Archive for October 2020

If the source of the leakage in the system cannot be determined, the hydraulic fluid quantity gauge for the affected system should be monitored during and after actuation of the crossover valve lever. If a fluid loss of the unaffected system is observed, return the _______ to _________

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If the source of the leakage in the system cannot be determined, the hydraulic fluid quantity gauge for the affected system should be monitored during and after actuation of the crossover valve lever. If a fluid loss of the unaffected system is observed, return the _______ to _________



Answer: crossover; normal

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

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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


Answer: built up; maintained

Given: the left hydraulic pressure gauge indicates 1,800 psi with no other indications. You have determined that the accumulator preload is low and have repressurized the system. To check the actual system pressure, read the ____________ gauge by cycling the pilot's brakes

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Given: the left hydraulic pressure gauge indicates 1,800 psi with no other indications. You have determined that the accumulator preload is low and have repressurized the system. To check the actual system pressure, read the ____________ gauge by cycling the pilot's brakes



Answer: reserve brake

Given: A loss of quantity in the left hydraulic system with no other indications. You have followed the procedure through closing the supply switch for the outboard pump, but there is still a fluid loss. You would now try to isolate the leak by placing __________ to cutoff.

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Given: A loss of quantity in the left hydraulic system with no other indications. You have followed the procedure through closing the supply switch for the outboard pump, but there is still a fluid loss. You would now try to isolate the leak by placing __________ to cutoff.



Answer: inboard spoiler switch

Given: Loss of quantity in the right system with no other indications. Depressurizing the right hydraulic system does not stop the fluid leak. The next step is to close the __________ for the ______ pump.

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Given: Loss of quantity in the right system with no other indications. Depressurizing the right hydraulic system does not stop the fluid leak. The next step is to close the __________ for the ______ pump.



Answer: pump supply switch; inboard

Given: the number four hydraulic pump inoperative light comes on with no indications of fluid loss and remains on after the right hydraulic system is depressurized and repressurized. Set the _________ pump supply switch to closed.

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Given: the number four hydraulic pump inoperative light comes on with no indications of fluid loss and remains on after the right hydraulic system is depressurized and repressurized. Set the _________ pump supply switch to closed.



Answer: #4

Indications of possible fuel leakage include:

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Indications of possible fuel leakage include:



Answer: Excessive Fuel Flow; Inadequate Fuel Flow; Fuel Low PX warnings; Low Fuel QTY indications; Fuel line leakage in strut/nacelle area; Body tank Fuel QTY increasing


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

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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



Answer: trim position; trim wheel; landed

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 _______________________

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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 _______________________



Answer: stop the trim wheel with hand

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.

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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.



Answer: shallow descent; AOA

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.

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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.



Answer: fire switch; contact

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.

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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.



Answer: to cutoff; additional damage

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.

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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.



Answer: 15%; hot/hung start

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.

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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.



Answer: safe to do so; 30 sec

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.

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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.



Answer: airspeed; 10,000ft

(Fuselage Fire) Boom operator and or navigator shall institute firefighting procedures. One crewmember shall keep the ______ informed of the fire condition until it is extinguished or determined to be uncontrollable.

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(Fuselage Fire) Boom operator and or navigator shall institute firefighting procedures. One crewmember shall keep the ______ informed of the fire condition until it is extinguished or determined to be uncontrollable.



Answer: Pilot or Copilot

All fires will create toxic combustion products. Adequate respiratory and eye protection should be sought as soon as the primary fire emergency will permit. Breathing __________ will provide respiratory protection.

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All fires will create toxic combustion products. Adequate respiratory and eye protection should be sought as soon as the primary fire emergency will permit. Breathing __________ will provide respiratory protection.



Answer: 100% O2

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.

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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.



Answer: 65

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.

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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.



Answer: 10

(Ditching Operations) Hold the wings level. With wind speed in excess of 30 kts and sea conditions greater than 20ft, it is recommended that ditching be made into the _____. Wind speeds in excess of 30kts are generally indicated by extensive _______ and blowing spray.

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(Ditching Operations) Hold the wings level. With wind speed in excess of 30 kts and sea conditions greater than 20ft, it is recommended that ditching be made into the _____. Wind speeds in excess of 30kts are generally indicated by extensive _______ and blowing spray.



Answer: wind; white caps

When checking, removing or re-installing hatches in flight, the crewmember making the check must ensure that a _________ and seat kit (if available) are on and properly adjusted prior to making this check.

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When checking, removing or re-installing hatches in flight, the crewmember making the check must ensure that a _________ and seat kit (if available) are on and properly adjusted prior to making this check.



Answer: parachute/restraint harness + helmet

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.

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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.



Answer: 150kts; first

When the receiver is in or near the contact position, the pilot will initiate a ______ at the first indication of autopilot malfunction, including an inadvertent autopilot disconnect if accompanied by out of trim forces.

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When the receiver is in or near the contact position, the pilot will initiate a ______ at the first indication of autopilot malfunction, including an inadvertent autopilot disconnect if accompanied by out of trim forces.


Answer: breakaway

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