H65 Question bank 2007

List the PROHIBITED MANUEVERS that apply regardless of aircraft weight:

Nr high is limited to ______ KIAS and ____ degrees angle of bank.

“CHECK CDU” and “ENGINE EXCEED” annunciations DO/DO NOT constitute secondary indications of a malfunction

A “FEED TANK” warning light will illuminate at approx. ___ pounds of useable fuel remaining in the feed tank.

A FADEC safety feature stops/limits engine TQ to what percentage during normal operation on the FLI?

A heavy load hoist is ______ pounds and requires a ______ rest period between delivery and recovery.

A low speed _____ downwind turn, particularly in high winds, may allow a number of ULY factors to influence the helicopter.

A minor FADEC/governor failure will be indicated by the illumination of ____________.

A normal load hoist is _______ pounds and requires a _____ rest period between delivery and recovery.

A speed of ____ KIAS and _____ RPM will result in maximum autorotative glide distance.

A speed of ____ KIAS and _____ RPM will result in minimum autorotative rate of descent.

An engine shall run for a minimum of _____ seconds following an engine rinse.

An NVG − Aided Approach to a Controlled Hover (NATCH) may be executed when aided with NVGs if positive visual contact with the surface can be maintained at or above _____ ft AWL.

Any operation of the engines in the 30 Second power range will require major engine maintenance. The helicopter shall be landed ____________________

Assuming that no fuel fumes are present, how many times should a popped circuit breaker be reset?

At a ___ degrees nose up attitude, the tail skid and main landing gear (fully compressed struts) will contact simultaneously.

Due to degradation of depth perception below ___ ft while wearing NVGs, the SP shall continue to scan instruments, particularly RADALT, to prevent inadvertent descent and water contact.

Due to tail rotor control limitations, landing in crosswind components exceeding ____ knots is prohibited.

During a CATCH, the CDU will generate the pattern to place the helicopter approximately ____ feet short of the Hover At point.

During a MATCH, if determined by time alone, the GATE is arrived at 60 seconds after rollout on the windline in no−wind conditions. An additional ____ seconds is added for each ____ knots of wind.

During an ITO, consideration should be given to using the MFD _____ page as a reference and maintaining a centered vector arrow on climb out to achieve a straight as possible course when conducting the maneuver.

During engine start automatic engine shutdown will occur when _____ or _____?

During free fall deployments of the rescue swimmer, if flight conditions permit, remain at or below ____ feet RADALT once “GO ON HOT MIC, CHECK SWIMMER” has been given.

During HOVER FLIGHT, transient power spikes are limited to a maximum of ___on the FLI.

During night operations, it may take up to _____ minutes for eyes to adjust from NVG aided to unaided.

During the engine rinse, the maximum N1 decrease of the idled engine is ____%.

Engine oil pressure warning lights illuminate when the corresponding engine oil pressure drops below ____ PSI?

Extended use of NR HI above the ____________ airspeed, may cause damage to aircraft systems and has the potential to have long term fatigue effects on the main rotor system. Normally the Nr switch should not be in the HI position above ______airspeed.

FADEC 1 FAIL caution light, a red engine status light on the overhead quadrant, a dual-engine FLI display with OEI, and all other engine parameters normal are symptoms of what emergency?

Flight without main gearbox lubrication should be sustainable for approximately ______?

For any suspected engine malfunction, the following basic procedures apply and will be referred to as the "Big 4."

For avionics cooling purposes, the COOL switch shall be on when OAT is _____ degrees C or above.

Hover flight is defined as any zero or near zero ground speed operation in winds of ___ knots and below, or any steady state hover operation where the relative wind does not exceed ___ knots.

How long will a fully charged battery power the DC System with the avionics switches on?

How long will the battery power the DC system with the Avionic switches off?

If a suitable landing surface is not available for a tail rotor malfunction, a __________ to the best available area is required.

If engine does not stop immediately when FADC Control Switch is moved to off, the FADEC will shut down the engine ______ seconds later. Do not move the Emergency Fuel Shutoff Lever to the shutoff position before ____ seconds have elapsed.

If not manually secured, fuel will jettison to approximately ____ pounds remaining in the left system and approximately ____ pounds in the right system.

If pedal force is released while the helicopter is turning at a rate faster than ____ degrees per second in either direction, the AFCS does not hold heading until the yaw rate decreases to _____ degrees per second.

If the training switch is placed to flight at power settings above ____, actual OEI time may be accrued.

If thunderstorms are inadvertently encountered, trim the helicopter for level flight and establish the turbulence penetration airspeed of _______ KIAS.

If you suspect you have encountered "uncommanded left yaw", you should:

In an actual single engine situation, the maximum power available is attained at the _________ rating and _____RPM. Power decreases as NR drops below _____ RPM.

In back-up mode, FADEC will match the ____ of the affected engine to the ____ of the good engine.

In flight, the XMSN OIL pressure indication fluctuates and then slowly goes to zero. This is a symptom of what emergency?

In flight, you experience a GB CHIP annunciation on the WCA panel and a MGB CHIP annunciation on the VEMD Caution/Fuel page accompanied by yaw kicks. What emergency are you experiencing?

In flight, you have just noticed the MGB PRESS warning light, MGB PMP MAIN caution light, MGB PMP AUX caution light, and the vertical scale XMSN press is at zero. Your malfunction is ___________?

In flight, you observe N2 significantly above NR and zero torque on the malfunctioning engine. What emergency do you have?

In order to prevent settling with power, the maximum rate of descent is with an external load attached is_____?

In the event of an in-flight engine restart, the start sequence will not initiate until N1 is below _____?

In the event of dual DC generator failure, the T/R CAN/CANNOT power either main DC bus with the battery switches secured.

Limit the total number of starter engagements to ________ consecutive attempts. For cooling purposes, allow a minimum of ____ seconds between start attempts, and _____ minutes after the final attempt.

Limit use of starter cranking to ____ seconds maximum duration with a _____ second rest between each period. A maximum of ___ consecutive cranking periods are allowed, to be followed by a _______ minute rest.

List the bold-faced corrective actions for all engine start emergencies:

List the equipment that is hydraulically isolated during a Secondary Hydraulic System Low Fluid Level:

List the items interfaced through SCC1

List the items interfaced through SCC2

MGB/Engine oil cooler fan failure may not be evident at airspeeds above ____ KIAS.

Movement of the tail rotor pedals while the main rotor is below ____ RPM is prohibited?

Movement of the training switch back to flight with the FLI above ___ should only be done in extreme circumstances when aircraft damage is likely to result if the training switch is left in Idle 1/2.

Only the ____ has the authority to deploy the rescue swimmer.

Operation of the crank button with the EFSL pulled will cause severe damage to the _____________.

Radio transmissions should be minimized if fuel fumes are present. Due to antenna location, _________ is the best choice of radios.

Regardless of the nature and severity of the emergency, the overriding consideration must be to:

Restricted operations may be conducted up to what maximum weight?

Simultaneous fuel jettison from both systems occurs at a rate of ____ Lbs per minute.

T/F - Loss of the primary hydraulic system requires you to lower the wheels with the emergency landing gear handle.

T/F When inputting a HOLD into the CDU on the LS-2 line, you are inputting your outbound course.

T/F CO2 should be directed into the battery compartment to effect cooling or displace the explosive gases.

T/F During normal operation, the auxiliary element of the MGB oil pump is not used for lubrication. Therefore the corrective action in case of a MGB PMP AUX caution light is to continue flight as appropriate.

T/F HF radio transmissions are not recommended during DF operation as this will cause the BDI relative bearing pointer to swing.

T/F It is recommended that the MK-25 be deployed from a steady hover.

T/F Leaving the voltmeter switch in the BAT position for an extended period of time will deplete the battery.

T/F Maneuvers based solely on the TCAS traffic display are recommended.

T/F The CATCH procedure allows the helicopter to execute a precision approach to any waypoint while providing obstacle clearance along the final approach path.

T/F The term ABORT MISSION allows continued flight to the DESIRED RECOVERY BASE.

T/F The transfer pump will pump all fuel from the system being emptied, minus fuel in the feed tank and unusable fuel?

T/F When coupled to the AFCS, the flight director will command flight control movements in accordance with published aircraft limitations.

T/F While you are in the traffic pattern using the Abbreviated Landing Checklist, it is mandatory for the crewman to check the landing gear down before each landing.

T/F A CDU1 failure will result in a loss of radar scan-to-scan integration

T/F A combination of the engine oil pressure gauge decreasing or reading zero AND illumination of the OIL P warning light should be treated as an indicating malfunction.

T/F Due to the center of gravity of the basket, survivors shall be brought into the cabin feet first.

T/F During a BATTERY OVERTEMPRATURE/THERMAL RUNAWAY, securing the BATT RELAY switches will stop and reverse the battery over temperature/ thermal runaway.

T/F During a land/ditch immediately situation, the potential loss of the airframe after aircrew egress is sufficient to continue flight.

T/F During a ULY situation, it is recommended that you gradually apply right pedal to avoid a pedal-induced overtorque if possible.

T/F During in flight emergencies fuel system circuit breakers can all be reset, however, never more than once.

T/F During the Before Starting Engines checklist, you notice a steady “GOV” light illuminated on the WCA panel. You may recycle the BATT RLY switches as many times as necessary to extinguish the “GOV” light.

T/F It is recommended that the EP-1 handbook be referred to when completing non-critical corrective actions

T/F Loss of the REF input to the copilot’s HDG gyro will result in invalid VOR indications.

T/F Loss of the REF input to the pilot’s HDG gyro will result in invalid VOR indications.

T/F No fire extinguishing capability is provided for the Main Gearbox compartment.

T/F Only a qualified pilot may conduct the preflight walk-around inspection?

T/F Prior to take off you are required to check the CDU ECMS page as part of the “center instrument panel check”.

T/F Prolonged operation in salt water spray may result in engine parameter divergences due to salt ingestion by the engines.

T/F Simultaneous use of the hoist and cargo hook is prohibited.

T/F The engines can be started using external AC power.

T/F The most recently tuned COMM 1 frequency will be available after activation of the Emergency Electrical Cutoff Switch.

T/F The term ABORT MISSION allows for the aircraft to continue on its assigned mission so long as the failed component is not required to accomplish the mission and no airframe or component limitations have been exceeded

T/F The term LAND AS SOON AS POSSIBLE requires the aircraft to be landed at the first site at which a safe landing may be made.

T/F The term LAND AS SOON AS PRACTICALBE requires the aircraft to be landed at the first site at which a safe landing may be made.

T/F To prevent possible damage to the aircraft and a possible fuel spill, the hoist cable should not be sheared while the HIFR nozzle is connected.

T/F Use of the Quick Splice eliminates the hoist automatic hoist automatic speed reduction and up limit switches.

T/F: In the event the FCS is placed in the IDLE or FLIGHT position prior to the battery being turned on, FADEC logic will prevent the START sequence.

T/F: Once an engine is shutdown by the FADEC/BIM, overspeed protection is automatically inhibited on the second engine?

Takeoff is not authorized unless the temperature difference between the two FADEC thermal probes is less than or equal to ______ degrees C.

The ALT FD mode works in the _______ axis/axes.

The APPR FD mode works in the _______ axis/axes.

The BIM/FADEC will shut down an engine at an N2 speed of ____% or ____ RPM?

The bold-faced corrective actions for s MAIN DC BUS SHORT are:

The FADEC will automatically shut the engine down during start if the TOT exceeds ______ degrees C. The pilot shall initiate a shut down if it appears that the TOT will exceed ______ degrees C.

The flight mechanic tells you that the cabin sliding door is jammed. What is the only bold-faced corrective action for this emergency?

The GA FD mode works in the _______ axis/axes.

The HDG SEL FD mode works in the _______ axis/axes.

The HOV AUG FD mode works in the _______ axis/axes.

The IAS FD mode works in the _______ axis/axes.

The IAS-ALT FD mode works in the _______ axis/axes.

The IAS-VS FD mode works in the _______ axis/axes.

The instrument flight speed range is _____ KIAS to ______ KIAS.

The interval for repetitive hot refueling should not routinely exceed:

The landing gear _____ be kept extended whenever the cargo hook is installed.

The maximum amount of fuel that should be taken during a hot refuel evolution is ____ Lbs.

The maximum angle of bank with an external load attached is _____?

The maximum permissible cargo hook load weight is ________ lbs.

The NAV FD mode works in the _______ axis/axes.

The recommended transition point for a NATCH is defined as ____ nm downwind of datum at _____ ft AWL and _____ KIAS.

The T-HOV FD mode works in the _______ axis/axes.

The VS FD mode works in the _______ axis/axes.

Transition flight is defined as flight from zero to ____ KIAS.

Use of ALT FD mode is limited to minimum airspeed of ____________________.

Use of APPR FD mode is limited to airspeeds above ______ KIAS and _______ degree glidepath.

Use of GA FD mode is limited to a minimum of_____ feet AGL.

Use of HDG SEL FD mode is limited to minimum airspeed of ______ KIAS.

Use of HOV AUG FD mode is limited to ______________________.

Use of IAS-ALT FD mode is limited to minimum of _____ KIAS, rates of climb/descent from ________ FPM, and _____ % MCP.

Use of IAS-VS FD mode is limited to minimum of ________ KIAS, rates of climb/descent from ________ FPM, and ________ % MCP.

Use of NAV FD mode is limited to airspeeds above ______ KIAS.

Use of the IAS FD mode is limited to airspeeds above ____________________.

Use of T-HOV FD mode is limited to below __________ RADALT.

Use of VS FD mode is limited to minimum airspeed of _____ KIAS and rates of climb/descent from ______ FPM.

What are the bold faced corrective actions for an engine chip light?

What are the boldface steps for the engine shutdown in flight procedure?

What are the bold-faced actions for a lost swimmer at night?

What are the bold-faced actions for leaving a rescue swimmer on scene?

What are the bold-faced corrective actions for a dual engine oil cooler fan failure?

What are the bold-faced corrective actions for a major FADEC/governor failure?

What are the bold-faced corrective actions for a MGB Failure Imminent?

What are the bold-faced corrective actions for a primary hydraulic system failure?

What are the bold-faced corrective actions for a secondary hydraulic system failure?

What are the bold-faced corrective actions for an engine gearbox/output shaft failure?

What are the bold-faced corrective actions for an engine post shutdown fire?

What are the bold-faced corrective actions for an engine surge or compressor stall while on deck?

What are the bold-faced corrective actions when main rotor blade damage is known and airframe vibrations are more than mild with drastically altered flight characteristics?

What are the bold-faced procedures for an internal fire?

What are the bold-faced procedures for smoke & fume elimination?

What are the bold-faced steps for an engine lubrication system failure?

What are the five methods of deploying the rescue swimmer?

What causes the DIF N1 light to illuminate?

What equipment must be operating in order to execute a CATCH?

What is the absolute VNE (power off)?

What is the absolute VNE (power on)?

What is the bold-faced corrective action for a Loss of Tail Rotor Thrust in Forward Flight or Fixed Tail Rotor Pitch?

What is the bold-faced corrective actions for a BATTERY OVERTEMPRATURE /THERMAL RUNAWAY?

What is the FLI indication for Max Continuous Power?

What is the FLI indication for Max Takeoff Power?

What is the max unrestricted gross weight of the HH-65C?

What is the maximum airspeed with NR HI?

What is the maximum airspeed with skis installed?

What is the maximum airspeed with the float bags armed or inflated?

What is the Maximum allowable pressure for pressure refueling?

What is the maximum brake speed with a gross weight at or less than 8,900 Lbs?

What is the maximum brake speed with a gross weight greater than 8,900 Lbs?

What is the maximum cargo hook load speed?

What is the maximum continuous NR (power off)?

What is the maximum forward airspeed for cabin sliding door movement?

What is the maximum forward airspeed for rescue hatch movement?

What is the maximum forward airspeed with the cabin sliding door locked in the open position?

What is the maximum forward airspeed with the cabin sliding door removed?

What is the maximum forward airspeed with the rescue hatch locked open?

What is the maximum sideward airspeed for rescue hatch movement?

What is the maximum sideward airspeed with the rescue hatch locked open?

What is the maximum sideward flight speed?

What is the maximum touchdown speed with skis on snow?

What is the maximum touchdown speed?

What is the maximum transient NR (power off)?

What is the minimum continuous limit for NR (Power On)?

What is the minimum engine oil temperature for placing the FCS to flight?

What is the minimum equipment required for ship/helo operations?

What is the minimum floatation bottle pressure during preflight?

What is the minimum fuel pressure required for engine start?

What is the minimum landing gear blow down bottle pressure during preflight?

What is the minimum transient limit for NR?

What is the rotor brake limitation (NR) for stopping the rotor system?

Wheels _____ be down during over water operations unless a landing is not reasonably foreseeable due to the distance from a suitable landing spot.

When below _____ ft AWL and below _____KIAS, the sliding door shall be open over water.

When conducting an external power start, with the spike suppression switch in the "start protection" position, ensure that the _____________ light has extinguished to ensure proper operation.

When conducting an FMS approach, the aircraft should be within ____ feet of the FAF altitude as displayed on the CDU, otherwise VERT may not capture.

When may you jettison fuel?

When shooting a MATCH, if OADS airspeed information is unavailable, the maneuver becomes very demanding due to the possibility of backing down. Consideration should be given to maintaining at least ____ KIAS.

When should the rotor brake be applied after a successful water landing?

When using the BKP pump to extend the landing gear, allow approximately ______ seconds for the gear to extend and lock in the down position.

When you apply the rotor brake, what is the maximum application period allowed before you should release it and record the exceedance in ALMIS?

When you place the FADEC Control Switch to idle during engine start, the battery voltage must be _____?

Which AFCS channels are redundantly powered by the #1 and #2 main DC buses?

While not indicated on the FLI, the actual FADEC stop during AEO is set at _____% FLI

While taxiing to the ramp, the #2 engine FIRE light illuminates. You take the following bold-faced corrective actions:

With the NR HI set to HI, Nr is _____ rpm.

With the NR HI set to HI, Nr is _____ rpm.

With the START RBK switch depressed, engine idle is limited to ____% N1

With the START RBK switch depressed, the use of the engine is limited to ____ seconds if the Engine Oil Pressure is less than or equal to ____.

With the START RBK switch in the “off” position, the engine idles at ___% N1?