N624AG

Part: NONE — NONE · airframe 81,859 hrs · 24,350 cycles

SHIP 6818 EXIT SIGN MISSING AT 2R DOOR. CORRECTIVE ACTION: RESECURED EXIT SIGN AT 2R DOOR. (8418252)

Part: NONE — NONE · airframe 81,674 hrs · 24,310 cycles

SHIP 6818 L4 EMERGENCY EXIT SIGN MISSING. CORRECTIVE ACTION: REPLACED L4 EMERGENCY EXIT SIGN PER ER/A 569132-14 REV. ORIG AND B757 AMM 33-51. ACCOMPLISHED SECTION II OF ER/A 569132-14 REV. ORIG ON L4 SIGN. OPS CHECK NORMAL. OK FOR SVC. (8418204)

Part: NONE — NONE · airframe 82,093 hrs · 24,404 cycles

SHIP 6818 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588337-14 REV A. CORRECTIVE ACTION: REF ERA 588337-14 REV A. (2003229)

Part: NONE — NONE · airframe 81,344 hrs · 24,242 cycles

SHIP 6818 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588305-14 REV A. CORRECTIVE ACTION: REF ERA 588305-14 REV A. (1997793)

Part: SIGN — DETACHED (CABIN) · airframe 80,989 hrs · 24,162 cycles

SHIP 6818 EXIT SIGN AT DOOR 2R HAS FALLEN OFF. CORRECTIVE ACTION: RESECURED EXIT SIGN COVER AT DOOR 2R PER B757 AMM 33-50. (7914062)

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 80,858 hrs · 24,132 cycles

SHIP 6818 EXIT SIGN ABOVE THE 2R DOOR COMPLETELY FELL OFF. CORRECTIVE ACTION: SECURED EXIT SIGN. (7914027)

Part: DOOR — UNKNOWN (L2) · airframe 80,704 hrs · 24,101 cycles

SHIP 6818 2L DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED DOOR & CHKS NML. (7986668)

Part: PLATE — LOOSE (DOOR HANDLE) · airframe 80,356 hrs · 24,025 cycles

SHIP 6818 DOOR HANDLE PLATE LOOSEN- LOCATION 601. CORRECTIVE ACTION: SECURED DOOR HANDLE PLATE. CHKD OK. (7840454)

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 80,250 hrs · 24,003 cycles

SHIP 6818 EMERGENCY EXIT SIGN 2R FELL OFF. CORRECTIVE ACTION: SECURED EMERGENCY EXIT SIGN/COVER AT 2R NO DEFECTS NOTED. (7840414)

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 80,048 hrs · 23,961 cycles

SHIP 6818 604 SLIDE WARNING LEVER 1L "KNUCKLEKNOCKER" DOESN'T EXTEND. CORRECTIVE ACTION: CYCLED 1L DOOR PER B757 AMM 52-11. OPS CHECK GOOD. (7345950)

Part: DISPLAY — ODOR (RT COCKPIT) · airframe 79,983 hrs · 23,948 cycles

SHIP 6818 -ATB- ELECTRICAL FUMES IN COCKPIT AFTER T/O. FOLLOWED QRH AND RETURNED TO KEF. CORRECTIVE ACTION: REPLACED R/H MCDU PER B757 AMM 34-61. RESEATED PUSHED BACK PIN IN CONNECTOR D01489 PER B757 AWPM 20-10. INSTALLED NEW RECIRCULATION FILTERS PER B757 AMM 21-25 AND ERA591924-14 REV ORIG. ELECTRICAL HARNESSES AND CONNECTORS WERE INSPECTED AND NO ARCING OR DAMAGE FOUND. HIGH POWER RUN PERFORMED AND PACKS RUN WITH NO SMOKE SMELL.

Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 79,714 hrs · 23,879 cycles

SHIP 6818 AFTER PUSH ,CREW AND GATE AGENTS STATE THAT LT GUST LOCK NOT WORKING PROPERLY. CORRECTIVE ACTION: CLEANED AND LUBRICATED GUST LOCK . FOUND LOCK TO BE OPERATING PROPERLY. REF B757 AM 12-21. (7480388)

Part: GIRT BAR — BROKEN · airframe 78,551 hrs · 23,599 cycles

GIRT BAR FELL OFF MAINTENANCE FOUND BAR MECHANISM BROKEN. CORRECTIVE ACTION: REPLACED LIFTER ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: DUCT — DETACHED (PNEUMATIC SYS) · airframe 78,426 hrs · 23,573 cycles

THE CREW DIVERTED THE FLIGHT TO SLC TO AFTER RECEIVING A "RT BLEED DUCT LEAK" MESSAGE AND, PER THE QRH, UNABLE TO CONTINUE INTO ICING CONDITIONS. ISOLATED THE NR 2 ENGINE BLEED AIR PRESSURE AND THE MESSAGE SOON EXTINGUISHED. CORRECTIVE ACTION: MAINTENANCE FOUND THE ANTI-ICE DUCT ABOVE RT PYLON DETACHED WITH CLAMP DETERIORATED & SEAL MISSING. CLAMP WAS REPLACED AND THE LEAK CHECK WAS GOOD.

Part: COVER — MISSING (EXIT SIGN) · airframe 78,286 hrs · 23,535 cycles

L2 DOOR EXIT SIGN COVER MISSING ABOVE ENTRY DOOR. CORRECTIVE ACTION: REPLACED NEW EXIT SIGN COVER. SYSTEM OPERATION IS NORMAL.

Part: DRAG BRACE — DAMAGED (LT ENGINE) · airframe 78,000 hrs · 23,471 cycles

DURING INSPECTION FOUND CRACKED PAINT AROUND THE FASTENER HEAD NR 4 AND 8, LT ENGINE DRAG FITING CLAMP-UP & DIAGONAL BRACE DRAG FITTINGS. DRAG FITTINGS WERE REPLACED, PER ER/A 588337-14.

Part: DRAG BRACE — CORRODED (RT ENGINE) · corrosion level 2 · airframe 78,000 hrs · 23,471 cycles

WHILE PERFORMING RIGHT ENGINE DRAG FITTINGS CLAMP-UP AND DIAGONAL BRACE INSPECTIONS CORROSION WAS FOUND ON HOLES 2, 3, 4, 5, 7, 8, 9, 10, 12, 13, 14, 15, 16 & 18, COMMON TO THE RIGHT WING UPPER SKIN AND FORWARD DRAG FITTING. DRAG FITTINGS REPLACED, PER 588305-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,997 hrs · 23,470 cycles

FORWARD EMERGENCY LIGHTS NOT ILLUMINATING. CORRECTIVE ACTION: REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL

Part: HOUSING — BROKEN (EXIT LIGHT) · airframe 77,942 hrs · 23,458 cycles

SHIP 6818 ROW 44 EE PLS LIGHT HOUSING BROKEN. CORRECTIVE ACTION: REPLACED ROW 44 EEPLS LIGHT HOUSING. (6516466)

Part: GIRT BAR — DIRTY (AFT RT DOOR) · airframe 77,541 hrs · 23,379 cycles

(AIRCRAFT 6818, L/P 6528325) AFT RIGHT DOOR ARMING LEVER WILL NOT MOVE ALL THE WAY TO DISARM POSITION. CORRECTIVE ACTION: FOUND DEBRIS IN GIRT BAR. RMVD DEBRIS. DOOR OPERATES. REF B757 AMM 52-11.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 77,201 hrs · 23,305 cycles

SEAT 35D MISSING EMERGENCY WHITE LENS COVER. REPLACED LENS REF AIPC 33-51-11.

Part: ACTUATOR — INOPERATIVE (RUDDER TRIM) · airframe 75,857 hrs · 23,049 cycles

-ATB- DUE TO RUDDER TRIM BEING INOPERATIVE. REPLACED RUDDER TRIM ACTUATOR PER AMM.

Part: COOLING FAN — FAULTY (E&E BAY) · airframe 74,215 hrs · 22,745 cycles

SHIP 6818 EQUIPMENT COOLING MSG WITH VISIBLE SMOKE. CORRECTIVE ACTION: SMOKE/HAZE AND ODOR IN COCKPIT AND CABIN. EQUIP COOLING OVERHEAT ILLUMINATED. ENGINES OFF. PACKS ON APU. 2 HOURS ON GROUND ON TAXIWAY PRIOR TO EVENT. CLEARED IN 10 MIN. QRH COMPLETED. AFTER NOTED NO HEAT. T/S PER FIM 21-00-01. FOUND FWD EQUIP COOLING FAN AT FAULT. R/R AS PER AMM 21-58. PERFORMED NO-GO ODI PREVENTION STEPS 21-72 STEP 5. MCC CONF CALL C/W ALL CHKS GOOD. (1048027)

Part: DOOR — OUT OF TRIM (CABIN) · airframe 73,536 hrs · 22,616 cycles

SHIP 6818 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:603. CORRECTIVE ACTION: ADJUSTED DOOR TRIM OPS CK OK PER AMM 52-11. (0965587)

Part: INDICATOR — OBSTRUCTED (DOR) · airframe 72,946 hrs · 22,500 cycles

SHIP 6818 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:603 CORRECTIVE ACTION: CLEANED DEBRIS. OPS NML. (0900365)

Part: INDICATOR — INOPERATIVE (L2 DOOR) · airframe 71,866 hrs · 22,289 cycles

DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS: 2L / ACARS TEXT: FRC5212072L / INTERIOR. PERFORMED OPS CK OF 2L DOOR KNOCKER PER AMM 52-11. OPS CK GOOD. OK FOR SVC.

Part: INDICATOR — INOPERATIVE (DOOR ARMED) · airframe 71,616 hrs · 22,241 cycles

(AIRCRAFT 6818, L/P 0759402) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:603 / ACARS TEXT: FRC521207603 / INTERIOR.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 71,357 hrs · 22,194 cycles

1R DOOR WILL NOT ARM. DEBRIS REMOVED. OK FOR SVC.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 70,947 hrs · 22,121 cycles

L2 DOOR WILL NOT DISARM. FOUND DEBRIS IN THE GIRT BAR MECHANISM, CLEARED DEBRIS, DOOR OPS CHECKED OK IAW AMM 52-11.

Part: PROXIMITY SWITCH — DEFECTIVE (L2 DOOR) · airframe 70,772 hrs · 22,088 cycles

DOOR 2L SLIDE LIGHT STAYS ON ALTHOUGH DOOR IS DISARMED & OPEN. REMOVED AND REPLACED AFT POS GIRT BAR PROX SWITCH AT DOOR 2L PER AMM 25-66 AND SWDM 20-30.

Part: RESERVOIR — LOW PRESSURE (R2 DOOR) · airframe 70,658 hrs · 22,067 cycles

DUE SVC FOUND R2 DOOR EMERGENCY POWER RESERVOIR 0 PSI. REMOVED AND REPLACED R2 DOOR EMERGENCY POWER RESERVOIR PER AMM 52-11 OPS CK OK FOR SVC VERIFIED SAFETY PINS REMOVED RII.

Part: HEAT EXCHANGER — NOT REPORTED (AC BAY) · airframe 70,643 hrs · 22,064 cycles

DIV-SLC DUE TO CABIN PRESSURIZATION ISSUES. CREW HEARD THUMP AND THEN CABIN STARTED CLIMBING. FOUND CLAMP BLOWN OFF RT PACK AT CONDENSER. REPLACED LEFT PACK HEAT EXCHANGER.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 70,224 hrs · 21,983 cycles

ON LANDING, THE L2 DOOR OVERHEAD EXIT SIGN FELL OFF. INSTALLED THE SIGN IAW AMM 33-51. NO FURTHER DEFECT NOTED. ACFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DURING OTHER MAINTENANCE IN THIS AREA, THE SHEAR TIE AT STA 1360 BETWEEN STRINGER 28R AND 27R HAS SIGNS OF CORROSION. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02 ITEM 4 AND DWG 146N1009 REV D.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT LT "Z" ANGLE FROM STA 1540+10 TO THE BULKHEAD HAS AREAS OF CORROSION. REMOVED AND REPLACED LT Z-ANGLE AT STA 1530-1640 IAW SRM 51-40-02 AND DRAWING 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER STA 1468 TO 1471 RBL 3 HAS CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED FLOOR SUPPORT STRINGER FROM AFT CARGO COMPARTMENT STA 1440-1500, RBL 3 IAW SRM 51-40-02 PG 4, SRM 53-00-53 FIG 101 AND DWG 146N5390 REV C. INSTALLED NUTPLATES IAW B757-200 SRM 51-40-02 STEP 5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER STA 1468 TO 1471 RBL 7 HAS CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED FLOOR SUPPORT STRINGER FROM AFT CARGO COMPARTMENT STA 1440-1500, RBL 7 IAW SRM 51-40-02, PG 4 B757-200 SRM 53-00-532 FIG 101 AND DWG 146N5390 REV C. INSTALLED NUTPLATES IAW SRM 51-40-02 STEP 5.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DURING OTHER MAINTENANCE IN THIS AREA THE SHEAR TIE AT STA 1380 BETWEEN STRINGER 30R AND 29R HAS SIGNS OF CORROSION AROUND A FASTENER. REMOVED AND REPLACED SHEAR TIE IAW SRM. 51-40-02 ITEM 4 AND DWG 146N1010 REV C.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER STA 1468 TO 1471 RBL 3 HAS CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED WEB IAW SRM 51-40-02 DWG 146N8522 REV D.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, FUSELAGE FRAME STA 1400 BETWEEN STR 28L-29L, SHEAR TIE IS CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02 STEP 4 AND DWG 146N1011 REV E.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, FUSELAGE FRAME STA 1400 BETWEEN STR 29L-30L, SHEAR TIE IS CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02 AND DWG 146N1011 REV E.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, FUSELAGE FRAME STA 1400 BETWEEN STR 29R-30R, SHEAR TIE IS CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02 AND DWG 146N1011 REV E.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT STA 1401 RBL 3 FLOOR SUPPORT STRINGER HAS CORROSION AS MARKED AT THE FASTENER HOLE. REMOVED AND REPLACED FLOOR SUPPORT STRINGER IAW SRM 51-40-02 AND DRAWING 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT STRINGER AT STA 1500 RBL 11 LOWER SIDE AT NUTPLATE HAS CORROSION. REMOVED AND REPLACED FLOOR STRINGER IAW SRM 51-40-02 AND DWG 146N5390 REV C.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 153AF LOWER SURFACE HAS AREAS CORROSION. FABRICATED NEW FLOORBOARD PER AMM 25-50-04-404-004. TREATED WITH ALODINE AND PRIME PER SRM 51-20-01 AND CIC PER PS-900-2 NO 09.

Part: ANGLE — CORRODED (BS 1520) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

THE AFT CARGO BAY RT ZEE ANGLE FROM BS 1520+10 TO THE AFT BULKHEAD HAS AREAS OF CORROSION. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 146N5390, REV B.

Part: SPLICE — CORRODED (BS 1530) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

THE AFT CARGO BAY, RT FLOOR SIDE PLATE SPLICE WAS CORRODED BS 1530. REMOVED AND REPLACED THE SPLICE IAW SRM 51-40-02, AND DWG 146N5390, REV C.

Part: PLATE — CORRODED (BS 1310-1380) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY RT ZEE ANGLE SIDEPLATE AT BS 1310 TO 1380 HAD CORROSION ALONG THE SIDEWALL MOUNT AREAS. REMOVED AND REPLACED THE SIDE PLATE IAW SRM 51-40-02, AND 146N5390, REV A.

Part: WEB — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO, BS 1400 - 1420 WEB, RBL 3 WAS CORRODED. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 146N5399, REV B.

Part: ANGLE — CORRODED (BS 1440-1520) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, RT ZEE ANGLE, BS 1440 - 1520 HAD MULTIPLE AREAS CORROSION. REMOVED AND REPLACED THE ZEE ANGLE IAW SRM 51-40-02, AND DWG 146N5390, REV C.

Part: FRAME — CORRODED (1460) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY FRAME, BS 1460, RBL 1 TO RBL 5 HAD CORROSION ON THE FWD SIDE. REPAIRED THE FRAME IAW ERA 564989-14, REV 0, AND ERA 564989-14 , REV ORIGINAL.

Part: ANGLE — CORRODED (BS 1310-1430) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LEFT ZEE ANGLE, SIDEPLATE BS 1310 TO 1430 HAD CORROSION ALONG THE SIDEWALL MOUNT AREA. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02.

Part: SHEAR TIE — GOUGED (BS 1680) · airframe 70,192 hrs · 21,975 cycles

AFT CARGO FRAME, BS 1680, STRINGER 26L, LOWER SHEAR TIE ATTACH WEB HAD A DEEP GOUGE. REPAIRED THE SHEAR TIE IAW ERA 564982-14, REV 0, AND ERA 564982-14, REV ORIGINAL.

Part: WEB — NOT REPORTED (NOT REPORTED) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, WEB. REMOVED, FABRICATED, AND INSTALLED A NEW WEB IAW SRM 51-40-02, SRM 51-10-02, SRM 53-00-53, SRM 51-40-05, AND DRAW3ING 146N5401, REV. A.

Part: WEB — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO, BS 1400 TO 1420, LBL 3 WEB CORRODED. REPLACED THE WEB IAW SRM 51-40-02-06, AND DWG 146N5399, REV B.

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 70,192 hrs · 21,975 cycles

NR 2 ENGINE INBD T/R UPPER AFT COKE BOTTLE AREA (TRAILING EDGE CORNER) HAS A 1" LONG CRACK AS MARKED. INSTALLED REPAIR ON NR 2 ENG I/B T/R UPPER AFT AREA AS REQ'D. REF: CMM 71-11-75 (REPAIR 411782) AND ERA 564990-14 REV ORIG AND PRI ER/A 564990-14 REV 0.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMP RT FLOOR TIE DOWN CORRODED STA 1460 (FOUND AFTER SIDE PLATE REMOVAL). REMOVED AND REPLACED AFT CARGO COMPARTMENT RT FLOOR TIE DOWN AT STA 1460 IAW SRM 51-40-02 AND DWG 146N1014 REV D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER STA 1468 TO 1471 LBL 7 HAS CORROSION ON THE UPPER AND LOWER SURFACES. CORROSION TASK NR REMOVED AND REPLACED FLOOR STRINGER BETWEEN STA 1450-1500 LBL 7 IAW SRM 51-40-02 AND DWG 146N5390 REV D.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

STA 1360-1380 STR 26-27 L, INTERCOSTAL UPPER ATTACH ANGLE CORRODED. RECEIVED AND VERIFIED MATERIAL AS P/N BAC1490-2828-7075-T6. IAW DWG 146N5410 REV A AND 146N5448 REV A. TREATED IAW AMM 51-21-04-110-801, INSTALLED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT STA 1420 TO STA 1440 BL 0 FLOOR SUPPORT WEB IS CRACKED. REMOVED AND REPLACED FLOOR SUPPORT WEB AT STA 1420 TO STA 1440 BL O (AFT CARGO CEILING AREA) IAW SRM 51-40-02 AND DRAWING 140N2505.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT AT STA 1300 BETWEEN STR 23R AND STR 27R SLANT PANEL SUPPORT HAS CORROSION. REMOVED AND INSTALLED NEW SLANT PNL SUPPORT ANGLE IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02; APPLIED CIC IAW P/S 800-2 NR 09.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY FLOOR STRUCTURE STA 1400-1420 LBL 16, INTERCOSTAL WEB IS CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL WEB IN AFT CARGO STA 1400 TO 1420 LBL 16" IAW SRM 51-40-02, SRM 53-00-04, AMM 5-24-09-377 -001 AND DWG 146N5400 REV 'B'.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER STA 1468 TO 1471 HAS CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED FLOOR STRINGER IAW SRM 51-40-02 AND DWG 146N5447 REV A.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT STA 1401 RBL 3 INTERCOSTAL TO FRAME ATTACH CLIP HAS CORROSION. REMOVED, "OUT OF LIMITS" CLIP (100% LOSS) AND INSTALLED NEW CLIP IAW BAC DWG 146N5426 REV A AND SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LT Z-ANGLE/SIDE PLATE STA 1469 TO 1509 HAS CORROSION ALONG SIDEWALL MOUNT AREAS. REMOVED AND REPLACED "Z" ANGLE AT STA 1530 TO 1410 IAW SRM 51-40-02 AND DWG 146N5390 REV B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT GALLEY FLOOR STA 1680 RBL11-52 FLOORBEAM UPPER FLANGE HAS CORROSION AROUND FASTENER HOLES, MARKED. COMPLIED WITH PRI ER/A 564981-14 REV 0 DETAIL C AND ER/A 564981-14 REV ORIGINAL.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT GALLEY SHEAR DECK HAS CORROSION STA 1715-1719 RBL4-44. REPAIRED IAW SRM53-60-51-R17, PG 203 AND PRI ER/A 564981-14 REV A AND ER/A 564981-14 REV ORIGINAL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMP STR 26L STA 1660+12" HAS CORROSION. REPAIRED IAW SRM 53-00-53 REPAIR 1.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · airframe 70,192 hrs · 21,975 cycles

AFT GALLEY SHEAR DECK HAS CORROSION STA 1682-1715 RBL50-53, MARKED. REPAIRED SHEAR DECK IAW PRI ER/A 564981-14 REV 0 AND ER/A 564981-14 REV ORIGINAL PER PER SRM 53-60-50 REPAIR 11.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LOWER FUSELAGE STA 1202-1210 LBL 5-RBL 5, AREA UNDER LAV SERVICE (DUMP) FITTING HAS CORROSION ON OUTER SURFACE AND INNER FLANGE CONTACT AREA, MARKED. REMOVED AND REPLACED MOUNT RINGS IAW SRM 51-40-02 AND DWG 417N8301 REV A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT STA 1400 LBL 12 TO RBL 6 FRAME HAS CORROSION AS MARKED. REMOVED AND INSTALLED NEW FRAME AS PER BAC DWG 146N1011 REV E AND SRM 51-40-02 STEP 4B.

Part: BRACKET — CORRODED · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

ON DISASSEMBLY OF THE INTERCOSTAL, FOUND A BRACKET CORRODED. FABRICATED, LOCATED, DRILLED, AND RESTORED FINISH IAW SRM 51-40-05, DWG 146N5426, REV A. AMM 51-21-04-107-017, AND AMM 51-21-14-370-801.

Part: SHEAR TIE — CORRODED (BS 1400) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, FUSELAGE FRAME SHEAR TIE BS 1400, BETWEEN STRINGERS 27L - 28L, CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 146N1011, REV E, AND SRM 51-40-02, STEP 4B.

Part: CARGO TRACK — CORRODED (BS 1440) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, CARGO TRACK CORRODED BS 1440 RIGHT, INSTALLED A NEW CARGO TRACK IAW SRM 51-40-02, SRM 51-40-05, AND DWG 146N5420, REV B.

Part: FLOOR SUPPORT — CORRODED (BS 1325-1332) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY FLOOR SUPPORT BS 1325 TO 1332, RBL 11 HAD CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: WEB — CORRODED (BS 1480-1500) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY RT FLOOR WEB CORRODED BS 1480 - 1500, STRINGER 27R. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02, ITEM 4, AND DWG 146N5427, REV A.

Part: FLOORBEAM — CORRODED (BS 1688) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT GALLEY FLOORBEAM UPPER FWD FLANGE HAS CORROSION AROUND THE FASTENER HOLES BS 1688, LBL 2 - 54. REPAIRED IAW E/RA 564983-14, REV ORIGINAL, & PRI 564983-14, REV 0.

Part: FLOOR SUPPORT — CORRODED (BS 1280-1300) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, BS 1280 TO 1300, LBL 18 FLOOR SUPPORT HAD CORROSION ON THE UPPER ANGLE IAW B757-200 51-40-02. LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-05, SRM 51-20-01, SRM 51-20-01, SRM 51-40-02, AND SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 1280-1300) · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, BETWEEN BS 1280 AND 1300, STRINGER 27L INTERCOSTAL FOUND CRACKED. DRILLED, DEBURRED, AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-05, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1327-1332) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY FLOOR SUPPORT, BS 1327 TO 1332, RBL 7 HAD CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LEFT INBD MAIN FLAP LOWER SKIN HAS SURFACE CORROSION AT THE T/E WEDGE. REPAIRED IAW ER/A 568218-14, REV ORIG.

Part: FLOOR SUPPORT — CORRODED (BS 1321-1341) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY FLOOR SUPPORT, BS 1321 TO 1341, LBL 2 CORRODED ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1460) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY SHEAR TIE, BS 1460, RBL 1 TO RBL 5 CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 146N1014 REV D.

Part: FLOORBEAM — CORRODED (BS 1343) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO FLOORBEAM SPLICE AT BS 1343, RBL 11 HAS CORROSION ON LOWER LIP. INSTALLED A NEW SPLICE IAW SRM 51-40-02.

Part: SPLICE — CORRODED (BS 1310) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, RIGHT SPLICE PLATE AT BS 1310 WAS CORRODED. REMOVED AND REPLACED THE SPLICE PLATE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1500) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, RT FLOOR SUPPORT ATTACH ANGLE CORRODED BS 1500, RBL 16. FABRICATED A NEW FLOOR SUPPORT ANGLE IAW SRM 51-40-05, & DWG 146N1016, REV E. INSTALLED A NEW FLOOR SUPPORT ANGLE IAW SRM 51-40-05, 51-40-02, AND DWG 146N1016, REV E.

Part: ANGLE — CRACKED (BS 1320) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, BS 1320, STRINGER 29R, FOUND THE WED ANGLE CRACKED. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW SRM 51-40-02, DWG 146N5426, REV A, SRM 51-20-01, AND SRM 51-40-05.

Part: WEB — CORRODED (BS 1320-1340) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY BETWEEN BS 1320 AND 1340, STRINGER 29R WEB CORRODED. INSTALLED A NEW WEB IAW SRM 51-40-02, & DRAWING 146N5398, REV B.

Part: SPLICE — CORRODED (BS 968) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LOWER FUSELAGE LBL 6, AREA BS 968 DOOR SUPPORT STRUCTURE FOR THE LT PACK BAY DOOR, SPLICE FITTING IS CORRODED ON TOP AND SIDE SURFACES. EVALUATED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-12, DETAIL II. REPLACED THE SPLICE FITTING IAW SRM 51-40-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LEAD REQUESTED FOM LOWER BODY FAIRING SUPPORT STRUCTURE STA 12-1240 RBL 5.5 HAS CORROSION ON UPPER AND LOWER SURFACE AROUND NUTPLATES AND FASTENER HOLES. REMOVED AND REPLACED -6 FAIRING SUPPORT IAW SRM 51-40-02, PARA 4(D) & 7(D) AND DWG 149N7701 REV G.

Part: FLOOR SUPPORT — CORRODED (BS 1468-1471) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY FLOOR SUPPORT BS 1468 TO 1471, LBL 11 HAS CORRODED ON THE UPPER AND LOWER SURFACES. CORROSION REMOVED, FOUND TO BE ON REPAIR ANGLE NO LIMITS FOUND. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LOWER FAIRING SUPPORT FOR AFT LAV ACCESS DOOR STA 1210 HAS AREAS OF CORROSION BY THE FASTENER HOLES. REMOVAL AND INSTALLATION COMPLETED ON N/R 37361-1000-0001.

Part: CHANNEL — CORRODED (BS 1200-1240) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LOWER BODY FAIRING SUPPORT STRUCTURE BS 1200 - 1240 LBL 5.5 HAS CORROSION ON THE UPPER AND LOWER SURFACE AROUND NUTPLATES AND FASTENER HOLES. REMOVED AND REPLACED THE LWR FAIRING SUPPORT CHANNEL IAW SRM 51-40-02, PARA 4 & 7, AND DWG 149N7701, REV G.

Part: SPLICE STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY STA 1400 BETWEEN STR 29R-27L, SKIN SPLICE STRAP IS CORRODED. REMOVED AND REPLACED SPLICE STRAP IAW SRM 51-40-02 AND DWG 146N3300 REV H.

Part: FUEL TANK — CORRODED (BS 1000) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

PASSENGER CABIN BS 1000, LBL 60 - LBL 63, FUEL TANK UPPER SKIN HAS CORROSION BELOW STUB BEAM. REMOVED CORROSION IAW SRM 51-10-02. COMPLIED WITH ER/A 564980-14, REV 0, AND ER/A 564980-14, REV ORIGINAL.

Part: ANGLE — CORRODED (BS 1679) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

L4 DOOR LOWER SILL UPPER SURFACE, ANGLE HAD CORROSION ON UPPER SURFACE, BS 1679. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, STEP 4B, AND DWG 146N8712, REV K.

Part: SHEAR TIE — CORRODED (BS 1220) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, BS 1220, BETWEEN STRINGERS 28R AND 29R UNDER THE SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE.

Part: CHANNEL — CORRODED (R4 DOOR SILL) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

R4 DOOR LOWER SILL, UPPER SURFACE, FWD CHANNEL CORRODED, BS 1679. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-40-02, AND DWG 146N8712, REV K.

Part: FUEL TANK — CORRODED (BS 1000) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

BS 1000, RBL 60 - RBL 64, FUEL TANK UPPER SKIN HAS CORROSION BELOW STUB BEAM. REMOVED THE CORROSION IAW SRM 51-10-02. COMPLIED WITH ER/A 564980-14, REV 0, AND ER/A 564980-14, REV ORIGINAL.

Part: CREASE BEAM — CORRODED (BS 1180-1182) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

CREASE BEAM INNER STRUCTURE CORRODED, BS 1180 - 1182, RBL 64. REMOVED AND REPLACED THE CREASE BEAM ANGLE IAW SRM 51-40-02, AND DRAWING 1465590.

Part: SHEAR TIE — CORRODED (BS 1220) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, BS 1220, BETWEEN STRINGERS 28R AND 29R UNDER THE SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE.

Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CABIN FLOORBEAM, BS 1660, LBL 55 - 57 CORRODED ON THE UPPER SURFACE. INSTALLED A NEW SECTION, BETWEEN LBL 40 TO 65 IAW SRM 53-00-51, REPAIR 8.

Part: SKIN — DENTED (FUSELAGE) · airframe 70,192 hrs · 21,975 cycles

LT SIDE OF AFT FUSELAGE HAS PROTRUDING DENT APPROXIMATELY STA 1629 BETWEEN STRINGERS 24L AND 25L. REMOVED DENT AND REPAIRED IAW SRM 53-00-01 REPAIR 3. ADDITIONAL INSPECTIONS REQUIRED.

Part: WEB — CORRODED (BS 1440-1460) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO BAY, RT FLOOR WEB WAS CORRODED, BS 1440 - 1460, STRINGER 27R. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02, AND DWG 146N8222, REV E.

Part: STRIP — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT CARGO COMPARTMENT SPLICE STRIP ATTACHED TO FWD EDGE FLOOR PANEL 161AF HAS CORROSION. LOCATED AND DRILLED. TREATED AND PRIMED NEW SPLICE STRIP IAW SRM 51-40-05 AND AMM 51-21-04 370-801 AND DWG 453N1611 REV B.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4R LOWER SILL UPPER SURFACE, FWD "I" CHANNEL HAS CORROSION ON UPPER AND LOWER SURFACE STA 1645 RBL60-66, MARKED. REMOVED AND REPLACED BRACKET ASSY IAW SRM 51-40-02 AND DWG 146N8722 REV B.

Part: ANGLE — NOT REPORTED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

LOWER FUSELAGE FWD OF LT A/C BAY DOOR FWD HINGE, REPLACED NEW T-ANGLE IAW SRM 51-40-02-0G, STEP 7.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 70,192 hrs · 21,975 cycles

NR 2 ENGINE PYLON OUTBD SIDE UNDER ACCESS PNL 445AR FWD LOWER CORNER OF CUTOUT STRUCTURE, 1 EA ANGLE BRACKET IS CRACKED 2 EA AREAS AS MARKED. REMOVED CRACKED -17 CLIP AND INSTALLED NEW -17 CLIP IAW BAC DWG 313N3052 REV B AND SRM 51-40-02 STEP 7.

Part: FITTING — MISSING (R2 DOOR) · airframe 70,192 hrs · 21,975 cycles

R2 DOOR UPPER TRIGGER ADJUSTMENT SCREW MISSING SAFETY CLIP. PERFORMED CABLE TRAVEL CHECK AT THE EMERGENCY POWER SPRING CYLINDER IAW AMM 52-11-32-404-010 STEP E{16} CHECKS GOOD. SAFETIED R2 DOOR TRIGGER ADJUSTMENT STUD WITH SPRING CLIP IAW AMM 52-11-32-404-010 STEP E{16) (H).

Part: CREASE BEAM — CORRODED (BS 1005-1020) · corrosion level 2 · airframe 77,474 hrs · 23,365 cycles

(AIRCRAFT 6818, L/P 0540553) PASSENGER CABIN FLOOR CENTER WING SECTION, STA 1005-1020 RBL64 CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION AROUND FASTENER HOLES, MARKED. REPAIRED PASSENGER CABIN FLOOR SUPPORT CENTER WING SECTION STA 1005-1020 RBL 64 CREASE BEAM INNER CHORD I/A/W B757-200 SRM.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT PASSENGER CABIN, STA1315 LBL 24.5 & 45.5, LT LAV AFT TIE-DOWNS (2 EACH) HAVE CORROSION ON UPPER SURFACE, MARKED. REMOVED AND REPLACED 2EA AFT LAV TIE DOWN FITTINGS @ CABIN STA 1315 LBL 24.5 AND 45.5 IAW SRM 51-40-02 , PARA 2D AND DRWG 146N5270, REV .B . NO PUBLISHED LIMITS FOR LAV TIE DOWN FITTINGS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,192 hrs · 21,975 cycles

AFT PASSENGER CABIN FLOOR SUPPORT STA 1300-1320 HAS CORROSION ON UPPER AFT SURFACE, MARKED. REMOVED AND REPLACED CABIN FLOOR SUPPORT @ STA 1300-1320 LBL 24.5 IAW SRM 51-40-02 PARA,4B ORIGINAL MATERIAL THICKNESS .071 EVALUATED @ 100% MATERIAL LOSS.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

FWD CARGO COMPARTMENT FLOOR, STA 696-765 RBL19-26 OUTBOARD ZEE-ANGLE HAS SEVERAL AREAS CORROSION ON UPPER AND LOWER SURFACES AROUND FASTENER HOLES. BLENDED CORROSION ON SIDE PLATE AT BS 695 TO 720 RBL 19 TO 26. REMOVED AND REPLACED SIDE PLATE FROM BS 650 TO 765 IAW DRAWING 143N5320 REV E, SRM 53-00-53, AMM 53-88-01-801.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4L LOWER SURFACE, FWD "C" CHANNEL HAS CORROSION, STA 1645, MARKED. REMOVED AND REPLACED "C" CHANNEL IAW SRM 51-40-02 AND BAC DWG 146N8722 REV N.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4L LOWER SILL UPPER SURFACE, HAT CHANNEL HAS CORROSION ON LOWER SURFACE, STA 1668. MARKED. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-40-02 AND BAC DWG146N8722 REV. N.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4L SILL UPPER SURFACE, HAT CHANNEL HAS CORROSION ON LOWER SURFACE, STA 1664, MARKED. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-40-02 AND BAC DWG146N8722 REV N.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4L LOWER SILL UPPER SURFACE, FWD "I" CHANNEL HAS CORROSION ON LOWER SURFACE, STA 1660, MARKED. REMOVED AND REPLACED "I" CHANNEL IAW SRM 51-40-02 AND BAC DWG 146N8722 REV N.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

PASSENGER CABIN STA 1020- STA 1040, LBL 64, CREASE BEAM INNER CHORD HAS CORROSION AROUND NUTPLATE. REPAIRED CREASE BEAM INNER CHORD IAW SRM 53-00-13 REPAIR 2.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4L LOWER SILL UPPER SURFACE, HAT CHANNEL HAS CORROSION ON UPPER SURFACE, STA 1657, MARKED. REMOVED AND REPLACED STIFFENER IAW DWG 146N8722 REV B AND SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4R LOWER SILL UPPER SURFACE, HAT CHANNEL HAS CORROSION ON UPPER AND LOWER SURFACE AROUND FASTENER HOLES, STA 1667, MARKED. REMOVED AND REPLACED CORRODED HAT CHANNEL AT STA 1667 RBL 70 IAW SRM 51-40-02 PARA 4 & 7, DWG 146N8722 REV B. ORIG "T" .050", LOSS OF .009" FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15 DETAIL VIII.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

PASSENGER CABIN FLOOR SUPPORT, STA 377.7 LBL 47.5 HAS SIGNS OF CORROSION ON LWR SIDE OF T-CAP. CORROSION FOUND TO BE ON REPAIR PARTS. REPLACED -2 SUPPORT ANGLE IAW SRM 53-00-51 REPAIR 1. REPLACED -6 REINFORCEMENT STRAP IAW SRM 53-00-51 REPAIR 1. REPLACED DAMAGED STIFFENER IAW DWG 141N5170 REV C.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4L LOWER SILL UPPER SURFACE, HAT CHANNEL HAS CORROSION, STA 1674, MARKED. REMOVED AND REPLACED STIFFENER IAW DWG 146N8722 REB B AND SRM 51-40-02.

Part: CHANNEL — CORRODED (DOOR SILL) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

R4 DOOR LOWER SILL UPPER SURFACE, HAT CHANNEL HAS CORROSION ON UPPER AND LOWER SURFACE AROUND FASTENER HOLES, STA 1667, MARKED. REMOVED AND REPLACED CORRODED HAT CHANNEL AT BS 1667 RBL 70 IAW SRM 51-40-02, PARA 4&7, DWG 146N8722 REV B. FOUND THE BRACKET OUT OF LIMITS IAW SRM 53-60-15, DETAIL VIII.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

DOOR 4R LOWER SILL UPPER SURFACE, HAT CHANNEL HAS CORROSION ON UPPER AND LOWER SURFACE AT FASTENER HOLES, STA 1664 RBL70, MARKED. REMOVED AND REPLACED HAT CHANNEL PART 143N8328Y60 PER DWG 146N8722 REV B AND SRM 51-40-02. ORIGINAL MATERIAL .030" LOSS OF .007", WITH .043" REMAINING. BLEND FOUND TO BE OUT OF LIMITS.

Part: CHANNEL — CORRODED (R4 DOOR SILL) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

R4 DOOR LOWER SILL UPPER SURFACE, FWD CHANNEL HAS CORROSION ON UPPER AND LOWER SURFACE AROUND FASTENER HOLES, BS 1660, RBL 71, THE CHANNEL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, DETAIL VIII. REMOVED AND REPLACED THE CHANNEL IAW DWG 146N8722, REV B, AND SRM 51-40-02, PAR 7.

Part: FLOORBEAM — CORRODED (BS 1320) · corrosion level 2 · airframe 70,192 hrs · 21,975 cycles

AFT PASSENGER CABIN, FLOORBEAM UPPER FWD FLANGE HAS CORROSION ON UPPER AND LOWER SURFACE AT NUTCLIP BS 1320 LBL 24 - RBL 24. FABRICATED A REPAIR ANGLE AND INSTALLED IAW SRM 53-00-51, TREATED, PRIMED, AND BLENDED AREAS. AREAS WERE WITHIN LIMITS.

Part: CABLE — BROKEN (DOOR DISARM) · airframe 70,192 hrs · 21,975 cycles

L4 DOOR DISARM CABLE IS BROKEN. REMOVED AND REPLACED THE DISARM CABLE IAW AMM 52-11-13, AND AMM 52-11-20. CHECKED GOOD.

Part: LANYARD — EXPOSED (R4 DOOR SLIDE) · airframe 69,803 hrs · 21,886 cycles

FA STATED THAT THE R4 DOOR IS SHOWING THE LANYARD FROM SLIDE AREA. ALL INDICATIONS IN FLIGHT DECK CHECKED NORMAL. INSPECTED AND SECURED THE DOOR SLIDE LANYARD IAW AMM 52-11.

Part: NOT REPORTED — DIRTY (R4 DOOR) · airframe 69,729 hrs · 21,870 cycles

R4 DOOR WILL NOT ARM. REMOVED DEBRIS. DOOR ARMED. OK FOR SERVICE. AMM 52-11.

Part: NOT REPORTED — DIRTY (R1 DOOR) · airframe 69,729 hrs · 21,870 cycles

R1 DOOR WILL NOT ARM. REMOVED DEBRIS. DOOR ARMED. OK FOR SERVICE. AMM 52-11.

Part: CLAMP — OUT OF POSITION · airframe 69,190 hrs · 21,760 cycles

FOUND WORN HOLD DOWN LOCK INOPERATIVE. REPOSITIONED THE HOLD DOWN CLAMP. OPS NORMAL.

Part: BUSTLE — LOOSE (L3 DOOR SLIDE) · airframe 67,911 hrs · 21,500 cycles

L3 DOOR SLIDE BUSSEL LOOSE AND INTERFERING WITH DOOR ARM AND CLOSE. REMOVED ADJUSTED AND REINSTALLED L3 DOOR BUSTLE IAW AMM 25-66, OPS CHECKED NORMAL.

Part: DOOR — OUT OF ADJUST (L1) · airframe 66,991 hrs · 21,330 cycles

SUSPECT 1L DOOR OUT OF ADJUSTMENT. ADJUSTED 1L DOOR PER B757 AMM 52-11. OPS CHK NML.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR SLIDE) · airframe 66,793 hrs · 21,293 cycles

L2 DOOR WILL NOT ARM. CYCLED DOOR SEVERAL TIMES, FOUND DEBRIS AT GIRT BAR. DOOR OPS CHECKED GOOD. OK FOR SERVICE.

Part: D-RING — UNSECURE (L2 DOOR SLIDE) · airframe 66,879 hrs · 21,309 cycles

ENTRY DOOR ARMING LEVER HARD TO OPERATE. PERFORMED VISUAL INSPECTION OF L2 DOOR. FOUND D-RING STRAP WRAPPED AROUND GIRT BAR. POSITIONED IAW AMM 25-66. CKECKED OK. SLIDE ARM LIGHT WORKS NORMAL.

Part: GIRT BAR — DETACHED (L2 DOOR SLIDE) · airframe 66,693 hrs · 21,275 cycles

L2 DOOR WON'T ARM. FWD SIDE OF GIRT BAR SLIDER DISCONNECTED. ATTACHED THE GIRT BAR. SLIDE ARMS NORMAL IAW AMM 52-11.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 66,430 hrs · 21,227 cycles

1R DOOR WILL NOT ARM. FOUND LANYARD ON DOOR BUSTLE CAUGHT IN GIRT BAR. ADJUSTED LANYARD PER AMM 52-11. OPS CHK GOOD. A/C OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,314 hrs · 21,206 cycles

EMERGENCY LIGHTS REMAINED ILLUMINATED AT ROWS 27 - 35 ON THE RT SIDE WITH SWITCH IN AUTO & OFF POSITION. WHEN TURNED ON, THE BACK OF THE CABIN LIGHTS ON FLOOR WERE INOPERATIVE, FRONTCABIN OK. R & R THE BATTERY PACK. EMERGENCY LIGHTS CHECKED OK IAW AMM 33-12.

Part: DOOR — OBSTRUCTED (L2) · airframe 66,027 hrs · 21,150 cycles

L2 ENTRY DOOR WILL NOT ARM. REMOVED DEBRIS FROM THE DOOR, OPS CHECKED GOOD IAW AMM 25-66.

Part: LANYARD — OUT OF POSITION (PAX DOOR) · airframe 65,556 hrs · 21,046 cycles

1R PAX DOOR SURVIVAL PACK CORD HANGING. RESECURED SURVIVAL PACK LANYARD. NOW OK, RE-INSTALLED SLIDE BUSTLE AMM 25-66.

Part: TERMINAL — DEFECTIVE (CABIN) · airframe 65,308 hrs · 20,988 cycles

MID GALLEY FLOOR EMERGENCY LIGHT INOP. REF WDM 33-51 FOUND BAD GROUND AT GD1450 DETERMINATE TERMINAL AND NOW LIGHT CHECKS GOOD.

Part: MECHANISM — OUT OF SEQUENCE (R2 DOOR) · airframe 61,626 hrs · 20,261 cycles

2R EXIT DOOR WILL NOT OPEN HANDLE SHOWS OPEN WILL NOT MOVE TO THE CLOSED POSITION. FOUND DOOR 2R INSIDE HANDLE MECHANISM OUT OF SEQUENCE. REMOVED AND REINSTALLED DOOR 2R INSIDE HANDLE IAW AMM 52-1-13. DOOR OPEN AND CLOSED WITHOUT OBSTRUCTION. OK FOR CONTINUED SERVICE.

Part: FRAME — DAMAGED (BS 1000) · airframe 60,552 hrs · 20,034 cycles

FUSELAGE FRAME HAS TWO HOLES MISDRILLED, BS 1000, RBL 10. ROUTED OUT DAMAGE ON FRAME IAW SRM 53-00-07, REPAIR 1 PERFORMED HFEC OF CUTOUT AND HFEC INSPECTION OF EXITING FASTENER HOLES IAW SRM 53-00-07, REPAIR 1 FIG 204 NO CRACKS FOUND MADE INSURANCE CUT IAW SRM 53-00-07, REPAIR 1, FABRICATED TREATED AND PAINTED REPAIR PARTS AND FRAME IAW SRM 53-00-07, REPAIR 1. INSTALLED REPAIR IAW SRM 53-00-07, REPAIR 1.

Part: DOOR — OUT OF SEQUENCE (L2) · airframe 59,591 hrs · 19,827 cycles

L2 DOOR WILL NOT OPEN. FOUND DOOR OUT OF SEQUENCE. CYCLED DOOR, OPS CHECKED OK.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,047 hrs · 19,551 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS FOR ROWS 27-44 INOPERATIVE. POWER SUPPLY FUSE WAS REPLACED. LP7087937.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 57,213 hrs · 19,375 cycles

FOUND AISLE EMERGENCY LIGHTS BETWEEN SEAT ROWS 19 THRU 24 INOPERATIVE. FOUND CONNECTOR PLUG NOT PROPERLY SEATED. RECONNECTED & PROPERLY SEATED PLUG ENDS. OP'S CK'S GOOD, REF WDM 33-50.

Part: BOTTLE — DISCHARGED (R2 DOOR SLIDE) · airframe 56,814 hrs · 19,295 cycles

R2 DOOR SLIDE PRESSURE IN RED. REPLACED THE R2 DOOR SLIDE IAW AMDS WORK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 1720) · corrosion level 2 · airframe 54,006 hrs · 18,737 cycles

AFT CARGO BAY BS 1720, RBL 3, FLOOR SUPPORT CORRODED AT FLOOR AREA. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-40-02 & 53-60-51, FIG 101. FABRICATED NEW FLOOR SUPPORT IAW B DWG 146N5300, REV C & 146N5240 REV C. HEAT TREATED TO A T6 CONDITION IAW FORM FAS0115, REV .011 INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02 AND APPLIED REPAIR FLOOR PANEL IAW SRM 51-70-03, PARA G, PG 17, GENERAL.

Part: SKIN — DENTED (BS 1621-1640) · airframe 52,311 hrs · 18,379 cycles

FUSELAGE SKIN, BS 1621 - 1640, S19-20L, DENTED.

Part: FRAME — DENTED (BS 1280) · airframe 52,118 hrs · 18,340 cycles

DENT DAMAGE ON THE INNER ANGLES OF FS 1280 FRAME ABOVE S26R. REPAIRED PER ER/A 502789-14AD, REV. B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,393 hrs · 18,014 cycles

FOUND R4 DOOR EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED IAW AMM 33-51, CHECK OK.

Part: SKIN — CORRODED (BS 1202) · corrosion level 2 · airframe 50,144 hrs · 17,967 cycles

CORROSION TO THE FUSELAGE BILGE SKIN, COMMON TO THE SERVICE LINE FEED THROUGH HOLES FOR THE MID LAV SERVICE PANEL. DAMAGE IS COMMON TO TWO (2) OF THREE (3) SERVICE LINE FEED HOLES LOCATED AS FOLLOWS: ONE (1) RT FWD HOLE AT STA 1202.25, RBL 2, BETWEEN S29 - 30R, AND ONE LT AFT HOLE AT BS 1206.25, LBL 2, BETWEEN S29 - 30L.

Part: COMPUTER — ODOR (RIGHT) · airframe 48,950 hrs · 17,705 cycles

AT FL300, THE RT AUTOPILOT DISENGAGED FOLLOWED BY A FAINT ELECTRICAL ODOR IN COCKPIT FOR TWO MINUTES. F/A CONFIRM FAINT ODOR IN FIRST CLASS, STRONGER IN FWD GALLEY. FOUND RT FCC AS SOURCE OF ODOR. REPLACED RT FCC AND RT AUTOPILOT AILERON SERVO ENGAGE SOLENOID DUE TO LOW RESISTANCE.

Part: SKIN — PUNCTURED (BS 1630) · airframe 48,021 hrs · 17,518 cycles

3 X 4" PUNCTURE IN SKIN AT BS 1630 BETWEEN STRINGER S-20L AND S-19L REPAIRED AND INSTALLED PERMANENT REPAIR IAW ERA 509449-14 REV.

Part: SKIN — GOUGED (BS 1661) · airframe 48,021 hrs · 17,518 cycles

3 INCH LONG GOUGE IN SKIN AT STA 1661 AND STRINGER S-20L .015 TO .025" REPAIRED AND INSTALLED PERMANENT REPAIR IAW ERA 509451-14, REV.

Part: SKIN — GOUGED (BS 1696) · airframe 48,021 hrs · 17,518 cycles

1.5 INCH LONG GOUGE IN SKIN AT BS 1696 AT STRINGER S-20L .012 TO .018 INCH DEEP. REPAIRED AND INSTALLED PERMANENT REPAIR IAW ERA 509449-14, REV.

Part: CONTROL PANEL — ODOR (COCKPIT) · airframe 47,297 hrs · 17,368 cycles

AIR RETURN BACK TO DEPARTURE DUE TO BURNING ELECTRIC ODOR IN THE FLIGHT DECK AND CABIN. FOUND VOR/DME CONTROL PANEL WITH ELECTRICAL ODOR. R & R PANEL, CHECKED OK.

Part: SKIN — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

SKIN CORRODED AROUND UPPER AND LOWER SURFACE OF CTR LOWER LAVATORY PANEL. COMPLIED WITH ERA 503383-14 REV A,

Part: FLOORBEAM — DAMAGED (BS 418 LBL 55) · airframe 46,573 hrs · 17,222 cycles

FLOORBEAM UPPER CAP, DAMAGED AT BS 418 - LBL 55. REMOVED DAMAGED SECTION OF FLOORBEAM. BEGAN MAKING REPAIR PARTS REF SRM 53-00-511. REPAIRED PER PRI 503241-14 REV O.

Part: FRAME — DENTED (BS 1260) · airframe 46,573 hrs · 17,222 cycles

DURING HMV, ONE DENT WAS FOUND ON THE UPPER FLANGE OF THE BS 1260 LOWER FRAME BETWEEN STR 23L AND STR 24L. REPAIRED THE DAMAGE TO THE FRAME PER SRM 53-00-07 REPAIR 5, FIGURE 201, DETAIL III.

Part: FRAME — DENTED (BS 1300) · airframe 46,575 hrs · 17,223 cycles

DURING HMV, ONE DENT WAS FOUND ON THE LT SIDE C2 CARGO BAY BS 1300- FRAME FLANGE. REMOVED DAMAGED AREA PER SRM 53-00-07 REPAIR 5. PERFORMED HFEC INSPECTION OF CUTOUT, NO ITEMS NOTED. FABRICATED REPAIR AND INSTALLED. TREATED, PRIMED AND PAINTED REF ERA502791-14 REV ORIGINAL.

Part: SUPPORT — CORRODED (LAVATORY PANEL) · airframe 46,573 hrs · 17,222 cycles

CORROSION FOUND AT FORE & AFT SUPPORTS FOR LOWER CENTER LAVATORY PANEL. AFT SUPPORT REMOVED ON NR 262 LOCATED ALL FASTENER HOLES AND SIZED DWG 149N7701. INSTALLED AFT SUPPORT BRACKETS FOR BOTH LEFT AND RIGHT PANEL SUPPORT BRACKETS DRILLED HOLES FOR NUTPLATES PAINTED HOLES AND INSTALLED NUTPLATES.

Part: SUPPORT — CORRODED (LAVATORY PANEL) · airframe 46,573 hrs · 17,222 cycles

FORE AND AFT SUPPORTS UPPER AND LOWER SIDES FOUND CORRODED, OF LOWER LAVATORY PANEL. REMOVED SUPPORTS AND FOUND TO BE CORRODED BEYOND LIMITS. INSTALLED SUPPORT.

Part: FRAME — DAMAGED (BS 1300) · airframe 49,882 hrs · 17,917 cycles

FRAME DAMAGED BS 1300, S25L. REPAIRED IAW ERA 06-502791-14AD.

Part: FLOORBEAM — CORRODED (BS 1640)

DURING INSPECTION CORROSION WAS DISCOVERED TO THE UPPER CAP OF THE FLOORBEAM LOCATED AT STATION 1640 AROUND FASTENER HOLES AND AT DOOR THRESHOLD. REMOVED DAMAGE AREA AND INSPECTED. NO DISCREPANCIES NOTED. FABRICATED REPAIR AND TREATED AREA.

Part: FRAME — DENTED (BS 1480) · airframe 46,573 hrs · 17,222 cycles

FOUND DENT ON CARGO BAY FRAME BS 1480. REMOVED DAMAGE AREA PER SRM 53-00-07 REPAIR 5. PERFORMED HFEC INSPECTION OF CUTOUT PER SRM 53-00-07 REPAIR 5. COMPLIED WITH BHEC IN EXITING HOLES COMMON TO REPAIR IAW NDT MANUAL PT 6 51-00-16. FABRICATED REPAIR PER SRM 53-00-07. COLD WORKED HOLES PER SRM 53-00-07. INSTALLED REPAIR PER SRM 53-00-07

Part: FRAME — DENTED (BS 1460) · airframe 46,573 hrs · 17,222 cycles

FOUND DENT, ON FRAME BS 1460. REMOVED DAMAGE AREA PER SRM 53-00-07 REPAIR 5. PERFORMED HFEC INSPECTION OF CUTOUT PER SRM 53-00-07 REPAIR 5. COMPLIED WITH HFEC INSPECTION OF EXITING HOLES PER SRM 53-00-07 FIG 201. NO CRACKS FOUND, COLD WORKED END FASTENER HOLES PE SRM 51-40-09. FABRICATED REPAIR PER SRM 53-00-07 REPAIR 5 DETAIL 1. INSTALLED REPAIR PER SRM 53-00-07.

Part: FRAME — DAMAGED (BS 1000) · airframe 46,573 hrs · 17,222 cycles

FUSELAGE FRAME HAS TWO HOLES MISDRILLED, BS 1000, RBL 10. ROUTED OUT DAMAGE ON FRAME PER SRM 53-00-07 REPAIR 1. PERFORMED HFEC OF CUTOUT AND HFEC INSPECTION PER SRM 53-00-07 REPAIR 1 FIG 204. NO CRACKS FOUND MADE INSURANCE CUT PER SRM 53-00-07 REPAIR 1. FABRICATED TREATED AND PAINTED REPAIR PARTS AND INSTALLED FRAME PER SRM 53-00-07 REPAIR 1.

Part: FRAME — DENTED (BS 1500) · airframe 46,573 hrs · 17,222 cycles

FOUND DENT ON FRAME BS 1500. REMOVED DAMAGED AREA PER SRM 53-00-07 REPAIR 5. PERFOMED HFEC INSPECTION OF CUTOUT PER SRM 53-00-07 REPAIR 5. COMPLIED WITH BHEC IN HOLES EXISTING COMMON TO REPAIR IAW NDT MANUAL PT 6 51-00-16, INSTALLED REPAIR PER SRM 53-00-07 REPAIR 5.

Part: FRAME — DENTED (BS 1340) · airframe 46,573 hrs · 17,222 cycles

FOUND DENT ON FRAME BS 1340. REMOVED DAMAGED AREA PER SRM 53-00-07 REPAIR 5. PERFORMED HFEC INSPECTION OF CUTOUT PER SRM 53-00-07 REPAIR 5. DRILLED DOUBLER PER SRM 53-00-07 REPAIR 5. INSTALLED REPAIR PER SRM 53-00-07.

Part: FRAME — DENTED (BS 720) · airframe 46,573 hrs · 17,222 cycles

FOUND DENT ON FRAME BS 720. REMOVED DAMAGE PER SRM 53-00-07 REPAIR 5. FORMED REPAIR ANGLE PER SRM 53-00-07 REPAIR 5. HFEC INSPECTION OF DAMAGE CUT OUT OK IAW SRM 53-00-07. COMPLIED WITH HFEC OF HOLES COMMON TO THE REPAIR PER SRM 53-00-07 REPAIR 5. NO INDICATIONS NOTED, FABRICATED REPAIR AND DRILLED PER SRM 53-00-07 REPAIR 5. REPAIRED PER SRM 53-00-07 REPAIR 5.

Part: FRAME — DENTED (BS 1580) · airframe 46,573 hrs · 17,222 cycles

FOUND DENT ON FRAME BS 1580. REMOVED DAMAGED AREA PER SRM 53-00-07 REPAIR 5. PERFOMED HFEC INSPECTION OF CUTOUT PER SRM 53-00-07 REPAIR 5. FABRICATED REPAIR PER SRM 53-00-07 REPAIR 5. PERFORMED HFEC INSPECTION OF ALL INITIAL FASTENER HOLES PER SRM 53-00-07 REPAIR 5. DRILLED REPAIR PER SRM 53-00-07 REPAIR 5 AND INSTALLED PER SRM 53-00-07 REPAIR 5 DETAIL 1.

Part: FASTENER — DAMAGED (RWS 285.65)

DURING REWORK MAINTENANCE DISCOVERED DAMAGE TO TWO FASTENERS RT WING APPROXIMATELY RIB WS 285.65. LOCATED UNDERNEATH THE FWD END OF THE INBOARD SIDE LOAD FITTING. REMOVED FASTENERS AND PERFORMED INSPECTION. NO DISCREPANCIES NOTED. INSTALLED TWO FASTENERS REF: ERA 502311-14.

Part: FRAME — DAMAGED (BS 1120 S2R) · airframe 46,573 hrs · 17,222 cycles

FUSELAGE FRAME HAS TWO MISDRILLED HOLES BELOW STRINGER 2R. NOT WITHIN LIMITS PER SRM 53-00-07 FIG 1 SHEET 1. ROUTED OUT DAMAGE ON FRAME PER SRM 53-00-07 REPAIR 1. HFEC INSPECTED CUTOUT PER SRM 53-00-07 FIG 201. NO CRACKS FOUND MADE INSURANCE CUT TO ROUTED AREA PER SRM 53-00-07 REPAIR 1. HFEC FASTENER HOLES PER SRM 53-00-07 FIG 201 REP 1 STEP 4H. FABRICATED REPAIR PARTS, TREATED AND PAINTED FRAME, REPAIR PER SRM 53-00-07 REPAIR 1 AND INSTALLED.

Part: FRAME — DENTED (BS 1400) · airframe 46,573 hrs · 17,222 cycles

FRAME DENTED, C2 CARGO BAY LT SIDE BS 1400 - INNER "FREE FLANGE". REMOVED DAMAGED AREA PER SRM 53-00-07 REPAIR 5. PERFORMED HFEC INSPECTION OF CUTOUT PER SRM 53-00-07 REPAIR 5. COMPLIED WITH OPEN HOLE EC INSPECTION IAW NDT MANUAL PT 6 51-00-16. FABRICATED DOUBLER PER SRM 53-00-07. INSTALLED PER SRM 53-00-07 & SRM 53-00-07 REPAIR 5.

Part: INTERCOSTAL — CORRODED (BS 1600-1620) · airframe 46,573 hrs · 17,222 cycles

CORROSION LOCATED AT BS 1600-1620 ON INTERCOSTAL. REMOVED INTERCOSTAL, DRILLED NEW INTERCOSTAL PER DWG 146N5451. INSTALLED INTERCOSTAL PER DWG 146N5451.

Part: FRAME — DAMAGED (BS 1320) · airframe 46,573 hrs · 17,222 cycles

DENT C2, CARGO COMPARTMENT, LT SIDE STA 1320 - INNER FREE FLANGE. REMOVED DAMAGE AREA PER SRM 53-00-07 REPAIR 5. PERFORMED HFEC INSPECTION OF CUTOUT PER SRM 53-00-07 REPAIR 5. NO ITEMS REMOVED OLD DOUBLER AND FASTENERS PERFORMED BHEC INSPECTION PER SRM 53-00-07 REPAIR 5. NO CRACK FOUND STARTED TO FABRICATE NEW DOUBLER REF SRM 53-00-07 DETAIL III COMPLETED FABRICATION OF REPAIR PARTS PER SRM 53-00-07 REPAIR 5. TREATED AND PAINTED DOUBLER PER SRM 53-00-07 REPAIR 5. BEGAN INSTALL OF REPAIR PER SRM 53-00-07 REPAIR 5. FINISHED INSTALLATION OF REPAIR PER SRM 53-00-07 REPAIR 5.

Part: FRAME — DAMAGED (BS 1420)

DURING INSPECTION A DENT WAS DISCOVERED IN THE C2 CARGO COMPARTMENT LEFT SIDE BS 1420 - INNER FREE FLANGE. REMOVED DAMAGE AREA AND INSPECTED IAW SRM 53-00-07 REPAIR 5. NO DISCREPANCIES NOTED. FABRICATED REPAIR, INSTALLED AND TREATED AREA.

Part: FRAME — DENTED (BS 1520)

DURING INSPECTION A DENT WAS DISCOVERED IN THE C2 CARGO COMPARTMENT LEFT SIDE BS 1520 - INNER FREE FLANGE. REMOVED DAMAGE AREA AND INSPECTED REF: B757 SRM 53-00-07 REPAIR 5. NO DISCREPANCIES NOTED. FABRICATED REPAIR, INSTALLED AND TREATED AREA.

Part: STRINGER — DAMAGED (BS 1440)

WHILE PERFORMING MAINTENANCE, DISCOVERED A MISDRILLED HOLE AT LOCATION STATION 1440 STRINGER 2-R. ROUTED OUT DAMAGE ON FRAME AND MADE INSURANCE CUT TO AREA. INSPECTED, NO CRACKS FOUND. FABRICATED REPAIR AND TREATED & PAINTED.

Part: STRINGER — DAMAGED (BS 1340 S2L)

MAINTENANCE DISCOVERED TOOLING DAMAGE AT BS 1340 STRINGER 2L. ROUTED OUT DAMAGE, MADE INSURANCE CUT AND INSPECTED, NO CRACKS FOUND. FABRICATED REPAIR AND INSTALLED, TREATED/PAINTED AREA.

Part: SKIN — MISREPAIRED (BS 400 S5-7L) · airframe 46,573 hrs · 17,222 cycles

SKIN AT BS 400, STR 5L TO 7L MISREPAIRED. REPAIRED IAW ERA 502651-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1390-1420) · airframe 46,573 hrs · 17,222 cycles

FLOORBEAM CORRODED UNDER NUTPLATES, BS 1390-1420, LBL 3 . REMOVED CORROSION AND AREA OUT OF LIMITS PER SRM 53-00-53. REMOVED AND INSTALLED FLOORBEAM.

Part: FRAME — CORRODED (BS 1560 STR 26R) · airframe 46,573 hrs · 17,222 cycles

CORROSION ON FRAME AT STA 1560 ABOVE STR 26R IS CORRODED AT FASTENER HOLE. REMOVED FRAME REPLACED FORMER PER DRAWING 453N1801.

Part: INTERCOSTAL — CORRODED (BS 1520-1540) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL WEB CORRODED AT BS 1520-1540. REMOVED WEB, DRILLED AND INSTALLED NEW WEB AT AND BETWEEN LOCATION STA 1520-1540 REF DWG 146N5451.

Part: FRAME — CORRODED (BS 1560 S26L) · airframe 46,573 hrs · 17,222 cycles

FRAME AT BS 1560 ABOVE S26L IS CORRODED AT FASTENER HOLE. REMOVED FORMER REPLACED FRAME PER DWG 453N1801.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 46,573 hrs · 17,222 cycles

FLOORBEAM CORRODED, STA 324.0 UNDER GALLEY BEAM, BL0-TO CUSP LINE, CONDITION: CORROSION LOCATION FWD WET AREA POS: CN REPAIRED PER ERA 501777-14 PRI REV 3. REPAIRED PER ERA501777-14 PRI REV4 PRI 501777-14 REV 4 MATCHES ERA 501777-14 REV ORIG.

Part: FLOORBEAM — CRACKED (BS 1640) · airframe 46,573 hrs · 17,222 cycles

STABILIZATION STRAP CRACKED BS 1640, FLOORBEAM STABILIZATION STRAP, LOWER SURFACE OF BEAM, COMPLETED STEPS 1 AND 2 PER ERA384483-14MA REV C. INSPECTION OF STOP DRILL FOR CRACK CONTAINMENT OK, REF ERA 384483-14MA REV C STEP 3. FABRICATED AND DRILLED DOUBLER REF ERA 384483-14. TREATED AND PAINTED DOUBLER, INSTALLED DOUBLER AND COMPLETED ERA 384483-14MA

Part: CUSP WEB — DAMAGED (BS 1635) · airframe 46,574 hrs · 17,222 cycles

DURING INSPECTION, FOUND WEB DAMAGED AT CUSP ANGLE, LOWER SIDE BS 1635, LBL 65. MAINTENANCE REMOVED THE CUSP WEB, POSITIONED, LOCATED, AND SIZED ALL HOLES IAW DWG 146N8722, INSTALLED OTBD ROW OF FASTENERS AND REPLACED THE CUSP WEB IAW DWG 146N8722.

Part: ANGLE — CORRODED (BS 1672) · airframe 46,574 hrs · 17,222 cycles

DURING INSPECTION, FOUND THE CUSP WEB ANGLE CORRODED AT BS 1672. MAINTENANCE REMOVED AND REPLACED THE CUSP WEB ANGLE IAW SRM 53-00-51, AND DWG 146N8722.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL- DAMAGED LOCATION: STA 345 - 365 LBL 20. FABRICATED REPLACEMENT PART PER BAC DWG 141N5150. INSTALL INTERCOSTAL (QC 2058) REPLACED WEB REF BAC DWG 141N5150.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL- CORROSION LOCATION: BL 0 STA 1640-1660. REPLACED INTERCOSTAL REF BAC DWG 146N5230.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CHANNEL- CORROSION LOCATION: FLOOR SUPPORT CHANNEL LOCATED FROM STA 1500-1640 RBL 12.25 POS: AFT REMOVED FLOOR SUPPORT CHANNEL BEGAN DRILLING HOLES ON FLOOR SUPPORT CHANNEL. OK TO INSTALL FLOOR SUPPORT FINISH INSTALLATION OF FLOOR SUPPORT CHANNEL PER BAC DWG 146N5390.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

Z- ANGLE- CORROSION LOCATION: FLOOR SUPPORT RT OUTBD FLOOR SUPPORT STA 1300-1340. POS: AFT REMOVED Z ANGLE AT STA 1300-1340 RT OUTBD FLOOR SUPPORT FASTENER HOLES IN Z ANGLE AT STA 1300-1340. OK TO TREAT & PAINT PER PS 900-3-6 NR 3 BEGAN INSTALLATION OF Z ANGLE PER BAC DWG 146N5390 INSTALLED Z ANGLE PER BAC DWG 146N5390.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FIXED FLOOR PNL- CORROSION. LOCATION: RT SIDE FS 1200 -1310 C-2 BB. POS: AFT REMOVED FIXED FLOOR PER B757 SRM 53-00-53 (292233) DRILLED UP NEW FIXED FLOOR PANEL PER BAC DWG 146N5390 OK TO INSTALL. INSTALLED FIXED FLOOR PANEL PER BAC DWG 146N5390.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

SEAT TRACK - CORROSION LOCATION: STA 1640 RT OUTBD TRACK POS: AFT CLEANED TRACK AND FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-52 AND REMOVED TRACK SECTION FROM STA 1540 -1640 SEAT TRACK FABRICATED ON SHOP ORDER EY7737 BEGAN DRILLING SEAT TRACK. OK TO INSTALL NEW TRACK. REPLACED SEAT TRACK REF BAC DWG 146N5120.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CORROSION, AFT CARGO BIN, BILGE, STA 1618 BL-0. AFT CARGO POS: AFT REMOVED INTERCOSTAL FOUND CORROSION ON ADJACENT SKIN & FRAME. REMOVED FRAME CLIP & SEVERAL FASTENERS TO ACCESS CORROSION. REMOVED CORROSION ON SKIN & FRAME CLIP PER B757 SRM 53-00-01 & 53-00-07 PAINT ENT & CLIPS ALODINE & PRIMED SKIN & CLIPS PER B757 AMM 51-20. APPLIED TOP COAT TO SKIN & CLIPS REF B757 AMM 51-20, INSTALLED ANGLES ON NEW INTERCOSTAL & CLIPS/FRAME PER BAC DWG 146N5432.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT - CORROSION LOCATION: FS 1320 & 1330 BOTTOM SIDE, ABOVE STR 29R,C-2 BB POS: AFT FLOOR SUPPORT OUT OF LIMITS PER B757 SRM 53-00-53 BEGAN REMOVAL OF SUPPORT FINISHED REMOVING FLOOR SUPPORT AND DRILLED UP REPLACEMENT PER B757 BAC DWG 146N5390 (882888) OK TO INSTALL Z ANGLE, INSTALLED ANGLE PER B757 BAC DWG 146N5390.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 46,574 hrs · 17,222 cycles

DURING INSPECTION FOUND LEFT OTBD SEAT TRACK BS 1614, DAMAGED ON INNER LIP BEYOND ALLOWABLE LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK IAW DWG 146N5120.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT- CORROSION. LOCATION: STA 1640-1661, LBL 52 AT TOP AND BOTTOM OF FASTENER HOLES. REMOVED SUPPORT DRILLED NEW SUPPORT REF B757 DWG 146N5230. OK TO INSTALL. INSTALLED FLOOR SUPPORT REF B757 DWG 146N5230.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 46,574 hrs · 17,222 cycles

DURING INSPECTION FOUND LEFT OUTBD SEAT TRACK AT BS 1601.5, STUD HOLE DAMAGED BEYOND ALLOWABLE LIMITS. MAINTENANCE REMOVED SEAT TRACK, FABRICATED, AND REPLACED SEAT TRACK IAW DWG 146N5120.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

LT FIXED FLOOR PNL- CORROSION LOCATION: FS 1310-1410 C-2 BB POS: AFT BLENDED CORROSION AND FOUND AREA TO BE OUT OF LIMITS PER B757 SRM 53-00-53. REMOVED FIXED FLOOR PANEL BEGAN DRILLING NEW FIXED FLOOR PANEL REF BAC DWG 146N5391 OK TO INSTALL [1315]. FINISHED INSTALLING PANEL PER REF BAC DWG 146N5391.

Part: SEAT TRACK — DAMAGED (BS 1636) · airframe 46,574 hrs · 17,222 cycles

DURING INSPECTION, FOUND OTBD LEFT SEAT TRACK AT BS 1636, INNER LIP DAMAGED BEYOND ALLOWABLE LIMITS. MAINTENANCE REMOVED THE SEAT TRACK, FABRICATED, AND REPLACED THE SEAT TRACK IAW DWG 146N512.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

BRACKET - CORROSION LOCATION: STA 1300 STR 28R POS: AFT REMOVED BRACKET DRILLED UP NEW BRACKET INSTALL OF REPAIR BRACKET COMPLETED INSTALLATION OF BRACKET PER DWG 146N5400.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CARGO FLOOR PANEL BEAM CORRODED AT NUT PLATES. CORROSION LOCATION: AFT CARGO STA 1340-1440 RBL 10 POS: AFT TASK REMOVED CARGO FLOOR PANEL BEGAN AT FACTORY SPLICE STA 1340-1440 DRILLED UP REPLACEMENT SECTION OF BEAM PER BAC DWG146N5390 ALODINED REPLACEMENT BEAM PER BAC DWG 146N5390 OK TO TREAT AND PAINT. TREATED AND PAINTED PER BAC DWG 146N5390, INSTALLED PER BAC DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CHANNEL- CORROSION LOCATION: FLOOR SUPPORT CHANNEL LOCATED FROM STA 1500-1640 RBL 7.25 POS: AFT REMOVED FLOOR SUPPORT INSTALLED FLOOR SUPPORT CHANNEL PER BAC DWG 146N5390.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOORBEAM - CORROSION LOCATION: BL 0 STA 1640. REMOVE CORROSION & FOUND OUT OF LIMITS PER B757 SRM 53-00-51. T-CAP REPLACED ON N/R 459.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT- CORROSION LOCATION: STA 1650 -1660, RBL 52 CORROSION AT FASTENER HOLE ON TOP AND BOTTOM. REMOVED FLOOR SUPPORT BEGAN DRILLING UP NEW FLOOR SUPPORT PER BAC DWG 146N5230. COMPLETED DRILLING FLOOR SUPPORT PER BAC DWG 146N5230. INSTALLED SUPPORT PER BAC DWG 146N5230.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 46,573 hrs · 17,222 cycles

FIXED FLOOR PNL - CONDITION: CORROSION LOCATION: LT SIDE FS 1200-1310 C-2 BB BLENDED CORROSION STA 1200 - 1260 (348183) BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-53 (486125) BEGAN REMOVING FIXED FLOOR PANEL (486125). REMOVED FIXED FLOOR PANEL (604284) STARTED PICKING UP HOLES (348183) INSTALLED NUT PLATES (645474) OK TO INSTALL (1315). FINISHED INSTALLATION OF FIXED FLOOR PANEL PER BAC DWG 146N5391(201079) 696577 STA ATL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CHANNEL CONDITION: FLOOR SUPPORT CHANNEL LOCATED FROM STA 1500-1640 RBL 2.5. POS: AFT REMOVED CHANNEL. DRILLED UP NEW CHANNEL PER BAC DWG 146N5390. OK TO INSTALL. INSTALLED CHANNEL PER BAC DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CHANNEL- CORROSION LOCATION: FLOOR SUPPORT CHANNEL LOCATED FROM STA 1500-1640 LBL 2.5. POS: AFT REMOVED CHANNEL 29MAR12 DRILLED UP CHANNEL PER BAC DWG 1465390 OK TO INSTALL [1315] INSTALLED NEW CHANNEL PER BAC DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CHANNEL- CORROSION LOCATION: FLOOR SUPPORT CHANNEL LOCATED FROM STA 1500-1640 LBL 12.25 POS: AFT REMOVED FLOOR SUPPORT CHANNEL FROM STA 1500 TO 1640 LBL 12.25. OK TO INSTALL. STARTED INSTALLATION OF CHANNEL FROM STA 1500 TO 1600 (458447) INSTALLED CHANNEL PER BAC DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT- CONDITION: CORROSION LOCATION: INSIDE R4 DOOR, STA 1675-1679, RBL 50. REMOVED CORROSION CHECKED LIMITS PER B757 SRM 53-00-04 FIG 101 FOUND TO BE OUT OF LIMITS. DRILLED UP NEW SUPPORT ANGLE REF DWG BAC DWG 146N5230. REPLACED SUPPORT REF DWG BACDWG 146N5230.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CORROSION LOCATION: STA 1661- 1681, RBL 52 CORROSION AT TOP AND BOTTOM OF FASTENER HOLES REMOVED CORROSION CHECK LIMITS PER B757 SRM 53-00-04 FIG 101 AND FOUND TO BE OUT OF LIMITS. DRILLED UP NEW SUPPORT REF DWG 146N5230. REPLACED SUPPORT REF REMOVED CORROSION CHECK LIMITS PER B757 SRM 53-00-04 FIG 101 AND DWG 146N5230 352187 STA ATL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT- CORROSION STA 700-720 OUTBD SUPPORT AT NUT PLATE. REMOVE FLOOR SUPPORT (303914) DRILLED NEW FLOOR SUPPORT REF BAC DWG 143N5400. INSTALLED NEW FLOOR SUPPORT REFBAC DWG 143N5400.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT- CONDITION: CORROSION LOCATION: STA 680-700 AT NUT PLATE LOC NEAR FWD DOOR DRAIN FOR L-2 DOOR (MARKED). REMOVED FLOOR SUPPORT (303974) DRILLED NEW FLOOR SUPPORT REF BAC DWG 143N5400 (953289) INSTALLED NEW FLOOR SUPPORT (953289) REF BAC DWG 1435400.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT PANEL- CORROSION STA 720-740 AT NUT PLATE NEAR L2 DOOR AFT DRAIN POS: MID REMOVED FLOOR SUPPORT (303974) DRILLED NEW FLOOR SUPPORT REF BAC DWG 143N5400 (955289) OK TO INSTALL NEW FLOOR SUPPORT REF BAC DWG 143N5400.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CARGO PANEL FLOORBEAM CORRODED UNDER NUT PLATES. AFT CARGO STA 1390-1405, RBL 10 -- MKD. REMOVE CARGO FLOOR PANEL BEAM AT FACTORY SPLICE STA 1340-1440. DRILLED UP REPLACEMENT SECTION OF BEAM PER BAC DWG 146N5390 (882888). ALODINED REPLACEMENT BEAM PER BAC DWG 146N5390. TREATED AND PAINTED PER BAC DWG 146N5390 (492172). BEGAN INSTALLATION OF FLOORBEAM SUPPORT (492172). COMPLETED INSTALLATION PER B757 BAC DRAWING 146N5390.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR PANEL SUPPORT- CORROSION LOCATION: STA 720-740 AT NUT PLATE NEAR R-2 AFT DOOR DRAIN POS: MID REMOVED SUPPORT PER BAC DWG 143N5400 (320257) DRILLED NEW GUTTER SUPPORT REF BAC DWG 143N5400 (953289) OK TO INSTALL. INSTALLED NEW SUPPORT REF BAC DWG 143N5400.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL CORRODED STA 1280-1300 LBL 25, MARKED NUMBER 2- CORROSION LOCATION: MID LAV WET AREAS POS: AFT BEGAN REMOVAL OF INTERCOSTAL AT STA 1280 - 1300 REF BAC DWG 146N5270 (416338) REMOVED INTERCOSTAL STA 1280-1300 LBL 25 REF BAC DWG 146N5270 DRILLED NEW INTERCOSTAL (612456) OK TO INSTALL BEGAN INSTALLATION OF INTERCOSTAL REF BAC DWG 146N5270 (612456) INSTALLED INTERCOSTAL REF BAC DWG 146N5270.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT CORROSION LOCATION: STA 1661-1681, LBL 52 TOP AND BOTTOM OF FASTENER HOLES MARKED POS: CN REMOVED FLOOR SUPPORT (699498 27MAR12) DRILLED UP NEW SUPPORT AND INSTALLED STANDOFF CLIP PER B757 DWG 146N5230. INSTALLED NEW FLOOR SUPPORT PER B757 DWG 146N5230.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CHANNEL CORROSION LOCATION: FLOOR SUPPORT CHANNEL LOCATED FROM STA 1500-1640 LBL 7.25 POS: AFT REMOVED FLOOR SUPPORT CHANNEL PER BAC DWG 146N5390 (492172) DRILLED UP REPLACEMENT FLOOR SUPPORT CHANNEL PER BAC DWG 146N5390. INSTALLED FLOOR SUPPORT CHANNEL PER B757 BAC DRAWING 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT - CORROSION LOCATION: FS 1330 RT OF STR 30, BOTTOM SIDE,C-2 BB POS: C/W ON N/R CARD 163 (645474).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

FLOOR SUPPORT - CORROSION LOCATION: FS 1304 & 1320 RBL 2 BOTTOM SIDE, C-2 BB POS: AFT FLOOR SUPPORT OUT OF LIMITS PER B757 SRM 53-00-53 (453003) BEGAN REMOVAL OF SUPPORT (792172) COMPLETED REMOVAL OF FLOOR SUPPORT (497049) FABRICATED NEW ANGLE (645474) OK TO INSTALL FLOOR SUPPORT INSTALLED NEW FLOOR SUPPORT (645474) INSTALLED PER BAC DWG 146N5390.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CHORD - CONDITION: CORROSION LOCATION: INNER UPPER CREASE BEAM CHORD BETWEEN STA 729 - STA 740 APPROX LBL 64 POS: MID REMOVED DAMAGED CHORD AND DRILLED UP NEW PART PER BAC DWG 143N8322 (955289) INSTALLED NEW CHORD ANGLE REF BAC DWG 143N8322.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

CARGO FLOOR PANEL BEAM CORRODED UNDER NUT PLATES- CONDITION: CORROSION LOCATION: AFT CARGO STA 1438, LBL 3 -- MKD POS: AFT REMOVED CORROSION AND AREAS OUT OF LIMITS PER B757 SRM 53-00-53. REMOVED FLOOR SUPPORT. OK TO INSTALL WORK, COMPLETED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL CORRODED, STA 1260-1280 LBL 25 MARKED NUMBER 3- CORROSION LOCATION: MID LAV WET AREAS POS: CN BEGAN REMOVAL OF INTERCOSTAL AT STA 1260-1280 REF BAC DWG 146N5270 (416378 28MAR12) REMOVED INTERCOSTAL. BEGAN INSTALLATION OF INTERCOSTAL REF BAC DWG 146N5270 (612456) INSTALLED INTERCOSTAL REF BAC DWG 146N5270.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 46,573 hrs · 17,222 cycles

FLOORBEAM CORRODED, BS 324 UNDER GALLEY BEAM, BL 0 TO CUSP LINE. CORROSION FWD WET AREA. THE UPPER FLOORBEAM TEE WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER ERA 501777-14.

Part: CHANNEL — CORRODED (BS 1700-1718) · airframe 46,573 hrs · 17,222 cycles

HAT CHANNEL HAS CORROSION. REMOVED CORROSION AND CHECKED LIMITS PER SRM 53-00-51, FOUND TO BE OUT OF LIMITS. REMOVED SUPPORT. LOCATED HAT CHANNEL AND DRILLED REF DWG 146N5300. INSTALLED CHANNEL PER DWG 146N5300.

Part: INTERCOSTAL — CORRODED (BS 1280-1300) · airframe 46,573 hrs · 17,222 cycles

RT MID LAV INTERCOSTAL CORRODED BS 1280-1300 RBL 25. REMOVED CHANNEL BS 1280-1300. BEGAN INSTALLATION OF RT MID LAV INTERCOSTAL PER DWG 146N5270. COMPLETED INSTALLATION ON NEW INTERCOSTAL REF DWG 146N5270.

Part: INTERCOSTAL — CORRODED (BS 1300-1320) · airframe 46,573 hrs · 17,222 cycles

RT MID LAV INTERCOSTAL CORRODED, BS 1300-1320 RBL 25. REMOVED INTERCOSTAL BS 1300-1320 REF DWG 146N5270. DRILLED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL AT BS 1300-1320 RBL 25 REF DWG 146N5270.

Part: INTERCOSTAL — CORRODED (BS 1300-1320) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL CORRODED, STA 1300-1320,LBL 25. REMOVED INTERCOSTAL STA 1300-1320 REF DWG 146N5270. BEGAN INSTALLATION OF INTERCOSTAL REF DWG 146N5270. COMPLETED INSTALLATION OF INTERCOSTAL STA 1300-1320 LBL25 REF DWG 146N5270.

Part: INTERCOSTAL — CORRODED (BS 1240-1280) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL CORRODED STA 1240-1280 LBL 25. REMOVED INTERCOSTAL BS 1240-1260. TRANSFERRED HOLES TO NEW INTERCOSTAL PER DWG 146N5270. REPLACED CHANNEL PER REF 757 DWG 146N.

Part: CHANNEL — CORRODED (BS 1661-1681) · airframe 46,573 hrs · 17,222 cycles

HAT CHANNEL HAS CORROSION. FABRICATED CHANNEL PER DWG 146N5184. INSTALLED HAT CHANNEL REF DWG 146N5184.

Part: INTERCOSTAL — CORRODED (BS 370 RBL 53) · airframe 46,573 hrs · 17,222 cycles

INTERCOSTAL CORRODED STA 370, RBL 53-63 MARKED NUMBER 23. REMOVED CORRODED SUPPORT FOR REPLACEMENT PER DWG 141N5185. REINSTALLED REPLACEMENT SUPPORT PER DWG 141N5185.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 46,573 hrs · 17,222 cycles

CORROSION ON FLOORBEAM BS 345, BL-0 TO RBL 60. COMPLETED STEPS 1 & 2 PER SRM 53-00-51 REPAIR 3. BEGAN FABRICATION OF NEW FLOORBEAM PER SRM 53-00-51 FIG 201. COMPLETED STEPS 3 THRU 6 PER SRM 53-00-51 REPAIR 3. TREATED AND PAINTED PER SRM 53-00-51 REPAIR 3 STEPS 7 & 8. BEGAN INSTALLATION PER SRM 53-00-51 REPAIR 3. REPAIRED PER SRM 53-00-51.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 46,404 hrs · 17,161 cycles

DISBOND ON T/E OF LT INBD MAIN FLAP AT FLAP STA 237.88 TO 224.63.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 46,404 hrs · 17,161 cycles

EMERGENCY AISLE LIGHT AT SEAT ROW 3 RIGHT FAILED TO ILLUMINATE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 14,462 hrs · 5,690 cycles

FUSELAGE SKIN EXTERNAL DOUBLER BS 1825, RT STR 23-25. REPAIRED AMX-MEX-98-0005TR & AMX-MEX-98-0004RR DATED 13 JAN 98.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 14,462 hrs · 5,690 cycles

FUSELAGE SKIN FLUSH REPAIR BS 1613, RT STR 20-21. REPAIR SRM 53-00-01 FIG 206 FIG 201 REPAIR 5.