N523UA

Part: OXYGEN MASK — RUPTURED (COCKPIT) · airframe 74,900 hrs · 27,606 cycles

CAPTAIN`S O2 MASK INFLATION HEAD BAND RUPTURED. REPLACED CAPTAIN`S O2 MASK, OPERATIONS CHECKED OKAY.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 74,885 hrs · 27,601 cycles

SPEED SELECT ON MODE CONTROL PANEL STUCK AT 160 KNOTS. REPLACED AFCS MODE CONTROL PANEL, CHECKED NORMAL.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 74,586 hrs · 27,509 cycles

NR 1 ENG HAS A NICK ON THE INNER PORTION OF BLADE LE 18.75 INCHES FROM BLADE ROOT. BLENDED BLADE IAW AMM 72-31-02. ACCOMPLISHED CHECKED GOOD. NO FURTHER ACTION REQUIRED.

Part: WARNING MESSAGE — ACTIVATED (HYDRAULIC SYS) · airframe 74,548 hrs · 27,495 cycles

CREW REPORTS LT RESERVOIR PRESS EICAS MESSAGE WITH ASSOCIATED OVERHEAD PANEL LIGHT.

Part: LENS — MISSING (CABIN) · airframe 74,154 hrs · 27,366 cycles

LENS MISSING FROM EMERGENCY EXIT SIGN AT DOOR 2L.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 74,157 hrs · 27,368 cycles

FWD GALLEY COFFEE MAKER MADE A POPPING NOISE & A LITTLE SMOKE WHEN BREW BUTTON PRESSED.

Part: SOCKET — DAMAGED (GALLEY LIGHTS) · airframe 73,625 hrs · 27,189 cycles

FWD GALLEY OVERHEAD LIGHT ASSY HAS FOUR INBD BULB SOCKETS DAMAGED DUE TO AGE.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 73,515 hrs · 27,157 cycles

DURING SINGLE PACK OPERATIONS THE LT A/C PACK SYSTEM WOULD NOT MAINTAIN CABIN PRESSURE. CREW FOLLOWED QRH & WAS ABLE TO RECOVER PRESSURIZATION SYSTEM. PERFORMED PNEUMATIC HEALTH CHECK ON NR 1 ENGINE FOUND HIGH STAGE PILOT & PRESSURE REGULATING & SHUTOFF VALVE FAULT. REPLACED HIGH STAGE PILOT & PRESSURE REGULATING & SHUTOFF VALVE IAW AMM 36-11-08, 36-11-09. RAN NR 1 ENGINE & PRESSURIZED AIRCRAFT WITH SINGLE PACK TO 4 PSID. NO FAULTS.

Part: ENGINE — LEAKING (NR 2) · airframe 73,501 hrs · 27,152 cycles

F/O POINTED OUT OIL LEAKING FROM NR 2 ENGINE, FOUND OIL LEAKING OUT OF 2.5 BLEED PORT, ON FURTHER INSPECTION WITH BOROSCOPE, FOUND OIL RUNNING DOWN INSIDE OF ENGINE AT THE SEAM. SUSPECT IT IS A LEAK FROM THE NR 2 MAIN BEARING CARBON SEAL.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 73,403 hrs · 27,119 cycles

EMERGENCY PATH FLOOR LIGHTING CLEAR COVER DISLODGED AT 2L. INSTALLED CLEAR COVER ON EMERGENCY PATH LIGHTING AT 2L.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LGIHT) · airframe 73,344 hrs · 27,102 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE AT SEAT 37 AND 38 ABC. REPLACED LEAD-IN POWER STRIP, OPS CHECKED GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (FWD LAVATORY) · airframe 73,109 hrs · 27,027 cycles

FWD LAVATORY SMOKE DETECTOR IS INOPERATIVE. REPLACED SMOKE DETECTOR.

Part: GAUGE — FAULTY (POTABLE WATER) · airframe 73,067 hrs · 27,014 cycles

POTABLE WATER GAUGE INOPERATIVE. DOES NOT READ ACCURATELY. READING 22 WHEN TOLD FULL "35".

Part: FILTER — FAULTED (RECIRC FAN) · airframe 73,062 hrs · 27,013 cycles

HIGH PITCHED WHINE BEHIND INSTUMENT PANEL. REPLACED LT RECIRCULATION FAN FILTER. OPS CHECKED NORMAL.

Part: FAN — VIBRATES (COCKPIT) · airframe 73,067 hrs · 27,014 cycles

ABNORMAL NOISE, VIBRATION AROUND RT GLARESHIELD OR RT WINDSHIELD AREA. RADIO COMMUNICATION DIFFICULT. R & R LEFT CABIN RECIRCULATION FAN IAW AMM. OPS CHECKED GOOD.

Part: CAP — UNSECURE (EMERGENCY LIGHT) · airframe 72,987 hrs · 26,990 cycles

EMERGENCY LIGHT PLASTIC STRIP COMING UP AT ROW 14ABC. SECURED PLASTIC CAP IAW AMM.

Part: ANGLE — CORRODED (BS 615) · corrosion level 2 · airframe 72,726 hrs · 26,908 cycles

FWD CARGO DOOR CUTOUT LOWER ANGLE CORRODED AT BS 615. REPAIRED FWD CARGO DOOR CUTOUT IAW ECRA 5330-0415 CATEGORY 'A' REPAIR IAW SRM 51-00-06, OPS CHECKED GOOD. MAJOR REPAIR.

Part: WEB — DAMAGED (BS 324) · airframe 72,726 hrs · 26,908 cycles

BS 324 WEB HAS ELONGATED HOLES FROM RBL 30 - 62. REPLACED WEB AND ANGLES, AND REPAIRED FRAME IAW ECRA 5310-05720 AND REO-G16061 REV H. ACCOMNPLISHED HFEC IAW NTM PRT 6, 51-00-19, NO DEFECTS NOTED. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 72,726 hrs · 26,908 cycles

CABIN FLOORBEAM UPPER TEE CORRODED BEYOND SRM LIMITS AT BS 324, RBL 42-63. REMOVED DAMAGE SECTION OF TEE FROM LBL 7 TO RBL 64. HFEC CUT-OUT & BOLT HOLE, NO CRACK FOUND. FABRICATED & INSTALLED REPAIR SPLICE & UPPER TEE FROM LBL 7 TO RBL 68 PER SRM 53-10-08 RPR 1.

Part: SKIN — DENTED (BS 590-661) · airframe 72,726 hrs · 26,908 cycles

FUSELAGE SKIN AT BS 590-661 BETWEEN S14-19L HAS MULTIPLE DENTS ON EXISTING REPIR DOUBLER. REMOVED EXISTING DOUBLER, HFEC CUTOUT & BOLT HOLES, NO CRACK FOUND. FAB & INSTALLED REPLACEMENT SKIN & REINFORCEMENT DOUBLER BETWEEN S13-20L PER ECRA 5330-04510.

Part: CREASE BEAM — CORRODED (BS 1130) · corrosion level 2 · airframe 72,726 hrs · 26,908 cycles

MAIN CABIN CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 1130, LBL 68. REMOVED DAMAGED WEB, HFEC BOLT HOLES, NO CRACKS NOTED. FABRICATED & INSTALLED WEB REPAIR DOUBLER PER ECRA5340-01 504. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 72,726 hrs · 26,908 cycles

MAIN CABIN FLOORBEAM UPPER TEE AT BS 365, BL 0-RBL 64, WL 208 CORRODED. HFEC WEB CUT-OUT & BOLT HOLES, NO DEFECT NOTE. FABRICATED & INSTALLED UPPER TEE ANGLE REPAIR IAW ECRA5310-05536. MAJOR REPAIR.

Part: WEB — CORRODED (BS 1410) · corrosion level 2 · airframe 72,726 hrs · 26,908 cycles

MAIN CABIN FLOOR WEB AT AIR GRILL, CORROSION FOUND ON UPPER SURFACE BS 1410 RBL 65. FOUND CORROSION OUT OF LIMITS. FABRICATED FORMED AND INSTALLED WEB IAW DWG 146N5590-8 AND SRM 53-60-13 SEC 46 FIG 1 ITEM 5. INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 72,726 hrs · 26,908 cycles

MAIN CABIN FLOORBEAM UPPER TEE CORRODED BS 377 RBL 54- 58. REPAIRED UPPER TEE AT IAW EC RA 5310-05536. HFEC FOUND CRACK IN HOLES. COMPLIED WITH ECRA 5310-05712 HAS BEEN APPROVED FOR STAGE 1 VIA 8100- 9.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,563 hrs · 26,848 cycles

EMERGENCY EXIT LIGHT MOUNTED ON AFT CARGO DOOR INOPERATIVE. REPLACED LAMPS, OPS NORMAL.

Part: LANYARD — OBSTRUCTED (R4 DOOR) · airframe 72,222 hrs · 26,734 cycles

SLIDE ARMED LIGHT 4R DOES NOT ILLUMINATE WITH DOOR CLOSED AND ARMED. REMOVED SLIDE LANYARD FROM GIRT BAR NOT ALLOWING GIRT TO ARM TO PROX SENSOR, OPS CHECK ARMED DISARMED SLIDE LIGHT ON AND OFF NORMALLY, VERIFIED GIRT BAR POSITIONS AT ARM AND DISARMED, OP CHECK NORMAL.

Part: TIRE — FAULTY (NLG) · airframe 71,701 hrs · 26,559 cycles

NOSE GEAR SHIMMY ON TAKEOFF ROLL FELT IN RUDDER PEDALS, DAMAGE FROM TOWBAR BREAK? INSPECT NLG PER MM. REPORT FINDINGS TO TOMC. ACCOMPLISHED INSPECTION PER AMM. NO DEFECTS NOTED. REPLACED NLG TIRES AND WHEELS PER AMM PRECAUTIONARILY FOR NLG VIBRATION ON TAKEOFF.

Part: BLADE — NICKED (LT ENGINE FAN) · airframe 71,184 hrs · 26,393 cycles

LEFT ENGINE FAN BLADE IS NICKED, BLENDED BLADE REF MM 72-31-02, REF FIGURE 804. DAMAGE WAS IN AREA 8, 1-16TH DEEP, 1-8TH LONG.

Part: BEARING — FROZEN (PAX DOOR) · airframe 70,986 hrs · 26,326 cycles

FOUND FWD ARM DISARM TORQUE TUBE BEARING FROZEN. BEARING TURNING IN HOUSING. ARM DISARM TORQUE TUBE DISASSEMBLED AND HOUSING REMOVED, ROD TO ARM LEVER IS DISCONNECTED AT ARM LEVER. REPLACED FWD BEARING HOUSING REF IPC 52-11-01-034 VIEW "K". INSPECTION DOOR FOR SECURITY AND SAFETY, DOOR OPS CHECKED OK REF GROUP.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 70,934 hrs · 26,307 cycles

R4 DOOR DIFFICULT TO DISARM. REMOVED GIRT BAR. FOUND ARM DISARM INTERMITTENT (STILL BINDING). REINSTALLED GIRT BAR ARM DISARM STILL BINDING. REMOVED AND REINSTALLED R4 DOOR SLIDE ASSY REF MM. REMOVED SLIDE INFLATION PIN AND REARMED ASSIST BOTTLE. ADJUSTMENT ACCOMPLISHED, OPS CHECKED GOOD.

Part: BLEED VALVE — FAULTY (RT ENGINE) · airframe 70,294 hrs · 26,097 cycles

RIGHT ENGINE AMBER LIGHT, RETURNED TO FIELD. REPLACED HIGH STAGE BLEED VALVE AND PILOT PER MM.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 70,177 hrs · 26,050 cycles

DOOR 4R SLIDE ARMED LIGHT NOT ILLUMINATED WITH DOOR ARMED STOWED ESCAPE SLIDE LANYARD IN SKIRT PER AMM. DOOR 4R SLIDE IS ENGAGING FLOOR FITTINGS NORMALLY.

Part: OXYGEN BOTTLE — MISSING (CABIN) · airframe 69,689 hrs · 25,870 cycles

OXYGEN BOTTLE MISSING-USED AT VID-MONITOR MID-CBN CTR NR 1. 3 OXYGEN BOTTLES USED FROM AFT COACH :DISTRIBUTED BOTTLES EVENL Y TO ALL THREE STATIONS, PLACED DF STICKERS ON BOTTLE BRACKETS AND PLACED STICKER DF ON EMPTY BOTTLES, EMPTY BOTTLES LOCATED AT 1AB , 20ABC AND COMPT OUTSIDE FWD AFT LAV. REPLACED USED OXYGEN BOTTLES LISTED ABOVE.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,607 hrs · 25,838 cycles

BURNING PLASTIC SMELL NEAR DOOR 3L. INSPECTED ACFT CABIN AREA AROUND DOOR LAV AND GALLEY. OPERATED CHILLERS AND LIGHTS AND LAV ITEMS NO DEFECTS NOTED AND NO BURNING SMELL. OPERATED ALL AC PACKS AND RECIRC FANS NO SMELL NOTED. NEXT SEGMENT THE INBD F/A'S REPORTED SMELL IN AFT GALLEY AREA BY DOOR 4L. CHECKED AREA, NO ODOR NOTED. TRIED ALL ELECTRIC FUNCTIONS IN AREA, AND HAD PACKS RUNNING, NOTHING NOTED. OTBD F/A REPORTED SHE DIDN'T SMELL ANYTHING EITHER. CHECKED LOWER COMPT AFT OF BULKHEAD, NO ODOR NOTED THERE EITHER.

Part: VALVE — FAULTY (GALLEY) · airframe 69,466 hrs · 25,784 cycles

FOUND AFT GALLEY WATER SHUT OFF UNABLE TO STOP WATER FLOW. NEW VALVE REF IPC 25-30-00B-001A ITEM 55, VALVE PN (#641-1090). TIGHTENED SET SCREW ON KNOB. OPS CHECKS OKAY.

Part: VALVE — FAULTY (LT WING) · airframe 68,757 hrs · 25,514 cycles

FIRST START ATTEMPT NORMAL FF BUT NO LIGHT OFF. REPLACED LEFT WING SPAR VALVE. OPERATED VALVE SEVERAL TIMES, NORMAL OP'S.

Part: LINE — LOOSE (R4 DOOR) · airframe 68,040 hrs · 25,231 cycles

DOOR 4R LOOSE STRING. SECURED STRING FOR DOOR SLIDE 4R.

Part: FLOORBOARD — DAMAGED (AFT CARGO BAY) · airframe 67,849 hrs · 25,164 cycles

AFT CARGO PIT FLOORBOARD DAMAGE. REMOVED AFT PIT MIDDLE FLOORBOARD PANEL. REPAIRED REF SRM.

Part: ROLLER — FAULTY (R3 DOOR) · airframe 70,986 hrs · 26,326 cycles

R3 DOOR FWD AND AFT UPPER LATCH ROLLER ASSEMBLIES. REMOVED AND REPLACED FWD AND AFT LATCH ROLLERS. DOOR OPS CHECKED OKAY.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 67,693 hrs · 25,110 cycles

HYD FLUID ON BOTTOM SURFACE OF LEFT WING. OPERATED FLAPS AND SPEED BRAKES, NO LEAKAGE NOTED. CLEANED AREA AND CARRY FORWARD WITH RECHECK WITHIN 75 FLIGHT HOURS PER MM. FOUND AREA WET WITH HYD FLUID, CLEANED AREA. OPERATED HYD SYSTEMS IN AREA ON ACTIVE LEAKS NOTED. -INF- AREA IS THE OUTBD FLAP AREA. NR 2 SPOILER ACT LEAKING AT VALVE BLOCKING THERMAL RELIEF. LEAK OKAY PER MM.

Part: CAP — DEFECTIVE (RAT) · airframe 67,617 hrs · 25,081 cycles

RAT GREEN PRESS LIGHT IS OUT. REPLACED SWITCH CAP FOR RAT RELEASE SWITCH, OPS NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,352 hrs · 24,985 cycles

AT STA 1681 EXTENSIVE CORROSION FLOORBEAM. THIS IS A REINFORCING REPAIR DESIGNATED MAJOR, IT WILL RECEIVE FAA APPROVAL PER FORM 8100-9 AFTER COMPLETION. RECEIVED FINAL APPROVAL FORM 8100-9 ON EVA UA80829 REV.C

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,352 hrs · 24,985 cycles

FLOORBEAM STA 700 CRACKED AT LBL 45. RPRD PER SRM 53-00-51, RPR. 3 AND UA EVA 80770, ON SMB W-U F6397E.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,352 hrs · 24,985 cycles

EXT FUSE SKIN IS DENTED AND BULGED AT FRAME STA 600, AND 640 STR 17L AND 18L. OK TO ARC REF SRM 53-00-01 FIG 101 DETAIL III AND SRM 51-70-01, HFEC NO CRACKS. REPLACED SHEAR TIE ON WU"S D4028X, D4030X.

Part: SENSOR — OUT OF ADJUST (RT EMERGENCY EXI) · airframe 67,095 hrs · 24,888 cycles

RT WING EMER DOOR LIGHT CAME ON SHORT FINAL LIGHT WENT OUT AFTER LAND. ADJUSTED RT FWD OVERWING EMERGENCY EXIT HATCH SENSOR, OPS CK NORMAL.

Part: SWITCH — STICKING (MICROPHONE) · airframe 66,887 hrs · 24,804 cycles

F/O YOLK MIC SWITCH STICKS (INTERMITTENT HOT MIC). REPLACED F/O YOLK PTT SWITCH, CHECKS GOOD.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 66,849 hrs · 24,786 cycles

RT ENG SPAR VALVE ON, STAYED ON, ENG STARTED THEN FLAMED OUT. CYCLED ACTUATOR, CKD GROUND IAW MM. CLEANED CONNECTOR, STARTED NORMAL 2 TIMES AT GATE.

Part: IDG — FAILED (LT ENGINE) · airframe 66,630 hrs · 24,705 cycles

L GEN FAILURE, FLIGHT DIVERTED. REPLACED LEFT ENGINE IDG, OP CHECKS GOOD.

Part: BELLCRANK — DAMAGED (R4 DOOR) · airframe 66,264 hrs · 24,567 cycles

DOOR 4R WILL NOT DISARM PROPERLY. DISARM LEVER WILL NOT GO TO FULL DEFLECTION UNTIL DOOR IS OPENING AND LEVER MANUALLY MOVED TO FULL DISARM POSITION. WITH DISARM LEVER IN FULL DISARM POSITION WHEN DOOR HANDLE IS CLOSING ARMING LEVER MOVES TOWARD ARMED POSITION. REPLACED BENT BELLCRANK. INSTALLED GIRT AND FITTINGS.

Part: LAMP — INOPERATIVE (EMEGENCY LIGHTS) · airframe 65,434 hrs · 24,251 cycles

DOOR 2R EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, OPS CHECKED OK.

Part: FLOORBOARD — WEAK (AISLE ROW 28) · airframe 64,717 hrs · 23,974 cycles

ROW 28, AISLE FLOOR VERY WEAK AND SPONGY. INSTALLED DOUBLER. 5B PANEL TO BE REPLACED NEXT C-CHECK.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 64,592 hrs · 23,926 cycles

ACFT DAMAGE LT ELEVATOR T/E HAS (2) EACH LOCATIONS DAMAGED FROM CONTACT WITH LIFT DURING MX. REPLACED LT ELEVATOR.

Part: GIRT BAR — UNSECURE (DOOR 1R) · airframe 63,667 hrs · 23,561 cycles

CREW REPORT: DOOR 1R HAS GIRT BAR LOOSE AND HANGING DOWN WITH DOOR SLIGHTLY AJAR. SUPPLEMENTAL DATA UPDATE SECURED GIRT BAR. DOOR SLIDE ARM AND DISARM PROPERLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,530 hrs · 23,511 cycles

FOUND AFT IN FRONT OF LAV SMALL EGRESS LIGHTING STRIP NOT WORKING. REPLACED SMALL EMERGENCY LIGHT STRIP IN FRONT OF AFT FWD LAV DOOR. OK FOR SERVICE.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 61,775 hrs · 22,831 cycles

CAPTAIN'S O2 MASK MIKE IS NOT WORKING. REPLACED CAPTS AUDIO SELECT PANEL. SYSTEM CHECKS NORMAL AT THE GATE. ALSO CHANGED CAPTAIN'S O2 MASK ASSY. SYSTEM CHECKS NORMAL AT THE GATE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 60,301 hrs · 22,251 cycles

SEVERAL EMERGENCY EXIT LIGHTS ARE INOP. REPLACED AFT EEL FLOOR LIGHTING PLUG IN STRIP. CLEANED SOCKETS BULLNOSE LIGHTS. CHECKS OK.

Part: DUCT — DAMAGED (CABIN PRESSURE) · airframe 59,932 hrs · 22,121 cycles

PRESSURIZATION PROBLEM. RTFL. REPLACED BLOWN FLEX DUCT.

Part: SHIM — BROKEN (EVAC SLIDE) · airframe 59,932 hrs · 22,120 cycles

LEFT OFF-WING SLIDE PACK INFLATION HOSE ADAPTOR FITTING HAS A BROKEN MICARDA SHIM. REPLACED SHIM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,773 hrs · 21,679 cycles

FOUND DOOR 1L SLIDE ON FLOOR. RESECURED SLIDE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 57,412 hrs · 21,196 cycles

FLIGHT CREW REPORTS SMOKE IN COCKPIT. UNABLE TO DUPLICATE ON GROUND. PERFORMED TEST OF RT AND LT RECIRCULATION FANS, OPS CHECKED EQUIPMENT COOLING FANS, RAN APU WITH AI ON, TRIED DIFFERENT CROSSBLEED CONFIGS, NO ODOR EVER NOTED. THIS ISSUE NEVER APPEARED AGAIN AFTER 1/16/08.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

BS 1500 FRAME BETWEEN STR 28R - 29R HAS DAMAGE. FRAME REPAIR BETWEEN STR 28R-29R HA S BEEN DEEMED INTERIM WITH REPEAT INSPECTIONS EVERY 12000 CYCLES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

SEAT TRACK SUPPORT AT BS 365.25 AND RBL 24 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. INSTALLED STRAP REPAIR.

Part: GATE — CRACKED (R4 DOOR) · airframe 57,169 hrs · 21,102 cycles

THE R-4 DOOR UPPER GATE CRACKED AT SECOND LT HINGE MOUNT HOLES. REPLACED LOWER GATE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

SEAT TRACK SUPPORT AT BS 365.25 AND RBL 45 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: INSTALLED STRAP REPAIR.

Part: GATE — CRACKED (L2 DOOR) · airframe 57,169 hrs · 21,102 cycles

L-2 DOOR UPPER GATE CRACKED. INSTALLED NEW GATE.

Part: SKIN — DAMAGED (R2 DOOR) · airframe 57,169 hrs · 21,102 cycles

FOUND DOOR 2R UPPER HINGE ARM CUTOUT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 57,169 hrs · 21,102 cycles

FOUND DOOR 2L UPPER HINGE ARM CUTOUT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED STEEL DOUBLER REPAIR.

Part: WEB — PUNCTURED (L4 DOOR) · airframe 57,169 hrs · 21,102 cycles

DOOR 4L INTERNAL WEBBING PUNCTURED AT UPPER HINGE ASSY AREA. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: STRUCTURE — CORRODED (R4 DOOR) · airframe 57,169 hrs · 21,102 cycles

DOOR R4 HANDLE BOX HAS CORROSION AROUND AND IN INSERTS AND IN SHAFT FOR HANDLE MECHANISM. INSTALLED NEW HANDLE BOX.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

AFT PIT BS 1360 FRAME HAS DENT AND MINOR SURFACE CORROSION AT STR 25L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FRAME. FABRICATED & INSTALLED A REPAIR ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

STA 365.25 FLOORBEAM CORRODED FROM LBL 24 .75 TO RBL 45.5. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED T-CAP. FABRICATED & INSTALLED NEW CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

MAIN CABIN AFT SECTION AT STA 1640, RBL 20 TO RBL 40, FLOORBEAM CORRODED ON UPPER T-CAP. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, FABRICATED & INSTALLED NEW FLOORBEAM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

MAIN CABIN AT STA 700, LBL 24, FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. FABRICATED & INSTALLED NEW T-CAP REPAIR.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

LIGHTNING STRIKE DAMAGE AT STATIONS 490, 520 & 550 STR 6L. REPLACED BLIND FASTENERS WITH SOLID FASTENERS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

LIGHTNING STRIKE STA 1480 STRINGER 3L. REPLACED BLIND RIVET WITH SOLID RIVET.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

LIGHTNING STRIKE STA 418 BETWEEN S7L AND S8L. REPLACED BLIND FASTENER WITH SOLID RIVET.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,169 hrs · 21,102 cycles

LIGHTNING STRIKE STA 1530 STRINGER 3L & STA 1163 BTWEEN STRINGERS 5&6 MIDDLE OF FIELD. REPLACED FASTENERS WITH SOLID RIVETS.

Part: LAMP — INOPERATIVE (R3 DOOR SLIDE) · airframe 56,567 hrs · 20,853 cycles

THE 3R SLIDE ARMED LIGHT INOP. FOUND A FUSED LAMP. REPLACED LAMP.

Part: RADOME — CONTAMINATED (NOSE) · airframe 56,243 hrs · 20,730 cycles

FLIGHT DIVERTED DUE TO INOPERABLE WEATHER RADAR. UNRELIABLE WEATHER RADAR CELLS. RADOME FAILED MOISTURE TEST, REPLACED RADOME WEATHER RADAR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,689 hrs · 20,539 cycles

LEFT OVERWING ESCAPE HATCH EXTERIOR AFT LIGHT INOP. [06-22-07] RELAMPED OPERATES NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,689 hrs · 20,539 cycles

EMERGENCY ESCAPE PATH LIGHT (FLOOR) 1EA LIGHT INOP AT SEAT 34. REPLACED LAMP.

Part: LAMP — INOPERATIVE (SLIDE ARM LIGHT) · airframe 54,778 hrs · 20,214 cycles

DOOR 3R SLIDE ARMED LIGHT INOPERATIVE. [SUP 05-29-07] RELAMPED. OP CHECKED NORMALLY.

Part: STARTER — FAILED (RT ENGINE) · airframe 54,738 hrs · 20,198 cycles

DURING RT ENG START, NO N2, NO N1, RAMP REPORTED SPARKS FROM RIGHT ENGINE. [SUP 05-18-07] REPLACED STARTER DUE TO LOW OIL. ALSO REPLACED STARTER VALVE DUE TO FOD FROM STARTER FAILURE. OP CHECKS OK.

Part: CYLINDER — CORRODED (LT MLG) · airframe 53,617 hrs · 19,773 cycles

LT MLG OUTER CYLINDER INNER SURFACE IS CORRODED BETWEEN GLAND NUT THREADS AND CHROME PLATED SURFACE. LEFT MLG OUTER CYLINDER INNER SURFACE IS CORRODED BETWEEN GLAND NUT THREADS AND CHROME PLATED SURFACE, ITEM ROLLED FORWARD APPROX 270 DEGREES. REPLACED MAIN LANDING GEAR OUTER STRUT CYLINDER. SERVICED SHOCK STRUT, BLED BRAKES AND GEAR NORMAL. ACCOMPLISHED AUTOBRAKE AND ANTI-SKID TESTS.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 53,182 hrs · 19,605 cycles

AFTER FCU CHANGE NR 1 ENG HAD COMPRESSOR STALL ON DECEL AT APPROX 1.12 EPR, THEN 3 MORE STALLS AT IDLE THEN AUTO SHUTDOWN. NR 1 ENG RESTART FAILED, ENG HUNG STARTED AT 40% N2 WITH N1 ROTATION, EGT AT 225 DEG, FUEL FLOW NORMAL AT .6, DUCT PRESS WAS 30 PSI. FOUND VSV ACTUATOR LOWER ATTACH POINT BROKEN OFF. ENGINE WAS REPLACED.

Part: SKIN — DENTED (BS 1715 S18L) · airframe 51,850 hrs · 19,123 cycles

FOUND SKIN DENTED AT STATION 1715, 2 INCHES BELOW STR 18L. THE AIRCRAFT SKIN WAS DAMAGED AT STA 1715, 2 INCHES BELOW STR 18L. THE DAMAGED SKIN WAS REMOVED AND AN EXTERNAL SKIN DOUBLER WAS INSTALLED PER EVA NUMBER UA-EVA-60253A. THIS REPAIR RECIEVED SFAR APPROVAL PER FORM 8100-9 DATED 25APR06. DTA INFORMATION WILL FOLLOW.

Part: SKIN — LIGHTNING STRIKE (BS 460 S6-7L) · airframe 51,850 hrs · 19,123 cycles

FOUND LIGHTNING STRIKE STA 460 BETWEEN S6L & 7L. REMOVED FASTENER, HFC FOUND NO CRACKS, INSTALLED SOLID FASTENER.

Part: SKIN — LIGHTNING STRIKE (BS 443 S7L) · airframe 51,850 hrs · 19,123 cycles

FOUND LIGHTNING STRIKE STATION 443 STRINGER 7L. REMOVED FASTENER, HFC FOUND NO CRACK AND INSTALLED SOLID FASTENER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,604 hrs · 19,028 cycles

AFT CABIN EEL LIGHTS INOP FROM ROWS 23-31.

Part: WARNING SYSTEM — ACTIVATED (MLG) · airframe 50,114 hrs · 18,476 cycles

ANTI-SKID EICAS AND VIBRATION DURING TAKEOFF ROLL AND GEAR RETRACTION. REPLACED WIRING FR0M D2040 TO TB211, FOUND OPEN ON WIRE W4904-2501R-20. RE-SECURED SHIELDING PINS AT TB211 (LA4 AND LE4) ALL PER WD32-42-11. OPS CHK NORMAL.

Part: ODOR — DETECTED (COCKPIT) · airframe 49,899 hrs · 18,389 cycles

LIGHT SMOKE AND BURNING ODOR IN COCKPIT WITH RIGHT PACK OPERATING OFF APU. ACCOMPLISHED AIR CONDITIONING SYSTEM OIL CONTAMINATION MAINTENANCE PRACTICES PER MM21-00-01. NO SMELLS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 42,498 hrs · 15,682 cycles

AFT CABIN EEL LIGHTS BETWEEN ROW 23 AND 31 INOPERATIVE WITH TEST SWITCH AND MASTER SWITCH IN COCKPIT. REPLACED POWER SUPPLY BATTERY PACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,550 hrs · 13,787 cycles

CABIN FLOORBEAM HAD CORROSION MATERIAL REMOVED EXCEEDS LIMITS, STATION 345 RBL 52 UPPER FLANGE AFT SIDE. MAJOR REPAIR ACCOMPLISHED. UPPER CAP REPAIRED.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT CABIN FLOORBEAM AT STATION 1681.1 UPPER CAP LOWER SURFACE HAS EXCESSIVE MATERIAL REMOVED FROM LBL 11 TO LBL 13. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA TRIMMED OUT AND ANGLE DOUBLER AND TRIPLER INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

STATION 1681 FLOORBEAM UPPER CAP FORWARD FLANGE HAD CORROSION AND EXCESSIVE MAT LOSS AT RBL 30 THROUGH RBL 33 RBL 39 THROUGH RBL 41 AND RBL 47. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED, INSTALLED REPAIR ANGLES.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

CABIN FLOOR STATION 1680 SHEAR DECK RIGHT HAND DOUBLER HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT CABIN FLOORBEAM STATION 1681 FORWARD LOWER SURFACE EXCESSIVE MAT REMOVED AT LBL33. MAJOR REPAIR ACCOMPLISHED. ANGLE REPAIR INSTALLED.

Part: CLIP · airframe 38,308 hrs · 14,118 cycles

AFT PIT STATION 1520 STRINGER 22L CLIP MANUFACTURED FROM 2 SEPARATE T-CHORD ANGLES. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP WAS MANUFACTURED AND INSTALLED.

Part: FLANGE — GOUGED · airframe 38,308 hrs · 14,118 cycles

AFT PIT BODY FRAME UPPER FLANGE IS GOUGED LOC STATION 1520 BELOW STRINGER 26R. MAJOR REPAIR ACCOMPLISHED. FRAME BLENDED AND FABRICATED STRINGER CLIP.

Part: PLATE · airframe 38,308 hrs · 14,118 cycles

AFT CABIN DECK PLATE CUT OUT FOR ACCESS AT STATION 1681 AND LBL 33. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: PLATE — CORRODED · airframe 38,308 hrs · 14,118 cycles

AFT CABIN DECK PLATE CORRODED STATION 1681 LBL 12 - LBL4. MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

STATION 1640 CABIN FLOORBEAM HAS EXCESSIVE MATERIAL LOSS AT RBL 34-50. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED T-CAP REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT PIT FUSELAGE FRAME HAS DENT ON INNER FLANGE STATION 1420 STRINGER 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER ON INNER FLANGE.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT PIT BODY FRAME HAS 2 DENTS AT 1520 STRINGER 22L-23L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT CARGO COMPARTMENT CIRCUMFERENTIAL FRAME BODY STATION 1580 STRINGER 26L HAS DENT ON INNER CHORD. MAJOR REPAIR ACCOMPLISHED. REPAIRED DOUBLER AND STRINGER CLIP.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT PIT BODY FRAME INNER FLANGE HAS A DENT BODY STATION 1500, STRINGER 26L-27L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT PIT FUSELAGE FRAME HAS DENT STATION 1480 STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER ON INNER FLANGE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT PIT BODY FRAME INNER FLANGE LOWER SURFACE IS GOUGED BODY STATION 1500, RBL8, WL 147. MAJOR REPAIR ACCOMPLISHED. INNER J-ANGLE DOUBLER INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

STATION 520 BETWEEN STRINGER 24L AND 25L FUSE FRAME UPPER CHORD IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 38,308 hrs · 14,118 cycles

CABIN FLOORBEAM UPPER CHORD HAS CORROSION RBL 53 TO RBL 62 STATION 324. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF FLOORBEAM UPPER CHORD.

Part: FAILSAFE — DAMAGED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

AFT PIT BODY FRAME FAIL SAFE CHORD WAS BLENDED IN RADIUS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR DOUBLER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

MID CABIN CREASE BEAM INNER CHORD BODY STATION 1020 LBL 63 HAS SURFACE CORROSION ON UPPER FLANGE. MAJOR REPAIR ACCOMPLISHED. REPLACED INNER BULB ANGLE WITH SPLICE AT BODY STATION 1010.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

CABIN FLOOR STATION 377 LBL 22 HAS EXCESSIVE MAT LOSS ON UPPER CAP. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAPS INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

CABIN FLOOR STATION 77 LBL 42 HAS EXCESSIVE MAT LOSS ON UPPER CAP OF BEAM. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAPS 11 INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

EXT FUSELAGE STATION 610 TO STATION 620 AND STRINGER 16L AND STRINGER 17L DAMAGED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

MID CABIN FLOORBEAM T-CAP STATION 700 LBL 15 TO RBL 23 GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP AND ANGLE INSTALLED.

Part: SPLICE · airframe 38,308 hrs · 14,118 cycles

AFT PIT FUSE FRAME SPLICE CORRODED AT STATION 1520, STRINGER 24R. MAJOR REPAIR ACCOMPLISHED.REPLACED FRAME SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,308 hrs · 14,118 cycles

CABIN FLOORBEAM STATION 365 RBL 13 TO 28 CORRODED ON FWD SIDE OF FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: HOSE — RUPTURED (HYDRAULIC SYS) · airframe 32,965 hrs · 12,217 cycles

RETURNED TO DEN DUE TO LOSS OF HYDRAULIC FLUID IN THE LEFT HYDRAULIC SYSTEM. *S/D* PRESSURE HOSE FOR DOWNLOCK ACTUATOR WAS LEAKING. REPLACED HOSE.

Part: CONNECTOR — LOOSE (LT ENGINE BLEED) · airframe 32,092 hrs · 11,880 cycles

RETURNED TO THE FIELD AT ORD DUE TO LEFT ENGINE BLEED FAILURE. *S/D* LT ENGINE HIGH STAGE CONTROLLER WAS FOUND WITH A LOOSE CONNECTOR. CONNECTOR WAS SECURED AND HIGH STAGE MUSCLE LINES WERE REPLACED AS A PRECAUTION. NO FURTHER PROBLEMS HAVE OCCURRED SINCE THE CORRECTIVE ACTIONS.

Part: RESISTOR — FAILED (CIRCUIT CARD)

IN CRUISE FL350 GOT NO LAND 3. TRIED RIGHT AUTOPILOT, AC ROLLED HARD RIGHT. TURNED RIGHT A-P OFF AND PUT CENTER A-P ON. STRONG SMELL OF HOT ELECTRICAL INSULATION. TURNED RIGHT PACK OFF, SMELL DISSIPATED. DIVERTED TO DENVER. *S/D* FOUND RESISTOR BURNED UP. REPLACED RIGHT FCC COMPUTER AND TESTED PER MM 22-11-01, TESTED OK.

Part: COMPRESSOR — STALLED (LT ENGINE)

LEFT ENGINE COMPRESSOR STALLED. BLACK SMOKE CAME OUT FROM EXHAUST AT 1,500 FEET. AIRCRAFT RETURNED TO FIELD.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT SLIDE LIGHT INOP AT DOOR 2R. RELAMPED EMERGENCY EXIT SLIDE LIGHT AT DOOR 2R, OPERATION CHECKS NORMAL.

Part: COMPRESSOR BLADE — BROKEN (RT ENGINE)

CREW OBSERVED YELLOW FLASH ACCOMPANIED WITH A LOUD BANG ON RIGHT SIDE OF AIRCRAFT. ABORTED TAKEOFF AT 100 KTS. BORESCOPE REVEALED ENGINE NOT SERVICEABLE. *S/D* FOUR BROKEN 9TH STAGE COMPRESSOR BLADES. SCRAPPED ALL THE 6TH THROUGH 17TH STAGE COMPRESSOR BLADES AND REPLACED WITH NEW.