N102UW

Part: BOTTLE — RUPTURED (ZONE 800) · airframe 70,817 hrs · 38,393 cycles

AIRCRAFT WAS NOT GROUNDED: UPON ARRIVAL THE R1 DOOR DAMPENER WAS BLOW. DISC RUPTURED SHEERPIN SHEERED. MAINTENANCE REPLACED R1 DOOR DAMPER EMERGENCY OPERATION CYLINDE IAW AMM 52-11-14-000-001-B.

Part: SLIDE RAFT — BULGED (ZONE 800) · airframe 70,817 hrs · 38,393 cycles

AIRCRAFT WAS GROUNDED: UPON TRYING TO ARM DOOR 1R, F/A ADVISED COULDN'T MOVE HANDLE. REOPENED R1 FOR POSSIBILE RESET, STILL WON'T ARM. DOOR FELT CAUGHT FROM BELOW. MAINTENANCE REPLACED R1 DOOR SLIDE IAW J/C 27L00025011.

Part: APU — CONTAMINATED (ZONE 100) · airframe 70,718 hrs · 38,327 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORT DIRTY FEET SMELL ON DECENT. A FAINT ODOR WAS NOTED IN THE FLIGHT DECK. MAINTENANCE ACCOMPLISHED SMOKE / ODOR / FUME APU TROUBLESHOOTING TASK CARD 26L00021002 AND ACCOMPLISHED A DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM PER TASK CARD 26L00021014. A SATISFACTORY LEAK / OPERATIONAL CHECK WITH NO ISSUES OR ODORS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 70,718 hrs · 38,327 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORT DIRTY FEET SMELL ON DECENT. A FAINT SMELL WAS NOTED IN THE FLIGHT DECK. (OPEN)

Part: WIRE HARNESS — SHORTED (ZONE 200) · airframe 69,415 hrs · 37,512 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU (11WL) INDICATES A UNIT FAULT WHEN PERFORMING BITE CHECK. FOUND EMERGENCY LIGHT SEAT TO WALL CABLE AT ROW 9ABC SHORTED TO GROUND CAUSING UNIT FAULT INDICATION ON EPSU (11WL). MAINTENANCE REPLACED SEAT TO WALL CABLE AT ROW 9ABC IAW AMM 33-51-19-400-001-A.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 69,195 hrs · 37,376 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT ROW LIGHTS INOP. MAINTENANCE REPLACED EMERGENCY EXIT ROW POWER SUPPLY UNIT IN REF TO AMM 33-51-38.

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 69,105 hrs · 37,316 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK DISCOVERED EXIT ROW LIGHTS INOP. MAINTENANCE T/S EXIT ROW LIGHTS AND FOUND THE EMERGENCY POWER SUPPLY UNIT (EPSU) AT FAULT. REPLACED RIGHT EPSU UNIT IAW AMM 33-51-38

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 68,899 hrs · 37,196 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND EMERGENCY LIGHTS INOP AT ROW 9, 10 AND 11ON THE ISLE. FOUND EPSU 12WL WITH A UNIT FAULT AFTER BITE CHECK. REMOVED ANDREPLACED EPSU 12WL IAW AMM 33-51-38. ALL OPS TEST GOOD. A/C OK FOR SERVICE.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 68,487 hrs · 36,950 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND 2 EA SEAT EMERGENCY LIGHTS AND 2 EA RH SIDEWALL EMERGENCYLIGHTS INOP BETWEEN SEAT ROWS 9 -11. MAINTENANCE REPLACED EPSU 12WL OPS CHECK GOOD ALL IN REF AMM 33-51-38.

Part: LINE — LEAKING (APU OIL SYS) · airframe 68,414 hrs · 36,899 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK ODOR DETECTED ON FLIGHT DECK ONLY. FIRST NOTICED AFTER ENGINE START AND SUSPECTED IT WAS ASSOCIATED WITH HEAVY RAIN AT TIME. DISSIPATED AFTER CLIMBOUT AND SEEMED NORMAL DURING CRUISE. ODOR RETURNED DURING DESCENT IN CLEAR AIR WITH ENGINES AT IDLE POWER. MAINTENANCE FOUND APU LEAKING OIL FROM FLEX TUBES ON TOP OF CASE BEHIND COOLING FAN. DUE TO GOUGED CASE. REPLACED APU IAW J/C 26L31049003.

Part: UNKNOWN — ODOR (CABIN) · airframe 68,414 hrs · 36,899 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK ODOR DETECTED ON FLIGHT DECK ONLY. FIRST NOTICED AFTER ENGINE START AND SUSPECTED IT WAS ASSOCIATED WITH HEAVY RAIN AT TIME. DISSIPATED AFTER CLIMBOUT AND SEEMED NORMAL DURING CRUISE. ODOR RETURNED DURING DESCENT IN CLEAR AIR WITH ENGINES AT IDLE POWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 68,376 hrs · 36,872 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT ESCAPE PATH LIGHTING INOP AT ROWS 9 & 11. MAINTENACE REPLACED CABIN EMERGENCY POWER SUPPLY IAW AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 68,259 hrs · 36,793 cycles

AIRCRAFT WAS NOT GROUNDED: RH EPSU FAILED EMERGENCY LIGHTS OPS CK. MAINTENANCE REPLACED EPSU IAW AMM 33-31-58.

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 68,160 hrs · 36,729 cycles

AIRCRAFT WAS GROUNDED: WHILE PERFORMING J/C 26L00005005 FOUND OVER WING EXIT EMERGENCYLIGHTS OUT ADJACENT TO DOORS AND ABOVE AFT L2 DOOR EMERGENCY EXIT LIGHT OUT. RE-SECURED CONNECTOR ON L2 OVERHEAD LIGHT.

Part: PROXIMITY SENSOR — FAULTED (ZONE 700) · airframe 68,152 hrs · 36,724 cycles

AIRCRAFT WAS GROUNDED: L/G SYSTEM DISAGREE MSG AFTER LANDING AIRCRAFT RETURNED TO PHL FOR MAINTENANCE. PER TSM 32-31-00-810-842-A. FOUND 25GA PROX. SENSOR FAULTED PERFUNCTIONAL TEST 32-31-00-720-003-A. R&R PROX SENSOR 25GA AND RE-SHIMMED PER AMM 32-31-73-400.

Part: BOTTLE — LEAKING (L4 DOOR) · airframe 66,701 hrs · 35,862 cycles

AIRCRAFT WAS GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE FOUND AT ZERO PSI. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 66,634 hrs · 35,823 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR ASSIST BOTTLE PRESSURE 0 PSI. 2L DOOR ASSIST SERVICED.

Part: FITTING — CRACKED (LT MLG DOOR) · airframe 66,393 hrs · 35,679 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR AFT FITTING ON THE KEEL BEAM CRACKED. REPLACED FITTING PER EA 351818.

Part: FITTING — CRACKED (RT MLG DOOR) · airframe 66,393 hrs · 35,679 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITTING ON THE KEEL BEAM CRACKED. REPLACED FITTING PER EA 351815.

Part: PUMP — WARNING MESSAGE (ZONE 500 - LH WI) · airframe 66,081 hrs · 35,488 cycles

ARCRAFT WAS NOT GROUNDED: FUEL TANK PUMP 1 LOW PRESSURE MESSAGE AT FL 370 DURING CLIMB PUMP INDICATOR FLASH SEVERAL TIMES A MINUTE. DID NOT TRIGGED CAS UNTIL FL 370. REMOVED AND REPLACED TANK 1 BOOST PUMP 1.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 65,418 hrs · 35,113 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 12WL INDICATES UNIT FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORTY OPERATIONAL CHECK.

Part: LEVER — STICKING (ZONE 800 - DOORS) · airframe 64,876 hrs · 34,776 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT SERVICE R4 ARM LEVER CHAFFING AND DIFFICULT TO MOVE. LUBRICATED R4 DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR FRAME — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 64,373 hrs · 34,433 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN AND NOW WILL NOT CLOSE. ADJUSTED DOOR FRAME HEADER PANEL. DOOR OPENS AND CLOSES NORMALLY NOW.

Part: DAMPER — DEFECTIVE (L1 DOOR) · airframe 63,453 hrs · 33,797 cycles

AIRCRAFT WAS GROUNDED: DOOR 1L DOES NOT OPEN ALL THE WAY. MAINTENANCE REPLACED L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 63,435 hrs · 33,789 cycles

AIRCRAFT WAS GROUNDED: WHILE REPAIRING DAMAGE TO THE CABIN WINDSCREEN AT THE L1 DOOR, MAINTENANCE FOUND WIRES 3351-1960, 1961 DAMAGED FOR THE EMERGENCY LIGHT MOUNTED TO THE WINDSCREEN. MAINTENANCE REMOVED AND REPLACED WIRES 3351-1960, 1961 PER WDM 33-51-06 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 63,412 hrs · 33,772 cycles

AIRCRAFT WAS NOT GROUNDED: ECAM DOOR LEFT AFT EMERGENCY EXIT OVERWING FAULTMESSAGE, WITH THE LEFT SIDE OVERWING EXIT SLIDE ARMED LIGHT ON, NO LOSS OF CABIN PRESSURE, MAINTENANCE ADJUSTED PROXIMITY SWITCH HANDLE FLAP 2WV1 PER TSM 52-21-00-810-802-A AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WARNING MESSAGE — ILLUMINATED (LT OVERWING EXIT) · airframe 63,412 hrs · 33,772 cycles

AIRCRAFT WAS NOT GROUNDED: ECAM DOOR LEFT AFT EMERGENCY EXIT OVERWING FAULT MESSAGE, WITH THE LEFT SIDE OVERWING EXIT SLIDE ARMED LIGHT ON, NO LOSS OF CABIN PRESSURE. OPEN

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 63,346 hrs · 33,734 cycles

AIRCRAFT WAS NOT GROUNDED: SMOKE LAVATORY SMOKE ECAM IN FLIGHT UNABLE TO DETERMINE WHICH LAVATORY, ECAM INTERMENTENT. MAINTENANCE ACCOMPLISHED CIDS TEST AND SMOKE TEST NO FAULTS NOTED. GROUND OPERATION CHECKS NORMAL PER AMM 26-17-00.

Part: DOOR — OUT OF ADJUST (L1 LAVATORY) · airframe 63,321 hrs · 33,720 cycles

AIRCRAFT WAS NOT GROUNDED: L1 LAVATORY DOOR DIFFICULT TO CLOSE AND OPEN - STICKS. MAINTENANCE RE-ADJUSTED LAVATORY DOOR PER AMM 25-41-41 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — FAULTED (L1 DOOR) · airframe 63,312 hrs · 33,712 cycles

AIRCRAFT WAS GROUNDED: 1L SLIDE ARMED LIGHT FLASHES WHEN 1L ARMED. MAINTENANCE REPLACED L1 DOOR SLIDE PER TASK CARD 26L00025011.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 63,255 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR ASSIST BOTTLE ACCUMULATOR CHECK PRESSURE MESSAGE. MAINTENANCE SERVICED DOOR ASSIST BOTTLE ACCUMULATOR PER AMM 52-10-00.

Part: SLIDE — DEFORMED (PAX DOOR) · airframe 63,255 hrs · 33,675 cycles

AIRCRADFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 SLIDE HAS DEFORMATION. MAINTENANCE REPLACED SLIDE PER TASK CARD 26C83152008.

Part: HINGE FITTING — CRACKED (LT MLG DOOR) · airframe 63,255 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING AFT LUG WEB IN THE CORNER RADIUS ON THE KEEL BEAM. MAINTENANCE REPLACED HINGE FITTING PER EA 339820.

Part: HINGE FITTING — CRACKED (LT MLG DOOR) · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING AFT LUG WEB IN THE CORNER RADIUS ON THE KEEL BEAM. MAINTENANCE REPLACED HINGE FITTING PER EA 339820.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 63,255 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 12WL INOPERATIVE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 AND AMM 33-51-00.

Part: SLIDE — DEFORMED (ZONE 800 - DOORS) · airframe 63,255 hrs · 33,675 cycles

AIRCRADFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 SLIDE HAS DEFORMATION. MAINTENANCE REPLACED SLIDE PER TASK CARD 26C83152008.

Part: SLIDE RAFT — DEFORMED (ZONE 800 - DOORS) · airframe 63,255 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 SLIDE / RAFT DEFORMED. REPLACED SLIDE / RAFT ASSEMBLY PER TASK CARD 26C84152006.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK 2 ATTACHMNENT / ECCENTRIC BOLT BETWEEN WS 700 AND WS 1957, BETWEEN RIB 2 AND RIB 4. REPLACED BOLT PER TASK CARD 26C61057005.

Part: SIGN — BURNED (ZONE 200 - FUSE) · airframe 63,255 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: BURNED LIGHTS ON EMERGENCY EXIT SIGN BETWEEN LEFT HAND SIDE EMERGENCY EXIT DOORS. REPLACED EMERGENCY EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-16.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER AFT CORNER FITTING AT FR 68 AND S23L. REPLACED CORNER FITTING PER SRM 51-72-11.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPLACED LOWER SILL PER SRM 51-42-11.

Part: SKIN PANEL — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LOWER SKIN PANEL UPPER SURFACE BETWEEN RIBS 5 AND 6 AT STRINGER 2. REPAIRED SKIN PANEL PER EA 339295.

Part: TRACK — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP INTERNAL ATTACH FITTING TRACK 4, BETWEEN RIB 14 AND RIB 15. MAINTENANCE REPLACED FLAP PER AMM 27-54-62.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: DOOR — CRACKED (ZONE 100 - FUSE) · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CARGO COMPARTMENT DOOR INNER SKIN NEAR THE CUT OUT ADJACENT TO BEAM 4. AFT CARGO DOOR INTERNAL SKIN REPAIRED PER EA 338856.

Part: AILERON — CRACKED (ZONE 600 - RH WI) · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON CHANNEL CRACKED. MAINTENANCE REPAIRED AILERON PER EA 339447.

Part: SKIN — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SKIN PANEL 2 LOWER SURAFCE AT THE REAR SPAR TRAILING EDGE BETWEEN RIB 7 AND RIB 8. MAINTENANCE REPAIRED SKIN PANEL PER EA 338990.

Part: SKIN PANEL — CORRODED (ZONE 500 - LH WI) · airframe 63,256 hrs · 33,675 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE UPPER SKIN PANEL LOWER SURFACE BETWEEN RIB 7 AND RIB 8. REPAIRED SKIN PANEL PER EA 338990.

Part: DIAPHRAGM — LEAKING (ZONE 800 - DOORS) · airframe 62,944 hrs · 33,518 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND AFT PASSENGER DOOR EMERGENCY OPERATION CYLINDER NOT HOLDING PRESSURE. REPLACED PERCUSSION MECHANISM DIAPHRAGM PER AMM 52-10-00.

Part: COFFEEMAKER — SMOKE (ZONE 900 - LAV/G) · airframe 62,889 hrs · 33,472 cycles

AIRCRAFT WAS NOT GROUNDED: SMOKE REPORTED COMING FROM GALLEY 1 COFFEE MACHINE. REPLACED GALLEY 1 COFFEE MAKER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-32-00.

Part: LATCH — UNSECURE (ZONE 900 - LAV/G) · airframe 62,858 hrs · 33,451 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY HARD TO OPEN AND CLOSE SECURED LATCH ON AFT LAVATORY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HOOK — OBSTRUCTED (ZONE 800 - DOORS) · airframe 62,618 hrs · 33,276 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT DOOR EMERGENCY SLIDE LEVER "CREEPS " TO DISARMED POSITION AND INDICATES DISARMED IN FLIGHT. REMOVED DEBRIS FROM LEFT AFT GIRT HOOKS,LUBRICATED,AND OPERATED ARMING LEVER,NORMAL AT THIS TIME PER AMM .52-71-00, INDICATIONS NORMAL.

Part: ACCUMULATOR — LOW (ZONE 800 - DOORS) · airframe 62,428 hrs · 33,138 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR ACCUMULATOR REQUIRES SERVICE. SERVICED L4 DOOR ACCUMULATOR PER AMM 52-10-00.

Part: LOCK — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 62,117 hrs · 32,967 cycles

AIRCRAFT WAS NOT GROUNDED:: LAVATORY 3E DOOR LOCK IS STUCK CLOSED. LUBRICATED AND ADJUSTED DOOR LATCH. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-40-00.

Part: NONE — NONE · airframe 61,264 hrs · 32,454 cycles

AIRCRAFT WAS GROUNDED: DOOR R1 WILL NOT FULLY OPEN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DAMPER — DEFECTIVE (ZONE 800 - DOORS) · airframe 61,264 hrs · 32,454 cycles

AIRCRAFT WAS GROUNDED: DOOR R1 WILL NOT FULLY OPEN. **SUPPLEMENTAL REPORT FOR AALA202110255114: REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED ** (CLOSED)

Part: DAMPER — FAULTY (ZONE 800 - DOORS) · airframe 61,264 hrs · 32,454 cycles

AIRCRAFT WAS GROUNDED: DOOR R1 WILL NOT FULLY OPEN. REPLACED R1 DOOR DAMPER PER AMM 52-11-14

Part: COMPUTER — FAILED (SPOILERS) · airframe 60,953 hrs · 32,287 cycles

AIRCRAFT WAS NOT GROUNDED: DURING CLIMB THROUGH FL 360 ECAM FOR FLIGHT CONTROL GROUND SPOILER 1 AND 2 FAULT NO SPOILERS DEPLOYED DURING FLIGHT. REPLACED SPOILER ELEVATOR COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER 27-94-34-400.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,422 hrs · 31,985 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT IN SEAT EMERGENCY EXIT LIGHT INOPERATIVE AT ROWS 13, 17, 22, 26. REMOVED AND REPLACED RIGHT MID POWER SUPPLY UNIT AND AFT GALLEY POWER SUPPLY UNIT (AALA202106289008) PER AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,422 hrs · 31,985 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT IN SEAT EMERGENCY EXIT LIGHT INOPERATIVE AT ROWS 13, 17, 22, 26. REMOVED AND REPLACED RIGHT MID POWER SUPPLY UNIT (AALA202106289002) AND AFT GALLEY POWER SUPPLY UNIT PER AMM 33-51-38.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,230 hrs · 31,882 cycles

AIRCRAFT WAS GROUNDED: SEAT ROW 13 LEFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (AALA202106039004) AND BATTERY PER AMM 35-51-38-400-002-A.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,230 hrs · 31,882 cycles

AIRCRAFT WAS GROUNDED: SEAT ROW 13 LEFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY (AALA202106039007) PER AMM 35-51-38-400-002-A.

Part: O-RING — WORN (HYD SYSTEM) · airframe 59,316 hrs · 31,337 cycles

AIRCRAFT WAS GROUNDED. DURING DESCENT, ECAM FOR "HYD Y RSVR LO LEVEL" EMERGENCY DECLARED. ACCOMPLISHED ECAM PROCEDURES, LANDED NORMALLY, AND TAXIED TO GATE. FOUND BAD O-RING ON YELLOW SYSTEM HYDRAULIC POWER TRANSFER UNIT RETURN LINE QUICK DISCONNECT. REPLACED O-RING WITH NEW, IAW AMM 29-13-15. LEAK AND OPERATIONS CHECK GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 58,917 hrs · 31,074 cycles

AIRCRAFT WAS GROUNDED: DURING PERIODIC SERVICE CHECK FOUND EMERGENCY POWER SUPPLY UNIT AFT LEFT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY FOR EMERGENCY LIGHTS PER AMM 33-51-38.

Part: GFI — INOPERATIVE (FUEL SYSTEM) · airframe 58,323 hrs · 30,667 cycles

AIRCRAFT NOT GROUNDED. FUEL PUMP #2 INOP FOR CENTER TANK AFTER TAKE OFF, WOULD NOT RESET WITH ECAM PROCEDURE. REPLACED # 2 CENTER TANK PUMP GFI (70QA) PER ESPM 20-46-50 AND AMM 28-21-00.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 58,118 hrs · 30,521 cycles

AIRCRAFT NOT GROUNDED - DURING DESCENT BOTH NAVIGATIONAL DISPLAYS INDICATED "MAP NOT AVAIL" FOR ABOUT 15-20 SEC THEN RETURNED TO NORMAL. RESET FLIGHT MANAGEMENT GUIDANCE COMPUTER 1 & 2, OPERATIONAL CHECKS SATISFACTORY PER AMM 22-96-00-0501. PERFORMED LAND TEST SATISFACTORY PER AMM 22-97-00-0501. LMP STATUS - AIRCRAFT REMAINS CAT III DUAL STATUS PER TSM 22-83-00-0201.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 57,749 hrs · 30,316 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR LOWER SURFACE SKIN CRACKED 103.5 INCHES FROM THE INBOARD END AND 14.75 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-004.

Part: ATTACH FITTING — CRACKED (RT MLG DOOR) · airframe 57,749 hrs · 30,316 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR ACTUATOR AFT ATTACH FITTING VERTICAL LEG 2ND FASTENER HOLE FROM THE TOP CRACKED ON THE KEEL BEAM BETWEEN FR 42 AND FR 43 AT -Y440. REPAIRED ATTACH FITTING PER EA 302156.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,035 hrs · 29,887 cycles

AIRCRAFT IN BASE MAINTENANCE:L1 DOOR CUT OUT INTERCOSTAL CRACKED AT FR 16 AND DOOR STOP #7. REPLACED INTERCOSTAL PER EA 298384.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,035 hrs · 29,887 cycles

AIRCRAFT IN BASE MAINTENANCE:L1 DOOR CUT OUT FRAME CRACKED AT FR 16 AND DOOR STOP #1. REPAIRED FRAME PER EA 298359.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,035 hrs · 29,887 cycles

AIRCRAFT IN BASE MAINTENANCE:R1 DOOR CUT OUT INTERCOSTAL CRACKED AT FR 16 AND DOOR STOP #7. REPLACED INTERCOSTAL PER EA 298356.

Part: BEARING — WORN (RT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

RIGHT ELEVATOR, NR 5 HINGE FITTING BEARING HAD EXCESSIVE PLAY AND WAS WORN. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: BEARING — WORN (RT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (RT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (RT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (LT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

LEFT ELEVATOR, NR 3 HINGE FITTING BEARING HAD EXCESSIVE PLAY AND WAS WORN. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: BEARING — WORN (RT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (LT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (RT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (LT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (LT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (LT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: BEARING — WORN (LT ELEVATOR) · airframe 55,756 hrs · 29,128 cycles

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

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 55,224 hrs · 28,872 cycles

LEFT OVERWING EXIT EMERGENCY LIGHT POWER SUPPLY FAILED TO TEST. MAINTENANCE REPLACED THE POWER SUPPLY IAW AMM 33-51-38, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: STRAP — STUCK (L2 DOOR) · airframe 54,943 hrs · 28,706 cycles

THE AIRCRAFT WAS NOT GROUNDED. 2L DOOR RED STRAP STUCK IN DOOR FRAME. REMOVED RED STRAP FROM 2L DOOR FRAME AS REQUIRED.

Part: ENGINE — LEAKING (NR 2) · airframe 54,347 hrs · 28,341 cycles

AFTER TAKEOFF, A MILD ODOR WAS DETECTED IN THE MID TO AFT CABIN. THE ODOR WAS SLIGHTLY INTENSIFIED AND PASSENGERS COMPLAINED OF SINUS AND EYE IRRITATION. THE AIRCRAFT DIVERTED. ACCOMPLISED INITIAL SOF TC. FOUND EVIDENCE OF AN OIL LEAK ON VARIABLE STATOR VANE AREA AT THE 6'OCLOCK POSITION AND LOW PRESSURE TURBINE, AIR COOLING PIPE FORWARD AND AFT FLANGE WET OF OIL. REPLACED THE NR 2 RIGHT ENGINE IAW JC 26L40071001.

Part: AIR FILTER — CLOGGED (ZONE 200) · airframe 54,347 hrs · 28,341 cycles

THE AIRCRAFT WAS GROUNDED. ODOR IN CABIN- DIRTY SOCKS ON TAKEOFF MILD ODOR DETECTED MID TO AFT CABIN. LEVEL AT 19,000 ODOR SLIGHTLY INTENSIFIED AND TO PAXS. COMPLAINED ON SINUS/EYE IRRITATION. A RESIDUE CLOGGED AIR FILTER REVEALED TO BE THE SOURCE OF THE ODOR. REPLACED AEVC FILTER PER AMM 21-26-43. ACCOMPLISHED CABIN ODOR JOB CARD 26L00021001 WITH FLIGHT CREW ASSISTANCE. NO ODORS DETECTED DURING OR AFTER ENGINE AND APU RUNS. AIRCRAFT OK FOR SERVICE.

Part: ACCESS PANEL — DETACHED (EMERGENCY EXIT) · airframe 54,263 hrs · 28,289 cycles

ON FINAL APPROACH, LT DOOR FWD EMER EXIT ECAM ILLUMINATED, COVER CAME OFF OF THE HANDLE ACCESS. REINSTALLED LEFT FORWARD EMERGENCY EXIT DOOR HANDLE ACCESS PANEL IAW AMM 52-73-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,257 hrs · 28,283 cycles

ROW 11R EMERGENCY EXIT LIGHT LENS WAS MISSING. INSTALLED THE LENS. OK FOR SERVICE.

Part: CONTAINER — CRACKED (LT OVRWG SLIDE) · airframe 53,911 hrs · 28,068 cycles

FOUND A CRACK ON THE LEFT OVERWING SLIDE BOX ALONG THE AFT EDGE. REPLACED THE SLIDE ENCLOSURE J/C 26L20025014, CHECKED OK.

Part: HANDLE — DISPLACED (L1 DOOR) · airframe 53,817 hrs · 28,017 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR ASSIST HANDLE CAP FELL OFF. MAINTENANCE REINSTALLED DOOR ASSIST HANDLE AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 53,597 hrs · 27,884 cycles

FORWARD EMERGENCY LIGHT POWER SUPPLY FAULTY. REPLACED THE POWER SUPPLY IAW AMM 33-51-38-000-001A/400-001-A.

Part: CIDS — MALFUNCTIONED (R2 DOOR SLIDE) · airframe 53,513 hrs · 27,838 cycles

R2 DOOR WHEN ARMED DOES NOT SHOW SLIDE ON THE ECAM INDICATING THAT IT`S ARMED. ACCOMPLISHED A CIDS 1 & 2 RESET. SLIDE ARMED. OPS CHECKED IAW AMM 23-73-00.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 52,798 hrs · 27,441 cycles

L2 DOOR EMERGENCY CYLINDER DOOR DAMPER PRESSURE IS LOW, READING 800 PSI. CHARGED THE CYLINDER IAW MM 52-10-00-614-001-A.

Part: REGULATOR VALVE — CONTAMINATED · airframe 52,797 hrs · 27,440 cycles

ODOR IN REAR CABIN DURING DESCENT, AND AT THE GATE WITH APU RUNNING. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED J/C'S 26L00021001, TROUBLESHOT THE CABIN AIR QUALITY. APU ODOR IN CABIN. DECONTAMINATED THE ECS. FOUND AN INTERNAL OIL LEAK ON THE APU. ALL REQUIRED PACK COMPONENTS CHANGED. REPLACED THE AFT CARGO TRIM AIR VALVE IAW AMM 21-43-51.

Part: REHEATER — CONTAMINATED (ZONE 200 - FUSE) · airframe 52,797 hrs · 27,440 cycles

ODOR IN REAR OF THE CABIN DURING DESCENT, AND AT THE GATE WITH APU RUNNING. AIRCRAFT WAS GROUNDED. ACCOMPLISHED J/C 26L00021001, 26L00021002, AND 26L00021004. FOUND AN INTERNAL OIL LEAK IN THE APU, CHANGED THE APU IAW MIC 3200612. ALL PACK COMPONENTS CHANGED, IAW MIC 3200613, 3200614, 3200615, AND 320616. REPLACED THE APU IAW J/C 26L31049003.

Part: FILTER — CONTAMINATED (APU) · airframe 52,797 hrs · 27,440 cycles

ODOR IN REAR OF THE CABIN DURING DESCENT, AND AT THE GATE WITH APU RUNNING. AIRCRAFT WAS GROUNDED. ACCOMPLISHED J/C 26L00021001, 26L00021002, AND 26L00021004. FOUND AN INTERNAL OIL LEAK IN THE APU, CHANGED THE APU IAW MIC 3200612. ALL PACK COMPONENTS CHANGED, IAW MIC 3200613, 3200614, 3200615, AND 320616. REPLACED THE APU IAW J/C 26L31049003.

Part: CONDENSER — CONTAMINATED (APU) · airframe 52,797 hrs · 27,440 cycles

ODOR IN REAR OF THE CABIN DURING DESCENT, AND AT THE GATE WITH APU RUNNING. AIRCRAFT WAS GROUNDED. ACCOMPLISHED J/C 26L00021001, 26L00021002, AND 26L00021004. FOUND AN INTERNAL OIL LEAK IN THE APU, CHANGED THE APU IAW MIC 3200612. ALL PACK COMPONENTS CHANGED, IAW MIC 3200613, 3200614, 3200615, AND 320616. REPLACED THE APU IAW J/C 26L31049003.

Part: APU — LEAKING · airframe 52,797 hrs · 27,440 cycles

ODOR IN REAR OF THE CABIN DURING DESCENT, AND AT THE GATE WITH APU RUNNING. AIRCRAFT WAS GROUNDED. ACCOMPLISHED J/C 26L00021001, 26L00021002, AND 26L00021004. FOUND AN INTERNAL OIL LEAK IN THE APU, CHANGED THE APU IAW MIC 3200612. ALL PACK COMPONENTS CHANGED, IAW MIC 3200613, 3200614, 3200615, AND 320616. REPLACED THE APU IAW J/C 26L31049003.

Part: OIL SYSTEM — LEAKING (APU) · airframe 52,797 hrs · 27,440 cycles

ODOR IN REAR CABIN DURING DESCENT, AND AT THE GATE WITH APU RUNNING. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED J/C'S 26L00021001, TROUBLESHOT THE CABIN AIR QUALITY. APU ODOR IN CABIN. DECONTAMINATED THE ECS. FOUND AN INTERNAL OIL LEAK ON THE APU. ALL REQUIRED PACK COMPONENTS CHANGED. REPLACED THE AFT CARGO TRIM AIR VALVE IAW AMM 21-43-51.

Part: OIL COOLER — ODOR (NR 1 IDG) · airframe 52,790 hrs · 27,435 cycles

DURING DECENT BELOW 10,000 FEET, A STRONG ODOR OF POSSIBLE UNBURNED OIL, LIKE A SWEAT SOCK. AIRCRAFT WAS GROUNDED. TROUBLESHOT CABIN AIR QUALITY, CABIN ODOR TROUBLESHOT AND DECONTAMINATED. REPLACED THE NR 1 ENGINE INTEGRATED DRIVE GENERATOR OIL COOLER IAW AMM 73-11-60.

Part: LATCH — DIRTY (L1 GIRT BAR) · airframe 52,721 hrs · 27,398 cycles

L1 DOOR SLIDE ARMED INDICATION INTERMITTENT ON SIDS PANEL AND ON COCKPIT SYSTEM DISPLAY WITH THE HANDLE ARMED. REMOVED DEBRIS FROM THEL GIRT BAR LATCH.

Part: HANDLE — DETACHED (L2 DOOR) · airframe 52,721 hrs · 27,398 cycles

DOOR ASSIST HANDLE CAME OFF THE L2 DOOR. INSTALLED THE L2 DOOR ASSIST HANDLE CAP.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,545 hrs · 27,292 cycles

EMERGENCY EXIT SIGN AT SEAT 1C MISSING. INSTALLED A NEW LENS IAW AMM 33-51-00.

Part: PROXIMITY SWITCH — FAULTY (DOOR) · airframe 52,381 hrs · 27,218 cycles

AIRCRAFT NOT GROUNDED, CLIMBING THRU FL 200 GOT ECAM MSG " DOOR R FWD EMERGENCY EXIT" NO ABNORMAL CABIN PRESS NOTED.ADJUSTED PROXIMITY SWITCH ( 19WV2) AS REQ OPS CHECKK GOOD , NO DEFECTS NOTED.

Part: DOOR — UNKNOWN (R1) · airframe 52,359 hrs · 27,206 cycles

AIRCRAFT WAS NOT GROUNDED: ON DESCENT AT 10,000 FEET INTO CLT, RECEIVED AN ECAM MESSAGE REGARDING DOOR RIGHT FOWARD EMERGENCY EXIT, NO CHANGE IN CABIN PRESSURE. RESECURED RIGHT FOWARD DOOR PER AMM 52-70-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 52,352 hrs · 27,202 cycles

AIRCRAFT WAS NOT GROUNDED: ON CLIMBOUT, RIGHT OVERWING EXIT DOOR COVER FELL OFF, ARM LIGHT APPEARED, NO ABNORMAL CABIN PRESSURE WAS OBSERVED. REINSTALLED COVER FLAP ON FOWARD RIGHT EMERGENCY EXIT DOOR PER AMM 52-70-00.

Part: SELECTOR VALVE — LEAKING (CARGO DOOR) · airframe 52,343 hrs · 27,197 cycles

AIRCRAFT NOT GROUNDED. HOT OILY SMELL IN COCKPIT AND CABIN LEVELING 5000 FEET, LASTED APPROXIMATELY 8-10 MINUTES. SMELL SEEMED TO DISSIPATE LEVELING 4000 FEET. SMELLED AGAIN AFTER LANDING WITH #2 ENGINE SHUT DOWN AND APU ON. ALL ENGINE INDICATIONS NORMAL. REPLACED AFT CARGO DOOR SELECTOR VALVE PER AMM 25-54-00.

Part: COOLING FAN — ODOR (APU) · airframe 52,289 hrs · 27,158 cycles

AIRCRAFT WAS GROUNDED. CABIN CREW REPORTED STRONG FUMES IN THE AFT PART OF THE CABIN ON FINAL APPROACH. NO EMERGENCY DECLARED. LANDING UNEVENTFUL. ACCOMPLISHED JOB CARD 26L00021001 FOR CABIN AIR QUALITY AND FOUND APU TO BE SOURCE. REPLACED APU OIL COOLING FAN PER AMM 49-52-51. LEAK AND OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,203 hrs · 27,105 cycles

FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INDICATOR NOT FLASHING. REPLACED THE BATTERY IAW AMM.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

L2 DOOR EMERGENCY ASSIST RESERVOIR PRESSURE LOW. SERVICED THE DOOR ASSIST BOTTLE AMM.

Part: PIN — CORRODED (RT MLG PINTLE) · airframe 52,171 hrs · 27,085 cycles

RIGHT MAIN LANDING GEAR AFT PINTLE PIN WAS CORRODED. REPLACED PINTLE PIN IAW 26T00032001.

Part: PIN — CORRODED (LT MLG PINTLE) · airframe 52,171 hrs · 27,085 cycles

LEFT MAIN LANDING GEAR REAR PINTLE PIN WAS CORRODED. REPLACED THE PINTLE PIN IAW RD 26T00032001.

Part: LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 52,105 hrs · 27,041 cycles

RIGHT FOWARD EMERGENCY EXIT ILLUMINATED ON ECAM IN FLIGHT ALTITUDE 3000 FT. CHECKED RIGHT FOWARD EMERGENCY EXIT DOOR IAW AMM 52-20-00.NO FAULTS NOTED. NO HISTORY LAST 90 DAYS.

Part: GIRT BAR — DIRTY (R2 DOOR SLIDE) · airframe 52,009 hrs · 26,972 cycles

R2 DOOR DIFFICULT TO ARM. REMOVED DEBRIS FROM AFT R2 GIRT BAR TRACK, DOOR ARMS NORMALLY THIS PER AMM .

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,873 hrs · 26,880 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT LENS BROKEN OFF.

Part: LENS — MISSING (CABIN) · airframe 51,842 hrs · 26,859 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT ENTRY DOOR EMERGENCY EXIT LENS MISSING. INSTALLED LEFT ENTRY DOOR EMERGENCY EXIT LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 51,599 hrs · 26,734 cycles

R2 DOOR ASSIST BOTTLE LOW, REQUIRES SERVICE. SERVICED R2 DOOR ASSIST BOTTLE.

Part: FAN — FAILED (COOLING) · airframe 51,529 hrs · 26,701 cycles

DURING DESCENT, ENGINE IDLE, SMELLED A STRONG ODOR IN THE COCKPIT. HAPPENED AGAIN IN IDLE ON RAMP. SMELLED LIKE ENGINE EXHAUST. MAINTENANCE PERFORMED JOB CARD 26L00021001 CABIN AIR QUALITY AND 26L00021002 APU ODOR IN CABIN. REPLACED COOLING FAN IAW AMM 49-52-51. PERFORMED APU INLET CLEANING IAW JOB CARD 26T31049004 AND DECONTAMINATION IAW JOB CARD 26L00021004.

Part: COOLING FAN — MALFUNCTIONED (APU BAY) · airframe 51,457 hrs · 26,668 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A STRONG OBNOXIOUS ODOR WITH APU ON THROUGHOUT FLIGHT DECK AND CABIN. MAINTENANCE FOUND APU AIR INTAKE CONTAMINATED WITH DIRT AND FLUIDS. MAINTENANCE FOUND COOLING FAN LEAKING ON APU, REPLACED COOLING FAN PER AMM 49-52-51. PERFORMED APU INLET CLEANING PER J/C 26T31049004 AND DECONTAMINATION OF ECS PER J/C 26L00021004. ACCOMPLISHED SATIFACTORY OPERATIONS CHECK AND LEAK CHECK.

Part: CONNECTOR — BROKEN (CABIN) · airframe 51,294 hrs · 26,594 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY LIGHT AT ROW 18 HAS A BROKEN BACKSHELL AT 205WLA. REMOVED AND REPLACED BACKSHELL. OPERATIONAL CHECK GOOD.

Part: STRAP — MISROUTED (L1 DOOR SLIDE) · airframe 51,291 hrs · 26,593 cycles

L1 DOOR SLIDE HAS YELLOW RELEASE STRAP ROUTED THRU TRIGGER OF GIRT BAR. REPOSITION THE RELEASE STRAP ON THE L1 DOOR SLIDE.

Part: STRAP — MISLOCATED (R2 DOOR SLIDE)

R2 DOOR EMERGENCY EXIT SLIDE HAS YELLOW RELEASE STRAP ROUTED THRU TRIGGER OF GIRT BAR. REPOSITION YELLOW RELEASE STRAP R2 DOOR.

Part: STRAP — MISLOCATED (R1 DOOR SLIDE)

R1 DOOR EMERGENCY SLIDE HAS YELLOW RELEASE STRAP ROUTED THRU TRIGGER OF GIRT BAR. REPOSITION YELLOW RELEASE STRAP R1 DOOR.

Part: SIGHT GLASS — MISSING (PAX DOOR SLIDE) · airframe 51,183 hrs · 26,540 cycles

FOWARD LEFT DOOR ASSIST BOTTLE SIGHT LENS ON DOOR SUPPORT ARM LINING MISSING. INSTALLED SIGHT LENS IAW AMM 25-23-45.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 50,991 hrs · 26,417 cycles

FORWARD LEFT EMERGENCY EXIT COVER FELL OFF IN FLIGHT CAUSING ECAM WARNINGS. INSTALLED LENS COVER.

Part: GIRT BAR — FAULTY (L1 DOOR) · airframe 50,550 hrs · 26,166 cycles

AFTER TAKE OFF, THE L1 DOOR CABIN PRESSURE RED LIGHT BEGAN FLASHING. SLIDE ARMED INDICATIONS DISAPPEARED FROM THE DOOR INDICATOR AND FROM ECAM DOOR SYSTEMS PAGE. ACFT PRESSURIZED NORMALLY RED FLASHING CABINE PRESSURE LIGHT STOPPED AFTER LANDING. AIRCRAFT WAS GROUNDED. REPLACED THE GIRT BAR.

Part: BELLCRANK — CRACKED (L1 DOOR) · airframe 50,550 hrs · 26,166 cycles

AFTER TAKE OFF, THE L1 DOOR CABIN PRESSURE RED LIGHT BEGAN FLASHING.SLIDE ARMED INDICATIONS DISAPPEARED FROM THE DOOR INDICATOR AND FROM ECAM DOOR SYSTEMS PAGE. ACFT PRESSURIZED NORMALLY RED FLASHING CAB PRESS LIGHT STOPPED AFTER LANDING. AIRCRAFT WAS GROUNDED. REPLACED UPPER FLAP BELLCRANK ASSEMBLY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,806 hrs · 25,759 cycles

EMERGENCY LIGHT LENS MISSING AT 26C. MAINTENANCE INSTALLED THE LENS IAW AMM 33-51-19.

Part: SLIDE — OBSTRUCTED (L1 DOOR) · airframe 49,365 hrs · 25,514 cycles

L1 DOOR SLIDE RAFT HAS DEFORMATION AND CONTACTS FUSELAGE WHEN DOOR IS OPEN. REPLACED SLIDE RAFT PER AMM 25-62-44-400-007-A.

Part: SLIDE — OBSTRUCTED (L2 DOOR) · airframe 49,365 hrs · 25,514 cycles

L2 DOOR SLIDE RAFT HAS DEFORMATION AND CONTACTS THE FUSELAGE WHEN DOOR IS FULL OPEN. REPLACED SLIDE PER AMM 25-62-44-400-007-A.

Part: HINGE FITTING — CORRODED (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT AFT NOSE GEAR DOOR HINGE FITTING ASSY. REPLACED HINGE FITTING ASSY IAW SRM 51-42-11, SRM 51-49-00 AND DWG D52810089.

Part: FITTING — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON RIGHT FORWARD GALLEY CENTER FITTING BETWEEN FRAMES 16 - 20 AT STRINGER 23L. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112225.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY STR 26R BETWEEN FRAME 66 TO FRAME 67. REPAIRED STR IAW SRM 51-72-11 AND EA 263311.

Part: CONNECTOR — CORRODED (TE FLAP) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT WING INBD FLAP INTERCONNECTING STRUT ELECTRICAL CONNECTOR. REPLACED INTERCONNECTING STRUT IAW AMM 27-51-44-820-001-A.

Part: BELLCRANK — OUT OF ADJUST (PAX DOOR) · airframe 49,365 hrs · 25,514 cycles

PASSENGER CREW DOOR, 842 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PERCUSSION BELLCRANK FINGER DIMENSION IS OUT OF ADJUSTMENT. ADJUSTED PERCUSSION BELLCRANK FINGER DIMENSION IAW AMM 52-13-14-820-002-A.

Part: FRAME — CRACKED (FRM 4) · airframe 49,365 hrs · 25,514 cycles

CRACK ON RIGHT COCKPIT CENTER POST LOWER ATTACHMENT FRAME 4. REPAIRED FRAME IAW EA 262868.

Part: WINDOW FRAME — CRACKED (FRAME 4) · airframe 49,365 hrs · 25,514 cycles

CRACK INDICATION IN COCKPIT LEFT CENTER POST FRONT WINDOW LOWER ATTACHMENT UPPER FASTENER HOLE AT FR 4. REPAIRED FRAME IAW EA 262868.

Part: BOLT — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON LEFT WING FORWARD BOLT AT THE NR 1 SLAT, TRACK NR 4 BETWEEN RIB 5 - 6. REPLACED FORWARD BOLT IAW AMM 27-84-63-400-002-A.

Part: BOLT — CORRODED (LT WING) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON LT WING UPPER AFT SLAT BOLT AT SLAT NR 5, TRACK NR 12 BETWEEN RIB 25-27. REPLACED SLAT BOLT IAW AMM 27-84-67-400-002-A, STEP 4C, 2, A, B, F, H, M AND 4D 13.

Part: BOLT — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON LEFT WING UPPER FORWARD SLAT BOLT AT SLAT NR 5, TRACK NR 12 BETWEEN RIB 25 - 26. REPLACED THE SLAT BOLT IAW AMM 27-84-67-400-002-A.

Part: FITTING — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON LEFT FORWARD GALLEY LOWER SILL CENTER FITTING BETWEEN FRAMES 16 AND 20. REPLACED THE FITTING IAW SRM A320 51-72-11 AND DRAWING D53112225.

Part: BOLT — CORRODED (LT WING) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON LT WING UPPER FORWARD SLAT BOLT AT SLAT NR 2, TRACK NR 6 BETWEEN RIB 11-12. REPLACED SLAT BOLT IAW AMM 27-84-64-000-001-A AND AMM 27-84-64-400-002-A.

Part: BOLT — CORRODED (LT WING) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT WING UPPER SLAT BOLT AT SLAT NR 5, TRACK NR 11 BETWEEN RIB 23-24. REPLACED SLAT BOLT IAW AMM 27-84-67-400-002-A STEP 4C, 2, A, B, F, H, M AND 4D, 13.

Part: BOLT — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON LEFT WING LOWER SLAT BOLT AT SLAT NR 2, TRACK NR 6 BETWEEN RIBS 11-12. REPLACED THE BOLT AMM 27-84-64-400-002-A STEPS 4B(2)(A)(B) AND (D) AND 4C(8) THRU 4C (9) AND 4C(13).

Part: BOLT — CORRODED (RT WING) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT WING TRACK NR 4 PIVOT BOLT BETWEEN RIB 19-20. REPLACED PIVOT BOLT IAW AMM 27-54-62-000-001-A AND AMM 27-54-62-400-001-A

Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RT WING SLAT NR 4, TRACK NR 9, FORWARD BOLT BETWEEN RIB 18-19. REPLACED BOLT IAW AMM 27-84-66-400-002-A.

Part: HINGE PIN — CORRODED (LT WING) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT WING SPOILER NR 2 INBD HINGE PIN BETWEEN RIB 11-12. REPLACED HINGE PIN IAW AMM 27-64-42-400-001-A.

Part: BOLT — CORRODED (TE FLAP) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON RT WING PIVOT BOLT AT FLAP TRACK NR 3 BETWEEN RIB 12-13. REPLACED PIVOT BOLT IAW AMM 27-54-62-000-001-A AND AMM 27-54-62-400-001-A.

Part: HINGE PIN — CORRODED (RT WING) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON RT WING SPOILER NR 4 INBD INNER HINGE PIN BETWEEN RIB 17-18. REPLACED INNER HINGE PIN IAW AMM 27-64-44-400-001-A.

Part: HINGE PIN — CORRODED (RT WING) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RT WING SPOILER NR 5 INBD INNER HINGE PIN BETWEEN RIB 20-21. REPLACED INNER HINGE PIN IAW AMM 27-64-45-400-001-A.

Part: HINGE PIN — CORRODED (SPOILERS) · airframe 49,365 hrs · 25,514 cycles

CORROSION ON LEFT WING INNER HINGE PIN OUTBOARD ON NR 1 SPOILER BETWEEN RIBS 6-7. REPLACED THE HINGE PIN IAW AMM 27-64-41-400-001-A.

Part: BOLT — CORRODED (RT WING) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON RT WING LOWER SLAT BOLT AT SLAT NR 3, TRACK NR 8, RIB 16-17. REPLACED LOWER SLAT BOLT IAW AMM 27-84-65-400-002-A.

Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT WING SLAT 2, TRACK 6, UPPER FORWARD BOLT. REPLACED BOLT IAW AMM 27-84-64-400-002-A.

Part: HINGE PIN — CORRODED (RT SPOILER) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT WING SPOILER NR 4 OTBD INNER HINGE PIN BETWEEN RIB 17-18. REPLACED INNER HINGE PIN IAW AMM 27-64-44-400-001-A.

Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED ON RT WING NR 2 SLAT, NR 6 TRACK BOLT BETWEEN RIB 11-12. REPLACED SLAT BOLT IAW AMM 27-84-64-400-002-A.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON LT SIDE BOX BEAM UPPER FLANGE AT FRAME 43 AND +Y1650. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: HINGE PIN — CORRODED (FRAME 18) · airframe 49,365 hrs · 25,514 cycles

CORROSION ON NOSE LANDING GEAR TORQUE LINK HINGE PIN BOLT HEAD FRAME 18. REPLACED HINGE PIN BOLT IAW AMM 32-21-27.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 49,365 hrs · 25,514 cycles

CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL AT 640KB BETWEEN RIB 15-16. REPLACED ACCESS PANEL PER AMM 57-27-11-400-002A.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 49,365 hrs · 25,514 cycles

CRACK ON RIGHT SIDE BOX BEAM UPPER FLANGE AT FRAME 43 AND -Y1650. REPAIRED IAW EO 5315Y066.

Part: CLAMP — DAMAGED (RT WING) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, ELONGATED HOLE ON RT WING FUEL TANK ACCESS PANEL 640AB RING CLAMP. REPLACED FUEL TANK RING CLAMP IAW AMM 57-27-11-400-000-A.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON BULK CARGO COMPARTMENT DOOR LOWER SILL BEAM BETWEEN FRAME 60 TO FRAME 62, STRINGER 38R. REPAIRED LOWER SILL BEAM IAW SRM 53-41-49-300-003.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON BULK CARGO DOOR SILL BEAM AT FRAME 62, STR 38R. REPAIRED SILL BEAM IAW SRM 53-41-49-300-003.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STR IN AFT CARGO COMPARTMENT AT FRAME 58 AND S39L. REPAIRED STR IAW SRM A320 53-00-13-300-001, FIGURE 20101, SHEET 6.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT THRESHOLD SHEET BETWEEN FRAME 52A AND FRAME 56 AT STR 38R. REPLACED THRESHOLD SHEET IAW SRM A320 51-42-11 AND DWG D53475500.

Part: FLANGE — CORRODED (FRAME 21) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON LEFT LATERAL AVIONICS COMPARTMENT INTERNAL STRUCTURE CHECK VALVE AIR INLET RING FLANGE AT FRAME 21 BETWEEN STRINGERS 31 AND 32L. REPLACED RING FLANGE IAW SRM 51-72-11 AND DRAWING D53912684.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT COVER SHEET BETWEEN FRAME 52A TO FRAME 56 AT STR 38R. REPAIRED COVER SHEET IAW EA 262958.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-70) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOOR SUPPORT AT Y765 BETWEEN FRAMES 67 TO 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472800.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON AFT GALLEY FLOORBEAM BETWEEN FRAME 68 AND FRAME 70 AT -Y160. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472800.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOWER FUSELAGE PRESSURE DECK MEMBRANE, HOLE NR 14 AT FRAME 36 AND -Y1523. REPAIRED PRESSURE DECK MEMBRANE IAW EA 262491.

Part: FITTING — CRACKED (FRAME 2) · airframe 49,365 hrs · 25,514 cycles

CRACK BELOW CENTER WINDOW POST IN COCKPIT ON LEFT CONTINUITY FITTING AT FRAME 2 AND -Y17. REPAIRED CONTINUITY FITTING IAW EA 262868.

Part: FITTING — CRACKED (FRAME 2) · airframe 49,365 hrs · 25,514 cycles

CRACK BELOW CENTER WINDOW POST IN COCKPIT ON LEFT CONTINUITY FITTING AT FR 2. REPAIRED THE CONTINUITY FITTING IAW EA 262868.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOWER FUSELAGE PRESSURE DECK MEMBRANE HOLE NR 15 AT FR 36 AND -Y1523. REPAIRED PRESSURE DECK MEMBRANE IAW EA 262491 .

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOWER FUSELAGE PRESSURE DECK MEMBRANE HOLE NR 17 AT FRAME 36 AND -Y1523. REPAIRED PRESSURE DECK MEMBRANE IAW EA 262491.

Part: FITTING — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON FORWARD GALLEY LOWER FITTING AT STRINGER 23L BETWEEN FRAMES 16 AND 20. REPLACED THE LOWER FITTING IAW SRM 51-72-11 DWG D531-10339.

Part: WINDOW FRAME — CRACKED (FRAME 4) · airframe 49,365 hrs · 25,514 cycles

CRACK INDICATED ON RIGHT INTERNAL WINDOWSHIELD SIDE POST LOWER ATTACHMENT AT FR 4 RIGHT. REPAIR PERFORMED ON WINDOW FRAME IAW EA 262546 AND TP-PI-S2-17165-2015, PAGE 6, FIG 2 (SHEET 6).

Part: FITTING — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON FORWARD GALLEY LOWER SILL FITTING BETWEEN FRAMES 16 AND 20, STRINGER 23R. REPLACED THE FITTING IAW SRM A320 51-72-11 AND DWG D53112225.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FRAME 33, STR 41R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231535.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. AFT GALLEY FLOOR PANEL 261AG DELAMINATED. REPAIRED FLOOR PANEL 261AG IAW SRM 53-02-00-300-011 PAR, 1H, FIG 20109 AND IRM 9701, REV G.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RT AFT GALLEY LOWER SILL BETWEEN FRAME 66 TO FRAME 68 AT STR 23R. REPLACED LOWER SILL IAW EA 262548 AND SRM 51-72-11.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON RT AFT GALLEY LOWER SILL SPLICE BETWEEN FRAME 65 TO FRAME 66 AT STR 23R. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480019.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 261DF DELAMINATED. REPLACED FLOOR PANEL 261DF IAW EA 262580 AND SRM 53-02-00-201 AND IRM 9701, REVISION G.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FRAME 32, STR 42R TO STR 43R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231534.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 262BG DELAMINATED. REPLACED FLOOR PANEL 262BG PASSENGER CABIN IAW SRM 53-02-00-300-011, PAR 1H, FIG 20 105, IRM 9701, REV G AND EA 262581.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR PANEL DELAMINATED. REPAIRED FLOOR PANEL 251JF IAW SRM 53-02-00-300-013, PAR 1.H, ITEMS 11 TO 18.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FRAME 33 BETWEEN STR 42R-43R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231535.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FRAME 31 BETWEEN S40R TO S41R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231533.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 261BG DELAMINATED. REPLACED FLOOR PANEL 261BG IAW SRM 53-02-00-300-011, PAR 1H, FIG 20109 AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR PANEL 242GF DELAMINATED. REPLACED FLOOR PANEL 242GF IAW SRM 53-02-00-300-011, PAR 1H, FIG 20109 AND IRM 9701, REV G.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY CORNER FITTING AT FRAME 68 AT STRINGER 23R. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53480019.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RT AFT GALLEY LOWER SILL SPLICE BETWEEN FRAME 65 TO FRAME 66 AT STR 23R. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480019.

Part: COUPLING — DAMAGED (FRAMES 64-66) · airframe 49,365 hrs · 25,514 cycles

ELONGATED HOLE ON AFT GALLEY INBOARD UPPER FLOOR SUPPORT COUPLING AT Y765 BETWEEN FRAMES 64 TO 66. REPLACED COUPLING IAW SRM 51-72-11 AND DRAWING D53472000.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: FWD GALLEY FLOOR PANEL 231BF DELAMINATED. REPLACED FLOOR PANEL 231BF IAW SRM 53-12-00-300-006, PAR 1H, FIG 20106 AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 232FF DELAMINATED. REPLACED FLOOR PANEL 232FF IAW SRM 53-12-00-300-006 PAR 1H, FIG 20106 AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY FLOOR PANEL 261PF DELAMINATED. REPLACED FLOOR PANEL 261PF IAW SRM 53-02-00-300-011, PAR 4 H, FIG 20109 AND IRM 9701, REV G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM BETWEEN FRAME 64 AND FRAME 66 AT Y1292. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53474250.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON AFT GALLEY LOWER SILL COUPLING AT FRAME 66, Y1450. REPLACED COUPLING IAW SRM 51-72-11, EA 262547 AND DWG D53480019, D53474250.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY FLOORBEAM AT -Y1292 BETWEEN FRAME 12 AND FRAME 24. REPLACED FLOORBEAM IAW SRM A320 51-72-11 AND DWG: D53110900 AND D53110984.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

CORROSION ON AFT GALLEY FLOOR SUPPORT AT FRAMES 64 TO 66 +Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472000.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON AFT GALLEY LOWER SILL COUPLING AT FRAME 66, Y1450. REPLACED COUPLING IAW SRM 51-72-11 EA 262547 AND DWG D53480019, D53474250.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 231XF DELAMINATED. REPAIRED TOP LAYER FLOOR PANEL 231XF IAW SRM 53-02-00-300-013, PAR H.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON AFT GALLEY LOWER SILL COUPLING AT FR 66, Y1450. REPLACED COUPLING IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 231EF DELAMINATED. REPLACED FLOOR PANEL 231EF IAW SRM 53-12-00-300-006, PAR 1H, FIG 20106 AND IRM 9701, REV G.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY CORNER FITTING AT FRAME 68, STR 23L. REPLACED FITTING IAW SRM 51-72-11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FRAME AT FRAME 68, STR 23R. REPAIRED FRAME IAW EA262663, PART B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM BETWEEN FRAME 68 TO FRAME 69 AT -Y1162. REPLACE FLOORBEAM IAW SRM 51-72-11 AND DWG D534721892.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 231FF. REPLACED FLOOR PANEL 231FF IAW SRM 53-12-00-300-006, PAR 1H, FIG 20106 AND IRM 9701, REV G.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON CONNECTING SECTION BETWEEN FRAME 68 AND -Y1162. REPLACED CONNECTING SECTION IAW SRM A320-51-72-11.

Part: COUPLING — DAMAGED (FRAMES 64-66) · airframe 49,365 hrs · 25,514 cycles

ELONGATED HOLE ON AFT GALLEY INBOARD LOWER FLOOR SUPPORT COUPLING AT Y765 BETWEEN FRAMES 64 TO 66. REPLACED THE COUPLING IAW SRM 51-72-11 AND DRAWING D53472000.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL BETWEEN FRAME 66 TO FRAME 68 AT STR 23L. REPLACED LOWER SILL IAW SRM 51-72-11, EA 262547 AND DWG D53480019, D53474250.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY FLOOR PANEL 222EF DELAMINATED. REPLACED FLOOR PANEL 222EF IAW SRM 53-12-00-300-006, PAR 1H FIG 20106 AND IRM 9701, REV G.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM BETWEEN FRAME 64 AND FRAME 66 AT -Y1292. REPLACED FLOORBEAM IAW SRM 51-42-11, 51-72-11 AND DWG D53472816.

Part: COUPLING — DAMAGED (FRAMES 64-66) · airframe 49,365 hrs · 25,514 cycles

ELONGATED HOLE ON AFT GALLEY OUTBOARD LOWER FLOORBEAM COUPLING AT Y765 BETWEEN FRAMES 64 - 66. REPLACED COUPLING IAW SRM 51-72-11 AND DRAWING D53472000.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,365 hrs · 25,514 cycles

ACFT IN BASE MAINTENANCE: FWD GALLEY FLOOR PANEL 221EF DELAMINATED. REPLACED FLOOR PANEL 221EF IAW SRM 53-12-00-300-006, PAR 1H, FIG 20106 AND IRM 9701, REV G.

Part: COUPLING — ELONGATED (FRAMES 64-66) · airframe 49,365 hrs · 25,514 cycles

ELONGATED HOLE ON AFT GALLEY OUTBOARD UPPER FLOORBEAM COUPLING AT Y765 BETWEEN FRAMES 64 - 66. REPLACED THE COUPLING IAW SRM 51-72-11 AND DRAWING D53472000.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LT LOWER FUSELAGE PRESSURE DECK MEMBRANE HOLE NR 7 AT FRAME 36 AND Y1523. REPAIRED PRESSURE DECK MEMBRANE IAW EA 2662489A.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

ACFT IN BASE MAINTENANCE. CRACK ON LOWER FUSELAGE PRESSURE DECK MEMBRANE HOLE NR 8. REPAIRED PRESSURE DECK MEMBRANE IAW EA 262489A.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

ACFT IN BASE MAINTENANCE. CRACK ON LOWER FUSELAGE PRESSURE DECK MEMBRANE HOLE 27. REPAIRED PRESSURE DECK MEMBRANE IAW EA 262489A.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOWER FUSELAGE PRESSURE DECK MEMBRANE HOLE NR 23. REPAIRED PRESSURE DECK MEMBRANE IAW EA 262489A.

Part: PRESSURE DECK — CRACKED (FRAME 36) · airframe 49,365 hrs · 25,514 cycles

CRACK INDICATION ON LEFT PRESSURE DECK MEMBRANE OPEN HOLE AT FR 36, 6 INCHES FROM Y1523. REPAIRED IAW EA 262489A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 49,365 hrs · 25,514 cycles

EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 1 BEARING. REPLACED THE RUDDER HINGE ARM NR 1 IAW AMM 55-36-41-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER NR 7 RUDDER HINGE ARM BEARING. REPLACED NR 7 RUDDER HINGE ARM IAW AMM 55-36-41-0401.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON PRESSURE DECK MEMBRANE HOLE NR 15 AT FRAME 36 AND Y1523. REPAIRED PRESSURE DECK MEMBRANE IAW EA 262489A.

Part: HINGE FITTING — LOOSE (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. HOLE WEAR ON RT AFT NLG DOOR AFT HINGE OF FORWARD FITTING BETWEEN FRAME 18 AND FRAME 20. REPLACED HINGE FITTINGS IAW CMM 52-82-32 AND PERFORMED CHECK OF PLAY AT RT NLG AFT DOOR IAW AMM 32-22-00-220-002-A.

Part: FLOOR PANEL — DELAMINATED (FRAMES 49-53) · airframe 49,365 hrs · 25,514 cycles

AFT CARGO FLOOR PANEL 151DF HAS DELAMINATION. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011 AND IRM 9701 REV G.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON LT AFT NLG DOOR FORWARD HINGE OF AFT FITTING. REPLACED HINGE FITTING IAW SRM 51-72-11; CMM 52-82-32.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON LT AFT NLG DOOR AFT HINGE OF FWD FITTING AT STA 8077. REPLACED HINGE FITTING IAW CMM 52-82-32 PERFORMED CHECK OF PLAY IAW AMM 32-22-00-220-002-A; PLAY IS WITHIN LIMITS.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON LT AFT NLG DOOR AFT HINGE OF AFT FITTING AT STA 8077. REPLACED HINGE FITTING IAW SRM 51-72-11, CMM 52-82-32.

Part: HINGE FITTING — LOOSE (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. HOLE WEAR ON RT AFT NLG DOOR AFT HINGE OF AFT FITTING BETWEEN FRAME 18 TO FRAME 20. REPLACED HINGE FITTINGS IAW CMM 52-82-32 AND PERFORMED CHECK OF PLAY AT RT NLG AFT DOOR IAW AMM 32-22-00-220-002-A.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON LT AFT NLG DOOR FORWARD HINGE OF FWD FITTING AT STA 8077. REPLACED HINGE FITTING IAW SRM 51-72-11; CMM 52-82-32.

Part: HINGE FITTING — LOOSE (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. HOLE WEAR ON RT AFT NLG DOOR FORWARD HINGE OF AFT FITTING BETWEEN FRAME 18 AND FRAME 20. REPLACED HINGE FITTINGS IAW CMM 52-82-32 AND PERFORMED CHECK OF PLAY AT RT NLG AFT DOOR IAW AMM 32-22-00-220-002-A.

Part: HINGE FITTING — LOOSE (NLG DOOR) · airframe 49,365 hrs · 25,514 cycles

AIRCRAFT IN BASE MAINTENANCE. HOLE WEAR ON RT AFT NLG DOOR FORWARD HINGE OF FORWARD FITTING BETWEEN FRAME 18 AND FRAME 20. REPLACED HINGE FITTINGS IAW CMM 52-82-32 AND PERFORMED CHECK OF PLAY AT RT NLG AFT DOOR AMM 32-22-00-220-002-A.

Part: SLAT — BOWED (LT WING) · airframe 48,629 hrs · 25,160 cycles

AIRCRAFT WAS GNDED. LT WING NR 1 LE IS BOWED & WARPED. REPLACED LT WING NR 1 LE SLAT IAW TASK CARD 26L00027010.

Part: COMPUTER — DEFECTIVE (LE SLAT) · airframe 47,222 hrs · 24,394 cycles

EMERGENCY LANDING, CREW MESSAGED AT 0509Z THAT ACFT SLATS WERE LOCKED, BUT DID NOT STATE SLAT POSITION. THEY HAD CHECKED THE ECAM NON-NORMAL LANDING MANUAL & DECLARED AN EMER FOR LANDING RNWY 8. DISPATCH VERIFIED WITH ECAM MANUAL. CREW REPORTED AFTER LANDING THAT WING TIP BRAKE MSG SHOWN PASSING THROUGH 8000 FEET. CALCULATED LANDING DATA WAS 155 KT APPROACH SPEED, USING AROUND 5500 FEET OF RNWY. FIRST OFFICER REPORTED ACTUAL LANDING DISTANCE WAS AROUND 5000 FEET WITH MEDIUM AUTO BRAKE. SLAT POSITION WAS LESS THAN 1. LANDING REPORTED SMOOTH WITHOUT INCIDENT. RESET THE SLAT SYS WHICH UNLOCKED THE SLATS & REPLACED THE NR 2 SFCC. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 27-51-34, 27-80-00-869 & 27-81-00-740-002.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,025 hrs · 24,273 cycles

AFT CARGO FLOOR PANEL 151GF DELAMINATED. R & R AFT CARGO FLOOR PANEL 151GF IAW AMM 53-42-14.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 45,450 hrs · 23,396 cycles

2L DOOR SLIDE ARMED INDICATION IS INTERMITTENT. REMOVED DEBRIS FROM GIRT BAR LOCK, DOOR OPERATIONS CHECKED OK.

Part: WIRE — KINKED (EVAC SLIDE) · airframe 45,450 hrs · 23,396 cycles

LEFT AFT DOOR SLIDE PACK INDICATED UNARMED ON ECAM, CIDS PANEL & AT DOOR WHEN IN THE ARMED POSITION. REMOVED DEBRIS & LOOSENED KINKED WIRE AS REQUIRED. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 44,965 hrs · 23,120 cycles

2L DOOR FLASHLIGHT BATTERY LOW OR INOPERATIVE. REPLACED 2L DOOR JUMP SEAT FLASHLIGHT BATTERY WITH NEW. OPERATIONS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 44,580 hrs · 22,898 cycles

L1 DOOR EMER LIGHT LENS MISSING. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-11-401. OPERATIONS CHECKED OK.

Part: LENS — MISSING (CABIN) · airframe 44,569 hrs · 22,894 cycles

AFT RT SERVICE DOOR EMER EXIT LIGHT LENS COVER MISSING. REPLACED AFT RT SERVICE DOOR EMER EXIT LIGHT LENS COVER AS REQUIRED IAW AMM 33-50-00.

Part: LENS — MISSING (CABIN) · airframe 43,271 hrs · 22,264 cycles

EMERGENCY EXIT LIGHT LENS AT SEAT 4C IS MISSING. INSTALLED EMER EXIT LIGHT LENS AT SEAT 4C.

Part: LENS — MISSING (CABIN) · airframe 43,271 hrs · 22,264 cycles

EMERGENCY EXIT LIGHT LENS AT ROW 4C IS MISSING. INSTALLED EMER EXIT LIGHT LENS AT ROW 4C.

Part: LENS — MISSING (CABIN) · airframe 43,271 hrs · 22,264 cycles

EMERGENCY LIGHT LENS AT SEAT 11F MISSING. INSTALLED EMER LIGHT LENS AT SEAT 11F.

Part: CONTROL SERVO — EXCESS PLAY (RUDDER) · airframe 42,438 hrs · 21,828 cycles

AIRFRAME VIBRATION REPORTED BY FLIGHT ATTENDANT IN REAR OF ACFT DURING DESCENT. STOPPED WHEN SLOWED TO 250 KNOTS. REPLACED RUDDER SERVO CONTROLS & RUDDER HINGE ARM FITTINGS 2, 3 & 4 IAW NON-ROUTINES.

Part: LENS — MISSING (CABIN) · airframe 42,264 hrs · 21,733 cycles

DOOR R2 EMERGENCY EXIT LIGHT LENS IS MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS AT DOOR R2.

Part: CONTROL SERVO — INOPERATIVE (ELEVATOR) · airframe 42,189 hrs · 21,690 cycles

VIBRATION FELT IN FLIGHT AT 260 - 300. THE LAST HOUR OF FLIGHT VIBRATION FELT THE WORST IN THE TAIL. REPLACED LT INBD SERVO ACTUATOR IAW A320 AMM 27-34-51-400. ADJUSTED ELEVATOR ACTUATION SYS IAW A320 AMM 27-34-00-820-002-A & ELEVATOR FREE PLAY CHECKED IAW A320 AMM 27-34-00-200-001-A.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 42,127 hrs · 21,663 cycles

EMERGENCY LIGHTS AT OVERWING EXIT ROWS FAILED TO ILLUMINATE DURING TEST. REPLACED HARNESS 5409VB FROM SEAT ASSEMBLY 9DEF TO CONNECTOR 7261VC2-A IAW A320 AMM 33-51-07 PAGE 83 SHEET 1.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,100 hrs · 21,648 cycles

OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED RT OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY IAW A320 AMM 33-51-00, OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 41,875 hrs · 21,513 cycles

MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE R & R EPSU RT AT EMERGENCY EXIT. OPS CHECKED GOOD IAW AMM 33-51-38.

Part: HINGE FITTING — CORRODED (RT MLG DOOR) · airframe 41,095 hrs · 21,055 cycles

DURING C11 CHECK, DAMAGE & CORROSION ON BEARING BORE AT RT MLG DOOR FWD HINGE ASSY AT FR42, S42L. REPLACED GEAR DOOR FWD HINGE ASSY IAW SRM 51-72-11.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,247 hrs · 21,141 cycles

EMERGENCY LIGHT WILL NOT TEST. REPLACED POWER SUPPLY IAW AMM 33-51-39-0401-A.

Part: HYDRAULIC LINE — LOOSE (NR 2 ENGINE) · airframe 40,647 hrs · 20,830 cycles

UPON TAXI OUT "A" F/A REPORTED HAZE IN THE FWD CABIN AND THEN AN ACRID SMELL. WHEN REPORTED, BOTH ENGINES WERE RUNNING AND APU WAS SHUTDOWN. 5 PLUS MINUTES HAD LAPSED WHEN REPORT WAS RECEIVED AND WE HAD JUST BEEN CLEARED FOR T/O. CABIN ODOR WAS HYD FLUID, FOUND CAUSE TO BE HYD PUMP LEAK AT ENGINE NR 2. SECURED LEAKING LINE.

Part: FIRE BOTTLE — LOW PRESSURE (LAVATORY) · airframe 38,975 hrs · 19,970 cycles

AFT LEFT LAV TRASH FIRE EXTINGUISHER BOTTLE LOW PRESSURE. REMOVED AND REPLACED FIRE EXTINGUISHER IN AFT LEFT LAV IAW AIRBUS MAINTENANCE MANUAL 26-25-41.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 38,675 hrs · 19,795 cycles

DROP-IN - SEVERAL CRACKS ON FORWARD LEFT EMERGENCY EXIT DOOR AFT FRAME SEGMENT ANGLE BETWEEN FR38 TO FR39. REPLACED FORWARD LEFT EMERGENCY EXIT DOOR AFT FRAME SEGMENT ANGLE IAW EO EO5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 38,675 hrs · 19,795 cycles

DROP-IN - SEVERAL CRACKS ON FORWARD RIGHT EMERGENCY EXIT DOOR AFT FRAME SEGMENT ANGLE BETWEEN FR38 TO FR39. REPLACED FORWARD RIGHT EMERGENCY EXIT DOOR AFT FRAME SEGMENT ANGLE IAW EO EO5210Y228.

Part: FILTER — CONTAMINATED (CABIN) · airframe 36,705 hrs · 18,797 cycles

FLIGHT ATTENDANT REPORTED A DIRTY SOCK SMELL 25 MINUTES AFTER TAKEOFF. CREW ELECTED TO DIVERT TO PIT - DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT OZONE FILTER AND BOTH HEPA FILTERS.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 36,388 hrs · 18,645 cycles

WHILE EN ROUTE TO PHL, CREW REPORTED GREEN HYDRAULIC ENGINE 1 PUMP LOW PRESSURE INDICATION FOLLOWED BY GREEN SYSTEM LOW FLUID LEVEL INDICATION. FLIGHT CONTINUED TO PHL WHERE ALTERNATE EXTENSION WAS REQUIRED. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE HYDRAULIC PUMP IAW AIRBUS MAINTENANCE MANUAL 29-11-51-400-041. ALSO REPLACED THE CASE DRAIN FILTER AND CARBON SEAL.

Part: LINE — LEAKING (THRUST REVERSER) · airframe 33,651 hrs · 17,320 cycles

FLT1021 - RETURNED TO FIELD AND DECLARED EMERGENCY LANDING. LANDING AND LOST NOSE WHEEL STEERING. FOUND NR 1 ENGINE THRUST REVERSER PRESSURE LINE LEAKING. REPLACED LINE WITH FLEX LINE PER AMM 20-17-03 AND EA 116831. SERVICED GREEN SYSTEM & OPERATIONAL CHECK WAS GOOD. OPEN

Part: SELECTOR VALVE — DEFECTIVE (LANDING GEAR) · airframe 32,892 hrs · 16,930 cycles

FLT 1123 CLT-GCM - RTF - EXTENDED AIRFRAME VIBRATION ON GEAR RETRACTION. ECAM - L/G NOT LOCKED WHEN RETRACTED / LGCIU 1 FAULT / L/G DOOR DID NOT NOT CLOSE. WHILE AIRBORNE RECEIVED ECAM MESSAGE - ENG 1 APP IDLE ONLY INOP SYSTEM LGCIU1, REVERSER 1, GPWS. CREW RETURNED TO FIELD & ECAM MESSAGE AFTER TOUCHDOWN - GEAR DISAGREE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR DOOR SELECTOR VALVE 41GA IAW AIRBUS MAINTENANCE MANUAL 32-31-34 & PROXIMITY SENSOR 30GA IAW AMM 32-31-73. RIGGED NLG DOOR UPLOCK ASSEMBLY IAW AMM 32-31-14-04. ALSO FOUND NLG HARNESS WIRES FOR PROX SENSOR 25GA DETERIORATED - REPLACED WIRES IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-33-11.

Part: PROXIMITY SENSOR — DEFECTIVE (LANDING GEAR) · airframe 32,892 hrs · 16,930 cycles

FLT 1123 CLT-GCM - RTF - EXTENDED AIRFRAME VIBRATION ON GEAR RETRACTION. ECAM - L/G NOT LOCKED WHEN RETRACTED / LGCIU 1 FAULT / L/G DOOR DID NOT CLOSE. WHILE AIRBORNE RECEIVED ECAM MESSAGE - ENG 1 APP IDLE ONLY INOP SYSTEM LGCIU1, REVERSER 1, GPWS. CREW RETURNED TO FIELD & ECAM MESSAGE AFTER TOUCHDOWN - GEAR DISAGREE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR DOOR SELECTOR VALVE 41GA IAW AIRBUS MAINTENANCE MANUAL 32-31-34 & PROXIMITY SENSOR 30GA IAW AMM 32-31-73. RIGGED NLG DOOR UPLOCK ASSEMBLY IAW AMM 32-31-14-04. ALSO FOUND NLG HARNESS WIRES FOR PROX SENSOR 25GA DETERIORATED - REPLACED WIRES IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-33-11.

Part: PROXIMITY SENSOR — DEFECTIVE (NLG) · airframe 32,892 hrs · 16,929 cycles

FLT 1525 CLT-DEN - RTF - CREW RECEIVED MULTIPLE FAULT MESSAGES FOR GEAR DISAGREEMENT AND AIRFRAME VIBRATIONS WHILE RETRACTING THE GEAR. ECAM - L/G NOT UPLOCKED - L/G LGCIU 1 FAULT - L/G DOORS NOT CLOSED - ALL GEAR & FLAP UP FUNCTIONS WERE SLOW. CREW ELECTED TO RETURN TO FIELD AND ALL 3 GEAR PINS WERE INSERTED FOR TAXI TO GATE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE, THE NR 1 LGCIU (LANDING GEAR CONTROL INTERFACE UNIT), AND NLG PROXIMITY SENSORS 24GA & 25GA.

Part: SELECTOR VALVE — DEFECTIVE (LANDING GEAR) · airframe 32,892 hrs · 16,929 cycles

FLT 1525 CLT-DEN - RTF - CREW RECEIVED MULTIPLE FAULT MESSAGES FOR GEAR DISAGREEMENT AND AIRFRAME VIBRATIONS WHILE RETRACTING THE GEAR. ECAM - L/G NOT UPLOCKED - L/G LGCIU 1 FAULT - L/G DOORS NOT CLOSED - ALL GEAR & FLAP UP FUNCTIONS WERE SLOW. CREW ELECTED TO RETURN TO FIELD AND ALL 3 GEAR PINS WERE INSERTED FOR TAXI TO GATE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE, THE NR 1 LGCIU (LANDING GEAR CONTROL INTERFACE UNIT), AND NLG PROXIMITY SENSORS 24GA & 25GA.

Part: INTERFACE UNIT — DEFECTIVE (LANDING GEAR) · airframe 32,892 hrs · 16,929 cycles

FLT 1525 CLT-DEN - RTF - CREW RECEIVED MULTIPLE FAULT MESSAGES FOR GEAR DISAGREEMENT AND AIRFRAME VIBRATIONS WHILE RETRACTING THE GEAR. ECAM - L/G NOT UPLOCKED - L/G LGCIU 1 FAULT - L/G DOORS NOT CLOSED - ALL GEAR & FLAP UP FUNCTIONS WERE SLOW. CREW ELECTED TO RETURN TO FIELD AND ALL 3 GEAR PINS WERE INSERTED FOR TAXI TO GATE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE, THE NR 1 LGCIU (LANDING GEAR CONTROL INTERFACE UNIT), AND NLG PROXIMITY SENSORS 24GA & 25GA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 32,879 hrs · 16,924 cycles

PIT - EEL - S5 CHECK - EMERGENCY LIGHT POWER SUPPLY CONNECTOR LOCK PINS DAMAGED. REPLACED EMERGENCY LIGHT POWER SUPPLY BETWEEN EMERGENCY EXIT WINDOWS IAW JOB CARD 26C83252008. OPS TEST GOOD.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - MAJOR REPAIR - S4 CHECK - LEVEL 2 CORROSION ON NR 1 RIGHT SPOILER CENTER HINGE PINS. REPLACED NR 1 RIGHT SPOILER CENTER HINGE PINS IAW JOB CARD 26C60057086 JPC.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - MAJOR REPAIR - S4 - LEVEL 2 CORROSION ON R2 DOOR SILL AT FR 67, -Y1732. REPAIRED R2 DOOR SILL AT FR 67, -Y1732 IAW A320 SRM 53-41-14 AND EA 115899.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - DELAMINATION ON FLOORBOARD 251GF BETWEEN FR51 TO FR54. REPLACED FLOORBOARD 251GF BETWEEN FR51 TO FR54 IAW MCGILL IRM 9701 REV-G.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - DELAMINATION ON FLOORBOARD 251RF BETWEEN FR58 TO FR62. REPLACED FLOORBOARD 251RF BETWEEN FR58 TO FR62 IAW MCGILL IRM 9701 REV-G.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - DELAMINATION ON FLOORBOARD 252QF BETWEEN FR57 TO FR60. REPLACED FLOORBOARD 252QF BETWEEN FR57 TO FR60 IAW MCGILL IRM 9701 REV-G.

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - INSERTS MISSING ON FLOORBOARD 261PF BETWEEN FR68 TO FR70. REPLACED FLOORBOARD 261PF BETWEEN FR68 TO FR70 IAW MCGILL IRM 9701 REV-G.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - DELAMINATION ON FLOORBOARD 241JF BETWEEN FR42 TO FR47. REPLACED FLOORBOARD 241JF BETWEEN FR42 TO FR47 IAW MCGILL IRM 9701 REV-G.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON L-BRACKET AT AFT ENTRY DOOR CUTOUT LOWER AFT CORNER AT FR68, S23L. REPLACED L-BRACKET AT AFT ENTRY DOOR CUTOUT LOWER AFT CORNER AT FR68, S23L IAW A320 SRM 51-72-11.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - DELAMINATION ON FLOORBOARD 222CF BETWEEN FR12 TO FR16. REPLACED FLOORBOARD 222CF BETWEEN FR12 TO FR16 IAW MCGILL IRM 9701 REV-G.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON NR 4 SPOILER CENTER HINGE PINS. REPLACED NR 4 SPOILER CENTER HINGE PINS IAW JOB CARD 26C60057086.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM SUPPORT AT FR20, -Y189. REPLACED FLOORBEAM AT FR20, -Y189 IAW A320 SRM 51-72-11.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON NR 3 SPOILER CENTER HINGE PINS. REPLACED NR 3 SPOILER CENTER HINGE PINS IAW JOB CARD 26C60057086.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - CORROSION ON -189 SUPPORT AT FR20, Y189. REPLACED -189 SUPPORT AT FR20, Y189 IAW A320 SRM 51-72-11.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON NR 2 SPOILER CENTER HINGE PINS. REPLACED NR 2 SPOILER CENTER HINGE PINS IAW JOB CARD 26C60057086.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FRAME SUPPORT BETWEEN FR69 TO FR70, S23R. REPLACED FRAME SUPPORT BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-42-11.

Part: RETAINING RING — CORRODED (FUEL PANEL) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FUEL PANEL 540GB RETAINING RING. REPLACED FUEL PANEL 540GB RETAINING RING.

Part: RETAINING RING — CORRODED (FUEL PANEL) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FUEL PANEL 540CB RETAINING RING. REPLACED FUEL PANEL 540CB RETAINING RING.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FRAME SUPPORT BETWEEN FR69 TO FR70, S23R. REPLACED FRAME SUPPORT BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-42-11.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEFT ELEVATOR HAS AREA OF DELAMINATION AROUND SCREW HOLE NR 15 FROM INBOARD END UPPER TRAILING EDGE. REPAIRED LEFT ELEVATOR IN AREA AROUND SCREW HOLE NR 15 FROM INBOARD END UPPER TRAILING EDGE IAW A320 SRM 55-21-11 & 51-77-13.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEFT ELEVATOR HAS AREA OF DELAMINATION AROUND SCREW HOLE NR 27 FROM INBOARD END UPPER TRAILING EDGE. REPAIRED LEFT ELEVATOR IN AREA AROUND SCREW HOLE NR 27 FROM INBOARD END UPPER TRAILING EDGE IAW A320 SRM 55-21-11 & 51-77-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66, Y765. REPLACED FLOORBEAM AT FR66, Y765 IAW A320 SRM 51-72-11.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON NR 5 SPOILER CENTER HINGE PINS. REPLACED NR 5 SPOILER CENTER HINGE PINS IAW JOB CARD 26C60057086.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66, Y765. REPLACED FLOORBEAM AT FR66, Y765 IAW A320 SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD EXFOLIATION CORROSION ON SHEAR PLATE SUPPORT STRUCTURE BETWEEN FR69 TO FR70, -Y1162. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1162 IAW A320 SRM 51-42-01, 51-42-11 & 51-72-00.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD EXFOLIATION CORROSION ON SHEAR PLATE SUPPORT STRUCTURE BETWEEN FR69 TO FR70, -Y1162. REPLACED FRAME SUPPORT BETWEEN FR69 TO FR70, -Y1162 IAW A320 SRM 51-42-01, 51-42-11 & 51-72-00.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - MAJOR REPAIR - S4 CHECK LEVEL 2 CORROSION ON R2 DOOR SILL AT FR 67, -Y1732. REPAIRED R2 DOOR SILL AT FR 67, -Y1732 IAW A320 SRM 53-41-14 AND EA 115899.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW TYPICAL REPAIR 25-28-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, Y254. REPLACED FLOORBEAM AT FR16, Y254 IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR70, Y1292. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR70, Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR70, Y1292. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR70, Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, Y1292. REPLACED FLOORBEAM AT FR16, Y1292 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON L-2 DOOR SILL BETWEEN FR66 TO FR68. REPLACED L-2 DOOR SILL BETWEEN FR66 TO FR68 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, -Y765 IAW TYPICAL REPAIR 51-40-01A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR66 TO FR68, Y765. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR66 TO FR68, Y765 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR67 TO FR69, -Y464. REPLACED FLOORBEAM BETWEEN FR67 TO FR69, -Y464 IAW A320 SRM 53-00-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR70, Y1292. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR70, Y1292 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON LEFT AFT DOOR SILL FORWARD OF AFT GIRT BAR MOUNT. REPLACED LEFT AFT DOOR SILL IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, -Y765 IAW TYPICAL REPAIR 51-40-01A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66, Y1732. REPLACED FLOORBEAM AT FR66, Y1732 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR66 TO FR68, Y765. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR66 TO FR68, Y765 IAW A320 SRM 51-72-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD GALVANIC CORROSION ON FLOOR ANGLE BETWEEN FR12 TO FR13, S23R. REPLACED FLOOR ANGLE BETWEEN FR12 TO FR13, S23R IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION IN SEVERAL AREAS ON FLOORBEAM BETWEEN FR12 TO FR14, Y505. REPLACED FLOORBEAM BETWEEN FR12 TO FR14, Y505 IAW A320 SRM 51-72-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 WIDESPREAD GALVANIC CORROSION ON FLOOR ANGLE BETWEEN FR12 TO FR13, S23R. REPLACED FLOOR ANGLE BETWEEN FR12 TO FR13, S23R IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,879 hrs · 16,924 cycles

PIT - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM JOINT COVER BETWEEN FR12 TO FR14, Y50. REPLACED FLOORBEAM JOINT COVER BETWEEN FR12 TO FR14, Y50 IAW A320 SRM 51-72-11.

Part: FLAP — DELAMINATED (LT WING) · airframe 31,793 hrs · 16,392 cycles

PIT - C11 - MAJOR REPAIR - DELAMINATION ON LEFT WING FLAP 11 FEET 10 INCHES FROM INBOARD EDGE ALONG TRAILING EDGE. REPAIRED LEFT WING FLAP 11 FEET 10 INCHES FROM INBOARD EDGE ALONG TRAILING EDGE IAW A320 SRM 57-53-00.

Part: ELEVATOR — SATURATED (ZONE 300 - STABI) · airframe 31,793 hrs · 16,392 cycles

PIT - C11 - MAJOR REPAIR - LEFT ELEVATOR HAS 8.25 SQUARE INCHES OF WATER DAMAGE AT 16 INCHES OUTBOARD FROM INNER EDGE & 17 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR IAW A320 SRM 55-21-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,793 hrs · 16,392 cycles

PIT - C11 - MAJOR REPAIR - RIGHT ELEVATOR HAS 1.5 INCH POCKET OF WATER DAMAGE AT 22 INCHES OUTBOARD FROM INNER EDGE & 29 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR IAW A320 SRM 55-21-00 & 55-22-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,793 hrs · 16,392 cycles

PIT - C11 - MAJOR REPAIR - LEFT ELEVATOR HAS 20 SQUARE INCHES OF WATER DAMAGE AT 54 INCHES OUTBOARD FROM INNER EDGE & 5.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR SKIN IAW A320 SRM 55-21-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,793 hrs · 16,392 cycles

PIT - C11 - MAJOR REPAIR - RIGHT ELEVATOR HAS 1 INCH BY 1 INCH POCKET OF WATER DAMAGE AT 5 FEET 6 INCHES OUTBOARD FROM INNER EDGE & 5 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR IAW A320 SRM 55-21-00 & 55-22-11.

Part: LENS — BROKEN (CABIN) · airframe 31,401 hrs · 16,190 cycles

FLT 1537-DEN - EEL - FORWARD LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. MAINTENANCE REPLACED THE LENS.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,837 hrs · 36,257 cycles

CLT - C4 - MAJOR REPAIR - CRACK IN RIGHT HORIZONTAL STAB LOWER SKIN AT AFT SPAR STA 100. REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN AT AFT SPAR STA 100 IAW B737 SRM 55-10-01.

Part: LENS — IMPROPER PART (CABIN) · airframe 29,674 hrs · 15,422 cycles

LOG PAGE 4453212 - FLT 903-DEN - EEL - SEAT 9D WRONG EMERGENCY LIGHT LENS INSTALLED. MAINTENANCE INSTALLED THE CORRECT LENS AS REQUIRED.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 56,679 hrs · 38,143 cycles

MCN C19 MAJOR REPAIR NR 6126557 & 6126556 LT HAND INBOARD AFT FLAP DELAMINATED IN 2 PLACES. WBL117 ON LOWER SURFACE, AND WBL 107 ON UPPER SURFACE. REPAIRED LT HAND INBOARD AFT FLAP IN 2 PLACES. WBL 117 ON LOWER SURFACE, AND WBL 107 ON UPPER SURFACE IAW B737 SRM 51-70-10-2R4.

Part: SENSOR — UNRELIABLE (FUEL CELL) · airframe 27,184 hrs · 14,382 cycles

FLT 977 CLT- PDX - AIR TURN BACK - AFTER TAKEOFF, OUTER FUEL TRANSFER OCCURRED WITH WINGS AT 12,000 EACH SIDE AND CENTER TANK WOULD NOT AUTO FEED. CENTER TANK PUMPS DID AUTO FEED DURING TAXI OUT. CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. ACFT LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE FOUND WING TANK LEVEL SENSORS UNRELIABLE. REPLACED 15QJ1, 15QJ2, 16QJ1 & 16QJ2 PER AIRBUS MAINTENANCE MANUAL 28-46-15. OPERATIONAL TEST NORMAL. (S)

Part: SLIDE — FAULTY (PAX DOOR)

PIT - DURING OPERATIONAL TEST OF THE LEFT HAND, AFT DOOR EMERGENCY ESCAPE SLIDE, THE DOOR ONLY OPENED HALF-WAY, THE DOOR ASSIST BOTTLE DID NOT WORK, THE SLIDE COVER DID NOT FULLY RELEASE, AND THE BOTTOM HALF (UNDERSIDE) OF THE SLIDE DID NOT INFLATE. MAINTENANCE REPLACED THE LEFT HAND, AFT DOOR EMERGENCY ESCAPE SLIDE.

Part: EPSU — FAILED (CABIN)

THE LT CENTER EMERGENCY POWER SUPPLY UNIT FAILED DURING TEST. MAINTENANCE REPLACED THE LT CENTER EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONAL TEST NORMAL.

Part: EPSU — FAULTY (EMERGENCY LIGHT)

TPA - SEATS IN ROWS 3, 5, 14, 19, & 23 FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE MID CABIN, LEFT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: EPSU — DISCHARGED (CABIN)

PIT - SEAT MOUNTED ESCAPE PATH EMERGENCY LIGHTS WERE FOUND INOPERATIVE IN ROWS 3, 5, 14, 19 AND 23 DURING OPERATIONAL CHECK. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: EPSU — MALFUNCTIONED (EMERGENCY LIGHTS)

MDIS - EPSU "UNIT FAULT" LIGHT DISPLAYED ON UNIT AT MID LEFT CABIN LOCATION. MAINTENANCE REPLACED EPSU AND BATTERY, EMERGENCY LIGHT SYSTEM TEST IS SATISFACTORY.

Part: LANDING GEAR — UNKNOWN

AFTER TAKEOFF, THE LANDING GEAR TOOK 3 TO 4 TIMES LONGER TO RETRACT THAN NORMAL. CREW RECYCLED THE GEAR AND GOT THE SAME RESULT. WHEN THE GEAR FULLY RETRACTED, THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAISED THE AIRCRAFT AND PERFORMED AN EXTENSION/RETRACTION CHECK. ALL INDICATIONS AND TIME LIMITS WERE NORMAL.

Part: EPSU — FAULTY (EMERGENCY LIGHTS)

PHL - THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: EPSU — FAULTY (PASSENGER CABIN)

THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE LEFT HAND, MID CABIN EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONALLY CHECKS OK.

Part: EPSU — FAULTY (EMERGENCY LIGHTS)

DCA - THE EMERGENCY LIGHTS FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE LEFT HAND, MID CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: EPSU — FAULTY (EMERGENCY LIGHTS)

LAX - THE PASSENGER LEFT HAND EMERGENCY LIGHTING SYSTEM IN ROWS 14, 16, 19, AND 23 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: WIRE HARNESS — MISROUTED (ESCAPE SLIDE)

PHL - THE AFT, LEFT HAND SLIDE HAD A LIGHT HARNESS ROUTED INCORRECTLY AND A COVER RELEASE CABLE DISCONNECTED. MAINTENANCE CORRECTLY ROUTED THE LIGHT HARNESS ASSEMBLY AND CONNECTED THE COVER RELEASE CABLE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

PIT - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. THE AFT EMERGENCY POWER SUPPLY UNIT SHOWS INT AND EXT FLASHING RED LED'S. THE EMERGENCY POWER SUPPLY UNIT AT THE LEFT, MID-CABIN INDICATES A CONTINUOUS RED LED. MAINTENANCE PLACED SYSTEM ON MEL. RELAMPED EMERGENCY LIGHT ASSEMBLIES FIN 32WL AND FIN 33WL. OPERATIONALLY CHECKS OK.

Part: PSU — FAILED (EMERGENCY LIGHT)

PHL - THE EMERGENCY POWER SUPPLY UNIT IN THE AFT LEFT POSITION FAILED THE TEST. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT. OPS CHECK NORMAL. (M)

Part: FLOW VALVE — FAILED (NR 2 PACK)

GJT - FLT 82 - EN ROUTE SFO-PHL, WITH THE NR 2 PACK ON MEL, A NR 1 PACK FAULT OCCURRED. PRESSURIZATION WAS LOST AS A RESULT. FLIGHT MADE A RAPID DESCENT TO 10,000 FEET THE DIVERTED TO GJT DUE TO TERRAIN CONTRAINTS. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 PACK FLOW CONTROL VALVE. OPS CHECKED BOTH THE NR 1 AND NR 2 PACK SYSTEMS. OPS CHECKS OK. (M)

Part: SILL — CORRODED (FUSELAGE)

SILL, 2.0 INCH X 1.0 INCH X 0.06 INCH AREA, CORRODED. BETWEEN FR 66 & 68, BL Y11371, WL Z240. INSTALLED NEW SILL IAW SRM.

Part: SILL — CORRODED (FUSELAGE)

DOOR SILL, 1.0 INCH X 1.5 INCH X 0.07 INCH DEEP, CORROSION; LEVEL 2; FR 66 TO 68, -Y 1524, Z-240. REPLACED DOOR SILL IWA SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM, 2.5 INCH X 1.5 INCH X .030 INCH DEEP, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE)

ANGLE CORROSION, 2.0 INCH X 2.0 INCH X .02 INCH DEEP. REMOVED AND REPLACED PART IAW SRM.

Part: PLATE — CORRODED (FUSELAGE)

PLATE CORROSION, 4 INCH X 4 INCH X .70 INCH DEEP. REMOVED AND REPLACED PORT IAW SRM.

Part: FLOORBEAM — CORRODED (FR66,68,Y1270)

FLOORBEAM, 3.0 INCH X 1.5 INCH X .03 INCH AREA. CORROSION; LEVEL 2. REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM, 2.0 INCH X 2.0 INCH X .025 INCH D, BETWEEN FR 68-69, Y1270, Z240, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM, 2.0 INCH X 2.0 INCH X .035 INCH D, CORROSION BETWEEN FR 64 &66, +Y 1270, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK, 5.45 INCH X 0.813 INCH X .047 INCH D, CORROSION, FR17 AT Y 1270, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: PAD — CORRODED (GIRT BAR FITTING)

ADAPTER PAD, 11 INCH X 2 INCH X 0.050 INCH, CORROSION; LEVEL 2; AFT GIRT BAR FITTING, R1 DOOR, FR 19-20, Z240, Y1293. REPLACED PORT GIRT BAR FITTING ADAPTER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM, 1.5 INCH X 1.0 INCH X .02 INCH DEEP, CORROSION; LEVEL 2; FR 66-68, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM, 1.0 INCH X 1.0 INCH X .03 INCH D, CORROSION; LEVEL 2; FR64-66, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM, 3.0 INCH X 2.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FR66-68, +Y762,Z240. REPLACED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM, 1.0 INCH X 1.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FRAME 64 & 66, +Y787, Z240.

Part: BATTERY — FAILED (EMERGENCY LIGHT)

FORWARD LEFT EPSU FAILED TEST. MAINTENANCE REPLACED THE EPSU BATTERY. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

LEFT CENTER EPSU FAILED TEST. MAINTENANCE REPLACED THE EPSU. (M)

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND DISCHARGED. MAINTENANCE REPLACED THE BATTERY ON THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)

Part: SLIDE — DEFECTIVE (SERVICE DOOR)

PHL - RECEIVED 'EPSU EXT LOAD AFT L' FAULT DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT LEFT SERVICE DOOR EMERGENCY ESCAPE SLIDE. OPERATIONALLY CHECKS OK. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

DCA - FLT 6875 - EN ROUTE LGA-DCA, WHILE CLIMBING THROUGH FL180, THE CAPTAINS WINDSHIELD OUTER PANEL SHATTERED, ACCOMPANIED WITH BRIEF ARCING. QRH PROCEDURES WERE FOLLOWED. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD AND CHECKED THE WINDSHIELD HEAT. THE WINDSHIELD HEAT CHECKED OK. (M)