Navair F-14B, Emergency Procedure Tabs

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VAIR 01−F14AAP−1B
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322
CARD 6 of 10 DFCS IN FLIGHT FAULT MATRIX CARDS OFP 4.4
ARI DGR
LIGHT(S) ACRO(S) CONFIG FAILURE CAUSE(S) FUNCTIONALITY DEGRADED DCP FLT CODE(S)
ARI DGR
PITCH SAS
FCS CAUTION PA, PC,
PS, RS PA or UA 1. PITCH B computer fault.
1,5
2. DLC trim servo isolation fault.
1,5
1. Pitch SAS half auth.
OB spoilers inop. DLC, Autopilot
inop. ARI DGR after
maneuvering (WRS, LSXC
inop). 1. PC##.
2. DLT2.
ARI DGR
FCS CAUTION PS PA or UA 1. SCADC Mach invalid fault.
1
2. SCADC valid to roll computer
fault.
1,2
3. Air data computer (CADC) fault.
1,2,3,4
4. L AICS computer fault.
6
5. R AICS computer fault.
6
1. ARI degrade (fixed Mach gains).
2. Autopilot, Mach trim inop. YAW
DGR after maneuvering (WRS,
LSXC inop).
3. ARI degrade (fixed Mach gains).
Autopilot, Mach trim inop. YAW
DGR after maneuvering (WRS,
LSXC inop).
4−5. Equivalent of AOA /Mach 1F.
1. AD01.
2. AD04.
3. AD01, 04.
4. AOAL, MACL, &
AICX.
5. AOAR, MACR,
& AICX.
PA 1. AOA 2F.
2. Mach 1F (< 600 kts).
3. Mach 2F. 1. PA−ARI degrade (fixed AOA
gains).
2−3. ARI degrade (fixed Mach
gains).
1. AOAC/AC28,
AOAT, &
AOAL/AOAR.
2−3. AD01, 03, 04,
05 & MACL/R.
UA 1. Mach 1F (< 600 kts). 1. ARI degrade (fixed Mach gains).
LSXC, WRS inop.
1. AD01, 03, 04,
05 & MACL/R.
YS PA or UA 1. Rudder pedal position 2F. 1. ARI degrade.
UA LSXC, WRS inop.
PA pedal fadeout for LSRI,
RRC inop (slipped approach). 1. RPP#.
1
May also illuminate AUTOPILOT and ACLS A/P caution lights.
2
Will also illuminate MACH TRIM caution light.
3
Will also illuminate HZ TAIL AUTH caution light.
4
Will also illuminate RUDDER AUTH caution light.
5
Will also illuminate SPOILERS caution light.
6
Will also illuminate L INLET and R INLET caution light respectively.