N752US

Part: PIN — BROKEN (ZONE 200) · airframe 59,808 hrs · 41,005 cycles

AIRCRAFT IN BASE MAINTENANCE: ROW 21ABC SEAT WALL EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE FOUND WIRE BROKEN ON CONNECTOR OF HARNESS THAT CONNECTS TO 7260VC10. REPLACED PIN IAW ESPM 20-48-21 AND WDM 33-51-08.

Part: PIN — BROKEN (ZONE 200) · airframe 59,808 hrs · 41,005 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 20ABC SEAT WALL EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE FOUND WIRE BROKEN ON CONNECTOR OF HARNESS THAT CONNECTS TO 7260VC10. MAINTENANCE REPLACED PIN IAW ESPM 20-48-21 AND WDM 33-51-08.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 59,614 hrs · 40,858 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR BOTTLE NEEDS SERVICING. MAINTENANCE SERVICED 2L DOOR IAW AMM 52-13-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 59,614 hrs · 40,858 cycles

AIRCRAFT WAS NOT GROUNDED: 2R DOOR BOTTLE NEEDS SERVICING. MAINTENANCE SERVICED 2R DOOR IAW AMM 52-13-00.

Part: SKIN — CRACKED (ZONE 200) · airframe 58,040 hrs · 39,794 cycles

AIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACK FOUND RADIATING FROM FASTENER HOLE ON NOSE SKIN PANEL AT RIGHT HAND FR 13/14 AND Z+780 - Z+950. REPAIRED SKIN PANEL PER EA 362921

Part: SKIN — CRACKED (ZONE 200) · airframe 58,040 hrs · 39,794 cycles

AIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACK FOUND RADIATING FROM FASTENER HOLE ON NOSE SKIN PANEL AT LEFT HAND FR 13/14 AND Z+780 - Z+950. REPAIRED SKIN PANEL PER EA 362923.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 57,976 hrs · 39,745 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR ASSIST BOTTLE BELOW LIMITS. MAINTENANCE SERVICED R2 DOOR ASSIST BOTTLE PER 52-1-00.

Part: BATTERY — FAULTED (ZONE 200) · airframe 57,674 hrs · 39,554 cycles

AIRCRAFT WAS NOT GROUNDED: FWD L EPSU BATTERY FAULT. MAINTENANCE REPLACED FWD LH EPSU BATTERY IAW AMM 33-51-38.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 57,374 hrs · 39,351 cycles

AIRCRAFT WAS GROUNDED: EPSU L AFT COMM FAULT (13WL). MAINTENANCE REPLACED EPSU UNIT IAW AMM 33-51-38, NO FIX. REPLACED DEU-B (300RH5) IAW AMM 23-73-47.

Part: POWER SUPPLY — FAULTED (ZONE 200 -) · airframe 57,374 hrs · 39,351 cycles

AIRCRAFT WAS GROUNDED: EPSU BATT FAULT ON EPSU 11WL. MAINTENANCE REPLACED EPSU BATTERY AT 11WL IAW AMM 33-51-38.

Part: BOTTLE — READS LOW (DOOR ASSIST) · airframe 57,260 hrs · 39,280 cycles

AIRCRAFT WAS NOT GROUNDED: R/H AFT PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR REQUIRES SERVICING (READS 1100PSI AT 45 DEGREES FAHRENHEIT). MAINTENANCE SERVICED R/H AFT PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR IAW AMM 52-10-00 (SERVICED TO 1650PSI AT 45 DEGREES FAHRENHEIT).

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 57,260 hrs · 39,280 cycles

AIRCRAFT WAS NOT GROUNDED: L/H FWD PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR REQUIRES SERVICING (READS 1150PSI AT 45 DEGREES FAHRENHEIT). MAINTENANCE SERVICED L/H FWD PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR IAW AMM 52-10-00. (SERVICED TO 1650PSI AT 45 DEGREES FAHRENHEIT).

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 57,260 hrs · 39,280 cycles

AIRCRAFT WAS NOT GROUNDED: LAV D EMERGENCY LIGHT INOP. MAINTENANCE REPLACED LAV D MIRROR LIGHT ASSEMBLY IAW AMM 33-24-12. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 57,260 hrs · 39,280 cycles

AIRCRAFT WAS NOT GROUNDED: L/H AFT PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR REQUIRES SERVICING (READS 1400PSI AT 45 DEGREES FAHRENHEIT). MAINTENANCE SERVICED L/H AFT PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR IAW AMM 52-10-00 (SERVICED TO 1650PSI AT 45 DEGREES FAHRENHEIT).

Part: APU — ODOR (ZONE 100) · airframe 57,236 hrs · 39,260 cycles

AIRCRAFT WAS GROUNDED: MUSTY ODOR THROUGHOUT AIRCRAFT DURING DESCENT. MAINTENANCE TS ODOR TO APU AND REPLACED THE APU.

Part: INDICATOR — DEFECTIVE (ZONE 800) · airframe 57,092 hrs · 39,156 cycles

AIRCRAFT WAS NOT GROUNDED: UPON LANDING R1 DOOR OPEN INDICATION ON ECAM WITH DOOR CLOSED. **SUPPLEMENTAL REPORT FOR AALA202410021671: MAINTENANCE REPLACED THE R1 DOOR SLIDE ARMED WARNING PANEL INDICATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. ** (CLOSED)

Part: WARNING MESSAGE — ILLUMINATED (R1 DOOR) · airframe 57,092 hrs · 39,156 cycles

AIRCRAFT WAS NOT GROUNDED: UPON LANDING R1 DOOR OPEN INDICATION ON ECAM WITH DOOR CLOSED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LIGHT — DEFECTIVE (ZONE 800) · airframe 57,063 hrs · 39,133 cycles

AIRCRAFT WAS NOT GROUNDED: ON LANDING, R1 CABIN DOOR SHOWED OPEN ON ECAM AND DOOR PAGE. REPLACED INDICATOR LIGHT SLIDE ARMED

Part: PROXIMITY SENSOR — OUT OF ADJUST (ZONE 800) · airframe 57,051 hrs · 39,123 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER LANDING WHILE TAXING TO THE GATE GOT TWICE AN ECAM FORWARD CABIN DOOR OPEN (1R) AND SHOWING SLIDE ARM AND DOOR OPEN. FLIGHT ATTENDANT CONFIRMED DOOR WAS PROPERTLY CLOSE AND ARMED. MAINTENANCE ADJUSTED PROXIMITY SWITCHES PER AMM 52-71-00820-002-A. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (ZONE 800) · airframe 57,042 hrs · 39,118 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER LANDING, ECAM MESSAGE OF R1 DOOR OPEN, WHEN IT IS STILL CLOSED. CYCLED DOOR OPEN TO CLOSE, AND MESSAGE STILL APPEARS. MAINTENANCE ADJUSTED PROXIMITY SWITCHES PER AMM 52-71-00820-002-A. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 57,003 hrs · 39,085 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR ASSIST BOTTLE PRESSURE IS OUT OF RANGE. SERVICED L1 DOOR DAMPER PER AMM 52-10-00.

Part: RELAY — DEFECTIVE (ZONE 800) · airframe 57,003 hrs · 39,085 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR INDICATES OPEN WHEN IT'S CLOSED. MAINTENANCE REPLACED RELAY 12WN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 57,003 hrs · 39,085 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR ASSIST BOTTLE PRESSURE IS OUT OF RANGE. SERVICED L4 DOOR DAMPER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 57,003 hrs · 39,085 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR ASSIST BOTTLE PRESSURE IS OUT OF RANGE. SERVICED R4 DOOR DAMPER REF AMM 52-10-00.

Part: INDICATOR — FALSE INDICATION (ZONE 800) · airframe 57,003 hrs · 39,085 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR INDICATES OPEN WHEN IT'S CLOSED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)

Part: UNKNOWN — ODOR (CABIN) · airframe 56,745 hrs · 38,921 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED TRANSIENT SLIGHT PLASTIC SMELL THAT WAS DETECTED IN FRONT AND REAR CABIN DURING APPROACH. NO ODOR DETECTED IN FLIGHT DECK. (OPEN)

Part: ENCLOSURE — CONTAMINATED (APU BAY) · airframe 56,745 hrs · 38,921 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED TRANSIENT SLIGHT PLASTIC SMELL THAT WAS DETECTED IN FRONT AND REAR CABIN DURING APPROACH. NO ODOR DETECTED IN FLIGHT DECK. MAINTENANCE CLEANED THE APU COMPARTMENT AND THE APU INLET PER TASK CARD 26L00021002. A DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM WAS ACCOMPLISHED PER TASK CARD 26L00021014. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS / SMELL NOTED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 56,713 hrs · 38,899 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND L2 DOOR LOW ON BOTTLE ASSIST PRESSURE. SERVICED PASSENGER/CREW DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 56,713 hrs · 38,899 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND R2 DOOR LOW ON BOTTLE ASSIST PRESSURE. SERVICED PASSENGER/CREW DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 56,713 hrs · 38,899 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND R1 DOOR LOW ON BOTTLE ASSIST PRESSURE. SERVICED PASSENGER/CREW DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 56,713 hrs · 38,899 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND L1 DOOR LOW ON BOTTLE ASSIST PRESSURE. SERVICED PASSENGER/CREW DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: PROXIMITY SENSOR — WARNING MESSAGE (ZONE 800) · airframe 56,678 hrs · 38,880 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED RIGHT FORWARD CABIN DOOR SHOWS OPEN WHEN DOOR IS CLOSED. MAINTENANCE REPLACED PROXIMITY DETECTOR SWITCH 11WV2 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-11.

Part: PROXIMITY SENSOR — FALSE ACTIVATION (ZONE 800) · airframe 56,644 hrs · 38,857 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT ON TAXI IN TO AUS THE ECAM INDICATED RIGHT DOOR OPEN BUT THE DOOR WAS CONFIRMED CLOSED BY F;IGHT ATTENDANT. FLIGHT CREW REPORTED THAT CURRENTLY MESSAGE APPEARS TO BE INTERMITTENT. MAINTENANCE REPLACED R1 DOOR PROXIMITY DETECTOR SENSOR 11WV2 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-11.

Part: CONTACT — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,411 hrs · 38,691 cycles

AIRCRAFT WAS NOT GROUNDED: 22 AND 23 AISLE WAY EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW CONTACTS IN CANNON PLUG PER ESPM 20-48-25.

Part: ACCUMULATOR — LOW PRESSURE (SERVICE DOOR) · airframe 56,310 hrs · 38,626 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT SERVICE DOOR EMERGENCY CYLINDER / ACCUMULATOR NEEDS SERVICEING AT 1400 PSI SHOULD BE 1810 PSI. SERVICED AFT LEFT SERVICE DOOR EMERGENCY CYLINDER/ ACCUMULATOR

Part: ACCUMULATOR — LOW PRESSURE (PAX DOOR) · airframe 29,177 hrs · 12,001 cycles

AIRCRAFT WAS NOT GROUDNED: FORWARD LEFT SIDE ENTRY DOOR EMERGENCY CYLINDER / ACCUMULATOR NEEDS SERVICEING READING AT 1400 PSI SHOULD BE 1810 PSI. SERVICED FORWARD LEFT SIDE ENTRY DOOR.

Part: ACCUMULATOR — LOW PRESSURE (SERVICE DOOR) · airframe 56,310 hrs · 38,626 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT SERVICE DOOR EMERGENCY CYLINDER / ACCUMULATOR NEEDS SERVICEING AT 1400 PSI SHOULD BE 1810 PSI. SERVICED AFT RIGHT SERVICE DOOR EMERGENCY CYLINDER/ ACCUMULATOR

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 55,919 hrs · 38,354 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER LOW. SERVICED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: HINGE FITTING — WORN (NACELLE DOOR) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD SIDE FAN COWL CENTER HINGE FITTING ON PYLON WORN AT PYLON RIB 5. REPLACED HINGE FITTING PER SRM 51-42-11.

Part: HINGE FITTING — WORN (NACELLE DOOR) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD SIDE FAN COWL FORWARD HINGE FITTING ON PYLON WORN AT PYLON RIB 1. REPLACED HINGE FITTING PER SRM 51-42-11.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN. PERFORMED OPERATIONAL BITE TEST OF THE EPSU AND POWER UP TEST OF CIDS. REPLACED EPSU EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN.

Part: HANDLE — CRACKED (L SLIDING WINDOW) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER AMM 56-12-11.

Part: HANDLE — CRACKED (RT SLDING WINDOW) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER CMM 56-12-12.

Part: STRINGER — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER 42L BETWEEN FR 59 AND FR 60 IN THE AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER PER MSRM 53-41-13-300-010.

Part: FRAME — CRACKED (FRM 16) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FASTENER HOLE 6 AND FASTENER HOLE C IN THE DOUBLE JOGGLE AREA FOR DOOR STOP 7 AT FR 16 AND S10R. REPLACED FRAME PER EA 349690.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 AND S22R. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: BOTTLE — NO TEST (DOOR) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILS THE DAMPING FUNCTIONAL CHECK. **SUPPLEMENTAL REPORT FOR AALA202402203624: MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILS THE DAMPING FUNCTIONAL CHECK. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED DOOR STOP #1 INTERCOSTAL FITTING AT FR 16 AND S23R. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 232DF IN PASSENGER CABIN. REPLACED FLOOR PANEL 232D.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 262LG IN PASSENGER CABIN. REPLACED FLOOR PANEL 262 LG

Part: STRINGER — CORRODED (FRMS 30-34 S43L) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STR 43L BETWEEN FR 30 AND FR 34 ON FORWARD CARGO COMPARTMENT. PERFORMED TIME LIMITED REPAIR ON STRINGER PER EA 351071.

Part: SPIGOT — CORRODED (ZONE 400 - NAC/P) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON LOWER SPIGOT FITTING. MAINTENANCE REPLACED SPIGOT FITTING PER A319 SRM 54-51-12-300-001.

Part: SPIGOT — CORRODED (ZONE 400 - NAC/P) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON LOWER SPIGOT FITTING. MAINTENANCE REPLACED SPIGOT FITTING PER A319 SRM 54-51-12-300-001.

Part: BOLT — CORRODED (ZONE 500 SLAT) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #10 LOWER MID BOLT AT WS 11664 AND RIB 22. REPLACED BOLT PER TASK CARD 26C51057005.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK RIGHT HAND LATERAL POST WINDSHIELD FRAME UPPER ATTACHMENT BETWEEN FR 3 AND FR 8. REPLACED WINDSHIELD FRAME PER EA 349770.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK LEFT HAND LATERAL POST WINDSHIELD FRAME UPPER ATTACHMENT BETWEEN FR 3 AND FR 8. REPLACED WINDSHIELD FRAME PER EA 349770.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #2 UPPER AFT BOLT. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #3 LOWER BOLT. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #2 MID FORWARD BOLT. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #1 MID AFT BOLT. REPLACED BOLT PER TASK CARD 26C51057005.

Part: FLOORBEAM — NONE (ZONE 100 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BE ACCOMPLISHED PER EA 349911, ENGINEERING HAS REQUESTED THAT CABIN FLOOR BEAM AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 6 AT FR 36 AND -Y1292 BE REPAIRED AS OUTLINED IN THE EA INSTRUCTIONS SINCE IT WAS THE ONLY FLOOR BEAM IN THIS AREA THAT DID NOT HAVE DAMAGE DETECTED. MAINTENANCE REPAIRED FLOOR BEAM PER EA 349911.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK UPPER OUTBOARD SPLICE AT FR 66 AND -Y765. REPLACED SPLICE PER SRM 51-42-11.

Part: ANCHOR FITTING — CORRODED (WS 70) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / ANCHORAGE FITTING LOWER FACE BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND 3. REPAIRED ANCHORAGE FITTING PER SRM 57-26-13-300-025.

Part: STRINGER — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON DRY BAY ON STRINGER 3 BOTTOM SKIN UPPER SURFACE BETWEEN RIB 5 TO RIB 6 ON RIGHT HAND WING. PERFORMED PERMANENT REPAIR ON DRY BAY AREA UPPER SURFACE STRINGER PER EA 350576.

Part: FITTING — CORRODED (WS 70-141) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FITTING AREA UPPER AND LOWER SURFACES BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND 3. REPAIRED LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FITTING PER SRM 57-26-13-300-025.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON DRY BAY LOCATED BETWEEN RIB 5 TO RIB 6 BOTTOM SKIN UPPER SURFACE ON LEFT HAND WING. REPAIRED SKIN PER EA 350280.

Part: SHEAR PLATE — CRACKED (FRMS 69-70 S23L) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23L BETWEEN FR 69 AND FR 70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-42-11-801.

Part: FITTING — CRACKED (DOOR FRAME 16) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND DOOR STOP FITTING #7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FRMS 29-70) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23R BETWEEN FR 29 AND FR 70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-42-11-801.

Part: HINGE PIN — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #2 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C50027005.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED DOOR FRAME CUT OUT INTERNAL STRUCTURE AT FR 68 AND S8R. REPLACED FRAME PER SRM 51-42-11.

Part: HINGE PIN — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON HINGE PIN #4 AT WS 14057 AND RIB 26. REPLACED HINGE PIN PER AMM 27-14-41.

Part: BRACKET — WORN (LT WING TE FLAP) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE INBOARD FLAP INTERCONNECTING STRUT ATTACHMENT BRACKET ON FLAP WORN ALLOWING THE BEARING TO MIGRATE. MAINTENANCE REPLACED BRACKET PER SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENACE: CORROSION ON CABIN FLOOR PANEL 262BG SLEEVE. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: SKIN — CORRODED (FRMS30-34) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERNAL STRUCTURE ON SKIN LOCATED BETWEEN FR 30 AND FR 34 AND STR 42L AND STR 43L IN FORWARD CARGO COMPARTMENT. PERFORMED TIME LIMITED REPAIR ON INTERNAL STRUCTURE ON SKIN PER EA 351071

Part: FLOORBEAM — CRACKED (FRM 36) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 5 AT FR 36 AND -Y765. REPAIRED FLOOR BEAM PER EA 349911.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SUPPORT BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED FLOOR SUPPORT PER SRM 51-42-11.

Part: FRAME — CRACKED (FRM 35 S30L) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FACE AROUND FASTENER AT FR 35 AND S30L. REPAIRED FRAME PER EA 349944.

Part: FLOORBEAM — CRACKED (FRM 36) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 4 AT FR 36 AND -Y254. REPAIRED FLOOR BEAM PER EA 349911.

Part: PRESSURE DECK — CRACKED (FRM 36) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CENTER FUSELAGE LEFT HAND PRESSURE DECK PANEL CRACKED AT FR 36 BETWEEN +Y1292 AND +Y1523. REPAIRED PRESSURE DECK PANEL PER EA 349780.

Part: PRESSURE DECK — CRACKED (FRM 36) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CENTER FUSELAGE RIGHT HAND PRESSURE DECK PANEL CRACKED AT FR 36 AND -Y1292. REPAIRED PRESSURE DECK PANEL PER EA 349780.

Part: FLOORBEAM — CRACKED (FRM 36) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 3 AT FR 36 AND +Y254. REPAIRED FLOOR BEAM PER EA 349911.

Part: FLOORBEAM — CRACKED (FRM 36) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 2 AT FR 36 AND +Y765. REPAIRED FLOOR BEAM PER EA 349911.

Part: WINDOW FRAME — CRACKED (LEFT) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD LEFT HAND FRAME CENTER POST LOWER ATTACHMENT UPPER RADIUS BETWEEN FR 1 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME PER EA 349770.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CONTINUITY FITTING LOWER ATTACHMENT AREA ON THE LEFT-HAND SIDE. PERFORMED TIME REPAIR (REPLACED CONTINUITY FITTING LEFT-HAND SIDE LOCATED BETWEEN FR 1 TO FR 2 AND LEVEL OF Y0 PER EA 349770

Part: FLOORBEAM — CRACKED (RM 36) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 1 AT FR 36 AND +Y1292. REPAIRED FLOOR BEAM PER EA 349911.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK RIGHT HAND LATERAL POST WINDSHIELD FRAME LOWER ATTACHMENT BETWEEN FR 1 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME PER EA 349770.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK IN FORWARD GALLEY AREA LOCATED AT FR 21 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-72-11-911-001.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CONTINUITY FITTING LOWER ATTACHMENT AREA RIGHT-HAND SIDE. PERFORMED TIME LIMITED REPAIR (REPLACED CONTINUITY FITTING) RIGHT-HAND SIDE LOCATED BETWEEN FR 1 TO FR 2 AND LEVEL OF Y0 IAW EA349770

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 55,844 hrs · 38,308 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME HOLE D IN THE DOUBLE JOGGLE AREA OF DOOR STOP 7 AND FR 16 LEFT. REPAIRED FRAME PER EA 349691.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 55,600 hrs · 38,148 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE SKIN DEBONDED ON THE TRAILING EDGE AT RIB 10. REPAIRED FLAP PER EA 350159.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 55,416 hrs · 38,020 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 ATTACHMENT FITTING HINGE BOLT HAS AXIAL AND RADIAL MOVEMENT. REPLACED RUDDER HINGE #4 PER EA 5520Y001.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 55,416 hrs · 38,020 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 ATTACHMENT FITTING HINGE BOLT HAS AXIAL AND RADIAL MOVEMENT. REPLACED RUDDER HINGE #7 PER EA 5520Y001.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 55,416 hrs · 38,020 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 ATTACHMENT FITTING HINGE BOLT HAS AXIAL AND RADIAL MOVEMENT. REPLACED RUDDER HINGE #2 PER EA 5520Y001.

Part: POWER SUPPLY — DEFECTIVE (ZONE 200 - FUSE) · airframe 55,013 hrs · 37,766 cycles

AIRCRAFT WAS GROUNDED: OVERWING AIRCRAFT CENTER AND RIGHT EMERGENCY EXIT LIGHTS FLICKER IN ARMED POSITION. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-50-00.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 55,005 hrs · 37,759 cycles

AIRCRAFT WAS GROUNDED: FORWARD LEFT-HAND EMERGENCY POWER SUPPLY UNIT BATTERY INOPERATIVE. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: MOUNT — DEFECTIVE (ZONE 100 - FUSE) · airframe 55,005 hrs · 37,759 cycles

AIRCRAFT WAS GROUNDED: OVERWING EMERGENCY EXIT LIGHTS FLICKER IN ARMED POSITION IN FLIGHT. MAINTENANCE TROUBLESHOT PER TSM 33-51-00-810-819A AND REPLACED REPLACED DIODE MOUNT 1158VD. A SATISFACTORY OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED AND NO FLICKERING WAS NOTED.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 55,002 hrs · 37,757 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT SEATS 13, 14, 15 ILLUMINATED WHEN FLIGHT DECK SWITCH IS IN ARMED POSITION. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: RELAY — DEFECTIVE (ZONE 100 - FUSE) · airframe 54,997 hrs · 37,754 cycles

AIRCRAFT WAS GROUNDED: MID CABIN EMERGENCY EXIT LIGHT BLINKING. REPLACED RELAY 8WL PER FIM TASK 33-51-00-810-819-A11 AND ACCOMPLISHED A SATISFACTORTY OPERATIONAL CHECK.

Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 53,585 hrs · 36,845 cycles

AIRCRAFT WAS GROUNDED: FDURING DESCENT FLIGHT ATTENDANTS REPORTED A MELTING PLASTIC SMELL FROM AFT GALLEY. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE AFT GALLEY COFFEE MAKERS. (OPEN)

Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 53,585 hrs · 36,845 cycles

AIRCRAFT WAS GROUNDED: DURING DESCENT FLIGHT ATTENDANTS REPORTED A MELTING PLASTIC SMELL FROM AFT GALLEY. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE AFT GALLEY COFFEE MAKERS. AFT LEFT COFFEE MAKER AND THE AFT RIGHT COFFEE MAKER (AALA202301122638) PER AMM 25-35-15. ** (CLOSED)

Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 53,585 hrs · 36,845 cycles

AIRCRAFT WAS GROUNDED: DURING DESCENT FLIGHT ATTENDANTS REPORTED A MELTING PLASTIC SMELL FROM AFT GALLEY. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE AFT GALLEY COFFEE MAKERS. AFT LEFT COFFEE MAKER AND THE AFT RIGHT COFFEE MAKER PER AMM 25-35-15.

Part: O-RING — LEAKING (APU OIL COOLER) · airframe 53,322 hrs · 36,702 cycles

AIRCRAFT WAS GROUNDED: FUEL / FUME ODOR IN AFT GALLEY AREA. MAINTENANCE FOUND APU OIL COOLER TRANSFER TUBE O-RING LEAKING. REPLACED O-RING PER AMM 49-91-44 AND AMM 49-52-51. CLEANED APU INLET AND LOAD COMPRESSOR.

Part: UNKNOWN — ODOR (GALLEY) · airframe 53,322 hrs · 36,702 cycles

AIRCRAFT WAS GROUNDED: FUEL / FUME ODOR IN AFT GALLEY AREA. (OPEN)

Part: BOTTLE — LEAKING (HYD OVERFLOW) · airframe 53,227 hrs · 36,647 cycles

AIRCRAFT WAS GROUNDED: ON DECENT INTO BOS, FLIGHT ATTENDANTS REPORTED STRONG SMELL OF DIRTY SOCKS AND PLASTIC. SMELL.STARTED IN REAR OF AIRCRAFT AND CAME FORWARD, SMELL HAPPENED AROUND 600 FT WITH ENGINES ABOVE IDLE. MAINTENANCE FOUND THE HYDRAULIC SYSTEM OVERFLOW BOTTLE IN THE LEFT WHEEL WELL SPILLING HYDRAULIC FLUID ONTO THE FUSELAGE AND BEING INGESTED INTO THE APU INLET. MAINTENANCE PERFORMED A DECONTAMINATION OF THE PACKS ANDACCOMPLISHEE A SATISFACTORY OPERATIONAL CHECK WITH NO ODORS BEING NOTED.

Part: SLIDE — DEFECTIVE (ZONE 800 - DOORS) · airframe 53,193 hrs · 36,618 cycles

AIRCRAFT WAS NOT GROUNDED: DURING A SCHEDULED TIME CHANGE OF THE R1 DOOR SLIDE THE REPLACEMENT SLIDE WAS FOUND TO BE DEFECTIVE, CLASSIFIED AS BAD FROM STOCK AND THE ORIGINAL SLIDE WAS RE-INSTALLED ON THE AIRCRAFT PER TAKS CARD 26L00025010.

Part: APU — LEAKING (ZONE 100 - FUSE) · airframe 53,015 hrs · 36,483 cycles

AIRCRAFT WAS GROUNDED: ON DECENT, FLIGHT ATTENDANTS REPORTED BURNING RUBBER SMELL LOCALIZED IN BACK. CREW ACCOMPLISHED SMOKE/ FUMES CHECKLIST. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU WHICH WAS FOUND TO BE LEAKING OIL. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: OIL COOLER — LEAKING (ZONE 100 - FUSE) · airframe 53,015 hrs · 36,483 cycles

AIRCRAFT WAS GROUNDED: ON DECENT, FLIGHT ATTENDANTS REPORTED BURNING RUBBER SMELL LOCALIZED IN BACK. CREW ACCOMPLISHED SMOKE/ FUMES CHECKLIST. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU WHICH WAS FOUND TO BE LEAKING OIL. **SUPPLEMENTAL REPORT FOR AALA202210067912: MAINTENANCE FOUND THE APU OIL COOLER AND THE APU OIL COOLING FAN (AALA202210185553) LEAKING OIL AND REPLACED THEM PER AMM 49-91-44 AND AMM 49-52-51. A SATISFACTORY LEAK CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: COOLING FAN — LEAKING (ZONE 100 - FUSE) · airframe 53,015 hrs · 36,483 cycles

AIRCRAFT WAS GROUNDED: ON DECENT, FLIGHT ATTENDANTS REPORTED BURNING RUBBER SMELL LOCALIZED IN BACK. CREW ACCOMPLISHED SMOKE/ FUMES CHECKLIST. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU WHICH WAS FOUND TO BE LEAKING OIL. **ORIGINAL REPORT WAS AALA202210067912** MAINTENANCE FOUND THE APU OIL COOLER AND THE APU OIL COOLING FAN (AALA202210185553) LEAKING OIL AND REPLACED THEM PER AMM 49-91-44 AND AMM 49-52-51. A SATISFACTORY LEAK CHECK WAS ACCOMPLISHED.

Part: LOCK — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 52,966 hrs · 36,453 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR STICKS DIFICULT TO OPERATE. MAINTENANCE LUBRICATED DOOR LOWER LOCK PER AMM 12-22-52.

Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 51,753 hrs · 35,731 cycles

AIRCRAFT WAS GROUNDED: WHILE PERFORMING EMERGENCY LIGHT TEST RECEIVED EMERGENCY RIGHT BATTERY FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT AT RIGHT OVER WING EXIT DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 51,687 hrs · 35,688 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD OUTBOARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: DOOR — OUT OF POSITION (ZONE 800 - DOORS) · airframe 50,844 hrs · 35,169 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY (LEFT) DOOR IS STUCK. HARD TO MOVE. FOUND AFT LAVATORY LEFT DOOR OUT OF TRACK. RE SECURE DOOR PER AMM 25-40-00.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 50,095 hrs · 34,699 cycles

AIRCRAFT WAS GROUNDED: REPORT OF A STRONG ELECTRICAL BURNING SMELL AROUND ROW 10. AFTER A SHORT PERIOD SMELL DISSIPATED AND NOTICED SEATS 10 DEF POWER PORTS ALL HAVE RED LIGHTS SHOWING. ACCOMPLISHED SMOKE ODOR FUME JOB CARD 26L00021001. SEAT 10 DEF POWER SUPPLY IDENTIFIED AS SOURCE. REPLACED POWER SUPPLY PER AMM 25-21-38.

Part: DOOR — FOD (R2) · airframe 49,471 hrs · 34,361 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 2R DIFFICULT TO ARM DISARM. REMOVED DEBRIS AND SERVICED DOOR 2R PER MM 53-13-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 49,322 hrs · 34,286 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT EMERGENCY EXIT LIGHT POWER SUPPLY UNIT FAILS B.I.T.E. TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT EMERGENCY POWER SUPPLY UNIT (AALA202104189002) AND BATTERY (AALA202104199038) IAW AMM 33-51-38-0401.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 49,322 hrs · 34,286 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT EMERGENCY EXIT LIGHT POWER SUPPLY UNIT FAILS B.I.T.E. TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT EMERGENCY POWER SUPPLY UNIT (AALA202104189002) AND BATTERY (AALA202104199038) IAW AMM 33-51-38-0401.

Part: APU — LEAKING (ZONE 100) · airframe 49,196 hrs · 34,220 cycles

AIRCRAFT WAS GROUNDED: FAINT DIRTY SOCK ODOR STRONGER ON LANDING WHEN FLAPS DEPLOYED.STRONGER WHEN PACK 1 ONLY. REPLACED APU DUE TO OIL LEAK AND INGESTION PER TASK CARD 28L31049003.

Part: PIPE — BROKEN (EXTINGUISHER) · airframe 49,112 hrs · 34,153 cycles

AIRCRAFT WAS GROUNDED: #2 ENGINE REAR FIRE EXTINGUISHING DISCHARGE NOZZLE PIPE BROKEN / SHEARED OFF AT THE "Y" JUNCTION. REPLACED PIPE PER AMM 26-11-49

Part: PRESSURE SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 49,946 hrs · 34,618 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CABIN PRESSURE DETECTION PRESSURE SWITCH HOUSING CRACKED AND LEAKING. FIN (14WN). REMOVED AND REPLACED, INSTALLED FLEX LINE ON SWITCH (14WN) SWITCH LEAKING, REMOVED SWITCH (BAD FROM STOCK) PER AMM 52-73-12.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 48,463 hrs · 33,823 cycles

AIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED TEST. REPLACED BATTERY, PER AMM 33-51-38.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 47,227 hrs · 33,123 cycles

AIRCRAFT WAS GROUNDED: DURING CARGO INSPECTION FOR PS CHECK FOUND FLOOR PANEL 151CE DELAMINATED AND CONCAVED AFT CARGO. REPLACED FLOOR PANEL PER AMM 53-42-14.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,673 hrs · 32,303 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORTED DIRTY SOCK SMELL SHORTLY AFTER TAKE OFF AND DISSIPATING RAPIDLY BUT RETURNING FROM DESCENT UNTIL LANDING. MAINTENANCE FOUND APU TO BE SOURCE OF ODOR. MAINTENANCE REPORTS APU IS CLEAN AND DRY, NO LEAKS FOUND , NO OIL COMING FROM WITNESS DRAIN. APU WAS INSTALLED MAY 18. RAN APU AND #1 , #2 PACKS WITH BLEED AIR, NO SMELL NOTED. APU RETURNED TO SERVICE.

Part: APU — LEAKING (APU BAY) · airframe 45,039 hrs · 31,949 cycles

AIRCRAFT WAS GROUNDED: FA REPORTED DIRTY SOCK SMELL 30 MINUTES INTO FLIGHT, CLIMBING OUT OF LAX. SICKENING SWEET SMELL. APU ON MEL. MAINTENANCE ACCOMPLISHED CARD 26L0021002, NO FINDINGS. J/C 26L0021004 REQUIRES ACCOMPLISHMENT. DEFERRED DUE TO LT. SUPPLEMENTAL INFORMATION: MAINTENANCE FOUND EVIDENCE OF OIL AND CARBON DEPOSITS AT APU LOAD COMPRESSOR CAVITY DRAIN BELLOWS ON RT APU ACCESS DOOR. MAINTENANCE REMOVED AND REPLACES THE APU IAW JOB CARD 26L31049003. ACCOMPLISHED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM IAW JC 26L00021004. (CLOSED)

Part: LIFE LINE — MISSING (LEFT SIDE) · airframe 43,429 hrs · 31,018 cycles

ESCAPE LIFE LINE WAS MISSING ON THE LEFT SIDE. MAINTENANCE REPLACED THE LIFE LINE IAW 25-66-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 43,054 hrs · 30,788 cycles

THE EXIT SIGN LENS DETACHED AT THE RIGHT AFT DOOR. REPLACED THE SIGN LENS. OK FOR SERVICE.

Part: PIN — WORN (LT MLG) · airframe 41,134 hrs · 29,731 cycles

AIRCRAFT IN BASE MAINTENANCE: WEAR ON LEFT MAIN LANDING GEAR RETRACTION ACTUATOR, MAIN LANDING GEAR FITTING, PIN. REPLACED LEFT RETRACTION ACTUATOR MAIN LANDING GEAR PIN PER JOBCARD 26C73032004.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 41,134 hrs · 29,731 cycles

LEFT ELEVATOR TOP SKIN HAS INDICATION OF WATER INGRESS 1" DIAMETER 23" FROM T/E, 31.5" FROM INBD END. REPAIRED ELEVATOR SKIN IAW SRM 55-21-11-300-004.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 41,134 hrs · 29,731 cycles

LEFT ELEVATOR TOP SKIN HAS INDICATION OF WATER INGRESS, 1" DIAMETER,20" FROM T/E, 43" FROM INBD END. REPAIRED ELEVATOR SKIN PER SRM 55-21-11-300-004.

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 41,134 hrs · 29,731 cycles

CORROSION WAS FOUND ON FLOORBEAM AT FR 16, BL 0, Y1292. REPLACED THE FLOORBEAM IAW SRM 53-11-14.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 41,134 hrs · 29,731 cycles

CORROSION FOUND ON THE RIGHT FLOORBEAM AT STATION Y-1292, FRAME 66. REMOVED AND INSTALLED NEW IAW SRM 51-72-11/51-42-11.

Part: PLATE — CORRODED (FRAME 66) · corrosion level 2 · airframe 41,134 hrs · 29,731 cycles

CORROSION ON SILL PLATE FORWARD SPLICE AT STRINGER 23R, FRAME 66. REPLACED THE SILL PLATE IAW SRM 53-41-14.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 41,134 hrs · 29,731 cycles

CORROSION ON THE DOOR SILL AT -Y1589 AND FR 68. REPAIRED THE DOOR SILL IAW SRM 53-41-14-300, AND SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 41,134 hrs · 29,731 cycles

CORROSION AROUND NUTCLIP HOLE ON FLOORBEAM. REPAIRED FLOORBEAM IAW SRM 51-42-11, AND 53-41-14-300-001.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 41,134 hrs · 29,731 cycles

CORROSION FOUND ON THE L2 DOOR CUTOUT CENTER SILL SHAPE FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-11.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 40,303 hrs · 29,279 cycles

EMERGENCY POWER SUPPLY UNIT 11WL BY THE LEFT OVERWING ESCAPE HATCH SHOWED FAULTS DURING TEST. RESET EPSU IAW AMM 33-51-00. OPERATIONAL CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 40,145 hrs · 29,200 cycles

R2 DOOR EXIT COVER MISSING OFF THE EMERGENCY LIGHT. REPLACED THE LENS.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 39,397 hrs · 28,767 cycles

THERE WAS A LIGHT HYDRAULIC ODOR IN AFT GALLEY AND A FAINT ODOR IN THE COCKPIT. WHEN APU BLEED WAS TURNED OFF, THE ODOR DISSIPATED. FAINT ODOR RETURNED WHEN APU BLEED TURNED ON FOR ENGINE START, BUT DISSIPATED WHEN PACKS TURNED OFF FOR START. INCREASING HYDRAULIC ODOR OCCURRED WITH INCREASING ENGINE POWER TO LINE UP ON RUNWAY (APU WAS OFF). POWER BROUGHT UP TO 50% N1 FOR ABOUT 20 SECONDS. HYDRAULIC ODOR CONTINUED TO INCREASE IN INTENSITY. TAXIED BACK TO GATE FEELING CABIN AND COCKPIT ENVIRONMENT WAS UNSAFE TO BREATH. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED JC 26L00021001 AND FOUND APU TO BE SOURCE OF ODOR. MAINTENANCE ACCOMPLISHED JCS 26L00021002 AND 26L00021004 AND SATISFACTORY OPS CHECK WAS ACCOMPLISHED WITH NO EVIDENCE OF AN ODOR OR CONTAMINATION IN THE APU AREA.

Part: CONNECTOR — CONTAMINATED (ZONE 100 - FUSE) · airframe 39,195 hrs · 28,650 cycles

NOSE WHEEL STEERING FAULT, EMERGENCY WAS DECLARED AND RETURNED TO DEPARTURE. AIRCRAFT GROUNDED. FOUND EVIDENCE OF WATER ON NOSE WHEEL ELECTRICAL CONNECTOR CLEANED AND DRIED ELECTRIC CONNECTOR OF THE NOSE WHELL STEERING FOUND NO EVIDENCE OF CORROSION .

Part: CONTROL SERVO — FAILED (NLG STEERING) · airframe 39,195 hrs · 28,651 cycles

FLIGHT CREW REPORTED NOSE WHEEL STEERING FAULT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW; WHERE IT LANDED WITHOUT FURTHER INCIDENT AND TOWED TO GATE. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED NOSE WHEEL STEERING SERVO- CONTROL (6GC) AND THE NOSE WHEEL STEEERING FEED BACK SENSOR 4GC.

Part: SENSOR — DEFECTIVE (NLG STEERING) · airframe 39,195 hrs · 28,651 cycles

FLIGHT CREW REPORTED NOSE WHEEL STEERING FAULT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT AND AIRCRAFT WAS GROUNDED. REPLACED THE NOSE WHEEL STEERING SERVO CONTROL 6GC AND THE NOSE WHEEL STEEERING FEED BACK SENSOR 4GC.

Part: STARTER — MALFUNCTIONED (NR 1 ENGINE) · airframe 37,436 hrs · 27,725 cycles

AIRCRAFT WAS GROUNDED. WHILE STARTING NR 1 ENGINE, ECAM ENG 1 FAULT, ENG 1 STALL AND THE GROUND CREW OBSERVER REPORTED SMOKE AND SPARKS. MAINTENANCE REPLACED THE NR 1 ENGINE STARTER AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 80-11-10-000-002-A.

Part: LENS — MISSING (ZONE 800) · airframe 37,330 hrs · 27,665 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR EXIT LENS MISSING. INSTALLED MISSING EXIT LIGHT LENS AT R2 DOOR AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-00-710-007-A.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 37,145 hrs · 27,575 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM UPPER FLANGE, AFT FASTENER HOLE HAS CRACK INDICATION AT FRAME 43 & -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 37,145 hrs · 27,575 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM UPPER FLANGE AFT FASTENER HOLE HAS CRACK INDICATION AT FRAME 43 & +Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 36,928 hrs · 27,479 cycles

RETURNED & ACFT WAS GNDED. AFTER TAKEOFF VERY STRONG ODOR IN COCKPIT & CABIN. A FLIGHT ATTENDANT REPORTED A POSSIBLE SMOKE SMELL & RETURNED. COMPLETED JC 26L00021001TROUBLESHOOTING CABIN AIR QUALITY, 26L0021004 DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYS A319 20 21 ENGS, APU & JC 26L0021005 CABIN ODOR TROUBLESHOOTING & FOUND NO ODOR PRESENT. RETURNED THE ACFT BACK TO SERVICE.

Part: ENGINE — STALLED (NR 1) · airframe 36,928 hrs · 27,478 cycles

AIRCRAFT WAS GNDED. NR 1 ENG STALLED AT FL 350. NOISE & VIBRATION FELT & POWER REDUCED ON ITS OWN TO APPROX 50%. POWER WAS REDUCED TO IDLE & ENG IDLED NORMALLY. ENG SURGED & STALLED TWICE BEFORE POWER WAS BROUGHT TO IDLE. FLIGHT CREW DECLARED AN EMER, LANDED SAFELY & TAXIED TO THE GATE. REPLACED THE LT ENG IAW TASK CARD 26L40071001.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,669 hrs · 26,849 cycles

FORWARD FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,741 hrs · 26,305 cycles

FORWARD EMER FLASHLIGHT INOPERATIVE. REPLACED BATTERY FWD EMER FLASHLIGHT.

Part: WINDOW SHADE — STUCK (CABIN) · airframe 34,676 hrs · 26,263 cycles

WINDOW 9A SHADE STUCK IN CLOSED POSITION. REPLACED WINDOW SHADE FAIRING ASSEMBLY AT ROW 9 LT. OPERATIONS CHECKED GOOD AMM 25-23-43. NEF 25-20G, CONTROL 0223N30 CLEARED. ITEM CLEARED ON MICS.

Part: SLIDING WINDOW — LACK OF LUBE (COCKPIT) · airframe 34,593 hrs · 26,222 cycles

FIRST OFFICER`S SLIDING WINDOW WILL NOT OPEN, HAVE TO PUSH EXCESSIVELY OUTWARD ON THE HANDLE TO RELEASE THE BUTTON. LUBED & ADJUSTED SLIDING WINDOW ASSEMBLY IAW MM 56-12-11-400-001-A.

Part: SHADE — STUCK (CABIN) · airframe 34,529 hrs · 26,196 cycles

WINDOW SHADE AT 10 A WILL NOT RETRACT. R & R LT EMER WINDOW SHADE IAW AMM 52-21-11-000-001-A & 52-21-11-400-001-A PLUS EMER EXIT HATCH IAW AMM 56-31-17-000-001-A & 56-31-17-400-001-A. OPERATIONS CHECKED GOOD.

Part: DAMPENER — INOPERATIVE (L1 DOOR)

FOUND L1 DOOR DAMPER INOPERATIVE. REPLACED THE L1 DOOR DAMPER.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 33,754 hrs · 25,779 cycles

DOOR 2L IS HARD TO ARM. REMOVED DEBRIS FROM UNDER GIRT BAR AT DOOR 2L.

Part: FITTING — CRACKED (HYDRAULIC LINE) · airframe 32,654 hrs · 25,165 cycles

DIRTY SOCKS ODOR DURING TAKEOFF, DESCENT & LANDING ONLY IN THE REAR OF THE AIRPLANE. ACCOMPLISHED TROUBLESHOOTING. FOUND GREEN SYS HYD RETURN LINE FOR SERVO CONTROL ALUMINUM FITTING CRACKED, LOCATED BEHIND WATER TANK, INSULATION BLANKETS SOAKED WITH SKYDROL. REPLACED FITTING & BLANKETS OPERATIONS & LEAK CHECKED OK. ALSO ACCOMPLISHED JOB CARD 26L00021004 DECONTAMINATION OF THE ECS.

Part: ATTACH FITTING — DIRTY (L1 DOOR) · airframe 30,771 hrs · 23,859 cycles

THE 1L DOOR ARMING LEVER IS BINDING. CLEANED GIRT BAR ATTACH POINTS, OK FOR SERVICE.

Part: O-RING — LEAKING (ENGINE) · airframe 30,296 hrs · 23,492 cycles

STRONG ODOR IN ACFT DURING TAKEOFF, DESCENT AND LANDING. DESCRIBED AS A SOUR ODOR. MAINTENANCE TROUBLESHOT CABIN AIR QUALITY AND JC 26L00021004, DECONTAMINATION OF ENVIRONMENTAL CONTROL SYS. FOUND SOURCE OF ODOR TO BE THE NR 2 ENGINE LPT SHAFT SEAL. REPLACED LPT PLUG O-RING IAW AMM 72-55-00-960-002-A. NO EVIDENCE OF OIL LEAK NOTED AFTER ENGINE RUN.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 29,930 hrs · 23,182 cycles

MX REPORTED THE EMERGENCY LIGHT LENS MISSING AT ROW 12L. MX REPLACED EMERGENCY LIGHT LENS AT ROW 12L. OK FOR SERVICE.

Part: LENS — MISSING (L2 DOOR) · airframe 29,895 hrs · 23,149 cycles

EXIT LIGHT LENS AT L2 DOOR CAME OFF. REPLACED EXIT LIGHT LENS AT L2 DOOR .

Part: COVER — MISSING (CABIN) · airframe 29,407 hrs · 22,769 cycles

MX REPORTED 1C EMERGENCY LIGHT COVER MISSING. MX REPLACED 1C EMERGENCY LIGHT COVER. REFERENCE AMM 33-50-00.

Part: COVER — UNSECURE (CABIN) · airframe 29,105 hrs · 22,528 cycles

MAINTENANCE REPORTED 1L DOOR LOWER EMERGENCY EXIT LIGHT COVER NEEDS TO BE RESECURED. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT COVER.

Part: MOUNT BOLT — LOOSE (HYDRAULIC PUMP) · airframe 29,006 hrs · 22,456 cycles

STRONG ODOR/FUMES REPORTED BY ALL FOUR FLIGHT ATTENDANTS AFTER TAKEOFF. STRONGEST IN AFT CABIN, WEAKER IN FRONT. RETURNED TO CLT SHORTLY AFTER TAKEOFF. NO EMERGENCY DECLARED. CREW AND PASSENGERS DEPLANED ON GATE ARRIVAL. MAINTENANCE ACCOMPLISHED CABIN ODOR JOB. FOUND THE NR 1 ENGINE HYDRAULIC PUMP LEAKING AT MOUNTING BOLTS. SECURED BOLTS. NO LEAKS NOTED. NO ODOR NOTED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 28,931 hrs · 22,401 cycles

MAINTENANCE REPORTED THE AFT LEFT FLIGHT ATTENDANT FLASHLIGHT INOP AND MOUNT BRACKET BROKEN. MAINTENANCE REPLACED AFT LEFT FLIGHT ATTENDANT FLASHLIGHT BATTERY AND MOUNT BRACKET. CHECKED OK. REFERENCE AMM 25-65-53.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 28,779 hrs · 22,280 cycles

CREW REPORTED THE EMERGENCY FLASHLIGHT, AFT AIRCRAFT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BATTERY. OPS CHECK NORMAL.

Part: BOTTLE — LOW PRESSURE (ENTRY DOOR) · airframe 27,646 hrs · 21,471 cycles

IFE MOD - AFT LEFT ENTRY DOOR EMERGENCY CYLINDER ACCUMULATOR PRESSURE IS LOW READS 1625 PSI AT 72 F. SERVICED AFT LEFT ENTRY DOOR EMERGENCY CYLINDER ACCUMULATOR BOTTLE IAW A319 AMM 52-10-00-614-001.

Part: TRANSMITTER — FAULTY (OIL SYSTEM) · airframe 26,898 hrs · 20,915 cycles

IN-FLIGHT AT 11,000 FT ENGINE NR 1 OIL QUANTITY WENT TO LESS THAN 3 QUARTS, 5 MINUTES LATER, WENT TO 12 QUARTS. DECLARED EMERGENCY. REMOVED AND REPLACED NR 1 OIL QUANTITY TRANSMITTER PER AMM 79-31-15-400. OPS CHECKED GOOD.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - CRACK IN SEGMENT 1 AT RIGHT OVERWING EMERGENCY EXIT DOOR BETWEEN FR40 TO FR41. REPLACED SEGMENT 1 AT RIGHT OVERWING EMERGENCY EXIT DOOR IAW EO 5210Y228.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR65 TO FR66, Z-500, -Y1732. REPLACED FLOOR SUPPORT BETWEEN FR65 TO FR66, Z-500, -Y1732 IAW SRM 51-72-11.

Part: CYLINDER — LEAKING (ZONE 800) · airframe 26,588 hrs · 20,700 cycles

2S CHECK - L2 DOOR DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE GAUGE LEAKING FLUID. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER A319 AMM 52-13-13-400.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR21, -Y1292. REPLACED FLOORBEAM AT FR21, -Y1292 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR24, S23L, Z-500, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR24, S23L, Z-500, Y254 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR24, Z-500, -Y1292. REPLACED FLOORBEAM BETWEEN FR20 TO FR24, Z-500, -Y1292 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON R2 DOOR CENTER SILL SHAPE BETWEEN FR66 TO FR68, Z-500, -Y1589. REPLACED R2 DOOR CENTER SILL SHAPE BETWEEN FR66 TO FR68, Z-500, -Y1589 IAW SRM 51-72-11 & DRAWING 53480505.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, -Y1292. REPLACED FLOORBEAM AT FR16, -Y1292 IAW A319 SRM 51-72-11.

Part: SHEAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON LATERAL SHEAR WEB BETWEEN FR69 TO FR70, Z-500, Y1162.5. REPLACED LATERAL SHEAR WEB BETWEEN FR69 TO FR70, Z-500, Y1162.5 IAW SRM 53-41-14.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON DOOR SILL BETWEEN FR66 TO FR68, Z-500, -Y1589. REPLACED DOOR SILL BETWEEN FR66 TO FR68, Z-500, -Y1589 IAW AIRBUS DRAWING D53480505.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR68, -Y765. REPLACED FLOORBEAM AT FR68, -Y765 IAW 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Z-500, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Z-500, Y1292 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN FR66 TO FR67, Z-500, -Y1292. REPLACED FLOOR SUPPORT BETWEEN FR66 TO FR67, Z-500, -Y1292 IAW SRM 51-72-11 & 51-42-00.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON L2 DOOR CENTER SILL SHAPE BETWEEN FR66 TO FR68, Z-500, Y1589. REPLACED L2 DOOR CENTER SILL SHAPE BETWEEN FR66 TO FR68, Z-500, Y1589 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN FR66 TO FR67, Z-500, -Y1292. REPLACED FLOOR SUPPORT BETWEEN FR66 TO FR67, Z-500, -Y1292 IAW SRM 51-72-11 & 51-42-00.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON L2 DOOR SILL PLATE BETWEEN FR66 TO FR68, Z-500, Y1589. REPLACED L2 DOOR SILL PLATE BETWEEN FR66 TO FR68, Z-500, Y1589 IAW SRM 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, -Y1292. REPLACED FLOORBEAM AT FR20, -Y1292 IAW A319 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,583 hrs · 20,696 cycles

S2 CHECK, LEVEL 2 EXFOLIATION CORROSION ON RIGHT SHEAR TIE BETWEEN FR69 TO FR70, Z-500. REPLACED RIGHT SHEAR TIE BETWEEN FR69 TO FR70, Z-500 IAW SRM 53-41-14.

Part: LIGHT — BROKEN (CABIN) · airframe 25,061 hrs · 19,572 cycles

EMERGENCY ESCAPE PATH LIGHT AT ROW 4C & 20C BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTS (SEATS) AT ROW 4C AND 20C. OPERATIONAL CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 23,623 hrs · 18,489 cycles

FLT 2024 - DCA-BOS - EMERGENCY LANDING - NOTICED ENGINE NR 1 LOSING OIL QUANTITY. DECLARED EMERGENCY LANDING. REMOVED AND REPLACED ENGINE NR 1 PER JOBCARD 26L40071001. WILL FURNISH ROOT CAUSE INFORMATION UPON RECEIPT OF TEARDOWN REPORT.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 22,045 hrs · 17,266 cycles

FLT 751 - BOS - EEL - EMERGENCY EXIT LIGHT (LOWER) AT L-1 DOOR INOPERATIVE. MAINTENANCE REPLACED LOWER EMERGENCY EXIT LIGHT HOUSING AT L-1 DOOR.

Part: CONCENTRATOR — FAULTY (COCKPIT) · airframe 20,346 hrs · 15,960 cycles

FLT 1928 - RSW-PHL - FUMES - FLIGHT WARNING SYSTEM (FWS) SYSTEM DATA ACQUISITION CONCENTRATOR (SDAC) 1 FAULT. ELECTRICAL FUMES MOMENTARY. REMOVED AND REPLACED SDAC 1 PER TASK 31-55-34-400-001. OPERATIONAL CHECK WAS GOOD.

Part: CONCENTRATOR — FAULTY (CABIN) · airframe 20,212 hrs · 15,834 cycles

FLT 2030 - DCA - BOS - EMERGENCY EQUIPMENT - LEFT OVERWING SLIDE INDICATES DISARMED WHEN ALL DOORS CLOSED AND ARMED. ARMING L2 DOOR DISARMS LEFT OVERWING EXIT. REMOVED AND REPLACED SYSTEM DATA ACQUISITION CONCENTRATOR (SDAC) NR 1 PER MAINTENANCE MANUAL 31-55-34-000. OPERATIONAL CHECK WAS GOOD.

Part: COMPUTER — MALFUNCTIONED (BLEED AIR SYS) · airframe 19,947 hrs · 15,653 cycles

FLT 1485 - SFO-PIT - EMERGENCY LANDING - LOST BOTH BLEEDS AND PACKS. REMOVED AND REPLACED NR 1 AND NR 2 BLEED MONITORING COMPUTER (BMC). ACCOMPLISHED OPERATIONAL TEST OF BLEED AIR SYSTEM ON ENGINE RUN. OPERATIONAL TEST WAS GOOD.

Part: COMPUTER — INOPERATIVE (BLEED AIR SYS) · airframe 19,947 hrs · 15,653 cycles

FLT 1485 - SFO-PIT - EMERGENCY LANDING - LOST BOTH BLEEDS AND PACKS. REMOVED AND REPLACED NR 1 AND NR 2 BLEED MONITORING COMPUTER (BMC). ACCOMPLISHED OPERATIONAL TEST OF THE BLEED AIR SYSTEM ON ENGINE RUN. OPERATIONAL TEST WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,480 hrs · 15,301 cycles

FLT 1611 - CLT-LGA - EMERGENCY LIGHTS - EMERGENCY POWER SUPPLY UNIT (ESPU) BATTERY FAULT LEFT MID CABIN. REMOVED AND REPLACED LEFT MID EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

EEL-FLASHLIGHT "A" F/A JUMP SEAT NEEDS NEW BATTERY. REMOVED AND REPLACED BATTERY AND SAFETY STRAP. OPS CHECK WAS GOOD. (K)

Part: LINE — LEAKING (HYDRAULIC SYS)

CLT FLT 1667, EN ROUTE DCA - CLT. DURING DESCENT THROUGH FL 200, THE AIRCRAFT LOST THE GREEN SYSTEM HYDRAULIC PRESSURE. THE CREW FOLLOWED ECAM PROCEDURES AND COMPLIED WITH THE GRAVITY EXTENSION OF THE LANDING GEAR. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE HYDRAULIC PUMP CASE DRAIN LINE DUE TO A HOLE. SERVICED THE GREEN HYDRAULIC SYSTEM, AND RESET THE GRAVITY GEAR EXTENSION HANDLE, SYSTEM OK FOR SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 11,931 hrs · 11,931 cycles

RIGHT SILL PLATE (FWD END) AT FR 66 CORRODED. REMOVED CORRODED AREA & INSTALLED DOUBLER PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 X 1 INCH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 11,931 hrs · 11,931 cycles

FRAME 16 & Y254 CORRODED. INSTALLED REPAIR ANGLES & FILLER IAW SRM 53-11-14, FIG 204; CORR TASK JA-220-53500; LEVEL 1 DEFECT SIZE: 1 INCH DIA.

Part: PSU — INOPERATIVE (EMERGENCY LIGHT)

BOS - THE LEFT EMERGENCY LIGHT POWER SUPPLY FAULTED DURING TEST. MAINTENANCE REPLACED THE LEFT, MID CABIN EMERGENCY POWER SUPPLY UNIT. OPS CHECKS OK. (M)

Part: RELEASE CABLE — INCORRECT (EVAC SLIDE)

BOS - THE AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

LGA - FOUND THE RIGHT EPSU BATTERY DEAD. MAINTENANCE REPLACED THE RIGHT EPSU BATTERY. (M)

Part: ODOR — DETECTED (CABIN)

BOS - FLT 6402 - EN ROUTE DCA-BOS - DURING APPROACH TO BOS, NOTICED ELECTRICAL LIKE FUMES COMING FROM BOTH FORWARD AND REAR GALLEY AREAS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATED ALL ELECTRICAL SYSTEM. ALSO, VISUALLY CHECKED RELAYS AND ELECTRICAL CONNECTIONS IN OVERHEAD GALLEY AREAS. NO FAULTS WERE FOUND. OK FOR SERVICE. (M)