N401UA

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 87,815 hrs · 34,307 cycles

SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - CAB PR CAB PB 1 FAULT WORKED, PFR GIVES MESSAGES OF"CAB PR EXCESS CAB ALT" & "CAB PR SYS 1 FAULT". WILL NEED NEW CPC 1. REPLACED #1 CPC. OPS CHECKED OK. REMOVED CAP FROM SENSOR PORT.

Part: DRAIN LINE — NONE (R SIDE GALLEY) · airframe 87,494 hrs · 34,146 cycles

TR 2 INDICATIONS INOP ON ELEC SYSTEM ECAM PAGE - ELEC TR2 FAILED APROX 100KTSON TAKE OFF. DURING T/S NOTED ACTIVE WATER LEAK DIRECTLY ABOVE TR2 IN SUSPECT LEAK COMING FROM FORWARD GALLEY AREA AND NEEDS TO BE LEAK APPEARS TO BE COMING FROM #1 GALLEY WATER DRAIN SYSTEM. THE LATERAL AVIONICS (BATTERY) COMPARTMENT. TR2 REQUIRES FIXED BEFORE TR2 IS REPLACED. REMOVED FWD AND AFT GALLEY DRAIN PANELS FOR INSPECTION. NO REPLACEMENT DUE TO PUDDLING ON TOP OF TR2 & ADJACENT COMPONENTS DEFECTS NOTED. LEAK REMAINS. REQUIRE DVI TO ENSURE NO ADDITIONAL DAMAGE DUE TO WATER LEAK. FOUND MAIN DRAIN LINE RIGHT HAND SIDE OF GALLEY WITH BIG CUT IN IT JUST BEFORE BEND DOWN. REMOVED AND REPLACED DRAIN LINE. WATER DRAINS ALL THE WAY OUT TO DRAIN VET WITH NOW LEAKS.

Part: NONE — NONE (FWD AIRCRAFT) · airframe 87,433 hrs · 34,119 cycles

AIRCRAFT RETURNED TO FIELD (RNO) DUE TO "ELEC" SMELL REPORTED BY FLT ATTS IN FWD PART OF AIRCRAFT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. SETTING UP EFS PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. SETTING UP EFS TO PERFORM FURTHER CHECKS TO PERFORM FURTHER CHECKS ACCOMPLISHED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER AEVC, CABIN TEMP CONTROL. AND GENERATOR TEST CHECKED GOOD. POOR AND IS QUITE NOTICEABLE PRIOR TO LANDING. AMM 05-51-10-200-801-C1. FOUND NO AIRCRAFT DEFECTS BEING THE TESTED GALLEY COMPONENTS FOR SMELL AND FOUND NO BURT OR CAUSE OF SMOKE IN THE CABIN. AIRCRAFT ELECTRICAL CIRCUITS ELECTRICAL ORDER. NOTE. THERE IS HEAVY SMOKE IN AND AROUND THE CHECKED GOOD WITH APU, ENGS OR EXTERNAL POWER SUPPLYING POWER. RENO AIRPORT DUE TO WILD FIRES. THE SMOKE AND AIR QUALITY IS

Part: FASTENER — MISSING (INBD SIDE #2 PYL) · airframe 87,233 hrs · 34,016 cycles

FASTENER MISSISNG INBOARD SIDE NBR 2 PYLON REPLACED MISSING SCREW ON INBD SIDE OF #2 PYLON AS REQUIRED

Part: FUEL CAP — MISSING (FUEL PANEL) · airframe 85,675 hrs · 33,262 cycles

PDA 3 CREW REPORTS FUEL CAP MISSING ON WALKAROUND CREW APPLIED CDL 28A. FUEL CAP MISSING PER CDL. STICKER INSTALLED. DISPATCH DESK: 34 NAME: MISTY DATE: 24-JAN-22- DEFERRED DIRECTLY BY TOMC

Part: LINE — LEAKING (FWD PIT FRAME 35) · airframe 85,360 hrs · 33,119 cycles

REF LOGPAGE 7616396. WITHIN 7 DAYS ACCOMPLISH EC/RA 2011-01000, CARGO COMPARTMENT SPILL, SECTION 2.B. IN-DEPTH CLEANUP, IN THE APPROXIMATE AREA FROM BODY STATION FR-24 TO BODY STATION FR-35. BETWEEN STRINGER 41RH AND STRINGER 41LH. FWD CARGO PIT. UNDER POTABLE WATER TANK. D3817014300200 SEE PICTURE. WITHIN 7 DAYS, ACCOMPLISH EC/RA STRINGER 41LH THRU STRINGER 41RH 2011-01000 IN-DEPTH CLEANUP 2.B. FROM FRAME FR-24 THRU FR-35, REF LOGPAGE 7616396. COMPLIED WITH IMMEDIATE CLEAN UP OF POTABLE WATER LEAK, SOURCE OF LEAK WAS AT POTABLE WATER TANK LINE P/N OK TO DIP. IMMEDIATE CLEAN UP COMPLIED WITH. WITHIN 7 DAYS, TOMC-APPROVAL FROM SC1ELBYC COMMENT ACCOMPLISH EC/RA 2011-01000, LAVATORY SPILL, SECTION 2.B., IN-DEPTH CLEANUP, IN THE APPROXIMATE AREA FROM BODY STATION FR-24 TO BODY STATION FR-35. BETWEEN STRINGER 41RH AND STRINGER 41LH. FWD CARGO PIT. UNDER POTABLE WATER TANK. PER ECRA 2011-01000 REV AB QC REVIEWED RECORDS UPDATE QC REVIEWED T/A: 7 DAYS ...RJS/U250018 CONPLIED WITH IN DEPTH CLEANUP FROM FRAME 33 TO 36, STR 41L TO INSPECTION DIP. 41R IAW ECRA 2011-01000 SECTION 2B FOR CARGO COMPARTMENT., O DEFECTS NOTED. LEAKING LINE LOCATED AT FRAME 35-36, NO NEED TO INSPECT FWD TO FRAME 24. REF LOG PAGE 7657144 FOR SUPPLEMENTAL

Part: PUMP — INOPERATIVE (NA) · airframe 85,043 hrs · 32,969 cycles

CREW REPORTS HYD B RES LO LVL MESSAGE WITH INDICATION OF BLUE HYDRAULIC SYSTEM BEING EMPTY. LOCKED BY TOMC MGR DUE TO EMERGENCY DECLARED FOR LANDING. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CHECK RESERVOIR AND OTHER BLUE HYDRAULIC SYSTEMS. ITEM UNLOCKED TOMC SMITH REPLACED BLUE SYSTEM ELECTRIC HYDRAULIC PUMP REF AMM 29-12-15, REPLACED BLUE SYSTEM LP FILTER, HP FILTER AND CASE DRAIN FILTER PRECAUTIONARY, SERVICED BLUE SYSTEM. LEAK AND OPS CHECKS GOOD. ADD EMP:353556 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1994270 SN OFF 4877 PUMP, AC MOTOR OFF 31-2914-9-0001 4877 ON 31-2914-9-0001 2824

Part: SKIN — CRACKED (WING) · airframe 83,168 hrs · 32,129 cycles

FIGURE 6 VIEW ON TOP SKIN REFERENCE DRAWING # R574-40033 SHEET # 11 HOLE #3, 7 AND 9 HAVE CRACK LIKE INDICATIONS - A3NB-05-3-6106. REAMED HOLES 3, 7 & 9 TO FINAL HOLE SIZE .6405 IAW REO L22838 S TAGE 7 STEP 3 NDT INSPECTION COMPLETE WITH NO RELEVANT INDICATIO NS IAW NTM 51-10-01. ACCOMPLISHED PERMANENT REPAIR AT HAECO-LCQ PER REO-L22838 AND EC RA 5725-01071. ORIGINATING DOCUMENT IS UAL N/R 9290117.

Part: SKIN — CRACKED (WING) · airframe 83,168 hrs · 32,129 cycles

FIGURE 7 VIEW ON BOTTOM SKIN REFERENCE DRAWING #R574-40033 SHEET #12 HOLE #24, 27, 8, 32, AND 36 HAVE CRACK LIKE INDICATIONS. REAMED HOLES 24, 27, 18, 32 AND 36 TO FINAL SIZE OF .6405 AND AF T FLUSH FASTENER (TRAPPED BY SPIGOT FITTING) TO FINAL HOLE SIZE OF .5620 IAW REO L22838 STEP (3) STAGE 7. NDT INSPECTION COMPLET E WITH NO RELEVANT INDICATIONS IAW NTM 51-10-01IN DESCREPANCY DESCRIPTION HOLE # 8 SHOULD BE HOLE #18. REPAIR ACCOMPLISHED AT HAECO-LCQ PER REO L22838 AND ECRA 5725-01 071. EC/RA 5725-01071 ORIGINATING DOCUMENT IS UAL N/R 9290117

Part: SPAR — CORRODED (RT WING LE) · airframe 83,168 hrs · 32,129 cycles

RIGHT WING L/E FORWARD SPAR, AREA BETWEEN PYLON FWD ATTACH FITTI NGS, BOTTOM SKIN UPPER SURFACE HAS CORROSION (BEHIND FUEL CONNEC TING SLEEVE PIPE) - A3NB-05-3-6106. PERMANENT REPAIR ACCOMPLISHED PER ECRA 5725-01071.

Part: DOOR FRAME — CRACKED (R1) · airframe 83,168 hrs · 32,129 cycles

R1 DOOR STOP FITTING #7 FRAME 16 DOUBLE JOGGLE AREA HOLE 6 IS CR ACKED IN THE CORNER DOUBLER LAYER AT 1:00. "REPAIR BEFORE NEXT F LIGHT" - SUPPORT TASK - AD 2017-22-03. HOLE #6 ALONG WITH ASSOCIATED HOLE #5 REPAIRED PER ECRA 5311- 02492 PART 1 ITEM 1. FREEZE PLUG FOR HOLE #6 AND COLD WORK FOR HOLE #5. PER SAME ECRA PART 1 ITEM 2 NEED TO ACCOMPLISH INITIAL INSPECTIONS IN ECRA 5311-02492 PART 2 ON OR BEFORE THE ACFT REACHES 38,929 TOTAL ACFT FLIGHT CYCLES, FLIGHT HOURS NOT RELEVANT. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,300 FLIGHT CYCLES THEREAFTER, FLIGHT HOURS NOT RELEVANT. OK TO CARRY INSPECTIONS OF REPAIR TO BE ACCOMPLISHED ON OR BEFORE AIRCRAFT REACHES 38,929 TOTAL FLT CYCLES, (CURRENT CYCLES 32129) FLIGHT HOURS NOT RELEVANT. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3300 FLT CYCLES FLIGHT HOURS NOT RELEVANT THEREAFTER. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED : QC APPROVED RECORDS UPDATE TOMC APPROVED : QC APPROVED INIT: 38,929 TAFC.

Part: SKIN — CORRODED (RT WING LE) · airframe 83,168 hrs · 32,129 cycles

RIGHT WING L/E FORWARD SPAR, AREA BETWEEN PYLON FWD ATTACH FITTI NGS, BOTTOM SKIN UPPER SURFACE HAS CORROSION (BEHIND FUEL CONNEC TING SLEEVE PIPE) - A3NB-05-3-6106. PERMANENT REPAIR ACCOMPLISHED PER ECRA 5725-01071 AT HAECO-LCQ.

Part: SKIN — CRACKED (RT OVERWING AREA) · airframe 83,168 hrs · 32,129 cycles

RT AFT OVER WING HATCH FOUND CRACK AT THE OUTER SKIN 1 AFT OF THE LT LOAD PROFIL TOP AND BOTTOM OF THE NR 2 HORIZONTAL BEAM-A3N B-52-4-6031-AD RELATED NR 9290337/32337. REMOVED AND REPLACED DAMAGED LT SEGMENT FRAME ON RT AFT OW HATCH, IAW A320 SRM 51-42-11 51-42-11-911-001 AT HAECO LCQ REF 9290337.

Part: SKIN — CRACKED (RT OVERWING AREA) · airframe 83,168 hrs · 32,129 cycles

OVER WING HATCH RT AFT FOUND CRACK AT OUTER SKIN 1 IN IF RT LOAD TRANSMITTING PROFILE TOP SIDE OF NR 2 HORIZONTAL BEAM. A3NB-52- 4-6031-AD, PER HAECO LCQ N/R 9290343/32343. REMOVED AND REPLACED DAMAGED RT SEGMENT FRAME ON RT AFT OW HATCH, IAW A320 SRM 51-42-11 51-72-11-911-001 AT HAECO LCQ REF 9290343.

Part: SKIN — CRACKED (LT FUSELAGE) · airframe 83,168 hrs · 32,129 cycles

LT FWD OVER WING HATCH FOUND CRACK AT THE OUTER SKIN 1" AFT OF THE LT LOAD PROFIL TOP AND BOTTOM OF THE NR 2 HORIZONATL BEAM -AD RELATED-A3NB-52-4-6031, PER HAECO LCQ N/R 9290338/32338 GENERATED BY V914670. REMOVED AND REPLACED FWD AND AFT ANGLE SEGMENT AT LT FWD OVERWING HATCH, IAW A320 SRM 51-72-11-911-001 PARA 2(D). REMOVED DOT KF 13.

Part: SKIN — CRACKED (OVERWING EXIT) · airframe 83,168 hrs · 32,129 cycles

LT AFT OVER WING HATCH FOUND CRACK AT THE OUTER SKIN "1 AFT OF THE LT LOAD PROFIL TOP AND BOTTOM OF THE NR 2 HORIZONTAL BEAM A3N B-52-4-6031--AD RELATED, PER HAECO LCQ NR 9290335/32335.

Part: SKIN — CRACKED (OVERWING EXIT) · airframe 83,168 hrs · 32,129 cycles

RT FWD OVERWING HATCH FOUND CRACK AT THE OUTER SKIN 1" AFT OF THE LT LOAD PROFILE TOP AND BOTTOM OF THE NR 2 HORIZONTAL BEAM A3NB- 52-4-6031--AD, PER HAECO LCQ NR 9290336/32336.

Part: SKIN — DAMAGED (FRAMES 35-36) · airframe 82,749 hrs · 31,936 cycles

DURING INSPECTION OF RH FR35-36 FOUND MULTIPLE HOLES SHOWING DEFECTS ACCOMPLISHED INTERIM REPAIR IN REF TO ECRA 5331-02599 PART 1, AC COMPLISH PERMANENT REPAIR PER PART 3 OF ECRA 5331-02599 ON OR BE FORE 89,236 FLIGHT CYCLES OR 197,348 FLIGHT HOURS OKAY TO CARRY FORWARD WITH INTERIM REPAIR ACCOMPLISHED ON RIGHT HAND (RH) FUSELAGE FR35-36 AS DETAILED IN ECRA 5331-02599 PART 1. ACCOMPLISH DTA INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5331-02599 ON OR BEFORE THE AIRCRAFT REACH 89,236 TOTAL FLIGHT CYCLES (FC) OR 197,348 TOTAL FLIGHT HOURS (FH) WHICHEVER OCCURS FIRST. PLANNING TO CONTACT ENGINEERING AFTER 73,000 FC BUT BEFORE 74,000 FC FOR DETAILED INSPECTION REQUIREMENTS. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — DAMAGED (FRAMES 35-36) · airframe 82,749 hrs · 31,936 cycles

DURING INSPECTION OF LH FR35-36 FOUND MULTIPLE FASTENER HOLES SH OWING DEFECTS ACCOMPLISHED INTERIM REPAIR IN REF TO ECRA5331-02598 PART 1, ACCOMPLISH PERMANENT REPAIR PER PART 3 OF ECRA 5331-02598 ON OR BEFORE 89236 FLIGHT CYCLES OR 197348 FLIGHT HOURS OKAY TO CARRY FORWARD WITH INTERIM REPAIR ACCOMPLISHED ON LEFT HAND (LH) FUSELAGE FR35-36 AS DETAILED IN ECRA 5331-02598 PART 1. ACCOMPLISH DTA INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5331-02598 ON OR BEFORE THE AIRCRAFT REACH 89,236 TOTAL FLIGHT CYCLES (FC) OR 197,348 TOTAL FLIGHT HOURS (FH) WHICHEVER OCCURS FIRST. PLANNING TO CONTACT ENGINEERING AFTER 73,000 FC BUT BEFORE 74,000 FC FOR DETAILED INSPECTION REQUIREMENTS. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: ACTUATOR — FAILED (RT SLATS) · airframe 76,558 hrs · 29,184 cycles

SLATS FAULT DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. FOUND THE RT WING OTBD ROTARY SLAT ACTUATOR TORQUE LIMITER TRIPPED. REMOVED AND REPLACED THE SLAT ACTUATOR IAW AMM 27-84-49. PERFORMED OPS CHECKED AND SLATS MOVED AT A NORMAL RATE WITH NO FAULTS FOUND. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY — FAULTY (CABIN) · airframe 76,213 hrs · 29,014 cycles

EMERGENCY LIGHTS BATTERY CAPACITY TEST FAILED, EPSU BAT CAP EMER R & L AFT. REMOVED AND REPLACED LEFT AFT BATTERY 13WL, CHECKED OK AMM33-51-38-400-002A. IDT INSPECTED BATTERY REPLACEMENT/ SYSTEM OPERATION. OK.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 76,213 hrs · 29,014 cycles

EMERGENCY LIGHTS BATTERY CAPACITY TEST FAILED, EPSU BAT CAP EMER R. INSTALLED NEW BATTERY PACK AMM33-51-38. INSPECTED BATTERY INSTALLATION/ EMERGENCY EXIT LIGHTING.

Part: FAN — FAILED (AVIONICS BAY) · airframe 75,769 hrs · 28,808 cycles

AIR RETURN DUE TO SMOKE EVENT. CREW ISOLATED TO VENT EXTRACT FAN PER SMOKE EVENT FORM. EMERGENCY DECLARED. FOUND EXTRACT FAN 18HQ FAULT IN MCDU.ALSO CB AE2 POPPED. REMOVED AND REPLACED EXTRACTOR FAN 18HQ IAW AMM 21-26-51-000-001 -A AND 21-26-51-400-001A. PEFORM OPERATIONAL TEST IAW AMM 21-26- 00-710-001-A. SYSTEM CHECKS GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 75,744 hrs · 28,797 cycles

DURING A NR 2 SERVICE TEST OF EMERGENCY LIGHTS, CIDS FAULTED COMM EMER FWD L, COMM EMER AFT L. . SYSTEM WOULD NOT PASS TEST. EXTERIOR OVERWING LIGHT DID NOT ILLUMINATE. REPLACED POWER EMERGENCY SUPPLY 10WL IAW MM 33-51-38-000-001 AND 33-51-38-400-001. REPLACED THE BATTERY PACK, NOW MESSAGE WAS INT. LOADS FWD L, AND EXT LOAD FWD L, BATTERY EMER R, FOUND THE FWD LT DOOR WITH WRONG LIGHT BULBS INSTALLED, INSTALLED THE CORRECT BULBS, OPS CHECKED GOOD IAW AMM 33-51-00-710-001-A.

Part: FRAME — DAMAGED (FRM 51) · airframe 72,930 hrs · 27,568 cycles

FRAME 51 INNER FLANGE DAMAGED BETWEEN STRINGERS 37 - 38R. REPAIRED IAW SRM53-00-12 TBL 201, PARA 4.A. FIG 201.

Part: FRAME — DAMAGED (FRM 51) · airframe 72,930 hrs · 27,568 cycles

FRAME 51 INNER FLANGE DAMAGED BETWEEN STR 37R AND STR 38R. REPAIRED IAW SRM 53-00-12 TBL 201, PARA 4.A. FIG 201.

Part: SUPPORT FITTING — CORRODED (FRAME 51) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

AFT CARGO FRAME 51, STRINGER 37R SUPPORT FITTING COMMON TO PROFILE PANEL WAS FOUND CORRODED. FITTING WAS REPLACED IAW SRM51-42-11.

Part: FITTING — CORRODED (FRAME 42) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

AFT CARGO BAY FRAME REINFORCEMENT FITTING COMMON TO THE PROFILE PANEL CORRODED, FRAME 52, STRINGER 37R. FITTING WAS REPLACED IAW SRM 51-42-11.

Part: SKIN — CORRODED (FRAME 33) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

FWD CARGO BAY SKIN HAS CORROSION FRAME 33+3 BETWEEN STRINGERS 40 - 41R REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW A32053-21-11.

Part: STRINGER — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

AFT CARGO BAY STRINGER 43L FLANGE HAS CORROSION BETWEEN FRAMES 53 - 54. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW 53-41-13. INSTALLED REPAIR IAW SRM 53-00-13 PARA 4 B FIG 202. SRI 53-00-13--2-002-00 TABLE 210.

Part: STRINGER SPLICE — CORRODED (FRAME 30) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

FWD CARGO BAY, FRAME 30+18 STRINGER SPLICE 42L CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11 PARA 6 AND 51-72-11.

Part: WEB — CORRODED (FRAMES 53-56) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

AFT CARGO DOOR CUT-OUT THRESHOLD WEB AT FRAMES 53 - 56 CORRODED THROUGHOUT UPPER SURFACE. REMOVED AND REPLACED THE AFT CARGO DOOR THRESHOLD WEB IAW SRM53-42-11 PARA 6.

Part: SKIN — CORRODED (FRAME 69) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

EXTERNAL SKIN AT FRAME 69 HAS CORROSION AT WASTE TANK VENT. CUT OUT DAMAGED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-41-11 FIG 205.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

FRAME 68 CORROSION ON L2 DOOR SILL AROUND FAST HOLE. INSTALLED A NEW DOOR SILL IAW SRM 53-41-14, FIG 101, SH 1.

Part: DOOR SILL — CORRODED (R2) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

R2 DOOR SILL HAS HEAVY CORROSION AT AFT GIRT BAR FITTING. INSTALLED A NEW R2 DOOR SILL IAW SRM 53-41-14.

Part: SHEAR TIE — CORRODED (FRAME 31) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

FWD CARGO AT FRAME 31, STRINGERS 41-42R, SHEAR TIE IS CORRODED. INSTALLED A NEW SHEAR TIE IAW SRM 53-21-12, AND SRM 51-21-11.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

FWD CARGO AT FRAME 32, STRINGERS 41-42R SHEAR TIE IS CORRODED. INSTALLED A NEW SHEAR TIE IAW SRM 53-21-12, AND SRM 51-21-11.

Part: STRINGER SPLICE — CORRODED (FRAME 30) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

FWD CARGO BAY FRAME 30+18, STRINGER 41L SPLICE CORRODED. REMOVED DAMAGED STRINGER SPLICE AND INSTALLED NEW IAW SRM 51-42-11.

Part: DOOR SILL — CRACKED (FRAME 67) · airframe 72,930 hrs · 27,568 cycles

BELOW DOOR R2 DOOR SILL, FRAME 67 CRACKED AT DOOR SILL ATTACH POINT. REMOVED DAMAGED FRAME. MANUFACTURED NEW FRAME IAW DWG D53480076 & INSTALLED IAW SRM 51-42-11.

Part: SKIN — DENTED · airframe 72,930 hrs · 27,568 cycles

EXTERNAL FUSELAGE SKIN DENTED 2 FT AFT OF THE L2 DOOR. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE & INSTALLED EXTERNAL DOUBLER IAW SRM 53-41-11.

Part: SHEAR TIE — CORRODED (FRAME 30) · corrosion level 2 · airframe 72,930 hrs · 27,568 cycles

FWD CARGO BAY AT FRAME 30 STRINGERS 41-42R SHEAR TIE IS CORRODED. REPLACED THE SHEAR TIE IAW SRM 51-42-11.

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 72,930 hrs · 27,568 cycles

LEFT ELEVATOR UPPER SKIN PANEL HAS A PUNCTURE AND DISBONDED, 56 INCHES FROM INBD, 13.5 INCHES FROM TE, 1.5 INCHES IN DIAMETER. CUTOUT DAMAGE AND REMOVED MOISTURE, AND INSTALLED COMPOSITE REPAIR IAW SRM 55-21-11, PAR 5D.

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 72,930 hrs · 27,568 cycles

RIGHT ELEVATOR UPPER SKIN PANEL HAS A PUNCTURE, 28 INCHES FROM INBD, .75 INCHES FROM TE. DAMAGE REMOVED AND INSTALLED WET LAYUP REPAIR IAW SRM55-21-11, PAR 5D. SRI 55-21-11, TABLE 203.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 66,880 hrs · 25,044 cycles

FMGC NR 1 INOPERATIVE. R & R NR 1 FMGC IAW MM 22-83-34-000-001-A & 22-83-34-400-001-G. PERFORMED OPERATIONS TEST OF LAND CAT III CAPABILITIES IAW 22-97-00-710-001-A. LAND TEST PASSED, ACFT REMAINS FULLY CAT CAPABLE.

Part: UNKNOWN — MALFUNCTIONED (PA SYSTEM) · airframe 66,161 hrs · 24,762 cycles

PASSENGER ADDRESS INOPERATIVE. SEVERE FEEDBACK IN REAR CABIN OVER PA. ACCOMPLISH CHRONIC REVIEW, OPERATIONS CHECKED GOOD PA FROM REAR OF CABIN.

Part: POTABLE WATER — LEAKING · airframe 66,012 hrs · 24,703 cycles

POTABLE WATER LEAKING FROM BELLY OF ACFT NEXT TO HYD RESERVOIR FILLING PANEL.

Part: COMPUTER — FAULTY (NR 2) · airframe 65,316 hrs · 24,435 cycles

FIRST OFFICER`S TAT DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. REPLACED NR 2 PHC IAW AMM 30-31-34, OPERATIONS CHECKED OK, MESSAGED CLEARED.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT DOOR) · airframe 65,259 hrs · 24,412 cycles

COCKPIT DOOR KEYPAD INOPERATIVE. COMPLIED WITH MEL SEE MT 52-017, REPLACED DOOR CONTROLLER, CHECKED OKAY.

Part: MANIFOLD — LEAKING (BRAKE SYSTEM) · airframe 65,225 hrs · 24,403 cycles

HYD LEAK NEAR NORMAL BRAKE SERVO VLV ON THE RT MLG. R & R BRAKE MANIFOLD ASSEMBLY IAW MM 32-42-16 TO STEP E & REQUIRE COTTER KEY INSTALLED & SEALANT.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 65,157 hrs · 24,377 cycles

CAPTAIN'S FIXED SIDE WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACED CAPTAIN`S FIXED WINDOW IAW AMM 56-11-12-400-002-A, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DIRTY (LT MLG) · airframe 64,776 hrs · 24,236 cycles

LGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN LG. CLEANED PLUGS ON LT MLG DOOR UP LOCK SENSORS 27GA & 29GA. RESET LGCIU1 CB RAN BITE ON LGCIU1 USING MCDU IAW MM 32-69-00-740-001-A, NO FAULTS FOUND. ECAM STATUS IS NORMAL.

Part: DOOR SEAL — LEAKING (L2 DOOR) · airframe 64,751 hrs · 24,227 cycles

FLIGHT ATTENDANT REPORTS PRESSURE LEAK AT DOOR 2L. PRESSURIZED A-C FOUND AFT LOWER CORNER LEAKS & SMALL LEAK AT FWD LOWER CORNER, HAS HISTORY. REPLACED DOOR SEAL IAW MM.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 64,369 hrs · 24,078 cycles

FWD FLIGHT ATTENDANT CALL CHIME FROM COCKPIT INOP-INTERMITTENT. REPLACED FWD FLIGHT ATTENDATNT PUSH BUTTON SWITCH INSIDE COCKPIT, OPERATIONS CHECKED GOOD.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 63,794 hrs · 23,860 cycles

RIGHT WING FUEL TANK LANDING AT 640HB HAS 1 EA DAMAGED HOLE. MAJOR REPAIR. HOLE REPAIRED IAW REO-L01401 AND ECRA 5720-02412. THIS REPAIR HAS NO SUPPLEMENTAL INSPECTIONS REQUIRED. THIS ITEM CREATED FOR MAJOR REPAIR -SDR REPORTING.

Part: SKIN — DAMAGED (LT WING) · airframe 63,794 hrs · 23,860 cycles

LEFT WING TANK PLATE LANDING AT 540LB HAS 1EA ELONGATED HOLE. REPAIRED IAW REO-L01400 AND ECRA5720-02413. CAT "B" REPAIR. MAJOR REPAIR.

Part: SKIN — DAMAGED (LT WING) · airframe 63,794 hrs · 23,860 cycles

LEFT WING TANK PLATE LANDING AT 540PB HAS 2EA ELONGATED HOLES. REPAIRED IAW REO-L01400 AND ECRA 5720-02413. CAT "B" REPAIR.

Part: PANEL — DAMAGED (RT WING) · airframe 63,794 hrs · 23,860 cycles

RT WING FUEL TANK PANEL 640MB HAS 4 HOLES REPAIRED IAW SRM. TOTAL OF 5 HOLES REPAIRED ON RT WING PANEL 640MB NOT 4 DURING LCQ CK TO WHICH SRI APPLIES.

Part: PANEL — DAMAGED (RH WING) · airframe 63,794 hrs · 23,860 cycles

RT WING TANK LANDING FOR PANEL 640KB HAS 1 BOLT HOLE REPAIRED IAW SRM. REPAIR REQUIRES GVI INSPECTION EA 3600C OT 4500 T WHICHEVER COMES FIRST IAW SRI 57-21-11-2-002-00 TBL 20. NOTE: INITIAL INSP CRITERIA OF 54,600 T HAS BEEN EXCEEDED.

Part: SKIN — DAMAGED (RT WING) · airframe 63,794 hrs · 23,860 cycles

RIGHT WING TANK LANDING FOR PANEL 640NB HAD ONE HOLE REPAIRED IAW SRM. REPAIR REQUIRES GENERAL VISUAL INSPECTION EA 3600C OR 4500T WHICHEVER OCCURS FIRST IAW SRI 57-21-11-2-002-00, TBL 203. NOTE: ACFT HAS EXCEEDED ORIGINAL INSP CRITERIA OF 54,600 T. BY- 086636.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 63,300 hrs · 23,668 cycles

LARGE FLUID PUDDLE IN FRONT OF LEFT MAIN LANDING GEAR. RUNNING FROM ACTUATOR. REPLACED LEFT MLG LOCKSTAY ACT PER AMM. OPERATIONAL AND LEAK CHECK GOOD.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 63,241 hrs · 23,646 cycles

FWD CARGO COMPT FLOOR PANEL 131AF DELAMINATED NEAR AFT RIGHT CORNER. REMOVED FLOOR PANEL 131AF INSTALLED SERVICEABLE FLOOR PANEL PER.AMM 53-22-14-400-001-A CONTINUTE FROM PG 3 OF 5 PAR.B7. ACCOMPLISHED FINAL INSTALLATION OF FLOOR PANEL PER MM.

Part: TRIM PANEL — OUT OF POSITION (CABIN) · airframe 62,852 hrs · 23,490 cycles

CREW REPORT: ROW 24DEF LOWER BULKHEAD TRIM PIECE STICKING UP. STRAIGHTENED METAL TRIM AND TAPED IN PLACE. NO PASSENGER HAZARD.

Part: RUB STRIP — UNSECURE (THRUST REVERSER) · airframe 62,832 hrs · 23,484 cycles

CREW REPORT: 6 IN SEAL HANGING FROM ENG 2. FOUND TO BE THE ENG 2 REV LOWER DOOR TEFLON STRIP HANGING OUT AND LOOSE. REPAIR SEAL PER MT78-016 REPAIR PROCEDURE 2C. INSTALLED NEW LATCH DOOR SEAL.

Part: SPINNER — DAMAGED (NR 2 ENGINE) · airframe 62,794 hrs · 23,470 cycles

ENGINE 2 SPINNER HAS MINOR DAMAGE. REMOVED NR 2 ENGINE CONE SPINNER REF AMM 72-38-11-000-010-A 13 & INSTALLED NEW SPINNER CONE.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,584 hrs · 23,389 cycles

ROW 11 AISLE FEELS SPONGY. REPLACED AISLE FLOOR PANEL ROW 10 AND 11ABC.

Part: FASTENER — MISSING (EXHAUST NOZZLE) · airframe 62,455 hrs · 23,344 cycles

ENGINE 2 EXHAUST NOZZLE LOWER FIXED STRUT HAS ONE MISSING RIVET AFT MOST HOLE INBOARD SIDE. LOWER STRUT FAIRING AT 6:00 INBOARD IS MISSING ONE FASTENER. PER MT78-001 ITEM N (2) REPLACED MISSING FASTENER.

Part: SOCKET — LOOSE (EMERGENCY LIGHT) · airframe 62,416 hrs · 23,327 cycles

EMERGENCY LIGHT TEST FAILED. MAINTENANCE MESSAGE ON F/A PANEL IS "EXT LOADS EMER R". REPLACED LAMPS EXTERNAL EMERGENCY LIGHTS. FOUND LOOSE SOCKET. SECURED SOCKET. OPS CHECKED GOOD.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 62,255 hrs · 23,260 cycles

'G' HYD SYS LOSS, RTFL. PERFORMED MANUAL GEAR EXTENSION. REPLACED NR 1 ENGINE DRIVE PUMP AND FILTERS. SERVICED SYSTEM OPS AND LEAK CHECKS GOOD.

Part: PANEL — INOPERATIVE (CABIN) · airframe 62,106 hrs · 23,201 cycles

ATTENDANT CALL INDICATOR PANEL INOPERATIVE AT 998 (LOCATION NOT DEFINED - CHECK CABIN FORM FOR SPECIFIC LOCATIONS). CREW COMMENTS: PANEL AT DOOR 2L INOP. FOUND TO BEGIN WORKING NORMALLY ON GROUND DENVER DUE TO PREVIOUS HISTORY REPLACED AFT ATTENDANT PANEL REF AMM AND ACCOMPLISHED OPS CHECK. REF 23-73-00 -740-005-A ALL TESTS PASS.

Part: SCREEN — DAMAGED (NR 2 EXHAUST) · airframe 61,987 hrs · 23,164 cycles

NR 2 ENGINE, LEFT C-DUCT INNER WALL SHOWS WIRE MESH SCREEN DAMAGE. ACCOMPLISHED PERMANENT REPAIR REF MT 78-010.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 61,926 hrs · 23,140 cycles

CAPT MIC STAYS HOT AND UNABLE TO SELECT VHF NR 1 AND VHF NR 2. SWITCHED TO CAPT ON 3 AND CLEARED HOT MIC. OK TO DF REF MEL 2351AK. REPLACED CAPT ACP. INSTALLED NEW ACP AMM & TESTED PER AMM. ALL TESTS OKAY. REV'D DF #060 AC OK FOR SERVICE.

Part: O-RING — LEAKING (POTABLE WATER) · airframe 61,886 hrs · 23,120 cycles

WATER COMING OUT OF 4 DRAIN HOLES LOCATED BETWEEN FWD CARGO COMPT AND WING ROOT. REPLACED POTABLE WATER TANK LOWER SERVICE LINE FITTING O-RING. PRESSURE LEAK TEST REF AMM 38-10-00-614-001A CHECK GOOD. PERFORMED WATER CLEAN UP REF GNMM 4-06-004.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 61,756 hrs · 23,074 cycles

LOUD THUMP ON UNDERSIDE OF COCKPIT DURING DESCENT. SUSPECT POSSIBLE BIRD STRIKE. FOUND 5" CIRCULAR DAMAGE AREA LOWER LEFT OF RADOME. PER AMM OUT OF LIMITS, DISBOND OF SKIN TO HONEYCOMB.

Part: CIRCUIT BREAKER — FAULTY (ANTI-ICE SYS) · airframe 61,585 hrs · 23,009 cycles

L WING LEAK EICAS, FLIGHT DIVERTED. RESET CB D11, D12.Z22, Z23, F1, Q 7. NO FAULTS NOTED. PERFORMED BITE TEST OF BMC 1 & 2. NO FAULTS NOTED. PERFORMED IDLE RUN ON ENGINE 1 AND 2 FOR 5 MINS, RUNNING BOTH BLEED SYS. NO FAULTS NOTED.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 61,242 hrs · 22,874 cycles

MESSAGE 'EXT LOAD BAT RT' APPEARED ON CIDS SCREEN DURING 3SV EMERGENCY LIGHT TEST. REPLACED RIGHT SIDE BATTERY SUPPLY-CABIN EMERGENCY EXIT ALONG WITH BATTERY AND EXT OVERWING LIGHT BULB. EMERGENCY LIGHT A TEST OKAY.

Part: SOCKET — DIRTY (CABIN) · airframe 60,103 hrs · 22,446 cycles

EXT OVERWING EMERGENCY LIGHTS INOPERATIVE BOTH SIDES OF ACFT. TROUBLESHOT PER MM, CLEANED FWD LIGHT SOCKET ON AFT LIGHT ASSY. OPS CHECKED GOOD.

Part: KNOB — LOOSE (RMP PANEL) · airframe 60,030 hrs · 22,424 cycles

CAPTAIN`S RMP UPPER FREQUENCY KNOB LOOSE. BOTH KNOBS AND THE RMP OPS OK, JUST LOOSE. REMOVED AND REPLACED CAPTAIN`S RMP PANEL, OPS CHECKED GOOD.

Part: RAM AIR TURB — NO TEST · airframe 59,978 hrs · 22,401 cycles

RAT FAILED TEST. OPEN

Part: TRANSCEIVER — FAULTY (VHF COMM) · airframe 59,857 hrs · 22,359 cycles

NR 1 RADIO TRANSMIT BROKEN-UNINTELLIGIBLE MULTIPLE FREQS AND MICS. NEEDS VHF TRANSCEIVER. SWAPPED POSITION 2 WITH POSITION 3, NOW VHF-1 NORMAL. VHF-2 S-N 3393, VHF-3 S-N 3623, VHF-1 S-N 4612. VHF FAULT SEEMS TO BE VOICE TRANSMISSION PROBLEM ONLY, ACARS DATA FUNCTIONS ARE OPERATING NORMAL AT THIS TIME. ANY FUNCTION THAT CAN BE USED, MAY BE USED.

Part: SKIN — WORN (FUSELAGE) · airframe 59,302 hrs · 22,180 cycles

EXTERNAL FUSELAGE FRAME 34 STR 43L - FUSELAGE SKIN HAS DEEP WEAR FROM SCREW. ACP'D ON DOCK WU E5765G BY AMTS 38425, 054888, 181147, 163495. RPR'D PER SRM.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 62,371 hrs · 23,311 cycles

EMERGENCY LIGHT TEST FAULT, "EXT LOAD EMER R" ON CIDS. RIGHT OVERWING EMERGENCY POWER SUPPLY WILL NOT TEST. REPLACED EPSU PER MM AND BATTERY PER MM. EPSU AND EMERGENCY LIGHT SYSTEM OPS TEST NORMAL.

Part: SKIN — DENTED (L1 DOOR) · airframe 59,220 hrs · 22,154 cycles

ACCOMPLISHED VISUAL INSPECTION OF L1 DOOR DENTED AT LOWER DOOR EDGE. DOOR OPENS AND CLOSES WITH NO OBSTRUCTIONS, IS FAIRED AND SITS SQUARELY IN THE OPENING. REPAIRED PER SRM.

Part: WINDSCREEN — DELAMINATED (COCKPIT) · airframe 58,750 hrs · 21,951 cycles

CAPTAIN'S WINDSCREEN DELAMINATING. DELAMINATION WITHIN LIMITS. LEFT LOWER CORNER MOISTURE INGRESSION, WINDOW REPLACED.

Part: FLAP — DENTED (TE FLAP) · airframe 58,379 hrs · 21,793 cycles

RIGHT OTBD AFT FLAP HAS 2 EA DENTS. 1 EA AT 1 8 IN INBD OF CANOE AND 1 IN FROM TRAILING EDGE, 1.125 IN DIA NR 2 DENT LOCATED 2.5 IN INBD OF CANOE 4 IN FROM TRAILING EDGE. DENT IS 1.5 X 2.0 IN SIZE. BOTH DENTS ARE .062 DEEP. FOA ON ARR BY RAMP. NOT ENVIRONMENTAL. OK FOR 1000 FC REF 57-53-00 PG 124 FIG 117. DAMAGE IS ON RT OUTBOARD FLAP, INBD OF OUTBD CANOE FAIRING. ACCOMPLISHED HFEC OF BOTH DENTS NO CRACKS FOUND AT THIS TIME. REPAIRED AREAS PER GN-MM.

Part: COMPUTER — FAULTY (NR 1 ELAC) · airframe 58,211 hrs · 21,726 cycles

FLT CONTROL ELAC NR 1 PITCH FAULT. RESET ELAC NR 1 TWICE, COMES BACK ON FLT CONTROL CHECK. REPLACED ELAC NR 1 PER MM AND CAT III AUTOLAND PER MM. OPS CHECKED OKAY.

Part: SEALANT — DETERIORATED (TCAS ANTENNA) · airframe 58,048 hrs · 21,659 cycles

NOISE IN AREA OF THE UPPER TCAS ANTENNA. ANTENNA SEALANT FOUND DETERIORATED AND BLACK AIR STREAKS EMITTING FROM AREA. ACCOMPLISH CABIN PRESSURIZATION AND CHECK AREA FOR POSSIBLE NOISES ON THE INSIDE OF A-C AND OUTSIDE OF A-C AFTER REPLACEMENT OF TCAS ANTENNA. PRESSURIZED AIRCRAFT REF JRH2-40-80, FOUND NO LEAKS AT UPPER TCAS ANTENNA.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,045 hrs · 21,657 cycles

ELECTRICAL SMELL IN CABIN, FLT DIVERTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,721 hrs · 21,537 cycles

EMERGENCY LIGHT TEST AT FAP FAILS. *33-51-38 EXT LOADS EMER R*. RELAMPED, ALL BULBS ON RIGHT OVERWING EEL, OPS CHECKED GOOD P/N GE1810.

Part: FDU — FAILED (NR 2 ENGINE) · airframe 57,528 hrs · 21,461 cycles

NR 2 ENG FIRE TEST INOPERATIVE. NO ECAMS NO FIRE LIGHTS, ONLY SQUIB - DISCHARGE. REPLACED NR 2 FDU. TESTS OKAY.

Part: SKIN — DAMAGED (FAIRING) · airframe 57,266 hrs · 21,369 cycles

RT WHEEL WELL AFT SIDE OF WHEEL WELL FUSELAGE FAIRING DAMAGED. FAIRING SKIN CRACKED AROUND ATTACHMENT BASE OF FAIRING SUPPORT ROD FITTING. REMOVED PANEL 148FB AND BEGAN REPAIR REF SRM.

Part: SLIDE — OBSTRUCTED (CABIN) · airframe 57,201 hrs · 21,347 cycles

REPLACE THE LT OVERWING SLIDE ACCT. ONE OF THE SLIDE ENCLOSURE BALL-LOCK-PINS IS PAINTED OVER. REPLACED LEFT HAND OVERWING SLIDE PER MM.

Part: AUTOPILOT SYS — DISENGAGED (COCKPIT) · airframe 56,011 hrs · 20,869 cycles

AUTOPILOT DISENGAGED, FLIGHT DIVERTED. THIS OCCURRED 4 TIMES IN FLIGHT, ALSO HAD THE AUTOTHROTTLE DISENGAGE, AND THE NAV SCREENS GO BLANK WITH THE AUTOPILOT KICKING OFF. MX REMOVED FCU TO CHECK FOR DAMAGED PINS OR SOCKETS - NONE FOUND. REPLACED FCU CONTROL PANEL. ACCOMPLISHED AFS AUTOLAND CAT III AND SYS PASSED ALL TEST.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 55,371 hrs · 20,605 cycles

EMERGENCY LIGHT TEST FAILS EXT LOADS EMER R. RELAMPED, OP CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,107 hrs · 20,499 cycles

CABIN EMERGENCY LIGHT CHECK IAW NR 3 SERVICE CHECK FAILS. (EXT LOADS EMER R). FOUND RT OVERWING LIGHT POWER SUPPLY 12WL SHOWING EXT FAULT AT ROW 11DEF. RELAMPED RT OVERWING AFT SLIDE LIGHT ASSY. 12WL BITE TEST OK, EMERGENCY LIGHT CK REF 3SVC, OP CKS OK.

Part: POWER SUPPLY — OUT OF TOLERANCE (EMERGENCY LIGHT) · airframe 55,107 hrs · 20,499 cycles

POWER SUPPLY 11WL USED FOR TROUBLESHOOTING. REPLACED EMERGENCY LIGHT POWER SUPPLY 11WL. OP CKS OK.

Part: MOUNT — CRACKED (CARGO DOOR HANDL) · airframe 55,107 hrs · 20,499 cycles

FOUND DOOR OPENING HANDLE MOUNT CRACKED LETTING HANDLE INTERFERE WITH AND DAMAGING EXTERIOR SKIN PANEL UPON OPENING DOOR. BRACKET PLATE BROKEN, WILL NEED REMOVAL OF ENTIRE DOOR MECHANISM (HANDLE MECH) TO INSPECT FOR FURTHER DAMAGE. DOOR SKIN PANEL INSIDE AFT PIT. REMOVED AFT CARGO DOOR LOCKING HANDLE MECHANISM. REMOVED BASE BRACKET AND DRILLED NEW BRACKET TO FIT.

Part: ADIRU — INACCURATE · airframe 54,754 hrs · 20,339 cycles

NAV ACCURACY LOSS, FLIGHT DIVERTED. ACCOMPLISHED REALIGNMENT OF ADIRU'S. REALIGNMENT NORMAL. ACCOMPLISHED AFS TEST. FMGC'S OK. ENTERED LOCAL VOR-DME INTO MCDU. INDICATION NORMAL ON ND'S.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 54,092 hrs · 20,061 cycles

EMERGENCY LIGHTS TEST FAILS WITH 'EXTERNAL LOADS EMER R' MESSAGE. RELAMPED AFT OVERWING LIGHT ASSY.

Part: BULB — FAULTY (EMERGENCY LIGHT) · airframe 53,857 hrs · 19,960 cycles

3SV EMERGENCY LIGHT TEST DISPLAYED *EXT LOAD EMER R*. T/S TO INOP OVERWING LAMP IN AFT LIGHT, FWD LAMP. RELAMPED WITH BULB AND SYS TEST OK FROM PTP PANEL, REF 3SV FORM.

Part: SLIDE — READS LOW (R2 DOOR) · airframe 53,239 hrs · 19,714 cycles

NR 2 RT MED LOW PRESSURE REPLACED. ALSO SLIDE CAME APART UPON PUTTING SLIDE IN BOX. INSP SLIDE AT DOOR 2R FOUND SECURED ON DOOR, DOOR ASSIST BOTTLE REARMED AND SAFETIED. PIN REMOVED AND STOWED, EMERG LIGHT TEST OK ACFT RETURNED TO NORMAL.

Part: CONTROL PANEL — FAULTY (FMGC) · airframe 53,068 hrs · 19,638 cycles

FMGC NR 2 FAULT, RTFL. IN FLIGHT CB RESET: F-O MAP MODE WAS NOT AVAILABLE. REPLACE FMGC 2 AND PERFORM CAT 3 TEST. PFR FAULTS FMG2-RMP2. REPLACED FMGC2 AND RMP 2. PERFORMED AFS AND LAND TEST. OPS CHK NORMAL. RETURNED AC TO CAT III, NO MESSAGES.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,863 hrs · 19,556 cycles

EMERGENCY LIGHT TEST FAILS 3SV PROCEDURE. MSG INDICATED EXT LOADS EMER R. FOUND EMERGENCY LIGHT OUT RH OVERWING AFT LIGHT ASSY FWD BULB. REPLACED BULB. OP'S CHECKS GOOD.

Part: SLIDE — TORN (L1 DOOR) · airframe 52,124 hrs · 19,210 cycles

DURING ROUTINE RANDOM DEPLOYMENT OF L1 DOOR SLIDE THE RAFT SIDES DEFLATED IMMEDIATELY AFTER FULL DEPLOYMENT. IT WAS FOUND TO HAVE AN APPROX HALF INCH HOLE IN THE RAFT SIDE. THE BASE OF THE SLIDE REMAINED INFLATED. REPLACED SLIDE PER JIC 4S 2592024 BY 310166 AND INSPECTED BY LC49.

Part: WIRE — PINCHED (EMERGENCY LIGHTS) · airframe 52,124 hrs · 19,210 cycles

LEFT SEAT ROWS 13 AND 15 HAVE EMERGENCY LIGHT WIRES PINCHED IN SEAT TRACK. REMOVED SEATS AND REPAIRED WIRES. REINSTALLED SEATS.

Part: GENERATOR — FAULTY (NR 1) · airframe 51,786 hrs · 19,054 cycles

F/A REPORT EMERGENCY EXIT LIGHTS FLASHED 3 TIMES IN FLIGHT ALONG WITH CABIN LIGHTS FLASHING. OCCURRED AFTER REPLACEMENT OF IDG AND GCU. ACCMP ENG RUNS TO ISOLATE WHICH GEN CAUSING CABIN LIGHT FLICKERING. REPLACING NR 1 GENERATOR. RAN ENGINES AND TRANSFERRED POWER BETWEEN ENGINES AND APU. NO FLASHING OF LIGHTS NOTED.

Part: BATTERY — FAILED (CABIN) · airframe 51,786 hrs · 19,054 cycles

EMERGENCY LIGHT SYSTEM TEST FAILS BATTERY AFT LEFT. REPLACED BATTERY, UNIT PASSED SELF TEST.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 51,478 hrs · 18,931 cycles

CABIN EMERGENCY LIGHT CHECK PER A CHECK FAILED TEST. CODE, EMERGENCY BATTERY L DISPLAYED. REPLACED EXTERNAL MOST AFT, FWD LAMP. CABIN EMERGENCY LIGHT TEST OKAY.

Part: ATTACH FITTING — DISCONNECTED (EVAC SLIDE) · airframe 49,778 hrs · 18,232 cycles

FOUND DOOR 1L SLIDE UPPER AFT ATTACH FITTING DISCONNECTED (SPRING TYPE). REPLACED FITTING.

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 48,241 hrs · 17,654 cycles

WEATHER RADAR SYSTEM INOP. FLIGHT DIVERTED. REPLACED CONTROL PANEL AND REPLACED SCANNER, OPS CHECKED NORMAL.

Part: CONTROL UNIT — FAULTY (ELAC 1) · airframe 48,188 hrs · 17,632 cycles

ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC 1, OPS CHECKED NORMAL.

Part: WARNING LIGHT — ILLUMINATED · airframe 48,086 hrs · 17,593 cycles

L AILERON FAULT DISPLAYED ON UPPER ECAM SCREEN.

Part: SERVO — MALFUNCTIONED (LT AILERON) · airframe 48,086 hrs · 17,593 cycles

LT AILERON FAULT DISPLAYED ON UPPER ECAM SCREEN. CHRONIC A/C. MX WANTS TO WATCH THE LATEST FIX BEFORE CLOSING. REPLACED L B AILERON SERVO. ALL OPS NORMAL.

Part: SERVO — LEAKING (LT AILERON) · airframe 47,864 hrs · 17,510 cycles

AILERON SERVO FAULT DISPLAYED. LEFT AILERON SERVO FAILURE, INTERNAL HYDRO LEAKAGE. REPLACED LEFT AILERON GREEN SERVO CONTROLLER, OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,493 hrs · 17,380 cycles

EXTERNAL FUSELAGE SKIN IS DAMAGED AT FR 69+4 14" BELOW FLOOR. ACCOMPLISHED MAJOR REPAIR AT SFO.

Part: COVER — OUT OF POSITION (EVAC SLIDE) · airframe 47,202 hrs · 17,279 cycles

DOOR 1L SLIDE COVER HAS MOVED AND PREVENTS SEEING PRESSURE GAUGE. REPLACED ENTIRE SLIDE PACK ASSY.

Part: HOSE — DAMAGED (GREEN HYD SYS) · airframe 46,424 hrs · 16,984 cycles

FLIGHT LOST GREEN HYDRAULIC SYSTEM SOMETIME AFTER DEPARTING LCQ. DECLARED EMERGENCY WITH ATC. FOD DAMAGE IN WHEEL WELL. REPLACED THE RIGHT GEAR DOWNLOCK ACTUATOR HOSE. SERVICED GREEN HYDRO SYSTEM.

Part: POWER SUPPLY — NO TEST (EMERGENCY POWER) · airframe 45,820 hrs · 16,756 cycles

DURING OPERATIONAL TEST FOR THE EMERGENCY POWER SUPPLY UNITS, EPSU EXT LOAD AFT L IS SHOWN ON PTP PANEL (CIDS DIS). ELECTRICAL LEAD FAILURE IN 2L SLIDE PACK. REPLACED 2L SLIDE.

Part: SERVO CONTROL — INOPERATIVE (NLG STEERING) · airframe 45,732 hrs · 16,723 cycles

NOSE WHEEL STEERING INOPERATIVE. FAULTY NOSE WHEEL STEERING CONTROL SERVO 6GC. REPLACED NOSE WHEEL STEERING SERVO CONTROL.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 45,396 hrs · 16,599 cycles

RTFL DUE TO SLOW CABIN DEPRESSURIZATION.

Part: IDG — LEAKING (NR 1) · airframe 44,643 hrs · 16,317 cycles

RTFL DUE TO A IDG LOW OIL PRESSURE PROBLEM. [SUP 06-01-07] REPLACED NR 1 IDG. AT OVERHAUL, FOUND A LEAKING SEAL THAT WAS ALLOWING FLUID TO ESCAPE THE SYSTEM.

Part: WIRE — SHORTED (UNKNOWN) · airframe 44,457 hrs · 16,244 cycles

FOUND SHORTED WIRE BETWEEN SEC AND ACTUATOR. [SUP 05-16-07] FLT RTBL WITH EFCS TEST 1 FAILURE MESSAGE. EFCS FAULTED SEC 2. INITIALLY SWAPPED SEC 2 WITH SEC 3 TO DETERMINE IF FAULT WAS WITH THE SEC UNIT ITSELF. POST SWAP OPS CHECK FAILED, SO STARTED TO PERFORM RESISTANCE CHECKS ON CONNECTORS PER TSM. FOUND SEC 2 PIN 15D HAD 8 OHM RESISTANCE WITH GROUND AND TSM SPECIFIES THAT SHOULD HAVE HAD AT LEAST 100 MEGAOHM. UNWRAPPED WIRING BUNDLE FOR RT ELEVATOR OUTBOARD SERVO AND FOUND RED WIRE 5954-PF20 TO BE SHORTING UNDERNEATH THE CARGO COMPARTMENT FORWARD MOST FLOORBOARD. REPAIRED WIRE WITH ENVIRONMENTAL SPLICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 43,880 hrs · 16,026 cycles

DUE TO NR 2 ENG FLUCTUATING PARAMETERS & EGT INCREASE CREW SHUT DOWN ENGINE & RETURNED TO FIELD. REPLACED NR 2 ENGINE VARIABLE STATOR VANE ACTUATOR (VSVA). HIGH PWR RUN ACCOMPLISHED AND NO FURTHER FAILURE MESSAGES. THIS EVENT WAS CAUSED BY A DUAL CHANNEL FAILURE OF THE VSVA. THIS UNIT WAS RECEIVED AS AN EXCHANGE UNIT FROM GOODRICH IN MAY 06. ITS HAS FAILED FROM STOCK TWICE AND WILL BE REJECTED FROM UA'S INVENTORY AS A "ROUGE UNIT". SHOP FINDINGS INVESTIGATIONS ON GOING AT GOODRICH/MOOG.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 41,230 hrs · 14,947 cycles

AFTER SLIDE INSPECTION, RAN EMERGENCY TEST ON THE PTP. MESSAGES -BATT EMER R- AND -INT LOADS EMER R- APPEARED. REPLACED POWER SUPPLY 12WL AND BATTERY PACK. EMERGENCY LIGHTS OPS CHECK OKAY.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 39,255 hrs · 14,150 cycles

FLIGHT DIVERTED DUE TO WEATHER RADAR MALFUNCTION ALONG WITH FUEL AND WEATHER CONSIDERATIONS.

Part: DAMPER — LEAKING (NR 1 YAW) · airframe 33,583 hrs · 12,286 cycles

AIRCRAFT LANDED UNDER AMBER ALERT DUE TO FAILURE OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. SUBSEQUENT REPLACEMENT WITH NEW YAW DAMPER AND OPS CHECK WERE ACCOMPLISHED WITH NO FURTHER ANOMALY.

Part: SKIN — CONTAMINATED (ELEVATOR) · airframe 32,666 hrs · 11,957 cycles

WATER INGRESSION FOUND AT THE FOLLOWING LOCATIONS: LT ELEVATOR UPPER SURFACE - 2 2" BY 2" AREAS, 3.5 INCHES FWD OF TRAILING EDGE, 160.8 AND 187.6 " FROM THE IB END. LWR SURFACE HAS 7 2' BY 2" AREAS, 3.5 " FWD OF TE AND 139.2, 146.2, 153.6, 160.7, 175.3, 181.6, 187.6 INCHES FROM IB EDGE. REPAIRED DAMAGED AREAS IAW SRM 55-21-11 TO ELIMINATE WATER INGRESSION.

Part: STRUCTURE — CONTAMINATED (ELEVATOR) · airframe 32,666 hrs · 11,957 cycles

8 AREAS OF WATER INGRESS WERE FOUND ON THE RT ELEVATOR. UPPER SURFACE - 5 EACH AREAS 2 BY 2 INCHES, ALL 3.5 INCHES FWD OF THE TE, AND 132, 153.5, 1 61,168.8, 175 INCHES FROM IB EDGE. 3 EACH AREAS 2 BY 2 INCHES ON THE LWR SURFACE, ALL 3.5 INCHES FROM TE AND 153.5, 160.8, AND168 INCHES FROM IB END. REPAIRED DAMAGED AREAS IAW SRM 55-21-11 TO ELIMINATE WATER INGRESSION.

Part: APU — MALFUNCTIONED (APU BAY)

RETURNED TO FIELD UNDER AMBER ALERT DUE TO APU AUTO SHUTDOWN.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 25,730 hrs · 9,360 cycles

COMPRESSOR STALL ON NUMBER TWO ENGINE.

Part: BEAM — BENT (CARGO DOOR) · airframe 24,815 hrs · 9,040 cycles

FORWARD CARGO DOOR AFT ACTUATOR MOUNT BEAM IS BENT. REPLACED ACTUATOR ATTACH BEAM. MAJOR REPAIR ACCOMPLISHED.

Part: FUEL CONTROL — LEAKING (APU) · airframe 20,374 hrs

ON TAXI OUT AN AMERICAN AIRLINES CREW REPORTED FLAMES FROM THE APU EXHAUST. CREW SHUT DOWN THE APU AND RETURNED TO THE GATE. MM RESTARTED THE APU AND FLAMES RETURNED. FIRE BOTTLE WAS BLOWN AND FIRE DEPARTMENT CALLED TO STANDBY. *S/D* THE CAUSE OF THE FAILURE HAS BEEN ATTRIBUTED TO A PARTIALLY STUCK SOLENOID VALVE ON THE FUEL CONTROL UNIT. THIS PERMITTED FUEL TO ENTER THE COMBUSTOR FOLLOWING APU SHUTDOWN. THE APU SEIZURE OCCURRED AFTER THE FAILURE EVENT AND CAN BE ATTRIBUTED TO THE CORROSION IN THE GEARBOX AND INGESTED EXTINGUISHING AGENT IN THE LOAD COMPRESSOR AND POWER SECTION. ROTATING COMPONENTS WERE NOT RUBBED. CORROSION HAS BEEN ATTRIBUTED TO INGESTION OF WATER AND CHEMICAL EXTINGUISHING AGENT.

Part: AIR DIST — ODOR (CABIN)

STRONG OIL ODOR THROUGHOUT CABIN.

Part: PASSENGER SEAT — CRACKED (CABIN)

DURING FIRST HEAVY MAINTENANCE VISITS FOR AIRBUS A320-232, MAINTENANCE FOUND VIRTUALLY A 100 PERCENT FAILURE RATE OF THE SEAT PANS ON RECARO MODEL 3410, 720 SERIES PASSENGER SEATS. THE FAILURE ARE CRACKS IN THE SEAT PANS ADJACENT TO THE ATTACHMENT HOLES AT THE FORWARD EDGE OF THE SEAT PAN. THESE HOLES ACCEPT SCREWS THAT ATTACH TO THE SEAT PAN TO THE SEAT STRUCTURE. THERE ARE 3 OF THESE ATTACHMENT HOLES, AND ON EACH PAN, A MINIMUM OF ONE HOLE HAS BEEN FOUND WITH CRACKS ADJACENT TO IT. SUBMITTER STATED, IN MOST INSTANCES, 2 OF THE 3 HOLES HAVE BEEN FOUND WITH CRACKED AREAS ADJACENT TO THEM.

Part: FIRE LIGHT — ILLUMINATED (APU)

CREW REPORTED THE APU FIRE LIGHT CAME ON WHILE IN CRUISE. NO ASSOCIATED ECAM WARNINGS. THE APU WAS OFF, AND THE APU FIRE LIGHT IS INTERMITTANT. *S/D* POST FLIGHT REPORT SHOWS ECAM WARNING APU FIRE, BUT NO FAILURE MESSAGE. APU FDU TESTED OK. LAST LEG AND PREVIOUS LEGS REPORTS SHOW NO FAULTS. APU START AND RUN NORMAL. CHECKED FIRE LOOPS IN APU COMPARTMENT AND FOUND NO DISCREPANCIES.

Part: BRAKE SYST — MALFUNCTIONED (LANDING GEAR)

BRAKE FAILURE ON TAXI. NR 1 ENG RUNNING, SINGLE ENGINE TAXI. WHILE STARTING NR 2 ENG, ALL BRAKES FAILED. RECYCLED ANTI-SKID NWS SWITCH, NO HELP. *S/D* PERFORMED HYD QTY CK, DEPRESSURIZED AND REPRESSURIZED BRAKE ACCUM. BRAKES CHECKED NORMAL. RAN ENG 1 AND CONFIRMED PUMP PRESS. YELLOW PUMP PRESS ALSO GOOD. NO FAULTS FOUND.

Part: PROX SENSOR — OUT OF ADJUST (CARGO DOOR)

RETURNED TO FIELD AT IAD DUE TO REAR CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. *S/D* FOUND AFT CARGO DOOR LOCKING HANDLE MISALIGNED WITH PROXIMITY SENSOR IN DOOR.

Part: CIRCUIT BOARD — FAILED (ANN PANEL)

CREW ABORTED TAKEOFF AT 80 KNOTS DUE TO AVIONICS FAILURE ON THE AIRCRAFT. *S/D* OVERHEAD LIGHT FAILED TO ILLUMINATE WITH EXTRACT FAN SWITCH SET TO OVERRIDE MODE. REPLACED ANNUNCIATOR DIM TEST CARD 6LP. AIRCRAFT OPERATED NORMALLY WITH NO OTHER DEFECTS FOUND.

Part: MECHANISM — LACK OF LUBE (CARGO DOOR)

FLIGHT RETURNED TO PDX DUE TO AFT CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT WAS DISPATCHED WITH THE CARGO DOOR HANDLE FLUSH AND THE DOOR INDICATION LIGHTS NORMAL, HOWEVER, THE DOOR FLAPPER PANEL MOST LIKELY DID NOT SPRING BACK TO THE FLUSH POSITION. THE AIRCRAFT RETURNED TO THE FIELD WHERE THE DOOR HANDLE WAS FOUND PROTRUDING AND THE FLAPPER PANEL WAS NOT FAIRED. THE DOOR MECHANISM WAS LUBED AND OPERATED NORMALLY. NO FURTHER DEFECTS HAVE BEEN FOUND.

Part: RELEASE CABLE — TANGLED (L 1 DOOR SLIDE)

DURING SCHEDULED SLIDE DEPLOYMENT AT C-CHECK, SLIDE AT DOOR 1 LEFT DID NOT DEPLOY. SLIDE RELEASE CABLE WAS FOUND WRAPPED AROUND VALVE BODY PREVENTING SLIDE FROM DEPLOYING. AIRCRUISERS HAS CREATED A SERVICE BULLETIN TO ENSURE PROPER PACKING OF SLIDES. UNITED WILL ACCOMPLISH A FLEET CAMPAIGN TO REMOVE E ALL POTENTIALLY AFFECTED SLIDE RAFTS.