N923VA

Part: FLOOR PANEL — CORRODED (ZONE 100 - FUSE) · airframe 18,655 hrs · 4,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR PANEL 262LG SCREW HOLES. REPLACED FLOOR PANEL PER TASK CARD 26C26053014.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 18,655 hrs · 4,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R4 DOOR CUTOUT LOWER SILL AT FR 66 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,655 hrs · 4,768 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN CABIN FLOOR STRUCTURE SHEAR PLATE HAS CORROSION LOCATED BETWEEN FR 69 AND FR 70 AT STR 23R. REPLACED SHEAR PLATE PER SRM 51-70-11-911-001.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,655 hrs · 4,768 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO FLOOR STRUCTURE HAS CORROSION LOCATED AT FR 56 AND STR 41R. REPLACED FLOOR SUPPORT PER SRM 51-72-11-911-001.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · airframe 18,655 hrs · 4,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO DOOR CUTOUT SILL FITTING AT FR 24A AND S39R. REPLACED FITTING PER SRM 51-42-11.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 7,326 hrs · 2,012 cycles

ENG #1 IGN B FAULT (AFTER THIRD START ATTEMPT) GROUNDED - YES. PERFORMED TSM 74-21-00-810-809-A STEP 3(A)(G). REN #1 ENGINE THREE TIMES WITH NO FAULTS NOTED. REF AMM 71-00-00. NO MX ACTION NEEDED. THIS CLEARS MDDR 76108, MX PROCEDURES REVERSED, MEL LIST UPDATED. PLACARD REMOVED SEAMC ARNE NOTIFIED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE BOTTLES) · airframe 7,255 hrs · 1,993 cycles

FDW CARGO BTL 2 AND AFT CARGO BTL 2 FAULTS ON ECAM GROUNDED - YES. PERFORMED RESET AND OPS TEST OF THE CARGO FIRE EXT. SYS. OPS CHECK GOOD. OK FOR SVC, AMM REF . 26-23-00-710-001-A

Part: SENSE LINE — LEAKING (NR 2) · airframe 7,170 hrs · 1,973 cycles

CLASS II AIR BLEED, MX MESSAGE. GROUNDED - YES. IAW RMA 3654, REPLACED INDICATING TUBE NR 2 ENG, OPS AND LEAK CHECKED GOOD, CLEARS MDDR 75638, PERFORMED TSM 36-11-00-810-A61-A, LEAK CHECKED SENSE LINE, FOUND INDICATING TUBE LEAKING. REPLACED INDICATING TUBE FROM STEP 4A[7]-4E. PERFORMED OPS AND LEAK CHECK, NO LEAKS OR FAULTS NOTED.

Part: IGNITION SYS — FAULTED (NR 1 ENGINE) · airframe 7,076 hrs · 1,950 cycles

IGNITION B FAULT ON ENG 1 STARTUP GROUNDED - YES. DEFERRED

Part: DUCT — DAMAGED (NR 1 FAN AIR) · airframe 6,774 hrs · 1,881 cycles

WITH WING ANTI-ICE SELECTED ON ECAM FOR AIR ENG 1 BLEED LOW TEMP. GROUNDED - YES. BEGAN TSM 36-11-00-810-805-A. FOUND SHEARED SCREW AND WORN / DAMAGED ROD ON FAN AIR VALVE. FOUND ROUNDED OUT BOLT HOLES ON DUCT ASSY & DAMAGED SEAL PLATE ON DUCT. REMOVED FAV AND DUCT PER AMM 36-11-54 K.R.23267. CONTINUED ON LOG PAGE 8057927 ITEM 3

Part: SENSE LINE — LEAKING (NR 2 ENGINE) · airframe 6,225 hrs · 1,752 cycles

FOUND SENSE LINE/7HA2 XDCR BRAIDED AREA LEAKING GROUNDED - YES. REMOVED AND REPLACED SENSE LINE 7HA2 PER AMM 36-11-49. NO LEAKS NOTED AT THIS TIME. OK FOR SERVICE

Part: SKIN — CRACKED (FUSELAGE) · airframe 6,069 hrs · 1,714 cycles

CRACK INDICATION FOUND, DUE TO HOLE LOCATION AT PARTIAL RIVET PLUG, IN EXISTING AFT O/B MOUNT LUG HOLE, FR56 - FR57 @ 1.5" ABOVE S-3R GROUNDED - YES. FABRICATED AND INSTALLED REPAIR AT AFT O/B MOUNT LUG HOLE FR56-FR57 1.5" ABOVE S-3R. IAW ENGINEERING DEVIATION AUTHORIZATION DOCUMENT NR DV5471-MSN7861 REV A.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 5,991 hrs · 1,694 cycles

ENGINE 1 REV MINOR FAULT GROUNDED - YES. PERFORMED TSM 78-37-00-810-843-A. FAULT IS CLEARED AND NOT PRESENT 3 PREVIOUS FLIGHTS. A/C OK FOR SERVICE.

Part: CONTROL KNOB — INOPERATIVE (WX RADAR) · airframe 5,707 hrs · 1,623 cycles

WEATHER RADAR AUTOMATIC GAIN CONTROL (CAL) INOP, DOES NOTT DEPICT WEATHER IN AUTO MANUAL GAIN WORKS GOOD. GROUNDED - YES. VERIFIED WEATHER RADAR AUTOMATIC GAIN CONTROL (CAL) INOP. RELEASED PER MEL/CDL 34-41-01-03, MEL/CDL LOG UPDATED, AUTHORIZED BY AIRBUS SEAMC CARLOS.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 5,316 hrs · 1,516 cycles

CLASS 2 MX MESSAGE TEMP CTL2 GROUNDED - YES. RESET TEMP CTL 2 PER AMM 21-63-00-710-004

Part: TRANSDUCER — MALFUNCTIONED (BLEED SYSTEM) · airframe 5,196 hrs · 1,487 cycles

MAINTENANCE AIR BLEED MESSAGE AFTER BLOCK @ SFO. (7HA2 XDCR HAS BEEN REPLACED LOOK FOR LEAK IN THE BRAIDED SENSE LINE) GROUNDED - YES. TROUBLESHOT PER TSM 36-11-00-810-A61, SUSPECT PRESSURE XDCR 7HA2 BAD.

Part: TRANSDUCER — LOOSE (BLEED PRESSURE) · airframe 5,111 hrs · 1,469 cycles

CLASS II MAINTENANCE MESSAGE AIR BLEED. AIR BLEED MSG FAULTING SENSE LINE/ 7HA2 XDCR.PER TSM 36-11-00-810-A61-A CHECK SENSE LINE LEAKAGE AROUND THE BRAIDED AREA. HAD SIMILAR ISSUES WITH OTHER AIRCRAFT. GROUNDED - YES. R/R BLEED TRANSFERRED PRESSURE TRANDUCER (7HA2) IAW AMM 36-11-15. PERFORMED BITE TEST OF ENGINE BLEEED AIR SYS IAW AMM 36-11-00. OPS CHECK GOOD. THIS CLEAR MDDR 3002 MCC NOTIFIED.

Part: ENGINE — OIL CONSUMPTION (NR 2) · airframe 4,510 hrs · 1,311 cycles

REF 8025318 NR 1 ENGINE OIL CONSUMPTION GROUNDED - YES. ACCOMPLISHED TSM 79-00-00-810-842-A 1-4 AND 4B 1-4 NO DEFECT NOTED SERVICED NR 2 ENGINE WITH 4 QTS OF OIL REF. LP#8025322 (3) NR 2 ENGINE SN#598239 REPLACED PER W/O# 388938 & 388939.MDDR 64677 CLOSED , WATCH LIST UPDATED. MCC NOTIFIED.

Part: CONTROL UNIT — INOPERATIVE (AUTOPILOT SYS) · airframe 4,227 hrs · 1,228 cycles

FCU 1 INOP GROUNDED - YES. REMOVED AND REPLACED FCU PER AMM 22-81-12. CAT 3 OPS CHECK OK.

Part: PRESSURE SWITCH — FAILED (HYDRAULIC SYS) · airframe 3,973 hrs · 1,146 cycles

Y ENGINE PUMP 2 LO PRESSURE GROUNDED - YES. T/S PERFORMED IAW TSM 29-13-00-810-804-A. R/R PRESSURE SWITCH (3074GD) IAW AMM 29-13-17 PB 401 & OPS CHECK GOOD NO LEAKS FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 3,562 hrs · 1,031 cycles

ECAM ENG 1 MINOR FAULT. GROUNDED - YES. PERFORMED DADEC TEST PER AMM 73-00-00, NOT FAULTS, ECAM ENG 1 MINOR NOT SHOWING.

Part: WARNING MESSAGE — ILLUMINATED (NR 1 ENGINE) · airframe 3,489 hrs · 1,005 cycles

ENG 1 MINOR FAULT ECAM GROUNDED - YES. ON DEFERRAL

Part: SENSOR — MALFUNCTIONED (NR 2 N2 SPEED) · airframe 3,485 hrs · 1,001 cycles

ENGINE 1 MINOR FAULT ECAM GROUNDED - YES. R&R N2 SPEED SENSOR PER AMM 77-11-10,OPS CHK GOOD,PERFORMED ENG 1 IDLE RUN PER AMM .PERFORMED FADEC TEST .MDDR CLOSED,MCC NOTIFIED,MEL LIST UPDATED

Part: WARNING MESSAGE — ILLUMINATED (NR 2 FADEC) · airframe 2,997 hrs · 852 cycles

ON ENG SHUTDOWN CLASS 2 ENG 2 FADEC MESSAGE. GROUNDED - YES. ON DEFERRAL

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,831 hrs · 794 cycles

ENGINE 1 MINOR FAULT ECAM MESSAGE DURING ENGINE 1 START. RETURNED TO GATE GROUNDED - YES. *DEFERRED*

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 2,684 hrs · 746 cycles

ENGINE 1 MINOR FAULT ON ECAM. GROUNDED - YES. AIRBUS TFU ISI.73.00.00045 FLT PHASE 9 ENG. MINOR FAULT CAUSE BY SOFTWARE GLITCH REF TASK 77-31-00-810-816-A. NOTED BY JARED MOC.

Part: THRUST REVERSER — FAULTED (NR 1) · airframe 2,599 hrs · 710 cycles

ENGINE #1 REV MINOR FAULT GROUNDED - YES. *DEFERRED*

Part: ENGINE — FAULTED (NR 1) · airframe 2,537 hrs · 685 cycles

NR 1 ENGINE HAD A MINOR FAULT. ACFT GROUNDED.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 2,433 hrs · 653 cycles

WEATHER RADAR RECEIVER/TRANSCEIVER INOP. GROUNDED - YES. R&R WXR TRU FIN 13SQ1 PER AMM 34-41-51 PB 401. BITE CHECK GOOD.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 2,431 hrs · 652 cycles

PREDICTIVE WIND SHEAR INOP. WXR R/T FAULT ILLUMINATED, WX RADAR INOP GROUNDED - YES. R&R WEATHER RADAR TRANSCEVIER FIN 15Q21 REF AMM 34-41-33 PB401. PERFORMED BITE TEST. TEST OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,414 hrs · 638 cycles

ENGINE 1 MINOR FAULT ILLUMINATED AT ENGINE START. GROUNDED - YES. *ON DEFERRAL*

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,336 hrs · 614 cycles

ECAM ENGINE NR 1 MINOR FAULT GROUNDED - YES. *ON DEFERRAL*.

Part: UNKNOWN — FAULTED · airframe 2,228 hrs · 578 cycles

ENGINE 1 MINOR FAULT GROUNDED - YES. *ON DEFERRAL*

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,140 hrs · 554 cycles

ENGINE 1 MINOR FAULT ON ECAM GROUNDED - YES. PERFORMED OPS TEST PER AMM 73-29 00 TEST OK . COULD NOT DUPLICATE FAULT.

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 1,909 hrs · 499 cycles

ECAM FOR THE NR 1 ENGINE, MINOR FAULT. ACFT GROUNDED. PERFORMED ENGINE FADEC TESTS IAW AMM 73-29-00. NO FAULTS NOTED. CHECKED OK.

Part: CIDS — MALFUNCTIONED (NR 1) · airframe 1,542 hrs · 401 cycles

SMOKE DETECTOR AMBER FAULT ON LANDING. ACFT GROUNDED. PERFORMED A CIDS NR 1 SYSTEM RESET, OPS GOOD IAW AMM 23-73-00.

Part: CONTACTOR — FAILED (BCL 2) · airframe 1,503 hrs · 390 cycles

ELEC BCL 2 FAULT ECAM, ACFT GROUNDED. R & R THE CONTACTOR 6PB2 IAW AMM 24-38-55. OPS CHECKED GOOD. BCL 2 NO FAULTS. NO MATTER THE AMPERAGE BEING USED.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 1,256 hrs · 328 cycles

NR 1 ENGINE ANTI-ICE VALVE FAULT ECAM. ACFT GROUNDED. THE NR 1 ANTI-ICE TESTED WITH ENGINE RUN IAW AMM 30-21-00. OPS CHECKED GOOD. NO DEFECTS NOTED. OK FOR SERVICE.

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 1,219 hrs · 320 cycles

WHILE PERFORMING TC 730000-L1-1-VAM, FOUND SMR FAULT FOR THE NR 1 ENGINE CHANNEL A 0391 VIBRATION SYS. PERFORM TSM 77-11-00-810-852-A PARA 4.C. SUBTASK 77-11-00-810-166-A. ACFT GROUNDED. TROUBLESHOT IAW TSM 77-11-00-810-843-A. PERFORMED AN OPS ENGINE IDLE TEST FOR THE NR 1 ENGINE CHANNEL A, IAW AMM 73-29-00-740-803. NO CONFIRMATION OF THE FAULT. NO MAINTENANCE ACTION REQUIRED. OK FOR SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 670 hrs · 176 cycles

WITH AUTOPILOT ON DURING DESCENT, THERE WAS A ROLLING MOMENT LEFT AND RIGHT, VERY LIGHT. FLIGHT CONTROL PAGE SHOWED AILERON MOVEMENT. 250KTS AT 10,000 FT. AIRPLANE HAS BEEN RESTRICTED FROM ETOPS OPERATIONS DUE TO AUTOPILOT INOPERATIVE. ACFT GROUNDED.

Part: AUTOPILOT SYS — MALFUNCTIONED (NR 2) · airframe 634 hrs · 169 cycles

DURING DESCENT WITH AUTOPILOT NR 2 ON, AIRCRAFT ROCKS BACK AND FORTH. F/CT PAGE PULLED UP, SHOWS LT & RT AILERON MOVING BACK AND FORTH. ACFT GROUNDED. PERFORMED AFS TEST IAW 22-96-00. PERFORMED ELAC TEST IAW 27-93-34. PERFORMED CAT 3 TEST IAW 22-97-00. OPS TESTED GOOD.

Part: SENSOR — DEFECTIVE (NR 2 A/C PACK) · airframe 634 hrs · 169 cycles

DUE TO NUMEROUS HITS, REPLACE PACK 2 PRESSURE INLET SENSOR. ACFT GROUNDED. RMA 2048 ACCOMPLISHED, R & R THE NR 2 PACK PRESSURE INLET SENSOR IAW AMM 21-51-13.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 600 hrs · 159 cycles

MAINT AIR BLEED ON STATUS PAGE GROUNDED - YES. NO CURRENT STATUS MESSAGE DISPLAYED BMC TEST OK IAW AMM 36-11-00 OK FOR SERVICE.

Part: ENGINE — VIBRATION (NR 2)

INTERMITTENT NR 2 ENGINE HIGH N1 VIBRATION ECAM MESSAGE. N1 VIBRATION PEAK 7.1 - 8.0. VIBRATION WAS DETERMINED TO BE AN ISOLATED INDICATION ISSUE, CREW DID NOT PERCEIVE ANY PHYSICAL SIGNS OF VIBRATION. PERFORMED VIBRATION CHECK OF THE NR 2 ENGINE IAW AMM 71-00-00-710-813-A. HIGHEST N1 VIBRATION WAS 0.5 AT 70% N1. ENGINE IS OK FOR SERVICE. PERFORMED TSM 77-11-00-810-824-A N1 VIBRATION EXCEEDANCE ITEM 4 B 2 A -C FOR VISUAL INSPECTION OF FAN AND BOOSTER, VISUAL INSPECTION OF TURBINE EXHAUST AND DETAILED INSPECTION OF THE OIL DEBRIS, MONITORING.