N706TW

Part: FITTING — FOD (GIRT BAR) · airframe 102,400 hrs · 26,793 cycles

F/A ADVISES 2L DOOR APPEARS TO NOT ARM PROPERLY AT PUSHBACK. FOUND FWD GIRT BAR FITTING NOT DISENGAGING. CLEANED DEBRIS AND LUBRICATED DOOR FITTINGS. ALL CHECKS AND INDICATIONS NORMAL REF B757 AMM 25-66. (7715830)

Part: SLIDE — NO TEST (ZONE 800) · airframe 101,816 hrs · 26,546 cycles

DURING SCHEDULED TEST DEPLOYMENT OF L3 SLIDE, SLIDE FAILED TO FULLY EXTEND. REPLACED SLIDE REF JOBS 4 AND 10 ON WORK PACKAGE. (7620693)

Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 101,693 hrs · 26,472 cycles

L4 CABIN DOOR KNUCKLE KNOCKER NOT COMING OUT FULLY WHEN F/A ARMED THE DOOR. CLEARED OBSTRUCTION TO RESTORE NORMAL FUNCTION TO DOOR (4L) 4R POS 608 CABIN DOOR "KNUCKLE KNOCKER". OP CHK NORMAL. (6709475)

Part: LIGHT — DAMAGED (ZONE 200) · airframe 101,666 hrs · 26,452 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED/INOP AT LOCATIONS:41D. RE-SECURED PANEL BELOW OVHD BIN ON 41D AS PER B757 AMM 25-23, A/C OK FOR SVC. (LP 1202913)

Part: SWITCH — FAULTED (ZONE 800) · airframe 100,983 hrs · 26,105 cycles

6804 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S/ 1 RIGHT SLIDE LIGHT. CORRECTIVE ACTION: R/R "SLIDE" LIGHT SWITCH AS REQ'D. OPS NML. (1043774)

Part: LIGHT — DETACHED (ZONE 200) · airframe 100,686 hrs · 25,958 cycles

SHIP 6804 2 LEFT EXIT LIGHT FELL OFF. CORRECTIVE ACTION: REINSTALLED 2L EXIT LIGHT COVER AS REQ. (7425978)

Part: LINE — UNSECURE (L4 SLIDE) · airframe 100,635 hrs · 25,943 cycles

SHIP 6804 4L DOOR MOORING LINE HANGING OUT OF SLIDE PACK. RESTOWED MOORING LINE PER B757AMM 52-12 OPN CHECKS GOOD.

Part: COVER — LOOSE (ZONE 200) · airframe 100,261 hrs · 25,627 cycles

SHIP 6804 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. CORRECTIVE ACTION: RESECURED SIGN, OPS CHECK NORMAL. (0851516)

Part: SENSOR — FAULTED (ZONE 800) · airframe 100,261 hrs · 25,627 cycles

SHIP 6804 R1 DOOR SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: T/S PER B757 WDM 25-66-11. NO GRN AT ANN LIGHT 510216 OR 510217. REPLACED BOTH GIRT BAR SENSORS B757 AMM 25-66. CKS FOR FOR PWR AT LIGHT ASSY B757 WDM 25-66-11 CKS GOOD CKD FOR GND AT LIGHT ASSY BY ARMING DOOR NO GND CKED RIG OF GIRT BAR SENSORS FOUND AFT GIRT BAR MISSING ACTUATOR. VERIFIED GND IS GOOD AT GD2922AC. B757 WDM 25-66-11. INSTALLED MISSING ACTUATOR TO GIRT BAR. LIGHT WORKS AS SUPPOSED TO PER B757 AMM:25-66.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 100,252 hrs · 25,619 cycles

SHIP 6804 FOUND EMERGENCY LIGHTS BY ROW DEF INOP. REPLACED BATTERY, R/R EMERGENCY LIGHT TRAY (INVERTER) PER B757 AMM 33-51-11 ALL LIGHTS IN CIRCUIT OPERATED NML. M10699 INVERTER CHANGED. (5132220)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 INTERIOR EMERGENCY EXIT LITES IN CABIN ON RIGHT SIDE SEATS MID TO AFT AREA INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT LOCATIONS M734 M736 IAW B757AMM 33-51-07-902-001 TEST PASSED. (5705992)

Part: LOCK — MISSING (GIRT BAR) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 MISSING BAR LOCK AT R1 DOOR GIRT BAR. CORRECTIVE ACTION: INSTALLED NEW MISSING BAR LOCK AT R1 DOOR GIRT BAR IAW B757 AMM 25-66. (0749550)

Part: SEAT TRACK — MECHANIC ERROR (ZONE 200) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 *R022* WHILE WORKING THE D-2 FLOOR STRUCTURES,75S TO G MOD - MODIFY, RII, SECTION 3 - THE SEAT TRACK AT STA 680-700 LBL10 WAS MISSED DRILLED. CORRECTIVE ACTION: REMOVED AND REPLACE SEAT TRACK @ STA 680-700 LBL 10 IAW DELTA FLIGHT PRODUCTS DWG 21D20N004DDN03 AND DELTA VA 97936 REV Y. (0740162)

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

L4 DOOR THRESHOLD CENTER CHANNEL HAS CORROSION CENTER SCUFF PLATE. CORRECTIVE ACTION: ACCOMPLISHED L4 DOOR THRESHOLD CENTER CHANNEL PER ER/A 622637-14 REV ORIGINAL (0713232)

Part: GUIDE — WORN (ZONE 200) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 L2 DOOR CUTOUT, CENTERING GUIDE HAS WEAR MARKS.CORRECTIVE ACTION: REMOVED AND REPLACED L2 DOOR CUTOUT CENTERING GUIDE IAW B757 SRM 51-40-02-0G. PERFORMED ADJUSTMENT AT L2 DOOR CUTOUT CENTERING GUIDE IAW B757 AMM 52-11. (0700614)

Part: GUIDE — WORN (ZONE 200) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 L2 DOOR, CENTERING GUIDE BALL WORN. CORRECTIVE ACTION: REMOVED AND REPLACED L2 DOOR CENTERING GUIDE BALL IAW B757 SRM 51-40-02-0G. PERFORMED ADJUSTMENT AT L2 DOOR CENTERING GUIDE BALL IAW B757 AMM 52-11-00-825-001 STEP G. (6) ADJUSTMENT GOOD

Part: ROLLER — GOUGED (ZONE 800) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 NO 1 R.H PASS DOOR UPPER AFT ROLLER FITTING ON AFT DOOR FRAME CUTOUT IS GOUGED. CORRECTIVE ACTION: REMOVED AND INSTALLED NO 1 RH PASS DOOR UPPER AFT ROLLER FITTING ON AFT DOOR FRAME CUTOUT IAW B737 AMM 52-11-37. PERFORMED OPS CHECKS ADJUSTMENT IAW B737 AMM 52-11, OPS CHECKS GOOD. (0700606)

Part: ROLLER — GOUGED (ZONE 800) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 #3 L/H EMERGENCY EXIT DOOR LOWER LATCH ROLLER RECIVERS ARE GOUGED FWD AND AFT SIDE. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW #3 L/H EMERGENCY EXIT DOOR LOWER LATCH ROLLER RECIVERS FWD AND AFT SIDE IAW B757 SRM. (0700744)

Part: RESERVOIR — EMPTY (DOOR SLIDE) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 EMERGENCY POWER RESERVOIR DOOR L1 BOTTLE PRESSURE READS ZERO. CORRECTIVE ACTION: REMOVED AND. REPLACED. L1 RESERVOIR DOOR BOTTLE IAW B757 AMM 52- 11. (0696836)

Part: ROLLER — GOUGED (ZONE 800) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 #3 R/H EMERGENCY EXIT DOOR LOWER LATCH ROLLER RECIVERS ARE GOUGED FWD AND AFT SIDE. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW #3 R/H EMERGENCY EXIT DOOR LOWER LATCH ROLLER RECIVERS FWD AND AFT SIDE IAW B757 SRM. (0700794)

Part: ACTUATOR — NO TEST (AILERONS) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 AILERON TRIM ACTUATOR FAILED FREE PLAY CHECK OF BEARING AT STEP 9(A) PER CC# 2711-01030-01. CORRECTIVE ACTION: AILERON TRIM ACTUATOR FAILED FREE PLAY CHECK OF BEARING AT STEP 9(A) PER CC# 2711-01030-01. AILERON TRIM ACTUATOR WAS REPLACED ON CC # 00155. (0692172)

Part: SNUBBER — OUT OF TOLERANCE (ZONE 800) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 PASSANGER DOOR NO 4 L/H SNUBBER INDICATOR PIN IS NOT IN LIMITS. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW PASSANGER DOOR NO 4 LH SNUBBER IAW B757 AMM 52-11-10. (0639283)

Part: SNUBBER — OUT OF TOLERANCE (ZONE 800) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 L/H NO. 2 DOOR SNUBBER INDICATOR PIN IS OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SNUBBER AT LH NO. 2 DOOR IAW B757 AMM 52-11-10. (0639400)

Part: FRAME — GOUGED (ZONE 200) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 R/H FUSELAGE FRAME AT STA 1640 HAS A GOUGE AT STRINGER 16R ON FWD SIDE. (MARKED) REF 5311-01218-01B. CORRECTIVE ACTION: C/W ER/A 620661-14AD REV ORIGIANL SECTION I. (0632857)

Part: FITTING — DAMAGED (ZONE 200) · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 TOOL MARKS ON FITTING LOWER SURFACE AT STA 1640 STR14L NEAR INTERCOSTAL TEE CLIP. CORRECTIVE ACTION: C/W ER/A 620661-14 AD REV ORIGIANL SECTION I. (0585003)

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 CORROSION ON AFT CARGO LOWER THRESHOLD SIDE PANEL STA 1440-1530 RBL 19. CORRECTIVE ACTION: REMOVED, REPLACED AND INSTALLED LOWER THRESHOLD SIDE PANEL STA 1440 TO 1530, RBL 19 L. (0571952)

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

AIRCRAFT 6804, CORROSION AFT CARGO BAY ANGLE ON INTERCOSTAL STA 1440-1460 RBL 25. REPLACED AND INSTALLED ANGLE ON INTERCOASTAL AT AFT CARGO STA 1440 TO 1460, RBL 25 IAW B757-200 SRM 51-40-02-0G AND DWG 146N5413 REV.- L. (LP 0563127)

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 CORROSION ON AFT CARGO LOWER THRESHOLD INNER CHORD STA 1360-1460 RBL 21. CORRECTIVE ACTION: REMOVED, REPLACED AND INSTALLED LOWER THRESHOLD INNER CORD ON AFT CARGO BTW BS 1360 TO 1460, RBL 21 IAW B757-200 SRM AND DWG. (0551104)

Part: PANEL — CORRODED (THRESHOLD) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 CORROSION ON AFT CARGO LOWER THRESHOLD SIDE PANEL STA 1300-1380 RBL 19. CORRECTIVE ACTION: REMOVED, REPLACED AND INSTALLED LOWER THRESHOLD SIDE PANEL BTW STA 1310 TO 1380 IAW DWG AND B757-200 SRM. (0551221)

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 CORROSION AFT CARGO THRESHOLD SUPPORT HAS CORROSION BETWEEN STA 1380-1400. CORRECTIVE ACTION: REMOVED, REPLACED AND INSTALLED AFT CARGO THRESHOLD SUPPORT BETWEEN STA 1380 TO 1440 RH IAW DWG 146N5391 REV: F. AND B757- 200 SRM. (0551208)

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 CORROSION AFT CARGO BAY FITTING 1360+16 RBL 23. CORRECTIVE ACTION: REMOVED AND REPLACED FITTING LOCATED AFT CARGO STA 1360 + 16 RBL 23 IAW B757-200 SRM 51-40-02-0G AND BOEING DWG. (0549317)

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 100,250 hrs · 25,618 cycles

SHIP 6804 CORROSION AFT CARGO BAY ANGLE ON INTERCOSTAL STA 1360-1380 RBL 25. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE ON INTERCOSTAL BTWN STA 1360-1380 RBL 25 IAW B757-200 SRM 51-40-02-0G AND DWG. (0549296)

Part: GIRT BAR — DIRTY (ZONE 200) · airframe 100,161 hrs · 25,597 cycles

SHIP 6804 DOOR 4R WILL NOT STAY IN ARMED POSITION. CORRECTIVE ACTION: DISARMED DOOR, CLEANED GIRT BAR LATCHES AS NECESSARY. REARMED DOOR. (5705944)

Part: PROCESSOR — INACCURATE (FUEL QTY) · airframe 99,369 hrs · 25,402 cycles

SHIP 6804 -DIV- SUSPECTED FUEL LEAK DUE TO FUEL QTY IMBALANCE. CORRECTIVE ACTION: T/S PER FIM. INSPECTED AIRCRAFT AND ENGINE FOR LEAKS. REPLACED FUEL QTY PROCESSOR.

Part: NONE — NONE (NONE) · airframe 98,695 hrs · 25,253 cycles

SHIP 6804 ERA 616344-14 REV AB757 / FUESELAGE/ STA 620. CORRECTIVE ACTION: REF ERA 616344-14. (0250785)

Part: NOT REPORTED — DAMAGED (BS 610-630 S17) · airframe 98,685 hrs · 25,250 cycles

SHIP 6804 FOUND DAMAGE AND SCRATCHES BETWEEN S610 TO 630 AT STRINGER S17. CORRECTIVE ACTION: REF ERA 616244-14. (5026758)

Part: TIRE — UNKNOWN (UNKNOWN) · airframe 98,172 hrs · 25,128 cycles

SHIP 6804 -DIV/TIRE- TO ATL DUE TO NUMBER 3 MAIN TIRE FAILED ON TAKEOFF. CORRECTIVE ACTION: REPLACED NUMBER 3 AND 4 MAIN WHEELS AND COMPLETED BURST TIRE INSPECTION.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 93,690 hrs · 24,098 cycles

SHIP 6804 L1 DOOR KNOCKLE KNOCKER DOES NOT EXTEND CORRECTLY. DOOR SHOWS ARMED. CORRECTIVE ACTION: SECURED L1 DOOR MIDDLE LINING PER B757 AMM 52-11 AND CHECKED DOOR ARMED LIGHT AND KNOCKER PER B757 AMM 33-22 OPERATION NORMAL. (2511425)

Part: DRAG FITTING — DAMAGED (RT NACELLE) · airframe 93,473 hrs · 24,044 cycles

SHIP 6804 AD / AA] RH ENG DRAG FTG HOLES NBR 11 TO 12 & HOLE 14 TO HOLE 18 WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE 12 , SCRATCH ON FITTTNG 7 CLOCK POS ; HOLE 17, CORROSION ON SKIN 6 CLOCK POS ; IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00159: RH ENG DRAG FTG HOLES #12 AND #17 WERE REPAIRED PER PRI 588348-14 REV.2 AND ER/A 588348-14 REV.B SECTION VI: PERMANENT REPAIR. (2472191)

Part: DRAG FITTING — DAMAGED (RT NACELLE) · airframe 93,473 hrs · 24,044 cycles

SHIP 6804 [AD / AA] RH ENG DRAG FTG HOLES NBR 1 TO 10 & HOLE 13 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE 1, SCRATCHES ON SKIN BTW 8 - 11 CLOCK POS ; HOLE 3, SCRATCH ON SKIN BTW 1 - 2 CLOCK POS ; HOLE 6, SCRATCHES ON SKIN BTW 8 - 10 CLOCK POS ; HOLE 7, SCRATCHES ALL AROUND SKIN AND FITTING ; HOLE 8, SCRATCHES ALL AROUND SKIN ; HOLE 9, SCRATCHES ON SKIN BTW 6 - 9 , CORROSION BTW SKIN AND FITTTNG BTW 4 - 6 ; HOLE 10, SCRATCHES ON SKIN AND FITTING BTW 4 - 6 CLOCK POS ; HOLE 13, CORROSION ON SKIN AND FITTING BTW 3 - 8 IN REF TASK CARD. CORRECTIVE ACTION:SUMMARY OF NRC 00122: RH ENG DRAG FTG HOLES ,#3, #7, #9, #10, AND #13 WERE REPAIRED PER PRI 588348-14 REV.2 AND ER/A 588348-14 REV.B SECTION VI: PERMANENT REPAIR AND HOLES #1, #6 AND #8 WERE REPAIRED PER CARD. (2472199)

Part: DRAG FITTING — OUT OF TOLERANCE (LT ENGINE) · airframe 93,471 hrs · 24,043 cycles

SHIP 6804 AWR. A.A. MEASUREMENTS OUT OF TOLERANCE DIAMETER IN BORE HOLES # 2, #3, #8, #9 AND #18 AT LH ENG DRAG FITTING. (IN REF AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00154: HOLES # 2, #3, #8, #9 AND #18 AT LH ENG DRAG FITTING WAS REPAIRED PER ER/A 588348-14AD REV B SECTION I: PERMANENT REPAIR AND PRI 588314-14 REV 3. (2471003)

Part: NONE — NONE · airframe 93,471 hrs · 24,043 cycles

SHIP 6804 AFTER REMOVED ROTARY SNUBBER, DAMAGE INNER BEARING OF LOWER CAM PLATE WAS FOUND IN REF NRC 00080. CORRECTIVE ACTION: SUMMARY OF NRC 00195: INNER BEARING OF LOWER CAM PLATE WAS REPLACED PER BOEING SOPM 20-50-03. (2469189)

Part: SKIN — DEBONDED · airframe 93,471 hrs · 24,043 cycles

SHIP 6804 AD - AA - DISBONDED AREA OF 2.375IN LENGTH AND 1.25IN WIDTH WAS FOUND ON LOWER SKIN OF SLAT #2 AT OSS 675 APPROX. CORRECTIVE ACTION: SUMMARY OF NRC 00036:LOWER SKIN OF SLAT #2 AT OSS 675 APPROX WAS REPAIRED PER B757-200 S.R.M. (2459691)

Part: SNUBBER — OUT OF LIMITS (L4 DOOR) · airframe 93,471 hrs · 24,043 cycles

SHIP 6804 OUT OF LIMITS ROTARY SNUBBER PIN EXTENSION AT 4L DOOR. CORRCTIVE ACTION: SUMMARY OF NRC 0079: ROTARY SNUBBER OF DOOR 4L WAS REPLACED BY ROTARY SNUBBER PER B757-200 AMM 52-11. (2456337)

Part: SNUBBER — OUT OF LIMITS (R4 DOOR) · airframe 93,471 hrs · 24,043 cycles

SHIP 6804 OUT OF LIMITS ROTARY SNUBBER PIN EXTENSION AT 4R DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 0080: SNUBBER OF DOOR 4R WAS REPLACED BY ROTARY SNUBBER PER B757 -200 AMM 52-11-10. (2453842)

Part: DOOR — WILL NOT ARM · airframe 92,677 hrs · 23,858 cycles

SHIP 6804 4L DOOR WOULD NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS CKS GOOD PER B757 AMM 52-11. (8845192)

Part: NONE — NONE · airframe 92,120 hrs · 23,733 cycles

SHIP 6804 R1 SLIDE LIGHT INOP. CORRECTIVE ACTION: RELAMPED, CHANGED MODULE OPS NRML. (8838486)

Part: NONE — NONE · airframe 91,689 hrs · 23,634 cycles

SHIP 6804 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:608. CORRECTIVE ACTION: FOUND 4R DOOR KNUCKLE KNOCKER NOT FULLY EXTENDING DUE TO DEBRIS. REMOVED/CLEANED DEBRIS AND CHK'S OK. ARM/DISARM NORMAL. REF B757200 AMM 25-66. (2142313)

Part: NONE — NONE · airframe 91,285 hrs · 23,540 cycles

SHIP 6804 3L DOOR WON'T ARM. CORRECTIVE ACTION: REMOVED FROZEN DEBRIS FROM FWD GIRT BAR FITTING. OPS NML REF B757 AMM 52-21. (8255760)

Part: NONE — NONE · airframe 90,746 hrs · 23,417 cycles

SHIP 6804 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588314-14AD REV.A. CORRECTIVE ACTION: REF ERA 588314-14AD. (2023615)

Part: NONE — NONE · airframe 90,746 hrs · 23,417 cycles

SHIP 6804 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588348-14AD REV.A. CORRECTIVE ACTION: REF ERA 588348-14AD.

Part: NONE — NONE · airframe 90,630 hrs · 23,387 cycles

'SUPPLEMENTAL INFORMATION' SHIP 6804 4R DOOR MISSING DOOR HANDLE TRIM COVER PLATE. CORRECTIVE ACTION: RPLD TRIM PLATE AS PER B757 52-10 CKS GOOD (8089746)

Part: NONE — NONE · airframe 90,353 hrs · 23,325 cycles

SHIP 6804 DOOR 4R KNUCKLE KNOCKER DOES NOT EXTEND WHEN DOOR ARMED. CORRECTIVE ACTION: 4R DOOR KNUCKLE KNOCKER OPS NORMAL NO FAULT. (7783710)

Part: INDICATOR — INOPERATIVE (DOOR) · airframe 90,037 hrs · 23,255 cycles

SHIP 6804 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:608. CORRECTIVE ACTION: CLEANED AND REMOVED BLOCKAGE OPS CHK NML. (1942797)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,811 hrs · 23,205 cycles

SHIP 6804 EMER LIGHT 4AB, 2L DOOR, 22,25,29ABC INOP. CORRECTIVE ACTION: R/R BATTERY PACK M733 PER AMM 33-51 OPS CHK NML. (7933811)

Part: LIGHT — MALFUNCTIONED (R1 DOOR SLIDE) · airframe 88,952 hrs · 23,014 cycles

SHIP 6804 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: INDICATOR LIHT FOR SLIDE R1 FOUND TO BE WORKING NORMAL IAW AMM 25-12. (1820143)

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 88,862 hrs · 22,995 cycles

SHIP 6804 EXIT LIGHT COVER ABOVE 2L HAS FALLEN OFF, CORRECTIVE ACTION: PUT PNL BACK ON. (7200598)

Part: PROXIMITY SWITCH — FAULTED (L4 DOOR SLIDE) · airframe 88,606 hrs · 22,938 cycles

SHIP L4 DOOR SLIDE LIGHT ILLUMINATED IN BOTH ARM AND DISARM POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED FWD PROX SWITCH S10222 AT L4 DOOR REF B757 AMM CH. 20. (7613056)

Part: FITTING — OUT OF POSITION (GIRT BAR) · airframe 88,369 hrs · 22,883 cycles

SHIP 6804 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 4R. CORRECTIVE ACTION:REPOSITIONED GIRT BAR DOOR FITTING. OPS CHECK GOOD. (1765704)

Part: DRAG BRACE — CRACKED (LT ENGINE) · airframe 87,012 hrs · 22,591 cycles

DURING INSPCTION FOUND CRACKS AT HOLES 2, 3, 4, 5 & 8 AND CORROSION AT HOLES 1,6, 7, 9, 10, 13 & 16 CLOCK POSITION. LT ENGINE DRAG FITTINGS INBOARD AND OUTBOARD WERE REPAIRED, PER ERA 588314-14AD.

Part: SKIN — DAMAGED (WING) · airframe 87,012 hrs · 22,591 cycles

DURING INSPECTION DAMAGES WERE FOUND ON ALL HOLES IN THE FOLLOWING ORDER: HOLE NR 2 SCRATCHES AND CRACK ON SKIN AND FITTING AT 8 O`CLOCK POSITION; HOLE NR 3 CORROSION ON SKIN AND FTG AT 9 O`CLOCK POSITION; HOLE NR 4 SCRATCHES AND CORROSION ON SKIN AT 2 O'CLOCK POSITION; HOLE NR 5 SCRATCHES ON SKIN AT 2 AND 8 O'CLOCK POSITION; HOLE NR 7 SCRATCHES AND CORROSION ON SKIN AT 8 O'CLOCK POSITION; HOLE NR 9 SCRATCHES AND CORROSION ON SKIN AND FITTING AT 8 TO 10 O`CLOCK POSITION; HOLE NR 10 SCRATCHES ON SKIN AT 3 O'CLOCK POSITION. AT RT ENGINE DRAG FTG CLAMP-UP RT ENGINE DRAG FITTING INBOARD WAS REPAIRED AND RT ENGINE DRAG FTG OUTBOARD WAS REPLACED, PER ERA 588348-14AD.

Part: ATTACH FITTING — NOT REPORTED (WING) · airframe 87,012 hrs · 22,591 cycles

DURING INSPECTION FOUND BUSHING ON INBOARD WING ATTACH FITTING STRUT AT LT ENGINE PYLON. REPLACED PER ER/A 588315-14.

Part: BUSHING — MIGRATED (RT PYLON) · corrosion level 2 · airframe 87,300 hrs · 22,652 cycles

DURING REMOTION OF MIGRATED BUSHINGS MAINTENANCE FOUND CORROSION ON OUTBOARD LUG ON UPPER LINK ATTACH POINT AT RIGHT PYLON AND REPAIRED, PER SRM 54-51-90.

Part: SEAT TRACK — CORRODED (BS 1635-1640) · corrosion level 2 · airframe 87,012 hrs · 22,591 cycles

CORROSION LEVEL 2, DURING INITIAL INSPECTION FOUND CORROSION ON SEAT TRACK INBOARD LT BETWEEN 1635 TO 1640 AT CPAX. SEAT TRACK REPAIRED, PER SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 1635-1640) · corrosion level 2 · airframe 87,012 hrs · 22,591 cycles

CORROSION LEVEL 2, DURING INITIAL INSPECTION FOUND CORROSION ON SEAT TRACK OUTBOARD LT BETWEEN 1635 TO 1640 AT PASSENGER CABIN. SEAT REPAIRED, PER SRM 53-00-52.

Part: SKIN — DAMAGED (BS 610-660) · airframe 87,012 hrs · 22,591 cycles

DURING INITIAL INSPECTION FOUND FUSELAGE SKIN BS 610 TO 660 BETWEEN STG 14L TO STG 19L DAMAGED. REPAIRED, PER ERA 475126-14.

Part: SKIN — NOT REPORTED (BS 600-660) · airframe 98,655 hrs · 25,242 cycles

ERA 588128-14 SECTION I ISSUED FOR REPAIR TO STA 600-660 L14L-L1 9L SKIN. CORRECTIVE ACTION: REF ERA 588128-14AD. (1629601)

Part: CUSP WEB — CORRODED (BS 1180-1200) · corrosion level 2 · airframe 87,012 hrs · 22,591 cycles

(CORROSION LEVEL 2) DURING INITIAL INSPECTION : CORROSION FOUND ON CUSP WEB FROM STA 1180/1200 LH AND AT PASSENGER CABIN (CPAX). REPLACED WEB. (LP 1627360)

Part: ACTUATOR — CORRODED (R2 DOOR) · corrosion level 2 · airframe 87,012 hrs · 22,591 cycles

DURING INITIAL INSPECTION FOUND CORROSION ON HYDRAULIC DOOR ACTUATOR AT R2 PASSENGER DOOR. REPLACED DOOR.

Part: INTERCOSTAL — CRACKED (BS 660-685) · airframe 87,012 hrs · 22,591 cycles

DURING INITIAL INSPECTION: CRACK ON INTERCOSTAL BETWEEN STA 660/685 AND STR 12 RT AT PASSENGER CABIN (CPAX). REPLACED PER SRM.

Part: INTERCOSTAL — CRACKED (BS 660-685) · airframe 87,012 hrs · 22,591 cycles

DURING INITIAL INSPECTION A CRACK WAS FOUND ON INTERCOSTAL BETWEEN STA 660/685 AND STR 12 LT AT PASSENGER CABIN. CRACK WAS DELIMITED WITH 0.437" LENGTH, PER B757 NDT MANUAL. INTERCOSTAL BETWEEN STA 660/685 AND STR 12 LT WAS REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 1600-1610) · corrosion level 2 · airframe 87,012 hrs · 22,591 cycles

CORROSION LEVEL 2, DURING INITIAL INSPECTION, CORROSION ON FLOOR SETTLEMENT BETWEEN STA 1600 TO 1610 AND RBL 59 AT PASSENGER COMPARTMENT FLOOR STRUCTURE. REPAIRED PER SRM.

Part: BATTERY — DAMAGED (ESCAPE SLIDE) · airframe 87,012 hrs · 22,591 cycles

DURING ININITIAL INSPECTION FOUND DAMAGED ESCAPE SLIDE BATTERY ON R-4 DOOR SLIDE. CORRECTIVE ACTION: ESCAPE SLIDE BATTERY WAS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 86,884 hrs · 22,566 cycles

(AIRCRAFT 6804, L/P 9801176) DESCENDING THRU 10,000 FT ENG #2 WAS AT IDLE AND UNRESPONSIVE TO THROTTLE INPUTS, PER THE QRH ENGINE LIMIT OR SURGE CHECKLIST WAS ACCOMPLISHED. #2 ENG RECOVERED AFTER STEP 8 (BLEED OFF THEN ON). CORRECTIVE ACTION: T/S PER B757 FIM 76-11 TASK 811. FOUND MOISTURE IN PB SENSE LINE IN TO EEC. REMOVED AND REPLACED EEC AND FCU REF B757 AMM 7321. PERFORMED HIGH PWR RUN. OPS CK GOOD. C/W ALL STEPS OF NO GO ODI PREVENTION LOG 1522095. NO DEFECTS NOTED. MCC NOTIFIED.

Part: DOOR — OBSTRUCTED (L2) · airframe 85,014 hrs · 22,201 cycles

(AIRCRAFT 6804, L/P 6634458) 2L DOOR WILL NOT ARM. CORRECT ACTION: FOUND DEBRIS UNDER 2L DOOR REMOVED DEBRIS OPS OKPER AMM 25-63.

Part: GIRT BAR — DAMAGED (R2 DOOR SLIDE) · airframe 82,893 hrs · 21,809 cycles

SHIP 6804 DURING R2 SLIDE CHANGE-FOUND GIRT BAR UNSERVICABLE. R/R R2 SLIDE GIRT BAR PER AMDS WORK CARD.

Part: PANEL — UNWANTED DEPLOY (OXYGEN MASKS) · airframe 81,772 hrs · 21,591 cycles

SHIP 6804 OXYGEN PANEL MASK DEPLOYED: OXYGEN MASKS CAME DOWNAT TAKEOFF AT 30ABC DID NOT START / INTERIOR. CORRECTIVE ACTION: RE-SECURED PSU OXYGEN PANEL AS PER B757 AMM 35-20, OPS CHK NML (0874896)

Part: LENS — CRACKED (EXIT SIGN) · airframe 80,554 hrs · 21,356 cycles

OVERHEAD EXIT SIGN LENS BETWEEN SEAT ROWS 33 HAS CRACKS AT BOTH ENDS. REPLACED LENS AT ROW 33 PER AMM 33-51-10.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 80,554 hrs · 21,356 cycles

GIRT BAR NOT ENGAGING SMOOTHLY DURING ARMING AS PER STEP 25 OF ORIG TASK CARD. ADJUSTED R2 DOOR GIRT BAR PER AMM 25-66-00.

Part: SKIN — DENTED (CARGO DOOR) · airframe 80,554 hrs · 21,356 cycles

FUSELAGE EXTERIOR DENT ON AFT CARGO DOOR AT LOWER FWD SIDE(M).

Part: SLIDE — UNLACED (R1 DOOR) · airframe 80,554 hrs · 21,356 cycles

R1 DOOR SLIDE UNLACED. SLIDE RE-LACED PER CMM 25-61-36 ON NON-ROUTINE CARD 284.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 80,302 hrs · 21,310 cycles

EMERGENCY EXIT SIGN LENS WAS LOOSE. SECURED THE SIGN LENS.

Part: LANYARD — OUT OF POSITION (R2 DOOR SLIDE) · airframe 77,238 hrs · 20,704 cycles

DURING DEPARTURE, THE R2 DOOR WOULD NOT ARM. FOUND THE LANYARD ON THE SLIDE PACK INTERFEREING WITH GIRT BAR. POSITIONED AND SECURED THE LANYARD. THE R2 DOOR OPS NORMAL IAW AMM 25-66.

Part: LIGHT — DAMAGED (SEAT 36D) · airframe 74,243 hrs · 20,140 cycles

SEAT 36D MOUNTED EMERGENCY LIGHTING DAMAGED. REPLACED EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 74,039 hrs · 20,092 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED/INOP LOCATIONS:36D. SECURED LIGHT.

Part: PROXIMITY SENSOR — INOPERATIVE (R2 DOOR) · airframe 72,775 hrs · 19,825 cycles

FOUND 2R ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOP. RELAMPED BULBS AND SWAP WITH KNOWN GOOD LIGHT NO HELP. ADJUSTMENT OF GIRT BAR PROX SENSORS PER AMM 25-66. RMVD AND RPLCD DOOR 2R FWD GIRT BAR PROX SENSOR W SVCBLE UNIT REF MM 25-66.

Part: SNUBBER — LEAKING (L2 DOOR) · airframe 72,431 hrs · 19,756 cycles

L2 DOOR SNUBBER IS LEAKING. REPLACED THE SNUBBER IAW AMM 52-11.

Part: SEAL — UNSECURE (NLG DOOR) · airframe 72,431 hrs · 19,756 cycles

CUTOUT SEAL NOT SECURE AT RT NLG WW DOOR FWD HINGE. CLEANED, PREPPED AND SECURED ORIG. SEAL IAW MM 20-00.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 71,754 hrs · 19,630 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. SECURED EMERGENCY EXIT COVER AT LOCATION 604.

Part: ENGINE — FIRE (NR 2) · airframe 71,236 hrs · 19,538 cycles

CREW RECEIVED A RIGHT ENGINE FIRE INDICATION JUST AFTER TAKEOFF. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO DEPARTURE. FOUND EVIDENCE OF FIRE. REMOVED AND REPLACED NR 2 ENGINE.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,906 hrs · 18,286 cycles

DURING EMERGENCY LIGHT TEST IAW JC 3351-7001 FOUND DOOR 4L EMERGENCY LIGHT TEST SWITCH INOPERATIVE. R & R EMERGENCY LIGHT TEST SWITCH IAW WD 33-51-15, OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 64,895 hrs · 18,284 cycles

AFTER PUSH BACK, THE CREW REPORTED THAT THERE WAS SMOKE AND ODOR IN THE MID CABIN. THE ACFT RETURNED TO THE GATE. RESTORED CABIN TO DEPARTURE CONFIGURATION WITH FLIGHT ATTENDANTS AND COULD NOT DUPLICATE. T/S IAW 21-00-01-301. INSPECTED OVERHEAD LIGHTS AND BALLASTS, READING LIGHTS AND PSUS. INSPECTED IF & EMPOWER OUTLETS, OVENS & COFFEEMAKERS NOTHING FOUND. PERFORMED INSPECTION OF LT & RT PACK BAY AREAS ALL NORMAL, INSPECTED LT & RT RECIRCULATION FANS AND MONITOR ALL CHECKED NORMAL. INSPECTED NR 2 LT & RT DOOR AREA HEATERS ALL NORMAL. CALL COMPLETE, OK FOR SERVICE.

Part: SKIN — DENTED (BS 305) · airframe 64,097 hrs · 18,116 cycles

FOUND DENT AND BENT LONGERON AT FORWARD CARGO BAY BS 305 LONGERON 28R. CUTOUT DAMAGE AND INSPECTED, INSTALLED REPAIR IAW SRM.

Part: SKIN — DAMAGED (BS 514) · airframe 64,050 hrs · 18,105 cycles

SKIN DAMAGED AT BS 514 BETWEEN S27-28L. INSTALLED EXTERNAL REPAIR DOUBLER IAW ER/A 504710-14 REV 0.

Part: VERTICAL BEAM — CORRODED (BS 377) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

CORROSION ON VERTICAL BEAM, LT SIDE OF NOSE WHEEL WELL STRUCTURE AT ATTACHMENT TO BS 377.7, FRAME, LOWER END OF VERTICAL BEAM, FOUND OUT OF LIMITS IAW SRM. INSTALLED NEW BEAM IAW DWG 141N9940, REV C.

Part: BLANKING PLATE — CORRODED (BS 1500-1520) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

SKIN BLANKING PLATE LOCATED BETWEEN S27-28R AND BS 1500-1520 IS CORRODED. REMOVED IAW ER/A 504714-14 REV 0.

Part: FITTING — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

AFT CARGO DOOR FRAME LOWER SILL AREA BEAM FITTING HAS CORROSION ON AFT SIDE. FOUND TO BE OUT OF LIMITS. R & R THE FITTING IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 1320-1340) · airframe 64,050 hrs · 18,105 cycles

FLOOR SUPPORT CRACKED BS 1320-1340, RBL 44. R & R FLOOR SUPPORT IAW SRM.

Part: FITTING — CORRODED (CARGO DOOR SILL) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

AFT CARGO DOOR FRAME SILL BEAM FWD FITTING HAS CORROSION ON FWD SIDE. FOUND TO BE OUT OF LIMITS IAW DWG 69-45578, REV D. R & R THE FITTING IAW SRM.

Part: ANGLE — BENT (EMERGENCY EXIT) · airframe 64,050 hrs · 18,105 cycles

NR 3 EMERGENCY DOOR SECOND STRINGER FROM TOP AFT ANGLE BENT. REMOVED ANGLE AND FABRICATED NEW, TRIMMED AND INSTALLED IAW DWG 146N6346 AND SRM.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

UPON REMOVAL OF LT AIRPHONE ANT BLANKING PLATE, CORROSION FOUND ON FUSELAGE SKIN. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 504714-14, REV 0.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

DURING REMOVAL OF RT AIRPHONE ANTENNA BLANKING PLATE, CORROSION FOUND ON FUSELAGE SKIN. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 504714-14, REV 0.

Part: SKIN — DENTED (BS 520) · airframe 64,050 hrs · 18,105 cycles

SKIN FOUND DENTED BS 520 BETWEEN S27-28R. REPAIRED THE SKIN IAW ER/A 504710 -14, REV 3.

Part: FLOOR SUPPORT — CORRODED (BS 1320) · airframe 64,050 hrs · 18,105 cycles

AFT CARGO BAY FLOOR SUPPORT CRACKED STA 1320, LBL 25. REMOVED, FABRICATED NEW FLOOR SUPPORT AND INSTALLED IAW DWG 140N2502, REV E & SRM.

Part: SKIN — DAMAGED (BS 490) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

BS 490 AREA OF PREVIOUS BLEND WITH CORROSION ABOVE CAPTAIN`S STATIC PORT S21L. REPAIRED IAW ER/A 504715-14, REV 0.

Part: FLOOR SUPPORT — CORRODED (BS 320-324) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN WET AREA FLOOR SUPPORT BETWEEN BS 320-324, LBL 21 HAS CORROSION. REPAIR THE FLOOD SUPPORT IAW ER/A 504711-14, REV O.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN WET AREA FLOOR SUPPORT BETWEEN BS 324-345, RBL 39 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW DWG 14IN5160, REV CD, SRM.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN WET AREA FLOOR SUPPORT BETWEEN BS 324-345 RBL 55 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED NEW SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

FLOORBEAM TEE CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. CUTOUT DAMAGE LOCATED AND DRILLED NEW TEE AND FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

FLOOR SUPPORT CORRODED AND FOUND TO BE OUT OF LIMITS. REMOVED THE FLOOR SUPPORT AND FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN AFT WET AREA FLOORBEAM TEE CORRODED BS 1660 BL 0. REMOVED CORROSION AND FOUND OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED IAW SRM.

Part: CHANNEL — CRACKED (RT MLG WW) · airframe 64,050 hrs · 18,105 cycles

INBOARD CHANNEL CRACKED AT RT MLG WW BS 1180, BULKHEAD INBD JUST BEFORE KEEL BEAM. FABRICTED NEW CHANNEL AND INSTALLED NEW CHANNEL IAW SRM AND IAW DWG 144N2563, REV BM.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN AFT WET AREA FLOORBEAM TEE CORRODED BS 1640, BL 0-LBL 57. REMOVED CORROSION, FOUND OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED, IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1660) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN AFT WET AREA FLOOR SUPPORT CORRODED BETWEEN BS 1640-1660 BL 0. BLENDED SUPPORT AND FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT AND INSTALLED NEW IAW SRM IAW DWG 146N5230, REV B.

Part: SKIN — DAMAGED (BS 490) · airframe 64,050 hrs · 18,105 cycles

RT FUSELAGE PREVIOUS BLEND OUT JUST AFT OF CAPTAIN'S STATIC PORT BS 490 BETWEEN STR 20-21R. FOUND OUT OF LIMITS, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW SRM.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

CORROSION FOUND AT BS 345 LBL 20 FLOORBEAM UPPER TEE. CUT OUT DAMAGE AND FABRICATED REPAIR & INSTALLED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN AFT WET AREA FLOOR SUPPORT CORRODED BETWEEN BS 1660-1680, RBL 57. REMOVED AND FABRICATED NEW FLOOR SUPPORT AND INSTALLED IAW SRM & DWG 146N5230, REV D.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN AFT WET AREA DECK CORRODED ALONG THE FLOORBEAM, BS 1680 BETWEEN BL 0 AND LBL 57. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED REF SRM.

Part: SEAT TRACK — BROKEN (BS 780) · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN SEAT TRACK, RBL 45 AT BS 780 SCALLOP BROKEN OFF. R & R SEAT TRACK IAW SRM AND DWG 143N5080RNA .

Part: SEAT TRACK — WORN (COCKPIT) · airframe 64,050 hrs · 18,105 cycles

CO-PILOT NR 3 SEAT TRACK FOUND WORN. R & R SEAT TRACK IAW SRM AND DWG 232N301, REV A.

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 64,050 hrs · 18,105 cycles

INBD "U" CHANNEL CRACKED AT LT MLG WW BS 1180, BULKHEAD INBD JUST BEFORE KEELBEAM. R & R THE CHANNEL IAW SRM.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN FWD WET AREA FLOORBEAM TEE CORRODED, BS 377.7, BL 0. REMOVED DAMAGE AND INSTALLED NEW TEE IAW SRM AND DWG 141N5190, REV C.

Part: FLOOR SUPPORT — CORRODED (BS 1647-1655) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN AFT WET ARE FLOOR SUPPORT CORRODED BETWEEN BS 1647-1655, RBL 57. REMOVED DAMAGE AND INSTALLED NEW FLOOR SUPPORT IAW SRM AND DWG 146N5230, REV D.

Part: SEAT TRACK — CORRODED (BS 740-780) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN BS 740 - 780, LBL 45. REMOVED SEAT TRACK FROM BS 700 - 780 AND INSTALLED A NEW SEAT TRACK IAW SRM.

Part: SEAT TRACK — GOUGED (BS 1178) · airframe 64,050 hrs · 18,105 cycles

SEAT TRACK LBL 45, BS 1178 GOUGED. R & R THE SEAT TRACK FROM BS 1087-1180 IAW SRM AND DWG 144N 5021.

Part: SEAT TRACK — GOUGED (BS 1100) · airframe 64,050 hrs · 18,105 cycles

SEAT TRACK, RBL 24 IS GOUGED AT BS 1100+2. R & R THE SEAT TRACK SECTION FROM BS 1080 - 1180 IAW DWG 144N5021.

Part: SEAT TRACK — GOUGED (BS 1243) · airframe 64,050 hrs · 18,105 cycles

SEAT TRACK RBL 24 IS GOUGED AT BS 1243. R & R THE SEAT TRACK SECTION FROM BS 1180-1280 IAW DWG 146N5130.

Part: SEAT TRACK — GOUGED (BS 1241) · airframe 64,050 hrs · 18,105 cycles

SEAT TRACK LBL 45 HAS A DEEP GOUGE AT BS 1241. R & R THE SEAT TRACK SECTION FROM BS 1180 - 1280 IAW DWG 146N5120.

Part: FLOOR SUPPORT — DAMAGED (BS 320) · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN WET AREA AT BS 320 RBL 4, FLOOR SUPPORT DAMAGED. R & R THE FLOOR SUPPORT IAW SRM AND DWG 141N5160, REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN WET AREA, BS 365.2 BETWEEN BL 0 - RBL 3 FLOORBEAM TEE CAP CORRODED ON BOTH SIDES. REPAIRED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1320) · airframe 64,050 hrs · 18,105 cycles

LAVATORY FLOOR SUPPORT HAS CORROSION, BS 1320. CLEANED AREA IAW SRM. SUPPORT FITTING OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1320) · airframe 64,050 hrs · 18,105 cycles

LAVATORY FLOOR SUPPORT CRACKED AT BS 1320, RBL 25. REMOVED THE FLOOR SUPPORT IAW SRM,

Part: SUPPORT FITTING — CORRODED (BS 1720) · corrosion level 2 · airframe 64,050 hrs · 18,105 cycles

MAIN CABIN AFT WET AREA SUPPORT FITTING CORRODED BS 1720, RBL 39, REMOVED AND REPLACED THE SUPPORT FITTING IAW DWG 146N5300, REV A, SRM.

Part: HEATER — MALFUNCTIONED (DOOR) · airframe 62,052 hrs · 17,735 cycles

DURING CRUISE, F/A REPORTED BLUE HAZE FUMES IN FWD GALLEY. FOLLOWED QRH PROCEDURE CONDITIONS DISSIPATED DURING INSPECTION FOUND A4 CIRCUIT BREAKER TRIPPED. REMOVED NR 1 DOOR HEATER IAW AMM 21-45. NEW PARTS AOG FROM ATL AT 2355 PERFORMED SMOKE AND FUMES OF AIR CONDITION SYSTEM IAW 21-00-01. INSTALLED NEW NR 1 DOOR HEATER IAW AMM 21-45. HEATER OPERATES NORMALLY.

Part: LIGHT — UNSECURE (CABIN) · airframe 60,990 hrs · 17,512 cycles

ROW 27 DEF EMERGENCY LIGHT LOOSE. FOUND LOOSE SCREW ON EMERGENCY LIGHT COVER. SECURED 27 DEF EMERGENCY LIGHT, OPS CHECKED GOOD.

Part: A/C PACK — ODOR · airframe 58,079 hrs · 16,964 cycles

VERY STRONG PUNGENT MUSTY ODOR COMING FROM ACFT SYS ONLY IN COCKPIT NOT CABIN, STRONGEST DURING INITIAL TAXI CLIMB DESCENT ON ENG BLEED NOT NOTICED IN CRUISE AS MUCH, RAN BOTH PACKS FOR SEVERAL MINUTES. COULD NOT DUPLICATE FAULT. SPRAYED DEODORANT THROUGHOUT CABIN. GOOD FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,904 hrs · 16,935 cycles

ON LIFT OFF, UP 10K, ENCOUNTERED AT VERY STRONG ODOR COMING FROM AIR CONDITIONING SYS. SMELLED OF MOLDY MUSTY ACIDY WITH SLIGHT STINGING OF EYES. FIRST CLASS PASSENGERS COMPLAINED OF EGG ODOR. DISIPATED ABOVE 10K. ON APPROACH, DESCENDING THRU 14.5K OVERWHELMING ODOR IN COCKPIT STINGING IN EYES OF ODOR. DONNED MASKED AND USED 02 THROUGH OUT LANDING.

Part: BOTTLE — LOW PRESSURE (LIFE RAFT) · airframe 56,809 hrs · 16,724 cycles

DURING SERVICE CHECK, MX FOUND LIFE RAFT IN RED BAND. MX REPLACED LIFT RAFT IN OVERHEAD BIN.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 56,041 hrs · 16,568 cycles

WEATHER RADAR INOPERATIVE ON TAXI OUT. TRANSCEIVER WILL SWEEP ANTENNA BUT WILL NOT PAINT WEATHER.

Part: LIGHT — INOPERATIVE (MID GALLEY) · airframe 48,035 hrs · 15,020 cycles

DURING LAYOVER CHECK, FOUND MID GALLEY EMERGENCY PATH LIGHT INOPERATIVE. MX REPLACED LIGHT ASSY.

Part: WIRE — BURNED (GALLEY) · airframe 47,378 hrs · 14,903 cycles

DURING FLIGHT, A FLIGHT ATTENDANT NOTICED AN ELECTRICAL SMELL IN THE AFT GALLEY NEAR THE COFFEEMAKER AREA. CREW SHUT OFF POWER TO SEVERAL GALLEY ITEMS AND THE SMELL DISSIPATED. MAINTENANCE FOUND THE COFFEEMAKER WIRES BURNED, DISABLED THE COFFEEMAKER. NEF CODE 253.08. (2010-D1290) (DL75E102943)

Part: WARNING LIGHT — ILLUMINATED (LT BLEED) · airframe 45,541 hrs · 14,529 cycles

LEFT ENG BLEED OFF, LIGHT ON WHEN SWITCH IN ON, POS DUCT PRESS NORMAL. PLACARD FOR MEL 36-21-02A NOTED BY MX.

Part: SENSOR — OUT OF LIMITS (AOA) · airframe 45,307 hrs · 14,488 cycles

ABORTED T/O DUE TO F/O AIRSPEED IND FAILING TO RISE 80KAIS ABORT. VISUAL INSPECTED PITOT TUBES FOUND NO DEFECTS. FOUND F/O AOA SENSOR OUT OF CONFIGURATION. REPOSITION TO NORMAL CONFIGURATION AND PERFORM MACH AIR SPEED TEST PER M/M 34-12-00-715, NO TROUBLE FOUND. OK FOR SERVICE. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: BULB — BROKEN (EMERGENCY LIGHT) · airframe 45,106 hrs · 14,450 cycles

SEAT 26D EMERGENCY PATH LIGHT ASSY BROKEN. PLACED LIGHT ASSY IN COCKPIT SPARE BULB CLOSET DEFERRED IAW MEL 33-51-03. SFO MX REPLACED 26D EMERGENCY PATH LIGHT ASSY.

Part: CONTROLLER — INOPERATIVE (CABIN TEMP) · airframe 43,925 hrs · 14,220 cycles

FLT DECK TEMP UNCONTROLLABLE PERFORMED BIT ON LT TEMP CONTROLLER. FAULT CONTROLLER AND TEMP CONTROL V/V. R & R LT PACK TEMP CONTROLLER AND R & R TEMP CONTROL V/V IAW M/M. OPS CHK NML. OK FOR SVC ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: MODULE — FAILED (E&E BAY) · airframe 42,978 hrs · 14,049 cycles

AUTO SPEED BRAKE FAIL ON TAXI OUT. NO HISTORY FWD TO MCO AND PLAC PER MEL 27-62-01B. BITE TEST - SCM FAIL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: IGNITER — FAULTY (NR 2 ENGINE) · airframe 42,691 hrs · 14,003 cycles

ENG EGT FAILED TO RISE DURING START WITH IGNITION SW IN NR 1 POSITION. STARTED OK WITH IGNITION SWITCH IN BOTH. FWD TO MCO PER MEL 74-00-01A PLAC INSTALLED. REMOVED AND REPLACED RT ENG NR 1 IGNITER AND HARNESS PER AMM. OPS CHECK NORMAL MC AND PLACARD REMOVED. CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: ACTUATOR — INTERMITTENT (RUDDER TRIM) · airframe 42,053 hrs · 13,866 cycles

RUDDER TRIM INOP INTERMITTANT. SOMETIMES RUDDER TRIM WILL STICK AND NOT MOVE, SOMETIMES IT WILL WORK BUT NOT PREDICTABLE. REMOVED AND REPLACED RUDDER TRIM ACTUATOR PER AMM. OPS TRIM CONTROL NORMAL.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 41,245 hrs · 13,698 cycles

AFTER LANDING EMERGENCY TRACK LIGHTS IN FIRST CLASS AND RIGHT SIDE CAME ON. FOUND AND REPAIRED CHAFED WIRE IN P37 PANEL PER AMM REF WDM 33-51-11 WIRE W1270-0621-22.

Part: SPEED BRAKE — MALFUNCTIONED · airframe 40,305 hrs · 13,531 cycles

AUTO SPEED BRAKE SYS INOP, FWD TO MCO PER MEL 27-62-01B MCO AND PLAC INSTALLED.

Part: PUMP — WARNING LIGHT (HYD SYSTEM) · airframe 40,271 hrs · 13,520 cycles

R ELEC HYD PUMP LOW PRESSURE LIGHT ON DURING TAXI OUT. OPERATED ALL SYSTEMS WITH RIGHT ELEC PUMP. SYSTEM PRESSURE NORMAL BUT LOW PRESSURE LIGHT ON IN SWITCH. FWD TO MCO AND PLACARD PER MEL 29-31-02B.

Part: SEAT TRACK — CORRODED (BS 1635) · airframe 40,198 hrs · 13,491 cycles

CABIN STA 1635, RBL45 SEAT TRACK HAS CORROSION.

Part: FLOORBEAM — CORRODED (BS 377.7) · airframe 40,198 hrs · 13,491 cycles

CORRSION ON MAIN CABIN FLOORBEAM AT STA 377.7 LBL-1 TO LBL-12 UPPER SURFACE AND UNDER FASTENER HOLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,198 hrs · 13,491 cycles

CABIN FLOORBEAM 1640 UPPER SURFACE HAS CORROSION INCLUDING AREAS AROUND FASTENER HOLES RBL 60 TO LBL 60.

Part: FLOOR PANEL — CORRODED (BS 1681) · airframe 40,198 hrs · 13,491 cycles

CABIN STA 1681 RBL 0 TO RBL 55 FLOOR PANEL HAS CORROSION INCLUDING AREAS AROUND FASTENER HOLES.

Part: STRUCTURE — CORRODED (BS 377-333) · airframe 40,198 hrs · 13,491 cycles

CORROSION ON MAIN CABIN LT INNER CHORD AT STA 377 TO STA 333 LBL-64.

Part: FLOOR PANEL — CORRODED (BS 1715) · airframe 40,198 hrs · 13,491 cycles

CABIN STA 1715 RBL5 TO RBL52 FLOOR PANEL HAS CORROSION ESPECIALLY AROUND FASTENER HOLES.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,198 hrs · 13,491 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT ON UPPER SURFACE AROUND 3 FASTENER HOLES AT STA 397 TO STA 402 RBL-52.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 40,198 hrs · 13,491 cycles

AFT CARGO COMPT RT AIRFONE ANTENNA BETWEEN STA 1500 AND STA 1520 DOUBLER HAS SUFACE CORRSION.

Part: DOUBLER — CORRODED (BS 1500-1520) · airframe 40,198 hrs · 13,491 cycles

AFT CARGO COMPT BETWEEN STA 1500 TO STA 1520 FOUND LT AIRFONE ANTENNA INNER SKIN DOUBLERS HAS A SURFACE CORROSION.

Part: SEAT TRACK — CORRODED (BS 640) · airframe 40,198 hrs · 13,491 cycles

MAIN CABIN SEAT TRACK AT STA 640 RBL 45.5 FOUND CORROSION.

Part: SEAT TRACK — CORRODED (BS 1635) · airframe 40,198 hrs · 13,491 cycles

CABIN STA 1635 RBL 24 SEAT TRACK HAS CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,198 hrs · 13,491 cycles

CORROSION ON MAIN CABIN FLOOBEAM UPPER SURFACE AND BOTTOM OF FASTENER HOLES AT STA365 BL-0 TO RBL-65.

Part: WEB — CORRODED (R1 DOOR SILL) · airframe 40,198 hrs · 13,491 cycles

CORROSION AT R-1 DOOR SILL WEB BOTTOM SURFACE AT STA 340 AND STA359.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,198 hrs · 13,491 cycles

DENT ON FUSELAGE AT STA 1614 AND 0.5 INCH BELOW LAP JOINT S-14L (MISSING ADF DECAL) CUSTOMER REQUEST TO BE EVALUATED DENT PER SRM INSTALL NEW DECAL IF WITHIN LIMITS. WRITE N/R IF FOUND OUT OF LIMITS ADVISE DELTA REP FOR ANT CHANGES I AD (MREF ADF ENTRY OOI).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,198 hrs · 13,491 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE AND UNDER FASTENER HOLE AT STA 345 TO STA 390 BBL.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 40,198 hrs · 13,491 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE AT STA 333 RBL-4.

Part: FLOORBEAM — CORRODED (BS 324 RBL 61) · airframe 40,198 hrs · 13,491 cycles

CORROSION ON MAIN CABIN BEAM UPPER SURFACE AT SAT 324 RBL 61.

Part: FLOORBEAM — CORRODED (FS 365) · airframe 40,198 hrs · 13,491 cycles

DURING CURRENT HMV CHECK, EXTENSIVE CORROSION WAS FOUND ON THE FS 365 FLOORBEAM UPPER CHORD, FROM BL0 TO RHS END. THE UPPER CAP WAS CUT OUT AND A NEW SECTION SPLICE IN PER BOEING APPROVED REPAIR INSTRUCTIONS, AS IS DOCUMENTED IN ER/A 472304-14.

Part: SKIN — DENTED (FS 1614 S14L) · airframe 40,198 hrs · 13,491 cycles

DURING CURRENT HMV, A DENT WAS FOUND NEAR STRINGER 14L AT FS 1614, ALSO IN CLOSE PROXIMITY TO THE BUTT JOINT. THE SUBJECT DENT WAS CUT OUT, AND A BOEING APPROVED REPAIR INSTALLED PER 472303-14.

Part: SEAT TRACK — GOUGED (BS 820 RBL 25) · airframe 40,198 hrs · 13,491 cycles

MAIN CABIN SEAT TRACK CROWN AT STA 820 RBL 25 FOUND GOUGE MARK, C/W AT SAA - SAT ON N/R 122467 SAA JOB 82000010001.

Part: FRAME — DENTED (BS 600 S25L) · airframe 40,198 hrs · 13,491 cycles

FWD CARGO COMPARTMENT STA 600 STR 25L CIRCUMFERENTIAL FRAME DENTS, C/W AT SAA, SAT N/R 116220 SAA JOB 81998010001.

Part: SKIN — DENTED (BS 395 L23-25R) · airframe 40,198 hrs · 13,491 cycles

FWD LOWER FUSELAGE FOUND INTERNAL DENT AT STA 395 BET L23R - L25R, C/W AT SAA, SAT ON N/R 124038 SAA JOB 81993760001.

Part: FRAME — DENTED (BS 580 S25L) · airframe 40,198 hrs · 13,491 cycles

FWD CARGO COMPT STA 580 STRINGER 25 L CIRCUMFERENTIAL FRAME DENTS, C/W AT SAA, SAT ON N/R 116219 SAA JOB 81998030001.

Part: ADC — INOPERATIVE (RIGHT) · airframe 40,181 hrs · 13,484 cycles

AIR TURN BACK, AFTER TAKEOFF MACH SPEED TRIM AND RUDDER RATIO EICAS MSG F/O AIRSPEED IND VERY SLOW TO INCREASE ABOVE 100KTS, LAGGED BEHIND CAPT AIRSPEED INDICATOR BY 30+ KNOTS. REMOVED AND REPLACED RT ADC AND FCC IAW MM.

Part: TERMINAL — MELTED (WINDOW) · airframe 39,876 hrs · 13,422 cycles

FLT CREW REPORTED SMOKE AND FUMES IN THE FLT DECK. DAL MTC DETERMINED R1 WINDOW HEAT TERMINAL MELTED. CONFIRMED SMELL.

Part: COFFEEMAKER — DIRTY (MID GALLEY) · airframe 39,477 hrs · 13,348 cycles

BURNING SMELL FROM MID GALLEY, F/O SIDE COFFEE POT HAD TO PULL C/B. CHECKED COFFEEMAKER LOCATED ON MID GALLEY F/O SIDE. OPS NORMAL. FOUND SMELL DUE TO DIRTY HOTPLATE. CLEANED SAME, OPS NORMAL.

Part: GEARBOX — MAKING METAL (NR 2 ENGINE) · airframe 39,431 hrs · 13,340 cycles

RIGHT ENGINE SHUTDOWN BY ITSELF. FOUND METAL ON GEARBOX CHIP DETECTOR.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 39,431 hrs · 13,340 cycles

RT ENGINE IFSD. REMOVED AND REPLACED MAIN AND ANGLE GEAR BOXES. REMOVED AND REINSTALLED IDG LUBE PUMP STARTER AND VALVE HYD PUMP PER PA W 2037 EMM, 475658. PERFORMED ENGINE RUN PER MM CHECKS NORM OK FOR SERVICE.

Part: BEARING — FAILED (NR 1 ENGINE) · airframe 38,698 hrs · 13,213 cycles

NR 5 BEARING FAILED OIL IN TAIL PIPE. REPLACED NR 1 ENG. REPLACED NR 1 ENG PER 6T103.

Part: BEARING — FAILED (NR 1 ENGINE) · airframe 38,649 hrs · 13,205 cycles

DUE TO HOC ON NR 1 ENGINE AND FAILURE OF BUMBER BEARING INSPECTION OPN 5122 LAX 20AUG. PLEASE REPLACE NR 1 ENGINE. REPLACED NR 1 ENG PER TRANS 6T103.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY EGRESS LIGHTS FROM SEAT ROW 17D TO AFT LAVATORY INOPERATIVE. REPLACED FLOOR PATH EMERGENCY LIGHTS GROUND POWER STRIP FROM SEAT ROW 17D TO AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SEA - EMERGENCY LIGHT ABOVE ROW 28ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT ABOVE ROW 28ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — MAKING METAL (LEFT)

DFW - EXPERIENCED LEFT HAND ENGINE OVERHEAT AND PARTIAL POWER FAILURE AT OR NEAR 132 KNOTS. MAXIMUM EXHAUST GAS TEMPERATURE 815. SHUTDOWN LEFT HAND ENGINE PER QRH. NO FIRE INDICATION. LANDED DFW WITHOUT INCIDENT. FOUND METAL IN TAIL PIPE. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 2AB)

AFT PORTION OF EMERGENCY FLOOR TRACK LIGHT AT 2AB INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHT ASSEMBLY AT ROW 2AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,534 hrs · 5,348 cycles

DURING CHECK-C MAINT FOUND STATION 650 STRINGER 17L, 4 FOOT FWD OF THE LEFT SIDE NUMBER 2 CABIN DOOR, WITH 2 EACH SMOOTH DENTS. THE FWD DENT WAS .75 IN BY .75 IN BY .1875 IN DEEP. AFT DENT WAS 1 IN BY 1 IN BY .0625 IN DEEP. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 53-00-01.

Part: VIDEO DISPLAY — FAULTY (CABIN) · airframe 15,204 hrs · 4,647 cycles

SMOKE WAS COMING FROM THE VIDEO MONITOR AT SEAT ROW 23, RT SIDE. CREW PULLED CIRCUIT BREAKER AND SHUT OFF THE VIDEO. MAINTENANCE PULLED ALL CIRCUIT BREAKERS, REMOVED THE CONNECTOR, AND DEFERRED CORRECTIONS PER MEL. THE VIDEO MONITOR WAS LATER REPLACED. CHECK-C 2-20-00 LAX.

Part: COMPUTER — MALFUNCTIONED (LT AUTO PILOT) · airframe 13,630 hrs · 4,109 cycles

THE LEFT AUTOPILOT SELF-ENGAGED DURING TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. THE LEFT AUTOPILOT WAS DEACTIVATED AND DEFERRED PER MEL. CHECK-C 2-20-00 LAX. ---OPEN--- S/D. THE AUTOFLIGHT CONTROL SYSTEM MODE CONTROL PANEL (MCP) WAS REPLACED. THE MANUFACTURER TESTING SHOWED THE MCP A SIDE PROCESSOR WAS NOT PROPERLY RETURNING FROM A PROCEDURE CALL, AND SIGNIFICANT PROBLEMS WITH THE INTERFACE TO THE RAM MEMORY DEVICES. THESE MCP FAILURES CAN CAUSE THESE UNCOMMANDED AUTOPILOT ANOMALIES TO OCCUR. THIS IS A CORRECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,645 hrs · 3,797 cycles

THE RT SIDE NUMBER 4 CABIN DOOR SLIDE LIGHT DID NOT ILLUMINATE WHEN ARMED. RELAMPED AND CLEANED THE PROX SWITCH. CHECK-C 2-20-00 LAX.

Part: STATIC PORT — LIGHTNING STRIKE (BS 490)

DURING CHECK-C MAINTENANCE, THE LEFT SIDE PRIMARY CAPTAINS AND FIRST OFFICERS STATIC PORTS HAD .1875 BY 0.008 DEEP LIGHTNING STRIKE ABOVE PORTS, APPROX STA 490 BETWEEN STRINGERS 20L AND 21L. BURNISHED AND FOUND TO BE WITHIN LIMITS OF SRM 51-10-01 PAGE 27. ALODINED AREA.