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flight.
1. Perform checks at a safe altitude in flaps-up
con@guration.
2. Affected SPOILER FLR ORIDE switch -
NORM (guard down).
3. Counter roll with at lease 1 inch of lateral stick.
Note
Stick deflection of over 1 inch enables
spoiler asymmetry logic and electrically fails
all affected spoilers down. Spoilers light will
illuminate.
4. If spoiler(s) fail down, failed SPOILER CONTF
cb -Pull (8G9 INBD, 9C5 OUTF3D) (go to stel
13).
5. If spoiler(s) remain up or floating, affecter
SPOILER FLR ORIDE switch - ORIDE.
6. MASTER RESET - Depress.
7. Failed SPOILER CONTR cb -Pull (8G9 INBD
9C5 OUTBD).
8. If spoiler(s) fail down, go to step 13.
Note
a Outboard spoiler position indicators will
indicate down with cb 8C5 pulled.
a With circuitbreakers 8G9 and 9C5 pulled,
ground-roll braking is inhibited.
Note
Allow up to 60 secondsf or spoilers to return
to trail.
9. If spoiler(s) remain up, malfunction was mechanical.
Failed SPOILER CONTR cb - Reset (8G9
INBD, 9C5 OUTBD).
10. Slow-fly aircraft in the flaps-up configuration to
determine minimum control speed.
11. Verify full remaining spoiler authority is available
by trimming laterally opposite of stick deflection.
12. Fly straight-in, flaps-up approacha bove minimum
control speed.
;f spoiler(s) fail down:
13. Slow-fly aircraft at a safe altitude in Saps-down
configuration to determine minimum control
speed.
14. If controllability is satisfactory, perform full-flap,
straight-in landing. If controllability characteristics
are not satisfactory, perform a no-flap or
maneuvering-flaps traight-in landing.
14.12.6 FLAP Light
14.12.6.1 Not After Landing/Takeoff Flap
Transition
1. Airspeed - Below 225 Knots.
2. FLAP handle -Ensure Full Up.
3. MASTER RESET pushbutton -Depress.
4. While holding MASTER RESET pushbutton
depressed, maneuver flap thumbwheel - Full
Forward.
5. Check FLAP light out (light can take up to 10
seconds to reilluminate).
14.12.9.2 After Landing/Takeoff Flap
Transition, or Reillumination
After Above Procedures
1. MASTER RESET pushbutton -Depress.
2. If light still illuminated, check FLAP handle and
indicator position, then proceed with appropriate
steps below.
NAVAIR 01-Fl4AAD-1
14.12.6.3 FLAP Handle Up and Flaps Not Fully
Retracted
1. FLAP handle - EMER UP.
If FLAP handle or flaps will not respond or FLAP
light remains illuminated, refer to Flap and Slat
Asymmetry procedures,p aragmph 14.12.9.
14.12.6.4 FLAP Handle Up and Flaps
Indicating Full Up
1. Flaps - Cycle.
If FLAP handle or flaps will not respond or FLAP
light remains illuminated, refer to Flap and Slat
Asymmetry procedures,p aragraph1 4.12.9.
14.12.6.5 FLAP Handle Down and Flaps Not
Fully Extended
1. Wing sweep - Ensure at 20”.
Flaps will not respond or FLAP light remains illuminated,
refer to Flap and Slat Asymmetry pro !-
dures, paragraph 14.12.9.
14.12.6.6 FLAP Handle Down and Flaps Down
1. Wing sweep -Ensure at 20”.
2. MASTER RESET pushbutton-Depress (allow
10 seconds for auxiliary flaps to extend).
Note
If FLAP handle or flaps will not respond or
FLAP light remains illuminated, refer to Flap
and Slat Asymmetry procedures, paragraph
14.12.9.
14.12.9 Flap and Slat Asymmetry. Flap and slat
asymmetry can occur with failure of an asymmetry sensor
and subsequent failure of the flap and slat drive
mechanism foronewing. The pilot’s only indicationwill
be an uncommanded roll followed by a FLAP light approximately
10s econdsla ter.T he flap indicatord oesn ot
indicate actual flap position, but the position to which
the flap and slat control box has been driven. The slat
indicator shows up, down, or transition (barber pole) for
the starboards lat only. The port slatp osition is not monitored.
Asymmetric flaps cause animmcdiate roll. Asymmetric
slats may not be apparent until just before wing
stall. Asymmetric slats can cause rapid rolloff above 15
units AOA. Slat position muat be monitored by the RIO
during transition.
NAVAIR gl-i=l4AAD-1
The we of lateral trim to reduce stick force
will reduce spoiler control significantly. An
uncontrollable situation can develop if lateral
trim is out of neutral before flap and slat
asymmetry or ifthe pilot trims laterally in the
neutral direction (opposite the roll) during
flap and slat transition. This situation will be
aggravateda nd recovery may not bep ossible
with roll SAS off because of reduced differential
　
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