/******************************************************************* AH-64 -10 CHAPTERS 5 AND 9 QUIZ SCRIPT DEFINITIONS Provided by www.gomotherrucker.com This file is an include to be used with the CH-47D 5 and 9 review .htm file. It contains all the five and nine questions and answers in arrays so they can be retrieved easily by the script. Carats (^) are placed around values that are to be substituted for blanks in the quiz. Add or remove carats as necessary to easily modify the quiz. CARATS MUST BE IN PAIRS around the values in order for this to work right. ^7^ will work but if ^7 is used without the following carat, this will create errors! If you have the know-how, feel free to modify this and tweak it however you see fit. Note: ° is HTML escape sequence for degree symbol.
is HTML line break. *******************************************************************/ //******************* Last_Updated="04DEC10"; //******************* //******************* Ticker_Text="Thanks to www.gomotherrucker.com for providing the AH-64 definitions for this quiz!"; Standalone_Ticker_Text="NEW Quizzer! Thanks to www.gomotherrucker.com for providing the AH-64 definitions for this quiz!"; //******************* fivequestion=new Array(); fiveanswer=new Array(); ninequestion=new Array(); nineanswer=new Array(); //predefined strings to create colored boxes for instrument limits function box(color){ return " "; } redbox=box("ff0000"); yellowbox=box("ffff00"); greenbox=box("00ff00"); bluebox=box("004080"); blankbox=" "; //******************************************************************* fivequestion[0]="Np Limits"; fiveanswer[0]="^121^ Max (greater than ^121^ red with box)
^115^ engine overspeed annunciated
^106^ to ^121^ Transient operation ^12^ seconds (Yellow with box at ^107^)
^0^ to ^105^ Normal Operation"; fivequestion[1]="Gross Weight:"; fiveanswer[1]="The aircraft maximum gross weight is ^20260^ pounds, except for ^non^ ^tactical^ ^ferry^ flights, which may not exceed ^23000^ pounds."; fivequestion[2]="Nr Limits"; fiveanswer[2]="^110^ max ( >^110^ RED)
^106^ to ^110^ transient operation
^106^ High Rotor Warning Annunclated
^95^ to ^105^ Normal Operation
^0^ to ^94^ Transient Operation"; fivequestion[3]="Engine Starter Limitations"; fiveanswer[3]="Temp 16 Degrees C and Below:
^two^ ^consecutive^ start cycles may be made, followed by a
^3^ minute rest period followed by ^two^ additional start cycle. A ^30^ ^minute^ rest period is then required before any additional starts.

Temp above 16 degrees C
^two^ ^consecutive^ start cycles may be made. A ^30^ ^minute^ rest period is then required before any additional starts.

Dual Engine Starts
Duel engine starts are ^prohibited^ due to ^insufficient^ ^ipas^ ^air^"; fivequestion[4]="701C Engine, TGT (degrees C) DIGITAL READOUT"; fiveanswer[4]="^0^ to ^810^ Normal operation (Green)
^810^ Maximum Continuous Power
^811^ to ^851^ Intermediate rated power ^30^ minutes limit (Yellow)
^851^ Maximum during Start
^852^ to ^878^ Intermediate rated power ^10^ minutes limit (Yellow)
^879^ to ^903^ Single engine contigency ^2.5^ minutes limit (Yellow)
^904^ to ^949^ Single engine transient ^12^ second limit (Yellow)
^949^ Maximum (greater than ^949^ Red)
Dual Eng TGT limiter: ^867^ plus or minus ^12^ degrees C
Single Engine TGT limiter: ^896^ plus or minus ^12^ degrees C"; fivequestion[5]="Extended APU Ground Operations Caution"; fiveanswer[5]="Do not operate the APU for more than ^5^ minutes at a main transmission oil temperature of ^120^ - ^130^ degrees C. Shutdown APU to prevent damagining ^accessory^ ^gearbox^ ^components^"; fivequestion[6]="Ng Limits"; fiveanswer[6]="^105.1^ Maximum (Greater than ^105.1^ Red)
^102.3^ to ^105.1^ Transient ^12^ second limit (Yellow)
^63.1^ to ^102.2^ Normal Operation (Green)
^63^ Minimum engine out warning annunciated (less than ^63.0^ (don't forget decimal) Red with Box)"; fivequestion[7]="APU Operating Limitations"; fiveanswer[7]="APU operation is prohibited during ^normal^ ^flight^. After a fault or aborted start, wait ^30^ seconds after the compressor has stopped before attempting another start. After ^2^ consecutive start attempts, wait ^20^ minutes before third start attempt. No more than ^3^ start attempts are permitted in ^1^ hour."; fivequestion[8]="Hydraulic Pressure Limits" fiveanswer[8]="> ^3410^ Transient operation permitted for ^5^ seconds (yellow)
^3310^ - ^3400^ Transient operation permitted for ^5^ minutes (yellow)
^2750^ - ^3300^ Normal Operation (green)
^1260^ Minimum (Less than ^1260^ red w/ box)
^2600^ Min PSI needed for APU Start"; fivequestion[9]="APU Operating Limitations Caution"; fiveanswer[9]="Avoid prolonged operation at ^94^ to ^96^% Nr with the APU running. The APU clutch will oscillate from engaged to disengaged. This creates ^high^ ^loads^ on the ^clutch^ and shall be avoided"; fivequestion[10]="Torque Limits"; fiveanswer[10]="With less than 50% Nr
^30^% Max
^0^ to ^30^% Normal
With less than 90% Nr
^70^% Max
^0^ to ^70^ Normal
DUEL Engine
^115^ Max
^101^ to ^115^ Transient ^6^ seconds
^0^ to ^100^ Normal
Single Engine
^125^ Max
^123^ to ^125^ Transient ^6^ seconds
^111^ to ^122^ Single Engine Contingency ^2.5^ Minutes
^110^ Single Engine Max Continuous
^0^ to ^110^ Normal Operation"; fivequestion[11]="Engine Oil PSI Limits"; fiveanswer[11]="^120^ Max (Greater than ^120^ Red w/ box
^23^ to ^120^ Normal Operation (green)
^23^ Minimum Less than ^23^ red"; fivequestion[12]="Manuever Limits"; fiveanswer[12]="Maximum rearward/sideward flight speed is ^45^ KTAS for ^all^ ^gross^ ^weights^"; fivequestion[13]="Autorotation Airspeeds"; fiveanswer[13]="Max ^145^ KTAS
Min rate of descent ^77^ KTAS
Max glide distance ^107^ KTAS"; fivequestion[14]="Airspeed"; fiveanswer[14]=" Maximum airspeed with symmetrically loaded external fuel tanks (2 or 4) installed is ^130^ KTAS to prevent ^structural^ ^damage^ to the airframe"; fivequestion[15]="Flight into Icing Conditions"; fiveanswer[15]="Intentional flights into ^moderate^ icing are prohibited. Flight into ^known^ or ^forecast^ ^trace^ or^light^ icing conditions is authorized and not considered a hazard unless the condition is encountered for extended period (over ^1^ ^hour^)"; fivequestion[16]="Landing Limits"; fiveanswer[16]="Do not complete a landing in terrain which produces a ^pitch^ ^attitude^ ^change^ from a ^hover^ greather than ^7^ degrees nose up or ^12^ degrees nose down; or a ^roll^ ^attitude^ greater than ^10^ degrees. Data is not available beyond these limits at gross weights above ^17650^"; fivequestion[17]="Prevent Excessive Tail Rotor Loads"; fiveanswer[17]="Avoid ^large^ ^pedal^ ^step^ inputs in arresting ^right^ ^hovering^/^low^ ^speed^ ^yawing^ turns greather than ^60^ degrees per sec. This is to prevent ^excessive^ ^tail^ ^rotor^ ^drive^ ^system^ ^loads^"; fivequestion[18]="Use of Force Trim"; fiveanswer[18]="Force trim will not be selected ^off^ except in a ^failed^ or ^partial^ ^failed^ mode."; fivequestion[19]="Rotor Limitations - Start and Stop Limits"; fiveanswer[19]="Maximum wind velocity for rotor stop or stop is ^45^ knots to prevent ^droop^ ^stop^ ^damage^."; fivequestion[20]="Manuevering Limits"; fiveanswer[20]="Intentional maneuvers beyond attitude of +/- ^30^ degrees in pitch or +/- ^60^ degrees in roll are prohibited."; fivequestion[21]="Airspeed with one engine in op"; fiveanswer[21]="a. ^67^% of VNE determined from figure 5-13 using ^gross^ ^weight^ line.

b. The speed for minimum ^power^ determeined from chapter 7 (701) or Chapter 7A cruise charts using maximum ^endurance^ / maximum ^rate^ of ^climb^"; fivequestion[22]="Flight with Canopy Enclosure Open"; fiveanswer[22]="^flight^, ^hovering^ ^flight^, and ^air^ ^taxiing^ with the canopy enclosure open are prohibited, except for ^smoke^/^fume^ ^elimination^"; fivequestion[23]="Flight into IMC"; fiveanswer[23]="This aircraft isn't qualified for ^IMC^ ^flight^. The ^backup^ ^flight^ ^instruments^ are required to be ^installed^ and ^operational^ for all flights."; fivequestion[24]="Max airspeed for stores jettison"; fiveanswer[24]="Max ^130^ KTAS
^hover^ to ^45^ KTAS (minimize sideslip. if possible)
^45^ to ^130^ KTAS (Ball centered if possible)"; fivequestion[25]="TGT Limitations 701 Engine"; fiveanswer[25]="^965^ Maximum (Greater than ^965^ Red)
^920^ to ^965^ Single engine transient ^12^ second limit (Yellow)
^865^ to ^919^ Single engine contigency ^2.5^ minute limit (yellow)
^869^ Maximum during start
^808^ to ^864^ Intermediate rated power, ^30^ minute limit (Yellow)
^807^ Maximum continuous power
^0^ to ^807^ Normal operation (Green)"; fivequestion[26]="Maximum Airspeed during Manual Stabilator Operations"; fiveanswer[26]="Maximum airspeeds are based on ^stabilator^ ^position^. The stabilator position and nominal airspeed restrictions are displayed on the ^flt^ page, ^flt^ ^set^ page, as well as the ^sys^ page, as described in ^paragraph^ ^2.68^."; fivequestion[27]="Maximum Airspeed for Searchlight Extension:"; fiveanswer[27]="The searchlight is designed for operation (^extend^/^retract^/^rotate^) at speeds up to ^90^ knots. However, as long as operation is not attempted, the lighthead can be left in any extended position at speeds up to ^200^ knots."; fivequestion[28]="External Tanks"; fiveanswer[28]="1. Normal load factor of ^2G^s shall not be exceeded.
2. Maneuvers are limited to those required to ^takeoff^, ^climb^ to ^optimum^ ^altitude^, ^heading^/^course^ ^corrections^, ^obstacle^ ^avoidance^, ^descend^, and ^land^.
3. ^230^gal external fuel tanks shall be in the flight stow position (^4^° nose ^up^) with respect to the waterline.
4. Rapid and step-shaped pedal inputs in excess of ^0.5^ inch(use decimal) shall be avoided.
5. Operation of the aircraft with the ^230^ ^gal^ Extended Range Fuel System (ERFS) is ^prohibited^ during operations where ^hostile^ ^fire^ ^is^ ^highly^ ^probable^."; //******************************************************************* ninequestion[0]="UFD MESSAGES
ENG 1 OIL PSI"; nineanswer[0]="^emerg^ ^engine^ ^shutdown^ (when conditions permit)
^land^ as ^soon^ as ^practicable^"; ninequestion[1]="UFD MESSAGES
Both XMSN 1 OIL HOT and XMSN 2 OIL HOT"; nineanswer[1]="^land^ as ^soon^ as ^possible^"; ninequestion[2]="UFD MESSAGES
UTIL HYD PSI"; nineanswer[2]="^land^ as ^soon^ as ^possible"; ninequestion[3]="UFD MESSAGES
ROTOR BRAKE ON/LK"; nineanswer[3]="^rtr^ ^brk^ ^switch^ - ^off^
^land^ as ^soon^ as ^possible^"; ninequestion[4]="UFD MESSAGES
MAIN XMSN CHIPS"; nineanswer[4]="^land^ as ^soon^ as ^possible^"; ninequestion[5]="UFD MESSAGES
GEARBOX VIBRATIONS"; nineanswer[5]="^land^ as ^soon^ as ^possible^"; ninequestion[6]="UFD MESSAGES
Both ENG 1 FUEL PSI and ENG 2 FUEL PSI"; nineanswer[6]="^fuel^ ^page^ ^boost^ button press ^on^
^land^ as ^soon^ as ^possible^"; ninequestion[7]="UFD MESSAGES
ENG 1 FUEL PSI LOW"; nineanswer[7]="Achieve ^safe^ ^single^ engine ^airspeed^
^land^ as ^soon^ as ^practicable^"; ninequestion[8]="Land Without Delay"; nineanswer[8]="The term land without delay is defined as ^landing^ in which the ^primary^ ^consideration^ is continued ^control^ of the ^aircraft^ and ^survival^ of the ^occupants^"; ninequestion[9]="EMERGENCY ENGINE SHUTDOWN (Define and EP)"; nineanswer[9]="CAUTION: Monitor TGT after shutdown. if TGT rises above^540^ degress C or there is evidence of combustion as indicated by a rapid rise in TGT, place the engine ^start^ switch in ^ign^ ORIDE position and mointor engine until TGT decreases below ^540^ degrees C.
DEFINATION: The term EMER ENG SHUTDOWN is defined as ^engine^ ^shutdown^ ^without^ ^delay^
EP: ^power^ ^lever^ (affected engine) - ^off^"; ninequestion[10]="Emergency Egress"; nineanswer[10]="1. ^helmet^ ^visors^ ^down^
2. ^area^ ^around^ ^helicopter^ - ^clear^ of ^personnel^
3. ^canopy^ ^jettison^ ^handle^ - ^turn^ 90 degrees, ^release^ then ^push^ to ^jettison^ ^canopy^."; ninequestion[11]="Duel Engine Failure - Low Altitude/ Low Airspeed and Cruise"; nineanswer[11]="^autorotate^
^chop^ ^button^ - ^reset^ only if an ^engine^ ^chop^ warning message is present. Reset may be accomplished by either ^crewmember^.
^wing^ ^stores^ ^jettison^ - ^as^ ^appropriate^"; ninequestion[12]="Single Engine Failure - Low Altitude/Low Airspeed"; nineanswer[12]="1. ^wing^ ^stores^ ^jettison^ - ^as^ ^appropriate^
2. ^land^ as ^soon^ as ^practicable^"; ninequestion[13]="Loss of Tail Rotor Thrust in Cruise Flight"; nineanswer[13]="Continued Flight Possible

1.^airspeed^ - ^100^ KTAS minimum (until ^10^ to ^20^ feet above touchdown)
2. ^wing^ ^stores^ ^jettison^ - ^as^ ^appropriate^
3. ^power^ ^levers^ - ^retard^ as ^necessary^ (^5^ to ^10^ ft above touchdown)

Continued Flight Not Possible
1.^collective^ ^reduce^ (compromise between rate of ^turn^ and rate of ^descent^)
2. ^wing^ ^stores^ ^jettison^ - ^as^ ^appropriate^
3. ^minimize^ ^rate^ of ^descent^ (^10^ to ^20^ feet above touchdown)
4. ^power^ ^levers^ - ^off^ (^5^ to ^10^ feet above touchdown)"; ninequestion[14]="Engine 1 or 2 Overspeed - Np Failed High"; nineanswer[14]="1. ^collective^ ^adjust^ to maintain rotors within limits
If conditions persists:
2. ^power^ ^lever^ (affected engine) - ^retard^ to ^equalize^ ^torque^.
3. ^land^ ^as^ ^soon^ ^as^ ^practicable^."; ninequestion[15]="Low RPM Rotor - Np Failed Low"; nineanswer[15]="1. ^collective^ ^adjust^ - to maintain Nr within limits.
If conditions persists.
2. ^power^ ^lever^ (affected engine) - ^lockout^ and ^then^ ^retard^ to equalize torque output of both engines.
If manual control is not possible:
3. ^power^ ^lever^ (affected engine) - ^idle^
4. ^land^ as ^soon^ as ^practicable^
if continued flight is not possible, proceed as in 9.7 SINGLE ENGINE FAILURE."; ninequestion[16]="Compressor Stall"; nineanswer[16]="1. ^collective^ - ^reduce^.
2. ^power^ ^lever^ (affected engine) - ^retard^.
If THT decreases and there is no further evidence of stall.
3. ^power^ ^lever^ (affected engine) - ^fly^
if stall condition recurs:
4. ^power^ ^lever^ (affected engine) - ^idle^
5. ^land^ as ^soon^ as ^practicable^"; ninequestion[17]="Main Tranmission Input Drive Clutch Failure (Part I)"; nineanswer[17]="Inflight
1. ^power^ ^lever^ (affected engine) - ^idle^
If Np (affected engine) is below Nr (indicating the clutch is disengaged.
2. ^emer^ ^eng^ ^shutdown^ (affected engine)
3. ^land^ as ^soon^ as ^practicable^
If Np (affected engine) does not drop below Nr (indicating theh clutch has failed to disengage)
4. ^land^ as ^soon^ as ^possible^
5. ^emer^ ^eng^(s) ^shutdown^ (^both^ ^engines^ simultaneously)."; ninequestion[18]="Main Tranmission Input Drive Clutch Failure (Part II)"; nineanswer[18]="On Ground (with indications of the clutch has failed to engage)
1. ^emer^ ^eng^ ^shutdown^ (affected engine ^only^).
2. Check Ng is less than ^10^% (affected engine).
3. ^normal^ ^engine^ ^shutdown^ - ^perform^
On Ground (with indications that a clutch has failed to disengage
^emer^ ^eng^ ^shutdown^ (^both^ ^engines^ simultaineously)"; ninequestion[19]="Abort Start Procedures"; nineanswer[19]="1. ^power^ ^lever^ - ^off^.
2. ^eng^ ^start^ switch - ^ign^ ^oride^ for ^30^ seconds and TGT is below ^540^ degrees C"; ninequestion[20]="Primary Hydraulic Pressure Low and Utility Hydraulic Pressure Low"; nineanswer[20]="1. ^emerg^ HYD button - ^press^ ^on^
2. ^land^ ^without^ ^delay^
3. ^emer^ ^eng^(s) ^shutdown^"; ninequestion[21]="Both Generators Fail / Complete Loss of Electrical Power"; nineanswer[21]="1. ^gen1^ and ^gen2^ - ^reset^ ^pilot^ ^gen^ ^rst^ panel
If Conditions persists:
2. ^land^ as ^soon^ as ^possible^"; ninequestion[22]="Smoke and Fume Elimination"; nineanswer[22]="1. ^airspeed^ - Slow to ^20^ KTAS maximum
2. ^canopy^ ^door^ (affected ^crewstation^) - ^open^ to intermediate position
3. ^land^ as ^soon^ as ^possible^"; ninequestion[23]="Electrical Fire in Flight"; nineanswer[23]="1. ^gen1^ and ^gen2^ - ^off^ (SYS page).
2. ^land^ as ^soon^ as ^possible^"; ninequestion[24]="Stabilization Equipment Malfunction"; nineanswer[24]="1. ^fmc^ release ^button^ - ^press^
2. ^fmc^ - Re-engage unaffected ^fmc^ axes ( A/C UTIL page)"; ninequestion[25]="BUCS Fail/ BUCS ON (Light On)"; nineanswer[25]="1. ^land^ as ^soon^ as ^possible^
2. ^apu^ ^on^
3. ^emer^ ^eng^(s) ^shutdown^"; ninequestion[26]="Stabilator Auto/Manual Mode Failure"; nineanswer[26]="^land^ ^as^ ^soon^ as ^practicable^"; ninequestion[27]="Wing Stores Jettison"; nineanswer[27]="A. Selected Armament Wings Stores
1. ^airspeed^ - ^130^ KTAS maximum
2. Selected ^stores^ ^jettison^ buttons - ^press^ to ^arm^
3. ^jett^ ^button^ - ^press^
B. All Armament Wing Stores:
1. ^airspeed^ - ^130^ KTAS ^maximum^
2. ^collective^ ^jett^ ^button^ - press
C. External Fuel Wing Stores:
1. ^airspeed^ - ^100^ KTAS ^maximum^
2. ^selected^ ^stores^ ^jettison^ buttons - ^press^ to ^arm^
3. ^jett^ ^button^ - press"; ninequestion[28]="PNVS Failure"; nineanswer[28]="^nvs^ ^select^ ^switch^ (Pilot) - ^tads^"; ninequestion[29]="IHADSS/HDU Failure"; nineanswer[29]="1. ^nvs^ ^mode^ switch - ^fixed^
2. ^nvs^ ^select^ switch - ^tads^ or ^pnvs^
3. ^mpd^ ^vid^ - ^plt^ or ^cpg^ ^hmd^ (as necessary)"; ninequestion[30]="IHADSS Single DP Operation"; nineanswer[30]="1. ^nvs^ ^select^ ^switch^ - reselect (^pnvs^ or ^tads^)
2. ^crewmember^ (not on ^controls^) - ^assume^ ^control^"; ninequestion[31]="Duel DP/ Duel SP Failure"; nineanswer[31]="Duel DP Failure:
^land^ ^as^ ^soon^ ^as^ ^possible^
Duel SP Failure:
^land^ ^as^ ^soon^ ^as^ ^possible^"; ninequestion[32]="Deck Fire"; nineanswer[32]="^land^ ^as^ ^soon^ ^as^ ^possible^"; ninequestion[33]="Engine Fire - In Flight"; nineanswer[33]="1.^emer^ ^eng^ ^shutdown^ (^affected^ ^engine^) - when conditions permit
2. ^illuminated^ ^eng^ ^fire^ button - ^press^ and ^rdy^ light illuminates
3. ^fire^ ^disch^ ^button^(s) - ^press^
4. ^land^ as ^soon^ as ^possible^"; ninequestion[34]="APU Compartment Fire - On Ground"; nineanswer[34]="1. ^APU^ - ^off^
2. Illuminated ^APU^ ^fire^ ^button^ - ^press^ and ^rdy^ light illuminates
3. ^fire^ ^disch^ ^button^(s) - ^press^"; ninequestion[35]="APU Compartment Fire - In Flight"; nineanswer[35]="1. Illuminated ^APU^ ^fire^ ^button^ - ^press^ and ^rdy^ light illuminates
2. ^fire^ ^disch^ ^button^(s) - ^press^
3. ^land^ as ^soon^ as ^possible^"; ninequestion[36]="Engine Fire - On Ground"; nineanswer[36]="1. ^emer^ ^eng^(s) ^shutdown^.
2. ^illuminated^ ^eng^ ^fire^ button - ^press^ and ^rdy^ light illuminates.
3. ^fire^ ^disch^ ^button^(s) - ^press^."; ninequestion[37]="Fuselage Fire - On Ground"; nineanswer[37]="1. ^emer^ ^eng^(s) ^shutdown^
2. ^apu^ - ^off^ (if applicable)"; ninequestion[38]="Abort Start CAUTION"; nineanswer[38]="Abort start for any of the following reasons:
1. If it becomes apparent that TGT will exceed ^869^°C (701) or ^851^°C (701C) before NG idle speed (^63^% ^or^ ^more^) is attained.
2. If ^tgt^ does not increase within ^45^ seconds after moving POWER lever to IDLE.
3. If no ^np^ within ^45^ seconds after moving POWER lever to IDLE (unless rotor is locked).
4. If positive ^oil^ ^pressure^ indication does not occur within ^45^ seconds after moving POWER lever to IDLE.
5. If engine 1 or 2 start advisory is removed prior to attaining ^52^% NG."; ninequestion[39]="BUCS Fail:"; nineanswer[39]="WARNING
Activation of one of the BUCS FAIL cautions in-flight shall signal a ^flight^ ^control^ emergency. It can mean either a ^failure^ ^within^ ^the^ ^system^ or a mistrack between the ^crew^ ^station^ ^controls^. The CPG should only activate the BUCS trigger select if the pilot is ^incapable^ of ^maintaining^ ^control^ of the ^aircraft^.
If BUCS has been activated, attempt to land as ^far^ ^away^ from any ^known^ ^transmitters^ as practical."; ninequestion[40]="Tail Rotor Fixed Pitch Settings" nineanswer[40]="IGE Uncontrolled left: Reduce ^power^ ^levers^ in coordination with an ^increase^ in collective.

IGE Uncontrolled right: Reduce ^collective^ to begin a descent. At approximately ^5^ to ^10^ feet AGL, perform a hovering autorotation by ^CHOP^ ^button^ - ^press^ or ^power^ ^levers^ - ^off^.

OGE Flight: If little or no right rotation or if left rotation is experienced and control can be maintained, the aircraft should be ^accelerated^ into forward flight and perform ^approach^ and ^landing^ appopriate to ^power^ ^setting^ and ^condition^ at time of failure. If the aircraft cannot be ^accelerated^ into forward flight, initiate a ^power^-^on^ descent. ^Collective^ should be adjusted so that an acceptable compromise between ^rate^ of ^turn^ and ^rate^ of ^descent^ is maintained. At approximately ^5^ to ^10^ ft above touchdown, perform a ^hovering^ ^autorotation^ by ^chop^ ^button^ - ^press^ or ^power^ ^levers^ - ^off^."; ninequestion[41]="Main XMSN Input Drive Clutch Failure"; nineanswer[41]="CAUTION: When a clutch fails to ^disengage^, damage to the affected engine will result (due to lack of ^oil^ ^pressure^) if both engines are not shut down simultaneously. When a clutch fails to ^engage^, do not shut down both engines simultaneously. Damage may result if there is a sudden ^engagement^.

Indications:
1. Erratic ^torque^ indication on ^affected^ ^engine^.
2. Complete loss of ^torque^ indication on ^affected^ ^engine^.
3. ^NP^ of affected engine exceeding ^NR^."; ninequestion[42]="Engine Fires"; nineanswer[42]="WARNING: Prior to moving ^power^ ^lever^ or pressing any ^eng^ ^fire^ button, either achieve a ^safe^ ^single^ ^engine^ ^airspeed^ or prepare for a ^single^ ^engine^ ^landing^"; ninequestion[43]="Immediate Action Emergency Steps"; nineanswer[43]="NOTE: The urgency of certain emergencies requires ^immediate^ ^and^ ^instinctive^ action by the pilot. The most important single consideration is ^helicopter^ ^control^. All procedures are ^subordinate^ ^to^ ^this^ requirement^."; ninequestion[44]="Land As Soon As Possible"; nineanswer[44]="The term Land As Soon As Possible is defined as ^landing^ ^at^ ^the^ ^nearest^ ^suitable^ ^landing^ ^area^ (e.g., ^open^ ^field^) ^without^ ^delay^. The primary consideration is to ^ensure^ ^the^ ^survival^ ^of^ ^occupants^."; ninequestion[45]="Land As Soon As Practicable"; nineanswer[45]="The term Land As Soon As Practicable is defined as ^landing^ ^at^ ^a^ ^suitable^ ^landing^ ^area^. The primary consideration is the ^urgency^ ^of^ ^the^ ^emergency^."; //ninequestion[46]="After Emergency Action"; //nineanswer[46]="After a malfunction of equipment has occurred, ^appropriate^ ^action^ ^steps^ have been taken, and the helicopter is ^on^ ^the^ ^ground^, and entry will be made in the ^remarks^ Section of DA Form ^2408-13-1^ describing the malfunction. ^Ground^ and ^fligh^ operations will be ^discontinued^ until ^corrective^ ^action^ has been taken."; ninequestion[46]="Engine Power Loss - Partial or Complete Engine Malfunction or Power-Limiting"; nineanswer[46]="WARNING: Prior to movement of either ^power^ ^lever^, it is imperative that the ^malfunctioning^ ^engine^, and the corresponding ^power^ ^lever^ be identified.

Engine failure is normally indicated by a rapid drop in ^NG^, ^NP^, ^torque^, ^TGT^, ^oil^ ^pressure^, and the symbolic torque value on the MPD/HMD displays flashing."; ninequestion[47]="Engine Restart During Flight"; nineanswer[47]="WARNING:
1. A failed engine should not be restarted unless it can be determined that it is ^reasonably^ ^safe^ ^to^ ^do^ ^so^.
2. When attempting to restart ENG 1 following a single engine failure a ^malfunctioning^ ^cross^ ^feed^ ^valve^ could cause the remaining engine (ENG2) to fail."; ninequestion[48]="Autorotaion (Both Engines Fail)"; nineanswer[48]="The cyclic should be adjusted as necessary to attain and maintain the desired airspeed of ^77^ to ^107^ KTAS. In autorotation, as airspeed increases above ^70^ - ^80^ KTAS, the rate of descent and glide distance ^increase^ significantly. Below ^70^ KTAS the rate of descent will also ^increase^ but glide distance ^decreases^."; ninequestion[49]="Engine Alternator Malfunction"; nineanswer[49]="If an alternator failure is suspected and the ^affected^ ^engine^ accelerates to ^maximum^ ^power^, proceed as in ^ENGINE^ ^1^ or ^2^ ^OVERSPEED^ - NP Failed High."; ninequestion[50]="Tail Rotor Malfunctions"; nineanswer[50]="WARNING: Pilot ^situational^ ^awareness^ is critical in the successful accomplishment of these procedures. The ^low^ ^inertia^ ^rotor^ system, coupled with high ^rates^ ^of^ ^descent^ during vertical autorotation, may not provide the pilot with adequate ^reaction^ ^time^ and ^collective^ ^pitch^. Activation of the ^CHOP^ ^button^ or reduction of the ^power^ ^levers^ prior to reduction of the ^collective^ will result in a ^rapid^ ^decay^ of rotor rpm. Successful completion of an ^OGE^ hovering autorotation is doubtful.";