N684DA

Part: GIRT BAR — DETACHED (ZONE 800) · airframe 99,463 hrs · 42,712 cycles

SHIP 684 F/A'S HAVE ISSUE ARMING THE 1L DOOR. CORRECTIVE ACTION: FOUND GIRT BAR DETACHED. REATTACHED SAME. DOOR NOW ARMS - SYS CKS GOOD PER B757 AMM 25-66. (5693032)

Part: SKIN — DAMAGED (ZONE 500) · corrosion level 2 · airframe 99,276 hrs · 42,590 cycles

SHIP 684 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589971-14AD REV D. CORRECTIVE ACTION: REF ERA 589971-14AD.

Part: GIRT BAR — INCORRECT (ZONE 800) · airframe 99,182 hrs · 42,520 cycles

SHIP 684 1L DOOR NOT ARMING CORRECTLY W/ LIGHT. CORRECTIVE ACTION: RE-SECURED GIRT BAR AT 1L. DOOR ARMS NML. REF B757 AMM 52-11. (7036362)

Part: LENS — WRONG PART (ZONE 200) · airframe 98,784 hrs · 42,320 cycles

SHIP 684 ON S/C FOUND E-LIGHT LENS INCORRECT COLOR ON AFT POSITION OF SEAT ROW 18. CORRECTIVE ACTION: NSTALLED CORRECT WHITE LENS ON AFT POS OF SEAT ROW 18. IN REF TO B757 AMM 33-51 NOW CKS GOOD. (6450466)

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 98,691 hrs · 42,263 cycles

SHIP 684 1R DOOR WILL NOT CLOSE AND ASM PROPERLY. CORRECTIVE ACTION: ADJUSTED DOOR IAW B757 AMM 52-11. (6778794)

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 98,637 hrs · 42,234 cycles

SHIP 684 DOOR ARM LGHT ABOVE ONE LEFT INOP. ALL OTHER INDICATIONS SHOW 1L SLIDE IS ARMED. CORRECTIVE ACTION: REPLACED SLIDE LIGHT CAP ASSY PER B757 AMM 25-66 OPS CHK NML. (6778766)

Part: HYDRAULIC LINE — CRACKED (ZONE 600) · airframe 98,439 hrs · 42,148 cycles

SHIP 0684 -MISC/DE- DUE TO LOSS OF LEFT HYDRAULIC QUANTITY ON APPROACH. MAINTENANCE FOUND CRACKED TUBE AT RIGHT AILERON, REMOVED AND REPLACED. R/R #1 ENGINE EDP. R/R LT HYD SYS, PTU PRESSURE, ACMP PRESSURE AND CASE DRAIN FILTERS.

Part: INDICATOR — INOPERATIVE (DOOR) · airframe 98,012 hrs · 41,820 cycles

SHIP 684 3R KNEE KNOCKER PLACARD DOES NOT EXTEND WHEN DOOR IS ARMED. CORRECTIVE ACTION: FOUND LOWER LINING SLIGHTLY MISALIGNED AND PREVENTING KNUCKLE KNOCKER FROM EXTENDING. ADJUSTED LINING AND OPS CKS GOOD IAW B757 AMM 52-11. NO 'M' PROC. PLACARD REMOVED. (6435996)

Part: COVER — DETACHED (ZONE 200) · airframe 97,786 hrs · 41,645 cycles

SHIP 684 AISLE EXIT LIGHT COVER CAME OFF. CORRECTIVE ACTION: RE-INSTALLED SIGN. (5657936)

Part: INDICATOR — FAILED (ZONE 800) · airframe 97,777 hrs · 41,638 cycles

SHIP 684 2L DOOR KNUCKLE KNOCKER FLUSH BUT DOOR SHOWS ARMED. CORRECTIVE ACTION: OPS CHECKED DOOR ARM & DISARM SEVERAL TIMES, FOUND PLAC ON KNUCKLE KNOCKER CURLED UP & CATCHING, CLEANED EDGE OF PLAC, KNUCKLE KNOCKER OPS NML REF B757 AMM 52-11. (5657930)

Part: LANYARD — UNSECURE (ZONE 800) · airframe 97,772 hrs · 41,634 cycles

SHIP 684 1R DOOR WONT ARM, SEEMS LIKE SOMETHING JAMMING. CORRECTIVE ACTION: RESECURED LANYARD UNDER 1R DOOR, NOW ARMS NORMAL. (5657918)

Part: INDICATOR — OBSTRUCTED (ZONE 800) · airframe 97,739 hrs · 41,616 cycles

SHIP 684 2L KNOCKER DOES NOT COME OUT WHEN DOOR IS ARMED. CORRECTIVE ACTION: TRIMMED RAGGED EDGE OF PLACARD BLOCK 2L DOOR KNUCKLER PER B757 AMM 11-30. OPS CK DOOR OPS CK NML. (5657904)

Part: PROXIMITY SENSOR — MISINSTALLED (ZONE 800) · airframe 97,735 hrs · 41,611 cycles

SHIP 684 L2 DOOR SLIDE ARMED LIGHT DOES NOT ILLUMINATE WHEN ARMED. CORRECTIVE ACTION: T/S FOUND INCORRECT MOUNTING HARDWARE ON BOTH GIRT BAR PROX SENSORS AND BOTH SENSORS LOOSE. R/R BOTH PROX SENSORS PER B757 AMM 25-66 AND INSTALLED CORRECT HARDWARE AND VERIFIED WIRED CORRECT. SLIDE INDICATION CKS GOOD. (5049791)

Part: INDICATOR — INOPERATIVE (L3 DOOR) · airframe 97,667 hrs · 41,567 cycles

SHIP 684 L3 DOOR KNUCKLE BUSTER INOP. CORRECTIVE ACTION: FOUND DOOR LINER INTERFERING W/ KNUCKLE KNOCKER, REPOSTIONED LINER REF B757 AMM 52-11. KNUCKLE KNOCKER OPS NORMAL REF B757 AMM 25-66. (5049719)

Part: GIRT BAR — FOD (L4 DOOR) · airframe 97,662 hrs · 41,564 cycles

SHIP 684 DOOR 4L WOULD NOT ARM. CORRECTIVE ACTION: CLEANED OUT PIRT BAR AREA. (5049716)

Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 97,624 hrs · 41,539 cycles

SHIP 684 3L DOOR KNUCKLE KNOCKER DOES NOT INDICATE ARMED POSITION. CORRECTIVE ACTION: DOOR OPERATES AS REQ. (5917782)

Part: INDICATION SYS — FAULTED (ZONE 800) · airframe 97,624 hrs · 41,539 cycles

SHIP 684 DOOR SLIDE ARMED LIGHT STAYS ON WITH DOOR DISARMED AND OPEN. CORRECTIVE ACTION: CYCLED DOOR. CHKS NML @ THIS TIME. NO LIGHT STAYING ON WHEN DISARMED & WITH DOOR OPEN. (5917786)

Part: GIRT BAR — FAULTED (ZONE 200) · airframe 97,607 hrs · 41,527 cycles

SHIP 684 1L DOOR WONT INDICATE ARMED. CORRECTIVE ACTION: REPLACED L1 GIRT BAR PLUS LUBED GIRT BAR IAW B757 AMM 25-66. (5917760)

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON UPPER SKIN OF FWD. FLAP WSTA.85 AT LH WING INB. MAIN FLAP. CORRECTIVE ACTION: SUMMARY OF NRC 00176. AREA WAS REPAIRED PER ER/A 618970-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (0449633)

Part: THRESHOLD — WORN (AFT CARGO) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 HIDDEN DAMAGE IN REF NRC 00032: WEAR ON FASTENER HOLE AFT CORNER OF THRESHOLD AREA AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00632. AREA WAS REPAIRED PER ER/A 618773-14 REV ORIGINAL SECTION I: REPAIR INSTRUCTION AND PRI 618773-14 REV 4. (0449414)

Part: SKIN — DEBONDED (NR 7 SLAT) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 AD - 01 DISBONDED AREA WAS FOUND ON TRAILING EDGE WEDGE LOWER SKIN OF SLAT 7 OF 2.250IN LENGTH AND 2.00 IN WIDTH AT OSS 307 IN REFERENCE TO JOB 207-0001 CARD 5740-01145-05G. CORRECTIVE ACTION: SUMMARY OF NRC 00074: TRAILING EDGE WEDGE LOWER SKIN OF SLAT 7 OF 2.250IN LENGTH AND 2.00 IN WIDTH AT OSS 307 WAS REPAIRED PER B757-200 S.R.M. 51-70-10-2R PAR.18 AND 20. B. IN REFERENCE B757- 200 S.R.M. 57-43-02. (0447633)

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 DTE, ERA 618773-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN AT C2 CUTOUT, LOWER AFT CORNER. CORRECTIVE ACTION: REF ERA 618773-14. (0447815)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 IN REF NIRC 00460: CORROSION ON CUPS WEB BTW STA 1160 TO STA 1170 RBL.70 AT CPAX. CORRECTIVE ACTION: SUMMARY OF NRC 00694: CUPS WEB BTW STA 1160 TO STA 1170 RBL.70 AT CPAX. WAS REPAIRED PER ERA 618766-14 REV ORIGINAL SECTION I (0442610)

Part: DRAG FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE # 6 CORROSION ON SKIN AND FITTING BTW 5-7 O CLOCK POSITION & HOLE # 9 CORROSION ON SKIN AND FITTING BTW 9 TO 11 O CLOCK POSITION IN REF. CARD 5720-01100 -04A JOB # 121-0001 STEP 14 C. SUMMARY OF NRC 00502: HOLES 6 & 9 WERE REPAIRED PER PRI 589971-14AD REV 5 & ER/A 589971-14AD REV. C ".

Part: FRAME — DENTED (ZONE 100) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 DENT ON FRAME STA. 1260 ABOVE S-26R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00543: DENT ON FRAME STA. 1260 ABOVE S-26R AT AFT CARGO COMPARTMENT.WAS REPAIRED PER ER/A 618976-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (0442411)

Part: FRAME — NOT REPORTED (ZONE 100) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 DTE, ERA 618976-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME AT STA 1260 BETWEEN S-26R & S-27R. CORRECTIVE ACTION: REF ERA 618976-14

Part: SLIDER — OUT OF LIMITS (L2 GIRT BAR) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 IN REF. TASK 2566-2001-03 STEP 2: FWD GIRT BAR SLIDER, MEASURE OUT OF LIMITS AT 2L DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00111: FWD GIRT BAR SLIDER AT 2L DOOR WAS REPLACED BY NEW PER B757-200 AMM 25-66-10. (0439951)

Part: BALLSCREW — CORRODED (RT WING TE FLAP) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON BALLSCREW NUT ON OUTBD BALLSCREW FROM INBD TRAILING EDGE FLAP AT RH WING. CORRECTIVE ACITON:SUMMARY OF NRC 00472: OUTB BALLSCREW OF INBD TRAILING EDGE FLAP AT RH WING WAS REMOVED AND SERVICEABLE OUTB BALLSCREW OF INBD TRAILING EDGE FLAP AT RH WING WAS INSTALLED UNDER AMDS. (0438465)

Part: BEARING — STUCK (R2 DOOR) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 SECONDARY NRC: IN REF AMDS 5211-9001-2R, DURING TO PERFORM ADJUSTMENT DOOR, LOWER BEARING WAS FOUND STUCK. CORRECTIVE ACITON: SUMMARY OF NRC 00790: ESCAPE SLIDE ON PASSENGER DOOR 2R WAS REMOVED AND SAME WAS INSTALLED THEREFORE BEARING ON LOWER HINGE PASSENGER DOOR 2R WAS REPLACED BY NEW BEARING, PER. B757-200 AMM 20-10-02, SOPM 20-50-03 AND AMM 25-66-01. (0434670)

Part: STRINGER — CORRODED (S28L) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON STRINGER-28L BTW STA. 1630-1632 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00731: STRINGER-28L BTW STA. 1630-1632 AT AFT CARGO COMPARTMENT.WAS REPAIRED PER B757-200 SRM 53-00-03-2R REPAIR 1. (0429752)

Part: PLATE — DAMAGED (BS 1330-1390) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 ELONGATED HOLES ON SIDE PLATE LH SIDE BTW STA 1330 TO STA 1390 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00256 SIDE PLATE LH SIDE BTW STA 1310 TO STA 1410 AT AFT CARGO COMPARTMEN WAS FABRICATED AND REPLACED PER B757-200 SRM 53-00-53. (0429262)

Part: PLATE — CORRODED (BS 1280-1310) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 SECONDARY NRC :IN REF.NRC NO 246. AFTER REMOVAL OF CORROSION ON SIDE PLATE LH SIDE, BTW STA 1280 TO 1310 REMAINING THICKNESS WAS FOUND OUT LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00756 PERMANENT REPAIR ON SIDE PLATE LH SIDE, BTW STA 1280 TO 1310 WAS PERFORMED PER B757-200 SRM 53-00-53-2R PROCEDURE 2, REPAIR 2, PAR.4.

Part: FRAME — CORRODED (BS 1620 S28L/R) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON FRAME STA. 1620 BTW S-28L TO S-28R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00730 NEW SECTION FRAME STA. 1620 BTW BTW S-25L TO S-25R WAS FABRICATED PER B757-200 SRM 51- 40-05-0G AND DWG 146N1031 REV.G. AND REPLACED PER B757-200, SRM 51-40-02-0G, PAR.4. AND PAR.7. (0429193)

Part: FLOOR SUPPORT — CORRODED (BS 1470) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON FLOOR STRINGER SUPPORT ON STA 1470 LBL 2.9 ALSO 7.5 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00263: FLOOR STRINGER SUPPORT ON STA 1470 LBL 2.9 ALSO 7.5 AT AFT CARGO COMPARTMENT.WERE FABRICATED PER B757-200 DWG 146N5447 REV. C AND INSTALLED PER B757-200 SRM 51-40-02-0G PAR 7.D AND PAR 9. (0427809)

Part: STRINGER — CORRODED (BS 1630-1632S28L) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON STRINGER-28L BTW STA. 1630-1632 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00731: STRINGER-28L BTW STA. 1630-1632 AT AFT CARGO COMPARTMENT. WAS REPAIRED PER B757-200 SRM 53-00-03. (0429480)

Part: PLATE — CORRODED (BS 1235-1270) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 IN REF NRC 00248: CORROSION ON SIDE PLATE RH SIDE BTW STA 1235 TO STA 1270 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00710 PERMANENT REPAIR ON SIDE PLATE RH SIDE BTW STA 1235 TO STA 1270 AT AFT CARGO COMPARTMENT WAS PERFORMED PER B757-200 SRM. (0425947)

Part: FLOOR SUPPORT — CORRODED (BS 1440 RBL16) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON FLOOR STRINGER ON STA 1440 RBL 16.1 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00261 FLOOR STRINGER ON STA 1440 TO STA 1340 RBL 16.1 AT AFT CARGO COMPARTMENT WAS FABRICATED PER DGW 146N5417 REV A, REPLACED PER B757-200 SRM. (0423931)

Part: FRAME — CRACKED (BS 1560 S26-27R) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 A.A. CRACK OF 0.250 IN LENGTH ON RH FRAME INNER CHORD AT STA 1560 BTW S-26 RH AND S-27 RH AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00121: RH FRAME INNER CHORD AT STA 1560 BTW S-26 RH AND S-27 RH AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 618328-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (0419014)

Part: FRAME — CRACKED (BS 1560 S26-27R) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 FUSELAGE / MAIN FRAME / STA 1560 FRAME / INNER CHORD / BETWEEN S-26R & S-27R / CRACK DTE, ERA 618328-14. CORRECTIVE ACTION: REF ERA 618328-14. (0418561)

Part: CREASE BEAM — CRACKED (BS 420) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CRACK ON CREASE BEAM BTW STA 420 AND LBL 62 AT W1. CORRECTIVE ACTION: SUMMARY OF NRC 00384.CREASE BEAM BTW STA 420 AND LBL 62 AT W1 WAS REPAIRED PER PRI NO.618585-14 REV 1, AND ER/A NO.618585-14 REV.ORIGINAL SECTION I: PERMANENT REPAIR. (0416282)

Part: FLOOR SUPPORT — CORRODED (BS 691-696) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 IN REF NRC #00241. CORROSION ON FLOOR SUPPORT RBL 2.90 BTW STA 691-696 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00755 FLOOR SUPPORT RBL 2.90 BTW STA 634-704 AT FWD CARGO COMPARTMENT WAS REPLACED PER B757- 200 SRM 51-40-02-0G PAR.4. AND PAR.7. (0416341)

Part: ACCESS PANEL — DEBONDED (HORIZONTAL STAB) · airframe 97,555 hrs · 41,493 cycles

DISBOND COMPOSITE MATERIAL ON LEADING EDGE ACCESS PANEL 342DR (INB. SIDE) AT HORIZONTAL STABILIZER. LEADING EDGE ACCESS PANEL 342DR (INB. SIDE ) AT HORIZONTAL STABILIZER WAS REPAIRED IAW PRI ER/A 618656-14 REV. 0. AND ER/A 618656-14 REV. ORIGINAL.

Part: SKIN — DEBONDED (NR 2 SLAT) · airframe 97,555 hrs · 41,493 cycles

DISBONDED AREA WAS FOUND ON TRAILING EDGE WEDGE LOWER SKIN OF SLAT 2 OF 2.5IN LENGTH AND 1.0IN WIDTH AT OSS 576. TRAILING EDGE WEDGE LOWER SKIN OF SLAT NR 2 WAS REPAIRED PER B757-200 SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND SRM 57-43-02-2R PROCEDURE 1 REPAIR 1.

Part: SKIN — DEBONDED (NR 6 SLAT) · airframe 97,555 hrs · 41,493 cycles

DISBONDED AREAS WERE FOUND ON TRAILING EDGE WEDGE UPPER SKIN OF SLAT 6. 1.3 IN LENGTH & 0.6 IN WIDTH AT ISS 255.5, 2. 1.3 IN LENGTH & 0.5 IN WIDTH AT ISS 266, 0.8 IN LENGTH & 0.375 IN WIDTH AT ISS 270. TRAILING EDGE WEDGE UPPER SKIN OF SLAT 6 WAS REPAIRED IAW SRM 51-70-10-2R, PROCEDURE REPAIR GENERAL & SRM 57-43-02-2R, PROCEDURE 1, REPAIR 1.

Part: SKIN — DEBONDED (NR 1 SLAT) · airframe 97,555 hrs · 41,493 cycles

DISBONDED AREAS WERE FOUND ON TRAILING EDGE WEDGE UPPER SKIN OF SLAT 1, 4.0 IN LENGTH AND 2.125 IN WIDTH AT OSS 708, 2, 1.0 IN LENGTH AND 0.75 IN WIDTH AT OSS 802. TRAILING EDGE WEDGE UPPER SKIN OF SLAT 1 REPAIR IAW SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND SRM 57-43-02-2R PROCEDURE 1, REPAIR 1.

Part: SKIN — DEBONDED (NR 8 SLAT) · airframe 97,555 hrs · 41,493 cycles

DISBONDED AREA WAS FOUND ON TRAILING EDGE WEDGE UPPER SKIN OF SLAT 8 OF 1.125IN LENGTH AND 1.0IN WIDTH AT OSS 518 IN REFERENCE TO JOB 205-0001 CARD 5740-01145-05H. TRAILING EDGE WEDGE UPPER SKIN OF SLAT 8 WAS REPAIRED IAW SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND SRM 57-43-02-2R PROCEDURE 1 REPAIR 1.

Part: GIRT BAR — MISINSTALLED (L2 DOOR SLIDE) · airframe 97,555 hrs · 41,493 cycles

WRONG INSTALLED BAR ON SLIDE ARMING MECHANISM AT 2L DOOR. BAR ON SLIDE ARMING MECHANISM AT 2L DOOR, WAS INSTALLED CORRECTLY IAW AMM 52-11.

Part: FRAME — CORRODED (BS 1160 S16-17L) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

CORROSION ON FRAME WEB 1160 BTW S-16L AND S- 17L IN PAX CABIN. PERMANENT REPAIR ON FRAME WEB 1160 BTW S-16L AND S-17L IN PAX CABIN WAS PERFORMED PER PRI NO.618609-14. REV.1. AND ER/A NO.618609-14, REV.ORIGINAL , SECTION I.

Part: GIRT BAR — MISINSTALLED (L1 DOOR) · airframe 97,555 hrs · 41,493 cycles

WRONG INSTALLED BAR ON SLIDE ARMING MECHANISM AT 1L DOOR. BAR ON SLIDE ARMING MECHANISM AT L1 DOOR WAS INSTALLED CORRECTLY IAW AMM 52-11.

Part: FLOOR SUPPORT — CORRODED (BS 1180-1185) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

CORROSION ON ANGLE BETWEEN BS 1180 & 1185, RBL 65 IN PASSENGER CABIN FLOOR STRUCTURE. A PERMANENT REPAIR BETWEEN BS 1180 TO 1185, RBL.65 WAS PERFORMED IAW SRM 53-00-13-2R REPAIR 1.

Part: SKIN — DEBONDED (NR 5 SLAT TE) · airframe 97,555 hrs · 41,493 cycles

DISBONDED AREA WAS FOUND ON TRAILING EDGE WEDGE UPPER SKIN OF SLAT 5 OF 1.125IN LENGTH AND 1.0IN WIDTH AT OSS 264 IN REFERENCE TO JOB 210-0001 CARD 5740-01145-05E. TRAILING EDGE WEDGE UPPER SKIN OF SLAT 5 WAS REPAIRED IAW SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND SRM 57-43-02-2R PROCEDURE 1 REPAIR 1.

Part: SKIN — DEBONDED (NR 7 SLAT TE) · airframe 97,555 hrs · 41,493 cycles

DISBONDED AREA WAS FOUND ON TRAILING EDGE WEDGE UPPER SKIN OF SLAT 7 OF 1.0IN LENGTH AND 0.9IN WIDTH AT OSS 432 IAW JOB 207-0001 CARD 5740-01145-05G. TRAILING EDGE WEDGE UPPER SKIN OF SLAT 7 WAS REPAIRED IAW SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND SRM 57-43-02-2R PROCEDURE 1 REPAIR 1.

Part: FRAME — DENTED (BS 1580 S26R) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 DENTS ON FRAME STA. 1580 ABOVE S-26R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00437. FRAME STA. 1580 ABOVE S-26R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM 53-00-07-2R PROCEDURE 5. (0404406)

Part: FLOORBEAM — CORRODED (BS 340 LBL 13) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

CORROSION ON FLOORBEAM ON STA 340 AND LBL 13 ON W1 AT PAX CABIN FLOOR STRUCTURE. FLOORBEAM TEE BS 340 BTW LBL 53 TO RBL 8 WAS REPLACED IAW SRM 53-00-51-2R, REPAIR 10, PAR.4.

Part: SKIN — DEBONDED (NR 9 SLAT TE) · airframe 97,555 hrs · 41,493 cycles

DISBONDED AREAS WERE FOUND ON TRAILING EDGE WEDGE UPPER SKIN OF SLAT 9 AS FOLLOW: 1) 2.0IN LENGTH AND 1.125IN WIDTH AT OSS 600, 2) 0.75IN LENGTH AND 0.6IN WIDTH AT OSS 601 IN REFERENCE TO JOB 206-0001 CARD 5740-01145-05I.. TRAILING EDGE WEDGE UPPER SKIN OF SLAT 9 WAS REPAIRED IAW SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND SRM 57-43-02-2R PROCEDURE 1 REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON FLOOR BEAM BS= 1640 BTW RBL=38 TO LBL=45 AT CPAX. CORRECTIVE ACTION: SUMMARY OF NRC 00427 CORROSION LEVEL 2. FLOOR BEAM T CHORDBS= 1640 BTW RBL=60 TO LBL=60 AT CABIN PAX WAS REPLACED PER B757-200 SRM 53-00-51-2R PROCEDURE 9. (0402123)

Part: ACTUATOR — CORRODED (R1 DOOR) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON BODY OF ACTUATOR PNEUMATIC OF R1 DOOR BTW STA 310.5 /STA 324 AND S-14R /S-15R ON PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00413: ACTUATOR PNEUMATIC OF R1 DOOR BTW STA 310.5 /STA 324 AND S-14R /S-15R ON PAX CABIN WAS REPLACED BY SERVICIABLE PER B757-200 AMM 52-11-34. (0400639)

Part: FLOOR SUPPORT — CORRODED (BS 1645-1681) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 CORROSION ON INTERCOSTAL FROM BS= 1645-1681 AND BL=0 AT CPAX. CORRECTIVE ACTION: SUMMARY OF NRC 00432 ON INTERCOSTAL FROM BS= 1645-1681 AND BL=0 AT CABIN PAX WERE REPLACED PER B757-200 SRM. (0399103)

Part: DECK PLATE — CORRODED (BS 1718) · corrosion level 2 · airframe 97,555 hrs · 41,493 cycles

SHIP 684 IN REF NRC 00430: CORROSION ON DOUBLER OF DECK PLATE STA 1718 LBL 2 AT CPAX(W4). CORRECTIVE ACTION: SUMMARY OF NRC 00687 ON DOUBLER OF DECK PLATE STA 1718 LBL 2 AT CABIN PAX WERE REPLACED PER B757-200 SRM 53-60 -51-2R PROCEDURE 2, REPAIR 2. (0388511)

Part: FASTENER — ABNORMAL (FUSELAGE) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 PREVIOSLY REPAIR (PROTUDING FASTNER) WAS FOUND ON BAD CONDITION BTW STG 2-3 LH AND STA 480-500 ON FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00206 PERMANENT REPAIR CATEGORY "B" BTW STA 480- 500 AND STG 2-3LH ON FUSELAGE SKIN WAS PERFORMED PER B757-200 SRM 53-00-01-2R, REPAIR 29. (0385313)

Part: FASTENER — ABNORMAL (FUSELAGE) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 PREVIOSLY REPAIR (PROTUDING FASTNER) WAS FOUND ON BAD CONDITION BTW STG 2-3 LH AND STA 480-500 ON FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00206 PERMANENT REPAIR CATEGORY "B" BTW STA 480- 500 AND STG 2-3LH ON FUSELAGE SKIN WAS PERFORMED PER B757-200 SRM 53-00-01-2R, REPAIR 29, PAR.4. (0385307)

Part: LIGHT — DETACHED (CABIN) · airframe 96,802 hrs · 41,083 cycles

SHIP 684 EMER LIGHT (UNARMED) LIGHT ON O/H COVER/TILE FALLS OUT. CORRECTIVE ACTION: SECURED EMER LIGHT COVER - OPS NORMAL. (5393082)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,662 hrs · 40,996 cycles

SHIP 0684 -ATB- DUE TO RUDDER RATIO MESSAGE. QRH LANDING WEATHER RESTRICTION PREVENT CONTINUING. CORRECTIVE ACTION: RUDDER RATIO CHANGER ACTUATOR REPLACED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,689 hrs · 41,012 cycles

SHIP 684 EMERGENCY SEAT LIGHT COVER DAMAGED ROW 37D. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED ELP COVER AT ROW 37 D REF B757 AMM 33-51. (5393010)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,968 hrs · 40,544 cycles

SHIP 0684 2L DOOR WONT ARM. CORRECTIVE ACTION: ISNTALLED SAFTEY PIN FOR 2L DOOR. REMOVED AND REPLACED GIRT BAR REF B757 AMM 52-11 SAFTEY PIN REMOVED FROM 2L DOOR. INSTALLED SLIDE COVER OPS CHK GOOD OK FOR SVC. (4585604)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,794 hrs · 40,451 cycles

SHIP 0684 1L DOOR DIFFICULT TO ARM/DISARM. CORRECTIVE ACTION: REMOVED SLIDE COVERS FOUND AFT FLOOR MOUNTSHOWS WEAR, CLEANED MOUNTS AND GIRT BAR SIGNIFICANTLY EASIER TO ARM. (4857896)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,559 hrs · 40,299 cycles

SHIP 0684 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:603. CORRECTIVE ACTION: L1 DOOR KNUCKLE KNOCKER OPS CK GOOD REF 57 AMM 52-11. (2869793)

Part: UNKNOWN — UNKNOWN · airframe 94,681 hrs · 39,751 cycles

SHIP 684 REF: N/R 1 - RIGHT SIDE SKIN DAMAGED BY GROUND EQUIPMENT, LOWER FUSELAGE SKIN BETWEEN STA. 400 AND STA. 420 AND BETWEEN STR 21R AND STR 22R. CORRECTIVE ACTION: REF: N/R 1 - INSTALLED TEMPORARY EXTERNAL SKIN REPAIR REF: B757- 200 SRM 53-00-01-2R REPAIR 14. (N/R-1) CUT OUT DAMAGE TO SKIN AND REMOVED ALL NICKS, SCRATCHES, SHARP EDGES PER B757-200 53-00-01-2R REPAIR 14. FABRICATE DOUBLER I.A.W.B757-200 SRM. INSTALLED REPAIR WASHER I.A.W. B757-200 SRM. INSTALLED REPAIR DOUBLER I.A.W. B757-200 SRM. TOP COATED REPAIR DOUBLER I.A.W. B757-200 SRM. (9968731)

Part: UNKNOWN — UNKNOWN · airframe 94,681 hrs · 39,751 cycles

SHIP 684 REF: N/R 2 FOUND LIGHTNING STRIKE AT STATION 223.5" STR. 22 RT. CORRECTIVE ACTON: N/R 2 INSTALLED PERMANENT REPAIR REF: B757-200 SRM. (9968736)

Part: NONE — NONE · airframe 94,503 hrs · 39,623 cycles

SHIP 684 DOOR 1L WOULD NOT ARM. CORRECTIVE ACTION: FOUND GIRT BAR ATTACH LANYARD OUT OF POSITION. REPOSITION, NOW ARMS NORMAL. (9352222)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 94,426 hrs · 39,563 cycles

SHIP 684 2R DOOR DISARM LEVER STUCK. CORRECTIVE ACTION: 2R DOOR OPS CKS GOOD. (9890086)

Part: NONE — NONE · airframe 93,760 hrs · 39,115 cycles

SHIP 684 DOOR 3L HANDLE VIBRATES (MOVES) UPWARD PAST KNUCKLE KNOCKER DURING FLIGHT. CORRECTIVE ACTION: PR B757 AMM 52-11. ON DOOR 4L, INSTALLED DOOR RES + ESCAPE SLIDE SAFETY PINS. ADJUSTED UPPER + LOWER GATE PUSH RODS, ADJUSTED DOOR STOPS. PRESSURIZED AIRCRAFT, DOOR HANDLE OPS CHK'S NML. DOOR RES AND ESCAPE SLIDE SAFETY PINS RMVD+STOWED. C/W RII. VERIFIED SLIDE RES AND SLIDE PIN RMVD AND STOWED. (9090902)

Part: NONE — NONE · airframe 93,738 hrs · 39,107 cycles

'SUPPLIMENTAL INFORMATION' SHIP 684 3L DOOR KNUCKLE KNOCKER INOP. CORRECTIVE ACTION: REMOVED L4 DOOR BUSTLE NOT L3, NO L3 OR -200. INSTALLED SAFTY PIN ON SLIDE. REPLACED DOOR BRACKET ASSY REF B757 IPC 52-11. REMOVED SLIDE SAFTY PIN & STOWED. CLOSED DOOR BUSTLE OPS CK NML. (9033158)

Part: NONE — NONE · airframe 93,664 hrs · 39,053 cycles

SHIP 684 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:604. CORRECTIVE ACTION: REPLACED LIGHT DIFFUSER COVER @ R-2 DOOR LOC 604 PER B757 AMM 25 -21. (2405748)

Part: NONE — NONE · airframe 93,555 hrs · 38,955 cycles

SHIP 684 FOUND DURING GIRT BAR INSP 1R PAX DOOR FWD LWR BEARING PLATE MISSING. CORRECTIVE ACTION: INSTALLED BEARING PLATE IAW B757 AMM 52-11. (8979788)

Part: NONE — NONE · airframe 93,528 hrs · 38,933 cycles

'SUPPLIMENTAL INFORMATION' SHIP 684 1L SLIDE ARM LIGHT INOP. CORRECTIVE ACTION: INSPECTED 1L SLIDE LIGHT INDICATION ASSY W/ NO DEFECTS NOTED AND CONFIRMED POWER AND GROUND OKAY. FOUND FWD PROX SENSOR FAULTY. REMOVED AND REPLACED FWD 1L GIRT BAR PROX SENSOR IN REF W/ B757 AMM 25-66. OPS NML. (8979734)

Part: GIRT BAR — DIRTY · airframe 93,432 hrs · 38,863 cycles

SHIP 684 R2 DOOR SLIDE LIGHT REMAINS ILLUMINATED W/ SLIDE DISARMED. CORRECTIVE ACTION: CLEANED GIRT BAR AT 2R DOOR. PERFORMED OPS CHK OF ARMING AND DISARMING DOOR AND LIGHT. (9244382)

Part: NONE — NONE · airframe 93,405 hrs · 38,838 cycles

SHIP 684 WEAR ON UPPER SKIN ON LEADING EDGE AND WBL 556 OF OUTBOARD MAIN FLAP AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00098: WEAR ON UPPER SKIN ON LEADING EDGE AND WBL 556 OF OUTBOARD MAIN FLAP AT RH WING WAS REPAIRED PER PRI 600555-14 REV.0 / ER/A 600555-14 REV ORIGINAL AND B-757-200 SRM. (2336832)

Part: NONE — NONE · corrosion level 2 · airframe 93,402 hrs · 38,837 cycles

SHIP 684 H ENG DRAG FTG HOLES NBR 7 TO 10 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #8, CORROSION ON FITTING BTW 10 TO 1 CLOCK POS ; HOLE #9, CORROSION ON SKIN AT 6 CLOCK POS ; HOLE #10 CORROSION ALL AROUND SKIN AND FITTING ; IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00223 HOLE #8; HOLE #9; HOLE #10 WERE REPAIRED PER ER/A 589987-14AD REV. B SECTION VI: PERMANENT REPAIR AND PRI 589987-14, REV. 4. (2335152)

Part: NONE — NONE · corrosion level 2 · airframe 93,402 hrs · 38,837 cycles

SHIP 684 RH ENG DRAG FTG HOLES NBR 11 TO 13 AND 16 TO 18 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #11, GOUGE ON FITTING LOWER EDGE AT 4 CLOCK POS ; HOLE #12, GOUGE ON FITTING LOWER EDGE BTW 7 - 8 CLOCK POS ; HOLE #13 CORROSION ALL AROUND SKIN AND FITTING ; HOLE #16 CORROSION ON FITTING BTW 7 - 8 CLOCK POS ; HOLE #17 CORROSION ALL AROUND SKIN, ALSO CORROSION ON FITTING BTW 4 - 11 CLOCK POS ; HOLE #18 CORROSION ALL AROUND SKIN, ALSO CORROSION ON FITTING BTW 3 - 9 CLOCK POS. IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00224: HOLES OF RH ENG DRAG FITTINGS WERE REPAIRED PER ER/A 589987-14AD REV. B SECTION VI:PERMANET REPAIR AND PRI 589987-14, REV. 4. (2333776)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 WEAR ON LOWER SKIN 35 IN TO INBD EDGE AT TRAILING EDGE WEDGE SLAT 3. CORRECTIVE ACTION: SUMMARY OF NRC:00029 LOWER SKIN 35 IN TO INBD EDGE AT TRAILING EDGE WEDGE SLAT 3. WAS REPAIRED PER PRI 600677-14 REV 1 AND ER/A 600677-14 REV. ORIGINAL AND AREAS THAT ARE WITHIN LIMITS WERE REPAIRED PER B757-200 SRM. (2332697)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 NOISY R1 DOOR INNER HANDLE TO OPEN /CLOSE MOVEMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00368:LOWER LINNER/ BUSTLE COVER AND SAFETY PIN WAS REMOVED, HANDLE MECHANISM WERE LUBED, OPERATIONAL CHECK WAS VERIFIED AND OK TO SERVICE IR DOOR SERVICE / SAFETY PIN WAS STOWED, SAME LOWER LINNER AND BUSTLE COVER WERE INSTALLED PER B757-200 AMM 12-21. (2333602)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 WEAR ON LOWER SKIN 15 IN TO INBD EDGE AT TRAILING EDGE WEDGE SLAT 4. CORRECTIVE ACTION: SUMMARY OF NRC: 00030 LOWER SKIN 15 IN TO INBD EDGE AT TRAILING EDGE WEDGE SLAT 4 WAS REPAIRED PER PRI 600540-14 REV 1 AND ER/A 600540-14REV. ORIGINAL AND AREAS THAT ARE WITHIN LIMITS WERE REPAIRED PER B757-200 SRM. (2332769)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 AWR. A.A. MEASUREMENTS OUT OF TOLERANCE DIAMETER IN BORE HOLES # 1, 2,3,4,5,6,14 AT RH ENG DRAG FITTING. (IN REF AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00326: BORE HOLES # 1, 2,3,4,5,6,14 AT RH ENG DRAG FITTING. (IN REF AMDS 5720-01100-04B / 5720-01100-05B) WAS ATTENDED PER ER/A 589987-14AD REV. B AND PRI 589987-14 REV. 4.(2332547)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 WEAR ON LOWER SKIN 20 IN TO INBD EDGE AT TRAILING EDGE WEDGE SLAT 5. CORRECTIVE ACTION: SUMMARY OF NRC: 00031 LOWER SKIN 20 IN TO INBD EDGE AT TRAILING EDGE WEDGE SLAT 5 WAS REPAIRED PER PRI 600560-14 REV 0 AND ER/A 600560-14 REV. ORIGINAL. (2332246)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 AD, A.A. MEASUREMENTS OUT OF TOLERANCE IN HOLES # 4, 6, 7, 8, 11, 12, 14, , 17 AND 18 AT LH ENG DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00169: LH ENG DRAG FITTING WERE REPAIRED PER PRI 589971-14 REV. 1 & ER/A 589971-14AD REV. B SECTION VI PERMANENT REPAIR. (2330476)

Part: WEDGE — DEBONDED · airframe 93,402 hrs · 38,837 cycles

AIRCRAFT 0684, DISBONDS ON UPPER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE, RH WING OSS 305.5: 7.0IN LENGTH X 3.38IN WIDTH IN REFERENCE TO CARD 5740-01145-05G, STEP 3. CORRECTIVE ACTION: ON REF NRC 00123 THIS REPORT WAS COVERED WIHT THE LOWER REPAIR ON NRC 00164 DUE THE DAMAGE WERE ON THE SAME STA OSS 305.5. (2320294)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 INITIAL INSPECTION:PIN SNUBBER OUT OF LIMIT INDICATION AT 2R DOOR IN REFERENCE AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00158:PASSENGER DOOR 2R WAS REMOVED AND INSTALLED PER B757-200 AMM 52-11-01 AND SNUBBER ON 2R DOOR WAS REPLACED PER B757-200 AMM 52-11. (2318904)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

AIRCRAFT 0684, DISBOND OF 8.000 IN LENGTH X 4.500 IN WIDTH ON LOWER SURFACE LEADING EDGE SLAT 7 TRAILING EDGE WEDGE (INBD EDGE), RH WING. CORRECTIVE ACTION: LOWER SURFACE LEADING EDGE SLAT 7 TRAILING EDGE WEDGE (INBD EDGE), RH WING WAS REPAIRED PER 757-200 S.R.M. 57-43-02-2R PROCEDURE 1 REPAIR 1 FIGURE 201. DETAIL II NOTE D AND S.R.M 51-70-10-2R. (2315897)

Part: FLOOR PANEL — BROKEN · airframe 93,402 hrs · 38,837 cycles

AIRCRAFT 0684, BROKEN (FLOOR PANEL) ( 2EA) FIBERGLASS PAN ASSY BTW STA 775 TO 780 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: FIBERGLASS PAN ASSY BTW STA 775 TO 780 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B757-200 CMM 25-00-66 REPAIR 1-1 PAR. 4. B. (2313565)

Part: WEDGE — DEBONDED · airframe 93,402 hrs · 38,837 cycles

AIRCRAFT 0684, DISBOND ON LOWER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE, LH WING OSS 305.5: 2.3IN LENGTH X 2.0IN WIDTH IN REFERENCE TO CARD 5740-01145-05D, STEP 3. CORRECTIVE ACTION: TRAILING EDGE WEDGE, LH WING OSS 305.5 : 2.3 IN. LENGTH X 2.0 IN . WIDTH WAS REPAIRED PER B757-200 S.R.M. 51-70-10-2R. (2311695)

Part: WEDGE — DEBONDED · airframe 93,402 hrs · 38,837 cycles

AIRCRAFT 0684, DISBOND ON LOWER SURFACE, LE SLAT 1 TRAILING EDGE WEDGE, LH WING OSS 820.4: 0.953IN LENGTH X 0.625IN WIDTH. CORRECTIVE ACTION: LOWER SURFACE, L.E. SLAT 1 TRAILING EDGE WEDGE, LH WING OSS 820.4: 0.953IN. LENGTH X 0.625IN. WIDTH WERE REPAIRED PER B757-200 S.R.M. 51-70-10-2R PROCEDURE REPAIR GENERAL IN REFERENCE B757-200.S.R.M. 57-43-02- 2R-1. (2311707)

Part: BUSHING — MIGRATED · airframe 93,402 hrs · 38,837 cycles

SHIP 684 MIGRATED INBOARD BUSHING ON LOWER ATTACH POINT LUG OF UPPER LINK AT LH PYLON STRUT IN REF AMDS. CORRECTIVE ACTION:SUMMARY OF NRC 00322: BUSHINGS ON LOWER ATTACH POINT LUG OF UPPER LINK AT LH PYLON STRUT WERE REPLACED REPAIR PER B757-200 SRM. (2311027)

Part: WEDGE — DEBONDED · airframe 93,402 hrs · 38,837 cycles

AIRCRAFT 0684, DISBONDS ON METALBOND REPAIR AT UPPER SURFACE, LE SLAT 8 TRAILING EDGE WEDGE, RH WING OSS 490: 0.875IN LENGTH X 0.64IN WIDTH IN REFERENCE TO CARD 5740-01145-05H. CORECTIVE ACTION: AREAS ON METALBOND REPAIR AT UPPER SURFACE , L.E. SLAT 8 TRAILING EDGE WEDGE, RH WING OSS 490: 0.875IN. LENGTH X 0.64IN. WIDTH WERE REPAIRED PER BOEING 757-200 S.R.M. 51-70-10-2R PROCEDURE REPAIR GENERAL IN REFERENCE TO BOEING 757- 200 S.R.M. 57-43-02-2R. (2311720)

Part: WEDGE — DEBONDED · airframe 93,402 hrs · 38,837 cycles

AIRCRAFT 0684, DISBONDS ON UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING ISS 155: 0.8IN LENGTH X 0.75IN WIDTH, ISS 255: 1.125IN LENGTH X 1.0IN WIDTH. CORRECTIVE ACTION: AREAS ON UPPER SURFACE, L.E. SLAT 5 TRAILING EDGE WEDGE, LH WING ISS 155: 0.8IN. LENGTH X 0.75IN. WIDTH, ISS 255: 1.125IN. LENGTH X 1.0IN. WIDTH WERE REPAIRED PER B757-200 S.R.M. 51-70-10-2R IN REFERENCE B757-200 S.R.M. 57-43- 02-2R-1 F. (2311713)

Part: WEDGE — DEBONDED · airframe 93,402 hrs · 38,837 cycles

SHIP 684 A.A. - A.D. TWO DISBONDS OF 1.625 IN LENGTH X .750 IN WIDTH AND 1.250 IN LENGTH X 1.125 IN WIDTH ON EXTERNAL PRODUCTION DOUBLER LOWER SURFACE LEADING EDGE SLAT 8 TRAILING EDGE WEDGE (INBD EDGE ), RH WING IN REFERENCE CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00166 : AREAS OF 1.625 IN. LENGTH X .750 IN. WIDTH AND 1.250 IN. LENGTH X 1.125 IN. WIDTH ON EXTERNAL PRODUCTION DOUBLER LOWER SURFACE LEADING EDGE SLAT 8 TRAILING EDGE WEDGE (INBD EDGE), RH WING WERE REPAIRED PER BOEING 757-200 S.R.M. (2310598)

Part: SKIN — DAMAGED (LT WING) · airframe 97,555 hrs · 41,493 cycles

SHIP 684 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589971-14AD REV.A. CORRECTIVE ACTION: SUMMARY: REPETITIVE BHEC WAS PERFORMED PER ER/A 589971-14AD REV.A SECTION IV AND DISCREPANCIES WERE FOUND IN AMDS 5720-01100 -04A AND 5720-01100-05A AND AREA WAS REPAIRED. (2280509)

Part: LINER — OUT OF ADJUST · airframe 93,070 hrs · 38,638 cycles

SHIP 684 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:610. CORRECTIVE ACTION: ADJ DOOR LINER ON 4R DOOR PER B757 AMM 52-13. OPS NML. (2214859)

Part: NONE — NONE · airframe 92,984 hrs · 38,605 cycles

SHIP 684 CREW REPORTS GUSSETT LOCK WON'T HOLD DOOR OPEN. L2 DOOR. CORRECTIVE ACTION: REPLACED HOLD OPEN LOCK COLLAR ON 2L DOOR REF B757 AMM 52-11. OPS CHECKS GOOD. (8475078)

Part: NONE — NONE · airframe 92,917 hrs · 38,554 cycles

SHIP 684 KNUCKLE KNOCKERS WOULD NOT EXTEND TO ARM WITHOUT BEING PULLED OUT. CORRECTIVE ACTION: ADJ DOOR LINER ON 1R/2L DOORS PER B757 AMM 52-13. OPS NML. (2180919)

Part: NONE — NONE · airframe 92,887 hrs · 38,535 cycles

SHIP 684 2L AND 3R DOOR KNOCKER WILL NOT EXTEND. CORRECTIVE ACTION: ROUBLESHOT AND FOUND KNOCKER BINDING ON DOOR PANEL, ADJUSTED KNOCKER OPS TEST GOOD. (8475024)

Part: NONE — NONE · airframe 92,786 hrs · 38,473 cycles

SHIP 684 FOUND 2L DOOR STOP FITTING BEARING/ PLATE MISSING. CORRECTIVE ACTION: REPLACED ONE BEARING PLATE PER B757 AMM 52-11-00. (8593764)

Part: NONE — NONE · airframe 92,460 hrs · 38,289 cycles

SHIP 684 R AFT ENT DOOR EICAS MSG. CORRECTIVE ACTION: CYCLED DOOR MULTIPLE TIMES. INSPECTED SENSORS. NO FAULTS FOUND. OPS CKS GOOD PER B757 AMM 52-71. (8341382)

Part: NONE — NONE · airframe 92,406 hrs · 38,259 cycles

SHIP 684 2R DOOR DISARMED, ARMED LIGHT STILL ON. CORRECTIVE ACTION: ARM AND DISARMED R2 DOOR LIGHT EXTINGUISHED TEST OK VERIFIED GRIT BAR ARMS AND DISARMS. TEST OK PER B757 AMM 52-11. (8341355)

Part: NONE — NONE · airframe 92,232 hrs · 38,193 cycles

SHIP 684 SLIDE LT WILL NOT COME ON. CORRECTIVE ACTION: FOUND DEBRIS UNDER R1 DOOR. CLEANED DEBRIS OK FOR SVC LT COMES ON WHEN ARMED. (8076960)

Part: NONE — NONE · airframe 91,974 hrs · 38,043 cycles

SHIP 684 1R DOOR KNUCKLE KNOCKER NOT WORKING CORRECTLY. CORRECTIVE ACTION: READJUSTED 1R DOOR RAFT COVER. OPS CHK NML. REF B757 AMM 25-66. (8086123)

Part: NONE — NONE · airframe 91,739 hrs · 37,917 cycles

SHIP 684 SEVERAL DOOR STOP FITTINGS BEARING PLATES MISSING AROUND L-2 DOOR. CORRECTIVE ACTION: REPLACED MISSING DOOR STOP FITTING BEARING PLATES PER B757 AMM 52-11 AT R1 AND L2 DOORS. (8075130)

Part: PANEL — MISSING (WING LE) · airframe 91,080 hrs · 37,609 cycles

SHIP 684 DURING WALK AROUND FOUND LEADING EDGE PANEL MISSING. CORRECTIVE ACTION: REMOVED ACCESS PANELS FROM LE SLAT AND 8. FOUND MISSING PERI SEAL ON FLEXIBLE COUPLING , REMOVED AND REPLACED REF B757 AMM 30-11. REINSTALLED ACCESS ON #8 SLAT. #7 SLAT PANEL REINSTALLED AND SEALED. (7865708)

Part: INDICATOR — INOPERATIVE (R1 DOOR ARMING) · airframe 90,966 hrs · 37,557 cycles

SHIP 684 1R DOOR KNUCKLE KNOCKER NOT COMING OUT. CORRECTIVE ACTION: FOUND SCREW ON LINKAGE FOR POP OUT INDICATOR DISCONNECTED. REINSTALLED TIGHTENED OPS CHK GOOD. REF B757 AMM 52-11. (1839542)

Part: INDICATOR — LOOSE (L3 DOOR ARMING) · airframe 90,904 hrs · 37,527 cycles

SHIP 684 EMEGENCY ENTRY DOOR 3L KNUCKLE KNOCKER LOOSE. CORRECTIVE ACTION: ADJUSTED KNUCKLE KNOCKER. (7752646)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,876 hrs · 37,509 cycles

SHIP 684 EMERGENCY LIGHTS INOP AT ROWS 1 2 AND 3 AND R1 DOOR AND L1 DOOR. CORRECTIVE ACTION: REPLACED POWER SUPPLY AND BATTERY PACK AT M730 TESTS GOOD. (7752628)

Part: PANEL — DAMAGED (HORIZONTAL STAB) · airframe 90,814 hrs · 37,480 cycles

SHIP 684 LH HORIZONTAL STAB LOWER LEADING EDGE COMPOSITE PANEL IS DAMAGED REQUIRING REPAIR. CORRECTIVE ACTION: REMOVED L/E TO FOM REPAIR PER B757 AMM 55-15. REPAIRED PER B757-200 SRM PERMANENT REPAIR. INSTALLED L/E AFTER REPAIR PER B757 AMM 55-15.

Part: INDICATOR — INOPERATIVE (DOOR ARMING) · airframe 90,744 hrs · 37,452 cycles

SHIP 684 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:602. CORRECTIVE ACTION:CLEAN / REMOVE DEBRIS FROM KNUCKLE KNOCKER AT 1R DOOR. OP CK GOOD. (1797184)

Part: WARNING SYSTEM — INOPERATIVE (PASS CABIN DOOR) · airframe 90,513 hrs · 37,353 cycles

SHIP 684 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:609. CORRECTIVE ACTION: OPS CHK DOOR ARMING SWITCH AND KNUCKLE BUSTER OH DOOR 609 AFT L OPS CHK NML REF B757 AMM 52-11. (1767238)

Part: RIB — CONTAMINATED (FRONT SPAR) · airframe 90,399 hrs · 37,303 cycles

DURING INSPECITON MAINTENANCE FOUND EXISTING SEALANT NEEDS TO BE REMOVED FROM FRONT SPAR RIB OSS 345.80. C/W ERA 590353-14AD. (LP 1744898)

Part: PANEL — CHIPPED (WING STRUCTURE) · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND PANEL 521BB AND 621BB SEALANT CHIPPED. C/W ERA 590353-14AD.

Part: RIB — CONTAMINATED (LT WING) · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND EXISTANT SEALANT NEEDS REMOVED FROM UNDER LT WING RIB OSS 345.80. C/W ERA 590353-14.

Part: SEALANT — CHIPPED (WING L/E PANELS) · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND RT/LT WING FIXED L/E PANELS 521 AB , 621 AB HAS SEALANT CHIPPED OFF AROUND WASHER EXTERIOR SIDE OF PANEL. REMOVE AND REPLACED CHIPPED OFF SEALANT PER 590353-14.

Part: FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING NO 5 HOLE HAS AN INDICATION OF CORROSION AT THE 10 OCLOCK POSITION FACING AFT IN THE FITTING PORTION OF THE HOLE. REPAIRED PER ERA 589971-14. (LP 1744161)

Part: DRAG FITTING — CONTAMINATED (RT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 9 HAS INDICATION OF CRACK AND 10 - 11 OCLOCK POSITION FACING AFT IN THE FITTING. REPAIRED PER ERA 589971-14 (LP 1744218)

Part: FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE NO 16 HAS INDICATIONS OF CORROSION IN SKIN 360 DEGREES AROUND HOLE. REPAIRED PER ERA 589971-14. (LP 1744157)

Part: DRAG FITTING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 7 HAS INDICATION OF CORROSION IN SKIN. REPAIRED PER ERA 589987-14. (LP 1744219)

Part: DRAG FITTING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 13 HAS INDICATION OF CORROSION IN SKIN. REPAIRED PER ERA 589971-14 (LP 1744246)

Part: DRAG FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 3 HAS INDICATION OF CRACK AND CORROSION AT 10 OCLOCK POSITION FACING AFT IN FITTING AND INDICATION OF CRACK AND CORROSION AT 5 OCLOCK IN SKIN. REPAIRED PER ERA 589971-14. (LP 1744237)

Part: DRAG FITTING — CORRODED (LT ENG) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 2 HAS INDICATION OF CRACK AND CORROSION AT 9 OCLOCK POSITION FACING AFT IN SKIN AND FITTING. REPAIRED PER ERA 589971-14 (LP 1744239)

Part: DRAG FITTING — CORRODED (RT ENG) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 18 HAS INDICATIONS OF CORROSION IN THE FITTING 360 DEGREES AROUND HOLE. REPAIRED PER ERA 589987-14.

Part: DRAG FITTING — CORRODED (RT ENG) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 10 HAS INDICATION OF CRACK AT 10 OCLOCK POSITION FACING AFT IN THE SKIN. REPAIRED PER ERA 489971-14 (LP 1744244)

Part: DRAG FITTING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND RIGHT ENGINE DRAG FITTING HOLE # 16 HAS INDICATIONS OF LEVEL 2 CORROSION IN THE FITTING 360 DEGREES AROUND HOLE. REPAIRED #16 HOLE PER ERA 589987-14.

Part: FITTING — CRACKED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND LH ENG DRAG FITTING HOLE # 18 HAS INDICATIONS OF CRACK AT 3 OCLOCK POSITION IN FITTING AND AT 9 OCLOCK IN SKIN AND FITTING BOTH WITH CORROSION. FITTING HOLE REPAIRED PER ERA 589971-14. (LP 1744160)

Part: FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE NO 6 HAS INDICATION OF CORROSION IN SKIN AND FITTING 360 DEGREES AROUND. REPAIRED PER ERA 589987-14. (LP 1744216)

Part: DRAG FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 5 HAS INDICATION OF CORROSION IN SKIN AND FITTING 360 DEGREES AROUND HOLE. REPAIRED FITTING PER ERA 589971-14. (LP 1744242)

Part: DRAG FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 4 HAS INDICATION OF CRACK AT 10 OCLOCK POSITION FACING AFT IN FITTING. CORROSION REPAIRED PER ERA 589971-14. (LP 1744233)

Part: DRAG FITTING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 1 HAS INDICATIONS OF CORROSION IN THE SKIN AND FITTING 360 DEGREES AROUND HOLE. REPAIRED HOLE PER ERA 589971-14. (LP 1744228)

Part: DRAG FITTING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RIGHT ENGINE DRAG FITTING HOLE # 17 HAS INDICATIONS OF CORROSION IN SKIN AND FITTING 360 DEGREES AROUND HOLE. REPAIRED PER ERA 589987-14.

Part: FITTING — CRACKED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND LH ENG DRAG FITTING HOLE # HAS INDICATIONS OF BOTH CORROSION AND A CRACK IN THE FITTING AT THE 5 OCLOCK POSITION FACING AFT. REPAIRED FITTING PER ERA 589971-14. (LP 1744163)

Part: DRAG FITTING — CORRODED (RT ENGINE) · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND RIGHT ENGINE DRAG FITTING HOLE # 12 HAS INDICATION OF CRACK AT 9 OCLOCK IN FITTING. REPAIRED RIGHT ENGINE DRAG FITTING HOLE #12 PER ERA 589987-14AD (LP 1744278).

Part: FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE NO 8 AS AN INDICATION OF CORROSION IN THE FITTING AT THE 10 OCLOCK POSITION FACING AFT. REPAIRED PER ERA 589971-14. (LP 1744166)

Part: FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON L/H ENG DRAG FITTING NO. 4 HOLE HAS AN INDICATION OF CORROSION NOTED AT THE 10 OCLOCK DIRECTION FACING AFT IN THE SKIN SIDE AND AT THE SAME CLOCK POSITION IN THE FITTING SIDE AN INDICATION OF CORROSION WAS NOTED ALONG WITH A CRACK INDICATION. REPAIRED PER ERA 589971-14. (LP 1744156)

Part: DRAG FITTING — CORRODED (RT ENG) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITING HOLE # 14 HAS INDICATION OF CRACK WITH CORROSION AT 9 OCLOCK POSITION FACING AFT IN THE SKIN AND AN INDICATION OF CRACK WITH CORROSION AT 3 OCLOCK IN SKIN AND FITTING. REPAIRED PER ERA 589987-14. (LP 1744252)

Part: FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 90,399 hrs · 37,303 cycles

DURING INSPECITON MAINTENANCE FOUND CORROSION LEVEL 2 ON LT ENG DRAG FITTING HOLE NO 14 HAS INDICATION OF CRACK WITH CORROSION AT 3 OCLOCK POSITION IN FITTING AND SKIN. REPAIRED PER ERA 589971-14. (LP 1744147)

Part: SKIN — DAMAGED (LT WING) · airframe 91,622 hrs · 37,879 cycles

SHIP 684 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589971-14AD. CORRECTIVE ACTION: REF ERA 589971-14AD. (1743159)

Part: NONE — NONE · airframe 93,402 hrs · 38,837 cycles

SHIP 684 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589987-14AD. CORRECTIVE ACTION: SUMMARY: REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING WAS ACCOMPLISHED PER ER/A 589987-14AD REV.B SECTION VI. (1743157)

Part: SKIN — DAMAGED (RT WING) · airframe 91,622 hrs · 37,879 cycles

SHIP 684 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589987-14AD. CORRECTIVE ACTION: REF ERA 589987-14AD. (1743156)

Part: SLIDE — LOW PRESSURE (R2 DOOR SLIDE) · airframe 89,427 hrs · 36,937 cycles

DURING INSPECTION FOUND R2 DOOR SLIDE PRESSURE IN RED BAND. CORRECTIVE ACTION: REPLACED R2 DOOR SLIDE. SYSTEM OPERATION IS NORMAL.

Part: BULB — UNSECURE (LAVATORY INDICAT) · airframe 89,419 hrs · 36,931 cycles

WHILE IN FLIGHT, FORWARD LAV OCCUPIED INOPERATIVE BULB FELL OUT. AFTER REINSERTING PUSHED PRESS TO TEST AND OBSERVED ARCING AND SPARKS. CORRECTIVE ACTION: FOUND L9001 SWITCH BAD AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CONDENSER — CRACKED (CABIN) · airframe 89,300 hrs · 36,871 cycles

CREW NOTICED ODD SMELL AND HAZE IN COCKPIT AT FL 410, HAZE DISSIPATED QUICKLY, CALLED ATL MAINTENANCE TO TROUBLE SHOOT. TURNED OFF TRIM SWITCH AND HAZE RETURNED. RESET TRIM SWITCH AND HAZE WENT AWAY, TURNED OFF RIGHT PACK NO HAZE BUT SMELL STILL PRESENT. MAINTENANCE FOUND RIGHT CONDENSER/HEAT EXCHANGER CRACKED. SYSTEM OPERATION IS NORMAL.

Part: SWITCH — BROKEN (COCKPIT) · airframe 88,505 hrs · 36,491 cycles

(AIRCRAFT 684, L/P 6470655) NOSE GEAR LT WOULD NOT TURN OFF. SWITCH IS BROKEN AND SPARKED WHEN TRYING TO SHUT IT OFF. LANDING & TAXING LT CB (M31) PULLED TO TURN OFF LIGHT. CORRECTIVE ACTION: R/R'D LIGHT PANEL PER B757 AMM 33-42.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,000 hrs · 36,268 cycles

SHIP 684 TAKEOFF EMERG LTS ON F/O SIDE IN CABIN ILLUMINATED. ALL FA PANEL SWITCHES WERE OFF COCKPIT SWITCH WAS ARMED. TURNING COCKPIT SWITCH TO OFF EXTINGUISHED LIGHTS BUT THEY ILLUMINATED WHEN COCKPIT SWITCH WAS ARMED AGAIN. CORRECTIVE ACTION: ALSO FOUND SEAT LIGHTS AT 32-37 INOP. REPLACED BATTERY PACK AT SUPPLY M735 LIGHTS NOW ON. ALL SEAT LIGHTS AND ABOVE L2 DOOR COME ON IN ARM POSITION. LIGHTS ABOVE L4 DOOR INOP. CEILING EXIT SIGN ABOVE AFT GALLEY INOP. EXIT SIGN AT R4 INOP. R/R ALL EMERGENCY LIGHT BATT PACKS PER B757 AMM 33-51. ALL EMERGENCY LIGHTS OP NML.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 88,000 hrs · 36,268 cycles

SHIP 684 EMERG EXIT ROW COVER ROW26 RIGHT MISSING. CORRECTIVE ACTION: REPLACED COVER. (6242837)

Part: COVER — NOT REPORTED (R4 DOOR HINGE) · airframe 88,719 hrs · 36,587 cycles

(AIRCRAFT 684, L/P 6242834) R4 SERVICE DOOR LOWER HINGE COVERS. CORRETIVE ACTION: RPLCD LUG AND COVER OPS CK GOOD IAW B757 AMM 52-11.

Part: CHARGER — INFLT SEPARATION (CABIN) · airframe 87,554 hrs · 36,070 cycles

(AIRCRAFT 684, L/P 6196462) EMERG BATT AT M737 INOP. CORRECTIVE ACTION: R/R EMERG CHARGER AND BATTERY PER AMM 33-51.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHTS) · airframe 87,234 hrs · 35,944 cycles

FOUND EMERGENCY LIGHT AT SEATS 43-45 INTERMITTENT. REMOVED AND REPLACED M736 EMERGENCY POWER SUPPLY. OPS CK NORMAL PER B757 AMM 33-51.

Part: LENS — DAMAGED (CABIN) · airframe 87,097 hrs · 35,897 cycles

SHIP 684 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:G4B. CORRECTIVE ACTION: REINSTALLED DIFFUSER LENS COVER IAW AMM 33-51. (1181775)

Part: PLATE — MISSING (DOORS) · airframe 88,632 hrs · 36,556 cycles

DURING GIRT BAR LUBE, FOUND ONE DOOR STOP BEARING PLATE MISSING FROM THE R2 AND R4 DOORS. INSTALLED THE BEARING PLATES IAW AMM, OPS CHECKED OK.

Part: GROUND STUD — DIRTY (EMERGENCY LIGHTS) · airframe 85,618 hrs · 35,240 cycles

ON SVC CK FOUND EMERGENCY PATH LIGHTS L9154 AND L9155 ON R1 FLT ATTD CLOSET INOP. FOUND GND TERMINAL GD1420-DC WITH HIGH RESISTANCE. CLEANED GND STUD AND RETORQUED TERMINAL OPS NML PER AMM 33-51.

Part: SIGN — BROKEN (RIGHT SIDE) · airframe 85,166 hrs · 35,029 cycles

(AIRCRAFT 684, L/P 5320708) RIGHT SIDE EXIT ROW SIGN BROKEN WHILE PASSENGER DEPLANING. R/R EPL HOUSING @ 39D.

Part: GIRT BAR — LOOSE (R1 DOOR SLIDE) · airframe 85,156 hrs · 35,020 cycles

(AIRCRAFT 684, L/P 5320706) 1R DOOR WILL NOT ARM OR DISARM. FOUND GIRT BAT LOOSE ON FWD SIDE OF DOOR- SECURED GIRT BAR PER B757 AMM 25-66- OPS CKS GOOD.

Part: ARM — LACK OF LUBE (R2 DOOR) · airframe 85,056 hrs · 34,966 cycles

(AIRCRAFT 684, L/P 4749164) INBOUND CREW REPORTED DOOR 2R VERY HARD TO ARM AND DISARM. CLEANED & LUBED DOOR ACCESS ENGAGEMENT ARM. ARMS & DISARMS CORRECTLY DOR REQUIRES REASSEMBLY BS076047. REINSTALLED DOOR LINING IAW B757 52-11.

Part: DOUBLER — CORRODED (SERVICE PANEL) · corrosion level 2 · airframe 84,998 hrs · 34,935 cycles

(AIRCRAFT 684, L/P 0809398) INITIAL INSPECTION: CORROSION ON FUSELAGE SKIN BELOW OF AFT LAVATORY SERVICE DOUBLER ACP 0600-100-02Z (FUS). SUMMARY OF NRC #050;LEVEL CORROSION 2; DUE TO EXCESSIVE CORROSION ON FUSELAGE SKIN OF AFT LAVATORY SERVICE, WAS REPAIRED PER ETI-57-18-026 REV.1 AND ER/A 572571-14DA REV. A.MAINTENANCE REQUERIMENTS WERE VERIFIED AND THE FOLLOWING ACTIONS ARE NEEDED: IDENTIFY REPAIR PER P.S. 900-5-1, NO. 04 PER ERA 572571-14AD.

Part: CARTRIDGE — OUT OF LIMITS (LT OVRWG SLIDE) · airframe 84,998 hrs · 34,935 cycles

(AIRCRAFT 684, L/P 0809202) OUT OF LIMITS LEFT OVERWING DISCHARGE CARTRIDGE IN REF AMDS 2620-7051 STEP 2 A(2). SUMMARY OF NRC 00208: LEFT OVERWING DISCHARGE CARTRIDGE OFF WAS REPLACED PER B-757-200 AMM 25-65-02. ELECTRICAL SYSTEM SQUIB TEST WAS PERFORMED PER B-757-200 AMM 25-65-00-765-027 AND TEST IS OK.

Part: STRINGER — CORRODED (BS 1440-1470) · corrosion level 2 · airframe 84,998 hrs · 34,935 cycles

(AIRCRAFT 0684, L/P 0808128) INITIAL INSPECTION: CORROSION ON STR S-29L FROM STA 1440 TO 1470 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 0234; LEVEL CORROSION 2; STRINGER 29LH FROM BS:1430 TO BS: 1490 WAS FOUND WITH EXCESSIVE CORROSION; THEREFORE WAS REPAIRED PER ER/A 572683-14 REV. ORIGINAL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,998 hrs · 34,935 cycles

(AIRCRAFT 684, L/P 0808551) INITIAL INSPECTION: CORROSION ON INTERNAL PRODUCTION DOUBLE AT FWD LAVATORY SERVICE PANEL (E&E). SUMMARY OF NRC #383; LEVEL CORROSION 2; INTERNAL PRODUCTIONS DOUBLERS WERE FOUND WITH EXCESSIVE CORROSION; THEREFORE DOUBLER WERE REPLACED PER B757-200 SRM 51-40-02 PAR 4 AND 7.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

LEVEL CORROSION II. CORROSION OUT OF LIMITS ON STR 29L FROM STA 1460 TO 1480 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2: SECTION LONG 29 LT STA 1460 TO STA 1500 WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON RT SIDE PLATE FROM STA 1440 TO 1530 AT AFT CARGO COMPARTMENT. LEVEL CORROSION 2, SIDE PLATE WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 694, L/P 0802217) CORROSION ON LT SIDE PLATE STA 1400-1530 AT AFT CARGO COMPARTMENT IN REF NRC 00231 (C2) 2020-2379. SUMMARY (CORROSION LEVEL 2) REF NRC00580 LT SIDE PLATE STA 1400-1530 WAS REPLACED PER SRM 51-40-02 PAR. 4 AND 7.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

SHIP 684 CORROSION ON WASTE PANEL INT STRUCTURE BTW STA: 700-720 AT FWD CARGO. CORRECTIVE ACTION: NRC 395: (CORROSION LEVEL 2) DUE TO EXECIVE CORROSION ON DOUBLER OF WASTE PANEL STA 700-720 FWD CARGO, DOUBLER WAS REPLACED PER DWG. (0801350)

Part: BALLSCREW — CORRODED (TE FLAP) · airframe 84,994 hrs · 34,933 cycles

SHIP 684 CORROSION ON OB BALLSCREW NUT AT LT WING INB FLAP. CORRECTIVE ACTION: R/R O/B BALLSCREW NUT AT LT WING INBD FLAP. OPS TEST OK. (0801497)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

SHIP 684 CORROSION POINTS ON SUPPORTS LBL14.00-RBL14.00 ON STA: 690 AND STA: 740 AT FWD CARGO (CCD). CORRECTIVE ACTION: NRC 00131 CORROSION WAS REMOVED PER SRM, WITHIN LIMITS PER SRM. PANAMETRICS 38DL PLUS N/C:1507, TRANSDUCER . AND SUPPORTS STA 690 LBL 14 RBL 14 AND RBL 14 STA 740 WERE REPLACED PER SRM. (0800723)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON STR RBL16.10 TO LBL16.10 FROM STA 1500 TO 1520 AT AFT CARGO COMPARTMENT (C2). (CORROSION LEVEL 2) DOUBLERS OF PREVIOUS REPAIRS ON STR LBL 7.55, LBL 11.40 AND STRINGER 7.55 RBL WERE REPLACED PER SRM 51-40-02 PAR 7 DVI ON STR RBL 10.55, RBL 7.55 AND LBL 2.7 FROM STA 1500 TO 1520 WAS PERFORMED PER SRM 51-10-02 PAR 15A 5A AND NOT CORROSION WAS FOUND.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

SHIP 684 CORROSION POINTS ON STRINGERS INNER/OUTER FACE TROUGH STGR LBL16.00 - RBL16.00 FROM STA 639-660-680-700 AT FWD CARGO (CCD). CORRECTIVE ACTION: NRC 00130 STRINGERS RBL 16.10, LBL 10.45, LBL 16.10 AND RBL 7.55 WERE REPLACED PER SRM. (0800727)

Part: BALLSCREW — CORRODED (TE FLAP) · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0799246) RII: CORROSION ON OB BALLSCREW GIMBAL AT LT WING INBD FLAP (AI). OB BALLSCREW GIMBAL AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51-11-424-020 PAR. A TO E.

Part: BALLSCREW — CORRODED (TE FLAP) · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0799249) RII: CORROSION ON OB BALLSCREW SMALL SHAFT AT LT WING INBD FLAP (AI). OB BALLSCREW SMALL SHAFT AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51-11-424-020 PAR. A TO E.

Part: BALLSCREW — CORRODED (TE FLAP) · airframe 84,994 hrs · 34,933 cycles

SHIP 684 CORROSION ON OB BALLSCREW LARGE SHAFT AT LT WING INBD FLAP. CORRECTIVE ACTION: NRC S/N: 0224: OB BALLSCREW LARGE SHAFT AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51. OPERATIONAL TEST WAS PERFORMED PER AMM 27-51. (0799257).

Part: ADAPTER — CORRODED (TE FLAP) · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0799260) RII: CORROSION ON OB BALLSCREW ADAPTER AT LT WING INBD FLAP (AI). OB BALLSCREW ADAPTER AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51-11-424-020 PAR. A TO E.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON FRAME FITTING SUPPORT STA 1400 S-30 AT AFT CARGO COMPARTMENT (C2). (CORROSION LEVEL 2) FITTING SUPPORT WAS REPLACED PER DWG 140N2001-62 REV BN.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

LEVEL CORROSION 2. CORROSION OUT OF LIMITS ON RT SIDE PLATE FS STA 779 AT FWD CARGO COMPARTMENT. RT SIDE PLATE WAS REPAIRED PER SRM 53-00-53 REPAIR 2.

Part: DOUBLER — WORN (LT PYLON) · airframe 84,994 hrs · 34,933 cycles

WORN OUTBD PREVIOUS REPAIR DOUBLER ON STA NAC 104 AT LT PYLON UPPER SURFACE, ENGINE NR 1. PREVIOUS REPAIR DOUBLER WAS REPLACED PER SRM 54-51-02 REP 1.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0789489) CORROSON ON RT SIDE PLATE FROM STA 1270 TO 1310 AT AFT CARGO COMPARTMENT IN REF NRC S/N 00230 (C2). SUMMARY IN REF NRC 00522 (CORROSION LEVEL 2) SIDE PLATE WAS REPAIRED PER SRM 53-00-53 REP.3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON STR, S22R BTW STA 740-760 AT FWD CARGO COMPT. (CORROSION LEVEL 2) STR, S22R BTW STA 740-760 AT FWD CARGO COMPT WAS REPAIRED PER SRM 53-00-03 REP 1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON INTERCOSTAL STA 1380 AND STR 27L AT AFT CARGO COMPARTMENT (C2). (CORROSION LEVEL 2). INTERCOSTAL LT STA 1360 TO 1380 STRINGER 27 AND 28 WAS REPLACED PER SRM 53-60-04 FIG 1.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0787656) INITIAL INSPECTION. CORROSION ON FRAME CLIP STA 1380 BTW S-27L-S28L AT AFT CARGO COMPARTMENT (C2). SUMMARY NRC S/N 00521 (CORROSION LEVEL 2). FRAME CLIP STA 1380 WAS REMPLACED PER DWG 140N2002 REV B.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0785412) INITIAL INSPECTION: CORROSION ON STR, S22R BTW STA 740-760 AT FWD CARGO COMPT. SUMMARY IN REFERENCE NRC00160 (CORROSION LEVEL 2) STR, S22R BTW STA 740-760 AT FWD CARGO COMPT WAS REPAIRED PER SRM 53-00-03 REP.1. PERFORM A DECAL CONDITION INSPECTION EVERY L CHECK PER TOPP MANUAL 30-10-70.

Part: FRAME — CRACKED (RT PYLON) · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0781588) INITIAL INSPECTION: CRACKED OUTBD FRAME ON STA NAC 136 AT RT PYLON UPPER SURFACE. SUMMARY: IN REFERENCE NRC 00466 FRAME WAS REPLACED PER. SRM 51-40-02 PAR 7 AND DWG. 313N3100 REV. AY.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 84,994 hrs · 34,933 cycles

(AIRCRAFT 684, L/P 0782068) INITIAL INSPECTION: HOLE ON FLOOR PANEL NR: 297B (CPAX). SUMMARY OF NRC 00510: FLOOR PANEL NR. 297B WAS MANUFACTURED, REPLACED AND IDENTIFIED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON INTERCOSTAL FROM STA 1300 TO 1320 BTW S-28L AND S-28R AT AFT CARGO COMPARTMENT IN REF NRC S/N 00228. CORROSION LEVEL 2, INTERCOSTAL WAS REPLACED PER SRM 53-60-04 FIG 1.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

LEVEL CORROSION II CORROSION OUT LIMITS ON LT SIDE PLATE FROM STA 648-766 IN REF SER 200. SIDE PLATE WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7 LEVEL CORROSION 2.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

INITIAL INSPECTION. CORROSION ON RT DOOR LOWER SILL UPPER SURFACE BTW 1653-1669 AT AFT WET AREA. CORROSION LEVEL 2; FOR EXCESSIVE CORROSION IN (SUPPORT AND CLIP) RT LOWER DOOR SILL SUPERIOR SURFACE BTW 1653-1669 IS REPLACED BY DWG 146N5246 REV A AND SRM 51-40-02 PAR 4 AND 7.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

INITIAL INSPECTION, CORROSION ON SCUFF PLATE SUPPORT BTW STA 1644-1680 AND LBL 59 AT AFT WET AREA. CORROSION LEVEL 2; SCUFF PLATE SUPPORT WAS REPLACED PER DWG 146N5246 REV A, BAC5300-2 PAR 8.2 AND SRM 51-40-02 PAR 4 AND 7.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON PREVIOUS REPAIR DOUBLE STA 1716 AND BTW LBL 04-13 AT AFT WET AREA. LEVEL CORROSION 2, REPAIR DOUBLER STA 1716 BTW STA 04-13 AT AFT WET AREA WAS REPLACED PER SRM 53-60-51-2R-2.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER STA 1716 AND BTW RBL 35-44 AT AFT WET AREA. LEVEL CORROSION 2, REPAIR DOUBLER STA 1716 BTW STA 35-44 AT AFT WET AREA WAS REPLACED PER SRM 53-60-51-2R-2.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,994 hrs · 34,933 cycles

CORROSION ON PREVIOUS REPAIR STA 760 OVER STR 20R ACP 0600-100-02Z. LEVEL CORROSION 2, PREVIOUS REPAIR DOUBLER STA 760 OVER STR 20R WAS REPLACED PER ER/A 510131-14 AD REV ORIGINAL.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 84,490 hrs · 34,721 cycles

L1 AND R1 DOOR SLIDE ARMED LIGHTS ONE LED INOP IN EACH MODULE. INSTALLED 2 NEW SLIDE ARMED LIGHT MODULES OPS CK OK REF SPPM 20-84.

Part: LENS — MISSING (CABIN) · airframe 84,490 hrs · 34,721 cycles

ABOVE R2 DOOR EMERGENCY EXIT COVER ONE DIFFUSER LENS MISSING. REPLACED EXIT SIGN AND DIFFUSER AT R2 DOOR IAW AMM 33-51-01.

Part: DOOR — GOUGED (CABIN) · airframe 84,395 hrs · 34,683 cycles

DURING WALK AROUND FOUND GOUGE FWD 2L DOOR. REPAIRED PER ERA 569936-14 REV ORG. REPAIR INSTALLED COMPLETE PER ERA 569936-14 REV ORG.

Part: SKIN — GOUGED (FUSELAGE) · airframe 84,432 hrs · 34,701 cycles

WHILE ON THE LINE IN ATL, MTC FOUND GOUGE DAMAGE TO THE LT FUSELAGE SKIN AT STA 590 AND WL 208.1 BETWEEN STR 16L AND 18L AS SEEN IN FIGURE 1 OF THE INSTRUCTIONS. THE GOUGE DAMAGE HAS BEEN BLENDED OUT, MEASURES APPROX 2 UP/DOWN BY 2 FWD/AFT AND IS LOCATED 12.375 INCHES FWD OF AN EXISTING REPAIR DOUBLER INSTALLED PER ER/A 257031-14. THE SUBJECT SKIN IS MADE FROM 0.080 THICK 2024-T3 CLAD SHEET ALUMINUM LOCALLY CHEM-MILLED DOWN TO 0.063 WITH 0.040 THICK POCKETS IN THE REPAIR AREA. THIS ER/A AUTHORIZES MTC TO ACCOMPLISH AN SRM REPAIR WITH THE PROVISION OF HAVING AN EXISTING REPAIR WITHIN 20 LONGITUDINALLY OF THE REPAIR. DAMAGE TOLERANCE ANALYSIS IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED BY FAA ADVISORY CIRCULAR 120-93.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 84,316 hrs · 34,651 cycles

DURING SVC CHK FOUND FURTHEST AFT ESCAPE PATH LIGHT INOP. FOUND CONNECTOR BEHIND LAV WALL DIS-CONNECTED. RE-CONNECTED, OPS CHK GOOD.

Part: FRAME — CRACKED (BS 1681) · airframe 84,262 hrs · 34,631 cycles

BS 1681, RT SIDE, JUST BELOW FLOOR LINE, INBD FASTENER HOLE HAD A CRACK INDICATION IN FRAME WEB, COMMON TO THE CREASE BEAM CHANNEL FLANGE. VERIFIED BY HFEC INSPECTION. REPAIRED THE FRAME IAW ERA 569012-14AD, REV ORIGINAL.

Part: INDICATOR — OBSTRUCTED (L2 DOOR ARMING) · airframe 84,230 hrs · 34,619 cycles

THE L2 DOOR KNUCKLE KNOCKER INDICATOR WILL NOT EXTEND WHEN DOOR IS ARMED. ADJUSTED THE DOOR LINING COVER, FOUND TO BE RUBBING ON THE INDICATOR. OPS CHECKED GOOD IAW AMM 51-11.

Part: INDICATOR — INOPERATIVE (PAX DOOR) · airframe 83,948 hrs · 34,494 cycles

DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. TROUBLESHOT IAW AMM 52-11, OPS CHECKED GOOD.

Part: INDICATOR — CONTAMINATED (PAX DOOR) · airframe 83,908 hrs · 34,478 cycles

DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. THE KNUCKLE KNOCKER STICKS. REMOVED STICKY DEBRIS FROM KNUCKLE KNOCKER.

Part: NONE — NONE (NONE) · airframe 82,783 hrs · 33,985 cycles

(AIRCRAFT 684, L/P 0329050) EXISTING DOUBLERS INTERFERE WITH LUG DOUBLERS 5,6 BETWEEN FR 620 THRU 660 STR 2R. REFERENCE NR CARD 17 FOR CORRECTIVE ACTION REF SCEPTER LOG NBR 0329034.

Part: NONE — NONE (NONE) · airframe 82,783 hrs · 33,985 cycles

(AIRCRAFT 684, L/P 0329034) C/W PRI 563966-14. COMPLIED WITH PRI 563966-14 ( REV 2 ) A. RECEIVED FINAL ER/A 563966-14 REV A.

Part: RETAINING CLIP — MISALIGNED (FUSELAGE) · airframe 90,399 hrs · 37,303 cycles

WHILE IN DTW FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING D18470-22207 REV. C ) AT FS 660 BETWEEN S-2L AND S-3L, MTC FOUND AN EXISTING INSULATION RETAINING STUD HOLE IN THE LOCATION WHERE THE TEE CLIP EXTRUSION (P/N: P31839-001) IS TO BE INSTALLED TO THE FRAME AND MOUNTED TO THE #7 RH INTERCOSTAL. THE GOGO DRAWING REQUIRES FOUR (QTY 4) 3/16 HOLES TO BE USED FOR ATTACHING THE CLIP TO THE FRAME. C/W ERA 0325746.

Part: RETAINING CLIP — MISALIGNED (FUSELAGE) · airframe 90,399 hrs · 37,303 cycles

DURING THE ACCOMPLISHMENT OF THE 2KU INSTALLATION MAINTENANCE FOUND AN EXISTING HOLE (0.159 DIA) FOR AN INSULATION BLANKET RETAINING CLIP THAT WILL FALL UNDERNEATH THE INTERCOSTAL BRACKET AT FS 580 AND S-1 TO S-2L. C/W ERA 563974-14. (LP 0325033)

Part: RETAINING CLIP — MISALIGNED (FUSE - BLANKET) · airframe 90,399 hrs · 37,303 cycles

DURING THE ACCOMPLISHMENT OF THE 2KU INSTALLATION PER GOGO DWG D18470-22207 REV C, AND AMDS WORKCARD 2330-01349-01D, MAINTENANCE ENCOUNTERED AN EXISTING HOLE (0.159 DIA) AT FS 580 AND S1-2R FOR AN INSULATION BLANKET RETAINING CLIP THAT WILL FALL UNDERNEATH THE INTERCOSTAL BRACKET. ONCE THE PILOT HOLE WAS DRILLED THE CENTER TO CENTER DISTANCE OF THE TWO HOLES IS 0.400. C/W ERA 563975-14.

Part: RETAINING CLIP — MISALIGNED (FUSELAGE) · airframe 90,399 hrs · 37,303 cycles

WHILE PERFORMING 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING D18470-22207 REV. C AT FS 620 BETWEEN S-3R AND S-4R, MTC FOUND AN EXISTING INSULATION RETAINING STUD HOLE IN THE LOCATION WHERE THE TEE CLIP EXTRUSION (P/N: P31839-001) IS TO BE INSTALLED TO THE FRAME AND MOUNTED TO THE #6 RH INTERCOSTAL. C/W ERA 563980-14.

Part: RETAINING CLIP — MISALIGNED (FUSELAGE) · airframe 90,399 hrs · 37,303 cycles

DURING THE ACCOMPLISHMENT OF THE 2KU INSTALLATION PER GOGO DWG D18470-22207 REV C, AT FS 620 BETWEEN S-2R AND S-3R, MAINTENANCE FOUND AN EXISTING HOLE (0.159 DIA) FOR AN INSULATION BLANKET RETAINING CLIP THAT WILL FALL UNDERNEATH THE INTERCOSTAL BRACKET. REPAIRED PER ERA 563978-14.

Part: STRUCTURE — ABNORMAL (BS 620) · airframe 85,170 hrs · 35,033 cycles

SHIP 684 WHILE IN FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING REV. C AT FS 620 BETWEEN S-3L AND S-4L, MTC FOUND AN EXISTING INSULATION RETAINING STUD HOLE IN THE LOCATION WHERE THE TEE CLIP EXTRUSION IS TO BE INSTALLED TO THE FRAME AND MOUNTED TO THE #3 LH INTERCOSTAL. THE GOGO DRAWING REQUIRES FOUR (QTY 4) 3/16 HOLES TO BE USED FOR ATTACHING THE CLIP TO THE FRAME. CORRECTIVE ACTION: REF ERA 563979-14AD REV A. UPDATED FROM MINOR TO MAJOR (0325598)

Part: HANDLE — OUT OF ADJUST (L2 DOOR ARMING) · airframe 82,305 hrs · 33,824 cycles

ARMING HANDLE AT THE L2 DOOR INOPERATIVE. ADJUSTED . OPS CHECKED GOOD.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 81,817 hrs · 33,662 cycles

LEFT HYD SYSTEM FAILURE. FOUND A LEAK COMING FROM FLAP/SLAT DEPRESS MODULE. R & R O-RING. REMOVED AND REPLACED CASE DRAIN AND PRESSURE FILTERS IN EDP AND PTU. ALSO R & R PTU. ALL CHECKED NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 80,813 hrs · 33,364 cycles

DURING SERVICE CHECK FOUND EMERGENCY LIGHT ROW 23 HANGING FROM CEILING PANEL. RESECURED EMERGENCY LIGHT TO CEILING PANEL SEAT ROW 23. CHECKS GOOD.

Part: PANEL — CRACKED (LE SLAT) · airframe 79,905 hrs · 33,061 cycles

RIGHT WING NR 9 SLAT O/B TRACK COVE PANEL AT I/B SIDE OF TRACK IS CRACKED AT FASTENER. REMOVED AND REPLACED NR 9 SLAT O/B TRACK COVE PNL IAW SRM 51-40-02 AND DWG 114N4003 REV E.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 79,905 hrs · 33,061 cycles

AFT CARGO BAY, AFT CARGO DOOR SURROUND, DOOR SILL AT STR 27R BETWEEN STA 1400 TO STA 1425 IS DENTED, DOUBLE DRILLED AND CORRODED. REMOVED AND REPLACED AFT CARGO DOOR SILL AT STR 27R BETWEEN STA 1380-1440 IAW DRAWING 146N5390 REV D SRM 51-40-02, 51-40-05, AND ER/A 373211-14MA REV G.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 79,905 hrs · 33,061 cycles

FWD CARGO BULL NOSE SUPPORTS CORRODED. REMOVED AND. REPLACEDTHE SUPPORTS IAW DRAWING 143N8560 REV T AND 143N 8560 REV G, SRM 51-40-02 5, 51-10-02- 53-30-15, AND AMM 51-24-09-377-001.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 79,905 hrs · 33,061 cycles

AFT CARGO DOOR, PREVIOUS REPAIR AT FWD BOTTOM CORNER IS CRACKED AND BENT AT EDGE. REMOVED AND REPLACED THE REPAIR DOUBLER IAW SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,067 hrs · 32,268 cycles

SEAT ASSY 26DEF EMERGENCY LIGHT ON SEAT ASSY INOPERATIVE. R & R BULBS IAW AMM 33-51.

Part: ACCESS DOOR — DAMAGED (LAV SERVICE) · corrosion level 2 · airframe 76,072 hrs · 31,477 cycles

ON WALK AROUND, FOUND RT MID LAV SERVICE ACCESS DOOR CORRODED BEYOND REPAIR. INSTALLED NEW ACCESS DOOR ON ACFT. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 781) · airframe 72,158 hrs · 30,057 cycles

LIGHTNING STRIKE AT BS 781 STRINGER 3R. REPAIRED IAW PRI 525974-14 REV1.

Part: SKIN — DAMAGED (BS 635) · airframe 72,158 hrs · 30,057 cycles

LIGHTNING STRIKE ON UPPER FUSELAGE BS 635 STRINGER 2R. REPAIRED IAW ERA 525976-14 REV. ORIG.

Part: SKIN — DAMAGED (BS 635 & 781) · airframe 72,158 hrs · 30,057 cycles

LIGHTNING STRIKES ON UPPER SKIN BS 635 STRINGER 1R AND BS 781 NEAR STRINGER 3R. REPAIRED AT BS 635 PER PRI 525976-14 REV. O AND ERA 525976-14 REV. ORIG. BS 781 REPAIRED IAW PRI 525974-14 REV.1 END ERA 525974-14 REV.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 70,406 hrs · 29,431 cycles

ON ARRIVAL, FOUND AFT CARGO DOOR LOWER AFT CORNER DAMAGED. REMOVED DOUBLER IAW ERA 519309-14. HFEC OF HOLES COMMON TO DOUBLER IAW NDT MANUAL 51-00-16. FOUND CRACK INDICATIONS IN SEVERAL HOLES IN CORNER PAN ASSY ONLY. HFEC OF TRIMMED EDGE IAW NDT MAN 51-00-19, PT 6, NO ITEMS. REMOVED CORNER PAN ASSY AND REPLACED CORNER PAN ASSY IAW DWG 146N6621-4.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 69,565 hrs · 29,115 cycles

RED EMERGENCY LIGHT AT 1R GALLEY INOPERATIVE. FOUND AND REPAIRED BROKEN WIRE IAW WDM. OPS CHECKED GOOD.

Part: SKIN — DENTED (BS 1703 S15R) · airframe 68,025 hrs · 28,603 cycles

UPPER FUSELAGE APPROX BS 1703.5, 23.5" AFT OF R4 DOOR CUT OUT 7 INCHES ABOVE STRINGER S15R FOUND DENT. ACCOMPLISHED, ERA 510117-14, REV ORIG.

Part: SEAT TRACK — CORRODED (BS 680 LBL 45.5) · airframe 68,025 hrs · 28,603 cycles

CORROSION ON MAIN CABIN SEAT TRACK CROWN BOTTOM BETWEEN STA 680 AND STA 880, LBL 45.5. REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 1. (TO 235216)

Part: STRINGER SPLICE — CORRODED (BS 1500 S29R) · airframe 68,025 hrs · 28,603 cycles

STRINGER SPLICES CORRODED ON S-29R BETWEEN STA 1500-1520. ACCOMPLISHED SRM 53-00-03, REPAIR 1, FIG 201.

Part: STRINGER SPLICE — CORRODED (BS 1500 S29R) · airframe 68,025 hrs · 28,603 cycles

STRINGER SPLICE ON S-28R CORRODED BETWEEN STA 1500-1520. ACCOMPLISHED REPAIR IAW SRM 53-00-03, REP 1.

Part: SEAT TRACK — WORN (BS 872 LBL 45.5) · airframe 68,025 hrs · 28,603 cycles

WEAR MARKS ON MAIN CABIN SEAT TRACK CROWN AREA BETWEEN STA 868 AND STA 872, LBL 45.5. ACCOMPLISHED SRM REPAIR 53-00-52, FIG 201, REP 3.

Part: STRINGER — CORRODED (BS 1615 S29L) · airframe 68,025 hrs · 28,603 cycles

STRINGER 29L CORRODED ON INNER SURFACE STA 1615. REPAIRED IAW SRM 53-00-03, REPAIR 1 FIG 201.

Part: STRINGER — CORRODED (BS 1500 S-29L) · airframe 68,025 hrs · 28,603 cycles

STRINGER 29L CORRODED BETWEEN STA 1500-1520. ACCOMPLISHED REPAIR SRM 53-00-03, FIG 201, REPAIR 1.

Part: GATE — CORRODED (L4 DOOR) · airframe 68,025 hrs · 28,603 cycles

L-4 DOOR LOWER GATE INSIDE POCKET HAS CORROSION. REPLACED L-4 DOOR LOWER GATE IAW AMM 52-11-38-404-009.

Part: STRINGER CLIP — CORRODED (STRINGER 18L) · airframe 68,025 hrs · 28,603 cycles

ON REMOVAL OF STRINGER 18L, BS 1680-1701, LT FOUND ONE STRINGER CLIP AT STA 1701 CORRODED. R & R PART.

Part: ATTACH ANGLE — CORRODED (BS 1680-1700) · airframe 68,025 hrs · 28,603 cycles

ON REMOVAL OF FWD ATTACH ANGLE ON MAIN CABIN CUSP WEB BS 1680-1700 LT, FOUND ANGLE TO BE CORRODED. R & R ANGLE.

Part: STRINGER — CORRODED (BS 1680-1701) · airframe 68,025 hrs · 28,603 cycles

ON REMOVAL OF CUSP WEB, BETWEEN BS 1680-1701. FOUND STRINGER 18L CORRODED AT BS 1701. R & R STRINGER IAW SRM 51-40-02, PG 7.

Part: SEAT TRACK — CORRODED (BS 377 LBL 25) · airframe 68,025 hrs · 28,603 cycles

MAIN CABIN SEAT TRACK CORRODED AT STA 377, LBL 25. R & R SEAT TRACK IAW SRM 51-40-05, PG 7 AND 21.

Part: SEAT TRACK — CORRODED (STA 365 RBL 45) · airframe 68,025 hrs · 28,603 cycles

FOUND CORROSION ON FWD END OF SEAT TRACK SUPPORT AT BS 365, RBL 45. ACCOMPLISHED ERA 510126-14, REV ORG.

Part: SEAT TRACK — CHAFED (BS 864-872) · airframe 68,025 hrs · 28,603 cycles

WEAR MARKS ON MAIN CABIN SEAT TRACK CROWN BOTTOM AREA BETWEEN STA 864 AND 872 RBL 24.7. REPAIRED IAW SRM 53-00-52, REPAIR 3.

Part: SEAT TRACK — CORRODED (BS 680-880) · airframe 68,025 hrs · 28,603 cycles

CORROSION ON MAIN CABIN SEAT TRACK CROWN/BOTTOM BETWEEN STA 680 & 880, LBL 45.5. R & R SEAT TRACK & SPLICE CHANNEL, REPAIR ACCOMPLISHED IAW SRM 53-00-52.

Part: CREASE BEAM — CORRODED (BS 960 RBL 20.5) · airframe 68,025 hrs · 28,603 cycles

CREASE BEAM CORRODED IN MAIN CABIN STA 960-984 RBL 20.5. REPLACED CREASE BEAM IAW SRM 51-40-02, PG 4 AND 39.

Part: FLOORBEAM — CORRODED (BS 720 LBL 62) · airframe 68,025 hrs · 28,603 cycles

CORROSION ON MAIN CABIN FLOORBEAM UPPER CHORD STA 720, LBL 62. ACCOMPLISHED REPAIR IAW ER/A 481634-14MA, REV A.

Part: SEAT TRACK — CHAFED (BS 864-872) · airframe 68,025 hrs · 28,603 cycles

WEAR MARKS ON MAIN CABIN SEAT TRACK CROWN/BOTTOM AREA BETWEEN BS 864 AND 872 RBL 45.5. REPLACED SEAT TRACK FROM BS 849 TO 880.

Part: CUSP WEB — CORRODED (BS 1180-1200) · airframe 68,025 hrs · 28,603 cycles

CORROSION ON MAIN CABIN LT CUSP WEB BETWEEN STA 1180 AND 1200. REPAIR CUSP WEB IAW ER/A 510973-14, REV ORIGINAL.

Part: FAILSAFE — CORRODED (BS 1540 S14L) · airframe 68,025 hrs · 28,603 cycles

MAIN CABIN LT SIDE STA 1540 AT STR 14L FRAME HAS SURFACE CORROSION. ACCOMPLISHED ERA 508331-14, REV A.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 68,025 hrs · 28,603 cycles

CABIN FLOORBEAM FS 365, UPPER CAP UPPER SURFACE CORRODED. ACOMPLISHED REPAIR IAW SRM 53-00-51, REP 3 AT SAA DURING HMV.

Part: FLOORBEAM — CORRODED (BS 377) · airframe 68,025 hrs · 28,603 cycles

FLOORBEAM FS 377, RBL 6 TO LBL 63 UPPER TEE UPPER SURFACE CORRODED. ACCOMPLISHED ERA 510137-14, REV ORG.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 68,025 hrs · 28,603 cycles

CABIN FLOORBEAM, FS 345 UPPER CAP UPPER SURFACE CORRODED AT FASTENERS HOLES BL-0-LBL13. ACCOMPLISHED SRM 53-00-51, FIG 201 REPAIR AT SAA DURING HMV.

Part: CUSP WEB — CORRODED (BS 1180-1200) · airframe 68,025 hrs · 28,603 cycles

CORROSION ON MAIN CABIN LEFT CUSP WEB BETWEEN STA 1180-1200. COMPLIED WITH ERA 510973-14 REV ORIG.

Part: SKIN SPLICE — CORRODED (BS 1620 S29-30R) · airframe 68,025 hrs · 28,603 cycles

SKIN SPLICE CORRODED STA1620 S-30 - S29R. REPAIRED IAW ER/A 510139-14, REV ORIGINAL.

Part: CONTROL BOX — PUNCTURED (L2 DOOR) · airframe 68,025 hrs · 28,603 cycles

L2 DOOR ARM DISARM BOX HAS A PUNCTURE/ ACCOMPLISHED ERA 504268-14, REV ORIG DURING HMV.

Part: DECK PLATE — CORRODED (BS 1680-1720) · airframe 68,025 hrs · 28,603 cycles

MAIN CABIN FLOOR DECK PLATE CORRODED, STA 1680-1720, BL 0 - RBL 54. ACCOMPLISHED SRM 53-60-51, FIG 201, REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (BS 1718 LBL 52) · airframe 68,025 hrs · 28,603 cycles

MAIN CABIN FLOOR CHORD IS CORRODED STA 1718, LBL52. REPLACED FLOOR CHORD IAW SRM 51-40-02, PG 2 AND 4 DURING HMV.

Part: SHEAR TIE — CORRODED (BS 1480 S29-30L) · airframe 68,025 hrs · 28,603 cycles

CORROSION ON SHEAR TIE, FRONT & BACK STA 1480 BETWEEN S30L-S29L. R & R SHEAR TIE.

Part: CONTROL BOX — PUNCTURED (L4 DOOR) · airframe 68,025 hrs · 28,603 cycles

L4 DOOR ARM / DISARM BOX HAS PUNCTURE. ACCOMPLISHED ERA 504997-14, REV ORIG DURING HMV.

Part: STRINGER SPLICE — CORRODED (BS 1500-1520) · airframe 68,025 hrs · 28,603 cycles

STRINGER SPLICE CORRODED ON STR 29R BETWEEN STA 1500-1520. ACCOMPLISHED SRM 53-00-03, REPAIR 1, FIG 201.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 68,025 hrs · 28,603 cycles

L2 DOOR FRAME AT DOOR CLOSE ASSIST HANDLE ON AFT SIDE IS CORRODED. REPAIRED IAW ERA 507880-14, REV ORIG DURING HMV.

Part: GATE — CORRODED (L1 DOOR) · airframe 68,025 hrs · 28,603 cycles

L1 DOOR LWR GATE CORRODED ON EDGES. R & R.

Part: FRAME — CORRODED (BS 1460) · airframe 68,025 hrs · 28,603 cycles

AFT CARGO FRAME, BS 1460 HAS CORROSION ON FWD AND AFT SIDE FROM STR 26L TO 26R. R & R FRAME.

Part: GATE — CORRODED (L4 DOOR) · airframe 68,025 hrs · 28,603 cycles

L4 DOOR UPPER GATE INSIDE POCKETS HAS CORROSION. R & R GATE DURING HMV.

Part: SKIN — DENTED (BS 1623) · airframe 68,025 hrs · 28,603 cycles

MULTIPLE EXTERNAL OUTWARD, SKIN STA 1623 BETWEEN S23L AND S24L. REPAIRED IAW ERA 510122-14 REV, ORIG DURING HMV.

Part: SKIN — DENTED (BS 1490 S24-25R) · airframe 68,025 hrs · 28,603 cycles

FUSELAGE SKIN HAS AN OUTWARD DENT AT BS 1490 BETWEEN S24R AND S25R. REPAIRED IAW ERA 510964-14, REV ORG. (510964-14).

Part: STRUCTURE — DELAMINATED (NR 2 INLET COWL) · airframe 66,733 hrs · 28,131 cycles

MAINTENANCE DISCOVERED DELAMINATION ON THE NR 2 ENGINE NOSE COWL AT THE 7 O`CLOCK POSITION WHERE INLET LIP MEETS COMPOSITE. INSTALLED PERMANENT REPAIR TO NR 2 INLET COWL IAW SRM 54-11-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,297 hrs · 27,547 cycles

MAINTENANCE FOUND EMERGENCY FLOOD LIGHT INOPERATIVE IN FIRST CLASS CABIN. REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATION NORMAL.

Part: UNKNOWN — FUMES (CABIN) · airframe 61,566 hrs · 26,160 cycles

CREW REPORTED FUMES FROM THE ROW 33-36 AREA. FUMES DISSIPATED WITH UTILITY BUSSES AND RECIRCULATION FANS OFF. MX OPERATED THE APU, PACKS, FANS, AND ALL GALLEY EQUIPMENT WITH NO ODORS. ROW 33-36 AREA WAS INSPECTED WITH NO FINDINGS. ACFT CHECKED OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 48,864 hrs · 22,005 cycles

EMERGENCY FLASHLIGHT AT R4 DOOR INOP. REPLACED BATTERY.

Part: SKIN — MAINT ERROR (FUSELAGE) · airframe 47,715 hrs · 21,659 cycles

DURING HMV AT TIMCO LCQ, THE CRADLE SHORING INSTALLED AT FS 680 CAUSED DENTING ON THE FUSELAGE SKIN. DENTING IS JUST ABOVE S-24R TO JUST BELOW S-25R. THE DENT WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED, WITH TIME-LIMITED RESTRICTIONS PER ER/A 459984-14.

Part: SKIN — DENTED (BS 520) · airframe 47,715 hrs · 21,659 cycles

AT CURRENT HMV, THE CRADLE SHORING INSTALLED AT FS 520 CAUSED TWO DENTS IN THE AIRCRAFT SKIN. ONE DENT IS LOCATED JUST ABOVE S-23R AND THE SECOND DENT IS JUST BELOW S-24R. THE DENTS WERE TRIMMED OUT AND WERE REPAIRED WITH A SINGLE DOUBLER PER ER/A 459969-14.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1535) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO BS 1470 RBL 2.90 CARGO FLOOR SUPPORT STRINGER CORROSION AROUND NUTPLATES HOLES. FABRICATED AND INSTALLED FLOOR SUPPORT FROM BAC1510-1087 AND FLOOR SUPPORT FROM BAC 1517-22-9 7075-T6 .063", 7075-T6511 SPLICE PLATE 6" BY 10" BY 3" WIDE FROM 60-122 EXTRUSION 7075T6511 IAW B757 SRM 53-60-53, 51-70-12 FIG 1, AND 51-20-01 PG 3 - 7, 21.

Part: HOUSING — CORRODED (LAV DRAIN) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON TOP OF LAV DRAIN HOUSING IN E/E BAY BS 418 TO BS 440 S-26L TO S-28L. FABRICATED AND INSTALLED DOUBLER 6-12/" BY 9-1/4" FROM 2024-T3 .040", SUPPORT 16" BY 9-3/4" FROM 2024-T3 .050" IAW B757 SRM 51-20-01, B757 DWG 141N631 AND 51-40-02.

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON BASE OF FRAME AT BS 1400, B/L 2L IN BILGE OF THE AFT CARGO PIT. REMOVED CORRODED SHEAR TIES. REMOVED CORROSION ON FRAME, WITHIN LIMITS IAW B757 SRM 51-10-02, 53-60-07, 53-00-07. FABRICATED AND INSTALLED 2 NEW SHEAR TIES 4.0 BY 2.0 FROM 7075-T6 .050 IAW B757 SRM 51-40-05, 51-20-01 AND 51-30-01.

Part: BEAM — CORRODED (BS 1375-1440) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO COMPT LOCATED BS 1375 - BS 1440 RBL 21 ON TOP OF DOOR CUT OUT THRESHOLD BEAM (LOWER SILL INNER CHORD). REMOVED AND REPLACED CORRODED CHORD WITH P/N 146N8522-57 AND FITTING P/N 69-45578-7 IAW B757 SRM 51-40-02.

Part: SUPPORT FITTING — CORRODED (BS 1440) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT PIT RT SIDE BS 1440 S-26R E6 AVIONICS RACK BOLT RUSTED. REMOVED AND REPLACED SUPPORT FITTING WITH P/H 284N1633-1 IAW B757 SRM 51-40-02.

Part: SPLICE — CORRODED (BS 1400) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON SKIN SPLICE AT BS 1400 S-29L TO 30 IN AFT CARGO COMPARTMENT. FABRICATED AND INSTALLED SKIN SPLICE 36.0" BY 4.0" FROM 7075-T6 .071" IAW B757 SRM 51-40-02 AND BAC146N8522.

Part: PANEL — CORRODED (BS 1445-1530) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

FOUND CORROSION AFT CARGO BS 1445.6 TO BS 1530 LT TRANSITION SIDE PANEL CORROSION ON GILL LINER ATTACH AREA AND FLOOR PANEL ATTACH AREA. FABRICATED AND INSTALLED SPLICE PLATE 4" BY 6" BY 12" AND TRANSITION PANEL 654N0244-1033 (SEE ROUTINE 3770) IAW B757 SRM 51-10-02 AND 51-40-05 FIG 3, AMM 53-88-01-801.

Part: PANEL — CORRODED (BS 620-645) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

FWD CARGO COMPT RT TRANSITION PANEL HAS SURFACE CORROSION FROM BS 620 TO BS 645. CORROSION ON UPPER SURFACE AND AROUND FASTENER HOLES. ROUTED OUT CORROSION. FABRICATED AND INSTALLED DOUBLER 18" BY 8" FROM 7075-T6 .071" AND FILLERS FROM 2024-T3 .063" IAW B757 AMM 53-88-01-801.

Part: INTERCOSTAL — CORRODED (BS 1444) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

FOUND CORROSION AFT CARGO COMPARTMENT UPPER ATTACH ANGLE OF INTERCOSTAL AROUND NUTPLATES UNDERSIDE OF SIDE PANEL RT BETWEEN S-27R AND S-28R BS 1444. REMOVED WEB. FABRICATED AND INSTALLED INTERCOSTAL REPAIR 19.5" BY 6.0" FROM 7075-T6 .050" IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON INTERCOSTAL WEB BS 1400 TO BS 1420 LBL 3 ON LOWER LEG. REMOVED CORRODED INTERCOSTAL WEB. FABRICATED AND INSTALLED REPAIR WEB 19.5" BY 8.6" FROM 7075-T6 .032" IAW B757 SRM 53-60-04, 51-30-01 AND 51-40-02.

Part: SILL — CORRODED (BS 560-620) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION C-1 DOOR CUTOUT LOWER SILL RETAINER ATTACH POINT HOLES BS 560 TO BS 620. REMOVED AND REPLACED LOWER SILL T CHORD C-1 DOOR P/N NR 143N8522-15 IAW B757 SRM 51-40-02 AND 53-60-15 DETAIL V PAGE 102.

Part: PANEL — CORRODED (BS 1310-1380) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO RT TRANSITION PANEL AT BS 1310 TO BS 1380. HEAVY CORROSION BS 1343.5 TO BS 1380 AROUND GILL LINER ATTACH HOLES AND FLOOR PANEL ATTACH HOLES. DRILLED UP AND INSTALLED NEW TRANSITION PANEL 69-1/2" BY 7-1/2" P/N 146N5391U72 IAW B757 SRM 51-40-02.

Part: PANEL — CORRODED (BS 1530-1640) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON UPPER SURFACE OF AFT PIT RT TRANSITION PANEL FROM BS 1530 TO BS 1640. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED DOUBLER 16.0" BY 5.0" FROM 7075-T6 .063" IAW B757 AMM 53-88-01-801, B757 SRM 51-20-01, 53-00-53, 53-60-53 AND 51-40-05.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AT L-4 DOOR AFT FLOORBOARD SUPPORT BETWEEN BS 1660 AND BS 1680 B/L 54L I/B OF S-17L AT NUTPLATES. REPAIRED BY REMOVING FLOOR SUPPORT. INSTALLED P/N 146N5246U5 IAW B757 SRM 51-40-05 AND 51-40-02.

Part: SUPPORT FITTING — CORRODED (BS 580) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

FOUND CORROSION ON THE TIE BLOCK SUPPORT BRACKET NR 3 FROM FWD, AT FWD CARGO DOOR LWR SILL, ZONE 122. REMOVED BRACKET. INSTALLED TIE DOWN BLOCK FITTING P/N 69-45555Y11IAW B757 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AT BASE OF FRAME UNDER FLOOR SUPPORT STRUCTURE THE BULGE OF THE AFT CARGO PIT AT BS 1460 B/O 0 TO B/L 13L. REMOVED SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE 7.0" BY 2.0" FROM 7075-T6 .050" IAW B757 SRM 51-30-01, 51-10-021 AND 51-40-02.

Part: PANEL — CORRODED (BS 1386) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO DOOR THRESHOLD SIDE PANEL UNDERSIDE BS 1386 RBL 20. REMOVED CORRODED PANEL INSTALLED P/N 146N5391-24 IAW B757 SRM.

Part: FLOOR PANEL — CORRODED (BS 1200-1340) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

HEAVY CORROSION ON FLOOR PANEL BS 1200 TO 1340 IN AFT CARGO. REPAIRED BY FABRICATING AND INSTALLING FLOOR PANEL 129 BY 39.5 FROM 2024-T3 .071 IAW B757 SRM 51-10-02, PARA. 10A, 51-40-08 PARA 5C AND 51-20-01.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON UPPER SURFACE OF WEB BETWEEN FLOOR SUPPORTS AT BS 1520 TO BS 1540 RBL 7 RBL 11. REMOVED WEB. FABRICATED AND INSTALLED REPAIR INTERCOSTAL 20.0" BY 5.0" FROM 7075-T6 .032" IAW B757 SRM 51-40-02, 51-20-01 DELTA PS 900-4-01 NR 1.

Part: SUPPORT — CORRODED (BS 1470) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO BS 1470 RBL 16.10 CARGO SUPPORT STRINGER CORROSION AROUND NUT PLATE HOLE. REPAIRED BY REMOVING FLOOR SUPPORT BS 1445 TO BS 1555, FABRICATED AND INSTALLED NEW FLOOR SUPPORT 60" BY 3-1/2" FROM 7075-T6 .063" IAW B757 SRM 53-60-53, FIG 1, AND 51,10-01 PG 3-7, 21 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1400-1440) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON PNL UNDER CARGO FLOOR SUPPORT STRINGER IN AFT CARGO COMPT LOCATED AT BS 1400 TO BS 1440 RBL 16.1. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT PANEL 20" BY 5" FROM 7075-T6 .032" IAW 51-40-05 FIG 6, 51-20-01, DELTA PROCESS STANDARD 900-2 NR 5 AND 51-40-07 FIG 8.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON FRAME ATTACH CLIP AT BS 1540 LBL 9 AFT PIT. REMOVED CORRODED ATTACH CLIP. FABRICATED AND INSTALLED REPAIR CLIP 4.5" BY 2.0" FROM 7075-T6 .050" IAW B757 SRM 53-00-07, 51-20-01, 51-40-02 AND DELTA PS 900-4-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON LWR FLANGE OF FLOOR SUPPORT WEB AT BS 1620 LBL 3 IN AFT PIT. REMOVED CORRODED INTERCOSTAL WEB. FABRICATED AND INSTALLED REPAIR INTERCOSTAL WEB 20" BY 9" FROM 7075-T6 .040" IAW B757 SRM 51-30-01, 51-40-05, 51-20-01, 51-40-02.

Part: SUPPORT — CORRODED (THRESHOLD) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO DOOR THRESHOLD BOEING CASTING UNDER NUT PLATES BS 1438. REPAIRED BY REMOVING AND INSTALLING NEW SUPPORT P/N 65C80678-180 IAW B757 SRM 51-40-02, AND 51-40-04.

Part: WEB — CORRODED (BS 1420-1440) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AT BS 1420 TO BS 1440 SIDEWALL WEB RT. FABRICATED AND INSTALLED CUSP WEB 19.5" BY 9.5" FROM 7075-T6 .040" IAW B757 SRM 51-40-02, 53-60-13 AND 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AT BS 1380 TO BS 1400 STRINGER 17 WEB RT. REMOVED CORRODED CUSP WEB. FABRICATED AND INSTALLED REPLACEMENT WEB 19.5" BY 19.5" FROM 7075-T6 .040" IAW B757 SRM 51-40-02, 51-20-01 AND DELTA PS 900-2 NR 5.

Part: SUPPORT — CORRODED (THRESHOLD) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO DOOR THRESHOLD BOEING CASTING BS 1400. REPAIRED BY REMOVING AND INSTALLING NEW SUPPORT P/N 65C80678-180 IAW B757 SRM 51-40-02, AND 51-40-04.

Part: SUPPORT BRACKET — CORRODED (BS 984) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON SUPPORT BRACKET AT BS 984 JUST BELOW RT WING FWD EMERG ESCAPE DOOR. REPAIRED BY REMOVING BRACKET, FABRICATED AND INSTALLED REPAIR BRACKET 3" BY 2" FROM 7075-T6 .071" IAW B757 SRM 53-40-15, 51-40-02 AND 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AT BS 1400 AND BS 1420 RT CUSP WEB. REMOVED CUSP WEB. FABRICATED AND INSTALLED NEW WEB FROM 7075-T6 .040" 19.5" BY 9.5" IAW B757 SRM 51-40-05 FIG 3.6, 51-20-01 AND 51-40-02 AND DELTA PS 900-2 NR 5.

Part: FLOOR PANEL — CORRODED (BS 1330-1470) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

HEAVY CORROSION AFT CARGO FLOOR PANEL BS 1330 TO 1470. REMOVED CORRODED PANEL. FABRICATED AND INSTALLED PANEL 139.5" BY 40.0" FROM 2024-T3 .071" IAW B757 SRM 51-40-05, 51-40-08, 51-20-01.

Part: STRINGER CLIP — CORRODED (BS 1620 S30R) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION ON STRINGER CLIP AT BS 1620 STRINGER 30 IN AFT PIT. REPAIRED BY REMOVING CLIP, FABRICATED AND INSTALLED STRINGER CLIP 3" BY 5" AND END SPLICE 6.5" BY 3" FROM 7075-T6 .050" IAW B757 DRAWING 146N2821, 51-30-01 AND 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AFT CARGO LOCATED ON STRINGER 29R BS 1515. REMOVED CORRODED SECTION OF STRINGER. DRILLED AND INSTALLED EXTRUSION FROM BAC1498-204 7075-T62 CLAD IAW B757 SRM 53-00-03 FIG 201, 51-30-01 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION AT L-4 DOOR FWD FLOORBOARD SUPPORT BETWEEN BS 1640 AND BS 1680 B/L 54L I/B OF S-17L. REMOVED FLOOR SUPPORT, DRILLED AND INSTALLED NEW FLOOR SUPPORT P/N 146N5246U5 IAW B757 SRM 51-40-02, 51-40-05 AND 51-20-01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

CORROSION FOUND AT STRINGER 28R FROM BS 1500 TO BS 1520 IN AFT CARGO COMPARTMENT. REMOVED CORRODED SECTION OF STRINGER. FABRICATED AND INSTALLED SPLICE 7075-T62 CLAD 11" "Z" CHANNEL IAW B757 SRM 53-00-03 FIG 201, AND 51-40-02.

Part: SKIN — DENTED (BS 620-640) · airframe 47,715 hrs · 21,659 cycles

AIRCRAFT SKIN HAS DENT BETWEEN FRAME 620 TO 640, S-17-18 LT SIDE. CUT OUT DENTED AREA. HFEC CUT OUT IAW B757 SRM 51-20-02 AND NDT MANUAL. FABRICATED AND INSTALLED DOUBLER AND FILLER 5.00" ROUND FROM 2024-T3 .040" IAW B757 SRM 53-00-01 AND NDT MANUAL PT 6 51-00-19.

Part: SKIN — CORRODED (BS 1500-1520) · corrosion level 2 · airframe 47,715 hrs · 21,659 cycles

FOUND CORROSION RT AIRFONE ANTENNA MOUNT SURFACE FUSELAGE SKIN. CUT OUT CORRODED AREA 5/8" ROUND. FABRICATED AND INSTALLED REPAIR DOUBLER FROM 2024-T3 .063" AND FILLER 2024-T3 .040" IAW B757 SRM 51-20-1, 51-40-02.

Part: SPLICE — CORRODED (BS 1470) · corrosion level 2

FOUND CORRODED SPLICE IN AFT CARGO AT BS 1470. REPAIRED CORRODED SPLICE BY FABRICATING AND INSTALLING NEW SPLICE 1-3/4 BY 40 FROM BAC1505-100766 7075-T6 IAW B757 SRM 51-20-1, 51-40-02 AND DWG 453N1611.

Part: FLOOR PANEL — CORRODED (BS 700) · corrosion level 2

CORROSION FWD CARGO FLOOR SPLICE BS 700. FABRICATED AND INSTALLED NEW FLOOR PANEL 1-3/4" BY 39-3/4" FROM BAC 1505-100766 7075-T6 IAW B757 DWG 435N1611AND SRM 51-40-2.

Part: SPLICE — CORRODED (BS 1510) · corrosion level 2

FOUND CORROSION AFT CARGO FLOOR PANEL SPLICE AT BS 1510. REPAIRED CORRODED SPLICE BY FABRICATING AND INSTALLING NEW SPLICE 1-3/4 BY 40 FROM BAC1505-100766 7075-T6 IAW B757 SRM 51-20-1, 51-40-02 AND DWG 453N1611.

Part: SPLICE — CORRODED (BS 1330) · corrosion level 2

FOUND CORROSION AFT CARGO FLOOR PANEL SPLICE AT BS 1330. REPAIRED CORRODED SPLICE BY FABRICATING AND INSTALLING NEW SPLICE 1-3/4 BY 40 FROM BAC1505-100766 7075-T6 IAW B757 SRM 51-20-1, 51-40-02 AND DWG 453N1611.

Part: FLOOR PANEL — CORRODED (BS 700-780) · corrosion level 2

FOUND CORROSION FWD CARGO FLOOR PANEL RT BS 700 TO BS 780. REPAIRED CORRODED FLOOR PANEL BY FABRICATING AND INSTALLING NEW PANEL 94 BY 18 FROM 2024-T3 .032" IAW B757 SRM 51-20-1, 51-40-02, 53-00-01, AND 53-30-53.

Part: FLOOR PANEL — CORRODED (BS 700-780) · corrosion level 2

FOUND CORROSION AFT CARGO FLOOR PANEL LT BS 700 TO BS 780. REPAIRED CORRODED FLOOR PANEL BY FABRICATING AND INSTALLING NEW PANEL 94 BY 18 FROM 2024-T3 .032" IAW B757 SRM 51-20-1, 51-40-02, 53-00-01, AND 53-30-53.

Part: FLOOR PANEL — CORRODED (BS 650-700) · corrosion level 2

CORROSION FWD CARGO FLOOR PANEL BS 650 TO 700. FABRICATED AND INSTALLED NEW FLOOR PANEL 40" BY 47" FROM 2024-T3 .050" IAW B757 SRM 53-00-01 AND 51-40-2, 51-20-01.

Part: FLOOR PANEL — CORRODED (BS 720-760) · corrosion level 2

FOUND CORRODED AND CRACKED FLOOR FWD CARGO BS 720 TO BS 760 LT. FABRICATED AND INSTALLED NEW FLOOR PANEL 40" BY 47" FROM 2024-T3 .025 IAW B757 SRM 53-30-53, 53-00-01, 51-40-02 AND 51-20-01.

Part: FLOOR PANEL — CORRODED (BS 508-540) · corrosion level 2

FOUND CORRODED FWD CARGO FWD FLOOR PANEL AT BS 508 TO BS 540. REPAIRED CORRODED FWD CARGO FWD FLOOR PANEL AT BS 508 TO BS 540 BY FABRICATING AND INSTALLING NEW PANEL 39-3/4 BY 41-5/8 FROM 2024-T3 .071 IAW B757 SRM 51-40-02 AND 51-20-01.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 46,385 hrs · 21,132 cycles

RIGHT OIL QTY WENT TO ZERO RIGHT OIL TEMP RED LINE SMOKE IN COCKPIT. REPLACED NR 2 ENG PER TRANS 6T103.

Part: PANEL — FAULTY (COCKPIT) · airframe 44,830 hrs · 20,570 cycles

INFLIGHT SLIGHT ELECTRICAL BURNING ODOR DETECTED -NO SMOKE SEEN. ANTI COLLISION RED LT CB POPPED. TURNED RED ANTI COLLISION SWITCH OFF, ODOR WENT AWAY. FOUND BLACK BURN MARKS ON BACK OF LIGHT PANEL ON J2 CONNECTION ON BACKSHELL ON PANEL. REPLACED PANEL. CHECKS GOOD. NO FURTHER ODOR DETECTED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,309 hrs · 19,067 cycles

THE 4R FLASHLIGHT BATTERY NOT BLINKING. REPLACED BATTERY.

Part: BRACKET — DISLODGED (CABIN) · airframe 40,248 hrs · 19,043 cycles

AIR TURNBACK, A/C REPORTED SMOKE IN CABIN. SHUT DOWN RT PACK AND SMOKE AND SMELL DISSIPATED. MTC FOUND BRACKET DISLODGED FROM MAIN DISTRIBUTION DUCT ABOVE SEAT ROW 12. INSTALLED INTERN REPAIR PER ERA 095909-14.

Part: COVER — MISSING (EMERGENCY EXIT) · airframe 36,361 hrs · 17,572 cycles

AFT RT OVERWING EXIT SIGN COVER MISSING. REPLACED RT AFT OVERWING EXIT COVER.

Part: IRU — FAILED (E/E BAY) · airframe 33,017 hrs · 16,102 cycles

ON T/O FMC SCRATCH PAD-IRS NOTATION WITH BOTH YAW DAMPS AND FMC FAILURE MSGS. REPLACED CENTER IRU, ALIGMENT OK.

Part: RESERVOIR — DISCHARGED (R1 DOOR) · airframe 31,702 hrs · 15,463 cycles

R1 DOOR HAD PARTIAL SLIDE DEPLOYMENT/ INSPECTED SLIDE NOT ACTIVATED. REINSTALLED SLIDE BACK ON DOOR PER MM. FOUND EMERGENCY POWER RESERVOIR EMPTY. INSTALLED AND RIGGED NEW RESERVOIR PER MM.

Part: POWER UNIT — DISCHARGED (FLASHLIGHT) · airframe 30,163 hrs · 14,691 cycles

POWER UNIT, EMERGENCY FLASHLIGHT IS LOW BY R2 DOOR. REMOVED AND REPLACED POWER UNIT PER MM, CHECK OKAY.

Part: WIRE — DAMAGED (CABIN) · airframe 29,870 hrs · 14,559 cycles

ON L/O FOUND E+PATH LITE ON 2R FLIGHT ATTENDENT SEAT INOPERATIVE. FOUND WIREING TO BE DAMAGED UNDER SEAT. REPAIRED WIREING OPS CHECK NORMAL.

Part: OXYGEN BOTTLE — LOW (R2 DOOR) · airframe 29,110 hrs · 14,193 cycles

R2 DOOR PAX O2 BOTTLE LOW. REPLACED BOTTLE.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 28,970 hrs · 14,117 cycles

SMOKE BEHIND OVERHEAD FUEL BOOST PUMP PANEL IN COCKPIT. FOUND RT FWD BOOST PUMP SWITCH AT FAULT. REPLACE SAME.

Part: OVEN — SMOKE (GALLEY) · airframe 28,893 hrs · 14,077 cycles

STRONG ELEC SMOKE ODOR AND LIGHT SMOKE DETECTED FROM FIRST GALLEY OVEN AREA. REPLACED F/C OVEN.

Part: ENGINE — LEAKING (NR 1) · airframe 28,746 hrs · 14,013 cycles

FLT 1041 ATL-ONT AT 250 KTS AT APPROX FL 250 HAD LEFT ENG OIL PRESS EICAS MSG AND DISCRETE LIGHT. OIL QTY IND ZERO. PRESS CONTINUED TO DROP AND OIL TEMP IN RED WARNING AREA. S/D END PER POM PROCEDURE. WINDMILL TIME APPROX 10 MINUTES. CREW BELIEVES OIL PRESS IND 0 DURING WINDMILL BUT IS UNSURE. REMOVED FLT DATA RECORDER FOR READOUT CONFIRMATION OF PARAMETERS. CONTRACT MTC REPORTS ENG WET UNDER REVERSER HALVES. PENDING FLT DATA REPORTS LAX MTC WILL T/S.

Part: COFFEEMAKER — DIRTY (AFT GALLEY) · airframe 27,912 hrs · 13,597 cycles

BURNING ODOR COMING FROM R AFT GALLEY COFFEEMAKER. FOUND HEAVY COFFEE DEPOSITS ON HEATING PAN. CLEANED PAN AND ODOR WAS NO LONGER DETECTED DEACTIVATED UNIT AS A PRECAUTIONARY ACTION C/B COLLARDED. UNIT WAS NOT REPLACED, NOT IN STOCK AT THIS TIME.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 27,650 hrs · 13,479 cycles

NR 2 PYLON AFT CORNER PERMANENT REPAIR ACTL 3003-310854.

Part: CONNECTOR — FAILED (ROW 21)

SEAT ROW 21 SEAT MOUNTED EMERGENCY LIGHT INOP. REPLACED SEAT HARNESS FOR BROKEN CONNECTOR.

Part: BULB — FAILED (L4 DOOR)

ON LAYOVER, FOUND L4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND BULB BURNT. RELAMPED SAME AND OPERATIONAL CHECK NORMAL.

Part: BULB — FAILED (L2 DOOR)

ON LAYOVER, FOUND L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND LAMP BURNT. RELAMPED SAME AND OPERATIONAL CHECK NORMAL.

Part: SLIDE — DEPLOYED (R 1 DOOR)

R-1 DOOR SLIDE WAS NOT DEACTIVATED BY CREW PRIOR TO ARRIVAL AT GATE. R-1 DOOR SLIDE DID NOT DEPLOY PROPERLY WHEN DOOR WAS OPENED BY CABIN SERVICE. DOOR SLIDE DID NOT CLEAR DOOR SLIDE COVER, UPON DOOR OPENING. DOOR WAS HUNG ON DOOR SLIDE IN PARTIALLY OPENED POSTION. SLIDE AND DOOR ASSIST BOTTLE WAS CHANGED. WHEN DOOR SLIDE WAS REMOVED AT FLOOR ATTACH POINT THE DOOR OPENED FULLY.

Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)

IRR - ON LAYOVER, FOUND R1 EXTERIOR DOOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY M730. OPS GOOD.

Part: ENGINE — FAILED (NR 1)

ON CLIMBOUT, CVG HAD LT ENG COMPRESSOR STALLS FOLLOWED BY LOW OIL PRESSURE EICAS MSG ENG SHUTDOWN. MTC REPORTED EGT 691 FOR 37 SEC METAL IN TAIL PIPE. ENGINE WAS REPLACED AND ROUTED TO SHOP.

Part: STRAP — CRACKED (FS 380)

FOUND DURING LETTER CHECK E/E COMPT STRAP CRACKED FWD OF STA 380 RT SIDE OF NOSE GEAR WELL. REPAIRED PER SRM 53-10-51.

Part: CONNECTOR — FAILED (NR 2 ENGINE)

RIGHT ENGINE GENERATOR HAS HISTORY OF DROPPING OF LINE ON CLIMB-OUT AND CRUISE FOUND PLUG AND RECEPTABLE DAMAGED AND ARCED TOGETHER RIGHT ENG GENERATOR OFF LIT ILLUMINATED PIN B ON CONNECTOR WAS OPEN. CONNECTOR D01292J MFG PN FRF0-36-5P03-747 AND D1092P. REPLACED CONNECTOR AND REPAIRED DAMAGED WIRING OPERATION NORMAL.