N540US

Part: SEAL — OBSTRUCTED (ZONE 800) · airframe 83,660 hrs · 31,750 cycles

SHIP 5640 F/A REPORT VIBRATION IN THE AFT GALLEY. PILOTS FEEL SLIGHT VIBRATION IN RUDDER PEDALS. CORRECTIVE ACTION: FOUND SURVIVIAL KIT D-RING UNDER R4 DOOR PRESSURE SEAL. RESTOWED D-RING PER B757 AMM 25-66. (6702538)

Part: LENS — LOOSE (ZONE 200) · airframe 83,528 hrs · 31,671 cycles

SHIP 5640 LIGHT LENS COVER BY 2L DOOR LOOSE/DETACHED. CORRECTIVE ACTION: RESECURED LIGHT LENS COVER BY 2L DOOR. NO FURTHER ISSUES NOTED. (5720272)

Part: DOOR — FOD (ZONE 800) · airframe 83,310 hrs · 31,543 cycles

SHIP 5640 L3 DOOR WON'T ARM. CORRECTIVE ACTION: FOUND FOD BLOCKING SLIDE FROM ARMING. REMOVED FOD. OPS CHECK NML . A/C OK FOR SERVICE. ALL WORK DONE IAW B757 AMM 25-61. (5665640)

Part: DOOR — MISSING (L1 DOOR) · airframe 83,202 hrs · 31,487 cycles

SHIP 5640 L1 DOOR FWD LOWER BEARING PLATE MISSING. CORRECTIVE ACTION: INSTALLED BEARING PLATE REF B757 AMM 53-11. (5618356)

Part: SIGN — DETACHED (CABIN) · airframe 83,033 hrs · 31,388 cycles

SHIP 5640 EXIT SIGN ABEAM ENTRY DOOR (OVERWING) FELL OFF INFLIGHT. CORRECTIVE ACTION: RE-SECURED SIGN. (5640794)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 82,997 hrs · 31,373 cycles

2R EXIT SIGN DIFFUSER COVER MISSING FLOOD LAMP LENS. CORRECTIVE ACTION: INSTALLED FWD FLOOD LENS ON 2R EMERGENCY EXIT DIFFUSER AND ALL HARDWARE IS INTACT. REF B757 AMM 35-51.

Part: SIGN — DETACHED (CABIN) · airframe 82,997 hrs · 31,373 cycles

SHIP 5640 EXIT SIGN ABOVE DOOR R2 DETACHED. CORRECTIVE ACTION: REATTACHED EMERGENCY EXIT SIGN AT R2 DOOR AS PER B757 AMM 33-51. (5640762)

Part: SIGN — DETACHED (R2 AREA) · airframe 82,997 hrs · 31,373 cycles

SHIP 5640 2R EXIT SIGN FELL OFF. CORRECTIVE ACTION: REINSTALLED 2R EXIT LENS DIFFUSER PER B757 33-51. (5640764)

Part: SIGN — DETACHED (CABIN) · airframe 82,880 hrs · 31,305 cycles

SHIP 5640 2R DOOR EXIT SIGN FELL OFF DURING TO ROLL. CORRECTIVE ACTION: RESECURED SIGN AS REQ. (5901669)

Part: SIGN — DETACHED (CABIN) · airframe 82,876 hrs · 31,304 cycles

SHIP 5640 2R DOOR EXIT SIGN FELL OFF. CORRECTIVE ACTION: REECURED. (5901660)

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 82,739 hrs · 31,232 cycles

SHIP 5640 WRONG COLOR EMERGENCY PATH LIGHT INSTALLED AT SEAT 27D. CORRECTIVE ACTION: AT SEAT 27D FOUND AFT LIGHT RED. REPLACED LIGHT ASSY WITH WHITE REF B757 AMM 33-51. (5471593)

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 82,320 hrs · 31,013 cycles

SHIP 5640 2R DOOR EMERGENCY EXIT SIGN COVER LOOSE. CORRECTIVE ACTION: RESECURED LENS CKS OK PER 757 AMM 3350. (4831074)

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 82,310 hrs · 31,006 cycles

SHIP 5640 EMERGENCY LIGHT COVER FELL OFF ROW 19. CORRECTIVE ACTION: REINSTALLED EXIT ROW SIGN. (4831066)

Part: POWER SUPPLY — INOPERATIVE (SEAT ROWS 33-37) · airframe 82,223 hrs · 30,966 cycles

SHIP 5640 ON SVC CK FOUND SEAT 33-37 SEAT MOUNTED EMERGENCY PATH LIGHT INOP. CORRECTIVE ACTION: R/R POWER SUPPLY PER AMM 33-51. NO HELP. T/S PER WDM 33-51-22. FOUND CONNECTOR D9723P BAD. R/R D9723P CONNECTOR PER WDM 33-51-22 AND SWPM 20-60. OPS CK GOOD. (4831031)

Part: WIRE HARNESS — FAULTED (IFE) · airframe 82,045 hrs · 30,876 cycles

SHIP 5640 IFE SYSTEM INOP (PARTIALLY OPERATIVE) MULTIOPLE LOCATIONS: OBSERVES FAINT ELECTRACAL SMELL THAT EVENTUALLY WENT AWAY AFTER 2ND REBOOT. MORE MONITORS INOP AFTER EACH REBOOT. SOME POWER OUTLETS NOT WORKING THROUGHOUT MAIN CABIN. CORRECTIVE ACTION: FOUND HARNESS & SEB CONNECTORS AT 2D BURNT. R&R SEB PER ERA 615979-14 REV ORIGINAL REMOVED HARNESSES P/N RD-KM7827-136 & RD-KM 7394-036 AND INSTALLED HARNESSES IFE SYS TURNED ON IFE SYS BOOTED UP. READDRESS PASSED. SEATS 4CD - 45DEF & A/C IFE SYS & PED POWER OPS CHK NML. REF PAC D0C#1000543 SEB 23-32-07 AND PAC DOC #2000535 23-32, 23-81. (0205066)

Part: INDICATOR — INOPERATIVE (R2 DOOR SLIDE) · airframe 81,961 hrs · 30,832 cycles

SHIP 5640 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S/ 2R DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: T/S PER B757 FIM 25-66-815-802. REPLACED 2R DOOR FWD SENSOR PER B757 AMM 25-66-11. OPS CK NML. MEL/PLAC CLEARED. (0189564)

Part: INDICATOR — OUT OF POSITION (R2 DOOR) · airframe 81,839 hrs · 30,774 cycles

SHIP 5640 2R DOOR KNUCKLE KNOCKER DOES NOT DEPLOY WHEN ARMED. CORRECTIVE ACTION: REPOSITIONED DOOR LINER KNOCKER OPS CHK GOOD. (4586082)

Part: LANDING — WORN (ACCESS PANEL) · airframe 81,794 hrs · 30,752 cycles

SHIP 5640 LH PYLON INBD PANEL LANDING AREA HAS WEAR MARKS. CORRECTIVE ACTION: C/W ERA 614315-14 REV ORIGINAL AT LH PYLON INBD PANEL LANDING AREA. (0151324)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,793 hrs · 30,751 cycles

SHIP 5640 RH OFFWING SLIDE UNRAVELED. CORRECTIVE ACTION: REMOVED AND REPLACED RH OFFWING SLIDE IAW B757 AMM 25-65. (0114203)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,793 hrs · 30,751 cycles

SHIP 5640 L-2 DOOR EMERGENCY ESCAPE SLIDE PRESSURE GAUGE IS OUTSIDE OF GREEN BRAND. CORRECTIVE ACTION: REMOVED AND REPLACED L2 DOOR EMERGENCY ESCAPE SLIDE. IAW B 757 AMDS CARD 2040-0191. (0101260)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,357 hrs · 30,434 cycles

SHIP 5640 MID CABIN OVERHEAD EMERGENCY EXIT SIGN MISSING. CORRECTIVE ACTION: LOCATED SIGN ASSY AND REINSTALLED. CHKS GOOD. OK FOR SVC. (4910076)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,328 hrs · 30,423 cycles

SHIP 5640 EMERGENCY SEAT MOUNTED LIGHTNING DAMAGED / INOPERATIVE / LOCATIONS:102, RED EMERGENCY TRACK LIGHTNING DAMAGED AT 3R LAV. CORRECTIVE ACTION: REPLACED LENS ASSY PER B757 AMM 33-51. OPS CHECK GOOD. (2926962)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,328 hrs · 30,423 cycles

SHIP 5640 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:204, EMERGENCY TRACK LIGHTNING DAMAGED AT 3R LAV. CORRECTIVE ACTION: REPLACED LENS ASSY PER B757 AMM 33-51. OPS CHECK GOOD. (2926961)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,328 hrs · 30,423 cycles

SHIP 5640 EMERGENCY SEAT MOUNTED LIGHTNING DAMAGED / INOPERATIVE / LOCATIONS:610, EMERGENCY TRACK LIGHTNING DAMAGED AT 3R LAV. CORRECTIVE ACTION: REPLACED LENS ASSY PER B757 AMM 33-51. OPS CHECK GOOD. (2926963)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,213 hrs · 30,352 cycles

SHIP 5640 AFT CARGO DOOR FWD LWR CORNER HAS DENT. EVALUATED AND REPAIRED AFT CARGO DOOR IAW ERA 614260-14 REV ORIGINAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,192 hrs · 30,340 cycles

SHIP 5640 EMERGENCY EXIT LIGHT COVER FELL OFF. CORRECTIVE ACTION: RE SECURED COVER REF B757 AMM25-22. (4980474)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,137 hrs · 30,307 cycles

SHIP 5640 2L SLIDE LIGHT WILL NOT ILLUMINATE WHEN ARMED. CORRECTIVE ACTION: FOUND D-RING NOT SECURED RE-SECURED SAME SLIDE LIGHT WORKS NORMAL. (4980430)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,859 hrs · 30,170 cycles

SHIP 5640 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS: 1R. CORRECTIVE ACTION: REMOVED FOD. CHECK OK KNUCKLE KNOCKER OK PER B757 52-11 (2818630)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,483 hrs · 29,996 cycles

SHIP 5640 MIDSHIP OVERHEAD EMERGENCY EXIT SIGN LOOSE. CORRECTIVE ACTION: REINSTALLED EMERGENCY EXIT SIGN COVER AT MIDSHIP AS RQD IAW B757 AMM 33-24 - SIGN IS SECURE. (4816166)

Part: NONE — NONE · airframe 79,999 hrs · 29,731 cycles

SHIP 5640 COMPLY WITH ERA 606378-14 REV. ORIGINAL. CORRECTIVE ACTION: REF ERA 606378-14 RE ORG. (2648348)

Part: NONE — NONE · airframe 79,994 hrs · 29,730 cycles

SHIP 5640 VIASAT SYSTEM INSTALLATION ON FS 1260, FS 1280 & FS 1300 FRAMES. CORRECTIVE ACTION: REF ERA 606327-14. (2647695)

Part: NONE — NONE · airframe 79,994 hrs · 29,730 cycles

SHIP 5640 COMPLY WITH ERA 606327-14AD REV. A SECTION 1 FRAME HARDWARE INSTALLATION. CORRECTIVE ACTION: COMPLIED WITH ERA 606327-14AD REV. A SECTION 1. (2648245)

Part: NONE — NONE · airframe 79,994 hrs · 29,730 cycles

SHIP 5640 VIASAT SYSTEM INSTALLATION ON FS 1260 & FS 1280 FRAMES. CORRECTIVE ACTION: REF ERA 606327-14. (2647680)

Part: NONE — NONE · airframe 78,806 hrs · 29,243 cycles

SHIP 5640 AFT OVERHEAD LIFE RAFT UNSECURE. CORRECTIVE ACTION: REMOVED LIFE RAFT. INSTALLED AFT OVERHEAD LIFE RAFT REF B757 AMM 25-22. (9038856)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 SKIN PANEL DAMAGED FROM TAIL STRIKE STA 1787 -1862 OBL. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/006 00006 REPAIRED DAMAGED SKIN REF ERA 601456-14 REV A. (2385990)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 SKIN PANEL DAMAGED FROM TAIL STRIKE STA 1720-1787 OBL. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/004 00004 REMOVED AND REPLACED SKIN REF ERA 601399-14 REV ORIG AND ERA 601515-14 REV ORIG. (2384231)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 FORWARD CHORD WORN BETWEEN STA 28L AND 28R AT STA 1720. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/019 00019 REPAIRED FWD CHORD PER ER/A 601486-14 REV. ORIGINAL. (2382676)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 LOWER SECTION OF WEB @ STA 1720 BENT/WRINLKED. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/018 00018 REPAIRED WEB PER ER/A 601486-14 REV. ORIGINAL. (2382674)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 AFT CHORD WORN BETWEEN STA 28L AND 28R AT STA 1720. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/020 00020 REPAIRED AFT CHORD PER ER/A 601486-14 REV. ORIGINAL. (2382669)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 SKIN PANEL DAMAGED FROM TAIL STRIKE STA 1701-1720 OBL. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/003 00003 REPAIRED SKIN STA 1700 TO 1720, S-29L TO S-29R, TAIL STRIKE DAMAGE PER ER /A 601450-14 REV. A. PRI 601450-14 REV. 0 TO REV. 4 MATCH ER/A 601450-14 REV. A. (2373121)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 TAIL JACKING FITTING PN 148N9320-1 DAMAGED DUE TO TAIL STRIKE. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/016 00016 REPAIRED TAIL JACK FITTING REF ERA 601447-14 REV ORIG. PRI 601447-14 REVS 0-1 MATCH ERA 601447-14 REV ORIG. (2371940)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,239 hrs · 30,364 cycles

SHIP 5640 FUSELAGE / SKIN STA 1700 TO 1720, S-29L TO S-29R / TAIL STRIKE DAMAGE. CORRECTIVE ACTION: REF ERA 601450-14. (2372527)

Part: NONE — NONE · airframe 78,612 hrs · 29,172 cycles

SHIP 5640 BEAR STRAP WORN JUST AFT OF STA 1763 BETWEEN STR 29L/29R. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/026 00026 REPAIRED PER B757 SRM. (2370963)

Part: WAVE GUIDE — INOPERATIVE · airframe 78,581 hrs · 29,158 cycles

SHIP 5640 - ATB - TO MSP DUE TO WXR RADAR INOP. CORRECTIVE ACTION: REPLACED DRIVE UNIT AND RADAR WAVE GUIDE. ALL SYSTEM TEST PASSED. C/W NOGO PROCEDURES.

Part: NONE — NONE · airframe 78,322 hrs · 29,075 cycles

SHIP 5640 ON DESCENT INTO LAX AT 11,500' THE CAPTAIN'S ADI AND EHSI WENT BLANK AND BOTH SCREENS DISPLAYED "SG FAIL". A BRIEF ELECTRICAL SMELL WITH NO VISIBLE SMOKE OCCURRED AT THE SAME TIME. 30 SECOND DURATION. CORRECTIVE ACTION: PERFORMED B757 ATA 2172 NO-GO ODI STEPS 1-5. FOUND CAPTAIN'S EHSI INTERMITTENTLY INOP. INSPECTED WIRING AND PINS WITH NO DISCREPANCIES NOTED. REPLACED CAPTAIN'S EHSI IAW B757 AMM 34-22. REPLACED LEFT EFIS SYMBOL GENERATOR IAW B757 AMM 34-22. NO DISCREPANCIES NOTED. (9202856)

Part: UNKNOWN — UNKNOWN · airframe 77,340 hrs · 28,789 cycles

SHIP 5640 EXIT SIGN COVER ON CEILING AT OVERWING EXITS MISSING. CORRECTIVE ACTION: RESEURED OVERWING EXIT SIGN COVER OPS CKS GOOD. (8857170)

Part: TRANSMITTER — FAULTED (TE FLAP SYSTEM) · airframe 76,506 hrs · 28,566 cycles

SHIP 5640 -MISC/DE- EICAS MESSAGE TE FLAP ASYM DISPLAYED WITH ASSOCIATED LIGHT ON APPROACH INTO SEA. C/W QRH AND COMPLETED APPROACH. CORRECTIVE ACTION: REPLACED LEFT TE FLAP POSITION TRANSMITTER.

Part: NONE — NONE · airframe 76,441 hrs · 28,552 cycles

SHIP 5640 EMERGENCY LIGHTS INOP AT ROWS 18-22. CORRECTIVE ACTION: REPLACED BATTERY PACK FOR AFFECTED ROWS, R&R BATTERY POWER SUPPLY PER B757 AMM 33-51. FOUND POWER WIRE SHORTED TO SEAT TRACK AT ROW 18 APPLIED SHRINK TUBING OVER CHAFED WIRE PER SWPM 33-50 OPS CHECK NORMAL. (5134141)

Part: NONE — NONE · airframe 76,059 hrs · 28,430 cycles

SHIP 5640 LT WING I/B MAIN FLAP UPPER SURFACE IS CORRODED 94 INCHES FROM I/B EDGE. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON LT WING I/B MAIN FLAP UPPER SURFACE 94 INCHES FROM I/B EDGE IAW DELTA ER/A 595049-14 REV. ORIGINAL. (2007455)

Part: NONE — NONE · airframe 76,059 hrs · 28,430 cycles

SHIP 5640 LT WING I/B MAIN FLAP UPPER SURFACE DOUBLER IS CHAFED 20 INCHES FROM O/B EDGE. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON LT WING I/B MAIN FLAP UPPER SURFACE IAW DELTA ER/A 595049-14 REV. ORIGINAL. (2007451)

Part: COVER PLATE — MISSING (R3 DOOR HANDLE) · airframe 75,375 hrs · 28,245 cycles

SHIP 5640 3R DOOR HANDLE MISSING COVER PLATE. CORRECTIVE ACTION: INSTALLED NEW HANDLE LINING INSERT AT DOOR 4R. (7915144)

Part: COVER — DETACHED (L1 DOOR HANDLE) · airframe 75,582 hrs · 28,299 cycles

SHIP 5640 F/A SAID SMALL 2 PC PART FELL OFF FROM BEHIND 1L DOOR HANDLE. CORRECTIVE ACTION: INSTALLED COVER PLATE ON 1L DOOR AND OPS CHKS GOOD. REF B757 AMM 52-11. (7324531)

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 74,076 hrs · 27,903 cycles

SHIP 5640 AT GEAR DOWN EMERGENCY DOOR MSG ON EICAS MOMENTARILY. TWO OTHER MSGS BUT THEY WENT AWAY BEFORE I COULD READ THEM. CORRECTIVE ACTION: VISUALLY CHECKED ALL DOORS SLIDE PSI, INFLATION BOTTLE PSI, SQUIP TEST 1/2 GOOD. GIRT BAR ARM/DISARM SMOOTHLY NO PROBLEM. FAULTS COULD NOT BE DUPLICATD ON GROUND. (7395820)

Part: PRESSURE SWITCH — MALFUNCTIONED (FLAP SYSTEM) · airframe 73,381 hrs · 27,716 cycles

SHIP 5640 - THE "FLAP DISAGREE" EICAS MESSAGE DISPLAYED ON APPROACH WHEN THE FLAPS WERE SELECTED TO EXTEND. THE FLIGHT CREW PERFORMED A GO-AROUND, DECLARED AN EMERGENCY, AND USED THE ALTERNATE FLAPS FOR LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FLAP/SLAT DEPRESSURIZATION MODULE PRESSURE SWITCH AND COMPLIED WITH THE NO GO ODI PROCEDURES. AIRCRAFT HAS RETURNED TO SERVICE. (LP #7574196)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,823 hrs · 27,304 cycles

EMERGENCY CEILING LIGHTS AT ROW 25-30 ARE INOPERATIVE. FOUND POWER SUPPLY M10954 INOPERATIVE AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,809 hrs · 27,297 cycles

EMERGENCY LIGHTS FROM ROWS 23DEF - 37DEF ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,809 hrs · 27,297 cycles

L1 DOOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,809 hrs · 27,297 cycles

OVERHEAD EMERGENCY LIGHTS FROM 25-30 ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: PLATE — MISSING (L2 DOOR) · airframe 71,738 hrs · 27,275 cycles

SHIP 5640 L2 DOOR MISSING DOOR STOP PLATE AT CENTER FWD POS. CORRECTIVE ACTION: INSTALLED DOOR STOP PLATE. (6023768)

Part: LANYARD — OUT OF POSITION (L2 DOOR) · airframe 71,635 hrs · 27,249 cycles

SHIP 5640 DURING SERVICE CHECK FOUND DOOR L2 GIRT BAR LANYARD OUT OF POSITION. CORRECTIVE ACTION: REPACKED GIRT BAR LANYARD IN CORRECT POSITION. DOOR PINNED. LANYARD PACKED CORRECTLY. VERIFIED SLIDE PIN REMOVED AND STOWED REQUIRED INSPECTION ITEMS COMPLETED. (6023732)

Part: TRIGGER — MALFUNCTIONED (L4 DOOR) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1345182) MTC REQUEST. DURING L4 DOOR ADJUST CHECK, DOOR DOESNT UNLOCK CORRECTLY FROM OPEN TO CLOSE POSITION. (PTAS). CORRECTIVE ACTION: TRIGGER ON L4 DOOR WAS REPLACED PER B757-200 AMM 20-11-00.

Part: SKIN — DENTED (TE FLAP) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1345844) DENT ON INBD MAIN FLAP LWR SKIN MF STA 209 AT RH WING. (AD). CORRECTIVE ACTION: INBD MAIN FLAP LWR SKIN MF STA 209 AT RH WING WAS REPAIRED PER B757-200 SRM 57-53-01 REPAIR 1 DETAIL I AND SRM 51-70-10 REPAIR 2 PAR. 4.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1343842) INITIAL INSPECTION: CORROSION ON RH SIDE PANEL FROM STA 1440 TO 1530 BTW S-27R AT AFT CARGO COMPARTMENT. (C-2). CORRECTIVE ACTION: CORROSION LEVEL 2 SIDE PANEL WAS REPLACED PER B757-200 SRM 51-40-02 PAR 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1343138) CORROSION OUT OF LIMITS ON FLOOR STRINGER LBL 16.10, LBL 10.45, LBL 7.55, LBL 2.90 STA 653 AT FWD CARGO COMPARTMENT. (IN REF. NRC S/N 00370) (C1). CORRECTIVE ACTION: SUMMARY OF NRC S/N 00701:LEVEL CORROSION 2. STRINGERS LBL 16.10, LBL 10.45, LBL 7.55, LBL 2.90 WERE REPLACED PER B757-200 SRM 51-40-02 PAR. 4 AND 7.

Part: SKIN — CRACKED (R4 DOOR) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1337973) CRACK ON INNER SKIN ON R4 PASSENGER DOOR. CORRECTIVE ACTION: INNER SKIN ON R4 PASSENGER DOOR WAS REPAIRED PER B757-200 ETI-57-19-134 REV. ORIGINAL AND ER/A 582546-14 REV. ORIGINAL.

Part: PANEL — CORRODED (BS 1530-1560) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1335096) CORROSION OUT OF LIMITS ON RH SIDE PANEL FROM STA 1530 TO 1560 BTW S-27R AT AFT CARGO COMPARTMENT. (C-2). CORRECTIVE ACTION: SUMMARY: OF NRC 00722 , CORROSION LEVEL 2 . RH SIDE PANEL FROM STA 1530 TO 1560 BTW S-27R AT AFT CARGO COMPARTMENT WAS REPLACED PER B 757-200 SRM 51-40-02 PAR 4, 7 AND 9.

Part: SUPPORT — CORRODED (BS 1380-1440) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1334612) CORROSION ON LOWER SILL FROM STA:1380 TO 1440, S-27R , AT AFT CARGO COMPARTMENT. (C-2). CORRECTIVE ACTION: CORROSION LEVEL 2, LOWER SILL WAS REPLACED PER B757-200 SRM 51-40-02 PAR 4 AND SRM 51-40-02 PAR 7.

Part: STRAP — CRACKED (BS 362-377) · airframe 70,303 hrs · 26,887 cycles

SHIP 5640 INITIAL INSPECTION: CRACK STRAPS (2 E/AS) BTW STA 362-377, BTW, FLOOR BEAM LBL-24. TO LBL-45 AT E/E BAY. CORRECTIVE ACTION: SUMMARY OF NRC 00453: STRAPS WERE REPAIRED PER ER/A: 384483-14MA REV: D. (1334591)

Part: FLOOR SUPPORT — CORRODED (BS 1330) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1333327) CORROSION OUT OF LIMITS ON FLOOR STRINGER RBL 2.90 STA 1330 AT AFT CARGO COMPARTMENT. (IN REF. NRC S/N 00209)(C2). CORRECTIVE ACTION: CORROSION LEVEL 2: STRINGER WAS REPAIRED PER B 757-200 SRM 53-00-53 REPAIR 1, FIG. 201.

Part: FLOOR SUPPORT — CORRODED (BS 1330) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1333348) CORROSION OUT OF LIMITS ON FLOOR STRINGER LBL 7.55 STA 1330 AT AFT CARGO COMPARTMENT. (IN REF. NRC S/N 00211) (C-2). CORRECTIVE ACTION: CORROSION LEVEL 2: STRINGER WAS REPAIRED PER B 757-200 SRM 53-00-53 REPAIR 1, FIG. 201.

Part: SUPPORT BEAM — WORN (NR 1 NACELLE) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1332181) WEAR ON OUTBD FAN COWL SUPPORT BEAM STA NAC 102 AT ENGINE 1 PYLON (MOT 1). CORRECTIVE ACTION: FAN COWL SUPPORT BEAM WAS REPAIRED PER ETI-57-19-145 REV: 1 AND ER/A: 582388-14 REV: ORIGINAL SEC. I.

Part: FLOOR SUPPORT — CORRODED (BS 1330) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1333325) CORROSION OUT OF LIMITS ON FLOOR STRINGER RBL 10.45 STA 1330 AT AFT CARGO COMPARTMENT. (IN REF. NRC S/N 00207) (C2). CORRECTIVE ACTION: CORROSION LEVEL 2: STRINGER WAS REPAIRED PER B 757-200 SRM 53-00-53 REPAIR 1, FIG. 201.

Part: SKIN — CORRODED (RT WING) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1333163) CORROSION ON LOWER SKIN BTW STA. WS200 TO WS204 BTW L-5 TO L-6 AT RH WING. (AD). CORRECTIVE ACTION: (CORROSION LEVEL 1) SKIN WAS REPAIRED PER ER/A 582276-14 REV: ORIGINAL.

Part: SKIN — CORRODED (RT WING) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1333156) CORROSION ON LOWER SKIN BTW STA. WS200 TO WS204 BTW L-5 TO L-6 AT RH WING. (AD). CORRECTIVE ACTION: (CORROSION LEVEL 1) SKIN WAS REPAIRED PER ER/A 582276-14 REV: ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (BS 750) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1330803) CORROSION OUT OF LIMITS ON FLOOR STRINGER RBL 10.45 AND RBL 7.55, STA 750 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: FLOOR STRINGER RBL 10.45 AND RBL 7.55, STA 750 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B 757-200 SRM 53-00-53 REP. 1 FIG. 201.

Part: SKIN — DEBONDED (RT NR 9 SLAT) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1332012) AWR: (AD) DISBOND OF 1" X 1" WAS FOUND ON LOWER SKIN OF RH SLAT 9 TRAILING EDGE WEDGE APPROX STA WS 637 AND 8" FROM TRAILING EDGE. CORRECTIVE ACTION: DISBOND OF 1" X 1" ON LOWER SKIN OF RH SLAT 9 TRAILING EDGE WEDGE APPROX STA WS 637 AND 8" FROM TRAILING EDGE WAS REPAIRED PER B-757-200 S.R.M. 51-70-10 REPAIR GENERAL, TABLE 202 PAR. 19. F. AND PAR. 20. B. (3) TABLE 208 IN REFERENCE TO B-757-200 S.R.M. 57-43-02-2R-1 FIGURE 201. REPAIR CLASS 3 AND WEDGE TYPE "A": PERFORM AN ULTRASONIC LOW FREQUENCY BOND TEST WITHIN 600 TRAILING EDGE WEDGE FLIGHT CYCLES OR WITHIN 6 MONTHS (WHICHEVER OCCURS FIRST) PER B757-200 SRM 57-43-02 REPAIR 1 NOTE: E AND SB 757-57-0066 REPAIR CLASS 3 AND WEDGE TYPE "A": PERFORM A DETAILED VISUAL INSPECTION WITHIN 600 TRAILING EDGE WEDGE FLIGHT CYCLES OR WITHIN 6 MONTHS (WHICHEVER OCCURS FIRST) PER B757-200 SRM 57-43-02 REPAIR 1 NOTE: E AND SB 757-57-0066.

Part: SKIN — DEBONDED (RT NR 9 SLAT) · airframe 70,303 hrs · 26,887 cycles

SHIP 5640 AWR: (AD) DISBOND WAS FOUND ON LOWER SKIN OF RH SLAT 9 TRAILING EDGE WEDGE APPROX STA WS 637 AND 8" FROM TRAILING EDGE IN REFERENCE TO WORK CARD. CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO. 00031: DISBOND ON LOWER SKIN OF RH SLAT 9 WAS REPAIRED PER B-757-200 S.R.M. (1329134)

Part: SEAT TRACK — WORN (BS 870) · airframe 70,303 hrs · 26,887 cycles

SHIP 5640 WORN ON RH INBD SEAT TRACK STA 870 AT PAX CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: RH INBD SEAT TRACK STA 870 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B 757-200 SRM. (13238332)

Part: SEAT TRACK — WORN (BS 875) · airframe 70,303 hrs · 26,887 cycles

SHIP 5640 WEAR ON LH/INBOARD SEAT TRACK STA 875 AT FLOOR STRUCTURE PAX CABIN . CORRECTIVE ACTION: SUMMARY OF NRC 00102: LH/INBOARD SEAT TRACK STA 875 AT FLOOR STRUCTURE PAX CABIN WAS REPAIRED PER B 757-200 SRM. (1328322)

Part: SKIN — CORRODED (BS 1190-1200) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1325676) CORROSION ON INBD SIDE OF FUSELAGE SKIN BTW STA:1190 TO 1200 AND S-29L TO S-29R AT AFT CARGO COMPARTMENT. (FUS). CORRECTIVE ACTION: CORROSION LEVEL 1: AREA WAS REPAIRED PER ETI-57-19-140 REV. ORIGINAL AND ERA 582278-14 REV. ORIGINAL.

Part: FRAME — CRACKED (BS 1120) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1326073) INITIAL INSPECTION: CRACK ON FRAME AT STA 1120 BTW STR 9/8 RH AT PAX CABIN. (CPAX). CORRECTIVE ACTION: SUMMARY OF NRC 00348: FRAME WAS REPAIRED PER B757-200 SRM 53-00-07 REP 8. PERFORM DETAIL VISUAL INSPECION AT INTERVALE EVERY 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FRIST PER B757-200 SRM 53-00-07 REP. 8 STEP 5, TABLE 203, ZONE 3. (CURRENTLY A/C 26,887 CYCLES).

Part: FRAME — CRACKED (BS 1580) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 1324284) INITIAL INSPECTION. CRACK ON FRAME AT STA 1580 BTW STR 9/8 RH AT PAX CABIN. (CPAX). CORRECTIVE ACTION: SUMMARY OF NRC 00349: FRAME WAS REPAIRED PER B757-200 SRM 53-00-07 REP 8. MAINTENANCE REQUIREMENTS WERE VERIFIED AND FOLLOWINGS ACTION ARE NEEDED: PERFORM REPETIVE DETAIL INSPECTION AT INTERVALE EVERY 12,000 FLIGHT CYCLES OR 50,000 AIRFRAME CYCLES, WHICHEVER COME FIRST PER B757-200 SRM 53-00-07 REP 8 STEP 5 TABLE 203 (CURRENTLY A/C 26,887 CYCLES).

Part: FRAME — CRACKED (BS 1580) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640. L/P 1324296) INITIAL INSPECTION. CRACK ON FRAME AT STA 1580 BTW STR 9/8 LH AT PAX CABIN. (CPAX). CORRECTIVE ACTION: FRAME WAS REPAIRED PER B757-200 SRM 53-00-07 REP 8. MAINTENANCE REQUIREMENTS WERE VERIFIED AND FOLLOWINGS ACTION ARE NEEDED: PERFORM REPETIVE DETAIL INSPECTION AT INTERVAL EVERY 12,000 FLIGHT CYCLES OR 50,000 AIRFRAME CYCLES, WHICHEVER COME FIRST PER B757-200 SRM 53-00-07 REP 8 STEP 5 TABLE 203.

Part: SEAT TRACK — WORN (BS 875) · airframe 70,303 hrs · 26,887 cycles

SHIP 5640 INITIAL INSPECTION : WEAR ON LH/OUTBOARD SEAT TRACK STA 875 AT FLOOR STRUCTURE PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00104: SEAT TRACK WAS REPAIRED PER B-757-200 SRM. (1319998)

Part: SEAT TRACK — WORN (BS 870) · airframe 70,303 hrs · 26,887 cycles

SHIP 5640 INITIAL INSPECTION. WORN ON RH OUTBD SEAT TRACK STA 870 AT PAX CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00101: SEAT TRACK WAS REPAIRED PER B-757-200 SRM. (1319487)

Part: FLOOR SUPPORT — CORRODED (BS 1640-1670) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

CORROSION ON INTERCOSTAL UPPER CHORD AREA BTW STA Y=1640 TO STA Y=1670 BL 0,PAX CABIN STRUCTURE (W4). CORRECTIVE ACTION: INTERCOSTAL ON STA 1660-1680 WAS REPLACED PER B757-200 SRM 51-40-02 PAR 4 AND 7.

Part: FLOOR PANEL — DENTED (PAX CABIN) · airframe 70,303 hrs · 26,887 cycles

SEVERAL DENTS ON FLOOR PANELS 220-6 AND 220-7. IN THE PAX CABIN. NEW FLOOR PANELS WERE FABRICATED, AND INSTALLED IAW AMM 53-01-01-201.

Part: REPAIR — CORRODED (DECK PLATE) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

CORROSION ON PREVIOUS DOUBLER REPAIR AT DECK PLATE BTW STA 1675 TO STA 1690 AND RBL 6 TO RBL 20, PAX CABIN FLOOR STRUCTURE. DOUBLER REPAIR AT DECK PLATE BTW STA 1675 TO STA 1690 AND RBL 6 TO RBL 20 WAS REPLACED PER B757-200 SRM 53-60-51 REP 2.

Part: REPAIR — CORRODED (BS 1675-1690) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

CORROSION ON PREVIOUS DOUBLER REPAIR AT DECK PLATE BTW STA 1675 TO STA 1690 AND LBL 2 TO LBL 20, PAX CABIN FLOOR STRUCTURE (W2). CORRECTIVE ACTION: DOUBLER REPAIR AT DECK PLATE BTW STA 1675 TO STA 1690 AND LBL 2 TO LBL 20 WAS REPLACED PER B757-200 SRM 53-60-51 REP 2.

Part: REPAIR — CORRODED (BS 1700-1720) · corrosion level 2 · airframe 70,303 hrs · 26,887 cycles

CORROSION ON PREVIOUS DOUBLER REPAIR AT DECK PLATE BTW STA 1700 TO STA 1720 BL 0, PAX CABIN FLOOR STRUCTURE. DOUBLER REPAIR AT DECK PLATE BTW STA 1700 TO STA 1720 BL 0 WAS REPLACED PER B757-200 SRM 53-60-51 REP 2.

Part: SKIN — DENTED (BS 470) · airframe 70,303 hrs · 26,887 cycles

(AIRCRAFT 5640, L/P 5976084) DENT FOUND ON RIGHT SIDE FUSELAGE NEAR STATION 470 STRINGER 26. NEAR E/E DOOR. CORRECTIVE ACTION: SUMMARY: FUSELAGE SKIN BTW STA 470 BTW STRINGER 26RH AND 27RH WAS REPAIRED PER ETI-57-19-128. REV.5 AND ER/A 580564-14 REV. A SEC.III PERMANENT REPAIR. PLEASE CLOSE THIS LOG 5976084. AND PERFORM DAMAGE TOLERANCE EVALUATION ON OR BEFORE 24 MONTHS AFTER SECTION III, PER ER/A 580564-14 REV.A UNDER LP 1337637.

Part: NOT REPORTED — DENTED (FUSELAGE) · airframe 70,303 hrs · 26,887 cycles

SHIP 5640 DTE TRACKING FOR FUSELAGE DENT STA 470 STR 26R ADDRESSED VIA ER/A 580564-14 REVISION ORIGINAL. CORRECTIVE ACTION: PERMANENT REPAIR WAS C/W REF ERA 580564 SECTION III AND TRACKED ON LS 1337637. (1225330)

Part: LANYARD — OUT OF POSITION (ENTRY DOOR) · airframe 69,235 hrs · 26,612 cycles

SHIP 5640 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:602. CORRECTIVE ACTION: FOUND LANYARD CAUGHT IN GIRT BAR. SECURED SAME. DOOR SLID ARMING OPS NORMAL. (1142306)

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 68,540 hrs · 26,420 cycles

HANDLE FOR FOR DOOR R1 WILL NOT MOVE ALL THE WAY TO THE DISARM POSITION HANDLE STAYS MID WAY THROUGH TRAVEL. LOWER DOOR SEAL CAUGHT IN GIRT BAR MECHANISM CLEARED SEAL OUT OF THE WAY, DOOR ARMS/DISARMS NORMAL.

Part: DOOR — OBSTRUCTED (L2) · airframe 68,467 hrs · 26,401 cycles

L2 DOOR WILL NOT CLOSE. REMOVED OBSTRUCTION, NOW OPS NORMAL.

Part: PROBE — OUT OF LIMITS (RT MAIN TANK) · airframe 67,800 hrs · 26,222 cycles

SHIP 5640 - ATB, RETURNED TO DEPARTURE DUE TO RIGHT FUEL QUANTITY AND FUEL TOTALIZER BLANKED OUT 6 TIMES. RIGHT TU 8 OUT OF LIMITS. R/R'D RT MAIN TANK UNIT #8 PER BOEING 757 AMM 28-41-01. OPS CHECK GOOD.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 67,014 hrs · 25,999 cycles

SHIP 5640 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:602. EMERGENCY EXIT SIGN BROKEN 1R. CORRECTIVE ACTION: SECURED EXIT SIGN. (083526)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,144 hrs · 25,780 cycles

ON S/C FOUND EMER LIGHTS OUT AT ROWS 18-22 AND DOOR 2L. REMOVED AND REPLACED BATTERY PACK AT M732 PER AMM 33-51. CHECKS GOOD.

Part: INDICATOR — DIRTY (R2 DOOR) · airframe 65,732 hrs · 25,656 cycles

DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:604. CLEANED AREA AROUND KNUCKLE KNOCKER AT 2R DOOR OPS CHK GOOD.

Part: BUTTON — DAMAGED (SEAT 2C) · airframe 65,187 hrs · 25,504 cycles

SEAT 2C PASSENGER GOT FINGER STUCK IN ARMREST RELEASE BUTTON HOLE. REPLACED ARMREST IAW AMM 25-25.

Part: D-RING — UNSECURE (L1 DOOR) · airframe 64,869 hrs · 25,426 cycles

1L SURVIVAL PACK D-RING NOT SECURED IN APPROPRIATE SPOT. SECURED SURVIVAL PACK D-RING ON L1 DOOR- OK FOR SVC PER AMM 25-66.

Part: GIRT BAR — OBSTRUCTED (DOOR SLIDE) · airframe 61,412 hrs · 24,508 cycles

DOOR ARMED HANDLE INOPERATIVE, INSPECTED AND FOUND A METAL CLIP WITH LANYARD STUCK UNDER GIRT BAR. PLACED LANDYARD AND CLIP BACK INTO SLIDE. OPS CHECKED THE DOOR ARMING AND DISARMING. CHECKED GOOD IAW AMM 25-66. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,154 hrs · 24,440 cycles

SEAT ROW 43 TO 45 EMERGENCY LIGHT NOT TESTING. REMOVED AND REPLACED BATTERY ASSEMBLY ON M736. OPS CHECK NORMAL PER AMM 33-51.

Part: HANDLE — MALFUNCTIONED (R2 DOOR) · airframe 59,660 hrs · 24,056 cycles

R2 DOOR SHOWS CLOSED WITH HANDLE IN OPEN POSITION. HANDLE WILL NOT MOVE AND DOOR WILL NOT OPEN. REPOSITIONED THE R2 DOOR HANDLE TO CLOSED POSITION IAW AMM 52-11. OPS CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,633 hrs · 23,766 cycles

CEILING EMERGENCY LIGHTS ROW 21 AND 23 INOPERATIVE. FOUND BATTERY PACK AT M10919 BAD. REPLACED BATTERY PACK PER B757 AMM 33-51-07. OPS CHECKS GOOD. (9313692)

Part: SUPPORT BRACKET — DAMAGED (EMERGENCY LIGHT) · airframe 56,672 hrs · 23,206 cycles

ON SERVICE CHECK, FOUND DOOR 2R SUPPORT BRACKET THAT HOLDS EMERGENCY EXIT SIGN IN POOR CONDITION. REMOVED AND INSTALLED NEW EMERGENCY LIGHT ASSY AND FRAME ASSY. SLIDELIGHT AND EMERGENCY LIGHT OPS GOOD, IAW AMM 33-51.

Part: HANDLE — DETACHED (L4 DOOR) · airframe 55,870 hrs · 22,959 cycles

L4 DOOR HANDLE FELL OFF. REPLACED HANDLE, OK FOR SERVICE.

Part: DOOR SILL — CORRODED (BS 1440) · airframe 54,847 hrs · 22,634 cycles

AFT CARGO COMPARTMENT BS 1440, RBL20, DOOR SILL LOWER ANGLE FWD OF STANTION FITTING HAS AREAS OF CORROSION. REMOVED CORROSION AT BS 1440, RBL 20, DOOR SILL LOWER ANGLE, ORIGINAL MATERIAL THICKNESS .140", LOSS OF .025" WITH .115" REMAINING IS OUT OF LIMITS IAW SRM 53-60-15, PAGE 107, FIG 101 DETAIL VIII. COMPLIED WITH PRI 537913-14, REV 0 AND ER/A 537913-14 REV ORIGINAL FOR EXTENDED LIMITS ASSOCIATED ER/A 53-791314 ADDED FOR AC 5640.

Part: PAN — CORRODED (LAV SERVICE) · airframe 54,847 hrs · 22,634 cycles

AFT LAV SERVICE PANEL, PAN IS CORRODED AROUND DUMP TUBE, INTERIOR. EVALUATED CORROSION FOUND AFT LAV SERVICE PAN INTERNAL DOUBLER WITH 100 PERCENT MATERIAL LOSS REMOVED AND INSTALLED NEW INTERNAL DOUBLER IAW SRM 57-10-02, DWG 146N 36.50 PERFORMED TEST OF THE DRAIN DUCT HEATING GASKET IAW AMM 30-71-04-404-006 SUBTASK 704-025, STEP 9 PASS GOOD. PERFORMED LEAK CHECK ON AFT LAV WAST DRAIN SYSTEM IAW AMM 12-17-01, NO LEAKS NOTED.

Part: STRUCTURE — CORRODED (BS 334) · airframe 54,847 hrs · 22,634 cycles

PASSENGER CABIN FLOOR STRUCTURE BS 334, RBL 2, CHANNEL HAS AREA OF LIGHT CORROSION. BLENDED CORROSION IAW SRM 51-10-02, ORIG "T" .100 REMAINING .086 LOSS OF .014 LOSS IS OUT OF LIMITS IAW SRM 53-00-04, FIG 101. REPAIRED IAW PRI ER/A 537911-14, REV 0 AND ERA 537911-14, REV ORIGINAL ASSOCIATED ER/A 53-791114 ADDED FOR AC 5640.

Part: STRUCTURE — CORRODED (BS 334) · airframe 54,847 hrs · 22,634 cycles

PASSENGER CABIN FLOOR STRUCTURE BS 334, RBL 43, CHANNEL HAS AREA OF LIGHT CORROSION. BLENDED CORROSION IAW SRM 51-10-02, ORIG "T" .105 REMAINING .087 LOSS OF .018 LOSS IS OUT OF LIMITS IAW SRM 53-00-04. REPAIRED IAW PRI ER/A 537911-14, REV 0 AND ERA 537911-14, REV ORIGINAL ASSOCIATED ER/A 53-791114 ADDED FOR AC 5640.

Part: SKIN — DAMAGED (BS 310) · airframe 54,847 hrs · 22,634 cycles

UPPER FUSELAGE SKIN HAS A LIGHTNING STRIKE AT BS 310. REPAIRED IAW NDT PART 651-00-16, SRM 53-00-01.

Part: GUSSET — CRACKED (CARGO DOOR) · airframe 54,847 hrs · 22,634 cycles

FWD CARGO DOOR UPPER FWD CORNER INTERNAL SUPPORT STRUCTURE GUSSET CRACKED. EVALUATED AND REPLACED FWD CARGO DOOR UPPER FWD CORNER INTERNAL SUPPORT STRUCTURE GUSSET SUPPORT ANGLE IAW NDT PT6 51-00-19, SRM 51-40-02 PARA 4, 9; AMM'S 51-21-04-107-017, 51- 21-14-370-801, 51-21-10-377-003 & DWG 143N6603, REV AT.

Part: SKIN — DAMAGED (BS 1399) · airframe 54,847 hrs · 22,634 cycles

EXTERNAL FUSELAGE SKIN HAS 1 EA .0937" DIAMETER MISLOCATED FASTENER HOLE SPACED AT .350" FROM 1 EA .1562" DIAMETER FASTENER. HOLE AT BS 1399, 2" OTBD OF STR 2L. NDT AREA AND INSTALL RIVET IAW SRM 53-00-01, PARA 3.

Part: SKIN — DAMAGED (BS 1399) · airframe 54,847 hrs · 22,634 cycles

EXTERNAL FUSELAGE SKIN HAS 1 EA .0937" DIAMETER MISLOCATED FASTENER HOLE SPACED AT 0350" FROM 1 EA .1562" DIAMETER FASTENER. HOLE AT BS 1399, 2" OTBD OF STR 2R. NDT AREA AND INSTALLED RIVET IAW SRM 53-00-01, PARA 3.

Part: RESERVOIR — LOW PRESSURE (R2 DOOR) · airframe 53,788 hrs · 22,046 cycles

MAINTENANCE FOUND DOOR 2R RESERVOIR LOW. DOOR 2R EMERGENCY DOOR RESERVOIR WAS REPLACED. LP6755578.

Part: FUSE — LOOSE (EMERGENCY LIGHT) · airframe 53,582 hrs · 21,926 cycles

L4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE BATTERY PACK FUSE REPLACED FUSE LIGHT TEST OK IAW AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,124 hrs · 21,028 cycles

DURING SERVICE, FOUND ROW 29, ABC-33, EMERGENCY LIGHTS WOULD COME ON FOR 10-15 SEC THEN TURN OFF. SWAPPED BATTERY FOR NEW, NO HELP, SWAPPED CHARGER, NO HELP. REPLACED BATTERY PACK ON EMERGENCY LIGHTS POWER SUPPLY M10699, SYS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,065 hrs · 20,990 cycles

ON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE ON SEATS 29-33 ABC. REPLACED BATTERY CHARGER M735, CHECKED OK IAW AMM 33-51.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,916 hrs · 20,887 cycles

FOUND SEAT MOUNTED EMERGENCY LIGHTS BETWEEN ROW 29-33 INOPERATIVE. R & R CHARGER & BATTERY PACK AT ROW 30/31 IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,426 hrs · 20,595 cycles

L4 DOOR OVERHEAD EMERGENCY EXIT SIGN, R4 LOWER EMERGENCY EXIT SIGN AND OVERHEAD AFT GALLEY EMERGENCY EXIT SIGN INOPERATIVE. FOUND M737 EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY AT FAULT. REPLACED, ALL EMERGENCY EXIT SIGNS NOW CHECKED GOOD. MAINTENANCE DONE IAW AMM 33-51.

Part: FAN — FAILED (RECIRCULATION) · airframe 51,065 hrs · 20,352 cycles

CREW DECLARED EMERGENCY FOR LIGHT SMOKE/HEAVY ACRID ODOR IN COCKPIT AND FORWARD CABIN ON APPROACH, LANDING, & TAXI IN. REPLACED RT RECIRCULATION FAN AND FILTER. INSPECTED RIGHT FAN CHECK VALVE, CHECKS NORMAL. NO FAULTS FOUND ON VMU.

Part: ANGLE — CRACKED (NACELLE) · airframe 50,218 hrs · 19,833 cycles

ANGLE COMMON TO HYD DISCONNECT DOUBLER FOUND CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ALL IAW SRM 51-40-02 PG 6 & 7

Part: ANGLE — CORRODED (BS 765-770) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

FWD CARGO ZEE ANGLE CORRODED BS 765-770. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53 PG. 105. INSTALLED NEW ANGLE IAW SRM 51-40-02 PGS 1-12.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN, BS 720 RBL 45.5, OTBD SEAT TRACK FLANGE IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK AND INSTALLED NEW IAW SRM 53-00-52 1A-1, 51-40-02 PG 8-10, AND DRAWING 143A5120-4

Part: SEAT TRACK — CORRODED (BS 720) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN, R2 DOOR ENTRY AREA, O/B SEAT TRACK UPPER CROWN CORRODED BETWEEN BS 720. REPAIRED SEAT TRACK IAW ER/A 519870-14 REV ORIGINAL AND PRI 519870-14 REV O.

Part: SKIN — DAMAGED (BS 211) · airframe 50,218 hrs · 19,833 cycles

LOWER FUSELAGE SKIN, BS 211, RBL 25, SKIN IS RECESSED OR BLENDED AROUND FASTENER. REPAIRED SKIN IAW ER/A 519843-14 REV ORIGINAL AND PRI 519843-14 REV O.

Part: SKIN — DAMAGED (BS 265-269) · airframe 50,218 hrs · 19,833 cycles

LOWER FUSELAGE SKIN, BS 265 - 269, LBL 25 - RBL 30, SKIN IS RECESSED OR BLENDED AROUND FASTENERS. REPAIRED SKIN IAW ERA 519843-14 REV ORIGINAL AND PRI 519843-14 REV O.

Part: DOUBLER — CRACKED (NR 2 PYLON) · airframe 50,218 hrs · 19,833 cycles

NR 2 PYLON HYDRAULIC DISCONNECT PANEL DOUBLER CRACKED AT LOWER END BELOW LOWER AFT HYDRAULIC FEED THRU HOLE. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02 PG 6 & 7

Part: SEAT TRACK — CORRODED (BS 720) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN, R2 DOOR ENTRY AREA, SEAT TRACK UPPER CROWN CORRODED BETWEEN BS 720 RBL-24.5. REPAIRED SEAT TRACK IAW ERA 519870-14

Part: SKIN — DAMAGED (BS 310) · airframe 50,218 hrs · 19,833 cycles

LOWER FUSELAGE SKIN, BS 310, 4 INCHES OUTBOARD OF LEFT SIDE NOSE WHEELWELL CUTOUT, SKIN IS RECESSED OR BLENDED AROUND FASTENER. REPAIRED SKIN IAW ER/A 519843-14 REV ORIGINAL AND PRI 519843-14 REV O.

Part: SKIN — DAMAGED (BS 204-221) · airframe 50,218 hrs · 19,833 cycles

LOWER FUSELAGE SKIN, BS 204 - 221, LBL 3 - RBL 3, SKIN IS RECESSED OR BLENDED AROUND FASTENERS. REPAIRED SKIN IAW ER/A 519843-14

Part: ANGLE — CORRODED (BS 1260-1310) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO BS 1260-1310 ZEE ANGLE CORRODED . REMOVED AND REPLACED ANGLE IAW ERA NO 373211-14MA REV G.

Part: FLOOR SUPPORT — CORRODED (BS 1440) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO BAY BS 1440 FLOOR SUPPORT CORRODED FWD LOWER CORNER RBL 31. REPAIRED IAW SRM 51-40-02 PG 4-5 & DWG 146N3305.

Part: ANGLE — CORRODED (BS 720-760) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

FWD CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 720-760. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 PG 101 AND 105 DTL IV, REMOVED AND REPLACED SPLICE IAW SRM 51-40-02 PGS 1-5.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 50,218 hrs · 19,833 cycles

RIGHT OTBD FLAP LEADING EDGE WORN. BLENDED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01. REPAIRED IAW SRM 51-53-01 AND AMM 51-21.

Part: ANGLE — CORRODED (BS 1460-1472) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO, BS 1460-1472 ZEE ANGLE CORRODED AROUND FASTNER HOLES. REPLACED ANGLE FROM BS 1410-1530 IAW ERA 373211-14.

Part: SUPPORT ANGLE — CORRODED (BS 845) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

FWD CARGO BAY AFT WALL LOWER SUPPORT ANGLE CORRODED, BS 845 RBL 20-LBL 20. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED LOWER SUPPORT ANGLE AND FABRICATED REPAIR. PRIMED AND TREATED IAW SRM 51-10-02, SRM 53-00-53, SRM 51-40-02 AMM 51-21-04-107-017 PG 1-6, AMM 51-21-10-377-003 PGS 1-3 & DWG 453N814-16.

Part: THRESHOLD — CORRODED · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO DOORWAY BOTTOM THRESHOLD CORRODED AROUND FASTNER HOLES. REPAIRED IAW SRM 53-60-15 & AMM 51-21-10 PG 1-3.

Part: BRACKET — CORRODED (BS 1080) · airframe 50,218 hrs · 19,833 cycles

LOWER EXTERIOR FUSELAGE, BS 1080 + 10 AND 16" BELOW STRINGER 17L, WING TO BODY FAIRING SUPPORT BRACKET CORRODED. R & R BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CORRODED (BS 1060) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

LOWER EXTERIOR FUSELAGE, BS 1060 AND 16 INCHES BELOW S17R, WING TO BODY FAIRING SUPPORT BRACKET IS CORRODED. FOUND OUT OF LIMITS IAW SRM 53- 00-71. FABRICATED & INSTALLED NEW SUPPORT ANGLE IAW DWG 149N7550. SHEET 25 REV G.

Part: STRAP — BROKEN (FLOORBEAM) · airframe 50,218 hrs · 19,833 cycles

BS 377.7 LBL 24, PASSENGER CABIN FLOORBEAM STABILIZER STRAP BROKEN. CUT OUT DAMAGE, INSPECTED AND FABRICATED REPAIR IAW ERA 384483-14MA TREAT AND PRIMED.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO, CORROSION ON BOTH ENDS OF INTERCOSTAL BS 1480 TO 1500 BETWEEN STRINGERS 26 AND 27R. REMOVED CORROSION IAW SRM 51-10-02. MATCH DRILLED NEW INTERCOSTAL AND INSTALLED IAW SRM 51-40-05 AND SRM 51-40-02.

Part: BUSHING — MIGRATED (NR 1 NACELLE) · airframe 50,218 hrs · 19,833 cycles

NR 1 PYLON UPPER LINK FITTING BUSHING MIGRATED. REMOVED, INSPECTED AND REPAIRED IAW SRM 54-51-90.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO BAY BS 1510 FLOOR SUPPORT CORRODED AT LBL 7. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-40-02 SRM 51-40-05, AMM 51-21-10-377-003, AMM 51-24-03-917-011, AND DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN FWD WET AREA FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-15. REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 328-365) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN FWD WET AREA FLOOR SUPPORT CORRODED BS 328-365. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 PG 1-3.

Part: GROUND STUD — LOOSE · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

LEFT AIR CONDITION BAY, GROUND STUD BRACKET AND GROUND STUD GD01187S HAVE CORROSION, BS 900 LBL 15. REMOVED CORROSION FROM GROUND STUD BRACKET IAW SRM 53-00-01. REPLACED GROUND STUD AND BRACKET IAW DWG 287N4904.

Part: BRACKET — CORRODED (DOOR SILL) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

RIGHT PASSENGER DOOR LOWER SILL UPPER SURFACE, THRESHOLD PLATE MOUNTING BRACKETS CORRODED. REMOVED CORROSION , FWD BRACKET WITHIN LIMITS, TREATED, PRIMED AND TOP COATED IAW SRM 51-20-01. AFT BRACKET FOUND TO BE OUT OF LIMITS. FABRICATED AND REPLACED AFT BRACKET IAW DWG 146N8016 & 146N8722.

Part: ATTACH FITTING — CORRODED (BS 600) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

FWD CARGO DOOR CUT OUT LOWER SILL ATTACH ANGLE CORRODED RBL 22 BS 600 . REMOVED AND REPLACED ATTACH FITTING IAW DRAWING 143N8560, 143N8522 AND SRM 51-40-02 .

Part: SEAT TRACK — CORRODED (BS 377) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN FWD WET AREA SEAT TRACK CORRODED BS 377 LBL 24. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-52. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-05 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 334-342) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN FWD WET AREA FLOOR SUPPORT CORRODED, BS 334-342 LBL 21. REMOVED CORROSION IAW SRM 51-10-02 AND DRILL NEW FLOOR SUPPORT IAW DWG 141N1570 AND SRM 51-40-05 PG. 1.

Part: BRACKET — CORRODED (DOOR SILL) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

L4 DOOR LOWER SILL UPPER SURFACE, THRESHOLD PLATE MOUNTING BRACKET CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. REMOVED BRACKET IAW SRM 757 51-40-02 PG 1-7. NEW BRACKET FABRICATED IAW DWG 146N8016.

Part: SHEAR WEB — CORRODED (CABIN) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN SHEAR WEB. CLEANED CORROSION, FOUND OUT OF LIMITS AND REPAIRED IAW SRM 53-60-51.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN AFT WET AREA UPPER SURFACE OF SHEAR WEB ABOVE BS 1681.8 FLOORBEAM IS CORRODED FROM APPROX LBL-2 TO LBL-31. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51. REMOVED DAMAGE AND REPAIRED IAW SRM 53-60-51.

Part: FLOOR SUPPORT — CORRODED (BS 365) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN FWD WET AREA FLOOR SUPPORT CORRODED BS 365, BL 0. REMOVED CORROSION IAW SRM 53-00-04. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1661) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN LT AFT WET AREA FLOOR SUPPORT, INBD OF CUSP WEB, AT L4 DOOR SCUPPER DRAIN, BETWEEN BS 1640 AND 1661, LBL 58-56 CORODED. R & R FLOOR SUPPORT IAW SRM 51-40-02, DWG NR 146N8722 AND DWG 146N5230.

Part: FLOOR SUPPORT — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

PASSENGER CABIN LT AFT WET AREA FLOOR SUPPORT, INBD OF CUSP WEB, AT L4 DOOR SCUPPER DRAIN TROUGH, BETWEEN BS 1661 - 1681, LBL-54-56, CORRODED ON LOWER AND UPPER SURFACE. R & R FLOOR SUPPORT IAW DWG 146N5230.

Part: ANGLE — CORRODED (BS 1480-1500) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO, BS 1480-1500 ZEE ANGLE CORRODED AROUND FASTNER HOLES. ZEE ANGLE REPLACED. CORROSION CLEANED OUT OF LIMITS IAW SRM 53-00-53.

Part: ANGLE — CORRODED (BS 1508-1520) · corrosion level 2 · airframe 50,218 hrs · 19,833 cycles

AFT CARGO, BS 1508-1520 ZEE ANGLE CORRODED AROUND FASTNER HOLES. ZEE ANGLE REPLACED. CORROSION CLEANED OUT OF LIMITS IAW SRM 53-00-53.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 4,378 hrs · 1,446 cycles

DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHT AT ROW 29 TO 32 INOP. MAINTENANCE REPLACED WEAK BATTERY AT MID BATTERY PACK AT SEAT ABOVE ROW 30 AND 31. EMERGENCY LIGHTS NOW CHECK OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 44,560 hrs · 16,952 cycles

EMERGENCY LIGHT INOPERATIVE AT LAV S (DR2L). SECURED ELECTRIC CONNECTOR IN FRONT OF LAV S WALL. OK FOR SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 44,333 hrs · 16,874 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 5B INOPERATIVE. MAINTENANCE REPAIRED THE WIRES. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,327 hrs · 16,872 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 16C INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,079 hrs · 16,793 cycles

DOOR 2R EXTERNAL EMERGENCY LIGHT INOPERATIVE. PERFORMED PWE SUPPLY AT DOOR 2R AS PER MM B757 33-51-07. OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,052 hrs · 16,785 cycles

EMERGENCY LIGHT ON AFT CARGO DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT STATION 1240. AIRCRAFT IS NOW OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,862 hrs · 116,714 cycles

FOUND EMERGENCY PATH LIGHT AT ROWS 29 TO 33 INOPERATIVE. IN ADDITION, THE EXTERIOR EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. MAINTENANCE REPLACED BATTERY ASSEMBLY ABOVE 31DEF ON POWER SUPPLY. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 2,746 hrs · 899 cycles

DURING A LINE CHECK, MAINTENANCE FOUND AN EMERGENCY PATH LIGHT AT LAV 2L INOPERATIVE. MAINTENANCE REPAIRED THE WIRING. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 39,351 hrs · 15,183 cycles

DURING LINE CHECK FOUND SEATS 39ABC THRU 42ABC SEAT MOUNTED EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. MAINTENANCE REPLACED M736 POWER SUPPLY. SYSTEM OPERATION WAS NORMAL AFTER POWER SUPPLY WAS REPLACED.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 39,350 hrs · 15,182 cycles

DURING LINE CHECK FOUND AFT RIGHT SIDE EMERGENCY AISLE LIGHTS INOPERATIVE. MAINTENANCE REPLACED M736 POWER SUPPLY AND BATTERY. SYSTEM OPERATION WAS NORMAL AFTER POWER SUPPLY AND BATTERY WERE REPLACED.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS)

DURING AN OVERNIGHT LINE CHECK, THE EMERGENCY LIGHT FOR THE RT AFT OVER WING EXIT WOULD NOT ILLUMINATE. MX FOUND THE ASSOCIATED BATTERY PACK TO BE DEFECTIVE AND REPLACED IT. SYS OPERATION WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED. (K)

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 36,337 hrs · 14,092 cycles

DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTS FROM ROW 29 ON THE RT SIDE TO ROW 33 ON THE RT SIDE WERE INOPERATIVE. MX FOUND BATTERY PACK M10699 TO BE DEFECTIVE AND REPLACED IT. ALL OPS CHECKED NORMAL AFTER REPLACEMENT.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 36,310 hrs · 14,081 cycles

DURING OVERNIGHT MX THE ESCAPE PATH LIGHTING IN ROWS 28 THROUGH 33 WERE FOUND TO BE INOPERATIVE. THE BATTERY PACK ASSOCIATED WITH THESE LIGHTS WAS FOUND TO BE INOPERATIVE. MX REPLACED POWER SUPPLY K735. ALL OPS WERE NORMAL AFTER REPLACEMENT OF THE POWER SUPPLY.

Part: PROBE — UNKNOWN (NR 1 ENGINE) · airframe 36,230 hrs · 14,052 cycles

DURING CRUISE FLIGHT AT 37,000FT ENG NR 1 FLAMEOUT. FLIGHT CREW WAS SUCCESSFUL IN RESTARTING ENG NR 1 AND CONTINUED TO DESTINATION. MAINTENANCE REPLACED ENG NR 1 PT2/TT2 PROBE, EEC AND PERFORMED BOROSCOPE INSPECTION. (S)

Part: SKIN — DENTED (BS 625 S14L) · airframe 35,261 hrs · 13,700 cycles

DURING "M" CHECK FOUND DENT IN FUSELAGE SKIN AT BS 625 S14L. REPAIRED PER EA 56-210586 SECTION I, SECTION II REQUIRES SUPPLEMENTAL INSPECTION ON OR BEFORE 37,500 CYCLES ARE REACHED. SECTION III REQUIRES REPEAT INSPECTION NOT TO EXCEED EVERY 3000 CYCLES AFTER ACCOMPLISHMENT OF SECTION II.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,842 hrs · 13,552 cycles

DURING OVERNIGHT LINE CHECK, FOUND SEATS 4, 5, 6, LAV2L, AND F/A SEAT 2L EMERGENCY LIGHTS INOP WHEN TESTED. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: VIDEO UNIT — OVERHEATED (NR 2 CLOSET) · airframe 15,967 hrs · 6,484 cycles

EN ROUTE TO DTW, NR 2 GALLEY DOOR 2 PANEL INSIDE CLOSET AREA FEELS VERY WARM AND HAS WIRE/PLASTIC BURNING ODOR. REPLACED VIDEO MONITOR CONTROL BOX.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING PREFLIGHT, FOUND DOOR 1L EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK OK.

Part: BLADE — BENT (NR 1 ENG COMP)

DURING CLIMB AT 7,000 FT, NR 1 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. AIRCRAFT RETURNED TO MSP. GROUND MAINTENANCE FOUND TWO BENT FAN BLADES. REPLACED BLADES, PMA STATOR AND PROBE CURRENT SENSE RELAY. ENGINE OPERATIONAL CHECK OK.