N591NW

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 74,639 hrs · 24,818 cycles

SHIP 5811 ROW 24-27 EEPLS INOP AND RH LWR EMERG EXIT SIGN INOP. R/R BATTERY AND CHARGER ASSY M11488 REF B757 AMM 33-51 OPS GOOD ALSO REPLACED BATT AT M11384 REF B757 AMM 33-51 OPS GOOD. (7512992)

Part: OVEN — FIRE (ZONE 900) · airframe 74,370 hrs · 24,711 cycles

SHIP 5811 -DIV/FIRE/DE- TO ATL DUE TO REPORTED FIRE FROM FORWARD GALLEY OVEN WITH ELECTRICAL SMELL. CORRECTIVE ACTION: INSPECTED LIGHTS, BALLASTS, GALLEY WIRE HARNESS, COFFEE MAKERS AND OVENS. REPLACED FORWARD GALLEY OVENS 1 AND 2 AND COFFEEMAKERS 1 AND 2.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 74,285 hrs · 24,675 cycles

SHIP 5811 EMERGENCY EXIT ISLE LIGHTS OUT AT SEAT 24, 25, 26. CORRECTIVE ACTION: REPLACED PWR SUPPLY M11488 REF B-757 AMM 33-51 OPS CHECK GOOD. (7137156)

Part: GIRT BAR — OBSTRUCTED (ZONE 800) · airframe 74,274 hrs · 24,671 cycles

SHIP 5811 L4 DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND LANYARD FOULED GIRT BAR. REMOVED AND STOWED AS REQD. OPS NRML, REF B757 AMM 52-11. (7137148)

Part: SENSOR — OUT OF LIMITS (ZONE 800) · airframe 74,232 hrs · 24,657 cycles

SHIP 5811 R AFT ENTRY DOOR EICAS MESSAGE WITH ASSOCIATED DOORS LIGHT WAS INTERMITTANTLY APPEARING WHILE ON DESCENT AND ON APPROACH. CORRECTIVE ACTION: TROUBLESHOT PER B757 FIM 52-71. FOUND CLEARANCE AT OUTER EDGE OF LIMITS FOR TARGET AND SENSOR. ADJUSTED JAM NUT TO MIDDLE OF LIMITS, 0.093", PER B757 AMM 52-71-00-825-001. OPS CHECK GOOD. (7137134)

Part: GIRT BAR — FOD (ZONE 800) · airframe 74,076 hrs · 24,597 cycles

SHIP 5811 L4 WILL NOT ARM. CORRECTIVE ACTION: RMVD DEBRIS FROM GIRT BAR MOUNTS OPS CK GOOD. (6529284)

Part: BOTTLE — LOW (LIFE RAFT) · airframe 73,873 hrs · 24,515 cycles

SHIP 5811 ON SVC CVK FOUND AFT LIFE RAFT LOW PSI. CORRECTIVE ACTION: R/R AFT LIFE RAFT IAW B757 AMM 25-64. (6836362)

Part: INDICATOR — OUT OF ADJUST (ZONE 800) · airframe 73,384 hrs · 24,309 cycles

SHIP 5811 4R DOOR WILL NOT FULLY ARM. CORRECTIVE ACTION: T/S PER B757 FIM 52-11-20-825-001. CLEARED OBSTRUCTION IN GIRT BAR PATH AND ADJUSTED 4R DOOR KNUCKLE KNOCKER PER B757 AMM 52-11 -20. OP CHK NORMAL. (6553344)

Part: SIGN — MISSING (OVERWING EXIT LI) · airframe 73,309 hrs · 24,277 cycles

SHIP 5811 RIGHT OVERWING HORIZONTAL EXIT SIGN IS MISSING. CORRECTIVE ACTION: INSP AND FOUND THE FWD LENS TABS BROKEN. REPLACED THE RIGHT OVERWING EXIT SIGN LENS PER B757 AMM REF 33-51. OPS CKS NORMAL. (6467096)

Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 73,223 hrs · 24,241 cycles

SHIP 5811 4R DOOR LEVER NOT ENGAGING COMPLETELY FOR DISARM AND KNUCKLE KNOCKER NOT FULLY ENGAGING. CORRECTIVE ACTION: THAWED DOOR 4R. PERFORMED ARMING/DISARMING OF THE 4R DOOR PER B757 AMM 25-66. GIRT BAR, KNUCKLE KNOCKER AND SLIDE LIGHT OPS CKS NORMAL. (6467068)

Part: GIRT BAR — OUT OF LIMITS (ZONE 800) · airframe 73,143 hrs · 24,203 cycles

SHIP 5811 A.D. A.A. L4 DOOR GIRT BAR OUT OF LIMITS PER AMDS 2561-01257-01E STEPS 12 AND 14. CORRECTIVE ACTION: SUMMARY OF NRC 00019: GIRT BAR AT L4 DOOR WAS REPLACED PER B757-300 AMM 25-66-10 AND GIRT BAR LIMITS TEST WAS PERFORMED PER AMDS. (0647959)

Part: GIRT BAR — OUT OF LIMITS (ZONE 800) · airframe 73,143 hrs · 24,203 cycles

SHIP 5811 A.D. A.A. R1 DOOR GIRT BAR OUT OF LIMITS PER AMDS 2561-01257-01B STEPS 12 AND 14. CORRECTIVE ACTION: SUMMARY OF NRC.00018: GIRT BAR AT R1 DOOR WAS REPLACED BY SERVICEBLE GIRT BAR, MEASURE OF MINIMUM ENGAGEMENT WAS PERFORMED AND APLICABILITY WAS VERIFY PER B757-300 IPC 25-66-05. SEVICEABLE GIRT BAR WITHIN LIMITS. (0647830)

Part: SLIDE — UNLACED (ZONE 800) · airframe 73,143 hrs · 24,203 cycles

SHIP 5811 UNLACED LEFT OVERWING SLIDE FUS. CORRECTIVE ACTION: SUMMARY OF NRC 00111: LH OVERWING SLIDE WAS REPLACED UNDER AMDS 5200-8346 AND SCEPTRE LOG. (0647582)

Part: STRAP — CRACKED (ZONE 200) · airframe 73,143 hrs · 24,203 cycles

SHIP 5811 CRACK STABILIZER STRAP STA. 377 AND LBL 24 AT E/E COMPARTMENT CEILING AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00225: STABILIZER STRAP STA. 377 AND LBL 24 AT E/ E COMPARTMENT CEILING AREA WAS REPAIRED PER B757-300 SRM 53-00- 51-2R PROCEDURE 12. (0645608)

Part: GIRT BAR — OUT OF LIMITS (L2 DOOR) · airframe 73,143 hrs · 24,203 cycles

SHIP 5811 A.D. A.A. L2 DOOR GIRT BAR OUT OF LIMITS PER AMDS 2561-01257-01C STEPS 12 AND 14. CORRECTIVE ACTION: SUMMARY OF NRC 00021: GIRT BAR AT L2 DOOR WAS REPLACED BY SERVICEABLE GIRT BAR, MEASURE MINIMUM ENGAGEMENT WAS PERFORMED UNDER AD, A.A 2561-01257-01C STEP 12 AND 14, AND APPLICABILITY WAS VERIFY PER. B757-300 AIPC 25-66-05- 05 ITEM 110W, AND MEASURE OK. (0643223)

Part: GIRT BAR — OUT OF LIMITS (R2 DOOR) · airframe 73,143 hrs · 24,203 cycles

SHIP 5811 A.D. A.A. R2 DOOR GIRT BAR OUT OF LIMITS PER AMDS 2561-01257-01D STEPS 12 AND 14. CORRECTIVE ACTION: SUMMARY OF NRC 00020: GIRT BAR AT R2 DOOR WAS REPLACED BY SERVICEABLE GIRT BAR, PER B757-300 AIPC 25-66- 05-05 ITEM 110W. GIRT BAR AT R2 DOOR WAS INSTALLED PER AD, 2561- 01257-01D MEASURES WITHIN LIMITS. (0644401)

Part: COVER — DETACHED (ZONE 200) · airframe 72,583 hrs · 24,028 cycles

SHIP 5811 PLASTIC EMER DOOR EXIT SIGN COVER FELL OFF. RIGHT SIDE AIRCRAFT. CURRENTLY IN OVERHEAD BIN. CORRECTIVE ACTION: REINSTALLED EMER DOOR EXIT SIGN COVER OVER R3 DOOR PER B757 AMM 33-51. OPS CHECK GOOD. (5582928)

Part: FUEL CONTROL — FLUCTUATES (ENGINE) · airframe 72,434 hrs · 23,979 cycles

SHIP 5811-DIV/DE- DIVERSION TO PHX DUE TO LEFT ENGINE EPR AND N1 FLUCTUATION UNABLE TO CONTROL WITHOUT REDUCED THRUST. CORRECTIVE ACTION: REPLACED FUEL CONTROL UNIT, R/R SVA RODEND, R/R 14 STG CONV VLV, ALL TEST PASS.

Part: TRANSMISSION — FAULTED (FLAP SYS) · airframe 72,340 hrs · 23,947 cycles

SHIP 5811 -FCNT/DE- DUE TO FLAP LOCK OUT ON APPROACH. CORRECTIVE ACTION: T/S FOUND RT AND LT O/B TORQUE LIMITER POPPED. R/R #8 FLAP SKEW SENSOR, R/R RT AND LT O/B FLAP TRANSMISSIONS. OPS CK GOOD.

Part: INDICATOR — INOPERATIVE (L2 DOOR SLIDE) · airframe 72,107 hrs · 23,871 cycles

SHIP 5811 2L DOOR ESCAPE SLIDE ARMED CONDITION INDICATOR (KNUCKLE KNOCKER) INOP CORRECTIVE ACTION: ADJUSTED 2L DOOR LOWER LINING PER B757 AMM 52-11. OPS CHECK GOOD. (0415024)

Part: LIGHT — INOPERATIVE (SEAT ROW 32D) · airframe 71,716 hrs · 23,742 cycles

ON SERVICE CHECK FOUND OVERHEAD EMERGENCY LIGHT 32D INOP. CORRECTIVE ACTION: R/R CONNECTOR IAW B757 WDM 33-51 OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,673 hrs · 23,356 cycles

SHIP 5811 BEFORE PUSHBACK R FWD ENTRY DOOR WOULD NOT CLOSE AND ARM. CORRECTIVE ACTION: CYCLED DOOR, NO TROUBLE FOUND. (8392930)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,127 hrs · 23,141 cycles

SHIP 5811 -MISC/DE- DUE TO LEADING EDGE SLAT DISAGREE ON APPROACH. CORRECTIVE ACTION: COMPLETED FIM TASK, CLEARED FAULTS, FLAPS/SLATS OPS CHECK COMPLETED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,032 hrs · 23,106 cycles

SHIP 5811 FIRST CLASS MONITORS AT SEATS 1 C&D, 2 C&D, AND 3 C&D FAILED. AN ELECTRICAL BURNING SMELL WAS OBSERVED WHICH QUICKLY DISSAPATED. CORRECTIVE ACTION: REMOVED AND REPLACED DATA HARNESS. REMOVED AND REPLACED SEB TO SDU HARNESS. JUMPED IN HARNESS. SEB TOOK DATA, READDRESS PASSED. SEATS 1CD-3CD OPS CHK NML. REMOVED HARNESS, INSTALLED PER ERA 612988-14. 1CD-3CD OPS CHK NML WORK IAW B757 AMM 23-32. (9628728)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,615 hrs · 22,677 cycles

SHIP 5811 EXIT SIGN ON BACK OF OVERHEAD SIGN MISSING NEAR DOOR 3 L/R. CORRECTIVE ACTION: RE-ATTACHED EXIT SIGN NEAR DOOR 3. OPS CK NML. (4745612)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,288 hrs · 22,580 cycles

SHIP 5811 LEFT AFT OVERWING EMERGENCY EXIT COVER LOOSE CAUSING LOUD VIBRATION AND CUSTOMER CONCERNS. CORRECTIVE ACITON: RESECURED LOOSE EMERG EXIT SIGN COVER AND TIGHTENED TRIM PIECE. (9492884)

Part: FRAME — CRACKED (BS 1640) · airframe 67,548 hrs · 22,282 cycles

SHIP 5811 A.A. A.D. CRACKS ON BS 1640 FUSELAGE FRAME LEFT AS FOLLOW: ON UPPER OUTBOARD HOLE OF OUTER CHORD AND FRAME AT 03:00 AND 9:00 O CLOCK POSITION, ON UPPER INBOARD HOLE OF FRAME AT 03:00 AND 9: 00 O CLOCK POSITION. CONTACT LIAISON ENGINEERING FOR REPAIR INSTRUCTIONS. REPAIR MUST BE COMPLETED PRIOR TO FURTHER FLIGHT. REF WORK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00175: TEE CLIP WAS REPLACED PER PRI ER/A 605108- 14 REV 0,1,2 AND ER/A 605108-14AD REV ORIGINAL SECTION I PERMANENT REPAIR. (2598028)

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 67,548 hrs · 22,282 cycles

GOUGE ON UPPER SKIN AT LH HORIZONTAL STABILIZER BETWEEN STA128.248/STA152.248 AND REAR SPAR. GOUGE ON UPPER SKIN AT LH HORIZONTAL STABILIZER BETWEEN STA128.248/STA152.248 AND REAR SPAR WAS REPAIRED PER PRI 605415-14 REV 0, REV 1 AND ER/A 605415-14 REV ORIGINAL SECTION I: PERMANENT REPAIR.

Part: NONE — NONE (NONE) · airframe 67,548 hrs · 22,282 cycles

SHIP 5811 DTE, ERA 605415-14, MONITOR INSPECTION LOG REPAIR TO LH HORIZONAL STABILIZER UPPER SKIN, AT STAB STA 128 AND S2. CORRECTIVE ACTION: REF ERA 605415-14.

Part: NONE — NONE · airframe 67,548 hrs · 22,282 cycles

SECTION II REPAIR TO LH WING DRY BAY BARRIER AT WSTA 258.65- 313.50 REQUIRES SECTION III REPAIR WITHIN 24 MONTHS PER ERA 588939-14 REV A. REV ERA 588939-14 REV A.

Part: SNUBBER — OUT OF LIMITS · airframe 67,548 hrs · 22,282 cycles

SHIP 5811 PERFORMING AMDS, ROTARY SNUBER PIN EXTENSION IS OUT OF LIMITS IN R4 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00130: ROTARY SNUBBER 4R DOOR WAS REPLACED PER B757-300 AMM 52-11-10 AND 4R DOOR WAS REMOVED AND INSTALLED PER B757-300 AMM 52-11-01. (2592338)

Part: GIRT BAR — UNSERVICEABLE · airframe 67,548 hrs · 22,282 cycles

SHIP 5811 AD RELATED: INITIAL INSPECTION: GIRT BAR LEAF SPRINGS 2 E/A DOES NOT RETAIN THE SLIDERS OF R2 DOOR (NEED REPLACE GIRT BAR PER AMM 25-66-10-201 AND PERFORM CARD INSTRUCTIONS. CORRECTIVE ACTION: SUMMARY OF NRC 00057: GIRT BAR WAS REPLACED PER B757-300 AMM 25- 66-10 AND CARD INSTRUCTIONS STEP 11,12,13 AND 14 WAS PERFORMED TEST OK. (2591841)

Part: SNUBBER — INOPERATIVE · airframe 67,548 hrs · 22,282 cycles

SHIP 5811 PERFORMING AMDS 2040-0191-2L STEP 7, ROTARY SNUBER PIN EXTENSION IS OUT OF LIMITS IN L2 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00129: ROTARY SNUBBER 2L DOOR WAS REPLACED PER B757-300 AMM 52-11-10 AND 2L PASSENGER DOOR WAS REMOVED AND INSTALLED PER B757-300 AMM 52-11. (2591544)

Part: SKIN — GOUGED · airframe 67,548 hrs · 22,282 cycles

SHIP 5811 GOUGE AND DENT BTW STA 740 & STA 760 AND STR -15L & STR-16L ON EXTERNAL FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00030: GOUGE AND DENT BTW STA 740 & STA 760 AND STR-15L & STR-16L ON EXTERNAL FUSELAGE SKIN. WAS REPAIRED PER PRI 605019-14 REV 1 AND ERA 605019-14 REV ORIGINAL. (2589919)

Part: LEAF SPRING — DAMAGED (GIRT BAR) · airframe 67,548 hrs · 22,282 cycles

GIRT BAR LEAF SPRINGS 2 E/A DOES NOT RETAIN THE SLIDERS OF R4 DOOR (NEED REPLACE GIRT BAR IAW AMM 25-66-10-201 AND PERFORM CARD INSTRUCTIONS. R2 DOOR GIRT BAR WAS REPLACED & VERIFIED IAW IPC 25-66-05-05 AND STEPS 11, 12, 13 AND 14 OF AMDS 2561-01257-01F WERE PERFORMED SATISFACTORY TEST OK.

Part: SNUBBER — OUT OF LIMITS (L1 DOOR) · airframe 67,548 hrs · 22,282 cycles

PERFORMING AMDS 2040-0191-1L, ROTARY SNUBER PIN EXTENSION IS OUT OF LIMITS IN L1 DOOR. ROTARY SNUBBER 1L DOOR WAS REPLACED PER AMM 52-11-10 AND PASSENGER DOOR WAS REMOVED AND INSTALLED IAW AMM 52-11.

Part: STRAP — CRACKED (BS 364 BL0) · airframe 67,548 hrs · 22,282 cycles

CRACK ON STABILIZATION STRAP STA 365 BL 0 AT NLG WHEEL WELL UPPER AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00189: STABILIZATION STRAP WAS REPAIRED PER B757- 300 SRM. (2579760)

Part: INTERCOSTAL — CORRODED (BS 1540-1560) · airframe 67,548 hrs · 22,282 cycles

SHIP 5811 REFERENCE ER/A 596280-14 B757-300 / FUSELAGE / STA 1540 - 1560 / STR 27R TO 29R / LAV PAN INTERCOSTAL / CORROSION. CORRECTIVE ACTION: REF ERA 596280-14. (2570208)

Part: COVER — BROKEN · airframe 66,402 hrs · 21,875 cycles

SHIP 5811 RT AFT OVER WING EXIT COVER BROKEN AND WILL NOT STAY IN PLACE. CORRECTIVE ACTION: REPLACED HANDLE COVER ASSY PER B757 AMM 52-22. (8239198)

Part: NONE — NONE · airframe 66,081 hrs · 21,762 cycles

SHIP 5811 MID CABIN EXIT SIGN FELL OFF. CORRECTIVE ACTION: RE-ATTACHED EXIT SIGN LENS. (8846790)

Part: GIRT BAR — MISALIGNED · airframe 65,528 hrs · 21,565 cycles

SHIP 5811 4R-SLIDE LIGHT WILL NOT LIGHT WHEN IN ARM POSITION. CORRECTIVE ACTION: HAD TO ADJUST AND REALIGN GIRT BAR INTO PROPER POSITION PER B757 AMM 25-66. OPS CK DOOR. (8669726)

Part: NONE — NONE · airframe 65,277 hrs · 21,473 cycles

SHIP 5811 AFT SIDE OF 3 DOOR HANGING EXIT SIGN FELL OFF. CORRECTIVE ACTION: REATTACHED EXIT COVER LENS AS REQUIRED. (8146699)

Part: NONE — NONE · airframe 64,858 hrs · 21,320 cycles

SHIP 5811 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589116-14 REV A. CORRECTIVE ACTION: REF ERA 589116-14 REV A. (2116137)

Part: NONE — NONE · airframe 64,463 hrs · 21,181 cycles

SHIP 5811 ON WAKE UP WALK AROUND FOUND AFT LAV SERVICE PANEL CORROSION AROUND OUTER EDGE POPPING THRU SEALER AND PAINT. CORRECTIVE ACTION: REPAIRED PER ERA 596269-14 REV ORIG. (8145715)

Part: NONE — NONE · airframe 64,463 hrs · 21,181 cycles

SHIP 5811 CORROSION DAMAGE DISCOVERED COMMON TO THE FUSELAGE SKIN IN THE VICINITY OF THE AFT LAVATORY SERVICE PANEL CUT-OUT. FUSELAGE SKIN REPAIR ADDRESSED IN ER/A 596269-14. FOLLOW ON ACTION REQUIRED. CORRECTIVE ACTION: DOUBLER/TRIPLER REPAIR INSTALLED IN THE VICINITY OF THE AFT LAVATORY SERVICE PANEL CUT-OUT TO RESTORE STRENGTH TO BLENDED MATERIAL. REF ERA 596269-14. (2069519)

Part: NONE — NONE · corrosion level 2 · airframe 64,463 hrs · 21,181 cycles

SHIP 5811 CORROSION FOUND ON INTERCOSTAL ON TOP OF LAV PAN IN THE FWD INBD CORNER. THREE SPOTS. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:0514-2001/00900009 REPAIRED INTERCOSTAL PER ERA 596280-14 REV. ORIG. (2070169)

Part: NONE — NONE · airframe 64,460 hrs · 21,178 cycles

SHIP 5811 EMERGENCY BATTERY PACK FAILS DEEP CYCLE TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY BATTERY PACK M00730 BATTERY PER B757 AMM 33-51-07 OP/CKS GOOD. (8145711)

Part: NONE — NONE · airframe 64,368 hrs · 21,151 cycles

SHIP 5811 DOOR 2R DOSE NOT SHOW SLIDE LIGHT ILLUMINATED WITH DOOR ARMED. CORRECTIVE ACTION: CYCLED SLIDE ARM LEVER. SLIDE LIGHT INOP. OPENED DOOR WITH SLIDE DISARMED. SLIDE DEPLOYED. REMOVED SLIDE. REF LP 8119243 FOR EMER ESCAPE SLIDE R/R. UPON INSPECTION OF DOOR 24 SIDE DRAIN FOUND CLOGGED. CLEARED DRAINS. SLIDE LIGHT OPS GOOD AFTER SLIDE CHANGE. INSP GIRT BAR/FLOOR FITTINGS. NO FAULTS FOUND. (8119242)

Part: NONE — NONE · airframe 64,022 hrs · 21,052 cycles

SHIP 5811 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:655. CORRECTIVE ACTION: REINSTALLED EMERGENCY EXIT SIGN OPS CHECK OK. (2007423)

Part: NONE — NONE · airframe 63,618 hrs · 20,940 cycles

SHIP 5811 4R DOOR WONT ARM AT DEPT. CORRECTIVE ACTION: RESECURED GIRT BAR OPN NOW CHECKS GOOD PER B757 AMM 52-11. (7767374)

Part: LIGHT — UNSECURE (SEAT 41D) · airframe 63,350 hrs · 20,868 cycles

SHIP 5811 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:14D. CORRECTIVE ACTION: EMER LIGHT AT 14D CHECKS GOOD.. FOUND LOOSE EMER LIGHT ASSY AT SEAT 41D. RESECURED LIGHT ASSY. OPC GOOD. (1930703)

Part: CIRCUIT BREAKER — TRIPPED · airframe 63,131 hrs · 20,811 cycles

SHIP 5811 B R-34 "GRIT BAR ENT DIM" POP. CORRECTIVE ACTION: REMOVED AND REPLACED C/B. T/S PER B757 WDM 25-66-11, FOUND 1R SLIDE ARM IND LIGHT SORTED AT L404. RPLCD (L404) R1 SLIDE ARM IND LIGHT. FOUND BOTH PROX SWITCHES BAD. R/R R1 DOOR FWD AND AFT PROX SWITCHESPER B757 WDM 25-66. OPS CK NORMAL. (7799988)

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 62,460 hrs · 20,630 cycles

SHIP 5811 SLDE LIGHT 1L DOES NOT ILLUMINATE. CORRECTIVE ACTION: T/S PER B757 WDM 25-66 FOUND S10215 BAD RPLCD SAME CKS GOOD. (7601777)

Part: GUIDE — MISSING (R4 GIRT BAR) · airframe 62,186 hrs · 20,543 cycles

SHIP 5811 R4 DOOR GIRT BAR MISSING GUIDE. CORRECTIVE ACTION: INSTALLED NEW GIRT BAR LOCK REF 757 AMM 25 66.

Part: STATIC WICK — DAMAGED (RT WINGLET) · airframe 61,998 hrs · 20,465 cycles

SHIP 5811 STATIC DISCHARGBE RT WINGLET T/E 34" UP FROM ATTACH POINT. CORRECTIVE ACTION: PERFORMED BLEND OUT REPAIR IN ACCORDANCE WITH BOEING 757 SRM AND APPLY PROTECTIVE COATINGS PER BOEING 757 SRM. ACCOMPLISHED REPAIRS IN ACCORDANCE WITH BOEING SRM. (1784216)

Part: SKIN — DAMAGED (BS 230) · airframe 61,998 hrs · 20,465 cycles

SHIP 5811 BURNED RIVET AT FS 230, A/C RIGHT, 5" OUTBOARD FROM BLO, 2" FWD OF FWD ELECRICAL BAY. CORRECTIVE ACTION: BLENDED PNL PER 757 SRM. (1784240)

Part: SWITCH — FAULTED (R1 GIRT BAR) · airframe 61,792 hrs · 20,367 cycles

SHIP 5811 R1 DOOR SLIDE LIGHT WILL NOT EXTINGUISH. CORRECTIVE ACTION: R/R BOTH FWD AND AFT GIRT BAR SWITCHES PER B757 WDM 25-66. (7387303)

Part: GROUND WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 61,582 hrs · 20,272 cycles

SHIP 5811 EMERGENCY LIGHTS ARE ROW 33-40 ARE INOPERATIVE. MAINTENANCE FOUND GROUND WIRE WITH POOR CONNECTION AND SECURED GROUND WIRE. SYSTEM OPERATION IS NORMAL. (LP 6292596)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,536 hrs · 20,244 cycles

EMERGENCY AISLE LIGHT ARE INOPERATIVE AT ROWS 33-40. MAINTENANCE REPLACED THE BATTERY PACKS. SYSTEM OPERATION IS NORMAL.(LP 6292575)

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,313 hrs · 20,095 cycles

DURING REMOVAL OF FASTENERS, ELONGATE HOLES AND BULGED SKIN WERE FOUND BETWEEN STA 660 TO 6680, BETWEEN S-27R TO 27L AT OUTER FUSELAGE SKIN. REPAIRED PER ERA 589133-14.

Part: SKIN — DAMAGED (BS 660-680 S28LR) · airframe 71,041 hrs · 23,490 cycles

SHIP 5811 ERA 589133-14 ISSUED FOR REPAIR TO STA 660-680, S-28L TO S-28R. ENLONGATED HOLES / DENTS. CORRECTIVE ACTION: REF ERA 589133-14. (1686644)

Part: RETAINER — CORRODED (GIRT BAR) · airframe 61,313 hrs · 20,095 cycles

FOUND DURING INSPECTION CORROSION ON RETAINER PLATE OF GIRT BAR AT LIDES L1 AND L4. CORRECTIVE ACITON: RETAINER PLATE REPLACED.

Part: STRUCTURE — SCRATCHED (LT FUEL CELL) · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION MAINTENANCE FOUND SCRATCH ON DRY BAY (INNER FACE OF SETTLEMENT AREA) IN LT MAIN FUEL TANK BETWEEN WS 285.65/WS 313.50. REPAIRED PER ERA 588939-14.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON FLOOR STRINGERS, RBL 7.55 AT STA 1333, STA 1362, STA 1374, RBL 10.45 AT STA 1360, STA 1371 AND RBL 16.10 AT STA 1374. STRINGERS REPAIRED PER SRM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION CORROSION LEVEL 2 WAS FOUND ON FLOOR STRINGERS LBL 2.90, 7.55 AND 10.45, STA 1510 AT AFT CARGO COMPARTMENT. MAINTNENACE REPAIRED, PER SRM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INSPECION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRINGERS LBL 2.90, 7.55, 10.45 16.10, STA. 1470 AT AFT CARGO COMPARTMENT. STRINGER REPAIRED, PER SRM.

Part: PANEL — CORRODED (RIGHT) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RT SIDE PANEL (UPPER AND LOWER SURFACE), BETWEEN STA 1440 TO 1520 AT AFT CARGO COMPARTMENT. REPLACED SIDE PANEL, PER SRM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

INITIAL INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON FLOOR SUPPORT NEXT TO FLOOR STRINGER 10.45 RBL FROM STA 1460/1480 AT AFT CARGO COMPARTMENT. FLOOR SUPPORT REPAIRED, PER SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

REWRITE DUE TO MEASUREMENTS OF THE FLOOR STRINGERS ARE INCORRECT. CORROSION LEVEL 2 ON FLOOR STRINGERS RBL 2.90, 7.55, 10.45 16.10, STA 1470 AT AFT CARGO COMPARTMENT WERE REPAIRED PER SRM.

Part: FITTING — CORRODED (GALLEY FLOOR) · corrosion level 2 · airframe 61,406 hrs · 20,162 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION ON FLOOR FITTING ON G4. FITTING REPLACED PER ERA.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRINGER RBL 7.55 STA 1510 AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 53-00-53.

Part: NONE — NONE · airframe 66,920 hrs · 22,050 cycles

SHIP 5811 ERA 588939-14 ISSUED FOR LH WING DRY BAY REPAIR AT WING STATION 258.65-313.50. CORRECTIVE ACTION: REF ERA 588939-14. (1676433)

Part: PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LT SIDE PANEL AT AFT CARGO COMPARTMENT FROM STA 1420/1440. REPLACED SIDE PANEL PER SRM.

Part: WEB — DAMAGED (CABIN) · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION, MAINTENANCE FOUND HIDDEN DAMAGE ON WEB OF INTERCOSTAL BETWEEN STA 1500 TO STA 1500 TO 1520 BL 0 PASSENGER CABIN. REPAIRED PER SRM 51-70-13.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION, MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRUCTURE OF PASSENGER CABIN. REPAIRED PER SRM.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION, FOUND CORROSION LEVEL 2 ON FLOOR STRUCTURE OF PASSENGER CABIN BETWEEN STA 980 AND 1020 AND RBL 64.5 AT WING CENTER AREA. CORROSION REPAIRED PER SRM.

Part: INTERCOSTAL — CORRODED (CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON INTERCOSTAL BETWEEN STA 600 AND 620 AND BETWEEN S 26R AND 27R AT FWD CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED PER SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON LIMITS ANGLE FLOOR SUPPORT FROM STA 1596 TO 1602 AND 64 RBL PASSENGER CABIN. REPAIRED PER SRM.

Part: STRAP — CRACKED (CABIN FLOOR) · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION MAINTENANCE FOUND A CRACK ON STABILIZER STRAP STA 1640 AND 25 LBL AT PASSENGER CABIN FLOOR STRUCTURE. CRACK REPAIRED PER SRM.

Part: STRAP — CRACKED (PAX FLOOR) · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION MAINTENANCE FOUND A CRACK ON STABILIZER STRAP LBL 25, STA 365 AT PASSENGER FLOOR STRUCTURE. CRACK REPAIRED PER SRM.

Part: STRAP — CRACKED (CABIN FLOOR) · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION MAINTENANCE FOUND A CRACK ON STABILIZER STRAP STA 1620 AND 45 RBL AT PASSENGER CABIN FLOOR STRUCTURE AND REPAIRED, PER SRM.

Part: STRAP — CRACKED (CABIN FLOOR) · airframe 61,313 hrs · 20,095 cycles

DURING INSPECTION FOUND CRACK ON STABILIZER STRAP STA 1661 AND 25 RBL AT PASSENGER CABIN FLOOR STRUCTURE. STRAP REPAIRED, PER SRM 53-00-51.

Part: INDICATOR — OUT OF ADJUST (R4 DOOR) · airframe 60,385 hrs · 19,797 cycles

R4 DOOR KNUCKLE KNOCKER ARMED IN DICATION NOT PROPERLY RETRACTING AND EXTENDING PER PILOT AND FA PROCEDURES. ADJUSTED THE KNUCKLE KNOCKER, CHECKS NORMAL IAW AMM 52-11.

Part: RESERVOIR — LOW PRESSURE (L2 DOOR ASSIST) · airframe 60,385 hrs · 19,797 cycles

DURING A SERVICE CHECK, FOUND THE L2 DOOR EMP POWER RESERVOIR EMPTY. REMOVED AND REPLACED L2 DOOR ASSIST RESERVOIR ASSY IAW AMM 52-11-30. PRESSURE CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,319 hrs · 19,779 cycles

EMERGENCY LIGHTS INOP AT L4 DOOR AND ROWS 46-49. R/R BATTERY PACK AT M737 PER AMM 33-51. OPS CHK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 60,293 hrs · 19,770 cycles

SHIP 5811 RECEIVED L CTR ENT DOOR EICAS MESSAGE. REFERENCED QRH. CORRECTIVE ACTION: PERFORMED DOOR CHECK ON 2L REF B757AMM 52-11. DOOR OPERATES AND INDICATES NORMAL. (6680412)

Part: BYPASS VALVE — LEAKING (SLAT SYSTEM) · airframe 59,863 hrs · 19,625 cycles

SHIP 5811 -FUME- A OILY DIRTY SOCK ODOR WAS REPORTED IN THE COCKPIT AND CABIN, O2 MASKS WERE DONNED. CORRECTIVE ACTION: FOUND SLAT BYPASS VALVE LEAKING INTO (L) PACK BAY, SECURED LINE, CLEANED PACK BAY OP CHECKS NORMAL. C/W REMOVAL OF OIL CONTAMINATION IN A/C SYSTEM PER B757 AMM 21-00 AND REPLACED RECIRC FILTERS. NO ODOR PRESENT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,762 hrs · 19,593 cycles

SHIP 5811 SEAT 28E LOWER EMERGENCY EXIT SIGN INOP. CORRECTIVE ACTION: FOUND BATTERY PACK EQUIPMENT # M11384 DEAD R/R BATTERY PACK IAW B757 AMM 33-51. OPS NML. (6438745)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,474 hrs · 19,506 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE AT SEATS 24 - 26DEF, BINS 34, 42 AND 44, OVERWING EXITS, AND EXIT. R & R TWO BATTERY PACKS FOR EMERGENCY LIGHTING IAW AMM 33-51. OPS CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 59,298 hrs · 19,452 cycles

SHIP 5811 EMER LIGHTS INOP ROWS 46-49. CORRECTIVE ACTION: REPLACED FUSE POWER SUPPLY M737 REF B757 WDM 33-51-22 AND B757 AMM 33-51-07-962-017-002. OPS GOOD. (6363255)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 58,868 hrs · 19,315 cycles

EMERGENDCY LIGHT POWER SUPPLY BATTERY PACKS M11613 AND M11487 WILL NOT KEEP EMERGENCY LIGHTS ILLUMINATED FOR AT LEAST 15 MINS. REPLACED THE BATTERY PACKS. OK FOR SERVICE IAW AMM 3351.

Part: CAP — DEFECTIVE (R4 DOOR) · airframe 58,661 hrs · 19,256 cycles

(AIRCRAFT 5811, L/P 1282803) SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 4R. 4R SLIDE LIGHT WAS ON BUT TURNING OFF AFTER TAKEOFF EVEN THOUGH DOOR WAS STILL IN ARMED POSITION. CORRECTIVE ACTION: R/R R4 DOOR SLIDE LIGHT CAP L408 PER SSM 25-66-01. C/W W/C 5211-2301. ALL IND NORMAL.

Part: ENGINE — MAKING METAL (RIGHT) · airframe 58,629 hrs · 19,248 cycles

SHIP 5811- IFSD & DIV - AIRCRAFT DIVERTED INTO DEN DUE TO PILOT REPORT OF RIGHT ENGINE STALL THEN ROLL BACK TO IDLE. ENGINE SUBSEQUENTLY SHUT DOWN. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN THE TAILPIPE. ENGINE CHANGE ACCOMPLISHED ON LOGPAGE 1276788.

Part: SENSOR — DEFECTIVE (BLEED AIR SYS) · airframe 57,221 hrs · 18,884 cycles

SHIP 5811 -DIV- DIVERED TO DEN DUE TO LEFT ENGINE BLEED OFF LIGHT AND EICAS MESSAGE AT FL 360 AND ENGINE ANTI-ICE ON. FOLLOWED QRH AND RECEIVED RIGHT ENGINE BLEED OFF LIGHT AND EICAS MESSAGE. DESCENDED OUT OF VISIBLE MOISTURE AND RESET ENGINE BLEED AND SAME CONDITION RETURNED ENTERED VISIBLE MOISTURE AGAIN AT FL280. CORRECTIVE ACTION: REPLACED LEFT ENGINE HIGH STAGE PILOT, FAMVAND LEFT ENGINE FAN AIR TEMP SENSOR. PERFORMED OPERATIONAL PNEUMATIC TEST PER FIM OP TESTS GOOD. LP 5646792

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 57,172 hrs · 18,870 cycles

(AIRCRAFT 5811, L/P 5646771) DURING SVC CK FOUND EMERGENCY BATT POWER SUPPLY M11383 INOP. R/R PWR SUPPLY & BATTERY POS M11383 REF AMM 33-51. OPS NML.

Part: ANGLE — DAMAGED (RT HORIZ STAB) · airframe 56,479 hrs · 18,679 cycles

SHIP 5811 LWR AFT T-ANGLE ON RT HORIZONTAL STAB DAMAGED 30" IB FROM O/B EDGE. CORRECTIVE ACTION: REPAIRED PER ERA 576304-14 REV A. (5818719)

Part: LENS — MISSING (EXIT SIGN) · airframe 55,865 hrs · 18,484 cycles

SHIP 5811 EMERGENCY EXIT SIGN LENS MISSING AT ROW 38. CORRECTIVE ACTION: REPLACED LENS, CKS OK PER AMM 33-51. (5280258)

Part: PIN — BROKEN (L4 DOOR SLIDE) · airframe 55,358 hrs · 18,331 cycles

(AIRCRAFT 5811, L/P 0817270) L-4 DOOR EMERGENCY EXITSLIDE HAS LACING PIN DAMAGED/ BROKEN. DOT 004. I-29. REMOVED AND REPLACED L-4 DOOR EMERGENCY ESCAPE SLIDE IAW AMDS 2566-9001-4L.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 53,932 hrs · 17,960 cycles

LEFT ENGINE POPPING NOISE REPORTED BY TOWER AND OTHER AIRCRAFT. INSPECTED BOTH ENGINE INLETS AND OUTLETS, MASTER CHIP DETECTORS AND MCD'S IAW AMM 79-21- NTF. DOWNLOADED PCMCIA CARD BUT CARD UNABLE TO LOAD, R & R PCMCIA CARD IAW AMM 31-36. FOUND EPCS MESSAGE FOR NR 1 ENGINE, S-PDIU, S-274-18, S-275-15 AND S-354-29 IAW FIM 77-35 / FIM 71-01. REPLACED EEC ALTTERNATOR STATOR AND EEC IAW AMM 73-21. OPS TESTED OK. R & R THE 14TH STAGE BLEED VALVE IAW AMM 75-32. R & R NR 1 ENGINE ALTERNATOR OIL SEALS IAW AMM 72-61. INSTALLED THE STATOR IAW AMM 73-21. PERFORMED HIGH POWER RUN AND NO LEAKS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,480 hrs · 17,190 cycles

ROW 30 AND 33 OVERHEAD BIN MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FUSE — TRIPPED (EMERGENCY LIGHTS) · airframe 51,070 hrs · 17,053 cycles

LEFT OVERWING DOOR EMERGENCY LIGHTS INOPERATIVE. FOUND THE FUSE TRIPPED ON THE PSU, AFTER REPLACING FUSES ON PSU. FOUND SHORTED LIGHT BULB HANDLE LIGHT IAW WDM 33-51-13. REPLACED THE LAMPS. CHECKED OK.

Part: LIGHT — DETACHED (CABIN) · airframe 49,974 hrs · 16,764 cycles

EMERGENCY LIGHT AT 48 D IS DETACHED. INSTALLED NEW BRACKET. OK FOR SERVICE.

Part: GASKET — LEAKING (NR 6 PCA) · airframe 49,770 hrs · 16,698 cycles

ENROUTE, AIRCRAFT LOST THE RT HYD QTY FLUID. DURING APPROACH WITH FLAPS AT 30, THE AIRCRAFT EXPERIENCED A ROLL TO THE LEFT. CREW DID A GO AROUND, EXTEND THE FLAPS AND EXPERIENCED THE SAME PROBLEM. PLACED THE FLAPS AT 25 WITH NO PROBLEM. MAINTENANCE TROUBLESHOT IAW AMM. FOUND PCA SERVO GASKET LEAKING ON NR 7 SPOILER PCA. REPLACED THE GASKET. REMOVED AND REPLACED THE NR 6 SPOILER PCA. LEAK, OPS AND RIGGED CHECKED OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 49,476 hrs · 16,605 cycles

EMERGENCY LIGHT AT ROW 33D INOPERATIVE. FOUND A WIRE BROKEN UNDER SEAT. REPAIRED IAW SWPM 20. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SIGN — MISSING (CABIN) · airframe 49,060 hrs · 16,460 cycles

BACK SIDE OF CENTER AISLE OVERHEAD "EXIT SIGN MISSING BY ROW 38. REPLACED MISSING OVERHEAD EXIT SIGN AT ROW 38.

Part: LIGHT — INOPERATIVE (ROW 43) · airframe 49,042 hrs · 16,451 cycles

DURING A SERVICE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 43. REMOVED AND REPLACED THE LIGHT ASSY IAW AMM 33-50. OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 48,573 hrs · 16,283 cycles

FLOOR PATH EMERGENCY LIGHTS ARE INOP AT SEATS 14 DEF TO 20 DEF. INSP AND FOUND EMERGENCY LIGHT WIRING BROKEN UNDER SEAT ROW 20 DEF. REPAIRED WIRING UNDER SEAT. ALL LIGHTS OPS NORMAL.

Part: HOUSING — DAMAGED (CABIN) · airframe 48,050 hrs · 16,116 cycles

SEAT 35 RT EEPLS HOUSING DAMAGED. R&R SEAT 35 RT EEPLS HOUSING OK FOR SERVICE.

Part: LIGHT — BROKEN (SEAT 42D) · airframe 46,660 hrs · 15,653 cycles

EMERGENCY LIGHT UNDER 42D BROKEN. SEAT 42D UNDERSEAT EMERGENCY ESCAPE PATH LIGHT IS OPERATIVE BUT LIGHT ASSY BROKEN. TEMPORARILY SECURED IN PLACE WITH REINFORCING TAPE. DEFERRED LIGHT ASSY REF MEL 33-51-03A. REPLACED COVER IAW CMM 25-22 MEL/PLAC REMOVED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,885 hrs · 14,300 cycles

DURING ACFT SERVICE CHECK, FOUND EMERGENCY LIGHTING INOPERATIVE AT ROWS 33-36, 37-39. FOUND POWER SUPPLY AT FS 1334 OVERHEAD INOPERATIVE 1 OF 2. ABOVE CEILING PANEL R & R LT POWER PACK SUPPLY ASSY AND LOOSE PLUG ASSY. "D9104J" REF FS 1210 WIRING DIAGRAM 33-51-22. CEILING PANELS INSTALLED FS 1334. OK FOR SERVICE. EMERGENCY LIGHTS CK OK.

Part: ENGINE — MAKING METAL (RIGHT) · airframe 42,049 hrs · 14,012 cycles

DURING FLIGHT, DIVERTED DUE TO RT ENGINE OIL FILTER EICAS MESSAGE. INDICATION DID NOT EXTINGUISH WITH THROTTLE AT IDLE. ENGINE WAS SHUTDOWN IAW QRH. MAINTENANCE FOUND OUT OF LIMITS METAL IN MAIN OIL FILTER, MASTER CHIP DETECTOR AND NR 5 BEARING CHIP DETECTOR. REPLACED RT ENGINE DUE TO OIL FILTER BYPASS IAW AMDS WC 7100-9903E-02.

Part: STRINGER — CRACKED (BS 780) · airframe 41,450 hrs · 13,776 cycles

CRACK ON END OF STRINGER 16R AT BS 780+36 RG1. REPAIRED STRINGER IAW ER/A 515773-14, REV ORIG.

Part: STRINGER — CRACKED (BS 780) · airframe 41,450 hrs · 13,776 cycles

CRACK ON END OF STRINGER 16L AT BS 780+36 RG3. REPAIRED STRINGER IAW ER/A 528685-14, REV ORIGINAL.

Part: STRUCTURE — PUNCTURED (LT WING TE FLAP) · airframe 41,450 hrs · 13,776 cycles

PREVIOUS REPAIR HAS A VOID IN SEALANT ON THE LT WING OTBD AFT FLAP LOWER SURFACE AT APPROXIMATELY STA 537. REPAIRED HONEYCOMB PUNCTURE DAMAGE, PERFORMED WATER EVAC & APPLIED PRIMER & TOP COAT FINISHES TO THE LEFT WING OTBD AFT FLAP LOWER SURFACE AT APPROXIMATELY STA 537 IAW SRM 57-53-01, SRM 51-70-04, AMM 51-21-14-370-801 & AMM 51-21-15-370-801.

Part: CREASE BEAM — CORRODED (BS 1260) · corrosion level 2 · airframe 41,450 hrs · 13,776 cycles

CORROSION ON RT MAIN CABIN CREASE BEAM INNER ANGLE AT BS 1260. REPAIRED IAW ERA 529963-14, REV-ORIG.

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 41,450 hrs · 13,776 cycles

DOOR FAILED EMERGENCY POWER ACTUATION CABLE TRAVEL CHECK. ADJUSTED EMERGENCY POWER ACTUATION CABLE IAW AMM 52-11.

Part: GIRT BAR — NO TEST (R1 DOOR) · airframe 41,450 hrs · 13,776 cycles

R1 DOOR FORWARD FLOOR FITTING ON GIRT BAR FAILED GO-NO-GO TEST. R & R R-1 DOOR GIRT BAR.

Part: STRINGER — CORRODED (BS 780) · airframe 41,450 hrs · 13,776 cycles

CRACK ON END OF STRINGER 16R BS 780+24. REMOVED, FABRICATED AND INSTALLED STRINGER SECTION AT STRINGER IAW SRM.

Part: STRINGER — CRACKED (BS 780) · airframe 41,450 hrs · 13,776 cycles

CRACK ON END OF STRINGER 16L AT BS 780+24. REMOVED, FABRICATED AND INSTALLED NEW STRINGER IAW SRM.

Part: STRAP — CRACKED (BS 700) · airframe 41,450 hrs · 13,776 cycles

FWD CARGO CEILING STABILIZER STRAP RBL 25 IS CRACK AT BS 700. REPAIRED IAW ERA 384483-14 MA REV-D.

Part: CREASE BEAM — CORRODED (BS 730-740) · airframe 41,450 hrs · 13,776 cycles

CORROSION ON THE RIGHT CREASE BEAM INNER ANGLE BETWEEN BS 730 TO 740. REMOVED CORROSION AND FOUND OUT OF LIMITS. R & R CREASE BEAM IAW SRM.

Part: SEAT TRACK — CORRODED (BS 377) · corrosion level 2 · airframe 41,450 hrs · 13,776 cycles

CORROSION ON MAIN CABIN SEAT TRACK BS 377.7, LBL 071 94. FOUND OUT OF LIMITS IN IAW SRM. R & R SEAT TRACK SUPPORT.

Part: STRAP — CRACKED (BS 580) · airframe 41,450 hrs · 13,776 cycles

FWD CARGO BAY CEILING STABILAZATION STRAP LBL 25 IS CRACKED AT BS 580. CEILING STABILIZATION STRAP REPAIRED IAW ERA 384483-14 REV.-D.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 41,450 hrs · 13,776 cycles

FWD CARGO DOOR INTERNAL STRUCTURES HAS UPPER ANGLES CRACKED ON FWD AND AFT CORNERS 97-09. FABRICATED AND INSTALLED 2EA UPPER ANGLES ON FWD CARGO COMPARTMENT DOOR INTERNAL STRUCTURE IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1640) · corrosion level 2 · airframe 41,450 hrs · 13,776 cycles

CORROSION ON MAIN CABIN SEAT TRACK AT BS 1640, RBL 46. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. R & R THE SEAT TRACK IAW SRM.

Part: STRAP — CRACKED (BS 365) · airframe 41,450 hrs · 13,776 cycles

FWD NOSE COMPARTMENT LT TUNNEL CEILING STABILIZATION STRAP IS CRACKED AT LBL 46 BS 365. REPAIRED THE STRAP IAW ER/A 384483-14MA, REV D.

Part: SEAT TRACK — MISALIGNED (BS 1600) · airframe 41,450 hrs · 13,776 cycles

SEAT TRACK SPLICE AT BS 1600, FOUND MISMATCH CONDITION RBL 24, RBL 45 AND LBL24 AND LBL 45. REPAIRED THE SEAT TRACK MISMATCH CONDITION IAW ER/A 528656-14 REV ORIG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 41,448 hrs · 13,775 cycles

BATTERY PACK DID NOT POWER LIGHTS FOR 15 MINUTES. R & R BATTERY PACK IAW AMM 33-51.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 40,478 hrs · 13,447 cycles

EXIT ROW SEAT 26C RED LENS MISSING. R & R EMERGENCY LIGHT ASSY.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 38,989 hrs · 12,952 cycles

SEAT ROWS 14-20 EMERGENCY LIGHTS INOPERATIVE. WIRE BROKEN FOUND. REPAIRED WIRE IAW WSPM 20-30. OPS CHECKED OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 38,439 hrs · 12,742 cycles

BOTH EMERGENCY LIGHT MODULES ON SEAT 25C INOPERATIVE. FOUND BROKEN SPLICE ON HARNESS. REPAIRED SPLICE IAW SWPM CHAP 20-30. BOTH LIGHT MODULES ON SEAT 25C, OPS CHECKED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,841 hrs · 12,495 cycles

SEVERAL EMERGENCY PATH SEAT LIGHTS BURNED OUT. REPLACED BULB. OPS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,568 hrs · 12,058 cycles

CREW REPORTED ACRID ODOR IN THE CABIN AND COCKPIT. PILOTS FOLLOWED QRH AND ODOR WENT AWAY THEN ODOR RETURNED. FLIGHT DIVERTED AS A PRECAUTION. MX REMOVED LT AND RT RECIRCULATION FAN FILTERS. FOUND PIECES OF FILTER IN DUCT ON BOTH SIDES. CLEANED DEBRIS AND REPLACED FILTERS. ALSO FOUND MID GALLEY OVEN EMITTING PLASTIC ODOR. REPLACED OVEN.

Part: SUPPORT — CRACKED (BS 720) · airframe 34,508 hrs · 11,320 cycles

FCB CEILING PANEL SUPPORT IS CRACKED BELOW BS 720 FLOORBEAM, LBL 24, WL 200. FCB CEILING PANEL SUPPORT IS CRACKED BELOW BS 720 FLOORBEAM, LBL 24, WL 200 C/W PRI 508084-14 REV 2 AND ER/A 508084-14 REV ORIGINAL.

Part: FLOOR SUPPORT — CRACKED (BS 364.5) · airframe 34,472 hrs · 11,305 cycles

MX DISCOVERED THE FLOOR SUPPORT CRACKED ON LOWER FLANGE AT AFT END OF BS 364.5 LBL 24. R & R CRACKED FLOOR SUPPORT AT BS 364.5, LBL 24, WL 206 IAW SRM 51-40-02.

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,974 hrs · 9,852 cycles

DURING A SERVICE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 23C INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,712 hrs · 8,713 cycles

DURING LINE CHECK FOUND DAMAGE TO FUSELAGE SKIN AT BS 305 S22R. REPAIRED PER ERA 486183-14 SECTION I, SECTION II OF ERA 486183-14 TO PER ACCOMPLISHED NO LATER THAN 15OCT11 PENDING BOEING DTA APPROVAL.

Part: PANEL — DELAMINATED (NACELLE) · airframe 27,709 hrs · 8,713 cycles

DURING L-CHECK FOUND DELAMINATION ON THE TOP SIDE OF PANEL 431AT. REPAIRED PER ERA 401869-14.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 27,709 hrs · 8,713 cycles

DURING L-CHECK FOUND CRACK ON LEFT WING UPPER SURFACE FIXED LEADING EDGE PANEL OSS 438. REPAIRED PER ERA 483182-14.

Part: SKIN PANEL — DAMAGED (RT WING) · airframe 27,709 hrs · 8,713 cycles

DURING L-CHECK FOUND RIGHT WING FIXED LEADING EDGE SKIN PANEL BULGING AND CRACKED AT OSS 436. REPAIRED PER ERA 486181-14.

Part: ANGLE — CRACKED (PYLON) · airframe 1,467 hrs · 435 cycles

PYLON TO FAIRING FIRESEAL ANGLE CRACKED JUST AFT OF AFT ENG MOUNT. VERIFIED WITH EDDY CURRENT (CRACKS BY 3 FASTENERS FROM OTBD END) REPLACED CRACKED ANGLE IAW SRM 51-10-02.

Part: ANGLE — CRACKED (NACELLE) · airframe 27,468 hrs · 8,621 cycles

PYLON TO FAIRING FIRESEAL ANGLE CRACKED JUST AFT OF AFT ENG MOUNT. VERIFIED WITH EDDY CURRENT (CRACKS BY 3 FASTENERS FROM OTBD END) REPLACED CRACKED ANGLE IAW SRM 51-10-02.

Part: SUPPORT ANGLE — CRACKED (LT NACELLE) · airframe 27,468 hrs · 8,621 cycles

LT PYLON VERTICAL SUPPORT ANGLE ABOVE SKATE ANGLE CRACKED. R & R CRACKED ANGLE IAW SRM 51-10-02.

Part: BRAKE ASSY — FIRE (MLG) · airframe 27,315 hrs · 8,568 cycles

WHILE TAXIING INTO THE GATE, THE BELOW-THE-WING PERSONNEL NOTICED THAT THERE WERE FLAMES COMING FROM THE NR2 AND NR6 BRAKES. ACS EXTINGUISHED FIRE ON BRAKES USING DRY CHEMICAL. FOUND UPPER PISTON PUCK ON NR 1 BRAKE SEPARATED FROM PISTON. INSPECTED AXLES FOR DISCOLORATION OR PAINT BLISTERING. NONE FOUND. NO TIRE FUSE PLUGS BLOWN. REPLACED NR 1, NR 2, NR 5 AND NR 6 BRAKE AND WHEEL ASSEMBLIES. OK FOR SERVICE.

Part: BRAKE ASSY — FIRE (NR 1) · airframe 16,860 hrs · 5,359 cycles

DURING ROLL UP TO GATE, NR 1 BRAKE CAUGHT FIRE AND THEN SPREAD TO NR 2 BRAKE. GROUND PERSONNEL USED FIRE EXTINGUISHERS TO EXTINGUISH THE FIRE. THERE WERE NO INJURIES. MAINTENANCE REMOVED AND REPLACED BOTH BRAKES AND TIRES, ALSO CLEANED AND INSPECTED THE MAIN AXLES. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARTRIDGE — INOPERATIVE (SLIDE) · airframe 9,184 hrs · 2,998 cycles

NR 1 LEFT OVERWING SLIDE SQUIB LIGHT INOP. FOUND SQUIB BLOWN, REPLACED SQUIB AND RETURNED AIRCRAFT TO SERVICE.

Part: LINE — CHAFED (RT WING) · airframe 4,457 hrs · 1,516 cycles

THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD.