Growler NATOPS

350K

• 500K
• 480K

• <250K
• <10,000'

• 10-45% during start
• flameout
• when throttle is in AB until AB is lit
• trigger squeeze +5 sec for any A/G or A/A weapon

• fuel boost/motive flow pump
• generator
• hyd pump

• increase speed until inlet tems are >5*C
• maintain AOA >6*
• lower gear as late as possible

• internal wing tanks>tank 4
• externals feed to tank 1>tank 2> left eng
• externals feed to tank 4>tank 3> right eng

• motive flow transfers engine feed (tanks 2/3) and wing tank fuel
• electric pumps for fuselage transfer (tanks 1/4) and dump
• engine bleed air transfers external tanks. External transfer stops with IFR probe extended or hook/gear handle down.

SDC keeps tanks 2/3 within 100# of each other once tank 4 is empty

• 1300#/min
• stops when:
•     -switch is off
•     -bingo reached
•     -tanks 1 and 4 are empty
•     -FUEL LOW caution comes on

<1125# in either feed tank

when wing tank asymmetry >350# 

• UA only
• on at 40*/sec
• solid at 60*/sec

• PA only
• on at 14*
• solid by 35*

• tank 1     1430#
• tank 2     2660#
• tank 3     2680#
• tank 4     3860#
• (total fuselage 10,630#)
• wings     1670#/1670#
• (total internal 13,970#)
• CL          3220#

• 3000psi   <380k
• 5000psi   >380k (500k if SE)
• utilities are always at 3000psi

• -lose circuit A if <50% remaining
• -regain A and lose B if <30% remaining
• -regain both if <15% remaining

if <900psi (+/- 100psi) on primary system, switching valve mechanically changes to secondary hydraulic power (switches back if primary system is >2000psi)

• gear handle up, gear up and locked
• launch bar
• antiskid
• wheel brakes
• NWS
• nose gear

• open with WonW, closed inflight
• aft isolation manually opened with hook retract or HYD ISOL switch in Oride
• arming valve manually opened by emer gear or emer probe extension
• hook retract
• parking brake
• emergency brake

• maintained by trickle charge from HYD 2A
• if HYD 2 fail will provide pressure for:
• emer landing gear
• emer probe extension
• emer NWS
• emer brakes

• full at 3000psi
• maintained by trickle charge from HYD 2A
• emergency brakes use HYD 2B and APU acuumulator
• will get BRK ACCUM light if pressure <2000psi (5 applications left)
• provides parking brake with engines off
• provides emer brakes with HYD 2 failure

• <7500'
• <175k
• >250fpm rate of descent
• gear not down and locked

• inop <14k
• inop with emergency brakes
• when gear lowered, system turned on inflight, or on deck with the parking brake set, system starts 4.5 sec bit after 9 sec (do not cycle anti-skid <30 sec prior to landing)

• gravity lowered
• need HYD 2B to retract

circuit pressure <1400psi

unable to provide 5000psi when commanded

Hyd 1B/2A/2B

• landing gear extend/retract
• antiskid
• wheelbrakes
• NWS
• normal probe extend
• launch bar

• on at 60%, off at 52%
• if either generator fails the bus tie will close, connecting the two buses

• ac buses are isolated
• parking brake NOT pulled prior to first engine start

• single TR-no indication
• dual TR will lose:
• -HUD
• -bleed air (pressure and OBOGS)

• provides 5-10 min of power to FCC
• auto shutoff after 2 min if APU is not online
• with 1 gen online, gauge should be >28v

• battery on without external AC power (before engine start)
• battery switch off inflight

• ladder
• canopy
• APU start
• gen tie logic
• SMP and maint code checks
• airborne: FCC and INS keep alive logic

• lose all displays
• lose cabin pressure
• caution lights inop
• RPM and EGT only on EFD
• comm 1 only
• must use standby instruments
• must use emer gear (no anti-skid)

• battery switch must be on to power FCCs
• if battery gauge = 28v, PMGs are powering FCCs
• if battery gauge = 24v, battery is powering FCCs (land ASAP)

resets generator, PMG or electrical relay

• L side: FCC 1 and 2, launch bar
• R side: FCC 3 and 4, hook, landing gear

• must be set to run anti-skid bit, gen tie logic, or INS alignment
• will get PARK BRAKE light if set with RPM>80%

• HYD 2A
• Nose gear will not retract if:
• -nose WonW switch failure
• -launch bar failed to retract

• acutuated by APU accum pressure
• <170k

• primary HYD 2A
• backup with HYD 2B and APU accum (NWS cue flashes if using APU accum pressure)
• auto disengage with:
• -WoffW
• -launch bar down
• -power off FCCs
• automatically engages on touchdown with WonW

• if accumulatore pressure is <2450psi
• inflight after
• -APU start
• -after emer gear extension
• -after emergency probe extension

• on at 50%, off at 20%
• one on each AMAD
• NOT controlled by generator switch

• generator is not producing AC power
• single GEN light with AMAD PR caution could indicate major mechanical damage

• valve located off of each engine, prior to Y junction
• will close if air or electricity is lost
• can be closed by BALD

• downstream of Y junction
• electrically controlled by the OFF and AUG PULL position of the bleed air knob
• will fail to the open position
• can be closed by BALD

• secures all 3 bleed air pressure and regulator shut-off valves
• will lose:
• -OBOGS
• -cabin pressure
• -external fuel transfer
• -crossbleed start
• -g-suit
• -windshield anti-ice and rain removal
• Bleed air valves will close during fire test. Must rotate BA knob OFF then NORM to reset valves and cautions.

• augments ECS air for avionics cooling
• will override APU shutdown
• must have:
• -WonW
• -APU on
• -bleed air knob in any position besides OFF

• AUTO (normal)
• -WonW and throttles idle - aft avionics cooling fan is primary source of avionics cooling, ECS is secondary
• -WonW, either throttle >74% or inflight - ECS provides all avionics cooling
• MAN (prohibited)
• OFF/RAM
• -stops normal flow
• -ram air for scoop for cockpit airflow
• -emergency avionics cooling fan for avionics cooling

• HIGH-airflow to windshield
• NORM-airflow to cockpit louvers and windshield
• LOW-airflow to cockpit louvers and foot heater

• 0-8k: ambient
• 8k-24.5k: 8,000'
• >24.5k: .4 x a/c altitude

• NORM: on schedule
• DUMP: dumps cabin pressure, normal ECS flow to cockpit and avionics
• RAM/DUMP: dumps cabin pressure, stops ECS airflow

• ram air scoop for emergency cooling of FCC A, one AHRS, right T/R
• maintain >325k

• shuts down ECS flow if leak detected
• if leak detected downstream of Y junction will get both L BLD/R BLD
• can close pri/sec pressure regulator valves

• concentration falls
• hose disconnected
• mask removed without securing Oxy flow

• Up-Auto (UA)
• -Flaps-AUTO
• ->240k
• Powered Approach (PA)
• -Flaps-HALF or FULL
• -<240k

• 120KCAS (+/- 10KCAS)
• yaw rate threshold exceeded
• -15-20*/sec for 15 sec or 50-60*/sec for 2s