N285VA

Part: FAULT MESSAGE — ABNORMAL (COCKPIT) · airframe 14,561 hrs · 4,904 cycles

AIR PACK #1 REGUL. FAULT GROUNDED - YES. PERFORMED BITE TEST OF THE TEMP CTL REF AMM 21-61-00 TEST OK NO FAULT NOTED

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 14,308 hrs · 4,782 cycles

CPC SYS 1 AND 2 FAULT UPPER ECAM. GROUNDED - YES. REMOVED AND REPLACED (12HL) CPC2 IAW AMM 21-31-34. PERFORMED AN OPS TEST ON THE 11HL AND 12HL CPC2 IAW AMM 21-31-00-710-002-A. TESTED OK.

Part: FAULT MESSAGE — ILLUMINATED (CONTROLLER) · airframe 14,259 hrs · 4,761 cycles

CABIN PRESSURE SYS 1 FAULT MESSAGE. GROUNDED - YES. FAULT HISTORY LOGGED, PRESS CONTR 1. ACCOMPLISHED TSM TASK 21-31-00-810-803-A. ALL TEST PASSED. NO HISTORY, ALSO REF MDDR 70390 - ETOPS RESTRICTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 14,259 hrs · 4,761 cycles

CABIN PRESSURE SYSTEM 1 FAULT MSG GROUNDED - YES. FAULT HISTORY LOGGED: PRESS CONTR 1, ATA 21-31-34. ACCOMPLISHED TSM TASK 21-31-00-810-803-A. ALL TEST PASSED. NO HISTORY, ALSO REF MDDR 70390. ETOPS RESTRICTED

Part: WARNING MESSAGE — ILLUMINATED (BLEED AIR SYS) · airframe 13,904 hrs · 4,619 cycles

CLASS II AIRBLEED MESSAGE GROUNDED - YES. OPEN

Part: LANDING GEAR — MALFUNCTIONED · airframe 13,899 hrs · 4,616 cycles

LANDING GEAR DID NOT EXTEND WITH LDG GEAR HANDLE ON THE DOWN POSITION. DOORS DID OPENED. CYCLED GEAR HANDLE AND GEAR EXTENDED. GROUNDED - YES. AC AOG. VERIFIED LANDING GEAR RETRACTION INOP. RELEASED PER MEL 32-31-00 MEL LOG UPDATED AUTOHORIZED BY SEAMC WILL. MAINT PROCEDURES ACCOMPLISHED 188VU VMO-MMO SWITCH PLACED TO THE L/G DOWN POSITION AND L/G SELECTOR PANEL PLACARDED.CHECKED POST FLT REPORT FOR LG FAULTS. NO FAULTS. PERFORMED BITE OF #1 AND #2 LGCIU. NO FAULTS IN BITE TEST OR TROUBLESHOOT REF AMM 32-69-00. GEN VIS. INSP. OF L/G NO DEFECTS. MEL 32-31-00 CONTINUES MAINTENANCE PROCEDURES FOR MEL 32-31-00 REMAIN IN PLACE/C.W. SEAMC WILL NOTIFIED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,649 hrs · 4,509 cycles

ON CLIMBOUT ECAM SHOWED AIR ENG 1 BLEED FAULT GROUNDED - YES. PERFORMED BITE OF BMC1 REF AMM 36-11-00-740-001-A , TEST OK. NO FAULT CURRENTLY , NO HISTORY 30 DAYS , SEAMC CONTACTEDPER LOGPAGE 8052445: VERIFIED ENG 1 BLEED INOP. EACH MX PROCEDURE CONTAINED IN THE MEL WAS ACCOMPLISHED. RELEASED PER MEL 36-11-01-02-A. MEL LOG UPDATED.

Part: SWITCH — FAILED (HYD RESERVOIR30) · airframe 13,596 hrs · 4,487 cycles

HYDRAULIC YELLOW RESERVOIR LOW LEVEL WARNING GROUNDED - YES. R & R LOW LEVEL SWITCH OF THE YELLOW HYD RESERVOIR IAW AMM 29-13-41 PB 401- OPS CHK AND LEAK CHK GOOD A/C OK FOR SERVICE

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 13,488 hrs · 4,443 cycles

NR 2 ENGINE SMR T3 FAULT T3 SENSOR J13, ECU GROUNDED - YES. REF TSM TASK 77-20-00-810-829-A. PERFORMED FADEC NON-MOTOR TEST ENG 2 CHA & CHB. NO FAULTS DETECTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL SYSTEM) · airframe 13,423 hrs · 4,414 cycles

AFTER LANDING, FUEL L & R OUTER XFR OPEN ON ECAM GROUNDED - YES. PERFORMED FUNCTIONAL (BITE) TEST OF FLSS CH1 & CH2 NO FAULTS. REF. AMM 28-46-00-740-00-A. ECAM MSG FUEL L&R OUTER XFR OPEN WERE NOT PRESENT

Part: APU — SHUTDOWN · airframe 13,419 hrs · 4,412 cycles

APU AUTO SHUTDOWN. GROUNDED - YES. PERFORMED TEST AND RESET OF APU. OPS CK GOOD PER A320 AMM 49-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,343 hrs · 4,379 cycles

CLASS II AIR BLEED MAINTENANCE STATUS MSG GROUNDED - YES. RESET FWC 1 & 2 PER AMM 36-00-00. OK FOR SVC

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,349 hrs · 13,256 cycles

SMOKE FWD CRG BTL2 FAULT. SMOKE AFT CRG BTL 2 FAULT GROUNDED - YES. RESET OF SYSTEM ACCOMPLISHED PER AMM 26-16-00. ALL FAULTS CLEARED.

Part: SENSE LINE — LEAKING (BLEED AIR SYS) · airframe 13,139 hrs · 4,302 cycles

#2 ENGINE HPSOV RAPIDLY OPENING+CLOSING GROUNDED - YES. PERFORMED BITE TEST OF FADEC SYSTEM AND ENG #2 RUN (5 MIN IDLE) PER AMM 73-29-00-710-040-01 FADEC AMD AMM 71-00-00-710-006 IDLE RUN. TEST OK NO DEFECTS NOTED. OK FOR SERVICEFOUND HP SENSE LINE LEAKING (BROKEN). IPC 36-11-49-02 ITEM 100, REMOVED AND REPLACED SENSE LINE IAW AMM 36-11-49. PERFORMED ENG RUN NO LEAKS AND NO FAULT NOTED. MCC CARLOS NOTIFIED.

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 2 A/C PACK) · airframe 13,085 hrs · 4,278 cycles

AIR PACK 2 REGUL FAULT ECAM IN FLIGHT GROUNDED - YES. PERFORMED OPERATIONAL TEST OF PACK TEMP CONTROL SYSTEM PER AMM 21-61-00 TEST OK. NO FAULTS NOTED. OK FOR SVC

Part: THERMOCOUPLE — FAILED (NR 1 ENGINE) · airframe 12,921 hrs · 4,227 cycles

MAINTENANCE ENGINE 1 FADEC FAULT GROUNDED - YES. R&R ENG 1 T3 THERMOCOUPLE PER AMM 77-23-10. OPS TEST GOOD. MEL 71-71-00-01-A REMOVED. MDDR 69890 CLEARED. NO MX ACTION REQUIRED. PLACARD REMOVED. MEL LOG UPDATED. MCC LESTER NOTIFIED.

Part: FADEC — MALFUNCTIONED (NR 1) · airframe 12,833 hrs · 4,189 cycles

MAINTENACE ENGINE 1 FADEC MESSAGE. GROUNDED - YES. GRND FADEC TEST THROU MCDU IAW AMM 73-22-34. NO FAULT DETECTED. A&P 3571457PERFORMED OPERATIONAL TEST OF THE FADEC REF AMM TASK 73-29-00-861-051-A. NO FAULTS FOUND

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,727 hrs · 4,151 cycles

PACK #1 REGUL FAULT STATUS MSG. ON PRE - FLIGHT GROUNDED - YES. RESET PACK 1 FAULT CLEARED OPS CHECK OKAY REF AMM21-61-00.

Part: SENSOR — FAULTED (T3) · airframe 12,288 hrs · 3,994 cycles

DURING PERFORMING T/C 730000-C2-1-VAM FOUND SCHEDULED MAINT REPORT ENGINE 2 CHANNEL A&B T3 SENSOR FAULT.T3 SENSOR, J13, ECU GROUNDED - YES. PERFORMED OPERATIONAL TEST OF FADEC 2A AND 2B NO FAULTS FOUND REF TSM 77-20-00-810-806-A TIS CLEARS MDDR 67730 AND TASK 730000-C1-1-VAM.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 11,917 hrs · 3,845 cycles

IN CRUISE FLIGHT AT FL360 WITH FUEL MODE NORMAL AND 0 FUEL IN CENTER TANK-GOT ECAM 'FUEL CENTER RIGHT TRANSFER FAULT + AMBER XX ON CENTER RIGHT PUMP-FUEL PAGE. GROUNDED - YES. PERFORMED RESET OF FLSCU, NO FAULTS NOTED, REF AMM 28-46-00. ECAM FUEL PAGE SHOWING PROPER INFORMATION.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 11,127 hrs · 3,553 cycles

PASSENGER OXYGEN MASK DROPPED FROM ROW 25 ABC GROUNDED - YES. RESECURED 25 ABC OXYGEN MASK AS REQUIRED PER AMM 35-21-43.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,120 hrs · 3,547 cycles

VENT AVNCS SYS FAULT ECAM, INLET AMBER XX GROUNDED - YES. DEFERRED PER MEL 21-26-05-02.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 10,984 hrs · 3,484 cycles

OXYGEN MASK DROPPED DURING LANDING AT SEAT 25R GROUNDED - YES. REPACKED OXY MASK PER AMM 35-21-41 PB 401. OPS CHECK GOOD, OK FOR SVC.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR) · airframe 10,782 hrs · 3,423 cycles

ENG 1 BLEED DID NOT CLOSE ENGINE SHUTDOWN GROUNDED - YES. RESET BMC SYSTEMS. PERFORMED TEST OF BMCS TEST OK. NO FAULTS FOUND REF AMM 36-11-00

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,253 hrs · 3,256 cycles

AIR PACK 1 REGUL FAULT. GROUNDED - YES. RESET OPS CHECK GOOD. IAW AMM 21-61-00710-001 OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,202 hrs · 3,240 cycles

AIRPACK 1 REGULATOR FAULT GROUNDED - YES. RESET TEMP CTRL SYST 1 OPS CK PER AMM 21-61-00, OPS CK GOOD. A/C OK FOR SERVICE. (AP) 3621974

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 9,985 hrs · 3,169 cycles

ON DESCENT PRESSURE FLUCTUATING RAPIDLY BETWEEN 200-700 FPM. GROUNDED - YES. PFR SHOWS NO FAULT CORRESPONDING TO CABIN PRESS SYS. PERFORMED BITE TEST OF CPC1 AND CPC2 PER AMM 21-31-00 FOUND ONLY CPC2 CLASS 3 FAULT "LGCIU SIG REPLACED". FOLLOW TSM 21-31-00-810-817A FOUND NO FAULTS. CPC1 AND CPC2 OPS CHK OK. ALSO CHECKED OUTFLOW VALVE FOR OBSTRUCTION- ALL FOUND CLEAR. A/C OK FOR SERVICE.

Part: BLEED VALVE — OPEN (NR 2 ENGINE) · airframe 9,792 hrs · 3,113 cycles

ECAM BLEED PAGE INDICATES THE NR 2 ENGINE HP BLEED VALVE WAS OPEN DURING CRUISE, AT THE GATE WITH ENGINE OFF, ACFT GROUNDED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 8,757 hrs · 2,805 cycles

APU AUTO SHUT DOWN ECAM DURING APU START GROUNDED - YES. OPS CHECKED APU AMM 49-40-00 OKAY. CLEARED FOR SERVICE

Part: CONTROL VALVE — FAILED (NR 1 A/C PACK) · airframe 8,643 hrs · 2,773 cycles

HOT AIR SYS INOPERATIVE. ACFT GROUNDED. R & R THE NR 1 PACK FLOW CONTROL VALVE IAW AMM 21-51-51. OPS CHECKED GOOD. NO LEAKS.

Part: SENSOR — FAILED (NR 1 A/C PACK) · airframe 8,641 hrs · 2,771 cycles

NR 1 A/C PACK REGULATOR FAULT DURING SHUTDOWN. ACFT GROUNDED. THE PACK REGULATOR RESET CARRIED OUT, MESSAGE CLEARED. THE NR 1 A/C PACK BITE NO FAULTS NOTED IAW AMM 21-61-00-710-001. OPERATED THE PACKS FOR 15 MINUTES, NO FAULTS IAW RMA, REPLACED THE NR 1 PACK DIFFERENTIAL PRESSURE SENSOR 23HB2 IAW AMM 21-51-11-000-001-A, & TASK 21-51-11-400-001-A.

Part: REGULATOR — FAULTED (NR 1 A/C PACK) · airframe 8,628 hrs · 2,763 cycles

NR 1 A/C PACK REGULATOR FAULTED. ACFT GROUNDED. RESET THE TEMP CONTROL CIRCUIT BREAKER IAW AMM 21-61-01, NO FAULTS NOTED.

Part: FAULT MESSAGE — FALSE ACTIVATION (CAB/CKPT TEMP) · airframe 8,524 hrs · 2,731 cycles

HOT AIR FAULT. ACFT GROUNDED. PERFORMED AN OPS CHECK OF THE COCKPIT AND CABIN TEMP CONTROL IAW AMM 21-63-00. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: REGULATOR — FAULTED (NR 1 A/C PACK) · airframe 8,435 hrs · 2,705 cycles

NR 1 A/C PACK REGULATOR FAULTED. ACFT GROUNDED. PERFORMED A RESET & OPS CHECK OF PSCK TEMP CONTROL, OPS CHECKED GOOD IAW AMM 21-61-00

Part: CONNECTOR — SATURATED (APU) · airframe 8,245 hrs · 2,642 cycles

ON TAXI IN, WHEN APU MASTER SELECTED ON, ECAM DISPLAYED "APU EMERG SHUTDOWN" GROUNDED - YES. FOLLOWED TSM 49-00-81-810-803-A, FOUND WATER INGRESS IN PNL 108VU, CLEANED AND DRY ELECT CONNECTIONS. REINSTALLED ONL 108VU AND PERFORMED APU OPS CHECK REF AMM 49-00-00, CHECKS GOOD.

Part: A/C PACK — MALFUNCTIONED (NR 2) · airframe 8,082 hrs · 2,600 cycles

NR 2 PACK PRESSURE FLUCTUATED BETWEEN 12 AND 34 PSI DURING DESCENT. CAUSED CABIN PRESSURE V/S TO FLUCTUATE FROM 150 FT/MIN TO 500FT/MIN. ACFT GROUNDED. NR 2 PACK SYSTEM TESTED IAW AMM 21-61-00-710-001. OPS AND TEST PASSED. CPC1 & CPC2 TEST AUTO IAW AMM 21-31-01 TEST PASSED. PFR AND LAST LEG REPORT NO FAULT. AIRCRAFT OK FOR SERVICE.

Part: SENSOR — FAILED (COMPRESSOR)

THE FLIGHT CREW REPORTED THE NR 1 A/C PACK 1 REGULATOR FAULT DISPLAYED ON ECAM DURING CRUISE. REMOVED AND REPLACED COMPRESSOR TEMP SENSOR 12HH IAW AMM 216111. NO FURTHER REPORTS ON SUBSEQUENT FLIGHTS.

Part: FADEC — FAILED (NR 2 ENGINE)

ACFT EXPERIENCED A NR 2 ENGINE FADEC B FAULT AT ENGINE START AND RETURN TO GATE. THE ACFT WAS TAKEN OUT OF SERVICE AND TROUBLESHOT IAW TSM 73-20-81-810-893-A. THE FAULT WAS CONFIRMED AND HE NR 2 ENGINE FADEC WAS REPLACED IAW AMM 73-21-60. NO FURTHER ISSUES REPORTED ON SUBSEQUENT FLIGHTS.