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CNO 041749Z SEP01 Page 3 of 6 NA 01-F14AAA-1 IC 148
NA 01-F14AAP-1 IC 46
NA 01-F14AAD-1 IC 26
NA 01-F14AAA-1B IC 104
NA 01-F14AAP-1B IC 30
NA 01-F14AAD-1B IC 15
D. UNCOMMANDED DIFFERENTIAL STABILIZER AND/OR
RUDDER AUTOMATIC FLIGHT CONTROL SYSTEM INPUTS
CAUSED BY ABNORMAL POWER TRANSIENTS.
E. HARDOVER RUDDER.
1. IF FLAP TRANSITION:
FLAP HANDLE -- PREVIOUS POSITION.
2. RUDDER AND STICK -- OPPOSITE ROLL/YAW.
NOTE
FOR SPOILER MALFUNCTION, USE LATERAL STICK AS
PRIMARY LATERAL CONTROL AND RUDDER ONLY AS NEEDED
TO MAINTAIN BALANCED FLIGHT.
3. AOA -- BELOW 12 UNITS.
4. DOWNWING ENGINE -- MAX THRUST (IF REQUIRED).
5. MASTER RESET PUSHBUTTON -- DEPRESS.
NOTE
DFCS SYNCHRONIZATION CAN TAKE UP TO 2 SECONDS
FOLLOWING A POWER INTERRUPT. IF THE MASTER
RESET PUSHBUTTON IS DEPRESSED DURING THE
SYNCHRONIZATION TIME, AN ADDITIONAL DEPRESSION OF
THE MASTER RESET PUSHBUTTON WILL BE REQUIRED TO
RESTORE SPOILER FUNCTIONALITY.
6. ROLL SAS -- ON.
7. ROLL TRIM -- OPPOSITE STICK (IF REQUIRED).
8. OUT OF CONTROL BELOW 10,000 FEET AGL -- EJECT.
9. CONTROL REGAINED -- CLIMB AND INVESTIGATE FOR THE
FOLLOWING:
A. FLAP AND SLAT ASYMMETRY.
B. SAS MALFUNCTION.
NOTE
SAS FAILURE MAY CAUSE UNCOMMANDED ROLL AND/OR
YAW, EVEN WITHOUT ILLUMINATION OF THE ASSOCIATED
LIGHTS.
C. SPOILER MALFUNCTION.
D. HARDOVER RUDDER.
E. STRUCTURAL DAMAGE.
10. SLOW-FLY AIRCRAFT TO DETERMINE CONTROLLABILITY AT
10,000 FEET AGL MINIMUM.
D. SPOILERS CAUTION LIGHT/SPOILER MALFUNCTION/SPOILER STUCK UP:
(1) DELETE:
REF A (F-14A NFM), DFCS SUPPLEMENT, PAGE 14-15X
AND 14-16X, PARAGRAPH 14.12.11.3 (SPOILERS CAUTION LIGHT/
SPOILER MALFUNCTION/SPOILER STUCK UP),
REF B (F-14B NFM), DFCS SUPPLEMENT, PAGES 14-15X AND 14-16X,
PARAGRAPH 14.12.9.3 (SPOILERS CAUTION LIGHT/SPOILER
MALFUNCTION/SPOILER STUCK UP), AND/OR
REF C (F-14D NFM), DFCS SUPPLEMENT, PAGES 14-17X AND 14-18X,
PARAGRAPH 14.12.7.3 (SPOILERS CAUTION LIGHT/SPOILER
MALFUNCTION/SPOILER STUCK UP):
(2) ADD (REPLACE WITH) AS PARAGRAPH 14.12.11.3 IN F-14A NFM,
AS PARAGRAPH 14.12.9.3 IN F-14B NFM, AND/OR
AS PARAGRAPH 14.12.7.3 IN F-14D NFM):
14.12.11.3 SPOILERS CAUTION LIGHT/SPOILER MALFUNCTION/
SPOILER STUCK UP.
_______________________________________________________________________
CNO 041749Z SEP01 Page 4 of 6 NA 01-F14AAA-1 IC 148
NA 01-F14AAP-1 IC 46
NA 01-F14AAD-1 IC 26
NA 01-F14AAA-1B IC 104
NA 01-F14AAP-1B IC 30
NA 01-F14AAD-1B IC 15
CAUTION
IF THE CURRENT CONFIGURATION IS ACCEPTABLE FOR
LANDING, CAREFUL CONSIDERATION SHOULD BE
GIVEN BEFORE DEPRESSING MASTER RESET WHEN A
SPOILER ACTUATOR MECHANICAL MALFUNCTION IS
SUSPECTED. A DEPLOYED SPOILER THAT RESULTED FROM
DFCS COMPUTERS DROPPING OFF LINE IS NOT
CONSIDERED A MECHANICAL FAILURE.
NOTE
USE LATERAL STICK AS PRIMARY CONTROL AND RUDDER
ONLY AS NEEDED TO MAINTAIN BALANCED FLIGHT.
NOTE
SUBSEQUENT DEPRESSION OF THE MASTER RESET
PUSHBUTTON MAY CLEAR FAILURE UNTIL SPOILER IS
COMMANDED TO MOVE AGAIN.
1. MASTER RESET PUSHBUTTON -- DEPRESS.
NOTE
DFCS SYNCHRONIZATION CAN TAKE UP TO 2 SECONDS
FOLLOWING A POWER INTERRUPT. IF THE MASTER
RESET PUSHBUTTON IS DEPRESSED DURING THE
SYNCHRONIZATION TIME, AN ADDITIONAL DEPRESSION OF
THE MASTER RESET PUSHBUTTON WILL BE REQUIRED TO
RESTORE SPOILER FUNCTIONALITY.
IF FAILURE REMAINS/REOCCURS:
2. AVOID ABRUPT LATERAL CONTROL MOVEMENTS AND HIGH ROLL
RATES.
CAUTION
WITH WINGS FORWARD OF 62 DEGREES, EXCESSIVE
HORIZONTAL TAIL DIFFERENTIAL MAY CAUSE SEVERE
STRUCTURAL DAMAGE.
IF SPOILER(S) FAIL DOWN:
3. PERFORM CONTROLLABILITY CHECK PROCEDURE, PARAGRAPH
14.11.7.
IF SPOILER(S) REMAIN UP OR FLOATING, OR IF CONTROL
UNSATISFACTORY WITH FLAPS DOWN:
NOTE
ANY SINGLE, FULLY-DEFLECTED, FAILED-UP SPOILER IS
CONTROLLABLE EVEN WITH FLAPS DOWN IF THE
REMAINING SPOILERS ARE OPERATING. WITH MULTIPLE
FAILURES, AIRCRAFT CONFIGURATION IS THE CRITICAL
FACTOR. WITH FLAPS DOWN, ROLL CONTROL USING
LATERAL STICK ALONE MAY BE IMPOSSIBLE. HOWEVER,
WITH FLAPS UP, ADEQUATE ROLL CONTROL TO REGAIN
WINGS LEVEL FLIGHT IS AVAILABLE WITH USE OF
LATERAL STICK ALONE. CHOICE OF FLAP POSITION FOR
LANDING AND CV RECOVERY/DIVERT DECISION SHOULD BE
MADE FOLLOWING A CONTROLLABILITY CHECK.
4. PERFORM CONTROLLABILITY CHECK PROCEDURE, PARAGRAPH
14.11.7, USING MANEUVERING FLAP/SLAT (PREFERRED) OR
NO-FLAP CONFIGURATION ONLY.
NOTE
IF CONTROLLABILITY IS UNSUITABLE FOR LANDING
　
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