N675DL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,205 hrs · 43,778 cycles

SHIP 0675 R FWD ENT DOOR WAS DISPLAYED ON EICAS ON FINAL APPROACH. CORRECTIVE ACTION: CLEANED/LUBE DOOR WARNING SENSOR. DOOR WARNING SYSTEM TEST I.A.W. B757 AMM 52-71. CHECKS GOOD AT THIS TIME. A/C OK FOR SVC. (4269874)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,161 hrs · 43,747 cycles

SHIP 0675 -FCNT/DE- DUE TO TRAILING EDGE ASYM MESSAGE. CORRECTIVE ACTION: REPLACED RIGHT FLAP POSITION TRANSMITTER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,028 hrs · 43,651 cycles

SHIP 675 ROW 24 EMERGENCY LIGHT LENS MISSING. CORRECTIVE ACTION: REMOVED AND REPLACED ROW 24 EMERGENCY ESCAPE PATH LIGHT IN REFERENCE TO B757 AMM 33-51. OPS CHECK GOOD. (4552694)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,991 hrs · 43,628 cycles

SHIP 0675 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS 4L SLIDE LIGHT INOPERATIVE. CORRECTIVE ACTION: REMOVED DEBRIS FROM DOOR SILL. SLIDE LIGHT OPS CKS GOOD. REF B757 AMM 25-66. OK FOR SERVICE. (0025211)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,718 hrs · 43,440 cycles

SHIP 0675 2L SLIDE LIGHT INOP AFTER PUSHBACK. RESET 2L SLIDE SYSTEM PER MCC DIRECTION. RESET SUCCESSFUL. SYS OPERATING NORMALLY. CORRECTIVE ACTION: INFO NOTED NO 2 DAY HISTORY SYSTEM CHECKS GOOD AT THIS TIME A/C OK FOR SVC. (9588682)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,713 hrs · 43,435 cycles

SHIP 0675 3L DOOR ARM LIGHT NOT ILLUMINATING PER FLIGHT ATTENDANT. CORRECTIVE ACTION: REPOSITIONED LANDYARD PER B757AMM 52-22. (9588672)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,991 hrs · 42,974 cycles

SHIP 675 RIGHT WING TIP AFT POSITION LIGHT ACCESS DOOR AND STATIC WICK MISSING UPON ARRIVAL. CORRECTIVE ACTION: ACCOMPLISHED SECTION I TIME LIMITED ALTERATION OF ER/A 609040-14 REV. ORIGINAL. R/R RIGHT WINGTIP PANEL, MONITOR CLEARED. REF N757 AMM 57-31. (9724946)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,827 hrs · 42,885 cycles

SHIP 675 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:602. CORRECTIVE ACTION: INSPECTED FOUND ALL DOOR EMERGENCY LIGHTS OPERATIONAL. (2745684)

Part: ARM — DAMAGED (GIRT BAR) · airframe 92,830 hrs · 42,283 cycles

SHIP 675 L2 DOOR WAS DIFFICULT TO OPEN. CORRECTIVE ACTION: AFT GIRT BAR ROTATING ARM UPPER FITTING BROKEN. PINNED L2 DOOR SLIDE, RMVD GIRT BART FROM GIRT BAR CARRIER. RMVD L2 DOOR SLIDE PER AMDS. RMVD AND INSTALLED NEW UPPER BEARING ARM AND ROD FOR AFT GIRT BAR ROTATING ARM IAW B757 AMM 52-11. GIRT BAR ROTATING ARMS CHECK NORMAL. RE-INSTALLED L2 DOOR SLIDE IAW JOB CARD. (9732102)

Part: NONE — NONE · airframe 92,476 hrs · 42,019 cycles

SHIP 0675 - ATB - DUE TO ELECTRICAL SMELL IN THE CABIN. CORRECTIVE ACTION: PERFORMED ENG WATER WASH ON THE LT AND RT ENG. INSPECTED CABIN FOR ELECTRICAL SMELL. REPLACED LT AND RT RECIRC FILTERS. C/W DUCT BURNOUT.

Part: NONE — NONE · airframe 92,474 hrs · 42,017 cycles

SHIP 675 - DIV - TO CVG DUE TO LOSS OF RIGHT ENGINE GENERATOR WITH APU ON MEL. CORRECTIVE ACTION: REPLACED GCU AND RT IDG, LK CK AND OPS CHECK GOOD. APU REPLACED.

Part: NONE — NONE · airframe 92,446 hrs · 41,996 cycles

SHIP 675 2L DOOR ARMING LEVER WILL NOT ARM. CORRECTIVE ACTION: ADJUSTED GIRT BAR AND LUBED. CKS GOOD. (9030164)

Part: NONE — NONE · airframe 92,194 hrs · 41,806 cycles

SHIP 675 - ATB- DUE TO TRAILING EDGE FLAP ISSUES. CORRECTIVE ACTION: CONFIRMED FAULT. REPLACED FLAP/SLAT DEPRESSURIZATION MODULE. C/W NOGO PROCEDURES.

Part: NONE — NONE · airframe 92,185 hrs · 41,798 cycles

'SUPPLIMENTAL INFORMATION' SHIP 675 2 LT DOOR KNUCLE KNOKER INTERMITTENT. CORRECTIVE ACTION: REMOVED ROCKER PANEL PER B757 AMM 52-11 INSTALLED RETAINING HARDWARE ON BACK OF PANEL REF AMM 25-00-00. INSTALLED ROCKER PANEL PER B757 AMM 52-11. OPS CHK GOOD.(8996220)

Part: NONE — NONE · airframe 92,029 hrs · 41,666 cycles

SHIP 675 LT AFT DOOR KNUCKLE ARMED INDICATOR WILL NOT COME OUT WHEN ARRMED. CORRECTIVE ACTION: TRIMMED AND CLEANED UP ROUGH SPOT ON DOOR COVER THAT WAS CATCHING ON KNUCKLE KNOCKER AT L4 DOOR. OPERATES NORMAL. (9166344)

Part: INDICATOR — DIRTY · airframe 92,014 hrs · 41,654 cycles

SHIP 675 L3 GIRT BAR KNUCKLE KNOCKER FLUSH. CORRECTIVE ACTION: CLEANED DEBRIS AND CW OPS CK PER B757 AMM 52-10.

Part: GIRT BAR — OUT OF ADJUST · airframe 91,988 hrs · 41,640 cycles

SHIP 675 2L DOOR GIRT BAR WILL NOT ENGAGE AND FALLS OFF. CORRECTIVE ACTION: ADJUSTED L2 DOOR GIRT BAR FWD MECHANISM IAW B757 AMM 52-11, OP CHECK GOOD. (9166310)

Part: PROXIMITY SENSOR — INOPERATIVE · airframe 91,979 hrs · 41,632 cycles

SHIP 675 2L DOOR SLIDE LIGHT @ 2L LOCATION INTERMITTENT. CORRECTIVE ACTION: REPLACED L2 DOOR GIRT BAR PROX SENSOR S10218 PER B757 WDM 25-66-11 ADJUSTED GIRT BAR MECHANISM REF B757 AMM 52-11-25, OPS CHECK GOOD. (8739590)

Part: LINER — OUT OF ADJUST · airframe 91,966 hrs · 41,617 cycles

SHIP 675 2L CABIN DOOR WHEN ARMED, KNUCKLE KNOCKER DID NOT FULLY EXTEND. CORRECTIVE ACTION: ADJUSTED L2 DOOR LINER PER B757 AMM 52-11 OPS CHECK GOOD. (8739577)

Part: DRAG FITTING — CORRODED · corrosion level 2 · airframe 91,955 hrs · 41,608 cycles

SHIP 675 [AD / AA] LH ENG DRAG FTG HOLES NBR 1 TO 10 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #1, CORROSION ON SKIN AND FITTING BTW 2-3 CLOCK POS ; HOLE #4, CORROSION ON SKIN 9 CLOCK POS ; IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00100: HOLES #1 AND #4 WERE REPAIRED PER PRI 588586-14 REV. 7 AND ER/A 588586-14AD REV. B SECTION VI. (2271077)

Part: DRAG FITTING — CORRODED · corrosion level 2 · airframe 91,955 hrs · 41,608 cycles

SHIP 675 A.D.// A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #12 CORROSION BTW SKIN BTW 2 TO 4 AND 6 OCLOCK POSITION ; HOLE #16 CORROSION BTW SKIN BTW 11 TO 12 OCLOCK POSITION. IN REF. CARD 5720-01100-05B JOB#015- 0001 STEP 14.C. CORRECTIVE ACTION: SUMMARY OF NRC 00061 HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE HOLE #12 AND HOLE #16 WAS REPAIRED PER . ER/A 588617-14AD REV B SECTION V. (2271316)

Part: DRAG FITTING — CORRODED · corrosion level 2 · airframe 91,955 hrs · 41,608 cycles

SHIP 675 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON SKIN AND FITTING BTW 2 AND 6 OCLOCK POSITION; HOLE #2, CORROSION BTW 2 TO 3 O?CLOCK POSITION ON BUSHING INSTALLED AT SKIN AND CORROSION ON FITTING AT 9 OCLOCK POSITION; HOLE #3 CORROSION BTW 8 TO 12 O?CLOCK POSITION ON BUSHING INSTALLED ON SKIN; HOLE #4 CORROSION ON SKIN AND FITTING BTW 7 TO 11 O?CLOCK POSITION; HOLE #5 CORROSION ON FITTING AT 6 OCLOCK POSITION; HOLE #8 CORROSION ON SKIN BTW 8 TO 10 OCLOCK POSITION; HOLE #10 CORROSION ON SKIN AND FITTING BTW 5 TO 6 OCLOCK POSITION AND CORROSION ON FITTING BTW 3 TO 4 OCLOCK POSITION, IN REF. CARD 5720-01100-04B. JOB # 106-0001 STEP 14. C. CORRECTIVE ACTION: SUMMARY OF NRC 00060: DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1, HOLE #2, HOLE #3, HOLE #4, HOLE #5, HOLE #8 AND HOLE #10 WERE REPAIRED PER ER/A 588617-14AD REV B; SECTION VI. (2271257)

Part: DRAG FITTING — CORRODED · corrosion level 2 · airframe 91,955 hrs · 41,608 cycles

SHIP 675 [AD / AA] LH ENG DRAG FTG HOLES NBR 11 TO 18 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #16, CORROSION ON SKIN AND FITTING BTW 7-8 CLOCK POS. IN REF TASK CARD 5720-01100-05A JOB #105-0001 STEP 14.B. CORRECTIVE ACTION: SUMMARY OF NRC 00101: HOLE #16 WAS REPAIRED PER PRI 588586-14 REV. 7 AND ER/A 588586-14AD REV. B SECTION VI. (2271084)

Part: WEDGE — DEBONDED · airframe 91,955 hrs · 41,608 cycles

SHIP 675 A.A. - A.D. DEBONDED (1.200IN X 1.000IN) ON ISS 248.6, UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING DEBOND ( 1.200IN X 1.000IN) ON ISS 248.6, UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING WAS REPAIRED PER B 757-200 SRM. (2250111)

Part: PAN — CORRODED · corrosion level 2 · airframe 91,955 hrs · 41,608 cycles

SHIP 675 CORROSION ON AFT LAVATORY PAN AT FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00018. AFT LAVATORY PAN WAS REPLACED PER B757-200 SRM. (2249774)

Part: NONE — NONE · airframe 91,955 hrs · 41,608 cycles

SHIP 675 ERA 502438-14 DENT WAS FOUND ON FUSELAGE SKIN PANEL OF SKIN INSTALLATION LOCATED NEAR STA 1661 BETWEEN S-21L AND S-22L. CORRECTIVE ACTION: REF ERA 502438-14 REV B.

Part: SKIN — NONE · airframe 91,945 hrs · 41,605 cycles

SHIP 675 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588586-14AD REV.A. CORRECTIVE ACTION: REF ERA 588586-14AD REV A. (2225378)

Part: SKIN — NONE · airframe 91,988 hrs · 41,640 cycles

SHIP 675 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588586-14AD REV.A. CORRECTIVE ACTION: REF ERA 588586-14 REV B. (2225380)

Part: NONE — NONE · airframe 91,226 hrs · 41,156 cycles

SHIP 675 AFT LIFE RAFT MISSING GUAGE. CORRECTIVE ACTION: REPLACED AFT LIFE RAFT REF B757 AMM 25-64-00. (8185064)

Part: NONE — NONE · airframe 91,190 hrs · 41,136 cycles

SHIP 675 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:507. CORRECTIVE ACTION: RESECURED CHKS GOOD. (2033689)

Part: NONE — NONE · airframe 91,173 hrs · 41,127 cycles

SHIP 675 SEAT 23 D EMERGENCY PATH LIGHTING INOP. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 23D PER B757 AMM 33-51. OPS CHECK GOOD. (8185027)

Part: ENGINE — FAULTED (RIGHT) · airframe 91,004 hrs · 41,046 cycles

SHIP 675 N CLIMB OUT ACCELERATING THROUGH 180 KNOTS, WHILE RETRACTING FLAPS FROM FL5 FL1 THE AIRCRAFT ROLLED AND SLIGHTLY YAWED RIGHT CONSISTENT WITH A MOMENTARY WAKE TURB ENCOUNTER THERE WAS ALSO A BANG NOISE ASSOCIATED WITH THIS EVENT BUT DIFFICULT TO DISCERN IF IT WAS A BIRD IMPACT OR ENGINE NOISE. PAX IN 39 DEF ALSO REPORTED SMALL FIRE BALL AND "STEAM" MOMENTARILY EMINATING FROM THE RIGHT ENGINE EXHAUST AREA. ALL ENGINE PARAMETERS REMAINED NORMAL WITH NO NOTED FLUCTUATIONS THROUGHOUT THIS EVENT. CORRECTIVE ACTION: PERFORMED BIRD STRIKE INSPECTION PER B757 FIM 71-05, NO FINDINGS. PERFORMED B757 FIM TASK 71-05 DUE TO WAKE TURBULENCE. C/W ERA 595307-14 REV ORIG SECTION I AND SECTION II PART 1. R/R @2 ENG MAIN OIL FILTER PER B757 AMM 79-21. NO ABNORMAL NOTED. (8195564)

Part: NOT REPORTED — NOT REPORTED · airframe 90,872 hrs · 40,969 cycles

SHIP 675 - MISC/DE - LEFT HYDRAULIC SYSTEM QUANTITY DECREASED AFTER TAKEOFF. COMPLIED WITH QRH AND CONTINUED TO DESTINATION. CREW DECLARED EMERGENCY (OPS DECISION) DURING APPROACH. CORRECTIVE ACTION: INSPECTED PTU RELATED HYDRAULIC FILTERS. REPLACED HYDRAULIC LINE IN PYLON AREA.

Part: NONE — NONE · airframe 90,861 hrs · 40,965 cycles

SHIP 675 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588617-14 REV A. CORRECTIVE ACTION: REF 588617-14 REV A. (1984206)

Part: LAMP — INOPERATIVE (L4 DOOR SLIDE) · airframe 90,409 hrs · 40,773 cycles

SHIP 675 EMERGENCY EXIT SLIDE LIGHT DOOR 4 LT INOP. CORRECTIVE ACTION: RELAMPED AND CLEANED SOCKET FOR LAMP PER B757 AMM 33-51. (8008619)

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 90,441 hrs · 40,782 cycles

SHIP 675 EMERGENCY EXIT SLIDE LIGHT DOOR 4 RT INOP. CORRECTIVE ACTION: RELAMPED AND CLEANED SOCKET FOR LAMP PER B757 AMM 33-51. (8008618)

Part: WINDSHIELD — FAILED (L1) · airframe 90,398 hrs · 40,765 cycles

SHIP 675 OUTER WINDSHIELD PANE SHATTERED AT FL 390. C/W QRH. CORRECTIVE ACTION: REMOVED AND REPLACED CAPT'S #1 WINDSHIELD IAW B757 AMM. (8008608)

Part: MECHANISM — BROKEN (L1 DOOR) · airframe 90,398 hrs · 40,765 cycles

SHIP 675 IL DOOR SLIDE ENGAGEMENT LIMIT IS INOP. CORRECTIVE ACTION: FOUND BROKEN DOOR MECHANISM (260397) REPLACED L1 DOOR CRANK PER 757 CMM 52-11. (7845298)

Part: SLIDE — MISINSTALLED (L1 DOOR) · airframe 90,261 hrs · 40,715 cycles

SHIP 675 L-1 DOOR SLIDE NOT INSTALLED CORRECTLY. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 006-0004:2020-2367-1R/003 00020 RE POSITIONED GIRT UNDER HARNESS AND REMOVED ESCAPE SLIDE PIN REF B757 AMM 25-66. (1891864)

Part: PLACARD — DETACHED (L1 DOOR) · airframe 90,200 hrs · 40,683 cycles

SHIP 675 L1 DOOR PLACARD INSIDE ARMING LEVER FELL OFF INSIDE DOOR HINGE. CORRECTIVE ACTION RE-SECURED FOR ARMING LEVER ON L1 DOOR. (LP 7845234)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,188 hrs · 40,674 cycles

SHIP 675 EMERGENCY LIGHTS IN AFT GALLEY AT 4L & 4R DOORS INOP. CORRECTIVE ACTION: REPLACED CHARGER & BATTERY M736 PER B757 AMM 33-51-07. CKS OK. (7845224)

Part: COVER — MISSING (RT AFT DOOR) · airframe 90,194 hrs · 40,679 cycles

SHIP 675 AFT RT DOOR HANDLE COVER MISSING. CORRECTIVE ACTION: INSTALLED MISSING DOOR HANDLE COVER PER B757 AMM 52-11. (1871243)

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 90,114 hrs · 40,628 cycles

SHIP 675 L2 PASSENGER DOOR WILL NOT ARM/DISARM. REMOVED DEBRIS ARM/DISARM DOOR SEVERAL TIMES OPS CHK GOOD LUBE GIRT BAR FLOOR FITTING PER B757 AMM 12-21. (6008194)

Part: INSERT — STRIPPED (L4 GIRT BAR) · airframe 89,739 hrs · 40,453 cycles

SHIP 675 DURING L4 SLIDE CHANGE FOUND GIRT BAR INSERTS STRIPPED OUT. CORRECTIVE ACTION: REMOVED L4 DOOR SLIDE GIRT BAR PER AMDS W/C. INSTALLED GIRT BAR PER AMDS W/C. (7773003)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,474 hrs · 40,346 cycles

SHIP 675 DURING S/C FOUND AFT GALLEY CEILING EMERGENCY EXIT SIGN LIGHT UP MOMENTARILY. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY AT SLED M736 IN AFT GALLEY CEILING IAW B757 AMM 33-51. CKS GOOD. (7589390)

Part: FSEU — INOPERATIVE (TE FLAP) · airframe 89,467 hrs · 40,340 cycles

SHIP 675 - MISC/DE- TE FLAP DISAGREE ON APPROACH WHEN SELECTING FLAPS 15. / CORRECTIVE ACTION: T/S PER B757 FIM 27-51. RAN FLAPS, NO BINDING. CK FLAP TRANSMISSION TORQUE LIMITERS, NOTE TRIPPED PER B757 FIM 27-51. ALL FLAP TRACK ROLLERS IN SERVICEABLE CONDITION, BALL SCREW TRANSFER TUBES NOT LIFTING. LUBED FLAPS PER B757 AMM 12-21. CK ADJUSTMENT OF LT AND RT POSITION XMTR, FLAP PDU XMTR AND FLAP CONTROL LEVER XMTR PER B757 AMM 27-51. FSEU 1 REPLACED.

Part: SENSOR — OUT OF ADJUST · airframe 89,469 hrs · 40,342 cycles

SHIP 675-MISC/DE L/E SLAT ASYMMETRY INDICATION. CORRECTIVE ACTION: T/S PER B757 WDM 27-81 POSSIBLE SHORT AT APPROX. 37 FT FROM CONNECTOR D41828P. REPLACED WIRE W4218-0002-22 FROM D42340J TO D41828. PERFORMED FSEU 1 AND 2 BITE NO FAULTS NOTED. PERFORMED FLAPS OPS TEST PER B757 AMM 27-51, OPS NML. C/W FLAP SLAT HEALTH CK PER W/C, ALL WITHIN LIMITS. PERFORMED ADJUSTMENT TEST OF INBD/OTBD L/E SLAT LOSS SENSOR PER B757 AMM 27-81 ALL CHECKS GOOD.

Part: DRAG FITTING — DAMAGED (ENGINE MOUNT) · airframe 88,556 hrs · 40,049 cycles

WHILE PERFORMING INSPECTION MAINTENANCE FOUND THE NR 1 ENGINE DRAG FITTING NR 4 OPEN HOLE HAS (1) INDICATION OF DEFECTS NOTED INDICATION IS IN THE FITTING AT THE 9 O'CLOCK POSITION JUST BELOW THE CENTER SHIM LOOKING AFT. REPAIRED PER ERA 588586- 14.

Part: DRAG FITTING — DAMAGED (ENGINE MOUNT) · airframe 88,556 hrs · 40,049 cycles

WHILE PERFORMING INSPECTION FOUND THE NR 1 ENGINE DRAG FITTING NR 2 OPEN HOLE HAS (2) INDICATIONS OF DEFECTS NOTED INDICATIONS ARE IN THE UPPER SKIN AT THE 11 AND 4 O`CLOCK POSITIONS JUST ABOVE THE CENTER SHIM LOOKING AFT. REPAIRED PER ERA 588586-14AD.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 88,551 hrs · 40,047 cycles

DURING INSPECTION MAINTENANCE FOUND A CRACK INDICATION AT LOWER INBOUND HOLE AT S-14R INTERCOSTAL. REPAIRED PER ER/A 588545-14AD.

Part: DRAG FITTING — CRACKED (RT NACELLE) · airframe 88,551 hrs · 40,047 cycles

DURING INSPECTION FOUND RIGHT HAND PYLON DRAG FITTING HOLE NUMBER 9 HAS TWO INDICATIONS OF CRACK LIKE DEFECTS IN THE FITTING AT THE 7 AND 5 O`CLOCK POSITIONS FACING AFT. C/W ERA 58617-14.

Part: DRAG FITTING — CRACKED (RT NACELLE) · airframe 88,551 hrs · 40,047 cycles

DURING INSPECTION FOUND RIGHT HAND SIDE PYLON DRAG FITTING HOLE NUMBER 2 INDICATION OF CRACK LIKE DEFECT FOUND IN THE UPPER SKIN AT THE 9 O`CLOCK POSITION FACING AFT. C/W ERA 588617-14.

Part: DRAG FITTING — CRACKED (RT NACELLE) · airframe 88,551 hrs · 40,047 cycles

DURING INSPECTION FOUND RIGHT HAND PYLON DRAG FITTING HOLE NUMBER 3 IN THE FITTING AN INDICATION OF A CRACK LIKE DEFECT WAS FOUND AT THE 6 O`CLOCK POSITION FACING AFT. C/W ERA 588617-14.

Part: SKIN — DAMAGED (LT AILERON) · airframe 88,551 hrs · 40,047 cycles

DURING INSPECTION MAINTENANCE FOUND LT AILERON HAS COMPOSITE DAMAGE ABOVE NR 5 HINGE FITTING. REPAIRED PER SRM.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 88,551 hrs · 40,047 cycles

DURING INSPECTION FOUND LEVEL 2 CORROSION ON LEFT SIDE FLOOR BEAM CORROSION AT STATION 377.7 LBL 62. REPLACED FLOOR STRAP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,551 hrs · 40,047 cycles

EMERGENCY LIGHT BATTERY PACKS (4 EA) NOT ILLUMINATING. CORRECTIVE ACTION: REPLACED BATTERIES 001 AT POSITION M730, M735 AND M10568. SYSTEM OPERATION IS NORMAL.

Part: NONE — NONE · airframe 91,955 hrs · 41,608 cycles

SHIP 675 ER/A 502440-14, REV A / SUPPLEMENTAL INSPECTIONS. CORRECTIVE ACTION: REF ERA 502440-14 REV A. (1544106)

Part: MECHANISM — OUT OF ADJUST (L2 DOOR) · airframe 88,522 hrs · 40,034 cycles

SHIP 675 2L DOOR KNUCKLE KNOCKER INOP ESCAPE SLIDE ARMED COND IND. CORRECTIVE ACTION: T/S PER AMM 52-11-20 TASK 825-001 PAR K *ADJUST RETRACTABLE DOOR MECHANISM* FOR ADJ/TEST OF CABIN DOOR KNUCKLE KNOCKER - CONTROL ROD. (1531993)

Part: INDICATOR — INOPERATIVE (L2 DOOR) · airframe 88,168 hrs · 39,874 cycles

(AIRCRAFT 675, L/P 6956082) 2L DOOR KNUCKLE KNOCKER NOT EXTENDED WHEN ARMED. CORRECTIVE ACTION: ADJUSTED KNUCKER KNOCKER INDICATOR.

Part: INDICATOR — OBSTRUCTED (L2 DOOR) · airframe 88,146 hrs · 39,865 cycles

SHIP 675 ESCAPE SLIDE ARMED COND IND 2L. CORRECTIVE ACTION: FOUND KNUCKLE KNOCKER INDICATOR BINDING ON DOOR LINER CUTOUT. REMOVED EXCESS PLASTIC ON CUTOUT. KNUCKLE KNOCKER INDICATOR OPS NORMAL. (1470200)

Part: LINER — OUT OF POSITION (L2 DOOR) · airframe 88,066 hrs · 39,830 cycles

L2 DOOR ESCAPE SLIDE ARMED COND INDICATOR, KNUCKLE KNOCKER NOT FULLY VISIBLE WHEN ARMED. ADJUSTED THE DOOR LINER.

Part: UNKNOWN — ODOR (CABIN) · airframe 87,837 hrs · 39,735 cycles

VERY STRONG DIRTY SOCK SMELL IN COCKPIT. STARTED IN CLIMB, FADED IN CRUISE AND STRONG AGAIN IN DESCENT.

Part: FITTING — MISSING (GIRT BAR) · airframe 86,852 hrs · 39,266 cycles

DURING GIRT BAR LUBE - FOUND R4 DOOR MISSING 1 FWD DOOR STOP FITTING. INSTALLED DOOR STOP FITTING BEARING PLATE IAW B757 AMM 52-11-00.

Part: ARMING LEVER — OBSTRUCTED (DOOR) · airframe 85,932 hrs · 38,825 cycles

(AIRCRAFT 675, L/P 1067442) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. DISARM LEVER IS STIFF. REMOVED DEBRIS FROM DOOR SILL AREA, KNUCKLE KNOCKER WORKS NORMALLY AND ARM/DISARM LEVER WORKS FREELY, REF AMM 52-11. OK FOR SVC.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 84,559 hrs · 38,216 cycles

SHIP 675 MID DOOR EXIT LIGHT COVER FELL OFF. CORRECTIVE ACTION: REINSTALLED LIGHT COVERS. (4593733)

Part: BEARING — CORRODED (LT MLG TRUNNION) · airframe 84,441 hrs · 38,171 cycles

(AIRCRAFT 675, L/P 0826556) RT MLG FWD TRUNNION BEARING HAS CORROSION ON INTERIOR SURFACE. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0003:3210-9901-RT/001 00004 REPLACED BEARING PER B757 AMM 57-54-05.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,316 hrs · 38,100 cycles

R4 OVER DOOR EXIT SIGN, L4 LWR FWD EXIT SIGN AND 4 LAST ROWS SEAT MOUNTED EXIT LIGHTS INOP. FOUND BATTERY PACK M736 AT FAULT. REPLACED BATTERY PACK PER AMM 33-51. ALL EMERGENCY LIGHTS AND SIGNS NOW CKS GOOD.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 83,525 hrs · 37,760 cycles

DURING BORESCOPE INSPECTION OF ESN 16445, FOUND ONE 3RD STAGE LPT BLADE WITH SULFIDATION, APPARENT LOSS OF MATERIAL AND CORROSION GROWTH THROUGH THE BLADE. PER AMM 72-00-00-803-POO. THIS CONDITION REQUIRES THE ENGINE TO BE CHANGED. THE NR 1 ENGINE S/N 16445 HAS BEEN REPLACED REF 7100-9902E-01. TRANSFERRED DISCREPANCY TO ENGINE HISTORY.

Part: ATTACH ANGLE — BROKEN (FUSELAGE) · airframe 83,190 hrs · 37,648 cycles

BULK CARGO FLOOR STRUCTURE MAIN FRAME LOWER END ATTACH ANGLE IS BROKEN BS 1620 RBL 3.0 (VIEW FROM AFT SIDE). CUT OUT DAMAGED SECTION AND REPAIRED BULK CARGO FLOOR STRUCTURE MAIN FRAME LOWER END ATTACH ANGLE AT STA 1620 RBL 3 IAW ERA 567757-14 REV ORIGINAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,190 hrs · 37,648 cycles

CORROSION ON THE BULK CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT INTERCOSTAL LOWER SURFACE BETWEEN BS 1600 TO BS 1620 RBL 3.0. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02 AND DRW 146N5436 REV B, PART HEAT TREAT FROM "0" CONDITION TO T6 IAW AMS 2770.

Part: SPRING — BROKEN (GIRT BAR) · airframe 83,191 hrs · 37,649 cycles

R4 DOOR GIRT BAR LEAF SPRING BROKEN. REMOVED AND REPLACED GIRT BAR AT R4 DOOR IAW AMM 25-66-10. ADJUSTMENT ACCOMPLISHED ON 2040-0057-4R STEP 14.

Part: SERVICE PANEL — CORRODED (LAV SERVICE) · airframe 83,191 hrs · 37,649 cycles

AFT LAV SERVICE PANEL 149GL CORRODED ON INNER SURFACE. REPAIRED AFT SERVICE PANEL IAW ERA 567764-14 REV ORIGINAL.

Part: FRAME — CRACKED (BS 1681) · airframe 83,190 hrs · 37,648 cycles

MAIN CABIN, FRAME, BS 1681, 2 INCHES ABOVE THE FLOOR CUSP WEB, A CRACK INDICATION AT THE FRAME WEB. REPAIRED THE FRAME IAW ER/A 567749-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1681) · airframe 83,190 hrs · 37,648 cycles

MAIN CABIN LT FRAME, BS 1681, 2 INCHES ABOVE FLOOR CUSP WEB, HAD A CRACK INDICATION. REPAIRED THE FRAME IAW ER/A 567750-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 460) · airframe 83,190 hrs · 37,648 cycles

PASSENGER CABIN BS 460 FRAME WAS CRACKED BETWEEN STRINGERS 12L AND 13L. ACCOMPLISHED A FRAME REPAIR IAW ERA 567751-14, REV ORIG.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 83,190 hrs · 37,648 cycles

CORROSION FOUND O THE CARGO FLOOR PANEL. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS, IAW ERA 491157-14MA STEP 1 REV A.

Part: FLOOR SUPPORT — CORRODED (BS 1620-1625) · corrosion level 2 · airframe 83,190 hrs · 37,648 cycles

CORROSION FOUND ON THE BULK CARGO FLOOR SPPORTTWEEN BS 1620 AND 1625, RBL. 7.5. REMOVED, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 53-00-04, 51-40-02, AND DWG 146N5451.

Part: STRINGER CLIP — CRACKED (BS 1520) · airframe 83,190 hrs · 37,648 cycles

STRINGER CLIP CRACKED, BS 1520, STRINGER 24L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — DAMAGED (BS 1681) · airframe 83,190 hrs · 37,648 cycles

BS 1681, STRINGER CLIP 21L WAS DAMAGED. REMOVED, FABRICATED AND INSTALLED A NEW STRINGER CLIP IAW SRM 51-40-02, DWG 146N8712, REV K, AND 140N2001, REV BN.

Part: STRINGER CLIP — DAMAGED (BS 1681) · airframe 83,190 hrs · 37,648 cycles

BS 1681, STRINGER CLIP 22L WAS DAMAGED. REMOVED, FABRICATED, AND INSTALLED A NEW STRINGER CLIP IAW SRM 51-40-02, DWG 146N8712, REV K, AND 140N2001, REV BN.

Part: SHEAR TIE — CRACKED (BS 1400) · airframe 83,190 hrs · 37,648 cycles

MAIN CABIN SHEAR TIE WAS FOUND CRACKED, BS 1400, RBL 58.22. REMOVED, FABRICATED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02, AND DWG 140N2002, REV EU.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,190 hrs · 37,648 cycles

MAIN CABIN INTERCOSTAL CLIP HAS CORROSION @ BS 984 AND S17L. REMOVED AND REPLACED MAIN CABIN INTERCOSTAL CLIP AT BS 984, S17L IAW SRM 53-40-13, 51-30-01, 51-40-02, AND DWG 144N5158 REV- .

Part: ANGLE — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 83,190 hrs · 37,648 cycles

CORROSION ON MAIN CABIN CREASE BEAM ANGLE BETWEEN BS 1020 - 1040 RT SIDE. REMOVED AND REPLACED CREASE BEAM ANGLE, FROM BS 900 - 1040 IAW SRM 51-10-02, 51-40-02, 51-40-05, 51-20-01, AMM 20-60-02, 51-21-00, AND DWG 144N5140, REV C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,190 hrs · 37,648 cycles

MAIN CABIN LEFT OUTBOARD SEAT TRACK CORROSION DAMAGE FOUND OUT LIMITS FROM STA 790 TO 900. REMOVED AND REPLACED MAIN CABIN LEFT O/B SEAT TRACK FROM STA 790 TO 900 IAW SRM 51-40-05, 51-40-02 AND SRM 53-30-52.

Part: INTERCOSTAL — CORRODED (BS 960-984) · corrosion level 2 · airframe 83,190 hrs · 37,648 cycles

MAIN CABIN INTERCOASTAL HAS CORROSION BETWEEN BS 960 & 984, STRINGER 17L. REMOVED, FABRICATED AND INSTALLED A NEW MAIN CABIN INTERCOSTAL IAW SRM 53-40-13, 51-10-02, AND DWG 144N5140, REV D.

Part: DOUBLER — NOT REPORTED · airframe 86,182 hrs · 38,949 cycles

C/W PRI 565911-14 REV O (EXISTING GPS ANTENNA DOUBLER). COMPLIED WITH ER/A 565911-14 REV O.

Part: LAMP — INOPERATIVE (INDICATOR) · airframe 82,436 hrs · 37,345 cycles

R1 DOOR SLIDE DOES NOT ILLUMINATE. REPLACED THE LAMPS IN THE INDICATOR.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 82,415 hrs · 37,336 cycles

L2 DOOR OVERHEAD EMERGENCY EXIT COVER MISSING 2 EA DIFFUSER LENSES. REPLACED L2 DOOR EMERGENCY LIGHT LENS PER AMM 33-51.

Part: DOOR — FROZEN (L3) · airframe 82,134 hrs · 37,241 cycles

(AIRCRAFT 675, L/P 3562812) L3 DOOR WILL NOT DISARM. T/S, FOUND DOOR TO BE FROZEN, THAWED FLOOR AREA, DOOR OP'S / NORMAL.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 81,105 hrs · 36,905 cycles

FLAPS BINDING ON APPROACH. LUBRICATED LEFTT AND RIGHT FLAPS, FOUND WATER IN NR 06 TRANSMISSION IAW AMM 12-21. CHECKED ADJUSTMENT OF LT & RT POSITION TRANSMITTERS, FLAP PDU TRANSMITTER, AND FLAP CONTROL TRANSMITTER IAW AMM 27-58 WITH PESU-40. DURING NORMAL FLAP TRAVEL, FOUND RT INDICATOR NEEDLE STALLING INTERMITANTLY. REPLACED THE RT FLAP TRANSMITTER AND INDICATOR IAW AMM 27-58. FLAPS OP NORMAL.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,011 hrs · 36,875 cycles

DURING LIGHT CHECK, FOUND THE OVERWING HANDLE EMERGENCY LIGHTS INOPERATIVE. REPAIRED IAW WDM 33-51-13. OPS CHECKED NORMAL.

Part: SIGN — UNSECURE (ROW 26) · airframe 80,614 hrs · 36,750 cycles

EXIT SIGN FROM OVERHEAD ROW 26 UNSECURE. SECURED THE EXIT SIGN AT ROW 26. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,023 hrs · 36,578 cycles

ROWS 4, 5, 15, AND 16 EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT EMERGENCY LIGHTING SYSTEM IAW WDM 33-51-21, PAGE 9B, SHT 1. FOUND M732 POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51. EMERGENCY LIGHTING SYSTEM OPS TESTED GOOD IAW AMM 33-51.

Part: FRAME — CORRODED (BS 1480) · corrosion level 2 · airframe 79,858 hrs · 36,519 cycles

FASTENER HOLE DAMAGED ON FRAME AT BS 1480, STRINGER 26R. REPAIRED IAW PRI555775-14 REV 3 AND COMPLIED WITH ERA 555775-14 REV ORIG.

Part: SHEAR TIE — CORRODED (BS 880) · corrosion level 2 · airframe 79,858 hrs · 36,519 cycles

DURING INSPECTION OF THE INTERNAL FUSELAGE, CORROSION WAS FOUND ON THE SHEAR TIE, BS 880, STRINGER 30 JUST AFT OF GROUND AIR CONNECTION. REPAIRED THE SHEAR TIE IAW DWG 140N2002 AND SRM 53-30-07.

Part: GROUND STUD — LOOSE (BS 395) · airframe 79,858 hrs · 36,519 cycles

GROUND STUD LOOSE LOCATED AT BS 395. TORQUED GROUND STUD IAW AMM 20-11-00.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 79,858 hrs · 36,519 cycles

ELONGATED HOLE, STA 540 S-5L AT STRINGER CLIP. REPAIRED REF SRM.

Part: FRAME — DENTED (FUSELAGE) · airframe 79,858 hrs · 36,519 cycles

AFT CARGO, STA 1600, LT FRAME, BELOW S-27, DENTED. REMOVED DAMAGE ON STA 1600 ABOVE STR 27 L/H (1.3" X .080" TRIMOUT) AND REPAIRED IAW SRM 53-00-07 REPAIR 5 ID REPAIR IAW PS 900-5-1 NR 4.

Part: ARM — WORN (L2 DOOR) · airframe 77,459 hrs · 35,255 cycles

L2 DOOR WILL NOT ARM, FOUND LIFTING ARMS WORN AND ALLOWING GIRT BAR TO COME INBD TOO FAR WHICH CAUSES GIRT BAR SLIDERS TO CONTACT FLOOR FITTINGS BOTH FOWARD AFT JAMMING ARMING PROCEDURES. REPLACED DAMAGED FWD AND AFT GIRT BAR LIFTER ASSY'S AND RIGGED IAW AMM 52-11-501, DOOR OP'S CK GOOD. RII C/W.

Part: BRACKET — LOOSE (LT WING TE FLAP) · airframe 77,419 hrs · 35,233 cycles

LEFT INBD FLAP, OTBB FLAP TRACK FAIRING, FWD INBD MOUNT BRACKET IS LOOSE. REPAIRED LT INBD FLAP, OTBD FLAP TRACK FAIRING, FWD INBD MOUNT BRACKET IAW ER/A 544311-14, REV'S 0-2.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 77,419 hrs · 35,233 cycles

AFT CARGO BAY FLOOR STRUCTURE BS 1500-1520 HAS CORROSION UNDER NUTPLATES, 10 EACH ON 8 BEAMS, MARKED. CORROSION AT 12 EA LOCATIONS, LBL 2.9, 7.55, 10.45, RBL 2.9, 7.55 , 10.45 BS 1500-1520 ARE FOUND TO BE OUT OF LIMITS. ORIGINAL .063" REMAINING, .031" LOSS OF .032. REPAIRED 12 EA LOCATIONS AS REQUIRED, REF: ERA, DAL 332525-14MA, REV D.

Part: SKIN — DENTED (BS 647) · airframe 77,419 hrs · 35,233 cycles

LOWER FUSELAGE BS 647 BETWEEN STR 25L-26L, SKIN HAS A PROTRUDING DENT. SMOOTHED OUT DAMAGE AND FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE AREA IAW SRM.

Part: BALL SCREW — CORRODED (RT WING TE FLAP) · airframe 77,419 hrs · 35,233 cycles

RIGHT OTBD T/E FLAP, INBD BALL SCREW, BALL NUTBUSHING SHAFTS ARE CORRODED. SCEPTRE ENTRY FOR REMOVED PART. WORK IN PROGRESS.BALL, SCREW & OFF 55-2754-9-0001 00107 ON. RT OTBD T/E FLAP. INBD BALLSCREW REPLACED ON CUSTOMER CARD 2751-2542.

Part: SKIN — CORRODED (BS 439-449) · airframe 77,419 hrs · 35,233 cycles

LOWER FUSELAGE BS 439-449 BETWEEN STR 29L-30L SKIN IS CORRODED AT FASTENERS AND TCAS ANTENNA DOUBLER. BLENDED CORROSION AND MATERIAL LOSS FOUND TO BE WITHIN LIMITS. (ORIG .080 REMAINING .076 LOSS .004). REF: B757-200 SRM 53-00-01 ALLOW DAM. 1 FIG 101, SHT 4, DETAIL II.

Part: ENGINE — FAILED (LEFT) · airframe 75,739 hrs · 34,552 cycles

AIR RETURN, DUE TO LT ENGINE SHUTDOWN. CREW REPORTED LOUD BANG FOLLOWED BY SMOKE IN THE COCKPIT AND OIL PRESSURE AND QUANTITY DROPPED TO ZERO. MAINTENANCE REPORTS CORE COWLS WET WITH OIL AND ZERO QUANTITY ON EICAS. ENGINE CHANGED AND DUCT BURNOUT PERFORMED.

Part: WIRE — FAILED (EMERGENCY LIGHT) · airframe 75,394 hrs · 34,406 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 30R. FOUND WIRE SECTION BAD AT SEAT 30R. REPLACED THE WIRED IAW SWPM. CHECKED GOOD. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 74,301 hrs · 33,952 cycles

EMERGENCY LIGHT INOPERATIVE AT MAIN CABIN SEAT ROW 32. TROUBLESHOOT AND FOUND BROKEN WIRE AT SEAT ROW 32. SPLICED WIRE IAW SWPM 20-30-12. PERFORMED TEST IAW AMM 33-51-00, TESTED OK.

Part: SKIN — DAMAGED (BS 1180) · airframe 74,227 hrs · 33,916 cycles

FUSELAGE, SKIN, BS 1180,S-9R TO S-10R, IN-FLIGHT DAMAGE, DTA STAGE III LIMIT. REPAIRED IAW ER/A 524269-14, REV A,

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 73,597 hrs · 33,610 cycles

EMERGENCY LIGHT AT ROW SEAT 24D INOPERATIVE. FOUND DAMAGED WIRE AT UNDERSEAT HARNESS CONNECTOR. REPAIRED IAW SWPM 20-30-12. OPS CHECKED OK.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,293 hrs · 33,476 cycles

SEAT 35DEF SEAT MOUNTED EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED SEAT WIRE HARNESS AND THE SEAT EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 72,933 hrs · 33,273 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 36 INOPERATIVE. REPAIRED BROKEN WIRE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 72,592 hrs · 33,100 cycles

AISLE EMERGENCY LIGHT INOPERATIVE AT 36D. FOUND CONNECTOR DISCONNECTED, RECONNECTED.

Part: SKIN — GOUGED (AFT CARGO DOOR) · airframe 72,483 hrs · 33,053 cycles

AFT CARGO DOOR EXTERIOR SKIN AFT LOWER CORNER, REPAIR DOUBLER GOUGED. REPAIRED IAW ERA502445-14, REV ORIG.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,483 hrs · 32,657 cycles

DURING SERVICE CHECK, FOUND RED EMERGENCY LIGHT AT MID LAVATORY INOPERATIVE. FOUND BROKEN WIRES AND REPAIRED IAW SWPM 20-30-12.

Part: SKIN — DAMAGED (BS 1160-1180) · airframe 71,450 hrs · 32,644 cycles

SKIN BS 1160-1180 S9-10R DAMAGED REPAIRED IAW SECTION I OF ER/A 524269-14.

Part: PLATE — CORRODED (R2 DOOR) · airframe 83,190 hrs · 37,648 cycles

R2 DOOR LOWER HINGE, UPPER CAMP PLATE CORRODED. REMOVED AND REPLACED THE CAM PLATE IAW ERA 476391-14MA, REV B, SECTION III.

Part: PLATE — CORRODED (R4 DOOR HINGE) · airframe 83,190 hrs · 37,648 cycles

R4 DOOR, LOWER HINGE, UPPER CAM PLATE CORRODED. REMOVED AND REPLACED UPPER CAM PLATE IAW ERA 476391-14MA, REV B, SECTION III.

Part: PLATE — CORRODED (L4 DOOR) · airframe 83,190 hrs · 37,648 cycles

L4 DOOR, LOWER HINGE, LOWER CAM PLATE CORRODED. REMOVED AND REPLACED THE CAM PLATE IAW ERA 476391-14MA, SECTION III, REV B.

Part: PLATE — CORRODED (L4 DOOR) · airframe 83,190 hrs · 37,648 cycles

L4 DOOR LOWER HINGE, UPPER HINGE PLATE CORRODED. REMOVED AND REPLACED THE L4 DOOR UPPER CAM HINGE PLATE IAW ERA 476391-14MA, REV B, SECTION III.

Part: PLATE — CORRODED (R2 DOOR) · airframe 83,190 hrs · 37,648 cycles

R2 DOOR LOWER HINGE, LOWER CAM PLATE CORRODED. REMOVED AND REPLACED THE CAM PLATE IAW ERA 476391-14MA, REV B, SECTION III.

Part: PLATE — CORRODED (R4 DOOR) · airframe 83,190 hrs · 37,648 cycles

R4 DOOR, LOWER HINGE, LOWER CAM PLATE CORRODED. REMOVED AND REPLACED R4 DOOR LOWER HINGE LOWER CAM PLATE IAW ERA 476391-14MA, REV B, SECTION III.

Part: SKIN — DENTED (BS 1661) · airframe 71,419 hrs · 32,627 cycles

FUSELAGE SKIN, BS 1661 S21-22L DENTED. REPAIRED IAW ER/A 502438-14, REV A.

Part: PUMP — FAILED (NR 1 HYD SYSTEM) · airframe 71,060 hrs · 32,476 cycles

CREW DECLARED AN EMERGENCY DUE TO NR 1 HYDRAULIC SYSTEM FAILURE. R & R LEFT ENGINE EDP IAW AMM 29-11.

Part: PANEL — DAMAGED (RT WING) · airframe 71,060 hrs · 32,476 cycles

COMPOSITE PANEL DAMAGED JUST FWD OF INBD SPOILER ON TOP OF RT WING. REPAIRED IAW ERA 524217-14, REV ORIGINAL.

Part: PANEL — DEPARTED (RT WING) · airframe 71,060 hrs · 32,476 cycles

F/A ADVISED A PANEL WAS MISSING FROM RT WING. HAD LT HYDRAULIC SYSTEM PRESSURE LOSS FOLLOWED BY TOTAL LT HYD FAILURE. RAN CHECKLIST AND LANDED WITH MANUAL FLAP AND GEAR EXTENSION. COMPLIED WITH PARTS DEPART ACFT INSPECTION IAW AMM 05-51. COMPLIED WITH TAP TEST OF HONEYCOMB PANEL ON LT WING ABOVE MLG BEAM IN WING ZONE 551, TWO PANELS AND ONE REMAINING PANEL ON RT WING IN ZONE 651 INBD OF PANEL THAT IS MISSING IAW NDT MANUAL 51-05-01. NO DAMAGE NOTED. DRILLED AND COUNTERSINKED REPLACEMENT PANEL IAW DWG. 113N1610. RESTORED FINISH.

Part: SKIN — DAMAGED (BS 1180) · airframe 71,450 hrs · 32,644 cycles

SKIN GOUGED IN A DENT FOUND AT BS 1180 BETWEEN STRINGERS 9-10R. REPAIRED IAW ERA 524227-14, REV A. SEC III.

Part: SKIN — DENTED (BS 1162-1168) · airframe 71,194 hrs · 32,534 cycles

SKIN DENTED AT BS 1162-1168 BETWEEN STRINGERS 9 - 10R. REPAIRED IAW ER/A 524227-14, REV ORIG AND ER/A 524269-14.

Part: DOOR — STUCK (R1) · airframe 69,396 hrs · 31,778 cycles

R1 DOOR WILL NOT ARM. REMOVED DEBRIS. DOOR OPS CHECKED NORMAL. OK FOR SERVICE.

Part: SNUBBER — DAMAGED (L1 DOOR) · airframe 67,415 hrs · 31,007 cycles

DOOR 1L OPENS ONLY HALF WAY. REMOVED DOOR 1L ACCESS PANEL 221AL OFF FOR T/S AFTER HEATING ROTARY SNUBBER DOOR 1L MOVES FREELY. R & R SERVICEABLE ROTORY SNUBBER IAW MM 52-11-10. REINSTALLED DOOR 1L ACCESS PANEL 221AL.

Part: BOTTLE — EMPTY (R4 DOOR ASSIST) · airframe 65,518 hrs · 30,175 cycles

DURING INSPECTION MAINTENANCE DISCOVERED R4 DOOR EMERGENCY DOOR ASSIST BOTTLE PRESSURE AT ZERO. REPLACED R4 DOOR ASSIST BOTTLE PER B757 AMM 52-11.

Part: SKIN — DENTED (BS 324 S18-19R) · airframe 65,309 hrs · 30,091 cycles

DURING INSPECTION MAINTENANCE DISCOVERED A DENT ON FUSELAGE SKIN AT BS 324 BETWEEN S18 AND19R. REMOVED DAMAGE AREA AND INSPECTED. NO DISCREPANCIES NOTED. FABRICATED REPAIR, INSTALLED AND TREATED AREA.

Part: SKIN — DENTED (BS 510) · airframe 69,887 hrs · 31,988 cycles

DURING HMV, FOUND A DENT IN FUSELAGE, SKIN, BS 510, S27-28L.

Part: CREASE BEAM — CORRODED (BS 1380-1400) · airframe 65,309 hrs · 30,091 cycles

CORRODED CREASE BEAM BS 1380-1400 RBL 70.5. REMOVED CORROSION ON CREASEBEAM WEB. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 PG1 3 DETAIL III. REMOVED CREASEBEAM IAW 51-40-02 PG31 FIG 8. INSTALLED CREASEBEAM WEB IAW SRM 51-40-02 PG7 AND PG21 FIG 4.

Part: CREASE BEAM — CORRODED (BS 996 RBL 70) · airframe 65,309 hrs · 30,091 cycles

CORRODED CREASEBEAM AT FS 996-1020 RBL 70.5, BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW CREASEBEAM WEB AND INSTALLED IAW B757 SRM 51-40-02 DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: CREASE BEAM — CORRODED (BS 1400-1420) · airframe 65,309 hrs · 30,091 cycles

CREASE BEAM EXFOLIATED AT BS 1400-1420 RBL 70.5. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED CREASE BEAM WEB REF SRM 51-40-02 PG 2.

Part: CREASE BEAM — CORRODED (BS 1440-1460) · airframe 65,309 hrs · 30,091 cycles

CREASEBEAM WEB CORRODED AT BS 1440-1460 RBL 70.5. BLENDED CORROSION ON CREASEBEAM WEB BS. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 PG 103 DETAIL III. REMOVED CREASEBEAM WEB IAW SRM 51-40-02 PG31 DETAIL I. INSTALLED CREASEBEAM WEB IAW SRM 51-40-02 PG21 FIG 4.

Part: STRINGER — CORRODED (BS 1445-1455) · airframe 65,309 hrs · 30,091 cycles

AFT CARGO STRINGER 28L CORRODED ON ALL SURFACES BS 1445-1455. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND REPLACED STRINGER SEGMENT IAW SRM 51-40-02.

Part: FRAME — DENTED (BS 1340 S26R) · airframe 65,309 hrs · 30,091 cycles

AFT CARGO FRAME DENTED AND GOUGED ON UPPER FLANGE STA 1340 ABOVE STR 26R OUT OF LIMITS DUE TO LOCATION OF DENT. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED AT FRAME STA 1340 STR 26R IAW SRM 53-00-07.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 65,309 hrs · 30,091 cycles

MAIN CABIN FLOORBEAM BS 1640 UPPER CHORD HAS CORROSION AROUND UPPER AND LOWER SIDE OF SEVERAL FASTENER HOLES FROM LBL 55 - RBL 55. COMPLIED WITH ERA 488913-14MA REV A.

Part: FLOORBEAM — MISREPAIRED (BS 740 LBL 9) · airframe 65,309 hrs · 30,091 cycles

MAIN CABIN FLOORBEAM WEB HAS A LARGE BORE CUTOUT WITH UNAPPROVED REPAIR, NO ED ON REPAIR FASTENERS AND NO ID TAG STA 740 LBL 9-18. REMOVED EXISTING REPAIR DOUBLERS AND STRAPS, FABRICATED NEW REPAIR ANGLES AND STRAPS PER ERA 362605-14 REV A.

Part: GATE — CORRODED (L4 DOOR) · airframe 65,309 hrs · 30,091 cycles

PITTING ON L4 DOOR LOWER GATE BOTTOM EDGE. BLENDED OUT DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LOWER GATE AT L4 DOOR PER AMM 57-11-38 404-009, ADJUSTMENT AND OPS CHECKED.

Part: DOUBLER — GOUGED (CARGO DOOR SKIN) · airframe 65,309 hrs · 30,091 cycles

AFT CARGO DOOR EXTERNAL SKIN AFT BOTTOM CORNER DOUBLER IS GOUGED. REMOVED DOUBLER, ACCOMPLISHED ERA 502445-14 REV ORIGINAL.

Part: SKIN — CANNING (BS 420-440) · airframe 65,309 hrs · 30,091 cycles

LEFT FUSELAGE SKIN IS OIL CANNING, BS 420-440 BTW STR14-17L. COMPLIED WITH PRI 502434-14 REV O. COMPLIED WITH ERA 502434-14 REV ORIG.

Part: SKIN — DENTED (BS 1652 S20R) · airframe 65,309 hrs · 30,091 cycles

DENT ON FUSELAGE RT SIDE AT STA 1652 ABOVE STR 20R. COMPLIED WITH PRI 502437-14AD REV O AND REV 1. ACCOMPLISHED ERA 502437-14 REV ORIG.

Part: SKIN — DENTED (BS 653 S17-18L) · airframe 65,309 hrs · 30,091 cycles

DENT ON LT SIDE OF FUSELAGE AT BS 653 BTW STR 17L AND 18L. ACCOMPLISHED PRI 502440-14 REV 0. ACCOMPLISHED ERA 502440-14 REV ORIG.

Part: SKIN — DENTED (BS 1662 S21-22L) · airframe 65,309 hrs · 30,091 cycles

DENT ON FUSELAGE LT SIDE AT BS 1662 BETWEEN S21-22L, COMPLIED WITH PRI 502438-14 REV2, COMPLIED WITH ER/A 502438-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 510 S27-28L) · airframe 65,309 hrs · 30,091 cycles

DENT ON FUSELAGE SKIN AT BS 510 BTW S27-28L. ACCOMPLISHED PRI 502431-14 REV O AND 1. ACCOMPLISHED ERA 502431-14 REV ORIG.

Part: SKIN — DENTED (BS 239) · airframe 65,309 hrs · 30,091 cycles

DENT ON LOWER FUSELAGE STA 239 805 RT OF FWD ASSY COMP DOOR CUTOUT/DENT FOUND TO BE OUT OF LIMITS, ACCOMPLISHED ERA 502433-14 REV.

Part: SKIN — DENTED (BS 324 S18-19R) · airframe 65,309 hrs · 30,091 cycles

DENT ON FUSELAGE SKIN LOWER BS 324 BTW S18-19R. COMPLIED WITH PRI 502439-14 REV 1. COMPLIED ERA 502439-14 REV ORIG.

Part: SKIN — DENTED (BS 1662 S18-19L) · airframe 65,309 hrs · 30,091 cycles

DENT ON FUSELAGE SKIN LT SIDE AT BS 1662 BTW S18-19L. ACCOMPLISHED PRI 502430-14 REV 1 AND 2. ACCOMPLISHED FINAL ERA 502430-14 REV A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 63,864 hrs · 29,513 cycles

HOLE WAS DISCOVERED IN AFT BAG BIG FLOOR. HOLE IS BEYOND ERA489384-14MA REPAIR. ATLANTA MAINTENANCE REPAIRED FLOOR FROM ERA 497070-14 REV 0. FABRICATE LOCATE DRILL COUNTERSINK DOUBLED PER ERA REV C. TIME LIMITED 2 REF FROM ERA 49707-14 REV 0.

Part: WIRE — BROKEN (CABIN) · airframe 63,624 hrs · 29,408 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE RED EMERGENCY PATH LIGHT AT THE MID LAVATORY INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 62,437 hrs · 28,937 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT ROW 33 INOPERATIVE. MAINTENANCE REPAIRED THE WIRING. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 62,218 hrs · 28,859 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND AN EMERGENCY PATH LIGHT AT SEAT 42DEF INOPERATIVE. MAINTENANCE REPAIRED THE WIRING NEAR THE LIGHT. OPERATIONAL CHECK WAS GOOD.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 61,114 hrs · 28,354 cycles

DURING PSV-16 VISIT IN ATL LIGHTNING STRIKE DAMAGE WAS FOUND ON A FASTENER AT SKIN LAP S-4L/STA407 IN THE UPPER SKIN ONLY. DAMAGE REPAIR COMPLETED PER ERA 487165-14 REV A. (DL757103238)

Part: SKIN — DENTED (FUSELAGE) · airframe 60,811 hrs · 28,215 cycles

09-15-10 ON ARRIVAL, DENTS FOUND AFT OF DOUBLER REPAIR AT L-2 2 INCHES OUTSIDE REPAIR, INSTALLED REPAIR DOUBLER. REPAIR IAW ERA 485677-14, REV 0.

Part: WIRE — BROKEN (CABIN) · airframe 60,173 hrs · 27,943 cycles

EMERGENCY LIGHT AT SEAT 6CD INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT HARNESS CONNECTOR. REPLACED WIRE SEGMENT. LIGHT CHECKS GOOD (DL757101767).

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,568 hrs · 27,647 cycles

SEAT 23D, EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS. OPS CHECKED OK.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,498 hrs · 27,610 cycles

EMERGENCY EGRESS AISLE LIGHTING INOP BETWEEN ROWS 29DEF AND 30DEF. REPLACED WIRE HARNESS AT ROW 29, AND LIGHT ASSY AT ROW 30. CHECKS OK.

Part: WIRE — BROKEN (CABIN) · airframe 58,362 hrs · 26,977 cycles

FAA INSPECTOR REPORTED EMERGENCY ESCAPE LIGHTS INOP, BROKEN WIRE AT 29 DEF. INSTALLED MALE CONNECTOR AT SEAT 29 DEF, PERSWPM. FOUND SEAT ESCAPE LIGHTS AT SEAT 20, 22, 28, 31 INOP. FWD TO MCO AND PLACARD PER MEL 33-51-03.

Part: SLIDE — PARTIAL INFLATE (RT OVERWING) · airframe 52,522 hrs · 24,150 cycles

UPON PERFORMING SLIDE DEPLOYMENT TRANSMITTAL 6T129 FOR RIGHT OVERWING ESCAPE SLIDE, SLIDE DID NOT FULLY DEPLOY

Part: TRIM SYSTEM — OUT OF POSITION (STAB) · airframe 50,522 hrs · 23,273 cycles

ABORTED T/O DUE CONFIG WARNING. CREW STATED STAB TRIM OUT OF GREEN BAND. REPOSITIONED STAB TRIM T/O WARN, OPS NORMAL.

Part: CIRCUIT CARD — FAULTY (CABIN) · airframe 48,504 hrs · 22,396 cycles

EVIDENCE OF SMOKING/BURNED AREA NEAR READING LIGHT CIRCUIT CARDS AT SEATS 1AB / 20A / 30A. REMOVED CARDS AND ROUTED TO ATL 757 FLEET MANAGER FOR ANALYSIS. DEFERRED LIGHTS PER MEL 25-20-01. REPLACED 20A READING LIGHT CIRCUIT CARD. OPS CHECK NORMAL. MCO/ PLACARD REMOVED.

Part: POWER SUPPLY — BURNED (CABIN) · airframe 47,912 hrs · 22,211 cycles

AFTER LEVEL OFF THE F/A CALL LIGHT AT 30A BEGAN SMOKING. CABIN LIGHTS WERE SECURED AND A DEADHEADING CREW MEMBER OPENED THE PANEL AND DISCONNECTED THE SHORTING LEADS FROM THE LIGHT. FOUND CTR READING LIGHT PWR SUPPLY MODULE BURNT. REPLACED OVHD PSU, CHECKS GOOD. MCO AND PLACARD REMOVED.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541FB. REMOVED AND REPLACED LT WING FUEL PANEL 541FB IAW B757 M/M 28-11-01.

Part: SKIN — CANNING (CARGO DOOR) · airframe 422,110 hrs · 21,979 cycles

DOOR SKIN CORNER OIL CANNED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER 8.5" BY 6.5" FROM 2024-T3 .071 AND FILLER 5.3" BY 3.75" FROM 2024-T3 .063 IAW B757 SRM 52-30-01 FIG 101, 52-30-01 PG 201 AND PROCESS STANDARD 900-5-1 NR 4, PG 4, 5 & 6.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541GB. REMOVED AND REPLACED LT WING FUEL PANEL 541GB IAW B757 M/M 28-11-01.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541HB. REMOVED AND REPLACED LT WING FUEL PANEL 541HB IAW B757 M/M 28-11-01.

Part: FLOOR SUPPORT — CORRODED (BS 1330 S28R) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON AFT CARGO COMPARTMENT FLOOR SUPPORT BS 1330 S-28R. CUT OUT SECTION OF CORRODED FLOOR SUPPORT SECTION. FABRICATED AND INSTALLED REPAIR SUPPORT SECTION 5.8" BY 1" BY 1" X .7" FROM .032 1/2H CRES IAW B757 M/M 53-82-01-801.

Part: STRAP — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION AFT CARGO NR 2 FLOORPANEL ON NUTPLATE SPLICE STRAP. FABRICATED AND INSTALLED NUTPLATE STRIP 39-5/8" X 1-14/16 FROM 7075-T6511 IAW B757 SRM 51-40-02, 51-20-01, 51-40-05.

Part: PANEL — CORRODED (BS 1376-1443) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON AFT CARGO COMPARTMENT RT TRANSITION PANEL BS 1376 TO BS 1443. REMOVED AND REPLACED TRANSITION PANEL IAW B757 SRM 51-40-02.

Part: SKIN — CRACKED (BS 615-620) · airframe 42,210 hrs · 21,979 cycles

FWD CARGO DOOR EXTERNAL SKIN CRACKED AFT LOWER CORNER. CUT OUT CRACKED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 5.85" BY 5.75" FROM 2024-T3 .071 IAW B757 SRM 52-30-01.

Part: INTERCOSTAL — CORRODED (BS 1500-1520) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION AFT CARGO INTERCOSTAL WEB BS 1500 TO BS 1520 LBL 2. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED INTERCOSTAL WEB REPAIR 19-3/4" BY 7-3/4" FROM 7075-T6 .040 IAW B757 SRM 51-40-02, 51-20-01.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1500) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON AFT CARGO COMPARTMENT FLOOR SUPPORT BS 1445 TO BS 1500 LBL 16. CUT OUT SECTION OF CORRODED FLOOR SUPPORT SECTION. FABRICATED AND INSTALLED REPAIR SUPPORT SECTION 29.5" BY 1.2" BY .8" FROM BAC1517-2227 AND REPAIR 7" BY 3/4" BY 3/4" FROM BAC1498-146 STRINGER REPAIR 2" BY 1" BY 1" X 1" FROM BAC1517-2229 IAW B757 SRM 51-20-01, 51-70-11.

Part: FRAME — CORRODED (BS 900) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION ON FAIRING FRAME AT BS 900 LBL 25 TO RBL 25. CUT OUT CORRODED SECTION OF FRAME. FABRICATED AND INSTALLED REPAIR ANGLE 44-1/4" BY 2-3/4" BY 1-1/4" FROM BAC1505-100403 7075-T6 IAW B757 SRM 51-70-12 FIG 1.

Part: INTERCOSTAL — CRACKED (BS 540-560) · airframe 422,110 hrs · 21,979 cycles

CRACKED INTERCOSTAL UPPER CHORD FLANGE AT PANEL HOLES, BETWEEN BS 540-560, AIRCRAFT CENTER LINE BL-0 WL-208.10. REMOVED CRACKED FLOOR SUPPORT ANGLE, FABRICATED AND INSTALLED ANGLE 19-1/2" BY 1" BY 1" FROM 7075-T6 .032 IAW B757 SRM 53-00-51 FIG 201 REPAIR 4, 51-20-01.

Part: FLOOR SUPPORT — CORRODED (BS 1670-1677) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON AFT CARGO COMPARTMENT FLOOR SUPPORT BS 1670 LBL 55. CUT OUT CORRODED SECTION OF SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT ANGLES 7.1" BY 1.8" BY 2.9" FROM 7075-T6 .090 AND 7.1 BY FROM 7075-T6 .071 IAW B757 SRM 51-70-11, 51-20-01.

Part: SKIN — BURNED (CARGO DOOR) · airframe 42,210 hrs · 21,979 cycles

FWD CARGO DOOR EXTERNAL SKIN BOTTOM EDGE HAS 5 AREA WITH STATIC BURNS. BURNISHED OUT BURN MARKS, NDT VERIFIED NO CRACKS OR DEFECTS. FABRICATED AND INSTALLED REPAIR DOUBLER 13.2" BY 3.9" FROM 2024-T3 .071 CLAD IAW B757 SRM 52-20-01, 51-20-01 AND PROCESS STANDARD 900-5-1 NR 4.

Part: CREASE BEAM — CORRODED (BS 960-1020) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON CREASE BEAM (CUSP) UPPER WEB SURFACE BETWEEN BS 960 AND 1020 AT LT OVERWING EXITS. FABRICATED AND INSTALLED WEB REPAIR 5.0" BY 3.25 FROM 7075-T6 .071 IAW B757 SRM 51-70-13, 51-20-01, AND 51-40-02.

Part: CLAMP — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641HB CLAMP UP RING. REMOVED AND REPLACED FUEL PANEL 641HB CLAMP RING P/N 69-35343-5 IAW B757 SRM 28-11-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 642BB. REMOVED AND REPLACED FUEL PANEL 642BB IAW B757 SRM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL 641EB. REMOVED AND REPLACED FUEL PANEL 641EB IAW B757 SRM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641KB. REMOVED AND REPLACED FUEL PANEL 641KB IAW B757 SRM 28-11-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 531CB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 531CB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

FOUND CORROSION NOTED ON RT WING FUEL PANEL 641GB. REMOVED AND REPLACED FUEL PANEL 641GB IAW B757 SRM 28-11-01.

Part: CLAMP — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL 641EB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 641EB CLAMP RING P/N 69-35343-5 IAW B757 SRM 28-11-01.

Part: CLAMP — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641DB CLAMP RING. REMOVED AND REPLACED RT WING FUEL PANEL 641DB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL 641FB. REMOVED AND REPLACED FUEL PANEL 641FB IAW B757 SRM 28-11-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541AB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 541AB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

FOUND CORROSION NOTED ON RT WING FUEL PANEL 643CB. REMOVED AND REPLACED FUEL PANEL 643CB IAW B757 SRM 28-11-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 531BB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 531BB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641JB. REMOVED AND REPLACED FUEL PANEL 641JB IAW B757 SRM 28-11-01.

Part: PANEL — CORRODED (BS 1520-1640) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON AFT CARGO COMPT TRANSITION PANEL RT BS 1520 - 1640. FABRICATED AND INSTALLED REPAIR PANEL 13.5" BY 5.3" FROM 7075-T6 .071 IAW B757 SRM 51-40-02, 51-20-01 AND 53-00-53.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541DB. REMOVED AND REPLACED FUEL PANEL 541DB IAW B757 MM 28-11-01.

Part: CLAMP — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641AB CLAMP RING. REMOVED AND REPLACED RT WING FUEL PANEL 641AB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641HB. REMOVED AND REPLACED FUEL PANEL 641HB IAW B757 SRM 28-11-01.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON CABIN FLOORBEAM BS 365 0 RBL 0 TO RBL 24. FABRICATED AND INSTALLED REPAIR ANGLE 22-1/4" FROM 7075-T6 .063 IAW B757 SRM 53-30-51 AND 51-20-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541DB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 541DB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541EB CLAMP RING. REMOVED AND REPLACED CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 642AB. REMOVED AND REPLACED FUEL PANEL 642AB IAW B757 SRM 28-11-01.

Part: CLAMP — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL 641FB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 641FB CLAMP RING IAW B757 SRM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641DB. REMOVED AND REPLACED RT WING FUEL PANEL 641DB IAW B757 MM 28-11-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541CB. REMOVED AND REPLACED FUEL PANEL 541CB IAW B757 MM 28-11-01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL 641MB. REMOVED AND REPLACED FUEL PANEL 641MB IAW B757 SRM 28-11-01.

Part: CLAMP — CORRODED (RT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON RT WING FUEL PANEL CLAMP RING 641GB. REMOVED AND REPLACED FUEL PANEL 641GB CLAMP RING IAW B757 SRM 28-11-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON LT WING FUEL PANEL 541EB. REMOVED AND REPLACED PANEL 541EB IAW B757 MM 28-11-01. LEAK CHECK GOOD.

Part: PANEL — CORRODED (BS 660-760) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

MULTIPLE SCREW HOLES, DOUBLED DRILLED SCREWS AND CORROSION O/B EDGE OF FWD CARGO COMPT TRANSITION PANEL RT SIDE. REMOVED CORROSION IAW B757 SRM 51-10-02. 100% MATERIAL LOSS. RECEIVED AND INSTALLED NEW PANEL P/N 143N5366-81. INSTALLED IAW B757 SRM 51-40-02 ON OPERATION NR 170.

Part: PANEL — CORRODED (BS 1440-1510) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BS 1440 - 1510 RT. REPAIRED CORRODED TRANSITION PANEL BY REMOVING AND REPLACING TRANSITION PANEL P/N 146N5391-110 IAW B757 SRM 51-40-05.

Part: PANEL — CORRODED (BS 560-640) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON FWD CARGO COMPT RT TRANSITION PANEL BS 560 - 640. REMOVED AND REPLACED TRANSITION PANEL P/N 143N5366U126 IAW B757 SRM 51-40-02.

Part: PANEL — CORRODED (BS 1200-1310) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON AFT CARGO COMPT RT TRANSITION PANEL BS 1200 - 1310. REPAIRED TRANSITION PANEL BY FABRICATING AND INSTALLING REPAIR DOUBLERS 23-1/2" BY 5" FROM 7075-T6 .071 IAW B757 SRM 51-20-01 AND M/M 53-88-01-801.

Part: PANEL — CORRODED (BS 1200-1310) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION NOTED ON AFT CARGO COMPT LT TRANSITION PANEL BS 1200 - 1310. REPAIRED TRANSITION PANEL BY FABRICATING AND INSTALLING 2 EACH REPAIR DOUBLERS 1" BY 1-3/4" BY 23" AND 1" BY 2-7/8" BY 24-1/2" FROM 7075-T6 .071 IAW B757 SRM 51-20-01 AND M/M 53-88-01-801.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION AND CRACK NOTED ON FWD CARGO COMPT SYSTEM SUPPORT BRACKET. FABRICATED AND INSTALLED NEW BRACKET 1-1/8" BY 1-1/4" BY 2-3/4" BY 5-3/4" FROM 2024-T3 .063 AT BS 740 R/H S-27 IAW B757 SRM 51-40-01.

Part: FLOOR SUPPORT — CORRODED (BS 1470-1480) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION AND DENT ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 1470 - 1480 LBL 3. REPAIRED BY CUTTING OUT 1" BY 1" CORRODED AREA, FABRICATED AND INSTALLED REPAIR 20" BY 1" FROM 7075-T6 .080 IAW B757 SRM 51-70-11.

Part: PANEL — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION AND ON AFT CARGO COMPARTMENT TRANSITION PANEL BS 1540 - 1640. REPAIRED BY REMOVING AND REPLACING WITH P/N 146N5431-41IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1470-1472) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 1470 LBL 11. REPAIRED BY CUTTING OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR 9-1/8" BY 8-1/4" BY 1.4" FROM 7075-T6 .080 IAW B757 SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (BS 1440-1500) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 1440 - 1500 LBL 7. REPAIRED BY CUTTING OUT CORRODED AREA OF FLOOR SUPPORT BS 1440 - 1500 LBL 7. FABRICATED AND INSTALLED REPAIR 8.4" BY 7" BY 1" BY 1.4" FROM 7075-T6 .080 IAW B757 SRM 51-70-11.

Part: INTERCOSTAL — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION AND ON AFT CARGO COMPARTMENT LOWER ANGLE OF VERTICAL INTERCOSTAL BS 1400 - 1420 S-28L. REPAIRED BY FABRICATING AND INSTALLING REPAIR 16.25" BY 3.0" FROM 7075-T6 .040 IAW B757 SRM 51-70-13.

Part: PANEL — CORRODED (BS 1410-1530) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BS 1410 - 1530 LT. REPAIRED CORRODED TRANSITION PANEL BY REMOVING AND REPLACING TRANSITION PANEL P/N 654N0244-406 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1340-1360) · corrosion level 2 · airframe 42,210 hrs · 21,979 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT WEB UPPER SURFACE BS 1340 LBL-9. REPAIRED CORROSION BY FABRICATING AND INSTALLING WEB REPAIR 20" BY 2.5" FROM 7075-T6 .040 IAW B757 SRM 53-60-04.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,870 hrs · 21,858 cycles

EMERGENCY AISLE SIDE PATH LIGHTS INOP (2EA) SEAT ROW 21 AND AFT LAV FLOOR LEVEL. RELAMPED LIGHT.

Part: POWER SUPPLY — INOPERATIVE (L-4 DOOR) · airframe 46,124 hrs · 21,607 cycles

LEFT SIDE L3 EMERGENCY LIGHT OUTSIDE ILLUMINATION LIGHT INOP. RELAMPED, NO HELP. REPLACED M737 POWER SUPPLY, CHECKS OK.

Part: AXLE — DAMAGED (NLG) · airframe 38,240 hrs · 18,538 cycles

ON TAXI OUT TO RUNWAY LT NOSE WHEEL ASSY BEARING AND OUTER RACE FAILED. REPLACED NLG AXLE AND WHEEL ASSEMBLY.

Part: LIGHT — BURNED OUT (#1 ENGINE) · airframe 37,206 hrs · 18,076 cycles

EXTERIOR EMERGENCY LIGHTS OUT AT 2L AND OVER LT WING CA RELAMPED

Part: LIGHT — BURNED (EXTERIOR) · airframe 31,452 hrs · 15,326 cycles

AFTER GEAR RETRACTION AND EXTENSION, A VERY STRONG ODOR OF BURNING RUBBER FILLED COCKPIT AND CABIN. ALL INSTRUMENT INDICATIONS NORMAL. FOUND RT RUNWAY TURNOFF SWITCH FUSED. REPLACED PANEL, NO FURTHER SMELL. INSPECTED WHEEL WELLS, WHEEELS, TIRES AND BRAKES ALL O.K. A/C O.K. FOR SERVICE.

Part: SWITCH — SHORTED (COCKPIT) · airframe 30,878 hrs · 15,055 cycles

ON FINAL APPROACH A BURNING RUBBER ODOR ENTERED COCKPIT. ODOR INCREASED INTENSITY DURING TAXI IN AND BECAME LIKE ELECTRICAL INSULATION. FOUND LT RUNWAY TURNOFF LIGHT SW SHORTING INTERNALLY AND OVERHEATING. FOUND SW AND WIRING BURNT. REPLACED SW AND WIRING PER MM.

Part: DRAIN LINE — CLOGGED (E/E BAY) · airframe 29,910 hrs · 14,584 cycles

NOTICED OBNOXIOUS ODOR IN COCKPIT ON TAKEOFF ROLL. ODOR LASTED ABOUT 1 MINUTE, AND ON FINAL ABOUT 2 MINUTES. PRIOR TO LANDING SMELL STAYED THROUGH LANDING ROLL. FLT ATTENTDANT DID NOT NOTICE SMELL. APPEAR TO ORIGINATE IN LEFT SIDE OF COCKPIT. SMELL RESEMBLES BURNT RUBBER OR ROTTEN EGGS, DISSIPATED QUICKLY. CLEARED CLOGGED DRAINS AND STAGNANT WATER FROM FWD E/E COMPARTMENT.

Part: SKIN — PUNCTURED (SLAT) · airframe 28,372 hrs · 13,845 cycles

AFTER ACCOMPLISHMENT OF S/B 757-57A0043, THE I/B LEADING EDGE SLAT, TRAILING EDGE WEDGE, UPPER SKIN WAS DAMAGED. DAMAGE LOCATED 1 AFT OF THE FWD EDGE OF THE TRAILING EDGE WEDGE UPPER SKIN AND 46 I/B FROM THE O/B EDGE. REPAIR PER ER/A 387545-14.

Part: SKIN — DENTED (BS 620)

THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL DENTS AT FS 620 BETWEEN STRINGERS 16L & 17L. THE DAMAGE WAS REMOVED WITH THREE SMALL CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 369257-14, REV A.

Part: LINE — RUPTURED (NR 1 ENGINE)

DURING CLIMBOUT, L HYD QTY LIGHT ILLUMINATED, FOLLOWED BY SYS PRESS LIGHT. STATUS PAGE SHOWS L HYD SYS 0.00RF. FOUND EDP PRESS LINE RUPTURED. CHECKED EDP PRESS AND CASE DRAIN FILTERS, BOTH CLEAN. REPLACED BOTH FILTERS AND EDP AS PRECAUTION. REPLACED LINE AND SERVICED HYD SYS. RAN ENG AND CHECKED EDP PER MM. PRESS AND LEAK CK OK. RE-CHECKED FILTERS, BOTH CLEAN.

Part: PUMP — LEAKING (LT ENGINE)

SLOW HYD LEAK IN LT SYS. REPLACED LT ENG HYD PUMP. CHECKED CASE DRAIN AND SUPPLY FILTERS, NO METAL FOUND. OPS AND LEAK CK OK.

Part: SIGN — LOOSE (DOOR 4L)

LIGHTED SIGN FOR EMERGENCY PATH LIGHTING AT 4L DOOR HANGING OFF WALL BY ITS WIRING. REPLACED LIGHTED SIGN ASSY, OPN NORMAL.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

AFTER TAKEOFF AT 500 FEET, HAD 3 COMPRESSOR STALLS ON RT ENGINE, THROTTLE RETURNED TO IDLE. EMERGENCY DECLARED AND RETURNED TO SFO WITH ENGINE AT IDLE. VISUALLY INSPECTED ENGINE AND CHECKED ALL CHIP DETECTORS AND MAIN OIL FILTER, ALL OK. BORESCOPE INSPECTION FOUND DAMAGE BEYOND LIMITS TO HPC STAGE 16. REPLACED RT ENGINE.

Part: RADOME — DELAMINATED (NOSE)

NOSE OF RADOME WAS DELAMINATED AND EXCEEDED MOISTURE LIMITS. REMOVED AND REPLACED INNER SKIN AS PER B-757 SRM 53-10-72. DAMAGE WAS REPAIRED DURING SHOP VISIT.

Part: OVEN — FAULTY (FWD GALLEY)

DURING CRUISE, NOTICED ELECTRICAL BURNING ODOR IN FORWARD GALLEY. DEACTIVATED GALLEY EQUIPMENT ODOR DISSIPATED. FOUND ODOR COMING FROM FWD OVEN, REPLACED OVEN OPERATION NORMAL.