N582UA

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,639 hrs · 21,672 cycles

EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACKS IAW MM, OPS CHECKED NORMAL.

Part: FITTING — CORRODED (R1 DOOR) · airframe 61,421 hrs · 21,584 cycles

DOOR 1R HANDLE HUB CRACKED FROM CORROSION. DOOR HANDLE FITTING.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 61,421 hrs · 21,584 cycles

PIN MISSING FROM DOOR 1R SLIDE PACK HARNESS. REPLACED DOOR 1R SLIDE ASSY.

Part: PACKING — DAMAGED (HYDRAULIC SYS) · airframe 60,749 hrs · 21,351 cycles

L HYD QTY EICAS. FLUID DROPPED TO .46RF. SECURED L ENG & ELEC PUMPS. LEAK STOPPED. PRESSURIZED LT SYSTEM. FOUND SPRAYING LEAK AT LT ELECTRIC PUMP. REPLACED PACKING AT OUTLET PRESSURE LINE FITTING. REPRESSURIZED SYSTEM - FOUND NO FURTHER LEAKAGE. SERVICED LT SYSTEM TO FULL.

Part: LIFE VEST — MISSING (CABIN) · airframe 60,705 hrs · 21,336 cycles

LIFE VEST MISSING FROM 10C, 11E, 14C AND 18A. INSTALLED VESTS.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 59,895 hrs · 21,050 cycles

EMERGENCY LIGHT AT FWD AFT LAV END CAP MISSING. REPLACED END CAP.

Part: FITTING — LEAKING (OXYGEN MASK) · airframe 57,400 hrs · 20,157 cycles

OBSV OXYGEN MASK STOW BOX O2 FITTING LEAKING. F/O SEAT INOP, LINE IS CAPPED, LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,101 hrs · 20,047 cycles

DR 2R AND DR 4L EXTERIOR EMERGENCY LIGHTS ARE INOP. REPLACED EXTERIOR EMERGENCY EXIT LIGHT LAMPS, OPS CHECK PER MM 33-51-06. CHECK IS OK. WORK IS ACP ON NR 2121N0004.

Part: LIGHT — INOPERATIVE (AFT LAV FLOOR) · airframe 56,276 hrs · 19,749 cycles

EMERGENCY FLOOR LIGHTING AT AFT LAV IS INOPERATIVE. LIGHTING FOUND INOP. REPLACED EMERGENCY LIGHTING SECTION. OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,851 hrs · 19,603 cycles

LT AFT EMERGENCY LIGHT ON STOWBIN BULL NOSE IS INOPERATIVE. RELAMPED, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,479 hrs · 19,472 cycles

EMERGENCY EXIT LIGHTING ON FLOOR AT THE AFT LAV IS INOP. RELAMPED EEL, OPS CHECKS GOOD.

Part: SKIN — CHAFED (TE FLAP) · airframe 55,432 hrs · 19,452 cycles

RIGHT WING INBOARD FLAP, OUTBOARD UPPER EXT SURFACE CHAFED. REMOVED PANEL AND INSTALLED REPAIR REF TIMCO REO-G13112 REV A. RE-INSTALLED PANEL REF SRM 51-40- 02. PERFORMED SPOILER TO FLAP CLEARANCE CHECK, CHECKS GOOD REF MM 27-61-00.

Part: SKIN — CHAFED (TE FLAP) · airframe 55,432 hrs · 19,452 cycles

LEFT WING INBOARD FLAP OUTBOARD UPPER SURFACE CHAFED. REMOVED UPPER PANEL AND REPAIRED REF REO-G13107 REV C. RE-INSTALLED PANEL REF SRM 51-40-02. PERFORMED SPOILER TO FLAP CLEARANCE CHECK, CHECKS GOOD REF MM 27-61-00.

Part: LIGHT — INOPERATIVE (CARGO DOOR) · airframe 55,432 hrs · 19,452 cycles

AFT CARGO DOOR EMERGENCY LIGHT INOP. RELAMPED AFT CARGO DOOR EMERGENCY LIGHT AND OPS CHECK GOOD.

Part: WIRE HARNESS — FRAYED (R1 DOOR SLIDE) · airframe 55,432 hrs · 19,452 cycles

MAIN CABIN R1 DOOR SLIDE HARNESS LOWER CENTER ATTACH POINT FRAYED. REPLACED R1 DOOR SLIDE HARNESS.

Part: WIRE HARNESS — DAMAGED (R4 DOOR SLIDE) · airframe 55,432 hrs · 19,452 cycles

MAIN CABIN R4 DOOR SLIDE WIRE WIRE HARNESS LOWER CENTER ATTACH POINT FRAYED. REPLACED R4 DOOR SLIDE HARNESS.

Part: BEARING — CORRODED (L4 DOOR) · airframe 55,432 hrs · 19,452 cycles

MAIN CABIN DOOR 4L DOOR TORQUE BLEEDING CORROSION FROM BEARING JUST ABOVE COCKING ROD ATTACH POINT. INSTALLED NEW BEARING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,432 hrs · 19,452 cycles

AFT FLOOR EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 54,936 hrs · 19,265 cycles

DOOR 2R SLIDE PRESS IN RED BAND (LOW). SAMC TEXT: DOOR 4R PRESSURE IS FAULTED, 2R CHECKS OK, 4R PRESSURE IS 4-5 NEEDLE WIDTHS TO LEFT OF GREEN BAND. TEMP STABLE FOR APPROX 8 HOURS, A/C ON AIRCRAFT ALL NIGHT. REPLACED SLIDE AT DOOR 4R.

Part: RING — OUT OF POSITION (DOOR 2L) · airframe 54,314 hrs · 19,044 cycles

THE 'D' RING AT DOOR 2L ON WRONG SIDE OF DOOR. SECURED 'D' RING ON CORRECT LOCATION.

Part: BUSHING — WORN (NR1 ENG OIL TANK) · airframe 53,729 hrs · 18,810 cycles

NR 1 ENGINE OIL TANK FWD MOUNT BEARINGS WEDGE FAILED WITH BEARING MIGRATION FWD INTO SUPPORT LUG BUSHING MIGRATION IS ABOUT .100 EVIDENCE OF WEAR IN BUSHING. REMOVED ENG OIL TANK ASSY. REPLACED BUSHINGS. OIL TANK WAS HUNG AND IS IN PLACE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,243 hrs · 18,614 cycles

EXT EMERGENCY LIGHT BY DOOR 1R DOES NOT TEST. REPLACED FWD EEL BATTERY, CHECK OK.

Part: LANYARD — OUT OF POSITION (L3 DOOR) · airframe 53,101 hrs · 18,555 cycles

DOOR 3L WILL NOT ARM. REPOSITIONED MOORING LANYARD & OPS CHECKED GIRT BAR OPERATION.

Part: LANYARD — OUT OF POSITION (L3 DOOR) · airframe 53,101 hrs · 18,555 cycles

DOOR 3L WILL NOT ARM. REPOSITIONED MOORING LANYARD & OPS CHECKED GIRT BAR OPERATION.

Part: LANYARD — OUT OF POSITION (L3 DOOR) · airframe 53,101 hrs · 18,555 cycles

DOOR 3L WILL NOT ARM. REPOSITIONED MOORING LANYARD & OPS CK'D GIRT BAR OPERATION.

Part: UNKNOWN — SMOKE (CABIN) · airframe 52,701 hrs · 18,415 cycles

CREW REPORTS ELEC SMELL IN CABIN WHILE BEING DEICED ( NOT DEICING FLUID SMELL). CAPT REPORTS A HEAVY BLACK SMOKE MOST PRONOUNCED BETWEEN DOOR 2 AND THE FIRST OW HATCH. CKD AND OPERATED ALL INTERIOR CABIN ITEMS, REMOVED CEILING PANELS, CKD WIRING AND DUCTS. RAN APU, ENGS WITH DIFFERENT PACK CONFIGURATIONS. CKD CARGO PITS AND NESTING SYS ALONG WITH ALL CB. NO SMELL OR SMOKE NOTED. ORIGIN CANNOT BE DUPLICATED.

Part: DOOR — LACK OF LUBE (L3 DOOR) · airframe 52,202 hrs · 18,231 cycles

DOOR 3L WILL NOT ARM. LUBED DOOR, REMOVED SMALL AMOUNT OF ICING.

Part: SIGN — DISLODGED (RT OVERWING) · airframe 51,271 hrs · 17,890 cycles

RIGHT OVERWING EXIT SIGN FELL OFF. *S/D* REPLACED RT WING EXT COVER. SYSTEM IS NORMAL.

Part: LIGHT — LOOSE (ROW 34) · airframe 49,789 hrs · 17,355 cycles

EXIT PATH LIGHTING FROM ROW 34 BACK IS LOOSE. RESECURED EEL STRIP.

Part: LINE — DISCONNECTED (DOOR ASSIST) · airframe 48,622 hrs · 16,949 cycles

EMERGENCY POWER RESERVOIR LINE WAS NOT CONNECTED TO DOOR ASSIST PRESSURE BOTTLE DOOR 2R.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,622 hrs · 16,949 cycles

DOOR 2R AND RIGHT OVERWING FWD EXTERIOR EMERGENCY LIGHTS INOP, WHEN SELECTED BY EMERGENCY LIGHT TEST ON NLG. RELAMPED.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 48,415 hrs · 16,875 cycles

FLIGHT DIVERTED DUE TO FLAP DISAGREE STATUS MESSAGE. LANDED UNDER AMBER ALERT AND TAXIED TO GATE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,707 hrs · 16,256 cycles

EMERGENCY SLIDE LIGHT INOP AT DOOR 4L. *S/D* RELAMPED WITH 767 LAMP.

Part: EXTINGUISHER — LEAKING (AFT CABIN) · airframe 46,040 hrs · 16,012 cycles

AFT WATER FIRE EXTINGUISHER APPEARS TO BE LEAKING. REPLACED WATER FIRE EXTINQUISHER.

Part: MODULE — MALFUNCTIONED (SPOILER SYSTEM) · airframe 45,379 hrs · 15,747 cycles

EICAS MESSAGE 'SPOILERS' DISPLAYED DURING CLIMB. SPOILERS LIGHT ILLUMINATED WITH SPEEDBRAKE LEVER SELECTED TO DOWN. FOUND SAME SPOILER CONTROL MODULE FAULTS AS BEFORE: 3L HAD PCA AND MOD FAULT BALLS.

Part: ODOR — DETECTED (GALLEY) · airframe 44,563 hrs · 15,445 cycles

ELECTRICAL SMELL IN FWD GALLEY. NO SOURCE FOUND AFTER A THOROUGH CHECK OF GALLEY WIRING, LIGHT BALLAST, OVENS, COFFEE MAKERS, HOT PLATES AND OTHER EQUIPEMENTS. SMELL CLEARED WHEN RIGHT RECIRC FAN SET TO ON. NO CONCLUSIVE REASONS CAN BE REPORTED FOR THIS INCIDENT. NO REPORT OF ANY RECURRENCE.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR) · airframe 43,447 hrs · 15,043 cycles

ELEV ASYM EICAS MESSAGE IS DISPLAYED. THE FAILED ELEVATOR ASYMMETRY LIMITER ACTUATOR WAS DETECTED BY THE STABILIZER TRIM/ELEVATOR ASYMMETRY MODULE (SAM). A DISCREPANCY IN THE ACTUATOR FAULT LOGIC CAUSES THE ELEV ASYM STATUS /MAINTENANCE MESSAGES TO DISPLAY. REMOVED AND REPLACED THE SUBJECT LIMITER ACTUATOR WITH NEW SERVICEABLE UNIT. SYSTEM WAS OPS CHECKED PER MM 27-31-03 WITH NO FAULTS OR DISCREPANCIES FOUND. THIS ITEM TO BE TREATED AS A ONE-TIME ISOLATED INCIDENT. THERE IS NO SIGNIFICANT HISTORY OF MAINTENANCE FAILURES FOR THIS COMPONENT. ENGINEERING WILL MONITOR FUTURE RELATED DISCREPANCIES AND, IF REQUIRED, MODIFY THE EXISTING MAINTENANCE PROGRAM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

DOOR 4L AFT FRAME CORROSION AT STA 1681 BOTTOM OF STR 17L. DAMAGE CAUSED BY TYPICAL FLOOR STRUCTURE CORROSION. DAMAGE WAS REMOVED AND REPAIR ANGLES WERE FABRICATED AND INSTALLED.

Part: SHEAR WEB — CORRODED (FUSLEAGE) · airframe 39,363 hrs · 13,587 cycles

SHEAR WEB STA 1700 CORRODED FROM RBL 8 TO RBL 38. DAMAGE CAUSED BY TYPICAL AFT PRESSURE DECK WEB CORROSION. CORROSION WAS REMOVED AND THE WEB WAS REPAIRED USING DOUBLERS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

STA 620 BETWEEN STR 16L AND 17L HAS HOLE DAMAGE. HOLE DAMAGE CAUSED DURING INSTALLATION OF AN EXTERNAL FUSELAGE SKIN REPAIR. SHEAR TIE WAS REMOVED, A REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

EXTERNAL FUSELAGE SKIN HAS MULTIPLE REPAIRS BS 550 TO BS 630 STR 14L-19L. ORIGINAL DAMAGE CAUSED BY JETWAY IMPACT. MULTIPLE TIME-LIMITED REPAIRS WERE REMOVED AND A PARTIAL SKIN REPLACEMENT WAS ACCOMPLISHED. CONSTANT THICKNESS SKIN SECTION WAS SPLICED IN USING DOUBLER STRAPS AND TRIPLERS.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

SHEAR TIES AT STA 580 BETWEEN STRINGERS 15L-16L, 16L-17L, AND 17L TO 18L HAVE HOLE DAMAGE. HOLE DAMAGE CAUSED DURING INSTALLATION OF EXTERNAL FUSELAGE SKIN REPAIR. SHEAR TIES WERE REMOVED, NEW SHEAR TIES WERE FABRICATED AND INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT AT STA 1540, APPROX AT STR 26R FRAME IS DENTED ON THE INBOARD FLANGE. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1580 FRAME DENTED ON INBOARD FLANGE AT STR 26R. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1440, STR 26L FRAME INBOARD FLANGE IS DENTED. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1480 AT STR 26L, FRAME IS DENTED ON INBOARD FLANGE. FRAME FLANGE WAS REPAIRED BY EXTENDING THE EXISTING SPLICE ANGLE TO REPAIR THE DAMAGED FLANGE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1280, STR 28L TO 29L FRAME SHEAR TIE IS CORRODED. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1460 AT STR 26L FRAME IS DENTED ON INBOARD FLANGE. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1620, STRINGER 29L, LONGERON SPLICE HAS CORROSION BEYOND LIMITS. DAMAGE CAUSED BY CORROSION. REMOVED CORRODED STRINGER SPLICE AND INSTALLED NEW STRINGER SPLICE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT FRAME IS DENTED 3 EA PLACES ON INBOARD FLANGE AT BS 1420, BETWEEN STR 23L AND 26L. FRAME FLANGE WAS REPAIRED BY EXTENDING THE EXISTING SPLICE ANGLE TO REPAIR THE DAMAGED FLANGE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

BS 365 FLOORBEAM CORRODED BEYOND LIMITS BETWEEN RBL 59 TO BL 0. TEE CAP WAS TRIMMED AND REPAIR ANGLES AND STRAPS WERE USED TO SPLICE IN NEW SECTION OF TEE CAP.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

SHEAR WEB AT STA 1680, RBL 74 IS CORRODED. REPAIR DOUBLERS WERE INSTALLED TO REPAIR THE AFT PRESSURE DECK WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 1380 AND 1400 RT SIDE. DAMAGE CAUSED BY CORROSION TYPICAL FOUND ON CREASE BEAMS. CREASE BEAM WEB REPLACEMENT WAS FABRICATED AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1620, RBL 2 SHEAR TIE HAS CORROSION. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

PIT SHEAR TIE HAS CORROSION, STA 1600, LBL 9. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1440 SHEAR TIE CORRODED BETWEEN STR 29L AND 30L. A REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

CABIN FLOORBEAM HAS CORROSION ON UPPER TEE CAP STA 324, RBL 46 - 59. TRIMMED TEE CAP AND INSTALLED ANGLE AND STRAP REPAIR FOR TEE CAP SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

FLOORBEAM STA 1640, RBL 44- 48 CORRODED. DAMAGED FLOOR BEAM WAS REMOVED AND A REPAIR USING SPLICE STRAPS AND ANGLES WAS INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,363 hrs · 13,587 cycles

AFT PIT STA 1520, RBL 11, SHEAR TIE CORRODED. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,476 hrs · 13,255 cycles

AFT LWR FUSELAGE SKIN DAMAGED BETWEEN STA 1393 AND 1420. DAMAGE CAUSED BY CARGO LOADER. DENTS AND CREASES REMOVED FROM THE FUSELAGE SKIN IN TWO SECTIONS. ONE EXISTING SKIN DOUBLER WAS REMOVED AND REPLACED WITH LARGER DOUBLER TO INCORPORATE ONE SECTION OF NEW DAMAGE. AN ADDITIONAL DOUBLER AND SPLICE DOUBLER WAS INSTALLED OVER REMAINING DAMAGED SECTION. SPLICE DOUBLER SPLICES AN EXISTING SKIN DOUBLER AND THE NEW SKIN DOUBLER.

Part: IDG — FAILED (LEFT) · airframe 37,430 hrs · 12,910 cycles

LEFT GENERATOR DRIVE LIGHT ILLUMINATED. LEFT AC INTEGRATED DRIVE GENERATOR (IDG) FAILED. REPLACED LEFT IDG. SHOP FINDINGS: HYDRAULIC MOTOR/PUMP GEAR FAILURE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,419 hrs · 12,906 cycles

FUSELAGE SKIN SPLICE STRAP BODY STATION 1400 BETWEEN STR 27L & STR 30L WAS FOUND CORRODED. FRAME AT BS 1460 AND RBL 5.6 TO LBL 14.5 WAS FOUND CORRODED. *S/D* MAJOR REPAIRS ACCOMPLISHED. J-CHANNELS INSTALLED ON THE FRAME. EXTERNAL DOUBLER INSTALLED ON SKIN SPLICE STRAP. INTERCOSTALS AND SHEAR TIES REPLACED.

Part: SPLICE — CORRODED (FUSELAGE SKIN) · airframe 37,419 hrs · 12,906 cycles

SKIN SPLICE STRAP AT STA 1400 CORRODED BETWEEN STRINGERS 27L AND 30. MAJOR REPAIR ACCOMPLISHED. REPLACED SECTION BETWEEN STR 26L AND 28L AND INSTALLED EXTERNAL DOUBLER CENTERED ON STR 29L.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 33,049 hrs · 11,412 cycles

NR 1 PYLON STRUT OUTBOARD SIDE SKIN IS CRACKED AT FORWARD ACCESS HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH DOUBLERS.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 29,820 hrs · 10,261 cycles

LEADING EDGE SLAT DISAGREE MESSAGE DISPLAYED. THE NUMBER 6 LEADING EDGE SLAT ROTARY ACTUATOR FAILED AND CAUSED SOME BINDING IN THE SLAT. THE BINDING WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT WHICH SUBSEQUENTLY SHUT DOWN THE SYSTEM AS FAILURE PROTECTION. THE NUMBER 6 SLAT ACTUATOR WAS REPLACED AND OPERATIONALLY CHECKED GOOD.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 29,819 hrs · 10,260 cycles

LEADING EDGE SLAT DISAGREE MESSAGE DISPLAYED. THE NUMBER 6 LEADING EDGE SLAT ROTARY ACTUATOR FAILED AND CAUSED SOME BINDING IN THE SLAT. THE BINDING WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT WHICH SUBSEQUENTLY SHUT DOWN THE SYSTEM AS FAILURE PROTECTION. THE NUMBER 6 SLAT ACTUATOR WAS REPLACED AND OPERATIONALLY CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,611 hrs · 9,456 cycles

FUSELAGE SKIN DENTED AT STA 600 TO 620 STR 16 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: WIRE — DAMAGED (GALLEY) · airframe 26,888 hrs · 9,185 cycles

ELECTRICAL SPARKS SEEN IN REAR GALLEY. *S/D* N43 CABLE FROM CONTROLLER TO CART WAS CRUSHED AND CABLE WAS DISCONNECTED FROM CONTROLLER CAUSING SPARKS IN THE REAR GALLEY. CABLE AND PIGTAIL DISCONNECT WERE REPLACED.

Part: ASSIST BOTTLE — RUPTURED (4 RT DOOR)

DOOR ASSIST BOTTLE FOR DOOR NR 4 RT FOUND EMPTY. REPLACED DOOR ASSIST BOTTLE AND ISOLATED CAUSE AS MATERIAL DEFECT. UAL HAS A RECOVERY PLAN AND IS CORRECTING.