N228NV

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 64,232 hrs · 22,752 cycles

FA'S AND PAX COMPLAINING OF DIRTY SOCK ODOR DURING CRUISE / R&R #2 ENG, AND COMPLIED WITH DECONTAMINATION OF ECS"

Part: FILTER — DIRTY · airframe 63,803 hrs · 22,534 cycles

AFT FA'S REPORTED AN ELECTRICAL BURNING ODOR DURING GEAR REACTION & EXTENSION/FOUND GREEN HYDRAULIC SYSTEM RETURN LINE UNION LEAKING AT FR68. TORQUED NUT, NO HELP. R&R RECIRCULATION FILTERS, AND ELBOW FITTING.

Part: INTAKE — CONTAMINATED (APU) · airframe 63,283 hrs · 22,288 cycles

DIRTY SOCK ODOR DURING DESCENT. FOUND RESIDUAL OIL IN THE FWD APU INTAKE PLENUM, CLEANED & INSPECTED THE APU, NO FAULTS NOTED.

Part: LIGHT — CONTAMINATED (GALLEY OVERHEAD) · airframe 61,873 hrs · 21,522 cycles

FA REPORTED A BURNING ODOR FROM 10000 FT THRU LANDING AND TAXI IN. NOTICED OVERHEAD READING LIGHT IN AFT GALLEY FLICKERING. NO VISIBLE SMOKE NOTED. FOUND AFT GALLEY OVERHEAD PANEL LIGHT MODULE & EWIS HAD CONTAMINATION CLEANED CONTAMINATION.

Part: FAN — FAILED (E/E BAY) · airframe 60,176 hrs · 20,637 cycles

AVIONICS SMOKE ECAM ACCOMPANIED BY ELECTRICAL BURNING ODOR. NO SMOKE OBDERVED. ECAM EXTINGUISHED WITH IN 2 SECONDS. REPLACED AVIONIC FAN 20HQ, OPS CHECKED OK. IAW TSM 05-50-00-810-831-A, AMM 21-26-00-710-001A. NO ODORS NOTED LEAK CHECK OK.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 60,101 hrs · 20,591 cycles

UPON GEAR RETRACTION, NOSE GEAR STARTED RETRACTING, WE HEARD AN UNUSUAL NOISE. NLG EXTENDED BACK DOWN. A FEW SECONDS LATER RECEIVED ECAM FOR LANDING GEAR, FOLLOWED BY LOW HYD PRESS ON GREEN SYSTEM. CONFIRMED THAT WE HAD LOST ALL FLUID IN GREEN SYSTEM. WE PERFORMED ALL QRH PROC AND DID A MANUAL GEAR EXTENSION. REPLACED GREEN SYSTEM CASE DRAIN FILTER. NO PARTICLES FOUND. RETORQUED LINES ON CASE DRAIN FILTER ASSY PER AMM 20-21-12 LEAK CHECK REQUIREDC/W GREEN SYSTEM BLEEDING PER AMM 29-00-00-870-002-A & 29-00-00-870-003-A.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 59,294 hrs · 20,147 cycles

AFTER TAKEOFF IN CLEAN CONFIGURATION, CHECKED HYD LEVEL. THE GREEN SYSTEM SHOWED THE LEVEL JUST ABOVE THE AMBER RANGE. CHOSE TO RETURN TO THE FIELD. LOWERED THE GEAR BEFORE FURTHER LOSS. RECEIVED ECAM FAULT, LANDING GEAR LEVER DISAGREE, GEAR EXTENDED SLOWLY, 30 SEC ONCE EXTENDED ECAM FAULT WENT AWAY. THE ACFT GEAR INDICATION WAS UNLOCKED. CONFIGURED NORMALLY. ON ROLLOUT RECIEVED, LANDING GEAR SYS, CAUTION DISAGREED. ALL GEAR INDICATIONS WERE GREEN, SWITCH, HYD LOW PRESSURE TUBE REMOVED IAW AMM 29-11-49, DL-5865. R & R LOW PRESSURE HYD TUBE IAW AMM 29-11-49. PERFORMED OPS CHECK, GOOD. COMPLIED WITH WO 00301401 AND 00301403 IAW TECH SERVICES. ACCOMPLISHED GREEN HYD SYSTEM SERVICE IAW AMM 12-12-29-611-001A PERF GREEN SYSTEM BLEEDING PROCEDURE IAW AMM 29-00-00-870-003A. PERF NLG DOOR OPEN PROX SENSOR FAULT IAW TSM 32-31-00-810-818A NO FAULTS FOUND.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 59,294 hrs · 20,147 cycles

GREEN HYD RESERVOIR LOW WITH GREEN SYS PRESS LOW ECAM, RAN ECAM & QRH. PERFORMED MANUAL GEAR EXTENSION & FOUND PIN HOLE RUBBED IN LINE FROM CLAMP. LINE PN 112441-507, REPLACED LINE IAW AMM 29-11-49. LEAK & OPERATIONS CHECKED GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 57,674 hrs · 19,365 cycles

LEFT EMER EXIT DOOR LIGHT FLASHING. ADJUSTED LT AFT EMER DOOR PROXIMITY SWITCH. PERFORMED OPERATIONS CHECK IAW AMM 52-73-11. NO DEFECTS NOTED & OPERATIONS CHECKED GOOD.

Part: ANGLE — CORRODED (L2 DR LWR SILL)

ANGLE CORRODED AT THE L2 DOOR SILL.

Part: ANGLE — CORRODED (R2 FWD DOORSILL)

ANGLE CORRODED AT R2 DOOR SILL.

Part: FLOORBEAM — CORRODED

FLOORBEAM CORRODED.

Part: ANGLE — CORRODED

NONE

Part: SEAT TRACK — CORRODED (STA 1282)

SEAT TRACK CORRODED AT BS 1282.

Part: FILLER — CORRODED (DOOR SILL)

FILLER CORRODED ON DOOR SILL.

Part: WEB — CORRODED (FRAME 20)

WEB CORRODED AT FRAME 20.

Part: WEB — CORRODED (FRAME 18)

WEB CORRODED AT FRAME 18.

Part: DOUBLER — CORRODED (NOT REPORTED)

DOUBLER CORRODED AT UNKNOWN LOCATION.

Part: FLOORBOARD — CORRODED

NONE

Part: FLOORBEAM — CORRODED (FRAME 64)

FLOORBEAM CORRODED AT FRAME 64.

Part: SEAT TRACK — CORRODED (CABIN)

SEAT TRACK CORRODED.

Part: FLANGE — CORRODED

NONE

Part: FLOOR SUPPORT — CORRODED

NONE

Part: FLOORBEAM — CORRODED (FRAME 66)

FLOORBEAM CORRODED AT FRAME 66.

Part: ANGLE — CORRODED (L2 DOOR)

ANGLE CORRODED AT L2 DOOR.

Part: FITTING — CORRODED

NONE

Part: SEAT TRACK — CORRODED (CABIN)

SEAT TRACK CORRODED.

Part: SUPPORT RIB — CORRODED (APU BAY)

APU BAY SUPPORT RIB CORRODED.

Part: FLOOR SUPPORT — CORRODED (FR 66)

FLOOR SUPPORT CORRODED AT FRAME 66.

Part: BRACKET — CORRODED (RUDDER HINGE)

RUDDER HINGE BRACKET CORRODED.

Part: TRANSITION PANEL — CORRODED (AFT CARGO)

TRANSITION PANEL FOUND CORRODED IN THE AFT CARGO BAY.

Part: FLOOR PANEL — CORRODED (FR66-68)

FLOOR PANEL CORRODED FRAMES 66-68.

Part: TRANSITION PANEL — CORRODED (AFT CARTO)

AFT CARGO BAY TRANSITION PANEL CORRODED.

Part: FLOOR SUPPORT — CORRODED

FLOOR SUPPORT CORRODED.

Part: FLOOR SUPPORT — CORRODED (FRAME 66)

FLOOR SUPPORT CORRODED.

Part: FLOORBOARD — CORRODED (FRAME 66)

FLOORBOARD CORRODED AT FRAME 66.