N26123

Part: LIGHT — UNKNOWN (CABIN) · airframe 75,624 hrs · 18,734 cycles

DOOR 1R SLIDE LIGHT NOT ILLUMINATED WITH DOOR ARMED UNABLE TO DUPLICATE. NORMAL CONDITION VERIFIED.

Part: COVER — LOOSE (R1 DOOR SENSOR) · airframe 75,624 hrs · 18,734 cycles

DOOR 1R SLIDE LT NOT ILLUMINATED WITH DOOR ARMED ON TAXI IN. FOUND FWD SENSOR COVER LOOSE, SECURED .

Part: STRAP — FRAYED (R1 DOOR) · airframe 75,251 hrs · 18,650 cycles

R1 EMERGENCY SLIDE SUPPORT Y STRAP, FRAYED/DAMAGED. REMOVED SLIDE AND INSTALLED NEW STRAP, REINSTALLED SLIDE IAW MM 25-66-01-404-044. OPS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 75,159 hrs · 18,630 cycles

PER 2SVC, FOUND EMERGENCY LITE AT 1EF STOW BIN NOT SECURED. EMERGENCY LIGHT AT 1EF IS SECURED.

Part: SWITCH — FAULTY (L1 DOOR LIGHT) · airframe 74,651 hrs · 18,522 cycles

L1 DOOR SLIDE LIGHT IS INOPERATIVE WHEN DOOR IS ARMED. R & R THE L1 DOOR SLIDE LIGHT SWITCH IAW SWPM 20-20-00. SYS OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 74,614 hrs · 18,515 cycles

SLIDE LIGHT ABOVE DOOR 1L DOES NOT ILLUMINATE WHEN DOOR ARMED. RELAMPED SLIDE LIGHT OPS CHECK OK.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 74,468 hrs · 18,489 cycles

DOOR 1L SLIDE LIGHT REMAINS ILLUMINATED WITH DOOR DISARMED. CHECKED GIRT BAR PROX SENSOR AND TARGET FOR SECURITY CYCLED ARMING HANDLE MULTIPLE TIMES COULD NOT DUPLICATE NO DEFECTS NOTED OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 72,949 hrs · 18,194 cycles

DOOR-MOUNTED ESCAPE SYSTEM DOOR 1L, GIRT BAR ENGAGEMENT LIGHT OFF WITH EVACUATION SLIDE ARMING LEVER IN ARMED/ENGAGE POS AT ENTRY /SERVICE DOOR. RELAMPED CKS NORMAL.

Part: STIFFENER — GOUGED (BS 158) · airframe 66,666 hrs · 16,932 cycles

VERTICAL STIFFENER GOUGED ON RIGHT FORWARD SPAR APPROXIMATELY FSS 158. REMOVED DAMAGED STIFFENER, FABRICATED & INSTALLED NEW STIFFENER IAW DWG 112N2038 & DWG 112N2002.

Part: FRAME — CORRODED (BS 1380 BULKHEAD) · airframe 66,666 hrs · 16,932 cycles

CORROSION ON INNER CHORD OF FRAME STATION 1380 AT STRINGER 27R, BOTTOM SIDE. INSTALLED REPAIR AT STATION 1380 IAW ECRA 5310-06554.

Part: INTERCOSTAL — CORRODED (BS 1360-1380) · airframe 66,666 hrs · 16,932 cycles

INTERCOSTAL ON STRINGER 27R, STATION 1360 - 1380 IS CORRODED AT AFT CORNER. R & R INTERCOSTAL 146N8515-2 & TIE DOWN FITTING ASSEMBLY 146N5442-2 IAW DWG 146N5421, SRM 51-40-02 & ECRA 5310-06554.

Part: SKIN — GOUGED (BS 1809) · airframe 66,666 hrs · 16,932 cycles

DAMAGE WAS A GOUGE AT LEFT FUSELAGE SKIN BELOW LEFT HORIZONTAL STABILIZER. INSTALLED REPAIR PARTS & APPLIED CORROSION INHIBITING COMPOUND TO INSIDE OF REPAIR AREA AT LEFT FUSELAGE LOWER FAIRING SKIN COMMON TO HORIZONTAL STAB LOWER BLADE SEAL APPROXIMATELY STATION 1809 IAW SRM 53-80-70 REPAIR 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

CABIN FRAME CRACKED AT STATION 760 AT PSU RAIL BRACKET INBD FASTENER BETWEEN STRINGER 7R & 8R. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

BELL FRAME AT BS 1580 HAS CRACK AT INBD FASTENER LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8L & 9L. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

FORWARD WET AREA, STATION 345 FLOORBEAM IS CORRODED FROM BL0 - 24L. REPAIRED FLOORBEAM UPPER CAP STATION 345 BETWEEN LBL 58 & RBL 60 IAW SRM 53-00-51 REPAIR 10 & ECRA 5310-06539.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

BELL FRAME AT BS 1540 HAS CRACK AT INBD FASTENER, LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8R & 9R. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

BELL FRAME AT BS 1580 HAS CRACK AT INBD FASTENER, LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8R & 9R. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

BELL FRAME AT BS 1540 HAS CRACK AT INBD FASTENER LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8L & 9L. INSTALLED REPAIR IAW SRM 53-00-07 REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

MID WET AREA, STATION 720 FLOORBEAM IS CORRODED, BETWEEN RT INBD & OTBD SEAT TRACKS. REPAIRED MID WET AREA IAW ECRA 5310-06546 & SRM 53-00-51.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

CABIN FRAME CRACKED STATION 760 AT PSU RAIL & BRACKET INBD FASTENER BETWEEN STRINGER 7L & 8L. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 1 PAR 4 STEPS A - S. IMITATED DIP TO PERFORM DETAIL VISUAL INSPECTION 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES FIRST & EVERY 12,000 FLIGHT CYCLES THEREAFTER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

FORWARD WET AREA FLOORBEAM AT STATION 365 FROM BL 0 TO BL 10R IS CORRODED. IAW ECRA 5310-05536 FABRICATED & INSTALLED ALL REPAIR PARTS & ANY ADJACENT STRUCTURE THAT WAS DISPLACED TO FACILITATE REPAIR. CORROSION INHIBITING COMPOUND TO BE APPLIED DURING WET AREA PREP SEQ 370. FLOOR PANEL TO BE INSTALLED ON SEQ 1021.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,666 hrs · 16,932 cycles

FLOORBEAM AT STATION 1640 BETWEEN RBL-54 & RBL-57 CORRODED ON TOP SIDE. REPAIRED FLOORBEAM STATION 1640, LBL 11 - RBL 65 IAW SRM 53-00-51 REPAIR 8.

Part: O2 GENERATOR — DENTED (CABIN) · airframe 65,864 hrs · 16,791 cycles

OXYGEN GEN AT ROW 36 RT DAMAGED. R & R OXYGEN GEN AT ROW 36 RT IAW AMM 35-21-04. OXYGEN GEN CANISTER FOUND DENTED UPON ARRIVAL.

Part: CONNECTOR — SHORTED (CABIN) · airframe 62,914 hrs · 16,227 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 7 - 12 AT PAX SEAT LOCATION FOUND SHORTED LIGHT CONNECTION AT ROW 12ABC, R & R OPERATIONS CHECKED GOOD.

Part: FUSE — SHORTED (BATTERY CHARGER) · airframe 62,914 hrs · 16,227 cycles

EMERGENCY SEAT MOUNTED LIGHTS INOPERATIVE FROM ROW 30 - 40. R & R SHORTED FUSE FROM AFT EMER LIGHT BATTERY CHARGER, OPERATIONS CHECKED GOOD.

Part: CHARGER — FAULTY (CABIN) · airframe 61,033 hrs · 15,880 cycles

TWO HOURS INTO THE FLIGHT MANY OF THE EMERGENCY LIGHTS CAME ON, LT FWD COACH FLOOR LIGHTS, DOOR 2L RT LIGHTS. THE LIGHTS EVENTUALLY EXTINGUISHED, FAULTY EMERGENCY LIGHT BATTERY CHARGER AT DOOR 2L M733. REPLACED CHARGER & BATTERY, REPLACED WEAK BATTERY AT CHARGER M737 AT DOOR 4L. ALL EMERGENCY LIGHTS OPERATE NORMAL.

Part: SWITCH — DIRTY (CABIN) · airframe 60,875 hrs · 15,852 cycles

EMERGENCY EXIT LIGHTS COME ON INTERMITTENTLY AT ROWS 30-35 ABC SIDE ONLY ON OVERHEADS. ROWS 7-28 ON BOTH SIDES WHITE OVERHEADS. ROWS 7-28 BOTTOM EMERGENCY EXIT LIGHTS. DOORS 2L & RT WINDOW EXIT LIGHTS. SWITCH AT FLIGHT ATTENDANT PANEL STICKING. CLEANED SWITCH & OPERATIONS CHECKED OK. .

Part: GOVERNOR — FAILED (FUEL FLOW) · airframe 60,119 hrs · 15,710 cycles

AFTER TAKE OFF, BROUGHT NR 2 ENGINE UP TO 35 PERCENT N1 AN RT ENGINE DIDN`T SPOOL UP. LOW SPEED RTO 5KTS MAX R & AMP; RT FFG IAW MM TASK 73-21-01-004-001-R-04 & TASK 73-21-01-4 04-013-R-04 ON NR 2 ENGINE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 58,997 hrs · 15,506 cycles

EMERGENCY LIGHT BETWEEN SEAT ROWS 19-27 INOPERATIVE. FOUND DAMAGED WIRE AT ROW 26A IN SEAT TRACK. SPLICED IN REPAIR REF WPM 20-13-12, PAGE 69.

Part: LIGHT — INOPERATIVE (FLIGHT DECK) · airframe 56,136 hrs · 14,993 cycles

EMERGENCY EXIT AND AISLE PATH LIGHT SYS ILLUMINATED FIRST TO TALLY AND THEN PARTIALLY THROUGH FRONT AND MID CABINS. THIS WAS NOT COMANDED BY FLIGHT DECK OR FWD GALLEY SWITCH. UNABLE TO EXTINGUISH LIGHTS FOUND EMERGENCY LIGHT SWITCH IN CP WORN. R & R EMERGENCY LIGHTS PAX O2 CONTROL PANEL IAW AMM 33-51-08.

Part: ENGINE — FLAMED OUT (LEFT) · airframe 50,978 hrs · 14,072 cycles

LEFT ENGINE FLAME OUT ON TAXI IN. AIRCRAFT BEHIND US REPORT FIRE IN LEFT ENGINE. NO COCKPIT INDICATIONS, SHUT ENGINE DOWN. T/S PER FIM TASK 71-05-00-815-806-ROO, REMOVED LP FUEL FIL BOWL NO WTR. NOTED. REMOVED HP FUEL FIL NO CONTAMINATION FOUND. RE- PLACED FUEL FIL. PERFORMED POWER ASSURANCE CHECK ALL PARAMETERS NORMAL. LEAK CHECKS GOOD. REF AMM 73-11-10/601 AND 73-11-12/401 A/C OK FOR SERVICE. ALSO PERFORMED BVCU AND TPU BITE ALL TEST PASSED.

Part: D-RING — OUT OF POSITION (L4 DOOR) · airframe 49,292 hrs · 13,726 cycles

THE 4L DOOR WILL NOT ARM. FOUND "D" RING STUCK IN ARMIN LINKG.RISTALT "D" RING STRAP. DOOR ARMS OPERATE NORMALLY. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 43,883 hrs · 12,615 cycles

FRAME AT STATION 1480 STRINGER 25RT-23RT HAS TOOLING MARKS ON TOP OF FRAME. INSTALLED REPAIR DOUBLER PER EC/RA 5310-04993, PART 1. INITIATED DIP TO REINSPECT FRAME REPAIR AT STA 1480, S-26R AT OR PRIOR TO 50000 TOTAL AIRCRAFT FLIGHT CYCLES AND INTERVALS NOT TO EXCEED 12000 FLIGHT CYCLES THEREAFTER PER EC/RA5310-04993 PART 2.

Part: HOUSING — SHORTED (EVAC LIGHT) · airframe 37,977 hrs · 11,432 cycles

EMERGENCY LAMPS AT OVERWING THAT SHINE DOWN ON HANDLES OF OVERWING EMERGENCY DOORS, LOCATED AT FWD POST - LEFT OVERWING BOTH DOORS AND AFT RIGHT OVERWING FWD LAMP ARE OUT, REPLACED BULBS, NO HELP. FOUND LIGHT ASSY AFT LEFT OVERWING SHORTING OUT AND BLOWING FUSE AT M10568 W/D 33-51-13 PG 2. REPLACED LIGHT HOUSING ASSY P/N 11- 5832-11 IPC 33-51-51-50 ITEM 45. REPLACED FUSE AT BATTERY CHARGER, OPS CHECKS GOOD.

Part: MONITOR — INOPERATIVE (ROW 17ABC) · airframe 27,656 hrs · 9,099 cycles

A STRONG ELECTRICAL SMELL WAS NOTICED IN THE CABIN AND THEN THE LCD VIDEO SCREEN AT ROW 17 ABC BLANKED OUT WHILE EN ROUTE TO LAX. THE POWER TO THE ENTERTAINMENT SYSTEM WAS REMOVED AND THE SMELL DISSIPATED. THE FLIGHT WAS CONTINUED TO LAX WHERE IT LANDED WITHOUT FURTHER PROBLEMS. THE LCD VIDEO MONITOR WAS FOUND AT FAULT. THE MONITOR WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 23-32-08, PAGE 401. IN ADDITION, THE ASSOCIATED WIRING WAS INSPECTED IAW MM 20-60-04, PAGE 201 AND NO DEFECTS WERE NOTED.

Part: SKIN — CORRODED (STA 1510) · airframe 19,397 hrs · 6,153 cycles

INSPECTION FOUND FUSELAGE SKIN AT STA 1510 UNDER L/H AFT AIRPHONE ANTENNA CORRODED. INSTALLED REPAIR IAW SRM 53-00-01, FIGURE 204.

Part: CHARGER — FAILED (CABIN) · airframe 16,610 hrs · 5,163 cycles

INSPECTION FOUND R-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW FIM 33-51-00.