N679DA

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,189 hrs · 42,206 cycles

SHIP 0679 HISTORY OF 2R DOOR ARMED SLIDE LIGHT. CORRECTIVE ACTION: TROUBLESHOOT PER B757 WDM 25-66. REMOVED AND REPLACED BOTH PROX SENSORS S10221 AND S10220 PER AMM 25-66-11. SYS OPS CK GOOD. (0025253)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,160 hrs · 42,190 cycles

SHIP 0679 R2 DOOR SLIDE LIGHT ILLUMINATED W/ LEVER DISARMED. CORRECTIVE ACTION: CYCLED R2 DOOR ARMING LEVER SEVERAL TIMES. DOOR ARM/DISARM OPS CK NORMAL REF B757 AMM 25-66. (4316209)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,152 hrs · 42,183 cycles

SHIP 0679 DOOR 1R GIRT BAR LOCK FOUND IN GALLEY. LOCK BROKEN FREE FROM GIRT BAR. CORRECTIVE ACTION: REINSTALLED R1 DOOR GIRT BAR SLIDER. DOOR ARMS OKAY PER B757 AMM 25-66. OKAY FOR SERVICE. (4604698)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,091 hrs · 42,146 cycles

SHIP 0679 F/A CALLED AFTER WE ARRIVED AT GATE INFORMED US THE 2R DOOR DISARM LEVER WAS DISARMED BUT THE SLIDE LIGHT REMAINED ILLUMINATED. CORRECTIVE ACTION CYCLED 2R DOOR ARM/DISARM LEVER AND SLIDE LIGHT OPERATES NORMALLY IAW B757 AMM 25-66. OK FOR SERVICE. (460466)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,996 hrs · 42,088 cycles

SHIP 0679 -MISC/DE- TO ATL DUE TO SUSPECTED BIRD STRIKE. CORRECTIVE ACTION: PERFORMED BIRD STRIKE INSPECTION. REMOVED AND INSTALLED FULL SET OF 1ST STAGE LPC BLADES ON #2 ENGINE. RAN ENGINE, ALL CHECKS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,975 hrs · 42,074 cycles

SHIP 0679 R2 DOOR SLIDE LIGHT STAYS ILLUMINATED WITH DOOR DISARMED. CORRECTIVE ACTION: ARMED AND DISARMED DOOR CKS NML PER B757 AMM 52-10.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,816 hrs · 41,979 cycles

SHIP 0679 2R SLIDE LIGHT REMAIN ILLUMINATED. CORRECTIVE ACTION: CYCLED SLIDE DOOR LEVER, SLIDE LIGHT OFF CKS GOOD OK FOR SERVICE. (4615730)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,813 hrs · 41,977 cycles

SHIP 0679 WHEN A/C WAS BROUGHT UP TO GATE, SUPER TUG COULD NOT OPEN L2 DOOR. CORRECTIVE ACTION: FOUND INTERIOR HANDLE ON 180 DEG OUT, RE INSTALLED HANDLE IN CORRECT POSITION, DOOR OPEN/CLOSES NML PER B757 AMM 52-11 (4615722)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,452 hrs · 41,739 cycles

SHIP 679 F/A REPORTS EMERG EXIT LIGHTS ILLUMINATED IN FLIGHT FROM OVERWING EXITS AFT. RESET F/A PANEL SWITCHES AND COCKPIT SWITXCHES, NO HELP.: CORRECTIVE ACTION: RESET EMER. LIGHT SYS, OPS CK NML. (4400610)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,344 hrs · 41,678 cycles

SHIP 679 ESCAPE SLIDE ARMED CONDITION INDICATORS 2L DOOR KNUCKLE KNOCKER INOP. CORRECTIVE ACTION: FLIGHT CREW PLACARD INSTALLED AT ATL PER MEL 25-66-04A. (2817888)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,103 hrs · 41,548 cycles

SHIP 679 DURING SERVICE CHECK FOUND LEFT FWD OVER-WING EMERGENCY EXIT LIGHT INOP AT SEATROW 26ABC. CORRECTIVE ACTION: OUND POWER SUPPLY BAD AT SIDEWALL/SEATROW 27ABC REPLACED POWER SUPPLY REF B757 AMM33-51. (4766587)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,912 hrs · 41,417 cycles

SHIP 679 2R DOOR SLIDE LIGHT WILL NOT DISARM. CORRECTIVE ACTION: CYCLED GIRT BAR HANDLE. SLIGHT LIGHT OPS CHECK GOOD. B757 AMM 52 -11. (8926482)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,903 hrs · 41,411 cycles

SHIP 679 ON SVC CHECK FOUND EMERG EXIT SIGN NOT LIGHTING ON TEST, LOC OWEED LH SIDE FWD, ROW 26A. CORRECTIVE ACTION: R/R LT OWEED LOWER EMERGENCY EXIT SIGN PER B757 AMM 33-51. OPS CHK GOOD. (8926476)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,903 hrs · 41,411 cycles

SHIP 679 N SVC CHECK FWD SEAT EMERG LIGHT AT 36D HANGING. CORRECTIVE ACTION: RE-SECURED LOOSE EMERGENCY ASSY AT SEAT 36D AS REQUIRED. (8926474)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,903 hrs · 41,411 cycles

SHIP 679 ON SVC CHECK FOUND L4 EXIT SIGN AND LOWER EMERG. EXIT SIGN ON LIGHTING ON TEST. CORRECTIVE ACTION: R/R L4 DOOR EMERGENCY BATTERY FOR EMERGENCY LIGHTS OPS CHECK GOOD REF B757 AMM 33-51. (8926475)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,890 hrs · 41,403 cycles

SHIP 679 R4 EMERGENCY LIGHTS AROUND DOOR INOP. CORRECTIVE ACTION: R/R R4 BATTERY PACK I.A.W. B757 AMM 33-51. OPS CK GOOD. (8926453)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,865 hrs · 41,386 cycles

SHIP 679 2R DOOR MANUALLY DISARMED HOWEVER SLIDE LIGHT STILL ILLUMINATED. CORRECTIVE ACTION: T/S IAW B757 AMM FRM/FIM 52-11-00-815-802. AND TESTED IAW AMM 52 -11-00-862-077.OPS. CHECKS NORMAL AT THIS TIME. (8926438)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,743 hrs · 41,328 cycles

SHIP 679 EMERG LIGHTS AT 4L DR WILL NOT SHUT OFF. CORRECTIVE ACTION: REMOVED & RE-INSTALLED BATTERY IN POWER SUPPLY, M737. REF B757 AMM 33-51. OPS CK GOOD. (4057688)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,750 hrs · 41,332 cycles

SHIP 679 2R EMERGENCY EXIT SIGN FELL OFF. CORRECTIVE ACTION: REINSTALLED EXIT SIGN PER B757 AMM 33-20. (4057692)

Part: UNKNOWN — UNKNOWN · airframe 91,633 hrs · 41,253 cycles

SHIP 0679 - ATB - JUST AFTER TAKEOFF WEATHER RADAR FAILED. CORRECTIVE ACTION: REPLACED WEATHER RADAR TRANSCEIVER, RADAR DRIVE UNIT. OPS CK GOOD.

Part: POWER SUPPLY — FAULTED (PAX DOOR) · airframe 91,142 hrs · 40,965 cycles

PRIOR TO PUSH BACK 2 FWD EMER DOOR CAS MESSAGE AND EMER DOOR LIGHT ILLUMINATED. R & R PSEU IAW AMM 32-09-04, OPS CHECKED GOOD, NO EICAS MESSAGE OR FAULTS PRESENT. ORIG SUBMISSION DATE: 12/23/2022

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 91,078 hrs · 40,928 cycles

EMERGENCY LIGHT AT SEAT 45D INOPERATIVE. REPAIRED A BROKEN WIRE AT SEAT CONNECTOR IAW 20-42-01 SWPM. OPS TESTED GOOD.

Part: LANYARD — OUT OF POSITION (L3 DOOR SLIDE) · airframe 90,988 hrs · 40,870 cycles

L3 DOOR HAS SLIDE LANYARD HANGING OUT BOTTOM OF DOOR. CORRECTIVE ACTION: CONNECTED BUSTLE STRAP.

Part: LANYARD — OUT OF POSITION (RAFT) · airframe 90,973 hrs · 40,863 cycles

L3 DOOR RAFT LANYARD STICKING OUT OF THE BOTTOM OF THE RAFT BAY. STOWED THE LANYARD.

Part: UNKNOWN — UNKNOWN · airframe 90,438 hrs · 40,481 cycles

SHIP 679 ESCAPE SLIDE ARMED CONDITION INDICATORS 2L KNUCKLE KNOCKER INOP. CORRECTIVE ACTION: INSPECTED DOOR 2L AND OP TEST OK AS PER B757 AMM 52-11 CANNOT DUPLICATE FAULT. KNUCKLE BUSTER EXTENDS FINE. (2380496)

Part: SCREW — MISALIGNED · airframe 90,145 hrs · 40,251 cycles

SHIP 679 F/A ADVISE DISARM PLACARD INTERRERING WITH ARMING LEVER ON 1R ENTRY DOOR. CORRECTIVE ACTION: RESSEUCRED SCREW ON HANDLE. WILL ARM RIGHTW/HANDLE. (8600533)

Part: NONE — NONE · airframe 90,131 hrs · 40,241 cycles

SHIP 679 EASUREMENTS OUT OF TOLERANCE IN HOLES # 2, 7, 10, 11, 12, 13, 15, 16 AND 17 AT RH ENG DRAG FITTING. (IN REF AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00234: HOLES OF RH ENG DRAG FITTING WERE REPAIRED PER ER/A 588833-14AD REV. B SECTION VI PERMANENT REPAIR AND PRI 588833-14, REV. 1 (2302598)

Part: NONE — NONE · airframe 90,131 hrs · 40,241 cycles

SHIP 679 MEASUREMENTS OUT OF TOLERANCE IN HOLES # 7 AND 8 AT LH ENG DRAG FITTING. (IN REF AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00248: REPAIR WAS PERFORMED PER PRI 588963-14 REV 0 AND ERA 588963-14AD REV B.SECTION V. (2299715)

Part: SKIN — CORRODED · corrosion level 2 · airframe 90,131 hrs · 40,241 cycles

SHIP 679 CORROSION ON UPPER SKIN OF INBD MAIN FLAP MFSTA. 220 APPROX AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00114: UPPER SKIN OF INBD MAIN FLAP MFSTA. 220 APPROX WAS REPAIRED PER B757-200 S.R.M. (2292292)

Part: FASTENER — DAMAGED · airframe 90,131 hrs · 40,241 cycles

SHIP 679 PROTUBERANCE AROUND REPAIR FASTENER, STA. 441 BTW. S-25R TO S-26R AT OUTER FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00050. AREA WAS REPAIRED PER PRI 600108-14 REV 2 AND ER/A 600108-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (2289142)

Part: WEDGE — DEBONDED · airframe 90,131 hrs · 40,241 cycles

SHIP 679 A.A. - A.D. 03 DISBONDS ON UPPER SURFACE, LE SLAT 6 TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC: 0030 UPPER SURFACE, LE SLAT 6 TRAILING EDGE WEDGE, RH WING. ISS 208:, ISS 171: AND ISS 158: WAS REPAIRED PER B757-200 S.R.M. (2286846)

Part: LEAF SPRING — INOPERATIVE · airframe 90,131 hrs · 40,241 cycles

SHIP 679 DURING INSPECTION OF THE GIRT BAR AT 1L DOOR, FWD/AFT LEAF SPRINGS DOESN T RETAIN THE SLIDER WHEN LIGHT FINGER PUSH IS APPLIED. (IN REFERENCE AMDS AD). CORRECTIVE ACTION: SUMMARY OF NRC 00150:FWD/AFT LEFT SPRINGS WERE REPLACED PER B757 -200 SRM 51-40-02-0G PAR 4B AND ENGAGEMENT TEST ON GIRT BAR AT 1L DOOR, FWD/AFT LEFT SPRINGS WAS PERFORMED PER AMDS. (2286422)

Part: NONE — NONE · airframe 89,107 hrs · 39,712 cycles

SHIP 679 EXTERIOR EMERGENCY LIGHTING SYSTEM /BATTERY POWERED/2L EXT DOOR EMERG LIGHT. CORRECTIVE ACTION: R+R LIGHT BULB R/R L2 EMERGENCY LIGHT BATTERY PACK PER B757 AMM 33-51. OPS GOOD. (8156461)

Part: NONE — NONE · airframe 89,060 hrs · 39,674 cycles

SHIP 679 JUST PRIOR TO DESCENT, EMERGENCY LIGHTS F/O SIDE SEAT 18-21, ROW 2L EMER EXIT SIGN AND EMER LIGHTS AT ROW 2L CAPTS SIDE ALL CAME ON. CORRECTIVE ACTION: UPON EXAMINATION, FOUND SEAT MOUNTED ESCAPE LIGHTS ROW 18-22 INOP. T/S PER B757 FIM 33-51. RESET CONNECTOR AT R2 DOOR EMERGENCY BATTERY PACK CHARGER; LIGHTS NOW OPERATE NORMALLY. (8156428)

Part: NONE — NONE · airframe 89,012 hrs · 39,656 cycles

SHIP 679 STRING HANGING OFF SLIDE ON DOOR 1 RT (ONE RIGHT). CORRECTIVE ACTION: RESECURED R1 SLIDE PACK LANYARD. (8016498)

Part: NONE — NONE · airframe 88,787 hrs · 39,544 cycles

SHIP 679 3L DOOR DOES NOT SEEM TO ARM PROPERLY. CORRECTIVE ACTION: CLEARED DEBRI FROM DOOR SILL. ARMING MECHANISM CKS OK. (6887372)

Part: SKIN — DAMAGED (RT WING) · airframe 88,487 hrs · 39,386 cycles

SHIP 679 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588833-14 REV A. CORRECTIVE ACTION: REF 588833-14 REV A. (1932655)

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 88,134 hrs · 39,227 cycles

SHIP 679 L-1 GIRT BAR DAMAGED. CORRECTIVE ACTION: REMOVED AND INSTALL GIRT BAR REF B757 AMM 25-66-10 AND ADJUSTED/ TESTED REF B757 AMM 52-11. (1891059)

Part: LATCH — BROKEN (L2 DOOR SLIDE) · airframe 88,134 hrs · 39,227 cycles

SHIP 679 L2 DOOR BUSTLE LOWER CTR LANYARD LATCH BROKEN. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 016-0001:0514-2001/008 00014 REPLACED LATCH. REF B-757 AMM 25-66. (1889564)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 87,774 hrs · 39,071 cycles

SHIP 679 AIRPLANE WAS DEPOWERED + EMERGENCY LIGHTS WERE ARMED + ONE SECTION OF EMERGENCY LIGHTS WERE ILLUMINATED. ONCE PWR WAS SUPPLIED TO AIRPLANEWE CHECKED EMER LIGHTS THEY ILLUMINATED FOR NO MORE THAN 15 SEC. CORRECTIVE ACTION: CHARGED THE POWER SUPPLY BATTERY PACKS PER B757 AMM 33-51-07 ALL EMERGENCY LIGHTS OPS CHECK GOOD PER B757 AMM 33-51. (7753153)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 87,616 hrs · 39,003 cycles

SHIP 679 FIRST FLIGHT OF DAY, AIRPLANE WAS DEPOWERED, EMERGENCY LIGHTS WERE ARMED, ONE SECTION OF EMERGENCY LIGHTS WERE ILLUMINATED. ONCE PWR WAS SUPPLIED TO AIRPLANE WE CHECKED EMER LIGHTS, THEY ILLUMINATED FOR NO MORE THAN 15 SEC THEN EXTINGUISH. CORRECTIVE ACTION: CHARGED THE POWER SUPPLY BATTERY PACKS. ALL EMERGENCY LIGHTS OPS CHECK GOOD. (LP 7753453)

Part: DRAG FITTING — CORRODED (LT ENG MOUNT) · corrosion level 2 · airframe 86,538 hrs · 38,572 cycles

WHILE PERFORMING LT ENGINE DRAG FITTINGS CLAMP-UP & DIAGONAL BRACE INSPECTIONS MAINTENANCE FOUND CORROSION ON HOLES 1-5, 7, 8, 11-18, AT OUTER WING UPPER SKIN AND DRAG FITTINGS. REPAIRED PER ERA 588963-14.

Part: DRAG FITTING — CRACKED (RT ENGINE) · airframe 86,538 hrs · 38,572 cycles

DURING INSPECTION, MAINTENANCE FOUND CRACKED PAINT AROUND THE FASTENER HEAD NR 3, 7 AND 8 RT ENGINE DRAG FITTING CLAMP-UP & DIAG BRACE. REPAIRED PER ERA 588833-14.

Part: DRAG FITTING — DAMAGED (RT ENGINE) · corrosion level 2 · airframe 86,538 hrs · 38,572 cycles

DURING INSPECTION MAINTENANCE FOUND HOLES AT RT ENGINE DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW: HOLE NR 1 SCRATCHES ON SKIN AND FITTING BETWEEN 9 AND 10 O'CLOCK POSITION; HOLE NR 2 TEARS ON SKIN AND FITTING BETWEEN 1 AND 2 O'CLOCK POSITION; HOLE NR 4 TEARS ON SKIN BETWEEN 9 AND 10 O'CLOCK POSITION AND TEARS ON FITTING BETWEEN 6 AND 7 O'CLOCK POSITION; HOLE NR 5 SCRATCHES ON SKIN AND FITTING AT 4 O'CLOCK POSITION; HOLE NR 6 CORROSION ON SKIN BETWEEN 2 AND 3 O'CLOCK POSITION; HOLE NR 9 CORROSION ON SKIN BETWEEN 2-3 AND 9-10 O'CLOCK POSITION AND CORROSION ON FITTING BETWEEN 9 AND 10 O'CLOCK POSITION; HOLE NR 10 TEARS ON SKIN AND FITTING BETWEEN 5 AND 6 O'CLOCK POSITION. REPAIRED PER ERA 588833-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,538 hrs · 38,572 cycles

DURING INSPECTION, MAINTENANCE FOUND TWO CRACKS ON HOLES COMMON TO THE STA 1640 FRAME OB CHORD & WEB, AT S-14R. REPAIRED PER ERA 58817-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,404 hrs · 41,710 cycles

SHIP 679 ERA 588672-14 SECTION I ISSUED FOR 2 DENTS FOUND BTWEEN 500-520 BETWEEN S27L AND 28L. CORRECTIVE ACTION: SUMMARY OF NR 00259. AREA WAS REPAIRED PER ER/A 588672-14 REV A SECTION III: PERMANTENT REPAIR. (1670742)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,538 hrs · 38,572 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AT AFT LAVATORY SERVICE DOOR FUSELAGE SKIN BETWEEN STA 1701-1681.80 & S-29R TO S-26R. REPAIRED PER ERA.

Part: SKIN — DAMAGED (BS 1681-1701) · airframe 93,992 hrs · 42,710 cycles

SHIP 679 ERA 588808-14 SECTION I ISSUED FOR REPAIR TO FUSELAGE SKIN AT AF T LAVATORY SERVICE PANEL STA 1681-1701. CORRECTIVE ACTION: REF ERA 588808-14. (1669850)

Part: STRUCTURE — CORRODED (LAV SERVICE DOOR) · corrosion level 2 · airframe 86,538 hrs · 38,572 cycles

DURING INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON INTERNAL STRUCTURE OF MID LAVATORY SERVICE DOOR PANEL NR 121AL AT LOWER FUSELAGE ACP600- 100-02Z (FUS). REPAIRED PER ERA.

Part: FITTING — CORRODED (FRAME) · corrosion level 2 · airframe 86,538 hrs · 38,572 cycles

DURING INSPECTION FOUND CORROSION LEVEL 2 ON FITTING OF FRAME STA 1680 INSIDE OF LAVATORIES SERVICE PANEL. PANEL REPLACED PER SRM.

Part: SKIN PANEL — CRACKED · airframe 90,131 hrs · 40,241 cycles

SHIP 679 CRACK SLAT # 10 COVE SKIN PANEL OUTBD MAIN TRACK. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00185. COVE SKIN PANEL OUTBD MAIN TRACK AT SLAT # 10 WAS REPAIRED PER B757-200 SRM 57-43-01-2R REPAIR 4. (1658739)

Part: FITTING — CORRODED (BS 1700 FRAME) · corrosion level 2 · airframe 86,538 hrs · 38,572 cycles

DURING INSPECTION FOUND CORROSION LEVEL 2 ON FITTING OF FRAME STA 1700 INSIDE OF LAV SERVICE PANEL. REPLACED FITTINGS PER SRM.

Part: LUG — CORRODED (NACELLE) · corrosion level 2 · airframe 86,538 hrs · 38,572 cycles

DURING INSPECTION FOUND CORROSION LEVEL 2 ON LUGS OF DRAG FITTING INBOARD AND OUT OF STRUT NACELLE SIDE RT. 2 LUGS OF DRAG FITTING INBOARD AND OUT WERE REPAIRED, PER SRM.

Part: PROXIMITY SENSOR — FALSE INDICATION (L3 DOOR) · airframe 86,031 hrs · 38,356 cycles

(AIRCRAFT 679, L/P 6489344) DOOR 3L SLIDE LIGHT IS ILLUMINATED W DOOR UNARMED. CORRECTIVE ACTION: REPLACED FWD PROX SENSOR S10224 PER B757 AMM 25-66-11.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 85,911 hrs · 38,302 cycles

(AIRCRAFT 679, L/P 6332792) 4L SLIDE LIGHT WONT GO OUT. CORRECTIVE ACTION: LOCATION IS DOOR 4L, CLEARED OBSTRUCTION FROM GIRT ATTACH AREA.

Part: SENSOR — DIRTY (L3 DOOR) · airframe 85,809 hrs · 38,274 cycles

L3 DOOR ARM LIGHT STAYED ON WITH THE DOOR DISARMED. CLEANED DEBRIS FROM LOWER SENSORS, OPS CHECKED NORMAL.

Part: FILTER — ODOR (RECIRC FAN) · airframe 85,728 hrs · 38,249 cycles

(AIRCRAFT 679, L/P 6332718) AFTER LEVEL OFF UNKNOWN ODOR REPORTED IN FIRST CLASS, 3-4 MINUTE DURATION AND DISSIPATED QUICKLY AFTER TURNING OFF RIGHT RECIRC FAN. CORRECTIVE ACTION: REPLACED RT RECIRC FAN FILTER PER B757 AMM 21-25.

Part: DOOR — OBSTRUCTED (L3) · airframe 85,911 hrs · 38,302 cycles

(AIRCRAFT 679, L/P 6131880) 3L ARMED LIGHT WOULD NOT EXTINGUISH. CORRECTIVE ACTION: REMOVED DEBRIS AND CLEANED AREA.

Part: SLIDE — FOD (L3 DOOR) · airframe 85,562 hrs · 38,159 cycles

(AIRCRAFT 679, L/P 6131834) L3 DOOE SLIDE WONT ARM. CORRECTIVE ACTION: REMOVED SLIDE COVER. REMOVED DEBRIS. REASSEMBLED BOTTOM. ACTUATED/ARMED SLIDE SEVERAL TIMES. OK FOR SVC.

Part: STRAP — OUT OF POSITION (L3 DOOR) · airframe 85,511 hrs · 38,143 cycles

(AIRCRAFT 679, L/P 6131804) 3L DOOR DIFFICULT TO DISARM. CORRECTIVE ACTION: STRAP HANGING: REPOSITIONED, OPS NORMAL.

Part: LANYARD — UNSECURE (L3 DOOR) · airframe 85,369 hrs · 38,061 cycles

(AIRCRAFT 679, L/P 6748704) 3L LANYARD LOOSE. STOWED LANYARD. DOOR OPS NML.

Part: PROXIMITY SWITCH — INTERMITTENT (L1 GIRT BAR) · airframe 85,272 hrs · 38,007 cycles

SHIP 679 L1 DOOR ARMED INDICATION INOP. CORRECTIVE ACTION: T/S PER B757 FIM 25-66-00-815-802 FOUND L1 DOOR FWD GIRT BAR PROXIMITY SWITCH INTERMITTENT. REPLACED SAME PER B757 AMM 25-66. L1 DOOR ARM INDICATOR NOW CKS GOOD. (5762248)

Part: SEAL — UNKNOWN (L3 DOOR SLIDE) · airframe 84,930 hrs · 37,836 cycles

3L SLIDE REMAINS ILLUM WITH DOOR DISARMED REPEAT GRIP. R/R SWEEPER SEAL @4L DOOR (3L). IAW B757 AMM 52-11 AND CMM 25-66. VERIFIED PROPER ENGAGEMENT OF GIRT BAR AND SLIDE LIGHT ILLUMINATED WHEN ENGAGED AND EXTINGUISHED WHEN NOT ENGAGED. A/C OK FOR SVC, REF B757 AMM 25-66.

Part: GIRT BAR — DIRTY (L3 DOOR SLIDE) · airframe 84,912 hrs · 37,830 cycles

L3 SLIDE LIGHT WON'T GO OUT WITH DOOR DISARMED. CLEANED GIRT BAR AND SENSOR. OP CKS GOOD REF B757 AMM 52-11.

Part: VALVE — MALFUNCTIONED (NLG DOOR) · airframe 84,682 hrs · 37,737 cycles

DUE GEAR DOOR LIGHTS ILLUMINATED. FERRIED AND REPLACED NOSE GEAR SAFETY VALVE & NOSE GEAR DOOR OPERATED SEQUENCE VALVE. OPS CHECKED OK.

Part: HANDLE — INOPERATIVE (EMERGENCY EXIT) · airframe 83,809 hrs · 37,378 cycles

SHIP 679 RIGHT EMERGENCY WING EXIT HANDLE LIGHTS INOP. CORRECTIVE ACTION: FOUND MISSING GND BETWEEN HANDLE LIGHT M10614 AND CONN D5678. RECONNECTED GND. OPS CK NORMAL. REF B757 WDM SUPPLEMENT 33-51-13 SH 2 OF 2. (5660674)

Part: GROUND WIRE — MISSING (HANDLE LIGHT) · airframe 83,824 hrs · 37,388 cycles

SHIP 679 LEFT EMERGENCY WING EXIT HANDLE LIGHTS INOP. CORRECTIVE ACTION: FOUND MISSING GND BETWEEN HANDLE LIGHT M10614 AND CONN D5778. RECONNECTED GND. OPS CK NORMAL REF B757 WDM. (5660675)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,189 hrs · 42,206 cycles

SHIP 0679 FUSELAGE / SKIN / FS 440 TO FS 460 / S-1 TO S-2R / EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 565755-14. (0943212)

Part: LATCH — BROKEN (L2 DOOR) · airframe 83,271 hrs · 37,151 cycles

L2 CABIN DOOR WILL NOT CLOSE PROPERLY. REPLACED BROKEN BUSSLE LATCH ON 2L DOOR AND SECURED DOOR TRIM SEAL. (5576938)

Part: SENSOR — FOD (L2 DOOR) · airframe 82,464 hrs · 36,820 cycles

(AIRCRAFT 679, L/P 4160768) DOOR 2L SLIDE LIGHT WENT OUT IN FLIGHT. REMOVED DEBRIS FROM AROUND 2L DOOR SENSOR. DOOR 2L ARMS NORMAL AND SLIDE OP CKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,440 hrs · 36,802 cycles

(AIRCRAFT 679, L/P 4160744) RH AFT WING EMERG EXIT LIGHT OUT. PER B757 AMM 33-51 REPLACED POWER SUPPLY M10568 OPS CK,D GOOD.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 82,400 hrs · 36,781 cycles

(AIRCRAFT 679, L/P 4160728) ROW 27FED, EMERGENCY EXIT DOOR LIGHTS ABOVE DOOR HANDLE INOP. REPLACED FUSE ON POWER SUPPLY PER AMM OPS CK GOOD OK FOR SVC. REF AMM AMM 33-51.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 82,400 hrs · 36,781 cycles

(AIRCRAFT 679, L/P 4160727) ROW 26ABC, EMERGENCY EXIT DOOR LIGHTS ABOVE DOOR HANDLE INOP. REPLACED FUSE ON POWER SUPPLY PER AMM OPS CK GOOD, OK FOR SVC. REF AIM 33-51.

Part: BATTERY — DISCHARGED (CABIN) · airframe 82,400 hrs · 36,781 cycles

(AIRCRAFT 679, L/P 4160726) EMERGENCY LIGHTS ROW 43-45 INOP, AFT GALLEY DOOR EMERGENCY EXIT LIGHTS INOP. CHARGED BATTERY PER AMM OPS CK GOOD OK FOR SVC. REF AMM 33-51.

Part: PROXIMITY SWITCH — OUT OF ADJUST (L1 DOOR) · airframe 82,321 hrs · 36,744 cycles

SHIP 679 1L SLIDE LIGHT INTERMITTENT. CORRECTIVE ACTION: ADJUSTED PROX SWITCHES PER AMM 25-66-11. OPS CHECKS GOOD. (4374480)

Part: PROXIMITY SENSOR — OUT OF ADJUST (L2 DOOR) · airframe 82,271 hrs · 36,714 cycles

SLIDE LIGHT ON 2L WILL NOT ILLUMINATE BELOW 10,000 FEET. T/S AMM 25-6. FOUND AFT DOOR PROX SENSOR OUT OF LIMITS, ADJ SAME. OP NOW OK PER AMM 25-66.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 81,904 hrs · 36,508 cycles

AFTER THE FLIGHT, CATERING FOUND A CORD HANGING OUT OF THE R1 DOOR BUSTLE. FOUND THE LANYARD PARTIALLY HANGING DOWN. STOWED THE LANYARD IAW AMM 25-66.

Part: ROD — MISSING (L1 DOOR SLIDE) · airframe 81,266 hrs · 36,279 cycles

L1 DOOR ARM INDICATOR NOT COMING OUT AND STICKING. FOUND THE DOOR ESCAPE SLIDE ROD MISSING. INSTALLED DOOR ESCAPE SLIDE ROD IAW AMM 52-11-20.

Part: NUT — CORRODED (FLAP BALLSCREW) · airframe 81,195 hrs · 36,258 cycles

CORROSION FOUND ON THE BALLSCREW NUT OF RIGHT WING INBOARD TRAILING EDGE FLAP. THE BALLSCREW ASSY WAS REPLACED.

Part: BALLSCREW — CORRODED (TE FLAP) · airframe 81,195 hrs · 36,258 cycles

PITTING CORROSION ON BALLSCREW NUT OF RIGHT WING INBOARD TRAILING EDGE FLAP. BALLSCREW ASSY OF INBOARD TRAILING EDGE FLAP AT RT WING WAS REPLACED.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION OUT LIMITS ON RT SIDE PANEL STA 1200 TO 1310 IN REF NRC 00322 AT AFT CARGO COMPARTMENT (CCT). CORROSION LEVEL 2. SIDE PANEL WAS REPAIRED PER SRM 53-00-53 REP 2.

Part: FLOOR PANEL — CORRODED (BS 1510-1582) · airframe 81,195 hrs · 36,258 cycles

CORROSION OUT OF LIMITS ON RH SIDE FLOOR PANEL (UPPER AND LOWER) FROM STA 1510-1582 AT AFT CARGO COMPARTMENT (CCT)(SM). SUMMARY OF NRC 00496: CORROSION LEVEL 2. SIDE PANEL WAS REPAIRED PER B-757-200 SRM 53-00-53 REP.3.

Part: DOUBLER — CRACKED (RT PYLON) · airframe 81,195 hrs · 36,258 cycles

DURING INSPECTION, A CRACKED INBD DOUBLER ON THE RT PYLON PPS 170. THE INBD DOUBLER WAS REPLACED IAW SRM 51-40-02-0G-0, AND DRAWING 313N3100.

Part: PANEL — CORRODED (BS 1200-1410) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION WAS FOUND ON THE LT SIDE PANEL, UPPER AND LOWER FROM BS 1200 - 1310 AND BS 1310 - 1410 IN THE AFT CARGO BAY. THE PANEL WAS REPAIRED IAW SRM 53-00-53, REP 3.

Part: FRAME — CORRODED (BS 800) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION OUT OF LIMITS ON FUSELAGE FAIRING SUPPORT FRAME BS 800, BETWEEN LONGERONS 28 AND 30L. THE FAIRING SUPPORT FRAME WAS REPAIRED IAW SRM 51-70-11 FIG 1.

Part: FLOORBEAM — CORRODED (BS 653) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION ON THE FLOORBEAM, RBL 2.9, RBL 7.55, RBL 10.45, AND RBL 16.10, BS 653 IN THE FWD CARGO BAY WAS FOUND OUT OF LIMITS. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-53, REPAIR 1.

Part: SKIN — DEBONDED (NR 6 SLAT) · airframe 81,195 hrs · 36,258 cycles

DESBONDED UPPER SURFACE OF THE TRAILING EDGE WEDGE OF THE NR 6 SLAT. REPAIRED IAW SRM 51-70-10, REP 4, PARAGRAPH 3. D, AND SRM 51-70-10, REP GRAL, PARAGRAPH 15, 18, AND 20 B.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1640) · airframe 81,195 hrs · 36,258 cycles

(AIRCRAFT 679, L/P 0573502) AWR IN REF NRC 00330 OUT LIMITS BY CORROSION ON FLOOR SUPPORTS 10 LBL STA 1460-1520, 1620-1640 7 LBL STA 1460-1520, 1620-1640, 2 LBL STA 1460-1640 AT AFT CARGO COMPARTMENT (CCT). SUMMARY OF NRC 00452: CORROSION LEVEL 2. FLOOR SUPPORTS WERE REPAIRED PER B757-200 SRM 53-0 0-53-R1.

Part: DOUBLER — CRACKED (RT PYLON) · airframe 81,195 hrs · 36,258 cycles

CRACKED OUTBD DOUBLER ON RT PYLON STA PPS 170 (RT PYLON). REPLACED PER DWG 313N3100 REV. REMOVE AND INSTALLED PER SRM 51-40-02 PAR 7. LENGTH CRACKED WAS FOUND .521.

Part: STRINGER — CORRODED (BS 740-760) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION WAS FOUND ON STRINGER 23R, BETWEEN BS 740 - 760 IN THE FWD CARGO BAY. REPAIRED THE STRINGER IAW SRM 53-00-03, REPAIR 1, FIG 201.

Part: STRINGER — CORRODED (BS 740-760) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION FOUND ON STRINGER 23R, BETWEEN BS 740 - 760 IN THE FWD CARGO BAY. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, REPAIR 1, FIG 201.

Part: STRINGER — CORRODED (BS 740-760) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 23R, BETWEEN BS 740 - 760 IN THE FWD CARGO BAY. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, REPAIR 1, FIG 201.

Part: INTERCOSTAL — BENT (BS 1380-1400) · airframe 81,195 hrs · 36,258 cycles

DURING INSPECTION, BENT INTERCOSTAL BETWEEN BEAM 6 AND LOWER EDGE BEAM AND BS 1380 - 1400 AT THE AFT CARGO DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, PAR 4, AND 7, AND DWG 146N6603, REV BP.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION FOUND ON THE FLOORBEAM, BS 1681, BETWEEN LBL 40 AND 49. THE FLOORBEAM WAS REPAIRED IAW ER/A 568928-14, REV ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (BS 1671) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION FOUND ON THE FLOOR SUPPORT AT THE L4 DOOR AREA BS 1671, LBL 54 AT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02, AND DWG 146N5246, REV D.

Part: FLOORBEAM — CORRODED (BS 690) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION FOUND ON THE FLOORBEAM BS 690 LBL13 AND RBL13, IN THE FWD CARGO. THE FLOORBEAM WAS REPLACED IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 1680) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION ON THE FITTING SUPPORTS OF THE L4 DOOR OUT OF LIMITS, BS 1680 BETWEEN LBL 54 AND 60. THE FITTING WAS REPLACED IAW SRM 51-40-02.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

CORROSION POINTS ON BEAM STA 740 RBL 14.0 AND LBL 14.0 AT FWD CARGO COMPT. LEVEL CORROSION 2, BEAM WAS REPLACED PER SRM 51-40-02 AND DWG 453N1632-38 REV H.

Part: FLOOR SUPPORT — CORRODED (BS 1600-1620) · corrosion level 2 · airframe 81,195 hrs · 36,258 cycles

FLOOR SUPPORT CORRODED OUT OF LIMITS, BS 1600 - 1620. REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 1320-1340) · airframe 81,195 hrs · 36,258 cycles

DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT, BS 1320 - 1340, LBL 25. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02, PAR 4, AND 7.

Part: SUPPORT — CRACKED (BS 720) · airframe 81,195 hrs · 36,258 cycles

DURING INITIAL INSPECTION, A CRACK WAS FOUND ON THE CEILING SUPPORT BS 720, RBL 24. THE SUPPORT WAS REPAIRED IAW ER/A 384483-14MA, REV D, SRM 53-10-01, REPAIR 1, DETAIL I, AND 51-20-01, PAR 2 AND 4.

Part: LIGHT — INOPERATIVE (SLIDE) · airframe 81,188 hrs · 36,253 cycles

SLIDE INDICATOR LIGHT INOPERATIVE. SECURED THE SLIDE LIGHT INDICATOR, CHECKED NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (L2 DOOR) · airframe 80,886 hrs · 36,125 cycles

L2 DOOR SLIDE LIGHT ILLUMINATED WITH DOOR OPEN. RESET THE L2 DOOR ARM DISARM LIGHT, CHECKED OK IAW AMM 25-66.

Part: LIGHT — MALFUNCTIONED (R1 DOOR) · airframe 80,886 hrs · 36,125 cycles

R1 DOOR ESCAPE SLIDE ARMED INDICATOR ARMED LIGHT DID NOT ILLUMINATE. ARMED AND DISARMED ALL SIX DOORS, NO DEFECTS NOTED. ALL LIGHTS ILLUMINATE, & L1 & R1 KNUCKLE KNOCKERS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 78,829 hrs · 35,353 cycles

EXIT SIGN COVER MISSING NEAR L2 DOOR. INSTALLED CENTER AISLE CEILING EXIT SIGN COVER. CHECKED GOOD IAW AMM 33-51.

Part: BRACKET — BROKEN (EXIT SIGN) · airframe 78,526 hrs · 35,255 cycles

OVERWING EXIT SIGN BRACKET IS BROKEN. INSTALLED A NEW SIGN.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 77,056 hrs · 34,519 cycles

SEAT ROW 25 EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR PIN LOCKS DAMAGED. REPLACED THE CONNECTOR, OPS OK. IAW AMM 33-40.

Part: LENS — MISSING (CABIN) · airframe 75,917 hrs · 34,004 cycles

DOOR 2R EXIT LIGHT LENS COVER MISSING. REPLACE MISSING RED LENS AT MID LAV.

Part: FLOOR PANEL — PUNCTURED (BS 590) · airframe 75,527 hrs · 33,845 cycles

FWD CARGO COMPARTMENT BS 590, RBL 20, FLOOR PANEL IS PUNCTURED. FABRICATED AND INSTALLED FLOORBOARD IAW SRM.

Part: CHANNEL — CORRODED (BS 620) · corrosion level 2 · airframe 75,527 hrs · 33,845 cycles

FWD CARGO COMPARTMENT BS 620, RBL 26, Z-CHANNEL IS CORRODED AT CARGO NET MOUNT FITTING. R & R Z-CHANNEL, PN 143N5366U126 IAW B-DWG, REV E AND ER/A 373211-14MA, REV G, SRM.

Part: RETAINER — CRACKED (RT MLG WW) · airframe 75,527 hrs · 33,845 cycles

RT MLG W/W, FWD OTBD CORNER SEAL RETAINER ANGLE CRACKED. R & R RT MLG WW FWD OTBD CORNER SEAL RETAINER ANGLE IAW BAC DWG AND SRM.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 75,527 hrs · 33,845 cycles

LEFT MLG WHEEL WELL, FWD OTBD CORNER SEAL RETAINER ANGLE CRACKED. R & R LT MLG WHEEL WELL FWD OTBD CORNER SEAL RETAINER ANGLE IAW DWG AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1300-1310) · airframe 75,527 hrs · 33,845 cycles

AFT CARGO FLOOR, Z-ANGLE IS CORRODED BS 1300-1310, RBL26. REMOVED CORROSION AND REMOVED DAMAGE IAW SRM. FABRICATED REPAIR AND INSTALLED IAW AMM AND SRM.

Part: RETAINER — CRACKED (NLG DOOR FRAME) · airframe 75,466 hrs · 33,828 cycles

NOSE GEAR CUTOUT RT SEAL RETAINER CRACKED. R & R NOSE GEAR CUTOUT RT SEAL RETAINER BRACKET. PN 141N0094-64, TAG A92566 IAW DWG 141N0094.

Part: FLOORBEAM — CORRODED (BS 1510) · airframe 75,481 hrs · 33,833 cycles

AFT CARGO COMPARTMENT, BS 1510, RBL 5, FLOOR SUPPORT ANGLE WITH REMOVED NUTPLATES HAS CORROSION ON LOWER SURFACE. REPAIRED AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT BS 1510, RBL5 IAW ER/A 332525-14MA.

Part: FLOORBEAM — CORRODED (BS 1510) · airframe 75,466 hrs · 33,828 cycles

AFT CARGO COMPARTMENT, BS 1510, BL2.90 LT FLOOR SUPPORT ANGLE WITH DAMAGED NUTPLATES HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW ERA 332525-14MA, REV D, SHT 2, STEPS 1-9.

Part: STOP FITTING — GOUGED (CARGO DOOR FRAME) · airframe 75,466 hrs · 33,828 cycles

FWD CARGO BAY DOOR CUTOUT, TOP AFT DOOR STOP BRACKET GOUGED, MARKED. BLENDED STOP FITTING ON FWD CARGO DOOR CUT-OUT AT TOP AFT POSITION REMOVED .055". NO PUBLISHED LIMITS FOR FITTING WHICH MAKES IT OUT OF LIMITS. R & R FITTING IAW DWG 143N8521 REV. H, AND SRM 51-40-02, PAGE 7 AND SRM 51-10-01, PAGE 10.

Part: SUPPORT BRACKET — CRACKED (LT WING TE FLAP) · airframe 75,466 hrs · 33,828 cycles

LEFT WING INBD FLAP T/E LOWER SURFACE, JUST OTBD OF NR 3 FLAP TRACK FAIRING , SUPPORT BRACKET IS CRACKED. R & R SUPPORT BRACKET IAW DWG 113N2003, REC A AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1510-1540) · airframe 75,466 hrs · 33,828 cycles

AFT CARGO COMPARTMENT, BS 1510-BS 1540, RBL 11.4" FLOOR SUPPORT ANGLE WITH REMOVED NUTPLATES HAS CORROSION ON LOWER SURFACE. REMOVED CORRODED FLOOR SUPPORT ANGLE 100 PERCENT MATERIAL LOSS AND INSTALLED NEW FLOOR SUPPORT STRINGER FROM BS 1500-1600 RBL 11.4. REF AMM 53-88-01-801 AND SRM 51-40-02, STEP 7.

Part: CHANNEL — CORRODED (BS 1380) · corrosion level 2 · airframe 75,466 hrs · 33,828 cycles

AFT CARGO BAY BS 1380, RBL 26, CHANNEL IS CORRODED AT CARGO NET MOUNT FITTING. REMOVED CORROSION AND OUT OF LIMITS. REPLACED SIDE PANEL AND SPLICE IAW DWG AND SRM.

Part: CARGO TRACK — CORRODED (BS 1320) · corrosion level 2 · airframe 75,466 hrs · 33,828 cycles

AFT CARGO TRACK IS CORRODED BS 1320, RBL 22. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. R & R THE CARGO TRACK IAW DWG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,103 hrs · 33,676 cycles

EMERGENCY LIGHTS ROWS 19-26, INOPERATIVE. R & R THE BATTERY PACK CHARGER IAW AMM 33-51.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 74,795 hrs · 33,558 cycles

CREW PERFORMED AN ALTERNATE GEAR EXTEND AFTER NOSE GEAR DID NOT INDICATE DOWN. GEAR BULB CHECKED, OK AND GEAR DISAGREE MESSAGE. NOSE GEAR INDICATED DOWN AFTER ALTERNATE GEAR EXTENSION. PSEU BITE FAULTED LANDING GEAR SYSTEM 2 TARGET FAULT, 079 AND 077, AND LANDING GEAR SYSTEM 1 TARGET FAULT 238 AND 066. TESTED ALL SENSORS GAPS GOOD, AND RESISTANCE GOOD. MEGGED WIRING GOOD. JACKED ACFT, EXTENDED & RETRACTED GEAR ON 1 AND 2 HYDRAULIC PUMPS. RETRACT - EXTEND TIMES GOOD, NO FAULTS. REPLACED NLG DOOR SEQUENCE VALVE AND NLG LOCK ACTUATOR. NO FAULTS NOTED. ALSO FOUND NLG AND BOTH MLG STRUTS WITH NO CHROME SHOWING, SERVICED ALL STRUTS IAW AMM 12-15-01/02.

Part: SKIN — DAMAGED (BS 600) · airframe 74,638 hrs · 33,492 cycles

LIGHTNING STRIKE AT BS 600 BETWEEN STRINGERS 5 AND 6R BEYOND ALLOWABLE DAMAGE LIMITS. INSTALLED BLIND RIVET IAW SRM 53-00-01. VISUAL INSPECTION AT 1000 FLT CYCLES. REPLACED NO LATER THAN 3000 FLT CYCLES OR 24 MONTHS. PERFORMED REPETITIVE INSPECTION IAW SRM 53-00-01. NO FURTHER DAMAGE NOTED, OK TO CONTINUE ON QC DEFERRAL.

Part: SKIN — DAMAGED (BS 1030) · airframe 74,638 hrs · 33,492 cycles

LIGHTNING STRIKE AT BS 1030 BETWEEN STRINGERS SR-2 AND SR-3 BEYOND ALLOWABLE DAMAGE LIMITS. INSTALLED BLIND RIVET IAW SRM 53-00-01. REPAIR 6, REPAIR OF LIGHTNING STRIKE. VISUAL INSP AT 1000 FLY CYCLES. REPLACED NO LATER THAN 3000 FLT CYCLES OR 24 MONTHS. INSPECTED RIVETS IAW SRM 53-00-01. NO FURTHER DAMAGE NOTED. OK TO CONTINUE, ON QC DEFERRAL.

Part: LIGHT — UNKNOWN (CABIN) · airframe 74,163 hrs · 33,262 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE, LOCATIONS:212. PUT EMERGENCY RED LIGHT LENS ON EMERGENCY PLACEMENT COVER PERFORMED AN OPS CHECK IAW AMM 33-51, OK FOR SERVICE.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHTS) · airframe 73,991 hrs · 33,176 cycles

DURING PREFLIGHT, NOTICED EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROW 38 BACK AND OVERHEAD 38 AND AFT GALLEY. FOUND PIN 8 OF CONNECTORS M736, M737, AND M9102 HAD RESISTANCE AND SHOULD HAVE VOLTAGE. FOUND CONNECTOR D40488J IN NOSE W/W SHORTING PIN D TO HIGH RESISTENCE GROUND. REPLACED CONNECTOR D40488J. ALL EMERGENCY LIGHTS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 73,986 hrs · 33,174 cycles

DURING DESCENT THROUGH 12000 FT, ALL EMERGENCY LIGHTS IN CABIN ILLUMINATED. EMERGENCY LIGHTS FUNCTIONED ON GROUND. UNABLE TO FAULT OPERATION. OK FOR SERVICE.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,929 hrs · 33,153 cycles

RAM-2 EMERGENCY LIGHTS COME ON UNCOMANDED. CAN NOT DUPLICATE PROBLEM, SHOOK WIRES DOWN AT ATTENDENTS PANEL AND PILOTS OVERHEAD PANEL, NO FAULTS NOTED. R & R FWD FLT ATT SW S10297 IAW WD 33-51-11, AS REQUESTED. NOTIFIED MAINTENANCE, REQUIRES FURTHER EVALUATION OK TO CONTINUE ON DEFERRAL. CAN NOT DUPLICATE FAULTS, OK TO CLOSE LOG.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 73,852 hrs · 33,125 cycles

EMERGENCY LIGHTS ILLUMINATED THROUGHOUT CABIN THEN IN 1ST CLASS ONLY DURING FLIGHT. REPLACED SWITCH S10035, NOSE GEAR EMERGENCY LIGHT TEST SWITCH REF AMM 33-51 AND WDM 33-51 ALL EMERGENCY LIGHTS CK GOOD.

Part: SWITCH — DAMAGED (EMERGENCY LIGHTS) · airframe 73,852 hrs · 33,125 cycles

RAM-1 EMERGENCY LIGHTS COME ON UNCOMANDED. REPLACED SWITCH, S10035, NOSE GEAR EMERGENCY LIGHT TEST SWITCH REF AMM 33-51 AND WDM 33-51. ALL EMERGENCY LIGHTS TEST GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 73,852 hrs · 33,125 cycles

ON SERVICE FWD GALLEY AND F/C EMERGENCY LIGHTS TURNED ON UNCOMMANDED WITH COCKPIT EMERGENCY SWITCH OFF. R & R EMERGENCY LIGHT CHARGERS AND BATTERY PACKS M730 AND M731 AND C/P D9031, REF AMM 33-51, NO HELP NOT ALL LIGHTS TURN ON NOW. T/ S WIRING IAW WDM 33-51-11. ALL WIRING FROM COCKPIT EMERGENCY LIGHTS SW TO M730, 731, M9101, CKS GOOD. ALSO FROM CABIN TEST SWITCHES TO SAME CK, GOOD. CLEANED NOSE GEAR EMERGENCY LIGHT TEST SWITCH S10035. REPLACED M731 AND M9101 FLOOR LIGHT PACK SYS NOW OPS GOOD.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 73,852 hrs · 33,125 cycles

CABIN EMERGENCY LIGHTS CAME ON UNCOMMANDED IN FLIGHT PASSING THRU 33000', REMAINED ON, UNTIL CYCLED THE EMERGENCY LT SWITCH. R & R COCKPIT EMERGENCY LIGHT, PASS OXY SWITCH PANEL IAW AMM 33-51. NO HELP. R & R FIRST CLASS BATTERY PACK AND CHARGER M730. NO HELP 866781. FOUND CHARGER M730 BAD FROM STOCK. REINSTALLED ORIGINAL CHARGER REF AMM 33-51. SYS OPS CKS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,832 hrs · 33,113 cycles

INFLIGHT, EMERGENCY LIGHTS CAME ON IN CABIN, TROUBLESHOT W/ MAINTENANCE, NO CHANGE. STAYED ON FOR 20 MINUTES THEN WENT OUT WHEN ACFT ENCOUNTED LIGHT NB. SENSOR, TS IAW FIM 33-51. R & R EMERGENCY LIGHT CHARGER M730 & BATTERY PACK. OPS CKS OK.

Part: FRAME — DAMAGED (BS 1640) · airframe 69,636 hrs · 31,296 cycles

BS 1640, FRAME WEB WAS FOUND WITH CHAFE DAMAGE BETWEEN S5-6R. IAW ER/A 504281-14, REV A.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,464 hrs · 30,817 cycles

EMERGENCY LIGHT 39DEF THRU 45DEF INOPERATIVE. REPLACED POWER SUPPLY M9002.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 68,152 hrs · 30,671 cycles

FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 30 ON SERVICE CHECK. FOUND WIRE HARNESS WIRE BROKEN. REPLACED WIRE HARNESS REF WDM 33-51-16. OPS CHECK OK.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 67,013 hrs · 30,189 cycles

BURNING WIRE ODOR IN COCKPIT AT SAME TIME THE PASSENGER NOTED A POP IN AUDIO HEADSET AND ALL AUDIO WENT OUT IN CABIN HEADSET. INSPECTED WIRE IN COCKPIT PANNEL P1. FOUND WIRE INTACT, NO SIGN OF BURNING. RESET IFE SYS VIDEO AND AUDIO, OPS NORMAL. NO POPPING SOUNDS OR ODORS.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 66,290 hrs · 29,915 cycles

EMERGENCY EXIT SIGN LIGHT COVER MISSING. R & R COVER IAW AMM 33-54.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 66,290 hrs · 29,915 cycles

DURING SERVICE FOUND EMERGENCY LIGHT AT SEAT 4DC AND 22FED INOPERATIVFE. REPLACED LIGHT ASSY AN SEAT 22FED AND R & R EXTENTION HARNESS ON SEAT 4DC. OPS CHECK GOOD IAW AMM 33-51.

Part: LIGHT — DAMAGED (ROW 21 AND 40) · airframe 66,083 hrs · 29,825 cycles

SEAT MOUNTED EMERGENCY PATH LIGHT SV INOPERATIVE AT ROW 21 AND ROW 40. REPLACED LIGHT ASSY IAW AMM 33-51-04.

Part: STRINGER — DAMAGED (BS 225 S24R) · airframe 66,041 hrs · 29,807 cycles

LIGHTNING STRIKE AT BS 225, STRINGER 24R. REMOVED FASTENER. HFEC INSPECTION IAW NDT PART 6 51-00-19. REPLACED FASTENER, TREATED, PRIMED, AND PAINTED IAW SRM 53-00-01.

Part: STRINGER — DAMAGED (BS 241 S24R) · airframe 66,041 hrs · 29,807 cycles

LIGHTNING STRIKE AT BS 241, STRINGER 24R. REMOVED FASTENER. HFEC INSP IAW NDT PART 6 51-00-19. REPLACED FASTENER, TREATED, PRIMED, AND PAINTED IAW SRM 53-00-01.

Part: LIGHT — INOPERATIVE (SEAT ROW 21) · airframe 64,859 hrs · 29,317 cycles

EMERGENCY PATH LIGHT OUT AT SEAT ROW 21. R & R LIGHT AND LENS ASSY IN REF TO AMM 33-51.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 64,731 hrs · 29,258 cycles

MX DISCOVERED ROW 19-27 EMERGENCY LIGHTS ON SEATS INOPERATIVE. FOUND WIRE BROKEN AT 27. REMOVED OLD SPLICES REPAIRED WIRING IAW SWPM 20-30-12. OPS CHECKED GOOD.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,700 hrs · 29,245 cycles

MX DISCOVERED ALL LOCATIONS EMERGENCY FLOOR LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT SWITCH. CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 64,424 hrs · 29,127 cycles

MX DISCOVERED THE EMERGENCY PATHWAY LIGHTS FROM ROW 21D THRU 27 INOPERATIVE. REPAIRED 2 BROKEN WIRES AND REPLACED LAMP ASSY AT ROW 21 -CKS GOOD.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 63,859 hrs · 28,897 cycles

FLAP RT INBD MAIN LOWER SKIN PANEL DENTED. REPAIRED PER ERA 504274-14 ORIG.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,584 hrs · 28,776 cycles

CORROSION ON MAIN CABIN DECKPLATE, BS 1680 TO 1718, BL 0 TO 55. CORROSION REMOVED PER SRM 53-60-51 PAGE 201 FIG 201. INSTALLED REPAIR DOUBLER AND SHIMS IAW SRM 53-60-51 PG 201 FIG 201 REPAIR 2 ALTERNATIVE I.

Part: FLOOR PANEL — CORRODED (BS 1680-1718) · airframe 63,584 hrs · 28,776 cycles

CORROSION ON MAIN CABIN DECKPLATE, BS 1680-1718, BL 0 - RBL 55. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51 PG 201 FIG 201. REPAIRED IAW SRM 53-60-51 P. 201 FIG 201 REPAIR 2 ALTERNATIVE I.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,584 hrs · 28,776 cycles

COROSION ON MAIN CABIN DECKPLATE BS 1715, BL0 TO RBL2.5. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51 PG 201 FIG 201 REPAIR 2. REPAIRED IAW SRM 53-60-51 PG 201 FIG 201 REPAIR 2 ALTERNATIVE I.

Part: SKIN — DENTED (BS 1651 S25-26R) · airframe 63,584 hrs · 28,776 cycles

DENT ON FUSELAGE SKIN AT BS 1651 BETWEEN S25 AND 26R. MEASURED DENT, FOUND TO BE OUT OF LIMITS, COMPLIED WITH ERA 503741-14 REV ORIGINAL.

Part: STRINGER — CORRODED (BS 1475 S23R) · airframe 63,584 hrs · 28,776 cycles

DURING HMV, AFT CARGO COMPARTMENT STRINGER 23 RT CORRODED AT BS 1475. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED SECTION OF STRINGER, FABRICATED NEW SECTION AND REPAIR FILLER AND INSTALLED IAW SRM 53-00-03.

Part: FRAME — CHAFED (BS 1640) · airframe 63,584 hrs · 28,776 cycles

FRAME CHAFED IN PASSENGER CABIN AT FS 1640, JUST ABOVE R4 DOOR CUTOUT. COMPLIED WITH ERA 504281-14 REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 63,584 hrs · 28,776 cycles

DURING HMV, FOUND LIGHT CORROSION ON MAIN CABIN FLOORBEAM AROUND FASTENER HOLES, STA 1640, RBL4 TO LBL 20. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED UPPER TEE OF FLOORBEAM, FABRICATED AND INSTALLED TEE REPAIR ANGLES AND STRAPS IAW B757 ERA 48913-14MA.

Part: SKIN — DAMAGED (BS 1550 S24R) · airframe 63,584 hrs · 28,776 cycles

CREASE ON FUSELAGE SKIN AT STA 1550 TO 1570 BETWEEN S24R AND S25R. COMPLIED WITH ERA 504277-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 1698 S20L) · airframe 63,584 hrs · 28,776 cycles

DENT ON FUSELAGE SKIN AT BS 1698 BELOW LAP JOINT S20L. DENT FOUND TO BE OUT OF LIMITS, COMPLIED WITH ERA 504273-14 REV ORIGINAL.

Part: FRAME — DAMAGED (BS 1460 S26L) · airframe 63,584 hrs · 28,776 cycles

AFT CARGO FRAME CORRODED BS 1460 STR 26L-25R. REMOVED SHEAR TIES FOR ACCESS, FOUND SHEAR TIES CRACKED AND CORRODED, COMPLIED WITH ERA 504608-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 1541 S26L) · airframe 63,584 hrs · 28,776 cycles

PROTRUDING DENTS ON FUSELAGE SKIN AT BS 1541 BELOW LAP JOINT S26L. MEASURED DENT, FOUND TO BE OUT OF LIMITS, COMPLIED WITH ERA 503740-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 1593 S25-26R) · airframe 63,584 hrs · 28,776 cycles

DURING HMV, FOUND PROTRUDING DENT ON FUSELAGE SKIN AT BS 1593, BETWEEN S25R AND S26R. DENT FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-00-01.

Part: FAILSAFE — CORRODED (BS 1520) · airframe 63,584 hrs · 28,776 cycles

AFT CARGO FRAME HAS CORROSION FWD AND AFT SIDE AND ON FAILSAFE BS 1520 RBL 26-LBL 26. REMOVED CORROSION, FOUND AREA TO BE OUT OF LIMITS. REMOVED AND REPLACED FAILSAFE IAW SRM 51-40-5 DURING HMV.

Part: SKIN — DENTED (BS 408 S16L) · airframe 63,584 hrs · 28,776 cycles

SKIN BS 408 HAS A DENT JUST BELOW S16L. DENT FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01.

Part: FRAME — DENTED (BS 540 S24L) · airframe 63,584 hrs · 28,776 cycles

FWD CARGO COMPARTMENT BS 540 BETWEEN STR 24L AND STR 25L FRAME WITH DENT. DENT OUT OF LIMITS, COMPLIED WITH ERA 504263-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 430 L17-18L) · airframe 63,584 hrs · 28,776 cycles

DURING HMV, SKIN HAS A DENT AT BS 430.5 BETWEEN L17-18L. DENT FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED SECTION. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-00-01.

Part: BUSHING — MIGRATED (LT NACELLE) · airframe 63,582 hrs · 28,775 cycles

LT ENGINE UPPER LINK FWD ATTACH OTBD INNER BUSHING MIGRATED. MAINTENANCE REPAIRED BUSHING IAW SRM 54-51-90.

Part: BUSHING — MIGRATED (LT NACELLE) · airframe 63,582 hrs · 28,775 cycles

LT ENGINE UPPER LINK AFT ATTACH OTBD INNER BUSHING MIGRATED. MAINTENANCE REPAIRED BUSHING IAW SRM 54-51-90.

Part: BUSHING — MIGRATED (RT NACELLE) · airframe 63,582 hrs · 28,775 cycles

RT ENGINE UPPER LINK AFT ATTACH OTBD INNER BUSHING MIGRATED. MAINTENANCE REPAIRED BUSHING IAW SRM 54-51-90.

Part: SPLICE — DAMAGED (CABIN) · airframe 63,306 hrs · 28,653 cycles

LINE MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT 19 TO 26 AS A RESULT OF A BAD WIRE SPLICE AT SEAT 26. WIRE RE-SPLICED LIGHTS OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (CABNI) · airframe 61,293 hrs · 27,816 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 2D INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — DENTED (BS 622 S17-18L) · airframe 59,371 hrs · 27,035 cycles

FUSELAGE SKIN DENTED AT STA 622, BETWEEN STRINGERS 17L AND 18L. TIME LIMITED REPAIR WAS ACCOMPLISHED IAW ERA 484738-14. CATEGORY B, INTERIM REPAIR WAS ACCOMPLISHED IAW SRM 53-00-01, FIG 201 ON NR CARD 1 AT PSV 16.

Part: FAN — FAILED (LT RECIRCULATION) · airframe 57,097 hrs · 25,970 cycles

LT RECIRC FAN MSG ON EICAS WITH AN OVBD EX VAL OPEN STATUS MESSAGE. R & R LT RECIRC FAN. CKS GOOD.

Part: SKIN — CRACKED (BS 562 S2R) · airframe 45,158 hrs · 20,704 cycles

AN EXISTING FUSELAGE SKIN BLENDED AREA WAS FOUND WITH A CRACK AT THE CENTER OF THE BLEND OUT. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — CRACKED (BS 460 S3R) · airframe 45,158 hrs · 20,704 cycles

A CRACK WAS FOUND IN A PREVIOUS FUSELAGE SKIN BLENDED AREA. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: ENGINE — UNKNOWN (NR 1) · airframe 44,381 hrs · 20,414 cycles

SHORTLY AFTER T/O HAD AN INDICATION OF LEFT ENGINE FIRE WARNING. RAN QRH PROCEDURE. NUMBER 1 ENGINE WAS SHUT DOWN INFLIGHT AND THE FIRE HANDLE WAS PULLED. NO BOTTLES WERE FIRED. FOUND BURN EVIDENCE AT NR 21 FUEL NOZZLE. REPLACED ALL NOZZLES AND MANIFOLDS.

Part: ACM — SEIZED (LEFT) · airframe 43,083 hrs · 19,956 cycles

LEFT PACK RUNNING HOT AND MAKING SMELL, REPLACED SEIZED ACM.

Part: TIRE — FAILED (MLG) · airframe 35,715 hrs · 17,136 cycles

NR 2 MLG TIRE CAP SEPERATED DURING T/O. REPLACED NR 2 MLG WHEEL ASSEMBLY

Part: TERMINAL — BROKEN (COCKPIT) · airframe 33,621 hrs · 16,121 cycles

SHORTLY AFTER T/O LOST LEFT FMC FOLLOWED RAPIDLY BY LOSS OF NUMEROUS LEFT AC POWERED EQUIPMENT. LOA PROBE, L AFT FUEL PUMP, CTR L FUEL PUMP, L FMC FAIL, L IRS ON DC, ANTISKID - NUMEROUS STATUS MESSAGES. ADVISED FLT CNTRL, MTC AND ATL. DECLARED EMERGENCY DUE TO OVERWEIGHT LANDING. FOUND CAPT INST XFER ON EICAS. REPLACED CAPT IBVSU, NO HELP. FOUND BROKEN TERMINAL ON C901 CIRCUIT BREAKER IN P31 PANEL. INSTALLED NEW TERMINAL, ALL OPS GOOD.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 27,477 hrs · 13,239 cycles

THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AT FS 1844 BETWEEN STRINGERS 25L & 26L. THE DAMAGE WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER. THE REPAIR WAS INSTALLED PER ER/A 258909-14, REV B.

Part: SKIN — GOUGED (FUSELAGE) · airframe 27,477 hrs · 13,239 cycles

THE FUSELAGE SKIN WAS FOUND GOUGED AT THE STRINGER 14L SKIN LAP SPLICE AT FS 1705. THE GOUGE WAS REMOVED WITH A CUTOUT IN THE UPPER AND LOWER SKIN PANEL. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 368721-14, REV B.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,731 hrs · 12,887 cycles

ON INSPECTION, FOUND AFT LT EMERGENCY FLASHLIGHT NOT FLASHING. REPLACED BATTERY, CHECKS GOOD.

Part: EEL PWR SUPPLY — FAILED (CABIN)

AFT FLOOR TRACK LIGHTING INOP. REPLACED EMERGENCY BATTERY PACK AND PWR SUPPLY.