N570UA

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 66,502 hrs · 24,391 cycles

DOOR 4L WILL NOT ARM. REMOVED ICE FROM GIRT BAR AND UPPER DOOR HINGE & APPLIED ICE RELEASE.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW O2) · airframe 66,353 hrs · 24,344 cycles

CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 TO LIMITS AS PER AMM. BEFORE SERV 1200 PSI. AFTER SERV 1500 PSI.

Part: COVER — LOOSE (CABIN) · airframe 66,041 hrs · 24,227 cycles

EMERGENCY EXIT LIGHT STRIP LOOSE AT ROW 12. REPLACED SECTION OF PLASTIC CLEAR COVER ON EEL STRIP.

Part: BLOCK — OUT OF ADJUST (SLIDING WINDOW) · airframe 65,993 hrs · 24,213 cycles

CAN'T LOCK F/O COCKPIT SLIDING WINDOW. ADJUSTED CAM BLOCK UPPER AFT CORNER IAW MM BECAUSE AFT UPPER CORNER OF WINDOW NEEDED TO BE POSITIONED OUTBOARD .1 OF A INCH.

Part: COOLING FAN — FAULTY (E&E BAY) · airframe 65,984 hrs · 24,211 cycles

SLIGHT ELEC BURNING SMELL TAXI IN THEN EQUIP CLG OVERHEAT AFTER ENGINE SHUT DOWN. FOUND CB FOR FWD EQ COOLING FAN NR 1 OPEN. REPLACED FAN PER MM, OPS CHECK NORMAL. NO FURTHER DAMAGE FOUND.

Part: SLIDE — DEPLOYED (L2 DOOR) · airframe 24,036 hrs · 65,500 cycles

AT DEPARTURE TIME, DOOR 2L SLIDE DEPLOYED BY CREW. REMOVED AND REPLACED SLIDE AND ASSIST BOTTLE ASSY IAW AMM.

Part: JAM-NUT — BINDING (COCKPIT WINDOW) · airframe 65,405 hrs · 24,008 cycles

REPEAT WRITE UP. CAPT'S WINDOW BINDING WON`T UNLOCK AFTER PRESSURE CYCLE. CHECK CAPTS SLIDING WINDOW PER AMM. FOUND LOWER AFT LINK ARM JAM NUT NOT TIGHT. CHECKED ADJUSTMENT AND TIGHTENED JAM NUT. PRESSURIZED AIRCRAFT. AFTER DEPRESSURZING OPERATED WINDOW LATCH HANDLE. OPS CHECKED GOOD. ALSO LUBED TRACK AREA. OK TO CONTINUE.

Part: CONTACT — DIRTY (SWITCH) · airframe 65,325 hrs · 23,984 cycles

ENGINE BOTTLE 1 DISCHARGE LIGHT INOPERATIVE. TROUBLESHOT PANEL LIGHT SWITCH BY SWAPPING WITH RIGHT SWITCH NEEDS NEW ENGINE FIRE PANEL. CLEANED CONTACTS AND HOUSING ASSY FOR ENGINE BOTTLE 1 DISCHARGE SWITCH LIGHT. OP'S CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (FUEL TRANSFER) · airframe 64,681 hrs · 23,767 cycles

FUEL TRANSFER FROM RT WING TO CENTER TANK AT CRUISE, WENT FROM 14.5-0-14.5 AT TOP OF CLIMB. ACCOMPLISHED BITE OF FQIS. NO FAULTS FOUND. SELF TEST GOOD. ALL THREE TANKS DRIPPED AND FOUND WITHIN TOLERANCE PER MM.

Part: INDICATOR — TRIPPED (TE FLAPS) · airframe 64,674 hrs · 23,764 cycles

SLOWING FOR APPROACH, RECEIVED TRAILING EDGE FLAP DISAGREE EICAS. SUPPLEMENTAL DATA UPDATE, FLAPS LOCKED AT 21 WHEN FLAP. HANDLE WAS MOVED TO 25, RAN QRH CHECKLIST TO SUCCESS. ACCOMPLISHED INSPECTION OF FLAP OVER LOAD INDICATORS, FOUND NR 1 INDICATOR POPPED. RESET CYCLED FLAPS, ALL CHECKED GOOD. ALSO, ACCOMPLISHED FSEU CHECK. NO FAULTS FOUND.

Part: COMPRESSOR — FAULTY (POTABLE WATER) · airframe 63,795 hrs · 23,448 cycles

AFTER CLIMBOUT CREW STATED NO WATER FROM THE LAV FAUCETS AND HAD VIBRATION. CREW REPORTS POTABLE WATER SYSTEM DRAINED TO EMPTY IN FLIGHT. FOUND LARGE BLOCK OF ICE AT WATER SERVICE PNL. SUSPECT OVERHEAT OF WATER HEATERS AND WATER COMPRESSOR BASED ON CREW COMMENTS. REPLACED WATER COMPRESSOR, OP CHECKS NORMAL.

Part: ACTUATOR — UNRELIABLE (ELEVATOR ASYM) · airframe 63,685 hrs · 23,405 cycles

DUE TO RECENT RELIABILITY ISSUES REPLACED THE ELEVATOR ASYMMETRY LIMITER ACTUATOR.

Part: STOP FITTING — GOUGED (FUSELAGE) · airframe 63,525 hrs · 23,343 cycles

FWD CARGO PIT AFT 2ND FROM THE BOTTOM STOP FITTING HAS A DEEP GOUGE. REPLACED REF IPC53-63-51- 010.

Part: MODULE — FAULTY (FIRE WARNING) · airframe 62,923 hrs · 23,127 cycles

FIRE SYS FAIL LIGHT INOPERATIVE. REPLACED M10445 S2 FAIL LIGHT ANNUNCIATOR AND ACP'D OPERATIONAL TEST OF ENGINE FIRE AND OVERHEAT DETECTION SYSTEM PER MM, CHECKS OKAY.

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 62,432 hrs · 22,940 cycles

FIRST OFFICERS WINDSHIELD CONNECTOR J1 DOES NOT SIT PARALLEL TO TERMINAL. REPLACED F/O NR 1 WINDSHIELD.

Part: TURBINE — OVERTEMP (NR 2 ENGINE) · airframe 62,181 hrs · 22,848 cycles

NR 2 ENG EGT EXCEEDED 645 DEGREES, NOT DURING SURGE. PEAK EGT WAS 656. FOUND EGT EXCEEDENCE NR 2 ENG. EGT RED 656 FOR :29SEC EGT REDLINE 640 FOR :28.8SEC 615 FOR : 28.8SEC MAX 656. CHECKED PER JRH2-5-62 AREA B NR 1-4, PERFORMED VISUAL WITH NO DAMAGE NOTED. CONTACTED ENGINE CNTRLR. DEFERED OVERTEMP HOT SECTION INSPECTION REF(MM72-00-00) SEE WRITEUP FOR DEFERAL. REPLACED NR 2 ENG.

Part: GIRT BAR — LACK OF LUBE (R1 DOOR SLIDE) · airframe 61,941 hrs · 22,758 cycles

DOOR 1R SLIDE ARMING LEVER STIFF BUT FUNCTIONAL. ACCOMPLISHED CHECK OF GIRT BAR MECHANISM, OP CHECKS GOOD. ACCOMPLISHED LUBE OF GIRT BAR FITTINGS. INSTALLED BUSSLE.

Part: ANGLE — CRACKED (BS 1180) · airframe 61,638 hrs · 22,642 cycles

EXTERNAL FUSELAGE ANGLE AT BS 1180 COMMON TO BODY FAIRING FRAME AT LBL 11 HAS A 1 INCH CRACK IN ANGLE RADIUS. MAJOR REPAIR ACCOMPLISHED OF FUSELAGE FAIRING SUPPORT ANGLE AT BS 1180 BETWEEN STRINGER 27L & 29L IAW EA PD57-53-138 AND EVA 80917 WITHOUT DEVIATION. DTA TRACKING UNDER CF9046.

Part: CREASE BEAM — CORRODED (BS 1050) · airframe 61,638 hrs · 22,642 cycles

CORROSION AROUND FASTENER ON CREASE BEAM AT RT STA 1050. COMPLETED REPAIR IAW EA PD 57-53-129.

Part: CREASE BEAM — CORRODED (BS 1166) · airframe 61,638 hrs · 22,642 cycles

CORROSION AROUND FASTENERS ON CREASE BEAM AT RT FS 1166. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL FOUND OUT OF LIMITS PER SRM. FABRICATED REPAIR PER INSTRUCTIONS ON EA PD 57-53-131 WITHOUT DEVIATION. THIS IS A PERMANENT REPAIR WITH FAA 8100-9 DATED MAY 31ST 2011.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · airframe 61,638 hrs · 22,642 cycles

CORROSION ON CREASE BEAM WEB INNER CHORD FROM RT FS 1020-1040 MAIN CABIN. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPAIR CHORD, SPLICE CHANNEL AND STRAP PER EA 57- 53-130.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · airframe 61,638 hrs · 22,642 cycles

CORROSION ON CREASE BEAM WEB INNER CHORD FROM RT FS 1020-1040 MAIN CABIN. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR CHORD, SPLICE CHANNEL AND STRAP BTW STA 1011 - 1040, RBL 58 PER EA 57- 53-130 ON NR 2647N00406.

Part: STRAP — FRAYED (EVAC SLIDE) · airframe 61,638 hrs · 22,642 cycles

DOOR 1L ESCAPE SLIDE HARNESS HAS A FRAYED STRAP. REPLACED THE L1 DOOR ESCAPE SLIDE HARNESS STRAP PER MM AND INSPECTED.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,638 hrs · 22,642 cycles

CORROSION AROUND FASTENER HOLES ON INNER CHORD OF CUSP WEB AT LT FS 1015 TO 1025 LBL68. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED INNER CHORD, SPLICE CHANNEL AND STRAP BTW STA 1011 - 1040, LBL 68 PER PEMCO EA PD57-53-133 ON PEMCO NR 2647N00404.

Part: FRAME — GOUGED (BS 1640 S6 & 8L) · airframe 61,638 hrs · 22,642 cycles

FRAME IS GOUGED AT STA 1640 STR 6L AND 8L INSIDE THE CABIN. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED: INSTALLED T-CLIP, REPAIR ANGLE, STRAP AND ATTACH ANGLE PER PEMCO EA PD57-53-128 AND UA EVA 80905 ON PEMCO NR 2647N00426. BS 1640 FRM REPAIR MUST RECEIVE A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 AND 26.43(D) AND THE DTI INCORPORATED IN THE ACFT MAINTENANCE PROGRAM MUST BE ISSUED WITHIN 24 MOS FROM 01 JUN 11 FOR THIS REPAIR APPROVAL TO REMAIN VALID AFTER 01 JUN 13. IF A NEW 8100-9 APPROVAL IS NOT OBTAINED ON OR BEFORE 01 JUN 13, THE ACFT BECOMES UNAIRWORTHY.

Part: FRAME — GOUGED (BS 1640 S6 & 8L) · airframe 61,638 hrs · 22,642 cycles

FRAME IS GOUGED AT STA 1640 STR 6L AND 8L INSIDE THE CABIN. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED: INSTALLED T-CLIP, REPAIR ANGLE, STRAP AND ATTACH ANGLE PER PEMCO EA PD57-53-128 AND UA EVA 80905 ON PEMCO NR 2647N00426.

Part: FRAME — GOUGED (BS 1640 S6-8L) · airframe 61,638 hrs · 22,642 cycles

FRAME IS GOUGED AT STA 1640 STR 6L AND 8L INSIDE THE CABIN. MAJOR REPAIR ACCOMPLISHED: INSTALLED T-CLIP, REPAIR ANGLE, STRAP AND ATTACH ANGLE PER PEMCO EA PD57-53-128 AND UA EVA 80905 ON PEMCO NR 2647N00426 BY TECH P531, INSP Q873. BS 1640 FRM REPAIR MUST RECEIVE A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 AND 26.43(D) AND THE DTI INCORPORATED IN THE ACFT MAINTENANCE PROGRAM MUST BE ISSUED WITHIN 24 MOS FROM 01 JUN 11 FOR THIS REPAIR APPROVAL TO REMAIN VALID AFTER 01 JUN 13. IF A NEW 8100-9 APPROVAL IS NOT OBTAINED ON OR BEFORE 01 JUN 13, THE ACFT BECOMES UNAIRWORTHY.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 61,638 hrs · 22,642 cycles

FWD ENTRY STA 324 FLOORBEAM CORROSION RBL 48-64. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED T CHORD PER INSTRUCTIONS ON PD 57-53-127 &D UA EVA 80888 WITHOUT DEVIATION. ALSO CREATED CF9042 FOR DTA REQUIREMENT.

Part: FLOORBEAM — CORRODED (STA 365 RBL 60) · airframe 61,638 hrs · 22,642 cycles

FWD ENTRY STA 365 RBL 60 FLOORBEAM CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION PER MM AND FOUND TO BE OUT OF LIMITS PER SRM. CUT OFF LBL 19 TO OUTBD RT, REPLACED UPPER FLOORBEAM CHORD PER SRM WITH BAC1505-100880. ALSO, REPLACED 2 ATTACH ANGLES AND 2 STRAPS. TREATED AND PRIMED PER AMM. INSTALLED ALL PARTS PER SRM.

Part: SKIN — DENTED (HORIZ STAB) · airframe 61,638 hrs · 22,642 cycles

LEFT UPPER SKIN OF HORIZONTAL STAB HAS DENT AT HSBL 18 AT HORIZONTAL STATION 50. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW B757 SRM. INSTALLED DOUBLER REPAIR OUT OF 7075-T6 .032 IAW B757 SRM. RESTORED FINISH IAW B757 AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,638 hrs · 22,642 cycles

CORROSION UNDER FLOORBEAM AROUND SCREW HOLE STA 377 LBL 50. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED FLOORBEAM FROM STA 377 LBL 37 TO LBL 64 PER SRM, FABRICATED REPAIR FLOOR BEAM AND ANGLES PER SRM, LOCATED AND DRILLED NEW REPAIR FLOORBEAM IAW SRM. INSTALLED ALL PRIMED AND TREATED PARTS IAW B757 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,638 hrs · 22,642 cycles

CORROSION ON FLOORBEAM TOP STA 661 RBL 57. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL FOUND TO BE OUT OF LIMITS IAW B757 SRM. FABRICATED NEW T-CHORD PER SRM, TREATED AND PRIMED NEW CHORD, STRAPS AND ANGLES IAW 757 AMM. INSTALLED ALL ANGLE AND STRAPS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,638 hrs · 22,642 cycles

CORROSION ON FLOORBEAM TOP STA 1640 RBL 23-58. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED PORTION OF T-CHORD AT STA 1640 LBL 9 TO RBL 67 IAW SRM. FABRICATED REPAIR ANGLES AND STRAPS IAW SRM 53-00-51 REPAIR NR 3. INSTALLED NEW T-CHORD P/N BAC1505-100880 PER SRM. TOP COATED AND PRIMED PER MM.

Part: SUPPORT — CORRODED (BS 1700) · airframe 61,253 hrs · 22,505 cycles

AFT CARGO COMPARTMENT LAVS, DUMP CHUTE SUPPORT STRUCTURE - LAV PAN AND SURROUNDING SKIN CORRODED AT BS 170 0, BETWEEN STR 27R-STR 29. REMOVED DAMAGED LAV PAN AND ADJACENT SKIN AREA, REPAIRED WITH NEW REPLACEMENT LAV PAN, PN 146N3650-64 AND EXTERNAL SKIN DOUBLER AND STRUCTURAL FILLER PER REO G13580, REV B ON NON ROUTINE 43771. PER EVA 80664.

Part: SHAFT — DAMAGED (PAX DOOR HANDLE) · airframe 61,253 hrs · 22,505 cycles

R-1 DOOR EXTERIOR HANDLES DO NOT STOW WITH DOOR OPEN. DISASSEMBLED EXTERIOR HANDLE MECHANISM AND INSPECTED PARTS. REPLACED THE CENTER SHAFT ASSY, CENTER SHAFT O-RING, COLLAR CLUTCH ASSY, INNER SHAFT ASSY AND BUTTERFLY HANDLE BEARING. OPS CHECKED GOOD.

Part: SHEAR TIE — CORRODED (BS 1700 S28L) · airframe 61,253 hrs · 22,505 cycles

AREA AFT OF BULK CARGO COMPARTMENT, SHEAR TIE CORRODED BETWEEN STR 28L AT BS 1700. MAJOR REPAIR ACCOMPLISHED: REMOVED CORRODED SHEAR TIE AND FABRICATED A NEW SHEAR TIE, -328 IAW DWG 140N2002 AND INSTALLED IAW SRM.

Part: HANDLE — FAULTY (L1 DOOR) · airframe 61,253 hrs · 22,505 cycles

L1 DOOR EXTERIOR BUTTERFLY HANDLE DOES NOT FULLY RETRACT INTO THE DOOR RECESS. SUPPLEMENTAL DATA UPDATE DISASSEMBLED EXTERIOR HANDLE AND BASKET CAM ASSY. REPLACED EXTERNAL HANDLE YOKE ASSY, P-N 140N2669-2, PER CMM. LUBED AND REINSTALLED DOOR EXTERIOR HANDLE ASSY AND OPS CHECK GOOD PER CMM.

Part: SHEAR TIE — CORRODED (BS 1460 S28-29L) · airframe 61,253 hrs · 22,505 cycles

SHEAR TIE CORRODED AT STA 1460 BETWEEN STR 29L TO 28L. MAJOR REPAIR ACCOMPLISHED: REMOVED SHEAR TIE AND FABRICATED A NEW SHEAR TIE PER BACO DWG 140N2002, REV. EU AND INSTALLED PER SRM.

Part: VALVE — BROKEN (OXYGEN BOTTLE) · airframe 61,253 hrs · 22,505 cycles

CREW O2 BOTTLE SHUTOFF VALVE KNOB IS BROKEN OFF. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED CREW O2 BOTTLE PER MM AND LEAK CHECK GOOD ON NON ROUTINE 43489 AND INSP QC384.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 61,253 hrs · 22,505 cycles

RT HORIZ STAB OTBD LWR LEADING EDGE SKIN DENTED 2 PLACES. INSTALLED LAY-UP REPAIRSPR'S PER SRM. REINSTALLED LEADING EDGE PER SRM.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 60,528 hrs · 22,221 cycles

FLOOR EMERGENCY LIGHT STRIP NOT LIGHTING FROM ROW 23 THRU 31. REPLACED POWER SUPPLY BATTERY AND CHARGER AT M735, TESTS OK.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 60,528 hrs · 22,221 cycles

EMERGENCY LIGHTS IN OVERHEAD BIN AREA NOT LIGHTING BY SEATS 20D, 24D, 21C. REPLACED M735 POWER SUPPLY.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,528 hrs · 22,221 cycles

EMERGENCY LIGHTING FLOOR STRIP AT "K" LAV INOP. SPLICED RIBBON NEW CABLE TO ATTACH TO POWER STRIP.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 60,229 hrs · 22,101 cycles

RUDDER TRIM STOPPED WORKING DURING APPROACH. PHASE (RT AND LT). WORKS NOW ON GROUND. REPLACED THE RUDDER TRIM ACTUATOR IAW MM. (RUDDER TRIM INTERMITTENT OPERATION). REPLACED THE RUDDER TRIM ACTUATOR.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 59,924 hrs · 21,993 cycles

DOME LIGHT WOULD NOT ILLUMINATE USING DOME LIGTH SWITCH OR WITH LIGHT OVERHEAD SWITCH ON. DOME LIGHT 3 LIGHTS BLOWS WHEN SWITCH IS TURNED ON LIGHT SHORTED NEED TO GET BEHIND LIGHT COVER ON SCREW STRIPPED NEED MORE TIME TO FIND SHORT. MECHANIC REPORTS THAT EMERGENCY LIGHT IN THIS DOME LIGHT ASSY ALSO DOES NOT WORK. RELAMPED DOME LIGHT WITH PROPER LAMP. CK GOOD. EMERGENCY LIGHT, FOUND WEAK GROUND AT LIGHT ASSY. RESEATED CONNECTOR D41280P. GRND NOW NORMAL. EMERGENCY LIGHT NOW OPS NORMAL.

Part: STRUCTURE — DAMAGED (BS 560-620) · airframe 59,733 hrs · 21,921 cycles

DAMAGE UNDER FWD C-DOOR. ACCOMPLISHED HFEC NDT TO DAMAGE CUTOUTS BETWEEN STA 560 AND 620 AROUND AREAS OF STRINGERS 28 AND 28R ACCOMPLISHED HFEC NDT PER 757 NDT PART 6 51-00-01. NO CRACK NOTED. MANUFACTURED REPAIR FOR DAMAGED AREA BETWEEN STA 600-620 AREA AND INSTALLED PER EVA 80039.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 59,580 hrs · 21,864 cycles

EMERGENCY FLOOR LIGHT STRIP INOP AT AFT FWD LAV DOOR. FOUND FLOOR LIGHT STRIP CONNECTOR OFF, SECURED CHECKS OK.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 56,000 hrs · 20,510 cycles

RIGHT INBOARD FLAP OUTBOARD AFT FAIRING IS DELAMINATED. FLAP REMOVED & SENT TO SHOP 273 FOR REPAIR. REPLACED RT TRAILING EDGE FLAP. CREW COMMENTS: GOOD TEST FLIGHT FOR FLAP REPLACEMENT.

Part: ENGINE — FIRE (RIGHT) · airframe 56,000 hrs · 20,510 cycles

TAILPIPE FIRE RIGHT ENGINE ON START. FLAP, CANOES, WING PANEL FIRE DAMAGE. NR 2 ENGINE REMOVED AND SENT TO SFO TEST CELL FOR EVALUATION. REPLACED NR 2 ENGINE.

Part: SKID SHOE — DAMAGED (LT WING SLAT) · airframe 53,865 hrs · 19,668 cycles

LEFT WING, AFT OF NR 3 LEADING EDGE SLAT ON TOP OF WING, A PREVIOUS OVERLAY REPAIR IS PEELING UP. AREA 2 BY 9 INCHES. DAMAGE BETWEEN LEADING EDGE SLAT AND FWD WING SPAR. PREVIOUS HOT BOND REPAIR ON NR 3 L/E SLAT IS SEPARATING. REMOVED DAMAGED MATERIAL FROM SLAT. NEW CORE MATERIAL CUT AND READY TO POT IN. FITTED HONEYCOMB FILLER MATERIAL. COMPLETED REPAIR IAW 51-70-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,627 hrs · 19,585 cycles

EEL LIGHT INOP AT 'K' LAV. FOUND BULB INOP. REPLACED FLOOR MOUNTED LAMP.

Part: SLIDE — LEAKING (L1 DOOR) · airframe 53,301 hrs · 19,468 cycles

DOOR 1L SLIDE PRESSURE LOW. *S/D* UNKNOWN LEAK. REPLACED SLIDE ASSY.

Part: OXYGEN MASK — DAMAGED (CAPTAIN'S) · airframe 53,171 hrs · 19,422 cycles

MIC ON CAPT O2 MASK HAS FRAYED WIRE. NEEDS TO BE REPLACED. *S/D* REPLACED CAPT O2 MASK ASSY, OPS CHECKED GOOD.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 52,452 hrs · 19,181 cycles

1L SLIDE PRESS IS IN THE RED. REPLACED SLIDE PACK.

Part: SKIN — DAMAGED (BS 641) · airframe 52,249 hrs · 19,107 cycles

DAMAGE FOUND ON CROWN AREA OF FUSELAGE ON RT SIDE AT STA 641 AND ONE INCH RT OF STRINGER S3R. REMOVED DAMAGE AREA THAT WAS OUT OF LIMITS. EDDY CURRENT ACP NO CRACKS NOTED. REPAIRED WITH SOLID FASTENER PER SRM 53-00-01 REPAIR 6 115824 THIS IS A PERMANENT REPAIR. DEEPEST PART OF DENT WAS REMOVED WITH REMOVAL OF GOUGE. NEW DENT MEASUREMENTS WITHIN LIMITS.

Part: BULB — INOPERATIVE (EMEGENCY LIGHTS) · airframe 51,775 hrs · 18,943 cycles

DOOR 2 LEFT EXTERIOR EMERGENCY LIGHT IS INOP. FOUND BULB OUT. RELAMPED BULB, OPS CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,281 hrs · 18,755 cycles

EXTERIOR EMERGENCY LIGHTS AT DOOR 3L AND RIGHT FWD OVERWING ARE INOP. FOUND LAMPS WERE FAULTY. RELAMPED DOOR 3L AND RT FWD OW EXIT SIGNS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 50,848 hrs · 18,593 cycles

RIGHT FWD OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — VIBRATES (FLAP HANDLE) · airframe 50,656 hrs · 18,517 cycles

AT FLAPS 1 HANDLE IN DETENT ON CLIMBOUT LOUD VIBRATION FELT AND HEARD IN FLAP HANDLE.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 50,652 hrs · 18,514 cycles

RT RVSM AREA: PORTION OF PREVIOUS DOUBLER REPAIR (APPROX 6IN SQUARE) EXTENDS INTO RVSM AREA APPROX 1.5 INCHES. MAJOR REPAIR ACCOMPLISHED: DOUBLER REPAIR INSTALLED.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 50,375 hrs · 18,408 cycles

SLIDE LIGHT INOP AT DOOR 2R. AFT OVERWING SLIDE LIGHT INOP ON RIGHT SIDE OF AIRCRAFT. RELAMPED SLIDE LIGHT.

Part: LIGHT — MISLOCATED (CABIN) · airframe 50,375 hrs · 18,408 cycles

EMERGENCY AISLE LIGHT LOCATED AT SEAT 2B IS IN WRONG LOCATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,375 hrs · 18,408 cycles

EEL LIGHT AT MID LAV INOP AND CARPETED OVER.

Part: DISK — RUPTURED (DOOR SLIDE) · airframe 50,190 hrs · 18,346 cycles

LOW BOTTLE PRESSURE. FOUND RUPTURE DISC LEAKING. REPLACED RUPTURE DISK.

Part: WARNING LIGHT — ILLUMINATED (APU EXTINGUISHER) · airframe 50,268 hrs · 18,369 cycles

APU BOTTLE DISCHARGE LIGHT IS ILLUMINATED. ACCOMPLISHED TROUBLESHOOTING ON ONE OF THE THREE LARGE CONNECTORS AFT LEFT SIDE OF GEAR TO CHECK FOR ANY SHORTING OF PIN 2-3; RECHECKED VOLTAGE AT SQUIB ON APU BOTTLE. THE PROGNOSIS IS ON A BAD CONNECTOR WITH A BAD PIN-SOCKET. REPLACED CONNECTOR AND CHECKED VOLTAGE AT THE CONNECTOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,894 hrs · 18,234 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 2R AND RT AFT OVERWING. [07-27-07] RELAMPED.

Part: GENERATOR — MALFUNCTIONED · airframe 49,608 hrs · 18,132 cycles

CREW REPORT: RIGHT GENERATOR TRIPPED IN DESCENT WHEN GEN DRIVE LIGHT FLASHED. [08-07-07] ACCOMPLISHED RECHECK FOUND RT IDG TOOK 90 PUMPS OR 4 PINTS TO FULL, AND FOUND OIL LEAK SIX DROPS PER MIN FROM FUEL OIL COOLER BY PASS VALVE DRAIN LINE. REPLACED FUEL OIL HEAT EXCHANGER BY-PASS VALVE AND IDG.

Part: ENGINE — ODOR (COCKPIT) · airframe 49,328 hrs · 18,027 cycles

ODOR OF OIL IN COCKPIT AFTER TAKEOFF. ODOR DISSIPATED AFTER SEVERAL MINUTES. [SUP 06-06-07] ACCOMPLISHED TROUBLE SHOOTING, REPLACED RECIRCULATION FILTERS (LT,RT). RAN ENGINES AND APU WITH PACKS ON, FOUND WHAT APPEARED TO BE OIL RESIDUE ALONG INNER DIAMATER OF NR 3 BEARING COMPARTMENT HUB AREA. OIL ODOR IN COCKPIT ON TAKE OFF. ODOR CAME DURING APPLICATION OF T.O. PWR UP TO ABOUT 5,000 AGL. SUSPECT NR 1 ENGINE CAUSE OF SMELL . BOROSCOPE NR 3 BRG COMPARTMENT FOR ANY EVIDENCE OF OIL. NR 1 ENGINE 4 FAN BLADES HAVE NICKS BLADES HAVE NUMBERS 28,17,18, 26. BLENDED BLADES PER UA SPECS. REPLACED NR 1 ENGINE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 48,317 hrs · 17,664 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY AND SEAL. OPS OK

Part: SENSOR — INOPERATIVE (RT PACK TEMP) · airframe 48,235 hrs · 17,626 cycles

RTFL DUE TO A FLIGHT DECK TEMPERATURE CONTROL PROBLEM. LEFT PACK WAS FOUND INOP. CREW TOOK SNAPSHOT FOR MAINTENANCE TRIED USING LEFT BLEED TO RIGHT PACK TO ISOLATE IF BLEED TEMP WAS CAUSE. REPLACED RT PACK TEMP SENSOR.

Part: GENERATOR — FAILED (ENGINE) · airframe 47,208 hrs · 17,217 cycles

DIVERTED TO MCI DUE TO LOSS OF SECOND ENGINE GENERATOR. TROUBLESHOOT IDG FAILURES. CHECKED BPCU FOR FAULTS AND IDG OIL SVC. BPCU BITE INDICATES LT IDG SYSTEM OK. RT IDG HAD FAULTS OF HIGH RISE TEMP, UNDER FREQ TRIP, AND PMG WIRING FAILED. RT IDG TRIPPED OFF AND WILL NOT RESET . REPLACED NR 2 IDG.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,254 hrs · 14,666 cycles

AFT PIT STA 1400, FRAME LT SIDE AT STR 27L IS DENTED. INSTALLED J-ANGLE DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,254 hrs · 14,666 cycles

AFT PIT STA 1440 FRAME LT SIDE AT STR 27L IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 40,254 hrs · 14,666 cycles

FLOOR SUPPORT AT STATION 1708 TO 1720 AND AT STR 14L TO 16L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (AFT CARGO PIT) · airframe 40,254 hrs · 14,666 cycles

AFT CARGO PIT STA 1420 FRAME DENTED ON UPPER FLANGE BY STR 26L. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE DOUBLER REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,254 hrs · 14,666 cycles

CABIN CREASE BEAM SHEAR WEB AT RBL 70.5 FROM STA 960 TO 984 CORRODED. FABRICATED NEW SHEAR WEB.

Part: SHEAR WEB — CORRODED (CREASE BEAM) · airframe 40,254 hrs · 14,666 cycles

CABIN CREASE BEAM SHEAR WEB AT LBL 70.5 FROM STA 960 TO 984 IS CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,254 hrs · 14,666 cycles

MAIN CABIN BODY STATION 680 TO 740 LBL 63 FLOOR CREASE BEAM HAS SEVERAL AREAS OF CORROSION. REPLACED CREASE BEAM.

Part: SHEAR WEB — CORRODED (FUSLAGE) · airframe 40,254 hrs · 14,666 cycles

MAIN CABIN FLOOR STA 1681.8 SHEAR WEB CORRODED. FABRICATED & INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,254 hrs · 14,666 cycles

CABIN FLOORBEAM AT STA 325 BETWEEN RBL 44 AND RBL 58 CORRODED ON TOP CAP OF BEAM. FABRICATED & INSTALLED DOUBLER REPAIR. FABRICATED & INSTALLED ANGLE REPAIR DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,254 hrs · 14,666 cycles

MAIN CABIN FLOORBEAM AT STA 1640 RBL 58 TOP RAIL CORRODED. FABRICATED & INSTALLED NESTED ANGLE REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,915 hrs · 13,093 cycles

FUSELAGE DENT NEXT TO DOUBLER AT FWD LOWER CORNER OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REMOVED & REPAIRED.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 38,303 hrs · 13,981 cycles

STRINGER 16L HAS DAMAGE AT STA 617. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 32,499 hrs · 11,864 cycles

ACRID SMELL AND SPARKS FROM RIGHT WINDSHIELD HEAT. RIGHT WINDSHIELD CRACKED. MOISTURE INGRESSION OF 1ST OFFICERS WINDSHIELD CAUSED ARCING OF THE HEATING ELEMENT. REPLACED WINDSHIELD ASSY AND WINDOW HEAT CONTROLLER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,821 hrs · 10,871 cycles

FUSELAGE SKIN DAMAGED AT STA 1280 STR 20 RT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,821 hrs · 10,871 cycles

FUSELAGE SKIN DENTED FWD OF STA 1720 STR 14 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.

Part: SEQUENCE VALVE — FAILED (NLG DOOR)

LANDED DCA UNDER AMBER ALERT DUE TO A GEAR INDICATION PROBLEM. *S/D* NLG DOOR SEQUENCE VALVE FAILED. REPLACED VALVE.

Part: BEARING — FAILED (NLG)

NOSE WHEEL BEARING FAILURE ON LANDING CAUSED A NOSE GEAR FIRE, WHICH THE AIRPORT FIRE DEPARTMENT EXTINGUISHED. *S/D* LEFT O/B NLG WHEEL BEARING FAILED. POSSIBLE CAGE FAILURE. REPLACED BEARING.

Part: TAT PROBE — FAILED (FUSELAGE)

RETURNED TO FIELD DUE TO TAT PROBE EICAS MESSAGE. *S/D* TAT PROBE FAILED. REPLACED TAT PROBE PER APPLICABLE MM.

Part: SLIDE — FELL OFF (DOOR 4R)

CATERERS PARTIALLY OPENED DOOR FOUR RIGHT, WITH DOOR ARMED, CAUSING SLIDE TO FALL OFF. *S/D* 757 HAS AN EMERGENCY ASSIST CYLINDER TO OPEN DOOR IN EMERGENCY (WITH SLIDE ARMED). AMIS WRITE UP IMPROPERLY REPORTED PARTIAL OPENING OF DOOR. SLIDE WAS BLOWN AND OPERATED NORMALLY. EMERGENCY RESERVOIR BOTTLE WAS REPLACED. DOOR SLIDE ASSY WAS REINSTALLED. OPS CHECK WAS OK. ALL CHECKS WERE OK.

Part: TURBINE VANE — CRACKED (RT ENGINE)

DURING RIGHT ENGINE BORESCOPE, FOUND TWO HIGH PRESSURE TURBINE VANES WITH A V-TYPE CRACK. TOTAL CRACK LENGTH EXTENDS GREATER THAN .25 INCH ON EACH VANE. REPLACED RIGHT ENGINE FOR HEAVY MAINTENANCE VISIT.

Part: SLIDE — POROUS (INFLATION TUBE)

SLIDE REMOVED FROM AIRCRAFT FOR TIME CONTROLLED OVERHAUL. UNIT FAILED AIR RETENTION DUE TO POROSITY ON THE UPPER AND LOWER TUBE. SCRAPPED INFLATABLE UNIT, REPLACED WITH NEW.