N804AW

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 78,660 hrs · 37,264 cycles

AIRCRAFT WAS GROUNDED: EPSU AFT LEFT FAULT BATT MESSAGE WHILE ACCOMPLISHING OPERATIONAL TEST OF THE EMERGENCY LIGHTS. MAINTENANCE REPLACED THE EPSU BATTERY FOR THE AFT LEFT EPSU IAW AMM 33-51-38.

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 78,660 hrs · 37,264 cycles

AIRCRAFT WAS GROUNDED: EPSU FWD LEFT FAULT BATT MESSAGE WHILE ACCOMPLISHING OPERATIONAL TEST OF THE EMERGENCY LIGHTS. MAINTENANCE REPLACED THE EPSU BATTERIES FOR THE FWD LEFT EPSU IAW AMM 33-51-38.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 78,004 hrs · 36,844 cycles

AIRCRAFT WAS NOT GROUNDED: R2 WITH CYLINDER PRESSUREIS LOW. SERVICED R2 PAX DOOR IAW AMM 52-10-00.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 78,004 hrs · 36,844 cycles

AIRCRAFT WAS NOT GROUNDED: AFT UPPER EMERGENCY EXIT SIGN HAS HALF OF THE LIGHTS INOPERATIVE. REPLACED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-17.

Part: BOTTLE — READS LOW (ZONE 800) · airframe 77,309 hrs · 36,405 cycles

AIRCRAFT WAS NOT GROUNDED: L2 AFT PASSENGER DOOR EMERGENCY CYLINDER ACCUMULATOR BELOW PSI MINIMUMS. ACCOMPLISHED SERVICING OF THE L2 PASSENGER DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-001-A.

Part: BOTTLE — READS LOW (ZONE 800)

AIRCRAFT WAS NOT GROUNDED: R2 AFT PASSENGER DOOR EMERGENCY CYLINDER ACCUMULATOR BELOW PSI MINIMUMS. ACCOMPLISHED SERVICING OF THE R2 PASSENGER DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-001-A.

Part: PROXIMITY SENSOR — FAULTED (ZONE 700) · airframe 77,078 hrs · 36,263 cycles

AIRCRAFT WAS GROUNDED: ON TAKE OFF NOSE WHEEL DID NOT RETRACT CORRECTLY. FOLLOWING ECAM PROCEDURE WE RECYCLED THE LANDING GEAR. GEAR RETRACTED NORMALLY ON SECOND ATTEMPT. DECESION WAS MADE TO RETURN TO PHL. MAINTENANCE T/S PER TSM 32-31-00-810-842-A. FOUND PROX SENSOR 24GA TO BE FAULTY. REPLACED PROX SENSOR 24 GA IAW AMM 32-31-73.

Part: SKIN — CONTAMINATED (ZONE 300) · airframe 77,023 hrs · 36,221 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR FAILED THERMOGRAPHIC INSPECTION DUE TO SHOWING SIGNS OF MOISTURE ON THE UPPER SURFACE INBOARD OF ELEVATOR RIB 4 AND INBOARD OF ELEVATOR RIB 10. MAINTENANCE REPLACED THE RIGHT HAND ELEVATOR PER TASK CARD 26L30027001.

Part: FITTING — CRACKED (ZONE 700 DOOR) · airframe 77,023 hrs · 36,221 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR AFT DOOR ACTUATOR FITTING CRACKED. REPLACED FITTING PER EA 358779.

Part: RADAR — INTERMITTENT (WX SYS) · airframe 76,066 hrs · 35,583 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO DCA DUE TO THE FLIGHT CREW REPORTING THAT ENROUTE INTO DCA DURING IMC CONDITIONS AT FL040 NEAR VAAL I INTERSECTION, THE WEATHER RADAR BECAME INTERMITTENT AND THEN UNUSABLE. THE AIRCRAFT LANDED SAFELY AT DCA WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE WEATHER RADAR CIRCUIT BREAKER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE WEATHER RADAR SYSTEM PER AMM 34-41-00 WITH NO ISSUES NOTED.

Part: SLIDING WINDOW — LACK OF LUBE (ZONE 200 - FUSE) · airframe 75,898 hrs · 35,461 cycles

AIRCRAFT WAS NOT GROUNDED: L2 SLIDING WINDOW IS DIFFICULT TO OPEN. ACCOMPLISHED SLIDING WINDOW LUBRICATION PER AMM 12-22-56.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 74,716 hrs · 34,729 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB AT FR 68 AND S22L. REPAIRED FRAME PER EA 349057

Part: PROXIMITY SENSOR — LOOSE (ZONE 800 - DOORS) · airframe 73,705 hrs · 34,096 cycles

AIRCRAFT WAS NOT GROUNDED: DURING FLIGHT ECAM MESSAGE DOOR RIGHT EMERGENCY EXIT LIGHT CAME ON INTERMITTENTLY 3 TIMES. OVER WING EXIT RIGHT CURRENTLY LIGHT IS OUT. MAINTENANCE FOUND RIGHT HAND EMERGENCY EXIT PROXIMITY DETECTOR SWITCH 21WV2 LOOSE AND CORRODED. REPLACED RIGHT HAND EMERGENCY EXIT PROXIMITY DETECTOR SWITCH 21WV2 PER AMM 52-71-13 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HINGE — STIFF (ZONE 800 - DOORS) · airframe 73,010 hrs · 33,635 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR VERY DIFFICULT TO CLOSE. MAINTENANCE LUBRICATED L1 DOOR HINGE POINTS PER AMM 53-40-01 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HINGE FITTING — LACK OF LUBE (ZONE 800 - DOORS) · airframe 73,010 hrs · 33,635 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD CABIN ENTRY DOOR DIFFICULT TO CLOSE. MAINTENANCE LUBRICATED HINGE FITTINGS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-10-00.

Part: BATTERY — FAILED (ZONE 200 - FUSE) · airframe 72,764 hrs · 33,465 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPISHING EMERGENCY LIGHTING BITE TEST, FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY FAULT DISPLAYED. MAINTENANCE REPLACED THE BATTERY FOR THE FORWARD EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LINER — UNSECURE (ZONE 800 - DOORS) · airframe 72,175 hrs · 33,075 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR DIFFICULT TO CLOSE. MAINTENANCE SECURED THE FORWARD ENTRY DOOR LININGS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-23-46.

Part: HINGE — EXCESS PLAY (ZONE 700 - GEARS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LAND GEAR RIGHT HAND AFT DOOR FORWARD HINGE HAS EXCESSIVE PLAY. REPLACED HINGE PER CMM: 52-82-32.

Part: HINGE — EXCESS PLAY (ZONE 700 - GEARS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LAND GEAR LEFT HAND AFT DOOR FORWARD HINGE HAS EXCESSIVE PLAY. REPLACED HINGE PER CMM: 52-82-32.

Part: HINGE — EXCESS PLAY (ZONE 700 - GEARS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LAND GEAR LEFT HAND AFT DOOR AFT HINGE HAS EXCESSIVE PLAY. REPLACED HINGE PER CMM: 52-82-32.

Part: HINGE — EXCESS PLAY (ZONE 700 - GEARS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LAND GEAR RIGHT HAND AFT DOOR AFT HINGE HAS EXCESSIVE PLAY. REPLACED HINGE PER CMM: 52-82-32.

Part: DAMPER — CRACKED (ZONE 800 - DOORS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DOOR DAMPER CYLINDER ACCUMULATOR CRACKED. REPLACED DOOR DAMPER CYLINDER ACCUMULATOR PER AMM 52-11-14 .

Part: DAMPER — DAMAGED (ZONE 800 - DOORS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: CUT ON PASSENGER CREW DOOR 831 SEAL OF GAUGE VISOR CYLINDER DOOR DAMPER. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 831 PER AMM 52-11-14-400-001-B

Part: ATTACH ANGLE — CRACKED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED WING TO BODY FAIRING AND KEEL BEAM ATTACHMENT ANGLES, SHEAR PLATE WEB AT FR 42, -Y254 AND Z 2343.94. REPAIRED WEB PER EA 337185.

Part: HANDLE — CRACKED (ZONE 200 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SLIDING WINDOW CRACKED. REPLACED HANDLE PER AMM 56-12-12-400-003-A.

Part: HANDLE — CRACKED (ZONE 200 - FUSE) · airframe 71,465 hrs · 32,623 cycles

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

Part: HOOK — WORN (ZONE 800 - DOORS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT PASSENGER / CREW DOOR 842 INNER CONTROL HANDLE HOOK WORN. REPLACED HOOK PER AMM 52-13-21.

Part: HOOK — WORN (ZONE 800 - DOORS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD PASSENGER / CREW DOOR 841 INNER CONTROL HANDLE HOOK WORN. REPLACED HOOK PER AMM 52-11-21.

Part: HOOK — WORN (ZONE 800 - DOORS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD PASSENGER / CREW DOOR 831 INNER CONTROL HANDLE HOOK WORN. REPLACED HOOK PER AMM 52-11-21.

Part: HOOK — WORN (ZONE 800 - DOORS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT PASSENGER / CREW DOOR 832 INNER CONTROL HANDLE HOOK WORN. REPLACED HOOK PER AMM 52-13-21.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR PANEL 231WG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV L.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR PANEL 232XG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV L.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR PANEL 241LF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR PANEL 261DF DELAMINATED. REPLACED FLOOR PANEL PER TASK CARD 26C26053014.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR PANEL 262BG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV L.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 222CF DELAMINATED. REPLACED FLOOR PANEL PER TASK CARD 26C22053014.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: STOP FITTING — WORN (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO DOOR CUT OUT STOP FITTING WORN. REPLACED STOP FITTING PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 222EF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006 AND IRM 9701 REV L.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #5 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #4 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #3 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #3 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT FLOOR PANEL 151VG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #5 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #6 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #2 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #6 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #4 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #1 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: NONE — CRACKED (ZONE 200 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LEFT HAND FRAME CRACKED AT FR 2 AND +Y511. REPLACED WINDSHIELD FRAME PER EO 5319Y017-003 AND EA 336815.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #2 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED RIGHT HAND CONTINUITY FITTING PER EO 5319Y017 AND EA 336815.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED LEFT HAND CONTINUITY FITTING PER EO 5319Y017 AND EA 336815.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 71,465 hrs · 32,623 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #1 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: WINDOW POST — CRACKED (ZONE 200 - FUSE) · airframe 71,399 hrs · 32,586 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND CENTER LATERAL WINDSHIELD / WINDOW POST CRACKED AT FR 4 AND -Y511. REPLACED WINDSHIELD / WINDOW POST PER EO 5319Y17-004 AND EA 336815.

Part: PROXIMITY SWITCH — NONE (ZONE 800 - DOORS) · airframe 71,313 hrs · 32,531 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR LEFT EMERGENCY EXIT. ECAM MULTIPLE TIMES DURING FLIGHT AND TAXI IN. REPLACED LEFT HAND EMERGENCY EXIT PROXIMITY SWITCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-13.

Part: PROXIMITY SWITCH — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 71,247 hrs · 32,486 cycles

AIRCRAFT WAS NOT GROUNDED: SPURIOUS ECAM MESSAGE LEFT EMERGENCY EXIT CABIN PRESSURE OK. ACCOMPLISHED TSM 52-21-00-810-806-A, FOUND LEFT EMERGENCY EXIT WARNING PANEL PROXIMITY SWITCH TARGET OUT OF TOLERANCE. THE GAP WAS 2.98 MM. ADJUSTED GAP TO 1.854 MM, PER AMM 52-71-13-400-001.

Part: PROXIMITY SWITCH — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 71,227 hrs · 32,468 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR LEFT EMERGENCY EXIT SPURIOUS ECAM MESSAGE. ADJUSTED LEFT HAND EMERGENCY EXIT HATCH PROXIMITY SWITCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-13.

Part: COVER — MISINSTALLED (ZONE 800 - DOORS) · airframe 71,187 hrs · 32,444 cycles

AIRCRAFT WAS GROUNDED: DOOR LEFT EMERGENCY EXIT ILLUMINATED IN FLIGHT. FLIGHT ATTENDANT REPORTS ASSOCIATED SLIDE ARMED LIGHT FLICKERING. RE-INSTALLED COVER FLAP ON LEFT HAND OVER WING EXIT DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-23-47.

Part: TARGET — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 71,187 hrs · 32,444 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT EMERGENCY EXIT LIGHT ECAM INTERMITTENT. ADJUSTED PROXIMITY TARGET ON LEFT EMERGENCY EXIT DOOR COVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-13-400-001-A.

Part: COVER — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 71,172 hrs · 32,436 cycles

AIRCRAFT WAS NOT GROUNDED: THE DUST COVER ON THE LEFT OVER WING EXIT IS LOOSE THIS CAUSED A WING EXIT WARNING ON ECAM, DOOR HANDLE WAS CHECKED AND FOUND FULLY SEATED. ADJUSTED AND INSTALLED LEFT HAND OVER WING EXIT COVER FLAP PER AMM 52-21-11.

Part: CONNECTOR — FAULTY (ZONE 200 - FUSE) · airframe 70,579 hrs · 32,074 cycles

AIRCRAFT WAS GROUNDED: SEAT 19ABC EMERGENCY LIGHTING INOPERATIVE. RE-TERMINATED WALL CONNECTOR PER ESPM 20-44-23.

Part: CONNECTOR — FAULTY (ZONE 200 - FUSE) · airframe 70,579 hrs · 32,074 cycles

AIRCRAFT WAS GROUNDED: SEAT 18ABC EMERGENCY LIGHT INOPERATIVE. RE-TERMINATED WALL CONNECTOR PER ESPM 20-44-23.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,154 hrs · 30,644 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN LIGHT AT RIGHT OVERWING EXIT INOPERATIVE. RELAMPED RIGHT OVERWING EXIT EMERGENCY EXIT SIGN LIGHT, PER AMM 33-51-16.

Part: MANIFOLD — CRACKED (BRAKE SYSTEM) · airframe 67,146 hrs · 30,067 cycles

AIRCRAFT WAS GROUNDED: LEAK ABOVE RIGHT WHEEL ASSEMBLY AND PUDDLING ON GROUND. LEAK FROM BRAKE MANIFOLD SAFETY VLV AREA. T/S SYS FOUND RELIEVE CAP LEAKING. REMOVED BRAKE MANAFOILD FOR INSPECTION, FOUND BRAKE MANAFOLD CRACKED. REMOVED AND REPLACED BRAKE MANIFOLD. PERFORDED BRAKE BLEED AND OPS CKS. SERVICED GREEN SYS. NO DEFECTS.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 65,795 hrs · 29,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND FORWARD DOOR CUT OUT INTERCOSTAL AT FR 16 AND DOOR STOP #1. REPLACED INTERCOSTAL PER SRM 51-72-11.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 65,795 hrs · 29,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND FORWARD DOOR CUT OUT INTERCOSTAL AT FR 16 AND DOOR STOP #7. REPLACED INTERCOSTAL PER SRM 51-72-11.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 65,795 hrs · 29,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND FORWARD DOOR CUT OUT INTERCOSTAL AT FR 16, S10R AND DOOR STOP #7. REPLACED INTERCOSTAL PER SRM 51-72-11.

Part: SEAL DEPRESSOR — CRACKED (R2 DOOR) · airframe 65,553 hrs · 29,155 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED UPPER FORWARD SEAL DEPRESSOR ON THE R2 DOOR CUT OUT AT FR 68 AND S9R. REPAIRED SEAL DEPRESSOR PER EA 297234.

Part: DOOR FRAME — CRACKED (AFT PAX DOOR ARE) · airframe 65,553 hrs · 29,154 cycles

AIRCRAFT WAS GROUNDED: AFT PASSENGER / CREW DOOR CUT OUT FRAME WEB JOINT CRACKED AT FR 68 AND S8R. REPAIRED THE FRAME WEB SRM 53-41-12.

Part: FILTER — ODOR (AFT GALLEY) · airframe 64,405 hrs · 28,490 cycles

FLIGHT ATTENDANTS IN AFT CABIN REPORTED AN ODOR DURING TAKE OFF AND ON LANDING. MAINTENANCE COMPLIED WITH WC 26L00021001, AND REPLACED ALL EXTRACT FILTERS IN THE AFT GALLEY. NO ODORS NOTED.

Part: FILTER — ODOR (AFT GALLEY) · airframe 64,002 hrs · 28,222 cycles

FLIGHT ATTENDANTS IN AFT CABIN, REPORTED AN ODOR DURING TAKE OFF AND LANDING. MAINTENANCE COMPLIED WITH WC 26L00021001. REPLACED THE EXTRACT FILTER IN AFT GALLEY, NO ODORS NOTED.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

LEFT ELEVATOR NR 6 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

LEFT ELEVATOR NR 4 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

RIGHT ELEVATOR NR 4 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

THE LEFT ELEVATOR NR 1 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

RIGHT ELEVATOR NR 2 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

LEFT ELEVATOR NR 5 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

RIGHT ELEVATOR NR 1 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

THE LEFT ELEVATOR NR 2 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

RIGHT ELEVATOR NR 5 HINGE FITTING WAS WORN AND HAS EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

RIGHT ELEVATOR NR 3 HINGE FITTING WAS WORN AND HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 64,002 hrs · 28,222 cycles

RIGHT ELEVATOR NR 6 HINGE FITTING WAS WORN AND HAS EXCESSIVE PLAY. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 63,632 hrs · 27,991 cycles

L2 DOOR HARD TO ARM AND DISARM. CLEANED L2 DOOR GIRT BAR FITTINGS. OPS CHECKED GOOD.

Part: SEAT — OUT OF ADJUST (CABIN) · airframe 63,503 hrs · 27,933 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND ROWS 136ABC AND 13DEF WERE RECLINED INTO EMERGENCY EXIT. MAINTENANCE ADJUSTED ROW 13ABC AND 13DEF AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: VALVE — STUCK (FUEL) · airframe 61,858 hrs · 26,992 cycles

FUEL CROSSFEED VALVE WILL NOT OPEN. RESET AND TESTED BOTH MOTORS OF THE CROSSFEED VALVE. OPS NORMAL IAW MM 28-23-00.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 61,621 hrs · 26,855 cycles

EMERGENCY LIGHTS IN THE MID CABIN ARE ON WITH EMERGENCY EXIT LIGHT SWITCH IN ARMED POSITION. IAW TSM-33-51-00, RESET CIDS. EMERGENCY LIGHTS TESTED GOOD.

Part: INTERFACE UNIT — FAULTY (ZONE 100) · airframe 61,069 hrs · 26,506 cycles

AIRCRAFT WAS GROUNDED: DURING LANDING GEAR RETRACTION, LANDING GEAR HANDLE APPEARED TO BE LOCKED IN THE DOWN POSITION. AFTER 3 ATTEMPTS, ABLE TO RAISE THE HANDLE. MAINTENANCE ACCOMPLISHED TSM 32-31-00-810-885-A AND FOUND FAULTING NR 1 LANDING GEAR CONTROL INTERFACE UNIT, NO DC VOLTAGE AT PIN W, CONTINUITY CHECKS SUCCESSFUL FROM LANDING GEAR CONTROL INTERFACE UNIT NR 1 TO LANDING GEAR SELECT HANDLE (6GA). REPLACED NR 1 LANDING GEAR CONTROL INTERFACE UNIT PER AMM 32-31-71 AND PERFORMED SUCCESSFUL OPERATIONAL CHECK WITH NO FAULTS.

Part: PIN — CORRODED (ZONE 700) · airframe 61,054 hrs · 26,496 cycles

AIRCRAFT NOT GROUNDED. CORROSION AT RIGHT HAND MAIN LANDING GEAR REAR PINTLE PIN. REPLACED RIGHT HAND MAIN LANDING GEAR REAR PINTLE PIN PER JOB CARD 26T0003.

Part: PIN — CORRODED (ZONE 700) · airframe 61,054 hrs · 26,496 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR REAR PINTLE PIN IS CORRODED. REPLACED PINTLE PIN PER TASK CARD 26T00032001.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 60,512 hrs · 26,210 cycles

AFT EMERGENCY POWER UNIT NOT TESTING. REPLACED POWER UNIT IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 60,304 hrs · 26,061 cycles

2L EXIT LIGHT COVER MISSING. REPLACED LENS COVER AT 2L EXIT.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 59,536 hrs · 25,619 cycles

ROW 14A LOWER EMERGENCY EXIT LIGHT COVER PLASTIC TAB BROKEN. REPLACED EMERGENCY LIGHT LENS AT SEAT 14A.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 59,184 hrs · 25,397 cycles

BATTERY FAULT AT EPSU 10WL. REPLACED THE BATTERY.

Part: COVER — MISSING (CABIN) · airframe 57,641 hrs · 24,573 cycles

AIRCRAFT WAS NOT GROUNDED, EMERGENCY EXIT LIGHT COVER AT SEAT 14A MISSING. INSTALLED EMERGENCY EXIT LIGHT COVER AT SEAT 14A.

Part: WINDOW SHADE — INOPERATIVE (CABIN) · airframe 57,508 hrs · 24,525 cycles

ACFT WAS NOT GROUNDED: LT EMERGENCY EXIT WINDOW SHADE WILL NOT OPEN. REPLACED WINDOW SHADE AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 25-23-47.

Part: SLIDE — CONTAMINATED (LT OVERWING) · airframe 57,326 hrs · 24,396 cycles

LEFT WING EMERGENCY SLIDE HAS WATER LEAKING FROM INSIDE SLIDE ENCLOSURE BOX. REPLACED THE SLIDE IAW TASK CARD 26C19053012.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,326 hrs · 24,396 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM AT FRAME 66 AND +Y1292. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,326 hrs · 24,396 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM AT FRAME 66 AND -Y1292. REPLACED FLOORBEAM IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,326 hrs · 24,396 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM BETWEEN FRAME 64 AND FRAME 66 AT +Y765. REPLACED BEAM IAW SRM 51-23-12, 51-72-11.

Part: MOUNT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 57,326 hrs · 24,396 cycles

CORROSION ON LAVATORY MOUNT HARD POINT AT -Y765 BETWEEN FRAMES 64 AND 66. REPLACED THE BEAM IAW SRM 51-72-11.

Part: SEAL — MISSING (R2 DOOR) · airframe 57,326 hrs · 24,396 cycles

AIRCRAFT IN BASE MAINTENANCE. R2 DOOR EMERGENCY OPERATION, DOOR DAMPER, GAGE, SIGHT GLASS CENTER SEAL IS MISSING. REPLACED R2 DOOR EMERGENCY OPERATION, DOOR DAMPER IAW AMM 52-13-14-0401.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 57,326 hrs · 24,396 cycles

LEFT SIDE BOX BEAM UPPER FLANGE AFT HOLE HAS CRACK INDICATION AT FRAME 43 AND +Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,326 hrs · 24,396 cycles

ACFT IN BASE MAINTENANCE: CORROSION ON R2 DOOR CUTOUT LOWER SILL BEAM. REPAIRED SILL BEAM IAW SRM 53-41-14-201, PRINCIPLE 5.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,326 hrs · 24,396 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR CUT OUT LOWER SILL AT FRAME 64 AND STRINGER 23 LT. REPAIRED SILL IAW SRM 53-41--14-201.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,326 hrs · 24,396 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LT SHEAR PLATE BETWEEN FRAME 69 ABD, FRAME 70 AT +Y1292. REPLACED SHEAR PLATE IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 57,326 hrs · 24,396 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR CUT OUT LOWER SILL. REPAIRED SILL IAW SRM 53-41-14-201, PRINCIPLE 5.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,136 hrs · 24,276 cycles

AIRCRAFT WAS NOT GNDED. AFT FLIGHT ATTENDANT OTBD EMER FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: APU — LEAKING (ZONE 100) · airframe 56,516 hrs · 23,902 cycles

AIRCRAFT WAS GNDED. ACFT HAS STRONG DIRTY SOCK SMELL. REPLACED APU IAW TC 26L31049005. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. COMPLIED WITH DECONTAMINATION CARDS 26L00021004, 26L00021001 & 26L00021002, O SMELL NOTED AT THIS TIME.

Part: GENERATOR — LEAKING (APU) · airframe 56,484 hrs · 23,884 cycles

AIRCRAFT WAS GNDED. FLIGHT ATTENDANTS REPORTED HAVING HEADACHES DUE TO A STRONG DIRTY SOCK SMELL IN PAX CABIN DURING CLIMB OUT & DURING TAXI TO GATE. ACCOMPLISHED TASK CARDS 26L00021001 & 26L00021002, DETERMINED THE APU WAS THE SOURCE OF THE ODOR. REPLACED APU GEN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 24-23-51, TASK CARDS 26L00021001, 26L00021002 & 26L00021004 WITH NO ODORS BEING DETECTED.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 56,147 hrs · 23,691 cycles

AIRCRAFT WAS GNDED. SUDDEN STRONG & RAPID VERTICAL AIRFRAME VIBE DURING CLIMB AT FL 250 M, .78 335 KIAS AT 25C SAT, STOPPED WHEN SLOW < 300K. REPLACED LT ELEVATOR HINGE, NR 1 FITTING. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA201512309009 FOR ADDITIONAL INFORMATION.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 56,147 hrs · 23,691 cycles

AIRCRAFT WAS GNDED. SUDDEN STRONG & RAPID VERTICAL AIRFRAME VIBE DURING CLIMB AT FL 250 M, .78 335 KIAS AT 25C SAT, STOPPED WHEN SLOW < 300K. REPLACED LT ELEVATOR HINGE, NR 3 FITTING. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA201512309008 FOR ADDITIONAL INFORMATION.

Part: FAN — DEFECTIVE (E&E BAY) · airframe 55,848 hrs · 23,539 cycles

VENT EXTRACT FAULT ON SHORT FINAL, AE 2 CB POPPED, ELEC SMELLS NOTED. REPLACED AVIONICS FAN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-26-51-000-001-A.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 55,781 hrs · 23,509 cycles

ON DESCENT OILY AIR SMELL IN COCKPIT, BUT NOT NOTICED IN CABIN. TROUBLE SHOT CABIN AIR QUALITY UTILIZING JC 26L00021001, 26L00021003 & FOUND NR 1 ENG DE-OILER SEAL LEAKING. R & R NR 1 ENG OIL BREATHER SEAL ASSEMBLY IAW AMM 72-60-31-001-010-A.

Part: PLENUM — LEAKING (APU) · airframe 55,764 hrs · 23,502 cycles

ON DESCENT LOW ALTS, FUMES FROM PACKS STRONG OILY, MUSTY SMELL, HURTS EYES & THROAT. ACCOMPLISHED TASK CARDS 26L00021001 & 26L00021001 FOUND RESIDUAL OIL AT APU INTAKE AT PLENUM SEAL. REMOVED RESIDUAL OIL & CLEANED PLENUM & INTAKE. NO FURTHER SMELL NOTED IN CABIN.

Part: PACKING — LEAKING (APU) · airframe 55,755 hrs · 23,498 cycles

SMELL OF OIL FOR A SHORT PERIOD OF TIME DURING CLIMB & DECENT, SMELL TOWARD FRONT OF ACFT. FOUND APU OIL COOLER FAN LEAKING OIL, REPLACED PACKINGS. ACCOMPLISHED A SATISFACTORY LEAK CHECK IAW AMM 49-52-51.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,727 hrs · 22,405 cycles

FLASHLIGHTS FOR FLIGHT ATTENDANT APPEAR TO NOT BE FLASHING FOR CHARGE. REPLACED BATTERY & RELAMPED FLASHLIGHT.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 53,205 hrs · 22,161 cycles

INFLIGHT 2L DOORS RED PRESS LIGHT FLASHING. ARM HANDLE MOVE UPWARD COCKPIT INDICATES DOOR IS LOCKED BUT NOT ARMED. CLEANED GIRT BAR AREA. 2L DOOR OPERATIONS CHECKED OK. SLIDE ARM INDICATION OPERATIONS CHECKED OK IAW AMM 52-13-00.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 52,275 hrs · 21,603 cycles

THE FWD INBD FLASHLIGHT BATTERIES DEPLETED & RETAINING STRAP BROKEN. R & R FWD INBD FLASHLIGHT BATTERY PACK & STRAPS. OPERATIONS GOOD.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 51,954 hrs · 21,421 cycles

ON TAKEOFF AT APPROX 80 KNOTS, CREW RECEIVED AN AMBER EPR MODE FAULT. AN AMBER N1 DEGRADED MODE MSG AS WELL AS AURAL ALERT & CAUTION LIGHT. CREW REJECTED TAKEOFF & RETURNED TO GATE. AMBER AUTO THRUST OFF MSG DISPLAYED. PERFORMED TSM TASK 73-22-00-810-817-B. RAN ENG NR 1 FOR 3 MINUTES. NO SYS FAULTS. SYS OPERATIONS CHECKED NORMAL AT THIS TIME. ACFT OK FOR SERVICE. THE PROBLEM REOCCURRED PRIOR TO THE NEXT TAKEOFF. THE NR 1 ENG EPR INDICATOR FAILED & RECEIVED AMBER EPR MODE FAULT & AMBER N1 DEGRADED MODE & AMBER AUTO THRUST OFF MSGS. AFTER ENG SHUTDOWN, TWO CLASS II MSGS, ENG 1 EIU & ENG 1 FADEC MSG DISPLAYED. R & R ENG NR 1 P2 & T2 SENSOR IAW AMM 73-22-11-000-010-A & AMM 73-22-11-400-010-A. PERFORMED OPERATIONAL TEST & HEATER TEST IAW AMM 73-22-11-710-040 & AMM 73-22-11-710-040-A. R & R ENG 1 EIU IAW AMM 73-25-34-000-041-A & AMM 73-25-34-710-042. OPERATIONS CHECKED GOOD. ACFT OK FOR CONTINUED SERVICE.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 51,053 hrs · 20,962 cycles

CREW REPORTED THE AFT FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY PACK ON AFT FLASHLIGHT, OPERATIONS GOOD.

Part: O-RING — LEAKING (APU) · airframe 50,575 hrs · 20,758 cycles

UPON ENTERING ACFT AS OUTBOUND CREW, CREW REPORTED A DIRTY SOCK SMELL, STRONG WHEN PACKS TURNED ON. MX COMPLIED WITH JOB CARDS 26L00021001, 26L00021002 & 26L00021004. FOUND APU NR 4 CAVITY VENT TUBES LEAKING. INSTALLED NEW O RINGS ON APU NR 4 BEARING CAVITY VENT TUBES IAW MM 49-91-53. CLEANED APU IAW MM 49-16-00-100-001. OPERATIONS CHECKED GOOD, NO LEAKS NOTED. FOUND NR 2 ENG DE OILER SEAL LEAKING. R & R NR 2 ENG DE OILER SEAL ASSEMBLY IAW MM 72-60-31.

Part: ACTUATOR — STICKING (NLG DOOR) · airframe 50,046 hrs · 20,545 cycles

AFTER GEAR RETRACTION, NOSE GEAR DOOR OPEN MESSAGE DISPLAYED. CYCLED GEAR & MESSAGE CLEARED. FLIGHT CONTINUED & LANDED AT DESTINATION IN PHX. MX PERFORMED TROUBLESHOOTING IAW TSM 32-31-00-810-859-A, STEPS 1 THRU 5. FOUND NLG ACTUATING CYLINDER STICKING. R & R NLG DOOR ACTUATING CYLINDER IAW AMM 32-31-16. FUNCTIONAL CHECKED, LEAK CHECKED GOOD. PERFORMED BITE CHECK OF LGCIU'S, CHECKED GOOD.

Part: UPLOCK — FALSE INDICATION (MLG) · airframe 49,882 hrs · 20,475 cycles

RECEIVED "NLG DOORS NOT CLOSED, CLASS 1" MESSAGE AFTER FIRST AND SECOND RETRACTIONS. SLOWED TO MINIMUM SPEED AND MAX BODY ANGLE BEFORE SUCCESS ACHIEVED. REPLACED NLG DOOR UPLOCK ASSY IAW AMM 32-31-14-400-001-A, ALL FUNCTIONS TEST NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,787 hrs · 20,432 cycles

CREW REPORTED THE EXIT LOCATION SIGN AT MAIN AILSE MID CABIN, FORWARD FACING NEEDS FIVE BULBS REPLACED. MAINTENANCE REPLACED MID CABIN MAIN AISLE EMERGENCY EXIT SIGN. CHECKS NORMAL.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 48,388 hrs · 19,806 cycles

MAINTENANCE REPORTED EPSU 10WL FAILS EMERGENCY LIGHTS TEST AND UNIT SELF TEST. MAINTENANCE REPLACED EPSU 10WL PER AMM 33-51-38-400. PASSES SELF TEST AND EMERGENCY LIGHTS TEST.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,204 hrs · 19,720 cycles

MAINTENANCE REPORTED WITH AIRCRAFT POWER OFF (OR IN GROUND POWER), SEATS 18, 14, 12 AND ALL OF AFT GALLEY EMERGENCY LIGHTS WILL NOT TURN ON. WITH AIRCRAFT POWERED UP, ALL OPS CHECK GOOD. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT 13WL. OPS CHECK GOOD PER AMM 33-51-38.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,548 hrs · 19,416 cycles

MAINTENANCE REPORTED ROW 20 EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPLACED SEAT LIGHT ASSEMBLY AND WALL CONNECTOR IAW SR33-008. OPS CHECK GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 47,082 hrs · 19,208 cycles

ENGINE 1 AGENT 1 DISCHARGE LIGHT CAME ON EN ROUTE PHX-ANC. ENGINE PARMETERS WERE NORMAL. DISCHARGE LIGHT WENT OFF AGAIN DURING DESCENT AND REMAINED OFF. ENGINE 1 FIRE LOOP B ALSO FAULTING INTERMITTENTLY. INSPECTED NR 1 ENGINE FOR ANY SIGN OF FIRE OR OVERHEAT WITH NONE NOTED. PERFORMED ENGINE 1 FIRE CIRCUIT TEST - SYSTEM OPS CHECKED NORMAL. REMOVED AND REPLACED ENGINE/APU FIRE PANEL.

Part: WIRE — DAMAGED (CABIN) · airframe 46,060 hrs · 18,708 cycles

SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT SEAT 18 LEFT. REPAIRED WIRE WITH SPLICE PER ESWPM 20-10-13. OPS CHECKED GOOD.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 39,457 hrs · 15,843 cycles

FLT 447 - DOOR R2 SLIDE ARMED INDICATION ON DOOR PAGE INTERMITTENT IN FLIGHT. FLIGHT ATTENDANT REPORTS THE DOOR ARMED HANDLE HAS A TENDENCY TO CREEP UP AND NEEDS TO BE PUSHED ARMED TO REMAIN ARMED. MAINTENANCE REPLACED THE R2 DOOR SLIDE.

Part: PROXIMITY SENSOR — DEFECTIVE (R2 DOOR) · airframe 39,412 hrs · 15,822 cycles

FLT 287 - PHX-SJC - EMERGENCY EGRESS SYSTEM - DOOR 2R SLIDE DOES NOT SHOW ARMED ON ECAM WHILE EN ROUTE. VERIFIED ARMED. REMOVED AND REPLACED R2 DOOR PROXIMITY SENSOR (7WN2). SYSTEM CHECKED GOOD PER AMM 52-73-11.

Part: SWITCH — OUT OF ADJUST (DOOR) · airframe 39,412 hrs · 15,822 cycles

FLT 366 - SMF-PHX - EMERGENCY EGRESS SYSTEM - DOORS 2L AND 2R SLIDE ARMED INDICATIONS LOST ON DOOR PAGE (LOWER ECAM) ABOVE FL190. ADJUSTED ESCAPE SLIDE DOOR HANDLE SWITCHES 7WN1 & 7WN2 PER AMM 52-71-00-820-002-01. OPERATIONAL CHECK WAS GOOD.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 39,374 hrs · 15,802 cycles

FLT 450 - PHX - EES - SLIDE FOR DOOR 2R WILL NOT STAY ARMED - HANDLE IS NOT QUITE FLUSH. PUSHING INTO ARM POSITION WILL SHOW ARMED ON THE ECAM. FLIGHT ATTENDANT REPORTED A SINGLE POP SOUND ABOUT THE TIME CREW NOTICED 2R NOT ARMED. WHEN RELEASED, REBOUNDS SLIGHTLY & SHOWS NOT ARMED. MAINTENANCE REMOVED DEBRIS FROM UNDER 2R DOOR GIRT BAR. DOOR SLIDE INDICATION OPERATIONAL TEST IS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 39,370 hrs · 15,800 cycles

FLT 447 - MSP - EEL - LOWER LEVEL EMERGENCY LIGHT LENS COVER AT SEAT 3C MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT LENS ON SEAT 3C.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,334 hrs · 15,782 cycles

CHECK - SAL - EMERGENCY LIGHTS - EMERGENCY LIGHT "ON" WHEN SWITCH IS IN ARM POSITION. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (EPSU). OPERATIONAL TEST WAS GOOD PER AMM 33-51-38-000-001 LEFT POSITION 11WL.

Part: DAMPER — LOW PRESSURE (R2 DOOR) · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - EES - LOW PASSENGER DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER AT R-2 DOOR. CHARGED THE DAMPER & EMERGENCY OPERATIONAL CYLINDER & LEAK TEST IAW A319 AMM 52-10-00-614-050.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT SHEAR PLATE AT MAIN CABIN FLOOR STRUCTURE BETWEEN FR69 AND FR70. REPLACED LEFT SHEAR PLATE AT MAIN CABIN FLOOR STRUCTURE, BETWEEN FR69 AND FR70 IAW EO 5307Y284.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT SHEAR PLATE AT MAIN CABIN FLOOR STRUCTURE, BETWEEN FR69 AND FR70. REPLACED RIGHT SHEAR PLATE AT MAIN CABIN FLOOR STRUCTURE, BETWEEN FR69 AND FR70 IAW EO 5307Y284.

Part: ROD — OUT OF ADJUST (L1 DOOR) · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - L-1 DOOR IS OUT OF ADJUSTMENT AT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER. PERFORMED ADJUSTMENT AT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER IAW A319 AMM 52-11-14-820-052.

Part: SKIN — SATURATED (ELEVATOR) · corrosion level 2 · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - AREAS OF TRAPPED WATER ON LEFT ELEVATOR UPPER SKIN BETWEEN ELEV STA 297 TO ELEV STA 601 & BETWEEN RIB 8 TO RIB 14. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN ELEV STA 297 TO ELEV STA 601 & BETWEEN RIB 8 TO RIB 14 IAW A319 SRM 55-21-11 & 51-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 38,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - AREAS OF TRAPPED WATER IN HONEYCOMB ON LOWER SURFACE OF LEFT ELEVATOR BETWEEN HORIZONTAL STAB STA 527 TO STAB STA 589. REPAIRED LOWER SURFACE OF LEFT ELEVATOR BETWEEN HORIZONTAL STAB STA 527 TO STAB STA 589 IAW A319 SRM 55-21-11 & 51-77-13.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - EXCESSIVE PLAY AT RUDDER HINGE BEARING NR 4 AT VERT STAB STA 2632. REPLACED RUDDER HINGE FITTING ASSEMBLY AT VERT STAB STA 2632, RIB 6 IAW A319 AMM 55-36-41 & SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - EXCESSIVE PLAY AT RUDDER HINGE NR 3. REPLACED NR 3 RUDDER HINGE FITTING ASSEMBLY IAW A319 AMM 55-36-41 & SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 39,334 hrs · 15,782 cycles

SAL - S4 - MAJOR REPAIR - EXCESSIVE PLAY AT RUDDER HINGE NR 1 AT VERTICAL STAB STA 780, RIB 2. REPLACED NR 1 RUDDER HINGE ASSEMBLY FITTING AT VERTICAL STAB STA 780, RIB 2 IAW A319 AMM 55-36-41 & SRM 51-72-11.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 30,177 hrs · 16,583 cycles

PHC-DFW - EMERGENCY LIGHTS - LEFT ROW 8 EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE WIRE AT EXISTING BUTT SPLICE UNDER SEAT 8B. RE-SPLICED WIRE. OPERATIONAL CHECK WAS GOOD.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 34,676 hrs · 13,624 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE AT INTERNAL STRUCTURE OF FORWARD CARGO COMPARTMENT FR29 + 2.5 INCHES, S43R. REPLACED SUPPORT ANGLE AT INTERNAL STRUCTURE OF FORWARD CARGO COMPARTMENT FR29 + 2.5 INCHES, S43R IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,676 hrs · 13,624 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK AT FR 19 + 19", -Y765. REPLACED CABIN SEAT TRACK AT FR 19 + 19", -Y765 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,676 hrs · 13,624 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL OF L-2 DOOR BETWEEN FR67 +17 INCHES AND FR68, Y1732 IN PASSENGER CABIN. REPAIRED LOWER SILL OF L-2 DOOR BETWEEN FR67 +17 INCHES AND FR68, Y1732 IAW A319 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,676 hrs · 13,624 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM AT FR 69 - FR 70, +Y765. REPLACED FLOORBEAM AT FR 69 - FR 70, +Y765 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSLAGE) · airframe 34,676 hrs · 13,624 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LATERAL SHEAR PLATE BETWEEN FR69 & FR70, S23L, Y1732. REPLACED LATERAL SHEAR PLATE BETWEEN FR69 & FR70, S23L, Y1732 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 34,676 hrs · 13,624 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 & FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 & FR70, S23R IAW A319 SRM 51-72-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,372 hrs · 13,508 cycles

FLT NR 0511 - SAN-PHX - EEL FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS)

LAS - EMERGENCY LIGHTS FLICKER ON AND OFF IN CABIN WITH EMERGENCY EXIT LIGHT SWITCH IN ARMED POSITION. MAINTENANCE REPLACED EMERGENCY LIGHT SWITCH (4WL). OPERATIONAL CHECK IS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 29,646 hrs · 11,581 cycles

LAS - EEL - EMERGENCY EXIT LIGHTS INOP ROWS 14, 18, AND 22, ALSO L2 AND R2 DOORS. MX REPLACED LT AFT BATTERY AND CHARGER. OPS CHECKED GOOD PER AMM 33-51-38-401.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 29,502 hrs · 11,525 cycles

SAL - CORROSION ON SHEAR PLATE (TRAY), +Y1175, FR.68 - FR 69. REPLACED SHEAR PLATE (TRAY), +Y1175, FR.68 - FR 69 IAW A319 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 29,502 hrs · 11,525 cycles

SAL - CORROSION ON CABIN FLOOR SUPPORT, +Y1292, FR 67 - FR 68. REPLACED CABIN FLOOR SUPPORT,+Y1292, FR.67 - FR 68 IAW A319 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 29,502 hrs · 11,525 cycles

SAL - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT, +Y1292, FR 68 - FR 70. REPLACED CABIN FLOOR SUPPORT ,+Y1292, FR 68 - FR 70 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 29,502 hrs · 11,525 cycles

SAL - CORROSION ON SHEAR PLATE, +Y1175, FR.69 - FR 70. REPLACED SHEAR PLATE, +Y1175, FR.69 - FR 70 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 29,502 hrs · 11,525 cycles

SAL - MAJOR REPAIR - CORROSION ON SHEAR PLATE, -Y1175, FR 69 - FR 70. REPLACED SHEAR PLATE, -Y1175, FR 69 - FR 70 IAW A319 SRM 51-72-11.

Part: FITTING — WORN (ZONE 800) · airframe 29,502 hrs · 11,525 cycles

SAL - R1 DOOR UPPER SUPPORT ARM FITTING WORN CAUSING BEARING TO MIGRATE OUT OF THE FITTING. REPLACED R1 DOOR UPPER SUPPORT ARM FITTING IAW A319 SRM 51-72-11.

Part: STRUCTURE — VIBRATION (EMPENNAGE)

CMH - CREW WAS EXPERIENCING SEVERE TAIL VIBRATIONS AND DIVERTED TO IND. THE AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX AND EXPERIENCED NO VIBRATION ISSUES.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,643 hrs · 9,579 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHT AT ROW 4L WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT, 10WL, IAW AIRBUS 319 MM 33-51-38. OPERATIONAL CHECKS WERE GOOD. *S/D* WILL BE SUBMITTED UPON RECEIPT OF VENDOR TEAR DOWN REPORT.

Part: SLIDE — WILL NOT TEST (RT OVERWING) · airframe 23,905 hrs · 91,050 cycles

LAS - EEL - DURING OVERNIGHT INSPECTION EMERGENCY SYS LIGHT CHECK FAILED, FAULTED EXTERNAL LIGHT LOAD RIGHT. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1A25301.

Part: SLIDE — FAILED (L1 DOOR) · airframe 22,646 hrs · 8,622 cycles

DURING 4 DAY CHECK DISCOVERED L1 DOOR ESCAPE SLIDE PRESSURE INDICATING ZERO. MAINTENANCE REMOVED AND REPLACED L1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304. VENDOR TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. UNIT WAS RECEIVED AND FOUND RESERVOIR ASSEMBLY WITH LOW PRESSURE, DAMAGED GAGE AND DAMAGED SAFETY PIN. RESERVOIR ASSEMBLY WAS REPAIRED WITH THE GAGE, SAFETY PIN AND GAGE WINDOW BEING REPLACED. SERVICE BULLETIN A320 004-25-72 WAS PERFORMED AND EO 2561-01018 WAS COMPLIED WITH. ALL WORK WAS PERFORMED IAW CMM 25-60-56 REV 11.

Part: HYDRAULIC LINE — BLOWN (NR 2 ENGINE) · airframe 20,377 hrs · 7,825 cycles

PHX - DIVERSION - FLT 0361 - EN ROUTE FROM LAX TO IAD RECEIVED ECAM MESSAGE HYDRAULIC RESERVOIR LOW LEVEL, YELLOW QUANTITY INDICATOR ALSO SHOWED LOW, DIVERTED INTO PHX FOR REPAIR. MAINTENANCE FOUND A BLOWN FLEX LINE FOR NR 2 ENGINE HYDRAULIC PUMP PRESSURE SWITCH. REMOVED AND REPLACED FLEX LINE, OPERATIONAL AND LEAK CHECKS WERE GOOD.

Part: HOSE — RUPTURED (RT MLG DOOR ACT) · airframe 20,089 hrs · 7,727 cycles

AFTER TAKEOFF FROM BOS EN ROUTE TO LAS, GREEN HYDRAULIC SYSTEM LOST FLUID DURING LANDING GEAR RETRACTION, TURNED BACK TO BOS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED HYDRAULIC FLEX LINE (A) AND FITTING AT R MAIN GEAR DOOR ACTUATOR AS PER STANDARD PRACTICES, LEAK AND OPERATIONAL CHECKS WERE GOOD. AS A PRECAUTION, REPLACED GREEN HYDRAULIC SYSTEM ENGINE DRIVEN PUMP AND 3 EACH FILTERS. SUPP PART INFORMATION HAS BEEN ADDED TO THIS SDR. PART NAME; SWIVEL, JOINT ASSY, MFG; EATON FLUID, P/N; AE84760Z, LOC; RT MLG DOOR ACTUATOR.

Part: STRUCTURE — DAMAGED (RT MLG DOOR) · airframe 19,721 hrs · 7,620 cycles

ON CLIMB-OUT OF PHX EN ROUTE TO RNO AT FL 200, FELT STRONG AIRFRAME VIBRATION ASSOCIATED WITH A WITH A LOAD RUMBLE, REDUCED SPEED FROM 340 KTS TO 320 KTS AND VIBRATION WENT AWAY, LANDING LIGHTS RETRACTED AT FL 100. MAINTENANCE PERFORMED ELEVATOR FREE PLAY CHECK; LT AND RT ELEVATOR SERVOS ARE WITHIN LIMITS. FOUND RT MLG RAMP DOOR MAIN ATTACH POINT HOLES ELONGATED CAUSING DOOR TO VIBRATE, REMOVED AND REPLACED RT MLG RAMP DOOR ASSEMBLY IAW T/C R4M32308. ALSO, REPLACED BUSHING ON LT MLG FIXED DOOR LOWER ATTACH POINT, OPERATIONAL TEST AND CLEARANCE CHECKS WERE GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FRAME SUPPORT JUST FORWARD OF FR 70, STR 23 LT. MAINTENANCE REMOVED CORRODED FRAME SUPPORT AT FR 70, STR 23 LT; FABRICATED A NEW REPLACEMENT FRAME SUPPORT; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG 1-3, 8, 14 & 17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD END OF SEAT TRACK Y1292 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 FROM FR 12 TO FR 24; INSTALLED NEW REPLACEMENT SEAT TRACK IAW A319 SRM 51-72-11 PG 1 & 2.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE AT AFT END OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF Y1292, BETWEEN FR 69 AND FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-72-11 PG 1 & 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

MC - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR BEAM Y765 FORWARD OF FR 66. MAINTENANCE REMOVED CORRODED BEAM Y765 FORWARD OF FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11, FIG. 101.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 FORWARD AND AFT OF FR 67. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 AT FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11.

Part: SILL — CORRODED (R-2 DOOR) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

DURING B-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT PROFILE SILL FORWARD OF THE R-2 DOOR AT FR 66. MAINTENANCE CUT OUT CORRODED SECTION OF PROFILE SILL AT FR 66; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A319 SRM 53-41-14 FIG 201.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

MCN - MAJOR REPAIR - DURING B-03 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE AT THE AFT END OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE Y1292 FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-3, 8, & 14-17.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,436 hrs · 7,223 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 AT FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 9-18.

Part: WIRE HARNESS — DAMAGED (SEAT ROW 14 LT) · airframe 18,344 hrs · 7,188 cycles

DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 14 LT FROM WALL DISCONNECT 7260V TO SEAT CONNECTOR 5751VC-A, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 12 LT) · airframe 17,197 hrs · 6,793 cycles

PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD.

Part: ACTUATOR — BINDING (SLATS) · airframe 13,071 hrs · 5,225 cycles

EMERGENCY LANDING - FLT 0571 - ON LANDING, RECEIVED CLASS 1 SLAT FAULT, EMERGENCY DECLARED, LANDED WITHOUT SLATS. MAINTENANCE INSPECTED SLAT SYSTEM AND FOUND THE TORQUE LIMITER INDICATOR VISIBLE ON THE NR 2 SLAT ROTARY ACTUATOR. REMOVED AND REPLACED THE NR 2 SLAT ROTARY ACTUATOR IAW AMM 27-84-49-04, OPERATIONAL CHECK WAS GOOD. VENDORS INSPECTION AND FUNCTIONAL TEST OF SLAT ROTARY ACTUATOR S/N 17022 WAS NO FAULT FOUND.

Part: LINE — LOOSE (NR 1 ENGINE) · airframe 11,364 hrs · 4,571 cycles

FLT 841 - ENROUTE FROM PHX TO RDU THE NR 1 ENGINE INDICATED LOW OIL QUANTITY, ENGINE WAS LOSING OIL AT A RATE OF 1 QUART OF OIL IN 5 MINUTES, DIVERTED AND LANDED AT BNA, UPON ARRIVAL AT GATE ENGINE HAD 7.5 QUARTS OF OIL REMAINING. MAINTENANCE INSPECTED THE NR 1 ENGINE AND FOUND THE OIL FEED LINE AT THE BOTTOM OF THE ENGINE JUST AFT OF THE FORWARD EDGE OF C-DUCTS LOOSE AND LEAKING OIL. RETORQUED AND SAFETIED THE LINE, RAN ENGINE WITH NO LEAKS NOTED. PERFORMED MAINTENANCE IAW AMM 70-23-11, AND 71-00-00-710-012.

Part: SMOKE — DETECTED (COCKPIT) · airframe 3,347 hrs · 1,369 cycles

ON LANDING, SMOKE OBSERVED IN COCKPIT, APU WAS OFF BOTH PACKS RUNNING, NO ECAM FOR AVIONICS SMOKE. INSPECTED AVIONICS AREA AND MAIN EQUIPMENT AREA. RAN PACKS, NO EVIDENCE OF SMOKE OR DAMAGE TO EQUIPMENT. OK FOR SERVICE. RECOMMENDATION: REMAIN OPEN, MONITOR.