N627VA

Part: DOOR FRAME — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

L1 DOOR CUTOUT, AFT LOWER CORNER AT FR20, STRUCTURE BELOW GIRT BAR FITTINGS/BLANKING PLATES HAS CORROSION IN MULTIPLE AREAS. GROUNDED - YES. REWORKED 3 EA FASTENER HOLES AT L1 DOOR AFT LOWER CORNER, GIRT BAR FITTING ATTACH POINTS IAW A320 SRM 53-11-14-283-005.

Part: DOOR FRAME — CORRODED (FRAMES 16-17) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

R1 DOOR CUTOUT, FWD LOWER CORNER AT FR16, STRUCTURE BELOW GIRT BAR FITTINGS/BLANKING PLATES HAS CORROSION IN 2 AREAS. GROUNDED - YES. REWORKED 2 EA FASTENER HOLES R1 DOOR CUTOUT, FWD LOWER CORNER GIRT BAR ATTACH POINTS IAW A320 SRM 53-11-14-283-005.

Part: DOOR SILL — CORRODED (FRAMES 67-68) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

L-2 DOOR LOWER SILL, AFT END, SCREW HOLES CORRODED. GROUNDED - YES. CUTOUT DAMAGE AND REPAIRED WITH FILLER AND DOUBLER PER AIRBUS A320 SRM 53-41-14 AT L-2 DOOR SILL AFT END

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

AFT WET AREA FLOOR BEAM BETWEEN FR66 AND FR70 AT Y464 HAS CORROSION AT MOUNT HARD POINT. GROUNDED - YES. REMOVED FLOOR BEAM AND REPLACED WITH NEW PER AIRBUS A320 SRM 53-41-14.

Part: SEAT TRACK — CORRODED (FRAME 20) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

MAIN CABIN SEAT TRACK CORRODED ON SCALLOPS AT GALLEY MOUNT FR20, -Y765. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-15-283-001. REMOVED AND REPLACE SEAT TRACK IAW A320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

MAIN CABIN, FWD BELOW FLOOR WET ARE AT FR16, -Y1292 HAS CORROSION ON UPPER FACE OF FLOOR BEAM. GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK FROM FR12-FR24 AT -Y1292 IAW A320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

MAIN CABIN FWD BELOW FLOOR WET AREA, FRAME C16, BL20R, CORROSION ON UPPER FACE OF FLOOR BEAM. GROUNDED - YES. TRIMMED OUT THE CORRODED SECTION OF THE FLOOR SUPPORT AND ACCOMPLISHED A CATEGORY 'A' REPAIR IAW A320 SRM 53-00-14-300-007.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

MAIN CABIN AFT WET AREA R/H SIDE, FLOOR STRUCTURE HAS CORROSION AROUND BLIND RIVET SHOP HEADS. GROUNDED - YES. REMOVED AND REPLACED FRAME SUPPORT IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 70) · corrosion level 2 · airframe 40,944 hrs · 12,311 cycles

MAIN CABIN AFT WET AREA BELOW FLOOR, FR70 AT Y765 MOUNT HOLE IS GALLED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11.

Part: OIL SYSTEM — LEAKING (APU) · airframe 39,928 hrs · 11,953 cycles

STRONG OIL ODOR IN COCKPIT DURING DESCENT, ACFT GROUNDED. OIL LEAKING FROM LOAD COMPRESSOR DRAIN. APU R & R IAW TASKCARD 4911.000002 & 4911.000003 IN WO 370325, AND OPS AND LEAK CHECKED OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 39,810 hrs · 11,906 cycles

ODOR IN THE CABIN, FROM ENGINE START TO TOP OF DESCENT. MORE NOTICEABLE IN AFT CABIN. ACFT GROUNDED. IAW TSM 05-50-00-810-831-A RAN THE NR 1 ENGINE, ODOR PRESENT ON THE NR 2 ENGINE. IAW TSM 71-00-00-810-802-A COMPLETED TROUBLESHOOTING. FOUND NO ODOR COMING FROM THE NR 1 OR 2 ENGINES DURING RUN AND TAXI. PERFORMED IDLE RAN ON ENGINE 1 & 2 ONE AT A TIME IAW AMM 71-00-00, AND OPERATED PACKS AND OBSERVED THE ODOR IN COCKPIT AND ENTIRE CABIN. NO BAD ODOR.

Part: PIN — FAILED (NLG)

EXPERIENCED THE FOLLOWING ISSUE DURING LANDING ROLL-OUT. ON LANDING AT 70KTS, THE NOSE OF THE ACFT BEGAN A SIGNIFICANT SHIMMY AND ONCE SLOWED ACFT WAS DIFFICULT TO STEER AS LONG AS TAXI SPEED WAS SLOW, WE COULD TAXI/STEER. UPON INSPECTION THE NOSE LANDING GEAR TORQUE LINK APEX PIN WAS FOUND BROKEN. THE APEX PIN, UPPER AND LOWER TORQUE LINKS REQUIRED REPLACEMENT. ALL REQUIRED INSPECTIONS AND OPERATIONAL CHECKS WERE ACCOMPLISHED IAW AMM 05-51-23-200-001-A, ANM05-51-22-200-001-A, ANM32-21-27 PB401 AND THE ACFT WAS RETURNED TO SERVICE.

Part: RELAY — FAILED (EMERGENCY GEN)

DURING OVERNIGHT MX, EMERGENCY GENERATOR TEST FAILED. R & R RELAY FIN 20XE IAW TSM 242400810804A.

Part: UNKNOWN — ODOR (CABIN)

REPORTED AN UNUSUAL ODOR IN THE CABIN. THE INFLIGHT TEAM SHUTDOWN THE IFE AND THE ODOR DISSIPATED. ON ARRIVAL TECHNICIANS ACCOMPLISHED TSM TASK 05-50-00-81-08-31A WITH NO FINDINGS, THE ITEM WAS CLEARED AND THE ACFT WAS RETURNED TO SERVICE. NO ODOR REPORTED ON SUBSEQUENT FLIGHTS.

Part: CONTROL VALVE — FAILED (PARKING BRAKE)

ACFT LANDED AFTER OPERATING FLIGHT. AFTER PULLING OFF RUNWAY HAD THE FOLLOWING DEFECT: AFTER LANDING, PARKING BRAKE WOULD NOT RELEASE WITH PARKING BRAKE SWITCH IN "OFF" POSITION. PARKING BRAKE PRESSURE STILL OBSERVED ON BRAKE PRESSURE GAUGE AND "PARKING BRAKE" ANNUNCIATION STILL DISPLAYED ON UPPER ECAM. R & R PARKING BRAKE ELECTRICAL CONTROL VALVE IAW AMM 32-45-53, PB 401, OPS & LEAK CHECKED GOOD.

Part: WIRE — BROKEN (L1 DOOR) · airframe 21,087 hrs · 6,288 cycles

ACFT WAS HAVING AN OPS TEST OF THE EMERGENCY LIGHT SYSTEM PERFORMED IAW TASK 33-51-00-710-001-A FOLLOWING THE REMOVAL AND REPLACEMENT OF THE R1 SLIDE. DURING THE OPS TEST, THE R1 DOOR PASSED BUT THE L1 DOOR SLIDE INDICATION FAILED THE TEST. UPON REMOVAL OF THE L1 DOOR SLIDE HINGE COVER FOR TROUBLESHOOTING, A SINGLE WIRE WAS FOUND TO BE BROKEN. THE IDENTIFIED WIRE WAS REPAIRED IAW THE ESPM AND THE L1 DOOR INDICATION FUNCTIONED PROPERTY WITH NO FURTHER ISSUES OR MESSAGES NOTED. THE ACFT WAS RETURNED TO SERVICE 1/13/2012 AT 1900Z.

Part: TRANSPONDER — FAULTY (ATC) · airframe 20,889 hrs · 6,219 cycles

AT FL320, ABOUT 45 MIN INTO FLIGHT, CREW SMELLED BURNING LIKE WIRING AND THEN SAW SMOKE COME INTO COCKPIT. RECEIVED AVIONICS SMOKE MSG ECAM, FOLLOWED ECAM AND QRH PROCEDURE WHICH INCLUDED PLACING BLOWER FAN IN OVERRIDE POSITION AND SMOKE AND SMELL DISSIPATED. AT THIS TIME ACFT DIVERTED WHERE EMERGENCY WAS DECLARED AND ACFT LANDED AND TAXIIED TO GATE WITHOUT INCIDENT. MX FOUND SMELL OF SMOKE IN AVIONICS COMPARTMENT BUT NO EVIDENCE OF ANY DEFECTIVE EQUIPMENT OR POPPED CB`S OR SMELL OF SMOKE ANYWHERE ELSE IN ACFT. ACFT HAD 1 MEL THAT WAS PREVIOUSLY ADDED FOR ATC FAIL LIGHT ON TRANSPONDER 2 WHICH WAS APPLIED ON 12/18/12, MEL 34-52-01-02. MX, WHEN REPLACING TRANSPONDER NR2 IAW MEL FOUND TRANSPONDER BOX TO HAVE A BURNING SMELL COMING FROM IT AS WELL AS NO POWER EVEN THOUGH BREAKER NOT POPPED. THIS APPEARS TO HAVE BEEN ORIGINAL SOURCE OF SMOKE REPORTED BUT SINCE WAS ON MEL SYSTEM WAS NOT CHECKED FOR FUNCTION AND BREAKER NOT POPPED. BLOWER FAN WAS ALSO REPLACED AND IFE SYS CHECKS WITH NO FINDINGS.

Part: WHEEL — GOUGED (MLG)

WHILE ACCOMPLISHING MPD TASK 322127-01-1, FOUND GOUGE DAMAGE TO NR 4 MLG WHEEL, PN 20195162, SN 34235/34235 INNER HEAT SHROUD AND WEAR DAMAGE TO NR 4 MLG BRAKE ASSY, PN C202255, SN 04712 MOST INBD DISK. IT APPEARS THAT THE 2 AREAS WERE CHAFING TOGETHER. THE TIRE WAS INSTALLED ON 01/01/2012 AND HAD 510 LANDINGS SINCE INSTALLATION. THERE IS NO RECORD OF THIS TIRE BEING REMOVED FOR ANY MX TASKS SINCE INSTALLATION. THE NR4 BRAKE WAS INSTALLED ON 08/16/2011.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ACFT CABIN FLOOR SUPPORT UNDER SHEAR PLATE AT FR 69-70 AFT LT CORRODED.

Part: SUPPORT — CORRODED (FUSELAGE)

AFT CABIN SUPPORT BEAM HAS CORROSION BETWEEN FR66-68 AT RBL50.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AFT CABIN FLOOR SUPPORT UNDER SHEAR PLATE AT FR 69-70, AFT RT CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT BEAM AT FR16, LBL8 IS CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AFT CABIN FLOOR SUPPORT BEAM HAS CORROSION AT FR, RBL10.