N563UA

Part: FITTING — LACK OF LUBE (GIRT BAR) · airframe 69,386 hrs · 25,382 cycles

CANNOT ARM DOOR 2L. LUBED GIRT BAR FITTINGS. CHECKED GOOD SEVERAL TIMES, NO DEFECTS NOTED.

Part: ADC — FAULTY (RIGHT) · airframe 69,226 hrs · 25,329 cycles

ELEV ASYMMETRICAL STATUS MESSAGE WILL NOT CLEAR. REPLACED RT AIR DATA COMPUTER DUE TO FAULT SET ON RT SAM MODULE. ELEV ASYMMETRICAL MESSAGE GONE. ACCOMPLISHED SUCCESSFUL CURRENT STATUS TEST 30, AIRCRAFT REMAINS FULL CAPABILITY.

Part: PROXIMITY SENSOR — FAULTY (L2 DOOR) · airframe 69,105 hrs · 25,289 cycles

SLIDE LT ON DOOR 2L, DOOR NOT ARMED. HAS HISTORY, LIGHT STAYS ON ALL THE TIME, CONFIRMED GIRT BAR ENGAGEMENT IAW MEL. REPLACED BOTH PROX SENSOR 720 & 730, ALSO ANN LT ASSEMBLY SYSTEM, OPERATIONS CHECKED NORMAL.

Part: SCREW — DEFECTIVE (CABIN SEAT) · airframe 69,000 hrs · 25,253 cycles

ROW 11 DEF ROW ROCKING BACK & FORTH. REMOVED SEAT, REPLACED ANTI-RATTLE SCREW, REINSTALLED ROW 11 DEF. SEAT SECURED & OK TO OCCUPY.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW) · airframe 68,351 hrs · 25,032 cycles

OXYGEN PRESSURE LOW. 950 PSI. SERVICED CREW OXYTEN SYSTEM IAW AMM.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,138 hrs · 24,969 cycles

NR 2 ENGINE BLADE, NR 16 DAMAGED. REPLACED NR 2 ENG BLADE, NR 16 AND MATE BLADE NR 34 WITH MATCHED PAIR IAW MM72-31-02.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,138 hrs · 24,969 cycles

NR 2 ENGINE BLADE NR 12 DAMAGED. REPLACED BLADE AND MATE BLADE WITH MATCHED PAIR IAW MM 72-31-02.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,138 hrs · 24,969 cycles

NR 2 ENGINE NR 30 BLADE DAMAGED. REPLACED NR 2 ENG BLADE NR 30 AND MATE BLADE NR 12 IAW MM 72-31-01.

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 68,138 hrs · 24,969 cycles

FOUND NR 2 ENG FAN BLADE NR 8 DAMAGED BEYOND REPAIRABLE LIMITS. REPLACED NR 8 AND NR 26 BLADES WITH MATCH SET. ACCOMPLISHED INSTALLATION OF COMPRESSOR INLET CONE IAW MM 72-31-01-401.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,138 hrs · 24,969 cycles

NR 2 ENGINE BLADE NR 14 DAMAGED BEYOND LIMITS. REPLACED NR 2 ENG BLADE NR 14 AND MATE BLADE NR 32 WITH A MATCHED PAIR IAW MM 72-31-02.

Part: STUD — LOOSE (SEATS 38DEF) · airframe 68,068 hrs · 24,949 cycles

CREW REPORT SEAT ASSY AT 38DEF IS LOOSE AT SEAT TRACK. REPLACED SEAT TRACK STUD AND NUT ON THE FWD INBD LEG OF SEAT ASSY 38DEF IAW AMM.

Part: LINK — OUT OF ADJUST (L2 DOOR) · airframe 68,024 hrs · 24,934 cycles

FLIGHT ATTENDANT REPORTS DOOR 2L DIFFICULT TO ARM. ADJUSTED GIRT BAR LIFTING SHOE LINK ADJUSTED SCREW.

Part: HANDLE — OUT OF SEQUENCE (L2 DOOR) · airframe 67,635 hrs · 24,824 cycles

2L PASSENGER ENTRY DOOR WOULD NOT CLOSE. REPORTED BY CUSTOMER SERVICE. 2L DOOR HANDLE OUT OF SEQUENCE, CYCLED DOOR OPEN AND CLOSED FROM INSIDE TO SEQUENCE HANDLE WITH DOOR MECHANISM. OPS OKAY.

Part: FILTER — CLOGGED (RECIRC FAN) · airframe 67,591 hrs · 24,811 cycles

WITH RIGHT RECIRCULATION FAN ON, F/A COMPLAINED CABIN VERY NOISY, DIFFICULT TO HEAR PA. ALSO VERY NOISY IN COCKPIT WITH PACKS ON AND RIGHT RECIRCULATION FAN OFF. FOUND RT RECIRCULATION FAN FILTER COLLAPSED FROM DIRT & PLEATED MATERIAL DISINTEGRATING. REMOVED AND REPLACED FILTER. SYS OPS CHECKED GOOD.

Part: SEAL — UNSECURE (R4 DOOR) · airframe 67,378 hrs · 24,749 cycles

LOUD SQUEAL AT R4 DOOR. FOUND R4 DOOR UPPER CORNERS FWD AND AFT LEAKING. SECURED SEAL, PRESSURIZED WITH NO FAULTS NOTED. OK TO CONTINUE.

Part: STRUCTURE — BROKEN (OVERWING EXIT) · airframe 67,364 hrs · 24,746 cycles

THE 20F OVERWING EXIT DOOR MOULDING BROKEN. MOULDING IN COCKPIT. WINDOW AT SEAT 20F OVERWING NEEDS A WINDOW SHADE ASSEMBLY. MOULDING FRAME AT WINDOW INOP. WINDOW SHADE WORKS OK. NO DAMAGE TO OVERWING EXIT DOOR. REPLACED MOULDING FRAME AT SEAT 20F, OK FOR FLIGHT.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 67,294 hrs · 24,725 cycles

FUEL LEAKING FROM ACCESS PANEL UNDER RIGHT WING. FOUND ACCESS PANEL 642AB IMPROPERLY INSTALLED. REMOVED AND INSTALLED ACCESS PANEL. LEAK CHECKED GOOD, NO DEFECTS NOTED.

Part: SKIN — DENTED (BS 1420-1440) · airframe 67,290 hrs · 24,723 cycles

DENT IN FUSELAGE SKIN ABOVE STR17L BTWN BS 1420 AND 1440. REMOVED DAMAGE IAW SRM 53-00-01. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01 FIG, 201 REPAIR 3.

Part: SKIN — DENTED (BS 1420-1440) · airframe 67,290 hrs · 24,723 cycles

SKIN DENTED BS 1420-1440, BETWEEN STRINGERS 16 - 17L. HFEC INSPECTION IAW NDT PT 6, 51-00-19, NO CRACKS NOTED. DENT SMOOTH AND CRACK FREE. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201. FABRICATED AND INSTALLED DOUBLER IAW 53-00-01 FIG 201.

Part: SKIN — DENTED (BS 876.5 S7R) · airframe 67,290 hrs · 24,723 cycles

DENT IN FUSELAGE SKIN ACROSS S7R BS 876.5. REPAIRED IAW ECRA 5330-04463 AND REO MO625 RE V IR.

Part: SKIN — DENTED (BS1455 S24-25L.) · airframe 67,290 hrs · 24,723 cycles

PROTRUDING DENT IN FUSELAGE SKIN BS 1455 BETWEEN S24-25L. REMOVED DAMAGE. FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLER IAW ECRA 5361-01043. MAJOR REPAIR

Part: ANGLE — CRACKED (BS 1160) · airframe 67,290 hrs · 24,723 cycles

BS 1160 LEFT ANGLE ISOLATOR CRACKED. REMOVED AND REPLACED ANGLE ON LT ISOLATOR AT BS 1160 IAW SRM 51-40-02.

Part: SKIN — DENTED (BS 768 S16L) · airframe 67,290 hrs · 24,723 cycles

DENT ON SKIN 2 INCHES BELOW S16L BS 768. REPAIR INSTALLED IAW SRM. PRP IS A CAT "B" REPAIR PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,290 hrs · 24,723 cycles

LIGHTNING STRIKE ON FUSELAGE LWR SKIN BS 403 RBL 9. REPAIRED LIGHTNING STRIKE DAMAGE LWR SKIN BS 403 RBL 9 IAW B757-200 SRM 53-00-01 FIG 201.

Part: SKIN — DAMAGED (BS 463) · airframe 67,290 hrs · 24,723 cycles

LIGHTNING STRIKE AT BS 463, SIX INCHES BELOW S27R. REPAIRED DAMAGE IAW SRM 53-00-01 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 87,290 hrs · 24,723 cycles

LIGHTNING STRIKE ON FUSELAGE LWR SKIN BS 414 BETWEEN STR 26R-27R. REPAIRED LIGHTNING STRIKE DAMAGE ON LWR FUSELAGE SKIN BS 414 BETWEEN STR 26R-27R IAW B757 -200 SRM 53-00-01 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,290 hrs · 24,723 cycles

BS 270 RBL 8 WL 138.50 HAS A LIGHTNING STRIKE. REPAIRED LIGHTNING STRIKE DAMAGE BS 270 RBL 8 WL 138.50 IAW B757-200 SRM 53-00-01 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,290 hrs · 24,723 cycles

BS 288 STR 27R WL 138.5 HAS A LIGHTNING STRIKE. REMOVED LIGHTNING STRIKE DAMAGE AT BS 288 STR 27R WL 138.5 IAW B757-200 SRM 53-00-01 FIG 201. INSTALLED REPAIR FASTENER IAW B757-200 SRM 53-00-01 FIG 201 SECTION 1.

Part: NUT — UNSECURE (SEAT 21C) · airframe 67,191 hrs · 24,691 cycles

SEAT 21C LOOSE AT FLOOR MOUNT. REPLACED SEAT ANTI-RATTLE NUT, SECURED SEAT. COMPLETED IDT INSPECTION, SEAT SECURE.

Part: ROLLER — DAMAGED (R1 DOOR) · airframe 67,156 hrs · 24,680 cycles

R1 DOOR WILL NOT CLOSE. DAMAGE TO AFT UPPER CRANK ROLLER AND LATCH CAM ON DOOR FRAME. R1 DOOR UPPER AFT ROLLER DAMAGED, UPPER CAM ALSO GOUGED DOOR WILL NOT CLOSE UNLESS PRESSURE IS PUT UPON UPPER RT CORNER AS DOOR GOES CLOSED. REPLACED UPPER ROLLERS AND AFT UPPER LATCH CAM FITTING. OPS CHECKED NORMAL.

Part: STRAP — CORRODED (FUSELAGE) · airframe 66,505 hrs · 24,455 cycles

AFT PIT, BS 1400 BUTT SPLICE STRAP IS CORRODED BETWEEN STR 27L-STR 28L. REMOVED DAMAGED SECTION OF BUTT SPLICE STRAP, (CIRCUMFERENTIAL SKIN SPLICE), AND FABRICATED AND INSTALLED A DOUBLER AND FILLER REPAIR PER EA PD57-53 -064 AND EVA 80344.

Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 66,357 hrs · 24,398 cycles

FWD CARGO DOOR SKIN SCRATCHES ON LOWER 12 INCH SECTION OF DOOR. ONE SCRATCH IS APPROX 3 INCH SOME JUST ABRASION SURFACE. NO CRACKS FOUND, DAMAGE WITHIN LIMITS REF SRM 52-30-01. DEPTH OF SCRATCHES MEASURED .006 AT DEEPEST POINT. HFEC ACCMP'D BLENDED AND TREATED AREAS. DOCUMENT LOCATION OF REPAIR, APPLY FINISH COAT AS REQUIRED AND ACCMP DENT DOT PROCESS PER GMM06-35-05.

Part: BLADES — DAMAGED (RT ENGINE) · airframe 66,231 hrs · 24,351 cycles

THREE BLADES ON RIGHT ENGINE NICKED. FOUND FOUR BLADES DAMAGED REPAIRED BLADES PER AMM.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 66,130 hrs · 24,318 cycles

DENT LEFT FUSELAGE 1.5" X .750" X .080" DEEP LOCATED 44" AFT OF DOOR 1L AFT CUTOUT 1" AFT OF FRAME STA 418 & 11" ABOVE WL BETWEEN STRINGER S16 AND S15. DAMAGE WITHIN LIMITS. BURNISHED LIGHT SCRATCH IN TOP COAT TREATED AND PRIMED. ITEM GENERATED FOR PAINT. PAINTED AREA.

Part: ROTARY SWITCH — INTERMITTENT (COCKPIT) · airframe 65,383 hrs · 24,062 cycles

APU SHUTDOWN. TWO START ATEMPTS. TROUBLESHOT APU FOUND ROTARY SWITCH IN COCKPIT TO BE INTERMITTANT WILL REQUIRED TO BE REPLACED (563-3109) PCN NIS EWR. REPLACED APU STARTER SWITCH. APU STARTS NORMAL, OPS NORMAL.

Part: ACTUATOR — FAILED (SPAR VALVE) · airframe 64,777 hrs · 23,854 cycles

LEFT ENGINE SPAR DISAGREE LIGHT IS ON, ALSO LT STAR VALVE CIRCUIT BREAKER ON P6 PANEL WILL NOT RESET. REPLACED LT SPAR VALVE ACTUATOR. REPLACED PER MM, OPS CHECKED OK.

Part: SCUFF PLATE — FAULTY (FUSELAGE) · airframe 64,342 hrs · 23,700 cycles

LOUD HUMMING NOISE COMING FROM BOTTOM LEFT CORNER OF DOOR 1R. TURNING CHILLER OFF NO HELP. REPLACED FWD AND CENTER 1R MED SCUFF PLATE IAW MM. LEAK CHECK GOOD.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 64,236 hrs · 23,662 cycles

NR 2 ENGINE INBD THRUST REVERSER DAMAGED. DAMAGE IS LOCATED NEAR THE CORE COWL VENT PANEL UPPER-FWD CORNER AREA. DAMAGE IS APPROXIMATELY 3 INCHES BY 3 INCHES. DETERMINED BOTH INNER AND OUTER FACE SHEETS ARE DAMAGED AT EDGE OF GRILL CUTOUT.

Part: ACTUATOR — MALFUNCTIONED (LT WING) · airframe 64,110 hrs · 23,613 cycles

L FUEL SPAR VALVE ENG START NORMAL. UNCOMMANDED SHUT DOWN. FOUND LEFT SPAR VLV CB AT LOCATION E01 ON P6-1 OPEN. REPLACED LEFT SPAR VALVE ACTUATOR. RAN ENGINE, NORMAL OPS.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 64,110 hrs · 23,613 cycles

L FUEL SPAR VAL. ENG START NORMAL. UNCOMMANDED SHUT DOWN. SAMC TEXT: CREW CONTACTED SAM. FOUND LEFT SPAR VLV CB AT LOCATION E01 ON P6-1 OPEN. REPLACED LEFT SPAR VALVE ACTUATOR. RAN ENGINE, NORMAL OPS.

Part: FASTENER — MISSING (LT WING) · airframe 64,065 hrs · 23,592 cycles

MISSING 1 SCREW ON TOP SEAM OF WING ROOT PANEL FWD OF L WING. REPLACED MISSING FASTENER.

Part: GIRT BAR — LACK OF LUBE (4L DOOR) · airframe 63,844 hrs · 23,513 cycles

AFT LEFT DOOR NOT ARMING. LUBED GIRT BAR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,705 hrs · 23,459 cycles

NR 2 MAIN ENTRY DOOR EXT EMER LIGHT INOPERATIVE. RELAMPED (RT) OPERATES NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,705 hrs · 23,459 cycles

NR 4 LT MAIN ENTRY DOOR EMER EXT LIGHT, INOPERATIVE. RELAMPED, OPERATES NORMAL.

Part: RESERVOIR — DISCHARGED (R4 DOOR) · airframe 63,657 hrs · 23,443 cycles

R4 DOOR SLIDE DEPLOYED. REPLACED DOOR EMERGENCY POWER RESERVOIR PER MM. REPLACED DOOR 4 RT SLIDE PACK PER MM.

Part: GIRT BAR — DAMAGED (R4 DOOR) · airframe 63,657 hrs · 23,443 cycles

DOOR 4R ARMING LEVER DIFFICULT TO ARM AND DISARM. UPON ESCAPE SLIDE INSTALLATION DOOR 4RT. FOUND AFT END OF GIRT BAR HANGING UP DURING ARMING AND DISARMING, GIRT BAR SPRING IS BENT. REPLACED WITH NEW GIRT BAR ASSY. DOOR OPS CHECKED GOOD.

Part: ATTACH FITTING — MISINSTALLED (R4 DOOR) · airframe 63,657 hrs · 23,443 cycles

DOOR 4RT FWD GIRT BAR LINKAGE ATTACH FITTING INSTALLED INCORRECTLY WITH SERRATED PLATE ON DOOR. (CENTER GROOVE NO ALIGNED WITH NOTCH IN PLATE). REPLACED FWD GIRT BAR LINKAGE ATTACH FITTING ON PASS DOOR 4R.

Part: LINKAGE — WORN (R4 GIRT BAR) · airframe 63,657 hrs · 23,443 cycles

R4 DOOR GIRT BAR LINKAGE FWD SIDE AT THE BOTTOM OF DOOR IS WORN AND VERY LOOSE. REPLACED FWD GIRT BAR LINKAGE ATTACH FITTING. ACCOMPLISHED INSPECTION OF GIRT BAR FITTING INSTALLATION.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 63,278 hrs · 23,298 cycles

NR 1 ENGINE NON LOCKING REVERSER ACTUATOR ON TOP, OTBD IS LEAKING 60 DROPS PER MINUTE. REMOVED AND INSTALLED NEW ACTUATOR IAW AMM.

Part: WINDOW — FAULTY (COCKPIT) · airframe 62,902 hrs · 23,151 cycles

DUE TO ELECTRICAL ODOR REPORT IN FLT DECK, PLZ CHK FLT DECK WINDOW ANTI-ICING. F-O REPORTED TO LOCAL MECH DURING DEBRIEFING THAT SMELL WAS MORE OBVIOUS IN FWD WINDOW AREA RT CORNER. MECHANICS NOTICED R1 WINDOW J5 TERMINAL LOOSE AND WIRE DISCOLORED NEAR TERMINAL. COULD NOT TORQ THE SCREW. THE REST OF FLT DECK WINDOWS TERMINAL CHECKED OK. R1 WINDOW HEAT DEFERRED PER MEL, R1 WINDOW TO BE REPLACED AT THE END OF FERRY FLT 9920. REPLACED NR 1 RT WINDOW PER MM, EVA UA81266 AND COA 507402. FO WINDOW RPL'D AND PIN & SOC ELECTRICAL CNTN ACP PER UA-EVA-81266.

Part: COMPUTER — FAULTY (ELEVATOR SYS) · airframe 62,383 hrs · 22,970 cycles

AT LOW AIRSPEEDS ELEVATOR FEEL HARD TO PULL BACK YOKE. REPLACED ELEV FEEL COMPUTER IAW MM, LEAK CHECK GOOD.

Part: STRUT — DAMAGED (SPOILER) · airframe 62,134 hrs · 22,885 cycles

SPOILER ISSUE, FLIGHT DIVERTED. THIS SPOILER FLOATING WAS CONFIRMED BY A FURLOUGHED UAL PILOT. FOUND RT STRUT TRUNNION GEAR DOOR MISSING ATTACH HARDWARE ALLOWING AIRFLOW UNDER NR 8 SPOILER. INSTALLED MISSING HARDWARE.

Part: BEARING — OUT OF POSITION (DOOR HINGE) · airframe 62,069 hrs · 22,863 cycles

UNABLE TO CLOSE DOOR 2L. LOWER GATE CONTACTS THRESHOLD. EXCESSIVE FORCE REQUIRED TO CLOSE AND AND LOCK DOOR 2L. FOUND LOWER HINGE BEARING MIGRATED. REPLACED BEARING AND INSTALLED DOOR. INSTALLED GUIDE ARM AND ADJUSTED DOOR.

Part: BOLT — UNSECURE (DOOR) · airframe 61,810 hrs · 22,758 cycles

PASSENGER ENTRY-SERVICE DOORS R FWD EVAC SLIDE ARM LEVER DIFFICULT TO POSITION. FOUND BOLT IN ROD END LOOSE CAUSING GIRT BAR TO BIND. SECURED BOLT. OPS CHECKED REF AMM.

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 61,804 hrs · 22,754 cycles

ELONGATED HOLE ON VERTICAL STAB PANEL 324 GZ. FABRICATED AND INSTALLED NEW DOOR PANEL P/N 172N1500-31 ON PEMCO NR 2529N00495 PER EA PD57-55-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

MAIN CABIN BETWEEN STA 700 - 760, LBL 58, WL 208.1, FLOORBEAM AND SUPPORT STRUCTURE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL FROM STA 680 - 700, STA 700 - 720, LBL 58 ON PEMCO NR 2529N00344 PER EA PD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

CORROSION ON MAIN CABIN FLOORBEAM AT STA 1681.8 RBL 50 UNDER DECK PLATE AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FABBED AND INSTALLED REINFORCING STRAP AND ANGLE STA 1681, RBL 41 - 58 ON PEMCO NR PER EA PD57-53-114.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

DENT ABOVE STR L-19, STA 1620 EXTERIOR. FABRICATED AND INSTALLED DOUBLER AND STRINGER SPLICE ON PEMCO NR #2529N00028 PER EA PD AND EVA 80826.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,804 hrs · 22,754 cycles

DOOR 1 LEFT EXTERNAL SLIDE LIGHT INOPERATIVE. REPLACED L1 DOOR EXTERNAL SLIDE LIGHT. OPS CHECKS GOOD.

Part: DECK PLATE — CORRODED (CABIN) · airframe 61,804 hrs · 22,754 cycles

CORROSION ON MAIN CABIN DECK PLATE STA 1681 - 1720, RBL 40 - RBL 53. MAJOR REPAIR ACCOMPLISHED: REPLACED DOUBLER FROM STA 1681 - 1707, RBL 46 TO OTBD EDGE ON PEMCO NR #2529N00217 PER PEMCO EA PD57-53-111.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,804 hrs · 22,754 cycles

DOOR R2 EXTERNAL SLIDE LIGHT INOPERATIVE. RELAMPED DOOR 2 RT EXTERNAL SLIDE LIGHT IAW B757, OPS CHECKS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

BS 741 BETWEEN STR 13L AND 14L OUT OF TOLERANCE. REPAIRED DURING HMV FOLLOWING INSTRUCTIONS ON EVA 80798 WITHOUT DEVIATION, A INITIAL 8100 WAS CREATED AND ACCEPTED. A NEW 8100-9 SHOWING COMPLIANCE TO CFR 25.571 AND 26.43(D) MUST BE RECEIVED NO LATER THAN APRIL 25 2013 FOR THIS REPAIR TO REMAIN VALID AND AIRCRAFT TO REMAIN AIRWORTHY.

Part: DECK PLATE — CORRODED (CABIN) · airframe 61,804 hrs · 22,754 cycles

CORROSION MAIN CABIN DECK PLATE STA 1681 - 1686, RBL 58 - LBL 30. THIS REPAIR (PEMCO NR #252 9N00230) IS ACCOMPLISHED ON PEMCO NR #2329N00217 (SMC010).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,804 hrs · 22,754 cycles

L1 AND L4 OVERWING EMERGENCY LIGHTS INOPERATIVE. RELAMPED L1 AND L4 OVERWING EMERGENCY LIGHTS. OPS CHECKS GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

DENT 15 INCHES AFT OF MED 2L, 4 INCHES BELOW WINDOW. DENT OUT OF LIMITS DUE TO PROXIMITY OF WINDOW CUTOUT. REPAIRED PER INSTRUCTIONS ON PEMCO PD AND UA EVA 80798.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

CORROSION AT ATTACH GUSSET STA 1681, RBL 33, MAIN CABIN. REMOVED AND REPLACED GUSSET PER SRM.

Part: INTERCOSTAL — CORRODED (STA 1650) · airframe 61,804 hrs · 22,754 cycles

CORROSION ON MAIN CABIN FLOOR INTERCOSTAL AT STA 1650. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

CORROSION ON T-FITTING STA 1720, RBL 53 IN THE MAIN CABIN. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED T-FITTING PER SRM.

Part: CHANNEL — CORRODED (BS 1688-1706) · airframe 61,804 hrs · 22,754 cycles

HAT CHANNEL ON AFT CABIN PRESSURE DECK CORRODED BETWEEN STA 1688 - 1706 ON RT FLANGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED 4 FREEZE PLUGS IN DISCREPANT LOCATIONS PER PEMCO PWI 809UA178, FABBED AND INSTALLED HAT CHANNEL PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,804 hrs · 22,754 cycles

CORROSION AT STA 1640 ON MAIN CABIN FLOORBEAM FROM RBL 54 - RBL 45. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FABRICATED AND INSTALLED T-CHORD AND 2 ANGLES PER SRM.

Part: WINDOW — DAMAGED (L3 DOOR) · airframe 61,454 hrs · 22,612 cycles

F-A REPORTED SCRATCHES IN VIEW INT AT DOOR 3L. REPLACED DOOR MOUNTED WINDOW PER AMM.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 60,768 hrs · 22,356 cycles

BURNING ODOR COMING FROM LIGHT BALLAST ABOVE LAV 136. DISSIPATED WHEN LIGHTS TURNED OFF. TURNED ALL LIGHTS ON, CHECKED PANELS AROUND AFT GALLEY AND LAVS, NO DISCREPANCY FOUND, ALL LIGHTS OPS NORMAL.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 60,639 hrs · 22,306 cycles

MAIN CABIN BS 324 FLOORBEAM T-CAP CORRODED AND MATERIAL REMAINING AFTER BLEND OUT EXCEEDS SRM LIMITS AT RBL 60 AND RBL 24. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF T-CAP AND FABRICATED AND INSTALLED NEW T-CAP AND REPAIR ANGLES AND STRAPS PER PEMCO EA PD57-53-063 AND UAL EVA 80342 ON NON ROUTINE. PER UAL EVA 80342 , A NEW FAA 8100-9 MUST BE ISSUED AND DTA 085625 INCORPORATED IN THE AIRPLANE MAINTENANCE PROGRAM WITHIN 24 MONTHS FROM 22NOV10. THE AIRPLANE WILL BECOME UNAIRWORTHY UNLESS A NEW FAA 8100-9 IS RECEIVED ON OR BEFORE 22NOV12.

Part: BUTTSTRAP — CORRODED (BS 1400 S27-28L) · airframe 60,639 hrs · 22,306 cycles

AFT PIT, BS 1400 BUTT SPLICE STRAP IS CORRODED BTWN STR 27L-STR 28L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF BUTT SPLICE STRAP, (CIRCUMFERENTIAL SKIN SPLICE), AND FABRICATED AND INSTALLED A DOUBLER AND FILLER REPAIR PER PEMCO EA PD57-53 -064 AND UAL EVA 80344 ON NON ROUTINE 2358N00239. PER UAL EVA 80344, A NEW FAA 8100-9 MUST BE ISSUED AND DTA INCORPORATED INTO THE AIRPLANE 085625 MAINTENANCE PROGRAM WITHIN 24 MONTHS FROM 23NOV10. THE AIRPLANE WILL BECOME UNAIRWORTHY UNLESS A NEW FAA 8100-9 IS ISSUED ON OR BEFORE 23NOV12, REF EG DTA LOG 10-123.

Part: SKIN — DAMAGED (BS 564-616) · airframe 60,639 hrs · 22,306 cycles

DURING OVER NIGHT VISIT IN ORD EXISTING SKIN REPAIR AT BS 564 TO BS 616 BTWN STR 28L AND STR 28R WAS REEVALUATED. MAJOR REPAIR ACCOMPLISHED: DUE TO THE PROXIMITY TO THE CARGO DOOR CUTOUT, UA EVA74040 CREATED TO ADDRESS THE REPAIR. THE REPAIR HAS 1ST STAGE APPROVAL (APVL FOR STC STGTH) ONLY, THE COMPLIANCE TO 14CFR25.571 AND 26.43D HAS NOT BEEN EVALUATED. AN FAA FORM 8100-9 FINDING COMPLIANCE WITH 14CFR26 .43D AND 25.571 MST BE ISSUED AND DAMAGE TOLERANCE INF, MUST BE INCORPORATED IN THE APLN MAINTENANCE PGM WTHIN 24 MOS. REMOVED EXISTING REPAIR DOUBLER AND FABRICATED A NEW DOUBLER AND 3 FILLERS AND INSTALLED PER PEMCO EA PD57-53-062 AND UAL EVA 80346 ON NON ROUTINE 2358N00 158.

Part: FLOORBEAM — CORRODED (BS 366.5) · airframe 60,639 hrs · 22,306 cycles

BS 366.5 FLOORBEAM UPPER CAP IS CORRODED AT RBL 3 AND MATERIAL REMAINING AFTER CORROSION REMOVAL EXCEEDS SRM 53-00-51, DETAIL III LIMITS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF T-CAP AND FABRICATED AND INSTALLED NEW CHORD, REPAIR ANGLES AND STRAPS PER SRM REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 60,639 hrs · 22,306 cycles

MAIN CABIN BS 345 FLOORBEAM CORRODED UNDER CLIP NUT AT RBL 12 AND MATERIAL REMAINING AFTER CORROSION REMOVAL EXCEEDS SRM LIMITS. MAJOR REPAIR ACCOMPLISHED: FABRICATED TWO REPAIR ANGLES IAW SRM, NDT INSP OF CUTOUT ACCOMPLISHED WITH NO CRACKS FOUND, ALODINED AND PRIMED REPAIR PARTS IAW SRM AND INSTALLED PARTS.

Part: RADOME — CRACKED (NOSE) · airframe 60,475 hrs · 22,246 cycles

RADOME CRACKED ON OUTSIDE WITH DELAMINATION ON INSIDE MEASURING APPROX 1'X 1 'AND 6"X 6" SEPARATED BY 4". REPLACED CRACKED NOSE RADOME.

Part: COMPUTER — FAULTY (POSITION 1) · airframe 59,848 hrs · 22,009 cycles

YOLK WAS DIFFICULT TO PULL BACK ON ROTATION. ONCE TRIMMED CONTROL FORCE NORMAL. REPLACED ELEVATOR FEEL COMPUTER, OPS CHECK OK.

Part: BATTERY — MALFUNCTIONED (MAIN) · airframe 59,535 hrs · 21,886 cycles

BATTERY CHARGER MAIN MSG APPEARED AFTER PUSHBACK, UNABLE TO CLEAR. REPLACED MAIN BATTERY & CHARGER PER MM.

Part: STOWAGE BOX — FAULTY (COCKPIT) · airframe 59,509 hrs · 21,876 cycles

ABNORMAL OXYGEN REGULATOR OPERATION AT POSITION 2. (1=CAPT, 2=1ST OFF, 3=1ST OBS). REMOVED AND REPLACED F/O CREW OXYGEN MASK STOWAGE BOX. OPERATIONAL CHECK OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,235 hrs · 21,770 cycles

DOOR 2 RT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED, OPERATES NORMAL.

Part: STRUT — CORRODED (MLG) · airframe 58,331 hrs · 21,423 cycles

FOUND CORROSION ON INNER WALL OF OUTER STRUT. NEW OUTER CYLINDER REPLACED, REASSEMBLING GEAR AND ALL COMPONENTS BEFORE INSTALL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,431 hrs · 21,077 cycles

EEL LIGHTING INOP AT ROW 15. REPLACED LAMP STRIP.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 56,827 hrs · 20,845 cycles

AFT CARGO COMPARTMENT FLOOR SIDE STRUCTURE PANEL CORRODED RT SIDE JUST AFT OF DOOR OPENING. LIFTED FLOOR PANEL AND INSPECTED AREA UNDER CORROSION AND FOUND NO EVIDENCE OF FURTHER CORROSION. SECURED FLOOR PANEL AFTER INSPECTION. CORR REMOVED AND NEW 'Z' ANGLE AND CARGO NET FITTING INSTALLED. DAMAGED REPAIRED AT SMB.

Part: LEAD — DAMAGED (CABIN) · airframe 55,147 hrs · 20,197 cycles

EMERGENCY PATH LIGHT AT FWD CLOSET INOP. REPAIRED LEAD, OPS CHECKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 55,147 hrs · 20,197 cycles

EMERGENCY PATH LIGHT AT ROW 23 INOP. INSTALLED NEW POWER SUPPLY M735 AND BATTERY. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,147 hrs · 20,197 cycles

EMERGENCY LIGHT CHARGER M10699 INOP. INSTALLED NEW BATTERY PACK AND CHARGER, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,147 hrs · 20,197 cycles

EMERGENCY PATH LIGHTING INOP FROM ROW 9 TO 13. REPAIRED EMERGENCY ESCAPE PATH LIGHTS BEHIND SEAT ROW 13. OPS CHECK GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 55,147 hrs · 20,197 cycles

EMERGENCY LIGHT BAR INOP AT K LAV. LIGHT BAR DISCONNECTED. CONNECTED LIGHT BAR. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,147 hrs · 20,197 cycles

EMERGENCY AISLE LIGHT INOP ROWS 13R AND 25L. RELAMPED EMERGENCY AISLE LIGHTS AT SEAT ROW 13R AND 25L AND OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,841 hrs · 19,365 cycles

BOTH 2 AND 3 DOOR EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED, ALL LIGHTS WORK AS NORMAL.

Part: SIGN — DISLODGED (EMERGENCY EXIT) · airframe 52,556 hrs · 19,258 cycles

EMERGENCY OVERWING EXIT SIGN FELL OFF RT SIDE. ADJUSTED LATCHING MECHANISM AND REINSTALLED SIGN PLATE.

Part: FEEDER CABLE — SHORTED (EMERGENCY LIGHTS) · airframe 52,388 hrs · 19,202 cycles

MID CABIN FLOOR EMERGENCY ESCAPE PATH LIGHTS INOP AT SEAT ROW 9ABC-13ABC. SUPPLEMENTAL DATA UPDATE CAUSE, JUMPER CABLE AT ROW 13ABC SHORTED. REPLACED JUMPER CABLE ASSY FOR ROW 13 ABC. OPS CHECKED OK.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 51,664 hrs · 18,952 cycles

FLASHLIGHT AT 2L POWER LIGHT INOPERATIVE. BATTERY FAILED. REPLACED FLASHLIGHT BATTERY.

Part: LENS — OUT OF POSITION (CABIN) · airframe 51,637 hrs · 18,940 cycles

EXIT SIGN LENS FELL OFF ROW 16F.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,542 hrs · 18,557 cycles

EXTERIOR EMERGENCY LIGHTS INOP AT DOORS 2R & 4L. 10-11-07 FOUND FUSED LAMPS. REPLACED LAMPS

Part: PROBE — OBSTRUCTED (TAT) · airframe 49,862 hrs · 18,308 cycles

RTFL DUE TO RESTRICTED ENGINE THRUST. [07-31-07] ON CLIMBOUT ENGINES PRODUCED ENOUGH THRUST FOR AN APPROX 1000' PER-MIN CLIMB RATE. TRUE AIR TEMP SHOWING +48C ON UPPER EICAS. SHOULD BE ABOUT 12 DEG-C. TAT PROBE HAD A BIRD STRIKE DURING TAKEOFF AND THE NORMALLY ASPERATED PROBE WAS CLOGGED WITH BIRD REMAINS CAUSING INACCURATE TAT READINGS. REPLACED TAT PROBE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,587 hrs · 18,202 cycles

F/O AISLE LIGHT INOPERATIVE. [06-22-07] RELAMPED OPS CHECK OK.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 49,587 hrs · 18,202 cycles

EEL LIGHTS INOP FROM ROW 30 TO AFT GALLEY. REPLACED INVERTER. OP CHECKS OKAY.

Part: PUMP — MALFUNCTIONED (LT ENGINE) · airframe 49,293 hrs · 18,095 cycles

LANDED UNDER AMBER ALERT DUE TO LOSS OF LEFT ENGINE HYDRAULIC PUMP. [SUP 06-01-07] LT HYD SYSTEM FAILED. REPLACED NR 1 ENGINE DRIVEN HYD PUMP. ALSO REPLACED LT EDP PRESSURE AND CASE DRAIN FILTER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,113 hrs · 18,027 cycles

EMERGENCY EXTERIOR SLIDE LIGHTS INOP AT DOORS 2R, 2L AND 4L. [SUP 05-08-07] RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,113 hrs · 18,027 cycles

EMERGENCY EXIT SIGN ABOVE RIGHT OVERWING EXIT IS INOP. [SUP 4-24-07] REPLACED BATTERY PACK FOR POWER SUPPLY M10568. PCN 563-1188, REF MM-33-51-07-201.

Part: CYLINDER — CORRODED (RT MLG STRUT) · airframe 49,044 hrs · 18,002 cycles

RIGHT MLG STRUT OUTER CYLINDER HAS CORROSION IN THE GLAND NUT THREAD AREA & IN THE GROOVE ABOVE THE THREADS 6 INCHES LONG ON THE FORWARD SIDE. [06-20-07] REMOVED RT MLG OUTER STRUT CYLINDER PER SFO GEAR SHOP, AND ROUTED TO GEAR SHOP FOR EVALUATION.

Part: SKIN — DENTED (BS 585) · airframe 47,520 hrs · 17,436 cycles

HORIZONTAL SCRAPES AND DENT ACROSS BOTTOM OF FUSELAGE AT STA 585 MEASURES 18 IN BY 5 IN BY .250 IN DEEP. INCLUDES DAMAGE FROM STA 564 TO STA 616. EXTENDS 3 INCHES ABOVE RADIO ANTENNA LT AND RT SIDES. FUSELAGE SKIN AND STRINGER DAMAGE UNDER FWD CARGO PIT. NO CRACKS OR HOLES IN FUSELAGE. THIS INCLUDES DAMAGE IN SMC001 AND SMC003. DOUBLER STA 564 TO STA 616. EXTENDS 3 IN ABOVE RADIO ANT. DAMAGE CONSISTS OF 2 AREAS DENT-GOUGED & 2-3 STRINGERS DENTED. CUT OUT ALL DAMAGE, HFEC INSP COMFIRM DAMAGE REMOVED. INSTALLED FILLERS AND DOUBLER REPAIR

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 45,771 hrs · 16,796 cycles

FOUND EMERGENCY HATCH HANDLE LIGHT AFT LAMP INOP AT SEAT 15F & 16F.

Part: SCREW — LOOSE (L2 GIRTBAR) · airframe 39,976 hrs · 14,677 cycles

DOOR 2L GIRT BAR LIGHT DOES NOT ILLUMINATE WITH DOOR CLOSED AND ARMED. MOUNTING SCREW FOR FLOOR ATTACH FITTING WAS BACKED OUT AND DID NOT ALLOW GIRT BAR TO ENGAGE FLOOR FITTING. SCREW WAS SECURED AND DOOR ARMS NORMALLY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,937 hrs · 14,660 cycles

CABIN FLOORBEAM AT FS 365 RBL 10 TO RBL 15 CORRODED. FABRICATED & INSTALLED NEW WEB AND ANGLE REPAIRS.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 39,937 hrs · 14,660 cycles

AFT CABIN PRESS DECK HAT CHANNEL STA 1715 TO 1730 IS CORRODED. FABRICATED & INSTALLED NEW HAT CHANNEL.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,773 hrs · 13,886 cycles

FUSELAGE RIGHT SIDE LOWER SKIN DENTED AND CREASED BS 215, STR 26R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR.

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE) · airframe 31,019 hrs · 11,372 cycles

NR 2 ENGINE FAILED TENTH STAGE BORESCOPE INSPECTION.

Part: ENGINE — FAILED (LEFT)

DURING DESCENT FROM 10,000 FT, LEFT ENGINE WENT TO 3.2 VIBES ON DESCENT. DURING SHUTDOWN MADE MOANING NOISE AND VIBRATION FELT THROUGH AIRFRAME. ENGINE SUFFERED A FAILURE OF A HPT 2ND STAGE BLADE. THE ENGINE WAS REPLACED.

Part: TRANSDUCER — SHORTED (ANTISKID SYS)

DIVERTED TO LAX DUE TO ANTI-SKID INDICATION. *S/D* NR 1 ANTISKID TRANSDUCER FAILED. REPLACED TRANSDUCER.

Part: UNION — FACTURED (NR 1 EDP)

LANDED SFO UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. *S/D* FOUND PRESSURE LINE UNION FITTING ON NR 1 EDP PRESSURE AND CASE DRAIN FILTER ASSY BROKEN. REPLACED UNION AND FILTERS, CHECKED ACMP AND EDPM FILTER FOR CONTAMINATION AND NONE WAS FOUND. ALSO, SYS CASE DRAIN FILTER CHECKED AND NO CONTAMINATION FOUND.

Part: AIRSPEED IND — FAILED (LT COCKPIT)

ABORTED TAKEOFF WHEN CAPTAIN'S AIRSPEED INDICATOR SHOWED ZERO. *S/D* DEFECTIVE AIRSPEED INDICATOR, REPLACED SAME.

Part: LIGHT STRIP — DISCONNECTED (CABIN)

EMERGENCY LIGHT STRIP INOP AT 13A. DISCOVERED EMERGENCY LIGHT STRIP DISCONNECTED. RECONNECTED, TESTS NORMAL.