All of the below info is from the article:
Following 25 ACARS Messages were received from the airplane:
2:10:10 - .1/WRN/WN0906010210 221002006 AUTO FLT AP OFF
2:10:16 - .1/WRN/WN0906010210 226201006 AUTO FLT REAC W/S DET FAULT
2:10:23 - .1/WRN/WN0906010210 279100506 F/CTL ALTN LAW
2:10:29 - .1/WRN/WN0906010210 228300206 FLAG ON CAPT PFD SPD LIMIT
2:10:34 #0210/+2.98-30.59
2:10:41 - .1/WRN/WN0906010210 228301206 FLAG ON F/O PFD SPD LIMIT
2:10:47 - .1/WRN/WN0906010210 223002506 AUTO FLT A/THR OFF
2:10:54 - .1/WRN/WN0906010210 344300506 NAV TCAS FAULT
2:11:00 - .1/WRN/WN0906010210 228300106 FLAG ON CAPT PFD FD
2:11:15 - .1/WRN/WN0906010210 228301106 FLAG ON F/O PFD FD
2:11:21 - .1/WRN/WN0906010210 272302006 F/CTL RUD TRV LIM FAULT
2:11:27 - .1/WRN/WN0906010210 279045506 MAINTENANCE STATUS EFCS 2
2:11:42 - .1/WRN/WN0906010210 279045006 MAINTENANCE STATUS EFCS 1
2:11:49 - .1/FLR/FR0906010210 34111506 EFCS2 1,EFCS1,AFS,,,,,PROBE-PITOT 1X2 / 2X3 / 1X3 (9DA),HARD
2:11:55 - .1/FLR/FR0906010210 27933406 EFCS1 X2,EFCS2X,,,,,,FCPC2 (2CE2) /WRG:ADIRU1 BUS ADR1-2 TO FCPC2,HARD
2:12:10 - .1/WRN/WN0906010211 341200106 FLAG ON CAPT PFD FPV
2:12:16 - .1/WRN/WN0906010211 341201106 FLAG ON F/O PFD FPV
2:12:51 - .1/WRN/WN0906010212 341040006 NAV ADR DISAGREE
2:13:8 - .1/FLR/FR0906010211 34220006 ISIS 1,,,,,,,ISIS(22FN-10FC) SPEED OR MACH FUNCTION,HARD
2:13:14 - .1/FLR/FR0906010211 34123406 IR2 1,EFCS1X,IR1,IR3,,,,ADIRU2 (1FP2),HARD
2:13:45 - .1/WRN/WN0906010213 279002506 F/CTL PRIM 1 FAULT
2:13:51 - .1/WRN/WN0906010213 279004006 F/CTL SEC 1 FAULT
2:14:14 - .1/WRN/WN0906010214 341036006 MAINTENANCE STATUS ADR 2
2:14:20 - .1/FLR/FR0906010213 22833406 AFS 1,,,,,,,FMGEC1(1CA1),INTERMITTENT
2:14:26 - .1/WRN/WN0906010214 213100206 ADVISORY CABIN VERTICAL SPEED
The cockpit effect messages mean:
- AUTO FLT AP OFF: The autopilot disconnected without crew intervention
- AUTO FLT REAC W/S DET FAULT: windshear detection is unavailable
- F/CTL ALTN LAW: FBW switched into alternate law (protections lost)
- FLAG ON CAPT PFD SPD LIM and FLAG ON F/O PFD SPD LIM: characteristic speeds (green dot, VLS, ...) lost due to loss of calculating function
- AUTO FLT A/THR OFF: Autothrottle disconnected other than by crew intervention or throttle levers were moved into the idle notch
- NAV TCAS FAULT: TCAS is inoperative, the message has not yet been explained
- FLAG ON CAPT PFD FD and FLAG ON F/O PFD FD: flight director bars have been removed from primary flight displays
- F/CTL RUD TRV LIM FAULT: The rudder limiter value computation is unavailable, the rudder remains limited to the present values until slat extension
- MAINTENANCE STATUS EFCS2 and MAINTENANCE STATUS EFCS1: not brought to the crew attention
- FLAG ON CAPT PFD FPV and FLAG ON F/O PFD FPV: flight path vector displays removed from the primary flight displays, red flags shown instead
- NAV ADR DISAGREE: Computers have rejected one ADR and then detected a disagreement between the remaining ADRs on one of the monitored paramenters.
- F/CTL PRIM 1 FAULT: Primary Flight Controls Computer 1 has stopped functioning either as result of a command or failure
- F/CTL SEC 1 FAULT: Secondary Flight Controls Computer 1 has stopped functioning either as result of a command or failure.
- MAINTENANCE STATUS ADR2: not brought to crew attention
- ADVISORY CABIN VERTICAL SPEED: cabin pressure changes at a rate of 1800 feet/minute or greater for 5 seconds.
Term Explanation
Normal Law: Regular operating mode of the fly by wire (FBW) including all protections.
Alternate Law: Some of the protections in normal law, the regular operating mode, are dropped.
Direct Law: The controls (sidestick) inputs are converted into direct movements of control surfaces without computations or checks.
ADIRU: Air Data and Inertial Reference Unit provides air data (airspeed, altimeter, ...) and positional data (attitude, position) to the instruments
ISIS: Integrated Standby Instrument System is a completely independent, self contained system providing a third independent set of basic instruments (attitude indicator, altimeter, airspeed indicator) to the crew
PRIM 1: Flight Control primary computer #1, three of them monitor each other, one of them controls the control surfaces as master
SEC 1: Flight Control secondary computer #1, each of the two can control all airplane control surfaces in direct law and can become master in case of failure of all primary flight control computers.
02:10Z: Autothrust off
Autopilot off
FBW alternate law
Rudder Travel Limiter Fault
TCAS fault due to antenna fault
Flight Envelope Computation warning
All pitot static ports lost
02:11Z: Failure of all three ADIRUs
Failure of gyros of ISIS (attitude information lost)
02:12Z: ADIRUs Air Data disagree
02:13Z: Flight Management, Guidance and Envelope Computer fault
PRIM 1 fault
SEC 1 fault
02:14Z: Cabin Pressure Controller fault (cabin vertical speed)