, the copilot will pull the ________ upon direction of the pilot. The engine should be visually...

When the landing gear and flaps have been retracted and a safe altitude has been reached, retard the throttle for the engine on fire to IDLE. Regardless of the duration of the light, place the throttle __________when thrust requirements permit. The source of the heat can cause _______________to the engine or its accessories even though the temperature has been reduced sufficiently for the light to go out.

When the landing gear and flaps have been retracted and a safe altitude has been reached, retard the throttle for the engine on fire to IDLE. Regardless...

Unless the engine is urgently needed, do not attempt an air start until it can be positively determined that a flameout was not caused by a ruptured fuel line or similar circumstance which might result in a fire. Do not attempt air starts without starter assist if the N2 is below ______. If an air start, without starter assist, is attempted under marginal windmill air start conditions (N2 below 15%), a ___________ can occur.

Unless the engine is urgently needed, do not attempt an air start until it can be positively determined that a flameout was not caused by a ruptured fuel...

An engine air start after an emergency shutdown should not be attempted unless it is ascertained that it is ________________. A recurrence of the emergency could be more serious than the first occurrence. If an engine air start is attempted and not completed, observe a ______ sec waiting period (if possible) before attempting subsequent starts. This is to allow fuel drainage from the rear nacelle thus preventing a possible nacelle fire.

An engine air start after an emergency shutdown should not be attempted unless it is ascertained that it is ________________. A recurrence of the emergency...

A controllability check is conducted to determine the min safe _________ to maintain during approach and landing following inflight structural damage, fuel imbalance, or differential airspeed readings. Ordinarily, the check should be conducted in the landing configuration at approx. _______ft. altitude.

A controllability check is conducted to determine the min safe _________ to maintain during approach and landing following inflight structural damage,...

When a complete thrust loss is experienced, flap extension should be initiated with sufficient altitude to allow for the increased flap extension time with wind milling engines. For example at an approach speed of 160kts, it take approx. _____sec or flaps to reach 20 deg with the engines wind milling.

When a complete thrust loss is experienced, flap extension should be initiated with sufficient altitude to allow for the increased flap extension time...

Because of the lack of outside references over water, it will be difficult to determine when to start the flare. This is especially true at night. The flare should be accomplished so as to level off approximately _____ft. above the crest of the swell. Slowly retard the throttles and permit water contact in a slightly higher than normal attitude. Contact the water at a low rate of sink and slow, controllable forward speed.

Because of the lack of outside references over water, it will be difficult to determine when to start the flare. This is especially true at night. The...

Emergency exit hatches should not be removed unless absolutely necessary. Reduce airspeed as low as partial, preferably below ________, before opening either of the over wing hatches or the aft emergency hatch. If both the over wing hatches and the emergency aft hatch are to be opened, the aft emergency hatch should be opened _____ to minimize the forces acting to push the hatch inward. All hatches may be expected to open with considerable inward force if the crew entry door has been jettisoned and the emergency exit spoiler extended.

Emergency exit hatches should not be removed unless absolutely necessary. Reduce airspeed as low as partial, preferably below ________, before opening...