N721TW

Part: INVERTER — ODOR (ZONE 200) · airframe 92,934 hrs · 23,952 cycles

DIV/DE- TO SLC DUE TO ELECTRICAL SMELL IN THE FLIGHT DECK AND STANDBY INVERTER MESSAGE. REPLACED STANDBY INVERTER.

Part: COVER — LOOSE (ZONE 200) · airframe 92,561 hrs · 23,857 cycles

EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:604. ADJUSTED EXIT SIGN AT LOC 604 PER B757, AMM 33-51. (1192624)

Part: COVER — LOOSE (ZONE 200) · airframe 92,550 hrs · 23,855 cycles

EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:604. INSTALLED EMERGENCY EXIT SIGN PER B757 AMM 33-51.OPS CHECK GOOD. (1190325)

Part: LANYARD — OUT OF POSITION (ZONE 800) · airframe 91,885 hrs · 23,703 cycles

SHIP 6810 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: REINSTALLED LAYARD ON BOTTOM-SIDE OF DOOR. (7408436)

Part: GIRT BAR — FOD (ZONE 800) · airframe 91,602 hrs · 23,630 cycles

SHIP 6810 RT DOOR WILL NOT ARM. CORRECTIVE ACTION: CLEARED DEBRIS & SECURED LANYARD AS REQUIRED. REF B757 AMM 25-61. (7542294)

Part: PLACARD — OUT OF POSITION (ZONE 800) · airframe 91,271 hrs · 23,542 cycles

SHIP 6810 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:601. DISARMED PLACARD DOES NOT DISPLAY PROPERLY. CORRECTIVE ACTION: REAJUSTED PLACARD LOCATION AND READJUSTED ENTRY DOOR ARMING LEVEL @ LOCATION 601. CHK NML. REF B757 AMM 52-10. (0958166)

Part: SWITCH — BROKEN (ZONE 200) · airframe 91,038 hrs · 23,477 cycles

SHIP 6810 "UNARMED" KORREY SWITCH BROKEN. CORRECTIVE ACTION: R/R EMERGENCY LIGHTS/PASSENGER OXYGEN CONTROL PANEL PER B757 AMM 33-51. (7034938)

Part: LINE — OUT OF POSITION (ZONE 800) · airframe 91,038 hrs · 23,477 cycles

SHIP 6810 1 RIGHT DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND MOORING LINE OBSTRUCTING GIRT BAR. RESTOWED MOORING LINE. GIRT BAR ENGAGES PROPERLY PER B757 AMM 52-66. (7034930)

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 90,856 hrs · 23,410 cycles

SHIP 6810 DURING W/C 3351-7001 FOUND BAD BATTERY CHARGER. CORRECTIVE ACTION: R+R BATTERY CHARGER AND BATTERY AT M730 FWD PER B757 AMM 33-51. OPS CHECK GOOD. (6721044)

Part: TRIM PANEL — LOOSE (ZONE 200) · airframe 90,613 hrs · 23,315 cycles

SHIP 6810 EMERGENCY LIGHT TRIM PANEL LOOSE SEAT ROW 37DEF. CORRECTIVE ACTION: RESCURE EMR LIGHT TRIM PANEL ROW 37 DEF OPS CHECK GOOD. (6347165)

Part: GIRT BAR — FOD (ZONE 800) · airframe 90,521 hrs · 23,296 cycles

SHIP 6810 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR "ARMED" CATCH HOUSING @ 1R DOOR OPS NML. (6347114)

Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 90,074 hrs · 23,177 cycles

SHIP 6810 2R KNUCKLED KNOCKER WILL NOT EXTEND WHEN DOOR IS ARMED. CORRECTIVE ACTION: FOUND KNUCKLE STUCK. GOT KNUCKLE UNSTUCK. ARMED DOOR 2R 4 TIMES IAW B757 AMM 52-11. OPS GOOD. (6643342)

Part: RECEIVER — DAMAGED (L1 DOOR FRAME) · airframe 90,042 hrs · 23,161 cycles

SHIP 6810 L1 DOOR FWD UPPER LATCH RECEIVER IS DAMAGED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW L1 DOOR FWD UPPER LATCH RECIEVER IAW B757 AMM 52-11-37. PERFORMED ADJUSTMENT AT L1 DOOR FWD UPPER LATCH RECIEVER IAW B757 AMM 52-11, ADJUSTMENT GOOD. (0705251)

Part: RECEIVER — DAMAGED (L1 DOOR FRAME) · airframe 90,042 hrs · 23,161 cycles

SHIP 6810 L1 DOOR AFT UPPER LATCH RECIEVER IS DAMAGED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW L1 DOOR AFT UPPER LATCH RECIEVER IAW B757 AMM 52-11-37 PERFORMED ADJUSTMENT AT L1 DOOR AFT UPPER LATCH RECIEVER IAW B757 AMM 52-11, ADJUSTMENT GOOD. (0705257)

Part: RECEIVER — DAMAGED (L1 DOOR FRAME) · airframe 90,042 hrs · 23,161 cycles

SHIP 6810 L1 DOOR AFT UPPER LATCH RECIEVER IS DAMAGED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW L1 DOOR AFT UPPER LATCH RECIEVER IAW B757 AMM 52-11-37 PERFORMED ADJUSTMENT AT L1 DOOR AFT UPPER LATCH RECIEVER IAW B757 AMM 52-11, ADJUSTMENT GOOD. (0705246)

Part: SNUBBER — OUT OF TOLERANCE (ZONE 800) · airframe 90,042 hrs · 23,161 cycles

SHIP 6810 SNUBBER AT L4 DOOR IS UNDER LIMIT. CORRECTIVE ACTION:REMOVED AND REPLACE SNUBBER AT LH DOOR. IAW. B757. AMM. 52-11-01 -004-001 AND IAW. B757. AMM. 52-11. (0696852)

Part: BOTTLE — DISCONNECTED (DOOR ASSIST) · airframe 90,042 hrs · 23,161 cycles

SHIP 6810 R4 DOOR ASSIST BOTTLE WAS FOUND DISCONNECTED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW EMERGENCY POWER ACTUATOR IAW B757 AMM 52-11. (0696926)

Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 90,000 hrs · 23,146 cycles

SHIP 6810 KNUCKLE KNOCKER ON 4L DOOR NOT RETRACTING IN DISARMED POSITION. CORRECTIVE ACTION: CLEANED EDGES AROUND KNUCKLE KNOCKER WHICH CAUSED JAMMING. NOW OPS CK OK REF B 757 AMM 52-02. (6643308)

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 89,543 hrs · 23,042 cycles

SHIP 6810 DOOR 2L DOOR GIRT BAR LOOSE. CORRECTIVE ACTION: FOUND THE 2L DOOR GIRT BAR LOOSE AND RE-SECURED IAW B757 AMM 25- 66-11. (6360140)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 89,032 hrs · 22,922 cycles

SHIP 6810 FALSE EMERGENCY EVAC WARNING ON APPROACH. CORRECTIVE ACTION: FLIGHT CREW VERIFIED CABIN PRESSURE NORMAL. NO EICAS MSG PERTAINING TO EVAC. VERIFIED EO IS ACCOMPLISHED PER B757 WDM 25- 63-11. (5703523)

Part: DUCT — UNSECURE (ZONE 100) · airframe 88,959 hrs · 22,908 cycles

SHIP 6810 -MISC/DE- DUE TO CABIN FLOOR AT ROW 24 HOT. CORRECTIVE ACTION: SECURED AFT CABIN ZONE TRIM MUFFLER DUCT AT MIX MANIFOLD.

Part: DOOR — FOD (L4) · airframe 88,035 hrs · 22,679 cycles

SHIP 6810 UNABLE TO ARM DOOR 4L. CORRECTIVE ACTION: CLEANED DEBRIS PER B757 AMM 52-11. DOOR OPS OK. ARMING OPS NML. (5616742)

Part: OXYGEN MASK — LEAKING (CREW NR 2) · airframe 87,985 hrs · 22,670 cycles

SHIP 6810 -DIV- TO LAS DUE TO CREW O2 PRESSURE DOWN TO 20 PSI INDICATED AT TOP OF CLIMB. CORRECTIVE ACTION: FOUND F/O MASK IN EMERGENCY MODE. C/W OVERWEIGHT LANDING. R/R F/O MASK AND CREW O2 BOTTLE.

Part: INDICATOR — FAULTED (R4 DOOR) · airframe 87,985 hrs · 22,670 cycles

SHIP 6810 R4 DOOR LIGHT IS EXTINGUISHED WHEN DOOR ARMED. CORRECTIVE ACTION: CYCLED ARM LEVER PER B757 AMM 25-66. OPS CHECK GOOD. (5616724)

Part: HEAT EXCHANGER — FAILED (A/C BAY) · airframe 87,324 hrs · 22,525 cycles

SHIP 6810 -DIV/PRES/DE- DUE UNABLE TO MAINTAIN CABIN PRESSURE WITH LEFT PACK ON MEL. CORRECTIVE ACTION: R/R ACM, R/R HEAT EXCHANGERS, R/R PLENUM ASSY, R/R CABIN PRESSURE CONTROLLER, R/R LT PK DUCT, RPLCD 2 BELLY DRAINS. CK AND CLEANED DOOR SEALS OF 1R AND 4R DOORS. CLEANED & RESEATED CARGO DOOR SEALS ON FWD & AFT CARGO DOOR. C/W PACK CONFIDENCE OPS CK, ALL ODI C/W.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,258 hrs · 22,244 cycles

SHIP 6810 PASSENGER SEAT 35D AISLE TRIM EMERGENCY ESCAPE PATH LIGHT ATTACHMENT BROKEN. CORRECTIVE ACTION: R/R ENDBAY BUMPER AND HOUSING REF B757 CMM 25-22-58. OPS CHECK GOOD. (0018603)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,262 hrs · 22,007 cycles

DOOR 4L SLIDE LIGHT INTERMITTENT. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR 4L FWD PROX SENSOR PER B757 AMM 25-66-11. CKS OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,154 hrs · 21,982 cycles

SHIP 6810 4L DOOR DISARMED BUT SLIDE ARM LIGHT IS STILL ILLUMINATED. CORRECTIVE ACTION: FOUND AND REMOVED DEBRIS FROM GIRTBAR SENSOR. DOOR ARMS AND DISARMS NORMALLY. SLIDE ARNED LIGHT OPS NORMALLY. (4144856)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,099 hrs · 21,962 cycles

SHIP 6810 -DIV/DE - TO MSP DUE TO RIGHT BLEED OFF INDICATION. CABIN PRESSURIZATION WARNING APPEARED AT FL360, EMERGENCY DECENT AND OXYGEN MASKS WERE USED. CORRECTIVE ACTION: T/S FOUND HOSE BLOWN OFF BETWEEN ACM AND HEAT EXCHANGER. REPLACED HOSE IN #1 PACK BAY, REPLACED SEAL AND DUCT CABLE, FOUND ELBOW GALLED ON LEFT ENGINE PRSOV, REPLACED MUSCLE LINE. R/R LT RFCC, TIGHTENED B NUT @REPLACED HPSOV SEAL, R/R HP VALVE, REPLACED REV FLOW CONTROLLER. PACK OPS CK NORMAL, NO LEAKS. C/W NO GO ODI.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,085 hrs · 21,958 cycles

SHIP 6810 4 LEFT DOOR SLIDE LITE STAYED ILLUMINATED AFTER DOOR DISARMED. CORRECTIVE ACTION: REMOVED DEBRIS. (4144802)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,907 hrs · 21,916 cycles

SHIP 6810 KNUCKLE KNOCKER ON 2R EXIT DOOR NOT WORKING PROPERLY. CORRECTIVE ACITON: REMOVED ESCAPE SLIDE COVER PER B757 AMM 52-11-02. REMOVED LOWER DOOR LINING PER B757 AMM 52-11-02. FOUND LINKAGE TO KNUCKLE KNOCKER DISCONNECTED. RECONNECTED ROD END TO LINKAGE. REINSTALLED LOWER LINING AND ESCAPE SLIDE COVER PER B757 AMM 52- 11-02. (4795344)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,186 hrs · 21,751 cycles

SHIP 6810 DURING SVC CHK CABIN WALK THROUGH FOUND 4R DOOR LOWER EMERGENCY EXIT LENS MISSING. CORRECTIVE ACITON: SECURED 4R DOOR LOWER EMERGENCY EXIT LENS COVER AS REQUIRED. (9599182)

Part: NONE — NONE · airframe 83,519 hrs · 21,598 cycles

SHIP 6810 2R SLIDE LIGHT STILL ILLUMINATED ON ARRIVAL TO A/C WHILE DOOR IS DISARMED. CORRECTIVE ACTION: PERFORMED INSP OF DOOR 2R GIRT BAR. NO DEFECTS NOTED. OPS CHK OF DOOR SLIDE ARM LIGHT NML. ALL PER B757-200 AMM 25-66. (4093040)

Part: STABILIZER — NONE · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 REPAIR TO LH HORIZ STABILIZER, AUX BOX, UPPER SURFACE, STA 70- 135, REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 603598-14AD. CORRECTIVE ACTION: REF ERA 603598-14AD. (2538596)

Part: FRAME — CORRODED (LAVATORY DOOR) · airframe 83,196 hrs · 21,517 cycles

CORROSION ON COUNTER FRAME OF DOOR OF LAVATORY C. THE COUNTER FRAME ON THE LAVATORY DOOR WAS REPAIRED IAW ERA 604216-14 REV. ORIGINAL SECTION I, REPAIR INSTRUCTIONS, AND PRI 604216-14 REV. 0 AND ERA 604025-14 REV. ORIGINAL SECTION I: REPAIR INSTRUCTIONS AND PRI 604025-14 REV 0.

Part: BRACE — DAMAGED (RT ENGINE) · airframe 83,196 hrs · 21,517 cycles

DAMAGE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE, HOLE NR 2 CORROSION ON SKIN AND FITTING BTW 2 TO 4 CLOCK POS; HOLE NR 4 CORROSION 0N SKIN BTW 7-10 CLOCK POS; HOLE #6 SCRATCHES 0N FITTING BTW 11 TO 1 CLOCK POS; HOLE #8 CORROSION 0N SKIN AND FITTING AT 8 CLOCK POS IN REF. CARD. OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW. HOLES #4 AND 6 WERE REPAIRED WITH CARD 5720-01100-02B, HOLES 2 AND 8 WERE REPAIRED PER PRI 589150-14 REV. 3 AND ER/A 589150-14AD REV. B SECTION VI.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON FLOOR STRINGERS 2, 7, 10 AND 16 LBL, FROM STA. 1460 TO 1480 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00207: FLOOR SUPPORT STRINGER LBL 2,10,16 WERE REPLACED PER B757-200 SRM AND FLOOR SUPPORT STRINGER LBL 7 WAS REPAIRED PER B-757-200 SRM. (2533210)

Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON FLOOR SUPPORT STRINGER (UPPER AND LWR SIDES) LBL 11.40, STA. 1510 AT BULK CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00169: FLOOR SUPPORT STRINGER LBL 11.40 WAS REPAIRED B757-200 SRM. (2533213)

Part: SPLICE — CORRODED (BS 1350) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON SPLICES ( 2 EAS). BELOW RH/LH SIDE PANEL, STA. 1350 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00186: SPLICES ( 2EA S ) RH/LH SIDE PANEL STA. 1350 WERE REPLACED PER B-757-200 SRM. (2531661)

Part: FLOOR SUPPORT — CORRODED (BS 1500-1640) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ALONG FLOOR SUPPORT STRINGER (UPPER AND LWR SIDES) RBL 7.45, BTW 1500 AND 1640 AT BULK CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00173: STRINGER WAS REPAIRED PER B757-200 SRM. (2531659)

Part: FLOOR SUPPORT — CORRODED (BS 1530-1565) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON FLOOR SUPPORT STRINGER (UPPER AND LWR SIDES) LBL 2.90, STA S 1530 AND 1565 AT BULK CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00171, FLOOR SUPPORT STRINGER WAS REPAIRED PER B757-200 SRM. (2530510)

Part: FLOOR SUPPORT — CORRODED (BS 1500-1635) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON FLOOR SUPPORT STRINGER (UPPER AND LWR SIDES) LBL 7.55 BTW STA. 1500 AND 1510 AND STA. 1635 AT BULK CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00170, FLOOR SUPPORT STRINGER WAS REPAIRED PER B757-200 SRM. THICKNESS MEASUREMENT INSPECTION WAS ACCOMPLISHED THEREFORE AREAS ARE OUT LIMITS PER B757-200 SRM. HFEC INSPECTION WAS ACCOMPLISHED ALONG THE CUT EDGES AND NO CRACKS WERE FOUND PER B757-200 SRM. (2530496)

Part: PANEL — CORRODED (BS 1350-1380) · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON RH SIDE PANEL FROM STA. 1350 TO 1380 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED PER B757-200 SRM. (2529417)

Part: PANEL — CORRODED (BS 1350-1410) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON LH SIDE PANEL (UP/LWR SIDE) FROM STA 1350 TO 1410 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00212, LH SIDE PANEL WAS REPLACED PER B757-200 SRM. (2529399)

Part: PANEL — CORRODED (BS 1440-1530) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORROSION ALONG RH SIDE PANEL FROM STA. 1440 TO 1530 IN THE BULK CARGO COMPARTMENT. RT PANEL WAS REPLACED IAW SRM.

Part: PANEL — CORRODED (BS 1310-1350) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORROSION ON RH SIDE PANEL (UP/LWR SIDE) FROM BS 1310 - 1350 IN THE AFT CARGO BAY. RT SIDE PANEL WAS REPLACED IAW DWG 146N5391, REV B, AND SRM.

Part: SUPPORT — CORRODED (BS 560-580) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORROSION ON SUPPORT AT FWD CARGO ENTRY LOWER EDGE BETWEEN STA 580 TO 560. THE SUPPORT WAS REPLACED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1495-1510) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORROSION ON FLOOR SUPPORT (UPPER AND LWR SIDES) RBL 11.40, BTW STA S 1495 AND 1510 AT BULK CARGO. FLOOR SUPPORT WAS REPAIRED PER B757-200 SRM. HFEC INSPECTION WAS ACCOMPLISHED ALONG THE CUT EDGES. NO CRACKS WERE FOUND PER B757-200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON FLOOR STRINGERS 2, 7, 10 AND 16 RBL, FROM STA. 1460 TO 1480 AT AFT CARGO COMPARTMENT. FLOOR STRINGERS 2, 7, 10 AND 16 RBL, FROM STA. 1460 TO 1480 AT AFT CARGO COMPARTMENT WERE REPLACED PER B757-200 SRM.

Part: ATTACH ANGLE — CORRODED (BS 1440-1500) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON INTERCOSTAL ANGLES (2 EAS) BTW STA 1440 TO 1460 ALSO BTW 1480 TO 1500, ABOVE S-27R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00251: INTERCOSTAL BTW STA 1440 TO 1460 ALSO BTW 1480 TO 1500, ABOVE S-27R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2522262)

Part: MOUNT — CORRODED (BS 140-1440) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 IN REFERENCE NRC 265 CORROSION ON MOUNT FITTING (1 EA) FROM STA. 1400 TO 1440 AT AFT CARGO COMPARTMENT (LOWER SILL AREA). IT IS OUT OF LIMITS PER B757-200 SRM. CORRECTIVE ACTION: SUMMARY OF NRC 00703: FITTING WAS REPLACED PER B757-200 SRM. (2523459)

Part: WEB — CORRODED (BS 740-760) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORROSION IN WEB STA 740 AND STA 760 BETWEEN S-26R/S-27R. AT FWD CARGO COMPARTMENT. WEB STA 740 AND STA 760 BETWEEN S-26R/S-27R, WAS REPLACED PER B-757-200 SRM.

Part: SKIN — CORRODED (RT NR 10 SLAT) · airframe 83,196 hrs · 21,517 cycles

CORROSION ON LEADING EDGE OF SLAT#10 AT RH WING. SLAT #10 WAS REMOVED AND SERVICEABLE SLAT WAS INSTALLED UNDER AMDS CARD.

Part: PANEL — CORRODED (BS 1530-1640) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ALONG LH SIDE PANEL FROM STA. 1530 TO STA. 1640 AT BULK CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00176: SIDE PANEL FROM STA. 1530 TO STA. 1640 WAS FABRICATED PER DWG 146N5431 REV.C AND WAS INSTALLED PER SRM.

Part: SNUBBER — OUT OF LIMITS (R1 DOOR) · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 IN REF. TO ROUTINE CARD 5211-3001-1R, STEP #3: MINIMUM EXTENSION PIN IS NOT CORRECT ON SNUBBER OF THE R1 PASSENGER DOOR. ROTATORY SNUBBER OUT OF LIMITS WAS REPLACED WITH SERVICEABLE ROTATORY SNUBBER PER B757-200 AMM 52-11 AND AMDS. (2518767)

Part: SUPPORT CHANNEL — CORRODED (BS 1460 S26L) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORROSION ON FRAME SUPPORT CHANNEL STA.1460 ABOVE S-26L AT AFT CARGO COMPARTMENT IS OUT OF WITHIN LIMITS PER B757-200 SRM. CORRECTIVE ACTION: SUMMARY OF NRC 00677. FRAME SUPPORT CHANNEL STA.1460 ABOVE S-26L AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 453N1817 REV D. AND B757-200 SRM. (2517517)

Part: STRAP — CRACKED (BS 365-377 LBL25) · airframe 83,196 hrs · 21,517 cycles

CRACKED STABILIZER STRAP, BS 365 - 377, LBL 25, IN THE NLG WHEEL WELL CEILING. THE STABILIZER STRAP WAS REPAIRED IAW SRM.

Part: DOOR SILL — CORRODED (BS 1340-1360) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORROSION ON R3 DOOR LOWER SILL AREA, FROM STA. 1340 TO 1360 AND RBL 63 AT AFT CARGO COMPARTMENT. THE DOOR SILL WAS REPLACED PER SRM.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORRODED SPLICE BS 1440 IN THE CARGO BAY. THE SPLICE WAS FABRICATED AND REPLACED IAW DWG AND SRM.

Part: ANGLE — CORRODED (CARGO BY) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORRODED INTERCOSTAL ANGLES IN THE BULK CARGO BAY. BS 1480 - 1500, S27L, AND BS 1540 - 1560, S27R & S27L. THE INTERCOSTAL ANGLES WERE REPLACED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 700-760 LBL45) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

CORRODED LH OTBD SEAT TRACK, BS 700 - 760 LBL 45, IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW SRM.

Part: WEB — CRACKED (BS 660-680 BL0) · airframe 83,196 hrs · 21,517 cycles

CRACK ON FLOOR WEB, BS 660 - 680, BL 0. THE WEB WAS REPAIRED IAW SRM.

Part: STRAP — CRACKED (BS 1280) · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CRACK ON STABILIZER STRAP STA 1280 AND LBL 45 AT AFT CARGO CEILING AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00237: STABILIZER STRAP STA 1280 AND LBL 45 AT AFT CARGO CEILING AREA WAS REPAIRED PER B757-200 SRM. (2512018)

Part: INTERCOSTAL — CORRODED (BS 1360-1380) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON INTERCOSTAL ANGLES (2 EAS) FROM STA 1360 TO 1380, BELO RH/LH SIDE PANELS AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00188: INTERCOSTAL ANGLES WERE REPLACED PER B757-200 SRM. (2512955)

Part: INTERCOSTAL — CORRODED (BS1420-1440 S29L) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 SECONDARY NRC, IN REF NRC 197. CORROSION ON INTERCOSTAL STA. 1420 TO 1440, S-29L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00680: INTERCOSTAL STA. 1420 TO 1440, S-29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 SECONDARY NRC, IN REF. NRC # 00671: CORROSION ON FLOOR BEAM (LWR FACE) AT STA 1681.8, BTW RBL 23 TO RBL 25.5. CORRECTIVE ACTION: SUMMARY OF NRC 00678: FLOOR BEAM (LWR FACE) AT STA 1681.8, BTW RBL 23 TO RBL 25.5. WAS REPAIRED PER B757-200 SRM. (2510410)

Part: PANEL — CORRODED (BS 1380-1440) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON RH SIDE PANEL FROM STA. 1380 TO 1440 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00195: RH SIDE PANEL FROM STA. 1380 TO 1440 AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG B757-200 SRM. (2508252)

Part: FLOOR SUPPORT — CORRODED (BS 1424) · corrosion level 2 · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 CORROSION ON FLOOR STRINGER RBL 16 (LWR SIDE ) STA. 1424 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 202: ZEE STRINGER AT RBL 16 BTW STA 1345 TO STA 1445 AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2508195)

Part: FRAME — NONE · airframe 83,196 hrs · 21,517 cycles

SHIP 6810 INITIAL INSPECTION: WEAR ON ANGLE (PREVIOUS REPAIR) AT PASSENGER CABIN FRAME, STA. 1280, ADJACENT TO S-12R AND S-10R. CORRECTIVE ACTION: SUMMARY OF NRC00416: ANGLE WAS REPLACED PER B757-200 SRM AND ER/A 553831-14AD REV. ORIG. SECTION 1 PERMANENT REPAIR. (2506339)

Part: SKIN — DAMAGED (RT WING) · airframe 83,196 hrs · 21,517 cycles

REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589150-14AD REV. A. VISUAL INSPECTION WAS ACCOMPLISHED ON OPEN HOLES #7 AND #14 , AT RH ENG DRAG FTG AND CORROSION WERE FOUND. PER ER/A 589150-14AD REV: A SECTION IV NDT TECHOPSMX A.M.M. 207813 14-DEC-22 (ET) HFEC OPEN HOLE INSPECTION WAS ACCOMPLISHED ON OPEN HOLES 1, 2, 3, 4, 5, 6, 8, 9, 10, 11, 12, 13, 15, 16, 17 AND 18 NO CRACKS WERE FOUND PER ER/A 589150-14AD REV.A SECTION IV SUMMARY: REPETITIVE BHEC INSPECTION WERE PERFORMED PER ER/A 589150-14AD REV A SECTION IV, ADDITIONAL FINDINGS WERE REPAIRED PER AMDS.

Part: NONE — NONE · airframe 82,568 hrs · 21,374 cycles

SHIP 6810 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS: 2R. CORRECTIVE ACTION: REPOSITIONED DOOR LINER, OPS CHECKS OK. (2359788)

Part: NONE — NONE · airframe 81,712 hrs · 21,178 cycles

SHIP 6810 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:604. CORRECTIVE ACTION: CLEARED DEBRIS OFF ARM KNOCKER. DOOR ARM KNOCKER OPERATING NORMAL IAW B757 AMM 52-11. (2227871)

Part: PANEL — MISALIGNED · airframe 81,610 hrs · 21,157 cycles

SHIP 6810 R2 DOOR KNUCKLE KNOCKER NOT WORKING. CORRECTIVE ACTION: ADJUSTED PANEL AROUND THE KNUCKLE KNOCKER WAS TOUCHING AS NECESSARY. OPS CHK GOOD. (8809888)

Part: FAN — FAILED (RECIRCULATION) · airframe 80,881 hrs · 20,995 cycles

SHIP 6810 -FUMES / DE- DUE TO ELECTRICAL SMOKE ODOR IN THE CABIN AND FLIGHT DECK. CORRECTIVE ACTION: VERIFIED NO FLUID CONTAMINATION. FOUND RT RECIRC FAN SEIZED AND INOP. REPLACED RIGHT FAN AND REPLACED THE FILTERS FOR THE LEFT AND RIGHT. C/W NO-GO ODI PROCEDURES.

Part: NONE — NONE · airframe 80,955 hrs · 21,011 cycles

SHIP 6810 DOOR HANDLE TRIM COVER PLATE DAMAGED / MISSING / LOCATIONS:601. CORRECTIVE ACTION: INSTALLED MISSING DOOR HANDLE TRIM COVER PLATE PER B757 AMM 52-10. (2113862)

Part: NONE — NONE · airframe 80,791 hrs · 20,973 cycles

'SUPPLEMENTAL INFORMATION' SHIP 6810 DOOR HANDLE DOOR 2(L) TRIM COVER PLATE MISSING. CORRECTIVE ACTION: REMOVED COVER FROM 1(L) DOOR HANDLE AND REPLACED IN 2(L) DOOR. INSTALLED MISSING TRIM ON DOOR HANDLE PER B757 AMM 52-02. (8571414)

Part: NONE — NONE · airframe 80,611 hrs · 20,927 cycles

SHIP 6810 L1 DOOR GUST LOCK RELEASE MISSING. CORRECTIVE ACTION: CLEANED, LUBE, EXERCISED GUST LOCK; OPS NORM. (8494434)

Part: NONE — NONE · airframe 80,519 hrs · 20,907 cycles

SHIP 6810 1L DOOR HDL NOT FLUSH. CORRECTIVE ACTION: 1L DOOR HANDEL RE CORRECTED OK FOR SVC. (8494409)

Part: NONE — NONE · airframe 80,111 hrs · 20,817 cycles

SHIP 6810 EMER LIGHT ABOVE SEAT 26D IN-OP. (LOCATED ON CURVED EDGE OF BAG STOWAGE BIN). CORRECTIVE ACTION: R/R O/H LIGHT AT 26D IAW B757 AMM 35-51, OPS CHK GOOD. (8407561)

Part: NONE — NONE · airframe 79,984 hrs · 20,784 cycles

SHIP 6810 FOUND FIRST CLASS EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: REPLACED BATTERY PACK PER B757 AMM 33-51. OPS CK GOOD. (8407515)

Part: SWITCH — ABNORMAL (EMERGENCY LIGHTS) · airframe 79,244 hrs · 20,625 cycles

SHIP 6810 DURING LIGHTS TEST FOUND DOOR L1 EMERGENCY LIGHT SWITCH INOP. CORRECTIVE ACTION: REMOVED, REPLACED AND OPS CHKED DOOR L1 EMERGENCY LIGHT TEST SWITCH IAW B757 AMM 25-21 AND WDM 33-51 OPS CHK GOOD. (7958630)

Part: NONE — NONE · airframe 82,641 hrs · 21,391 cycles

SHIP 6810 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589148-14AD. CORRECTIVE ACTION: REF ERA 589148-14AD. (1701456)

Part: NONE — NONE · airframe 82,641 hrs · 21,391 cycles

SHIP 6810 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589150-14AD. CORRECTIVE ACTION: REF ERA 589150-14AD. (1701263)

Part: BUSHING — DAMAGED (NR 2 NACELLE) · corrosion level 2 · airframe 77,102 hrs · 20,149 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION ON #2 PYLON UPPER LINK PIN PUSHING. BUSHING REPLACED. (LP1693444)

Part: SKIN — DENTED (BS 550 S18-19R) · airframe 83,196 hrs · 21,517 cycles

DENT ON SKIN FWD OF CARGO DOOR BS 550 BETWEEN STRINGERS 18-19R. SKIN REPAIRED IAW ER/A 603670-14 REV.ORIGINAL SECTION I.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,661 hrs · 20,046 cycles

DURING WALK AROUND FOUND 1 SECTION OF EMERGENCY LIGHTS NOT WORKING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: SCREW — MISSING (R4 DOOR) · airframe 76,293 hrs · 19,966 cycles

(AIRCRAFT 6810, L/P 5137550) FOUND 2 MISSING SCREWS ON DOOR 4R OUTSIDE BUTTERFLY HANDLE. CORRECTIVE ACTION: INSTALLED SCREWS OK FOR SERVICE.

Part: CONTROL ROD — NOT REPORTED (R4 DOOR SLIDE) · airframe 76,144 hrs · 19,936 cycles

SHIP 6810 4R PASSENGER DOOR SLIDE ARMED WARNING FLAPPER DAMAGED. CORRECTIVE ACTION: R/R CONTROL ROD PER B757 AMM 52-11. DOOR INDICATOR OPS NORMAL. (5137501)

Part: PROXIMITY SENSOR — DEFECTIVE (R1 DOOR) · airframe 74,398 hrs · 19,590 cycles

SHIP 6810 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: R/R 1R LEFT PROXIMITY SENSOR AS PER AMM 25-66. OPS CHK GOOD. (1248788)

Part: SENSOR — OBSTRUCTED (R1 DOOR) · airframe 73,884 hrs · 19,494 cycles

SHIP 6810 DOOR 1 R ARMED LIGHT NOT ILLUMINATED WITH DOOR ARMED. CORRECTIVE ACTION: REMOVED DEBRIS FROM R1 AFT GIRT BAR SENSOR. LIGHT CKS NML. (5990220)

Part: RESOLVER — FAILED (EEC) · airframe 72,262 hrs · 19,195 cycles

CREW PERFORMED A RTO DUE TO NO RIGHT ENGINE THROTTLE RESPONSE FROM IDLE. FOUND RH ENGINE INBOARD SLEEVE MIDDLE LOCKING ACTUATOR BROKEN AND BAD RESOLVER INPUT TO EEC. REPLACED MIDDLE LOCKING ACTUATOR IAW AMM 78-31. PERFORMED, TESTED AND ENGINE RUN WITH CONFIRMED INCREASE OF EPR. OK FOR SERVICE.

Part: PROXIMITY SENSOR — GROUNDED (L2 DOOR SLIDE) · airframe 71,782 hrs · 19,102 cycles

SHIP 6810 FOUND L2 DOOR SLIDE LIGHT STAYS ILLUMINATED. T/S PER B757 FIM 25-66-00-815-802. FOUND PROX SENSOR S10221 CAUSING GROUND. R/R SENSOR PER B757 AMM 25-66. (4734310)

Part: DOOR SILL — CORRODED (FWD CARGO BAY) · airframe 71,348 hrs · 19,013 cycles

SHIP 6810 AFT CARGO LOWER DOOR SILL, FORWARD AREA, CORROSION ON LOWER BEAM FUS STA.1380 STRINGER 27-RT. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0261:2020-2317/011 00271 C/W ERA 574069-14 REV ORIG. (0880072)

Part: SINK — CLOGGED (AFT LAVATORY) · airframe 71,127 hrs · 18,971 cycles

SHIP 6810 -DIV- DIVERTED INTO SLC DUE TO AFT LAV SINKS OVERFLOWING. WATER HAS BEEN SHUT OFF TO THE AFT SINKS. CORRECTIVE ACTION: FOUND BOTH SINKS CLOGGED, UNCLOGGED AFT RIGHT DRAIN. MEL'D AFT LEFT DRAIN. AFT LEFT DRAIN CLEARED IN SFO.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 18 DE) · airframe 70,392 hrs · 18,832 cycles

(AIRCRAFT 6810, L/P 4723746) O2 MASK DOOR AT SEATS 18 DE FELL OUT. NEED TO BE RESTOWED. RESTOWED O2 MASKS PER B757 AMM 35-11.

Part: ENGINE — ODOR (NR 2) · airframe 70,392 hrs · 18,832 cycles

(AIRCRAFT 6810, L/P 4723748) FA'S REPORTED STRONG " DIRTY SOCK" SMELL ON DESCENT. STRONGER TOWARD THE REAR OF THE AIRCRAFT. SEE LOG PAGE # 4723736. REFERENCE LP 0758072 - REPLACED NBR 2 ENGINE. PERFORMED SECTION II PERMANENT REPAIR PER ERA 571856-14 REV. ORIGINAL. OPS NORMAL. OK TO CLOSE THIS LOG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,392 hrs · 18,832 cycles

(AIRCRAFT 6810, L/P 4723744) EMERGENCY LIGHT AT R2 DOOR INOP (FORM SEAT 19F TO 25F). REMOVE AND REPLACE EMERGENCY BATTERY AT R2 DOOR, NO FIX. REMOVE AND REPLACE EMERGENCY BATTERY SUPPLY CHARGER PER B757. AMM 33-51. OPS CHECK OK.

Part: CHECK VALVE — FAILED · airframe 69,887 hrs · 18,738 cycles

LOST PRESSURIZATION AT FL 340, 2 HOURS. INTO FLIGHT UNCOMMANDED. CABIN ALTITUDE 10,000, DIFFERENTIAL 6.2, SHORTLY AFTERWARD RED CABIN ALTITUDE EICAS. OXYGEN MASKS DONNED AND AIRCRAFT FLOWN TO 10,000 FT. AIRCRAFT PRESSURE CLIMBED AND DESCENDED +/- 2,000 FT WHILE LEVEL. CABIN CLIMBED 1,000 FT/MIN WHILE DESCENDING OUT OF 10,000. WAS UNABLE TO CLOSE THE OUTFLOW VALVE MANUALLY ONLY TO 90%. TROUBLESHOT IAW NO GO ODI 2132. FOUND CLAMP DETACHED ON THE LT PACK OUTLET, CHECK VALVE LEAKING, AND B-NUT LOOSEON REHEATER LINE. TIGHTENED BOTH IAW AMM 20-11-00. BITE TESTED BOTH CPC IAW AMM 21-30-00-815-002, LOW INFLOW FAULT. LEFT PACK CHECK VALVE FAILED. R & R THE CHECK VALVE IAW AMM 21-51-1, PB401. R & R TWO PRESSURE CONTROLLERS IAW AMM 21-51-00-755-622 WITH NO FAULTS. EXCESSIVE CABIN PRESSURE LEAKAGE CHECKED IAW AMM 05-51-24. LEAKS WITHIN LIMITS. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — DETACHED (SEAT 44) · airframe 68,054 hrs · 18,400 cycles

EMERGENCY EXIT LIGHT AT SEAT 44 WAS FOUND DETATCHED FROM THE SEAT. SECURED THE LIGHT ASSY.

Part: COLLAR — WORN (L2 DOOR) · airframe 67,693 hrs · 18,325 cycles

ON ARRIVAL PHL FOUND L2 CANNOT CLOSE OR OPEN WITH EXTERIOR HANDLE. INSIDE HANDLE WORKS NORMALLY FOR OPEN AND CLOSED. FOUND EXTERIOR HANDLE ROLLER FITTING REQUIRING SHIMS ALSO FOUND CENTER SHAFT CLUTCH COLLAR WORN. REPLACED CLUTCH COLLAR AND SHIMMED ROLLER FITTING PER AMM 52-11.

Part: COVER — BROKEN (R4 DOOR HANDLE) · airframe 67,407 hrs · 18,268 cycles

R4 DOOR HANDLE TRIM COVER PLATE DAMAGED. REPLACED THE DOOR HANDLE. CHECKED OK IAW AMM 52-10.

Part: INDICATOR — OUT OF ADJUST (R4 DOOR) · airframe 66,965 hrs · 18,175 cycles

(AIRCRAFT 6810, L/P 3680689) DOOR 4 R KNUCKLE KNOCKER COMES OUT TOO FAR WHEN THE DOOR IS ARMED. ADJUSTED. OPS OK.

Part: LANYARD — UNSECURE (DOOR SLIDE) · airframe 65,510 hrs · 17,892 cycles

AFT RIGHT ENTRY DOOR SLIDE CORD PERTRUDING FROM UNDER DOOR. AFT RIGHT DOOR BUSTLE REMOVED AND RE INSTALLED. DOOR ARMING AND DISARMING, OPENING AND CLOSURE CHECKED GOOD IAW MM 52-20.

Part: SHAFT — WORN (L2 DOOR HANDLE) · airframe 63,590 hrs · 17,505 cycles

CABIN SERVICE COULD NOT CLOSE THE L2 DOOR PROPERLY WITHOUT SIDE HANDLE. REMOVED EXTERIOR AND INTERIOR HANDLES IAW AMM 52-11. FOUND CLUTCH COLLAR & CENTER SHAFT WORN. REPLACED IAW AMM 52-11 809006. OPS CHECKED GOOD, OK FOR SERVICE.

Part: ADAPTER — CRACKED (LT WING) · airframe 63,097 hrs · 17,382 cycles

LT WING TIP ADAPTOR PLUG UPPER INBD FLANGE CRACKED NOTICED UPON WINGLET REMOVAL. TRIMMED OUT DAMAGE 2 3\8"X3\4" AND REPAIRED LEFT WING TIP ADAPTOR PLUG UPPER I\B FLANGE IAW ERA 553834-14 REV O.

Part: FRAME — GOUGED (FUSELAGE) · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN STA 1280 BETWEEN STR 10R-11R GOUGED. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS REF SRM. REPAIRED FRAME IAW ERA 553831-14AD REV O.

Part: SKIN — DAMAGED (LT WING LE) · airframe 63,097 hrs · 17,382 cycles

LT WING FIXED L/E, DAMAGED NOTICED ON THE FIRST TRACK LOWER CUT-OUT FOR THE NR 5 SLAT. REPAIRED IAW ER/A 401339-14MA & SRM 51-70-17 PAR.4.G.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN BS 1640 BETWEEN LBL 44 - 53 TEE CAP ON FLOORBEAM CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM TEE IAW SRM.

Part: FLOORBEAM — CORRODED (MAIN CABIN) · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN TEE CAP ON FLOORBEAM CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. REPAIRED THE FLOORBEAM TEE IAW ERA 481634-14MA REV A.

Part: STRUCTURE — DAMAGED (LT WING SLAT) · airframe 63,097 hrs · 17,382 cycles

LEFT WING NR 5 SLAT, LOWER L/E PLASTIC STRIP IS PULLED AND CHIPPED. REPAIRED THE SLAT IAW SRM.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN FLOORBEAM TEE CORRODED BS 365, BL 0 - RBL 60. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR AND INSTALLED IAW SRM AND ERA 481634-14MA REV A.

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN RIGHT SEAT TRACK FROM BS 1640-1540 CORRODED. FOUND OUT OF ALLOWABLE LIMITS. REMOVED AND REPLACED MAIN CABIN SEAT TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN BS 1640, RBL 22 - 55 FLOORBEAM TEE CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM IAW ERA481634-14MMA REV A.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN FLOORBEAM BS 377 BETWEEN BL0 - LBL 55 CORRODED AROUND SCREW HOLES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED THE FLOORBEAM IAW ERA 481634-14MA REV A.

Part: CUSP WEB — CORRODED (BS 604-618) · corrosion level 2 · airframe 63,097 hrs · 17,382 cycles

CORROSION FOUND UNDER FLOOR CUSB WEB BS 604 - 618. REMOVED THE CORROSION IAW SRM AND FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR AND INSTALLED IAW DWG.

Part: SEAT TRACK — DAMAGED (BS 1640-1540) · corrosion level 2 · airframe 63,097 hrs · 17,382 cycles

MAIN CABIN RIGHT OTBD SEAT TRACK FROM BS 1640-1540 OUT OF LIMITS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM.

Part: SKIN — DENTED (LT WING SLAT) · airframe 63,098 hrs · 17,383 cycles

LEFT WING NR 5 SLAT, DENTED ON TRAILING UPPER EDGE, NEAR INBD SECTION OF SLAT. REMOVED DAMAGE AND ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-43-02, REPAIR 1, FIG 201, SRM 51-70-10, REPAIR 3, AND SRM 51-70-10.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 60,662 hrs · 16,935 cycles

R3 EMERGENCY EXIT SIGN LENS MISSING. INSTALLED EXIT SIGN LENS.

Part: LINE — FAILED (HYD SYSTEM) · airframe 58,567 hrs · 16,465 cycles

CREW PERFORMED ATB DUE TO LT HYD SYS FAILURE. NR 5 AND NR 6 TIRES ALSO FOUND TO HAVE FAILED. DECLARED AN EMERGENCY WITH ATC, ARFF MET THE ACFT AFTER STOPPING ON THE RUNWAY, AND ACFT WAS TOWED OFF THE RUNWAY. REPLACED A HYDRAULIC LINE FROM THE TILT PRESSURE SWITCH. INSTALLED NEW EDP CASE DRAIN FILTER. REPLACED THE ACMP CASE DRAIN AND PRESSURE /RETURN FILTERS. R & R THE ACMP AND EDP IAW AMM 29-11. PTU FILTER CHECKED AND CLEAN. OPS CK AND LEAK CK GOOD. REF ERA 541080-14 FOR WORK PERFORMED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,515 hrs · 15,880 cycles

TWO RIGHT & TWO LEFT EMERGENCY OVERHEAD ISLE LIGHT INOPERATIVE. R & R BATTERY CHARGER ASSY IAW AMM 33-51. FOUND GD502-DV LOOSE. SECURED GROUND. LIGHT TEST OK. 6745540.

Part: WEDGE — DAMAGED (LT WING) · airframe 53,790 hrs · 15,513 cycles

LEFT WINGLET T/E WEDGE FOUND TO HAVE LIGHTING STRIKE DAMAGE. C/W PERM REPAIR IAW ERA 529074-14, REV ORIGINAL.

Part: SKIN — DAMAGED (LT WING) · airframe 53,726 hrs · 15,500 cycles

DURING WALK AROUND, FOUND LIGHTNING STRIKE ON OTBD OF LT WINGLET. DAMAGED REPAIRED IAW ER/A 529074-14.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,570 hrs · 15,468 cycles

EMERGENCY LIGHTS BETWEEN ROWS 19-26 INOPERATIVE. R & R BATTERY CHARGER ASSY IAW AMM 33-52.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 51,875 hrs · 15,141 cycles

FIRST CLASS ROW 4 RT SEAT MOUNTED EMERGENCY LIGHT SIDE CONNECTOR BROKEN. R & R EMERGENCY LIGHT CONNECTOR AT ROW 4 RT IAW SWPM 20-63-00 PERFORMED SATISFACTORY OPS TEST OF EMERGENCY LIGHTS IAW AMM 31-51-00, NO DEFECTS NOTED AT THIS TIME.

Part: FAILSAFE — CORRODED (BS 1280) · corrosion level 2 · airframe 51,875 hrs · 15,141 cycles

FRAME FAILSAFE IN AFT CARGO BAY AT BS 1280 CORRODED BETWEEN STRINGERS 20-24L. CUT OUT DAMAGED SECTION OF FAILSAFE, 16.6" LONG, FABRICATED NEW FAILSAFE SECTION AND FILLER. INSTALLED REPAIR ALL IAW ER/A 523955-14.

Part: TRANSITION PANEL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 51,875 hrs · 15,141 cycles

AFT CARGO BAY TRANSITION PANEL BS 1380 LT HAS SURFACE CORROSION. CUTOUT DAMAGED AREA, FABRICATED NEW TRANSITION PANEL AND INSTALLED REPAIR PARTS ALL IAW SRM. HEAT TREATED NEW TRANSITION PANEL TO 7075 T6 IAW FAS ENG REPORT 2-37153-801A, REV A.

Part: SKIN — DAMAGED (BS 1410) · airframe 51,875 hrs · 15,141 cycles

FASTENER HOLE FOR ADAPTER RING AT STRINGER 1, BS 1410. FABRICATED & INSTALLED FILLER IAW ER/A 522817-14. PART II CUT OUT DAMAGED AREAS OF SKIN BETWEEN BS 1360-1380 S2-3R.

Part: STRUCTURE — CHAFED (BS 1520) · airframe 51,875 hrs · 15,141 cycles

AFT CARGO BAY AT BS 1520, S24 - 27R CHAFED. CUTOUT DAMAGED AREA OF FRAME FABRICATED REPAIR ANGLE. INSTALLED REPAIR ANGLE ALL IAW ER/A: 522809-14, REV ORIGINAL.

Part: SEAT TRACK — CORRODED (BS 700) · airframe 51,875 hrs · 15,141 cycles

MAIN CABIN SEAT TRACK AT BS 700, RBL 24.5 HAS CORROSION APPROXIMATELY 12 INCHES LONG. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW SRM 53-30-52, FIG 1 AND INSTALLED IAW 51-40-02, PAR. 7

Part: THRESHOLD — CORRODED (BS 1380-1420) · airframe 51,875 hrs · 15,141 cycles

AFT CARGO BAY THRESHOLD BETWEEN BS 1380-1420 CORRODED. REMOVED DAMAGED THRESHOLD IAW SRM 51-40-02, PAR 4, 7, FABRICATED NEW THESHOLD IAW SRM 51-40-05, 51-40-08 AND DWG 146N5371, REV F. INSTALLED IAW SRM 51-40-02, PAR 4, 7.

Part: TRANSITION PANEL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 51,875 hrs · 15,141 cycles

AFT CARGO BAY RT SIDE TRANSITION PANEL HAS CORROSION, FWD OF BS 1380. CUTOUT DAMAGE SECTION, FABRICATED REPAIR SPLICE AND NEW SECTION OF TRANSITION PANEL IAW IAW SRM 53-00-53, FIG 201, REP 2. HEAT TREATED REPAIR IAW FAS ENG REPORT 2-37153-801A, REV A. INSTALLED REPAIR IAW SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 1240-1310) · corrosion level 2 · airframe 62,610 hrs · 17,288 cycles

TRANSITION PANEL FROM BS 1240 TO 1310 CORRODED. REPLACED THE TRANSITION PANEL IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 1280-1300) · corrosion level 2 · airframe 51,875 hrs · 15,141 cycles

INTERCOSTAL HAS CORROSION AT BS 1280-1300 BETWEEN S25-26L. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02, FABRICATED NEW IAW SRM 51-30-01 AND DWG 46N5397 REV. B AND SRM 53-60-04 AND INSTALLED IAW SRM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,459 hrs · 14,461 cycles

DURING TRANSIT CHECK MX FOUND EMERGENCY LIGHTS AT 2 & 4 AND DOOR AT 1R INOPERATIVE. MX REPLACED BATTERY PACK FUSE, R & R SLIDE DOOR LIGHT AT 1R, AND LIGHT ASSY AT 2/4 IAW WDM. OPERATION OF LIGHTS NOW CHECK OK.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 46,648 hrs · 14,095 cycles

AFTER TAKEOFF, EMERGENCY UPPER LIGHTS FROM ROW 36 AFT AND LIGHTS AROUND DOOR ILLUMINATED. AFTER AN HOUR THE LIGHTS WENT OUT. MX CLEANED CONNECTOR AT M736 BATTERY PACK. OPERATED NORMAL OF FOR SERVICE.

Part: LIGHT — UNKNOWN (ROW 36) · airframe 46,623 hrs · 14,090 cycles

AFTER TAKEOFF, EMERGENCY LIGHTS ILLUMINATED FROM ROW 36 TO THE AFT ROWS. THE LIGHTS WENT OUT IN CRUISE AND AFTER LANDING CAME BACK ON. MX TESTED EMERGENCY LIGHTS ALL NORMAL. LIGHTS AGREE WITH SWITCH POSITION.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 40,779 hrs · 12,946 cycles

RAMP REPORTED HOLE IN AFT CARGO BIN FLOOR. FOUND 1 INCH HOLE IN AFT CARGO BIN FLOOR JUST FWD OF DOOR. COMPLIED WITH ERA 489384-14MA SECTION 1.

Part: FRAME — DENTED (BS 540 S24-25L) · airframe 38,348 hrs · 12,466 cycles

FWD CARGO FRAME DENTED IN 2 PLACES ON UPPER FLANGE AND RADIUS, STA 540 FROM STR 24 TO 25 LT. REPAIRED IAW ER/A 488006-14 REV, ORIGINAL.

Part: FRAME — DENTED (BS 520 S24-25L) · airframe 38,348 hrs · 12,466 cycles

FWD CARGO FRAME DENTED ON UPPER FLANGE STA 520 FROM 24 TO 25 LT. REPAIRED IAW ER/A 488097-14.

Part: CREASE BEAM — CORRODED (BS 333-377) · airframe 38,348 hrs · 12,466 cycles

MAIN CABIN CREASE BEAM INNER CHORD CORRODED STA 333-377, LT AT L1 DOOR OPENING. REPLACED CHORD.

Part: FRAME — DENTED (BS 660 S23-24L) · airframe 38,348 hrs · 12,466 cycles

FWD CARGO FRAME DENTED STA 660 ON UPPER FLANGE BTWN STR 23 & 24 LT. REPAIRED IAW 53-00-07, FIG 201, REPAIR 5.

Part: SEAT TRACK — CRACKED (BS 521 LBL 24) · airframe 38,348 hrs · 12,466 cycles

MAIN CABIN SEAT TRACK CRACKED IN FWD LOWER RADIUS STA 521, LBL 24. REPAIRED IAW SRM 53-00-52, FIG 201.

Part: SEAT TRACK — CORRODED (BS 521 LBL 24) · airframe 38,348 hrs · 12,466 cycles

MAIN CABIN SEAT TRACK CRACKED IN FWD LOWER RADIUS STA 521, LBL 24. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR III.

Part: PLATE — CORRODED (BS 1680-1720) · airframe 38,348 hrs · 12,466 cycles

MAIN CABIN AFT DECK PLATE CORRODED STA 1680-1720, BL 0-LBL 59. REPAIRED IAW SRM 53-60-51, ALTERNATIVE II, FIG 201, PG 202, STEP 10.

Part: STRUCTURE — CORRODED (BS 345-377) · airframe 38,348 hrs · 12,466 cycles

MAIN CABIN BL 0 CHORD CORRODED STA 345-377. REPLACED CHORD.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 38,348 hrs · 12,466 cycles

MAIN CABIN FLOORBEAM HAS AREAS OF CORROSION STA 1640, BL0 TO LBL 62. REPAIRED IAW ERA 481634-14MA.

Part: GIRT BAR — CORRODED (R4 DOOR) · airframe 38,348 hrs · 12,466 cycles

R4 GIRT BAR HAS CORRODED RESTRAINT. REPLACED RESTRAINT.

Part: BRACKET — GOUGED (ESCAPE SLIDE) · airframe 38,348 hrs · 12,466 cycles

L2 DOOR ESCAPE SLIDE SPADE BRACKETS ARE GOUGED 2 EA. R & R BOTH BRACKETS AFT BRACKET PN416N2201-16, FWD BRACKET PN 416N2201U17

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 33,168 hrs · 11,473 cycles

DUE TO HISTORY OF RT ENG PRI / SEC CONTROL MSG. REPLACED NR 2 ENGINE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: GCU — MALFUNCTIONED (LT ENGINE) · airframe 32,196 hrs · 11,295 cycles

LEFT ENGINE DRIVEN GEN DOES NOT POWER ELECTRICAL SYSTEM AFTER LEFT ENG START APU WAS SHUTDOWN AND ALL ELECTRICAL POWER WAS LOST LT/RT GEN SHOWS GCU ON BPCU. CLEAR BPCU AND RESEAT LT GCU RAN LT AND RT ENG GEN OPS AND INDICATION NORMAL OIL LEVEL NORMAL ON LT IDG ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 31,943 hrs · 11,257 cycles

LEFT ENG DRIVEN GEN DOES NOT POWER ELECTRICAL SYSTEM AFTER LEFT ENG START APU WAS SHUTDOWN AND ALL ELECTRICAL POWER WAS LOST. CA-LT/RT GEN SHOWS GCU ON BPCU. CLEAR BPCU AND RESEAT LT GCU - RAN LT AND RT ENG GEN OPS AND INDICATION NORMAL OIL LEVEL NORMAL ON LT IDG. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: FUEL CONTROL — MALFUNCTIONED (NR 2 ENGINE) · airframe 31,770 hrs · 11,223 cycles

DURING CLIMB, WE GOT 2 STATUS MESSAGES. RT ENG PRI/SEC CONT. WILL NOT ERASE. IAW FIM, NEEDS FCU REPLACED. REPLACED NR 2 ENG FCU IAW JIC 5034. RAN ENG AT IDLE, LEAK OK. PERFORMED ENG HIGH PWR RUN-UP IAW JIC 5034. REPLACED THE STATOR VANE ACTUATOR IAW JIC 7021. ENG RUN-UP- LEAK OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: IDG — FAILED (LEFT) · airframe 29,307 hrs · 10,737 cycles

AFTER PUSHBACK ON L ENGINE START AT 50 PERCENT N2 L GEN FAILED W ASSOC L BUSS TIE ISOLATION LIGHT. REPLACED K108 RELAY, NO HELP. FOUND B PHASE FROM IDG BAD. REPLACED IDG LEAK CK OK, OP CK OK.

Part: WIRE — DAMAGED (ANTI SKID SYS) · airframe 27,317 hrs · 10,237 cycles

AFTER PUSHBACK, EICAS ANNUN ANTI-SKID AND STATUS ANTI-SKID AND ALTN ANTI-SKID MSG WAS INTERMITTENT. BITE CK NR 1 TDCR. REPLACED TDCR AND CHECKED RES OF PINS 1 TO 3. CHECKED WIRING FROM E5 TO TDCR CKS OK SUSPECT CONTROL UNIT. RETERMINATED FERRULE AT REAR LANDING GEAR JUNCTION BOX, CHECKS OK.

Part: LIGHT — LOOSE (CABIN)

DFW - EMERGENCY PATH FLOOR LIGHTS NEAR ROW 12 AND 13DEF INOPERATIVE. SECURED EMERGENCY PATH FLOOR LIGHTS NEAR ROWS 12 AND 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - BULLNOSE EMERGENCY LIGHT AT SEATS 14C AND 18C INOPERATIVE. REPLACED BATTERY PACK FOR BULLNOSE EMERGENCY LIGHT AT SEATS 14C AND 18C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — BENT (GIRT BAR) · airframe 13,877 hrs · 4,759 cycles

THE EVACUATION SLIDE LEAF RETENSION SPRINGS WERE REPLACED ACCOUNT BENT AT THE L1 AND R2 CABIN DOORS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,775 hrs · 3,568 cycles

THE EMERGENCY LIGHT AT THE NUMBER 2 CABIN DOOR ON THE RIGHT SIDE, WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 11-12-00 LAX.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 10,313 hrs · 3,392 cycles

DURING CHECK-C MAINT FOUND INTERIM FUSELAGE SKIN REPAIR INSTALLED AT STA 405, BETWEEN STRINGER 10 AND 11 LEFT. ACCOMPLISHED EMLR 71586 AND INSTALLED PERMANENT REPAIR PER SRM 53-00-01, FIG 204.

Part: ENGINE — FAILED (RT ENGINE) · airframe 6,760 hrs · 2,256 cycles

DURING CLIMB CREW HEARD A LOUD BOOM AND THE RT ENG STARTED TO SPOOL DOWN. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO SFO. THE ENGINE WAS CHANGED. CHECK-C 11-12-00 LAX.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 5,283 hrs · 1,808 cycles

DURING CHECK-C MAINT ON RT WING T/E FLAP INBOARD FLAP UNDERSIDE WAS PUNCTURED 2.00 BY 0.50, AFT OF LANDING GEAR IN AFT FLAP CUTOUT. INSTALLED 6 INCH DIA REPAIR PER SRM 51-70-07. PROTECTION AND CONDUCTIVE COATING APPLIED PER NON-ROUTINE CARD.

Part: CONTACTOR — DIRTY (SLIDE LIGHT) · airframe 5,214 hrs · 1,792 cycles

THE EMERGENCY SLIDE DOOR LIGHT WAS INOPERATIVE ON THE R1, R2, L1, L2 AND L4 DOORS, AND AT ROW 21 RT SIDE AND ROW 29 LT SIDE. CLEANED LIGHT CONTACTS AT R1, R2, L1, L2, AND L4 DOORS, AND RESEATED THE LENS ASSEMBLY AT ROWS 21 RT SIDE AND 29 LT SIDE. NO CHECK-C.

Part: BULB — FAILRED (R1 & R4 DOORS)

THE EXTERIOR EMERGENCY LIGHTS AT THE NUMBER 1 AND 4 DOORS, RT SIDE, WERE INOPERATIVE. REPLACED THE BULB IN EACH.

Part: LIGHT — INOP (CABIN)

THE EXTERIOR EMERGENCY LIGHT AT THE NUMBER 2 CABIN DOOR, RT SIDE, WAS FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND BULB, NO HELP. DEFERRED CORRECTIONS PER MEL. ON ARRIVAL AT THE NEXT STATION THE LIGHT WAS FOUND OPERATIVE.

Part: GIRT BAR — DIRTY (PAX DOOR)

THE LEFT FORWARD CABIN DOOR ESCAPE SLIDE DID NOT ARM AFTER THE DOOR WAS CLOSED. FOUND DEBRIS WAS UNDER THE GIRT BAR, BLOCKING GIRT BAR ENGAGEMENT. REMOVED THE DEBRIS.