N286VA

Part: FAULT MESSAGE — FALSE ACTIVATION (FIRE LOOP B) · airframe 13,920 hrs · 4,611 cycles

ENG 2 FIRELOOP B FAULT GROUNDED - YES. PERFORMED BITE TEST OF FDU 2 PER AMM 26-12-00 PB501. TEST OKAY AND NO FAULT NOTED. THIS CLEARS MDDR 74409 PLACARD REMOVED. MEL LIST UPDATED. SEAMC WILL NOTIFIED.

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 13,907 hrs · 4,604 cycles

ENGINE 2 FIRE LOOP B FAULT. GROUNDED - YES. TROUBLESHOT PER TSM TASK 26-12-00-810-806-A, PERFORMED INDIVIDUAL #2 ENG B LOOPS RESISTANCE CHECKS, ALL CHECKED GOOD. ALSO PERFORMED RESISTANCE CHECK AT #2 FDU CONNECTOR 2WD2 BETWEEN PINS J & K, RESISTANCE CHECKED GOOD. FOUND CONNECTOR 2WD2-B AT #2 FDU NOT INSTALLED/LOCKED PROPERLY, RE-INSTALLED CONNECTOR. SYSTEM OPS CHECKS GOOD PER AMM 26-12-00 PG501. RELEASED FROM MEL 26-12-01-02. MEL LOG UPDATED. MCC CORY NOTIFED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 BLEED AIR) · airframe 13,870 hrs · 4,590 cycles

ENG 1 BLEED FAULT IMMEDIATELY AFTER TAKEOFF RESET SUCCESSFULL. *THIS HAPPENED ALSO ON 12/13. GROUNDED - YES. PERFORMED BMC1 BITE TEST IAW AMM 36-11-00-74-001-A. TEST OK,COULD NOT DUPLICATE AT THIS TIME.

Part: WARNING MESSAGE — FALSE INDICATION (NR 1 ENG BLEED) · airframe 13,843 hrs · 4,578 cycles

ON CLIMB OUT AIR ENG1 BLEED FAULT. PERFORMED RESET PER QRH AND FAULT CLEARED. GROUNDED - YES. PERFORMED BITE TEST OF BMC1 IAW TSM 36-11-00-810-809A. OPS CHK GOOD.

Part: LIGHT — NO INDICATION (APU) · airframe 13,404 hrs · 4,410 cycles

*APU INOP GPU & AIRSTARD REQD*DURING PREFLIGHT IN PDX FOUND NO RED APU FIRE DISC. GROUNDED - YES. DISC IS STILL INPLACE, BUT DISC IS CLEAR NOT RED. REL IAW MEL 26-22-05-02 (APU INOP/RED DISC).

Part: FIRE LOOP — FAULTED (APU) · airframe 12,830 hrs · 4,161 cycles

APU FIRE LOOP B FAULT. GROUNDED - YES. VERIFIED APU FIRE LOOP B FAULT. RESET APU FIRE LOOP B PER AMM 26-22-00-710-001-A. NO FAULT. TEST OK

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,220 hrs · 3,952 cycles

ENGINE 2 IGNITION B FAULT GROUNDED - YES. PERFORMED FADEC IGN TEST PER AMM 73-29-00. OPS CHECK GOOD. NO FAULT MESSAGE.

Part: SENSOR — FAILED (AC BAY) · airframe 12,167 hrs · 3,928 cycles

PACK 2 REGULATOR FAULT IN CRUISE. GROUNDED - YES. R+R SERNSOR/COMPRESSOR TEMP(32HH) IAW AMM 21-61-11 PB 401 OPS CHECK GOOD THIS CLEARS MDDR 68266 AND MEL 21-52-01-07 PLACARD REMOVED A/C RETURNED TO ORIGINAL CONFIG. MEL LIST UPDATED

Part: FCU — MALFUNCTIONED (COCKPIT) · airframe 11,544 hrs · 3,711 cycles

FCU 1 INOP GROUNDED - YES. PERFORMED FCU 1 RESET, FAULT COULD NOT DUPLICATED. AFS TEST ACCOMPLISHED PER AMM 22-96-00-710-001-A, TEST OK.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 11,528 hrs · 3,707 cycles

AIR PACK 1 REGULATOR FAULT GROUNDED - YES. PERFORMED OPERATIONAL CHK OF THE TEMP CTL PER AMM 21-61-00-710-001-A OPS CHK GOOD NO FAULTS FOUND.

Part: ACTUATOR — FAILED (APU INLET) · airframe 11,473 hrs · 3,684 cycles

APU AUTOSHUT DOWN AFTER LANDING 3 ATTEMPTS GROUNDED - YES. REMOVED AND REPLACED THE AIR INTAKE FLAP ACTUATOR IAW AMM 49-16-51-000-003-A OPS CHECK GOOD. THIS CLEARS MDDR 66012 PLACARD REMOVED MEL LIST UPDATED MCC NOTIFIED.

Part: WARNING MESSAGE — ILLUMINATED (FUEL SYSTEM) · airframe 11,236 hrs · 3,619 cycles

CLASS 2 MAINTENANCE FUEL MESSAGE GROUNDED - YES. DEFERRED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 11,074 hrs · 3,566 cycles

IN CRUISE FLT GOT MULTIPLE THRUST LOCK ECAMS IN QUICK SUCCESSION. AFTER A/THR OFF THEN ON, STATUS NORMAL. GROUNDED - YES. PERFORMED AFS TEST. REF AMM 202-96-00-710-001A, AND OPERATIONAL TEST OF THE LAND CAT III CAPABILITY, REF AMM 22-97-00-710-001A. TEST OK.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 10,710 hrs · 3,419 cycles

WEATHER RADAR IS NOT WORKING GROUNDED - YES. R&R WEATHER RADAR TRANSCEIVER IAW AMM 34-41-33 PB401. OPS CK GOOD. OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,468 hrs · 3,325 cycles

APU BLEED STATUS MSG ON ECAM GROUNDED - YES. RESET ECB C/BS MSG CLEARED REF TSM 36-12-00-810-801.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 10,297 hrs · 3,262 cycles

CABIN PRESSURE MASTER WARNING UPON MAIN CABIN DOOR CLOSURE AT GATE GROUNDED - YES. RESET C/BS' ASSOCIATED WITH CPC 1 & CPC 2 & RPCU AND PERFORMED BITE TEST REF 21-31-00 PB 501 OK: CLOSED ALL PAX DOORS AND TURNED ON PACKS: NO FAULT GENERATED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,202 hrs · 3,222 cycles

VENT AVIONICS SYS FAULT. GROUNDED - YES. PER AMM 21-26-00-710-001 TEST AEVC AND SYSTEM TEST OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,162 hrs · 3,202 cycles

FUEL X FEED VALVE FAULT. (FAILED OPEN POSITION) GROUNDED - YES. RESET SYS & PERFORMED OPS TEST OF FLSS. OPS TEST GOOD. REF TSM 28-26-00-810-801-A. NO FAULTS FOUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (FCU) · airframe 10,141 hrs · 3,194 cycles

AUTO FLT FCU 1 FAULT. GROUNDED - YES. ACCOMPLISHED FCU 1 RESET PER AMM 22-81-00. NO FAULTS FOUND. ACCOMPLISHED CAT III CAPABILITY TEST PER AMM 22-97-00. AND AFS TEST PER AMM 22-96-00. ALL CKS OK.

Part: FCU — NONE · airframe 10,083 hrs · 3,172 cycles

FCU # 1 INOP GROUNDED - YES. PERFORMED POWER-UP TEST AND BITE TEST OF AFS REF AMM 22-96-00 PB 501:OK FCU # 1

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,072 hrs · 3,168 cycles

FUEL X FEED VALVE FAULT ECAM DISPLAYED AFTER FUEL BALANCE PROCEDURE. GROUNDED - YES. PERFORMED OPS TEST PER AMM 28-23-00, NO FAULTS FOUND.

Part: REGULATOR VALVE — FAILED (NR 2 ENGINE) · airframe 10,050 hrs · 3,160 cycles

AIR ENGINE 2 BLEED A PRESSURE GROUNDED - YES. REMOVED AND REPLACED BLEED PRESSURE REGULATOR VALVE ON #2 ENG REF AMM 36-11-52 ENG RUN STILL REQUIRED TO COMPLETE OPS AND LEAK CHECK

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 10,050 hrs · 3,160 cycles

ENGINE 2 FIRELOOP B FAULT GROUNDED - YES. DEFERRED. ETOPS RESTRICTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,050 hrs · 3,160 cycles

WING ANTI ICE SYS FAULT GROUNDED - YES. OPS TEST WING ANTI ICE SYSTEM PER AMM 30-11-00-7-. OPS TEST OK.

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 10,007 hrs · 3,140 cycles

ENGINE 2 LOOP B FAULT ON ECAM GROUNDED - YES. ON DEFERRAL

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 9,968 hrs · 3,127 cycles

ENGINE 2 FIRE LOOP B FAULT GROUNDED - YES. SCHEDULED R+R FDU #2 ACCOMPLISHED OP SYS CKS OK FOR SERVICE AS PER AMM 26-12-34. MDDR 61531 CLOSED , PLACARD REMOVED.ETOPS RESTRICTED

Part: REGULATOR — FAILED (NR 2 ENG BLEED) · airframe 9,930 hrs · 3,117 cycles

AFTER TO, AIR ENG 2 BLEED ABNORM PR GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE BLEED PRESSURE REGULATORY VALVE IAW A320 AMM 36-11-52, LEAK CHECK GOOD PERFORMED OPERATIONAL TEST OF THE BLEED AIR REGULATOR SYSTEM IAW A320 AMM 36-11-00

Part: IGNITION UNIT — FAILED (APU) · airframe 9,502 hrs · 2,954 cycles

APU AUTO SHUTDOWN DURING START AT SFO GROUNDED - YES. REMOVED AND REPLACED IGNITION UNIT(8030KM) IAW AMM 49-41-38. OPS CK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,610 hrs · 2,413 cycles

WX RADAR INOP "WXR R/T" IN RED GROUNDED - YES. PERFORMED BITE TEST OF WEATHER RADAR PER AMM 34-41-00. TEST GOOD, NO FAULTS NOTED.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 7,571 hrs · 2,403 cycles

WX RADAR INOP GROUNDED - YES. ETOPS RESTRICTED. R&R XMTR RCVR AT 13SQ1 IAW AMM 34-41-51. BITE TEST OK NO FAULTS OK FOR SERVICE.

Part: CONTROL UNIT — FAULTED (FWD E/E BAY) · airframe 7,203 hrs · 2,305 cycles

FUEL STATUS MAINTENANCE MESSAGE. ACFT GROUNDED. FLSCU-1(7QJ) REMOVED AND REPLACED, SYSTEM TESTED OK IAW AMM 28-46-34.

Part: THERMOSTAT — FAILED (BLEED AIR) · airframe 6,961 hrs · 2,245 cycles

BLEED AIR FAULT. NR 1 PRECOOLER AMBER DURING FLIGHT. TEMP RANGE 85 - 105 DEGREES. ACFT GROUNDED. REPLACED THE NR 1 THERMOSTAT IAW AMM 36-11-43 PB 401, LEAK CHECKED GOOD.

Part: CONTROL PANEL — FAILED (FUEL SYSTEM) · airframe 6,797 hrs · 2,189 cycles

FUELERS UNABLE TO FUEL A/C USING AUTO FUEL PRE SELECT SWITCH MANUAL FUELING IS OK GROUNDED - YES. R&R PRESELECTOR FUEL QUANTITY PANEL IAW AMM 28-42-21. OPS CHECK GOOD. MEL LIST UPDATED. PLACARD REMOVED. MCC NOTIFIED.

Part: A/C PACK — FAULTED (NR 2) · airframe 66,227 hrs · 2,148 cycles

NR 2 A/C PACK FAULTED. ACFT GROUNDED. PERFORMED A RESET IAW TSM 24-00-00-810-818. OPS NORMAL.

Part: UNKNOWN — ODOR (CABIN)

NOTED STRONG BURNING ODOR DURING DESCENT. ODOR ALSO NOTED IN AFT GALLEY. NO ODOR NOTED IN FLIGHT DECK. PERFORMED TSM 05-50-00-810-831A NO BURNING ODORS NOTED IN FWD, AFT GALLEY OR IN MAIN CABIN.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT ATTENDANTS REPORTED THE CABIN FILLED WITH FUMES DESCRIBED AS AN OIL ODOR AFTER LANDING. FUMES SUBSIDED AFTER THE NR 2 ENGINE BLEED WAS TURNED OFF THE APU BLEED WAS TURNED ON. PERFORMED A SMOKE - OIL CHECK IN THE CABIN IAW TSM 05-50-00-810-831-A, AND TSM 71-00-00-810-802-A, NO FUMES OR ODORS IDENTIFIED. RAN THE NR 1 & 2 ENGINES FOR 1 MINUTE AT IDLE, NO OIL LEAKS OR SMOKE FROM FWD DRAIN NOTED.

Part: SENSOR — FAILED (NR 2 A/C PACK)

NR 2 AIR PACK REGULATOR FAULT. R & R THE NR 2 PACK SENSOR, COMPRESSOR TEMPERATURE FIN 32HH IAW AMM 21-61-11, OPS CHECKED OK. SENSOR WAS CONFIRMED BAD.

Part: SENSOR — FAILED (AC BAY) · airframe 5,369 hrs · 1,788 cycles

REPORTED THE FOLLOWING FAULT. AIR PACK 1 REGUL FAULT. R&R NR 1 COMPRESSOR OUTLET TEMP SENSOR 12HH IAW AMM 21-61-11-000-001-A. ACCORDING TO THE OPERATOR`S RECORDS, ALL AIRWORTHINESS DIRECTIVES, SERVICE BULLETINS, STC`S AND PMA`S ARE IN FULL COMPLIANCE WITH THE TYPE DESIGN CERTIFICATE AND ASSOCIATED REGULATORY REQUIREMENTS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,343 hrs · 1,780 cycles

REPORTED THE FOLLOWING FAULT. AIR PACK 1 REGUL FAULT. PERFORMED RESET SFO CLOSED ASSOCIATED CIRCUIT BREAKERS REF AMM 21-61-00. ACCORDING TO THE OPERATORS RECORDS ALL AIRWORTHINESS DIRECTIVES, SERVICE BULLETINS, STC`S AND PMA`S ARE IN FULL COMPLIANCE WITH THE TYPE DESIGN CERTIFICATE AND ASSOCIATED REGULATORY REQUIREMENTS.

Part: CONTROL VALVE — FAILED (NR 1 A/C PACK)

AIR PACK NR 1 REGULATOR FAULT WOULD NOT RESET. R & R PACK NR 1 FLOW CONTROL VALVE 23HB IAW AMM 21-61-11-00-00-01-4A AND REPLACED NR 1 PACK TEMPERATURE SENSOR 12HH IAW AMM 21-58-15-10-00-00-1A.