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MK-58HUNTER1Jan2011
Fuel-4
Chg-0
FUELGAUGE
◆
Oneorbothgaugesindicateempty.
◆
Readingsfluctuateerratically.
NOTES1
O
●
Ifable,applynegativeGtoverifytheproperoperationoflow
fuellights.
●
Balancefuelwithreferencetolowfuellights.
FUELIMBALANCE
◆
Leftandrightfuelquantitiesdifferbymorethan100lbs.
O
WARNINGS
●
Followingahydraulicfailuretheaircraftmustnotlandwithany
asymmetricloadotherthananemptyinboardexternalfueltank
unlessalow-speedhandlingcheckhasbeenmade.
●
Investigatethelow-speedhandlingcharacteristicsatasafe
altitude.
Ifaproportionerfailureissuspected,landwhilebothfronttanks
O
●
containfuel.
NOTE2
●
Attempttoensuretheimbalanceisnotcausedbyafuelleak.
O
MK-58HUNTER1Jan2011
Fuel-5
Chg-O
FUELGAUGE
ACTIONS:
N1
1.Boostpumps-VERIFYBOTHON(L)
2.Fueltransferpressure-VERIFYINLINE(MI)
O
3.Fueltankchangeover-VERIFYWING(MI)
Elec/Hyd/FItControl
IFUNABLETOMONITORFUELBYOTHERMEANS:
RTB
FUELIMBALANCE
Engine/Fire
O
ACTIONS:
1.Boostpump(lowside)-CYCLEASREQUIRED(L)
W
IFUNSUCCESSFULANDFUELQUANTITYANDBALANCEPERMIT:
RTB
OTHERWISE:
N2
Fuel
LANDASAP
O
LandingGear
O
FUELGAUGE/FUELIMBALANCE
Miscellaneous
MK-58HUNTER1Jan2011
Fuel-6
Chg-O
FUELLEAK
Fuelgaugereadingsaredecreasingmorequicklythan
normal.
O
O
O
O
MK-58HUNTER1Jan2011
Fuel-7
Chg-0
FUELLEAK
ACTIONS:
IFBOTHSIDESAREDECREASINGFASTERTHANNORMAL:
O
1.Boostpumps-CONFIRMBOTHON(L)
Elec/Hyd/FItControl
LANDASAP
IFONLYONESIDEISDECREASINGFASTERTHANNORMAL:
2.Boostpump(affectedside)-OFF(L)
IFAFFECTEDSIDECONTINUESTODECREASE:
3.Boostpumps-BOTHON(L)
IFFUELQUANTITYANDBALANCEPERMIT:
RTB
Engine/Fire
O
OTHERWISE:
LANDASAP
IFRANGEISCRITICAL:
4.Boostpump(leakingside)-ON(L)
5.Boostpump(goodside)-OFF(L)
Fuel
.Afuelimbalancemightbedeveloping.
WHENAFFECTEDSIDEREDUCESTO300LBS:
O
6.Boostpump(goodside)-ON(L)
7.Boostpump(leakingside)-OFF(L)
.Fuelmaystillbeleaking.
.Fuellowpressurelightmayilluminate.
IFFUELQUANTITYPERMITS,FORAPPROACHANDLANDING:
LandingGear
8.Boostpump(anyside)-ON(L)
IFLOWFUELSTATEISCRITICALATANYTIME:
O
9.Boostpumps-BOTHON(L)
FUELLEAK
Miscellaneous
MK-58HUNTER1Jan2011
Fuel-8
Chg-O
FUELPRESSURELOW
Fuellowpressurewarningison.
WARNING1
O
Ifenginesurgesorreactsabnormally,LANDASAP.
NOTE
IfthewarningremainsdespitetheproperRPM,thesensorisfaulty
andengineoperationisnotaffected.
FUELTANKCHANGEOVER
O
◆
Changeoverindicatorshowsintransitorreartank
whenthereartankshouldbeempty,andthe
associatedfuelgaugereadslessthan1300lbsorfront
tankcontentsonly.
WARNINGS2
●
Relyonlyuponthefuelinthefronttankontheaffectedside
O
(maximum770lbs);anincreasingfuelimbalanceisdeveloping.
●
Minimizethefuelimbalancebyexpeditingrecoveryand
obtainingpriority.
●
Adelaycausingsignificantunusableexternalfuelmayrequireas
muchas190ktstomaintainaircraftcontrol,makinglanding
verydifficultifnotimpossible.
Steepdivesmustbeavoided.
O
MK-58HUNTER1Jan2011
Fuel-9
Chg-O
FUELPRESSURELOW
ACTIONS:
1.RPM-MAINTAIN6000-7200UNTILLANDING
W1
O
2.Throttlesettingsandmovements-MINIMIZE
Elec/Hyd/FItControl
3.Boostpumps-VERIFYBOTHON(L)
N
4.Gforces-MAINTAINMORETHANZEROG
REGARDLESSOFSUBSEQUENTLOWFUELPRESSURELIGHTSTATUS:
RTB
Engine/Fire
O
FUELTANKCHANGEOVER
ACTIONS:
1.Fueltankselector-CYCLETHENSETWING(MI)
W2
IFUNSUCCESSFUL:
Fuel
2.Boostpump(affectedside)-OFF(L)
Anincreasingfuelimbalanceisdeveloping.
O
IFFUELQUANTITYANDBALANCEPERMIT:
RTB
WHENAPPROPRIATE:
3.Frontfueltanks-BALANCE
IFFUELQUANTITYPERMITS,FORAPPROACHANDLANDING:
LandingGear
4.Boostpumps-BOTHON(L)
O
FUELPRESSURELOW/FUELTANKCHANGEOVER
Miscellaneous
MK-58HUNTER1Jan2011
Fuel-10
Chg-0
FUELTRANSFERPRESSURE
◆
Transferpressurecrosslineandfuelquantityshows
fronttankcontentsonlyontheassociatedside.
◆
Alowfuellightisonandfronttankquantityis
O
decreasingwhentransfershouldbeoccurring.
WARNINGS
●
Relyonlyuponthefuelinthefronttankontheaffectedside
(maximum770lbs);anincreasingfuelimbalanceisdeveloping.
●
Minimizethefuelimbalancebyexpeditingrecoveryand
obtainingpriority.
O
●
Adelaycausingsignificantunusableexternalfuelmayrequireas
muchas190ktstomaintainaircraftcontrol,makinglanding
verydifficultifnotimpossible.
●
Steepdivesmustbeavoided.
O
O
MK-58HUNTER1Jan2011
Fuel-11
Chg-0
FUELTRANSFERPRESSURE
ACTIONS:
1.Fueltankselector-CYCLETHENSETWING(MI)
W
O
IFUNSUCCESSFUL:
Elec/Hyd/FItControl
2.Boostpumps(oneorboth)-CONFIRMON(L)
WITHATLEASTONEBOOSTPUMPOPERATING
3.Gforces-APPLYPOSITIVEANDNEGATIVEG
IFUNSUCCESSFUL:
4.Boostpump(affectedside)-OFF(L)
.Anincreasingfuelimbalanceisdeveloping.
Engine/Fire
O
IFFUELQUANTITYANDBALANCEPERMIT:
RTB
OTHERWISE:
LANDASAP
WHENAPPROPRIATE:
5.Frontfueltanks-BALANCE
Fuel
IFFUELQUANTITYPERMITS,FORAPPROACHANDLANDING:
6.Boostpumps-BOTHON(L)
O
LandingGear
O
Miscellaneous
FUELTRANSFERPRESSURE
MK-58HUNTER1Jan2011
Fuel-12
Chg-O
FUELVAPORVALVE
◆
Vapourreleasevalvehasfailedclosed.
◆
Lowfuellightcomesonprematurelywhilefuelremains
AND/
inwing,rearorexternaltanksandallotherindications
OR
arenormal.
Normallyonlyfronttankfuelcontentsareindicatedon
thegauge.Affectedfronttankslowlyrefillswhenits
boostpumpisoff.
◆
Fuelmaybeobservedflowingoutthemainbellyfuel
vent.
WARNINGS
●
Thoughallfuelremainsavailable,cyclingtheboostpumponthe
affectedsidetoavoidanemptyfronttankwillcausean
increasingfuelimbalance.
●
Minimizethefuelimbalancebyexpeditingrecoveryand
obtainingpriority.
●
Adelaycausingsignificantunusableexternalfuelmayrequireas
O
muchas190ktstomaintainaircraftcontrol,makinglanding
verydifficultifnotimpossible.
Avoidexcessiveattitudesandlowinternalfuelquantity.
NOTE
Thisissuewillcauseareducedfueltransferratetothefronttankon
theaffectedside,preventingthefronttankfromremainingfullwhile
transfercontinues.
O
MK-58HUNTER1Jan2011
Fuel-13
Chg-0
FUELVAPORVALVE
ACTIONS:
1.Boostpumps-VERIFYBOTHON(L)
W
O
THEN,WITHATLEASTONEBOOSTPUMPOPERATING:
Elec/Hyd/FItControl
2.Gforces-APPLYPOSITIVEANDNEGATIVEG
N
IFFUELQUANTITYANDBALANCEPERMIT:
RTB
OTHERWISE:
LANDASAP
IFAFFECTEDFRONTTANKQUANTITYREDUCESTO300LBS:
O
3.Boostpump(affectedside)-OFF(L)
Engine/Fire
Anincreasingfuelimbalanceisdeveloping.
IFAFFECTEDFRONTTANKQUANTITYINCREASES:
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