曝光台 注意防骗
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tail authority. Once asymmetry OCCUTS,
do not trim out stick forces. If lateral control
is marginal, trim opposite to the natural direction
until 111 spoiler deflection is avaiiable.
For example, stick to the right, trim let?.
If a roll is encountered during flap and slat transition
or if RIO notes asymmetric slat extension or
retraction:
Note
Uncommanded roll/yaw procedures take
precedence if appropriate. Otherwise perform
the procedures below.
1. FLAP/SLAT CONTR SHUT-OFF cb - Check In
wx I,,,,,,,(
Lack of asymmetry protection (RA2 circuit
breaker out) may cause uncommanded roil
and/or yaw during flap or landing gear handle
movement.
2. FLAPS -Match Handle With Flaps Position.
3. Obtain visual check if possible to ascertain position
of ail flap and slat surfaces.
I
4. Slow-fly aircrafi in approach configuration at or
above 10,000 feet AGL to determine approach
characteristics, conditions permitting.
5. Land as soon as practicable if aircraft is controllable
and minimum approach airspeed is within
shipboard arresting gear limits.
Ifasyrnmeny is so large as to make landing impossible or
minimum safe approachs peedi s aboves hipboarda rresting
gear limits with no possible divert field available:
6. Cliib above 10,000 feet AGL.
7. AUX FLAP/FLAP CONTR cb -Pull (8G3).
(,,,,,,,I
Failure to complete step 6 before the subsequent
steps can result in large uncommanded
pitch trim changes because of
auxiliary flap movement.
8. FLAP/SLAT CONTR SHU’T-OFP cb-Pull @X2).
9. Slowly move FLAP handle in dim&ion to minhnii
asymmetry and/or lateral control requirements.
10. Stop flap and slat travel before reaching full up or
down.
11. FLAP/SLAT CONTR SHUT-OFF cb - Reset
wb (,,,,,,,I
Asymmetric slats may not be apparent until
just before wing stall. Asymmetric slats can
cause rapid rolloff above 15 units AOA.
12. If asymmetry has been corrected, land using 15
units AOA.
13. If asymmetry has not been corrected, flaps and
slats did not respond to above procedure, or lateral
control problems exist, land using maximum safe
AOA if landing is elected.
14.12.10 WiNG SWEEP Advisory Light and
W/S Caution Legend
14.12.10.1 Advisory Light Only - No Loss of
Normal Control
1. MASTER RESET pushbutton-Depress.
14.12.102 WING SWEEP Light and W/S
Caution Legend - No Automatic
or Manual Control
1. Airspeed - Decelerate to 0.9 Mach or Less.
2. Check spider detent engaged.
3. MASTERRESETpushbutton-Depress(wait 15
seconds to determine system status).
If WING SWEEP light and W/S caution legend illuminate
again:
4. WING SWEEP DRIVE NO. 1 and WG SWP DR
NO. 2/ MANUV FLAP cb -Pull (LDl, LEl).
5. Emergency WING SWEEP handle - Comply
with below schedule:
a. < 0.4 Mach - 20°.
b. < 0.7 Mach - 25”.
c. < 0.8 Mach -50”.
d. < 0.9 Mach - 60”.
e. > 0.9 Mach - 6S”.
Avoid ACM and aerobatics.
14.12.11 Unscheduled Wing Sweep
1. Emergency WING SWEEP handle - Raise and
Hold.
Unscheduled wing sweep at supersonic
speed may cause structural damage.
2. Airspeed - Decelerate to 0.6 TMN or Less in Ig
Nonmaneuvering Flight.
3. Emergency WING SWEEP handle - Full
Forward.
If wings do not move till forward:
4. EMERGENCY WING SWEEP handle-Match
With Actual Wing Position.
5. WING SWEEP DRIVE NO. 1 and WG SWP DR
NO. 2MANUV FLAP cb - Pull (LDl, LEl)
(refer to aft wing-sweep landing).
NAVAIR Of-F14AAD-1
6. Land as soon as practicable.
Note
l After a wing-sweep malfunction, the
WING SWEEP advisory light and the
W/S legend may take I5 seconds to
illuminate/display.
l FLAP light will be illuminated with cb
LEl pulled.
14.12.12 CADC Light
1. MASTER RESET pushbutton - Depress.
2. CADC cb’s (LA2, LB2, LC2, LD2) -Cycle.
3. MASTER RESET pushbutton - Depress.
If light still remains illuminated:
4. Remain below 1.5 Mach.
One or mom of the following systems may be affected
by CADC malfunction that illuminates only the CADC
light.
a. Maxiium safe Mach
b. Autopilot
c. Idle lockup function of AFTC
d. Wing-sweep indicator
e. Cockpit cooling less than Mach 0.25
f. HUD Display.
Note
l Erroneous Mach inputs to the AFTC may
cause uncommanded acceleration of both
engines to near-military values in the PRI
engine mode.
a If illumination of the CADC light is accompanied
by other caution or advisory
light(s), refer to the appropriate procedure
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F-14D 飞行手册 Flight Manual 2(123)
