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9. Throttles . . . . . . . . . . . As Required
l 2. Landlng gear and flaps . . . Leave a5 Set
for Takeoff
FIRE LIGHT AND/OR FIRE IN FLIGHT
V. Throttle (affected engine) . . . . . . . IDLE
l 2. AIR SOURCE pushbutton . . . . . . . OFF
l 3. OBOGS master switch . . . . . . BACKUP
If light goes off (and no other secondary indications):
‘4. MASTER TEST switch . . . FIRE DET TEST
If light remalns illuminated, FIRE DET test falls,
or other secondary Indications:
l 6. FUEL SHUT OFF handle
(affected engine) . . . . . . . . . . . . Pull
l 6. Throttle (affected englne) . . . . . . . OFF
-7 Climb and decelerate.
l 6. Flreextingulsher pushbutton . . . Depress
COMPRESSOR STALL
*I. Unload aircraft (OSg to 1.0 g).
If greater than 1.1 Mach:
-2. Both throttles . . . . . . . . . . . . . . MIL
When 1.1 Mach or less:
*3. Both throttles . . . . . . . Smoothly to IDLE
If EGT above 935 “C and/or englne response
abnormal:
l 4. Throttle (stalled engine) . . . . . . . . OFF
ENGINE FLAMEOUT
‘I. Throttle . . . . . . . . . . . IDLE of Above
(affected englne)
l 2. BACK UP IGNITION switch . . . . . . . ON
If hung start or no start:
‘3. Throttle . . . . . . . Cycle OFF, Then IDLE
(affected engine)
If still hung or,no start:
‘4. ENG MODE SELECT . . . . . . . . . . SEC
If one engine is operable, perform a crossbleed
airstart.
If both engines flamed out/inoperative or
crossbleed not possible:
‘5. Airspeed . . . . . . . . . . . . . 450 Knots
(altitude permitting)
RAMPS LIGHT/INLET UGHT
‘1. Avoid abrupt throttle movements.
‘2. Decelerate to below 1.2 TMN.
‘3. Affected INLET RAMPS switch . . . STOW
ELECTRICAL FIRE
*I. Land R generators . . . . . . . . . . OFF
If uncommanded SAS or spoiler Inputs present:
l 2. ROLL and PITCH CMPTR AC cb’s . . Pull
@Al, LBI)
l 3. YAWSASswltch . . . . . . . , . . . . OFF
ECS LEAKS/ELIMINATION OF SMOKE
AND FUMES
‘1. AIR SOURCE pushbutton . . . . . . . OFF
*2. OBOGS master switch . . . . . . . BACKUP
“3. If smoke or fumes present:
a. AltitudeBelow 35,000 Feet
b. CABIN PRESS switchDUMP
“4. RAM AIRswItch . . . . . . . . . . . OPEN
LAD/CANOPY LIGHT WITH RIO’S CANOPY
LIGHT/CANOPY LOSS
‘4. Canopy . . . . . . . . . . . BOOST CLOSE
(canopy remalnlng)
l 2. EJECT CMD lever . . . . . . . . . . PILOT
UNCOMMANDED ROLL AND/OR YAW
l l. If flap transltlon:
FLAP handle . . . . . . . Prevlous Posltlon
NAVAIR Of-Ff4AAD-1
‘2. Rudder and stick . . , . Op~oslte Roll/Yaw
3. AOA . . . . . . . . . . . . . Below 12 Unite
l 4. Downwlng englne . . . . . . MAX THRUST
w WUlM
UPRIGHT DEPARTURE/FLAT SPIN
l l. Stick. . . . . . . . . . . . Forward/Neutral
Lateral, Harness-Lock
‘2. Throttles . . . . . . . . . . . . . BothIDLE
l 3. Rudder . . . . Opposite Turn Needle/Yaw
If no recovery:
l 4. Stick . . . . . . . . . . . . Into Turn Needle
If yaw rate is steady/increasing, spin arrow
flashing, or eyeball-out g Is sensed:
*5. Roll SAS - On; Stick - Full Into Turn
Needle and Aft.
If recovery indicated:
‘6. Controls. . . . . . . . . . . . NEUTRALIZE
‘7. Recover at 17 units AOA, thrust as required.
If flat spin verified by flat attitude, increasing
Yaw rate, increasing eyeball-out g, and lack of
pitch and roll rates:
*5. Canopy . . . . . . . . . . . . . . . Jettison
“9. EJECT . . . . . . . . (RIO Command Eject)
INVERTED DEPARTURE/SPIN
l l. Stick . . . . . . . . . . . . . Full Aft/Neutral
Lateral, Harness - Lock
‘2. Throttles . . . . . . . . . . . . . Both IDLE
‘3. Rudder . . . . Opposite Turn Needle/Yaw
If recovery Indicated:
*4. Controls. . . . . . . . . . . . . . Neutralize
“5. Recover at 17 units AOA, thrust as requlred.
If spinning below 10,000 feet AGL:
‘6. EJECT . . . . . . . . (RIO Command Eject)
WARNING/CAUTION/ADVISORY LIGHTS/DISPLAY LEGENDS
(WPIRNING(
ADVISORY
LIGHT/LEGEND
I
l-
WARNING LIGHT AND/OR DISPLAY LEGEND
(HUD, HUDIMFD, MFD) DISPLAY LEGEND
AAI ZERO (MFD)
I
L AIICE
R AlICE
(MW
A/P REF (MFD)
m
WW
MD)
L AUG
R AUG
MD)
0 1RIGINAL
\
CAUSE
VIA tracking radar detected.
4CLS or autopilot disengagement.
4irbome interceptor tracking detected.
Designated engine anti-ice is on or anttce
valve has failed opposite
commanded position.
Selected A/P reference is not engaged.
　
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