N709TW

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 89,700 hrs · 23,867 cycles

R2 DOOR SLIDE LIGHT INOP DURING GIRT BAR LUBE. PERFORMED ADJUSTMENT OF THE GIRT BAR MECHANISM PER B757 AMM 52- 11-25. OPS CHECKS GOOD. ALL RIIS COMPLETE. (7684770)

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 89,569 hrs · 23,835 cycles

SHIP 6806 DURING SERVICE CHECK FOUND D4L SLIDE BELOW PRESSURE. CORRECTIVE ACTION: REMOVED SLIDE 4L PER WORKCARD 2566-9001-4L SAFETY PINS FOR ASSIST BOTTLE INSTALLED. INSTALLED NEW SLIDE PER B757 JIC 2566-9001-4L. RII TASK C/W. (7684726)

Part: SWITCH — FAULTED (ZONE 800) · airframe 89,504 hrs · 23,820 cycles

DOOR 4R SLIDE ARM LIGHT DID NOT ILLUMINATE WITH SLIDE ARMED. REMOVED AND REPLACED DOOR 4R "SLIDE" LIGHT KORRY SWITCH REF B757 AMM 25-66. PERFORMED ADJUSTMENT OF GIRT BAR PROX. SWITCH IAW AMM 25-66 PERFORMED 4R DOOR GIRT BAR MECHANISM OPS CHK PER B757 AMM 52-11. OPS CHK GOOD. (7794586)

Part: LINE — OUT OF POSITION (ZONE 800) · airframe 89,484 hrs · 23,816 cycles

WHILE COMPARING DOOR 4R MODE SELECTOR LEVER TO DOOR 4L FOUND 4L SELECTOR LEVER NOT COMPLELY ARMING. UPON INSPECTION OF THE GIRT BAR, FOUND THE MOORING LINE CLIP SITTING UNDER THE BAR RETURNED IT BACK INTO THE SLIDE PACKDOOR SLIDE ARMED AND DISARMED W/NO ISSUES. (7794575)

Part: ELEC CONNECTOR — MISINSTALLED (ZONE 200) · airframe 88,525 hrs · 23,598 cycles

FOUND 41DEF OVERHEAD EMERGENCY LIGHT INOP. R/R HOUSING ASSY PER B757 AMM 32-51. UPON LOCATING BATT PACK M736 & M737 FOUND CONNECTORS INSTALLED INVERSELY. SWAPPED CONNECTORS TO CORRECT CONFIG. FAULT NOW LOCATED AC LEFT SIDE @ SEATS 40 ABC TO AFT. 41DEF NML. RR M736 BATT AND CHARGER IAW AMM 33-51. ALL EMERG LIGHT TEST GOOD. (7774124)

Part: HOUSING — DETACHED (ZONE 200) · airframe 88,261 hrs · 23,536 cycles

FOUND EMERGENCY LIGHT HOUSING BROKEN OFF AND WIRE HANGING UNDER SEAT 39DEF. R/R SEAT 39DEF EMERGENCY LIGHT HOUSING IN REF TO B757 AMM 25-25 -OPS CHECK NML.

Part: CHECK VALVE — ODOR (ZONE 100) · airframe 88,147 hrs · 23,492 cycles

AIRCRAFT 6806, PLASTIC SMELL IN COCKPIT. REPLACED RIGHT GROUND PNEUMATIC CONNECTION CHECK VALVE PER AMM 36-11-03. (LP 1103565)

Part: BUSTLE — LOOSE (ZONE 800) · airframe 87,600 hrs · 23,363 cycles

SHIP 6806 COMPONENTS HANGING FROM UNDER SLIDE BUSTLE WHEN DOOR OPEN. CORRECTIVE ACTION: REMOVED BUSTLE AND SECURED LOOSE MATERIAL. REINSTALLED BUSTLE. RII C/W. (0998462)

Part: BUSS — FAULTY (ZONE 100) · airframe 87,008 hrs · 23,179 cycles

SHIP 6806 -DIV/DE- TO PHX DUE TO RIGHT GEN INOP WITH APU ON MEL. CORRECTIVE ACTION: R/R BPCU AND IDG.

Part: LAMP — INOPERATIVE (ZONE 800) · airframe 86,560 hrs · 23,021 cycles

SHIP 6806 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:604. CORRECTIVE ACTION: RELAMPED AND PERFORMED ADJUSTMENT OF D2R GIRT BAR MECHANISM IAW B757 AMM 52- 11-25, ENGAGEMENT LIGHT CHECK OK

Part: SIGN — LOOSE (ZONE 200) · airframe 86,295 hrs · 22,929 cycles

SHIP 6806 L2 DOOR EMERGENCY EXIT SIGN COVER OVER L2 DOOR LOOSE. CORRECTIVE ACTION: ACCOMLISHED SECTION I TIME LIMITED REPAIR PER RI ER/A 623032-14 REV ORIGINAL. C/W B757 ER/A 623032-14 REV ORIGINAL SECTION III PERMANENT REPAIR IAW ER/A INSTRUCTIONS. (6491909)

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 86,242 hrs · 22,910 cycles

SHIP 6806 L AFT ENT DOOR EICAS CAME ON MOMENTARILY WHEN GEAR WAS SELECTED DOWN AT 170 KTS 2100 FT. WENT OUT AFTER A FEW SECONDS. CORRECTIVE ACTION: OPS CHECK DOOR IAW B757 AMM 52-11. DOOR INDICATIONS NORMAL. NO DEFECTS NOTED. (6491398)

Part: WIRE — DAMAGED (ZONE 200) · airframe 85,677 hrs · 22,743 cycles

SHIP 6806 EMERGENCY FLOOR PATH LIGHTS INOP AT SEATS 1R-4R INOP. CORRECTIVE ACTION: T/S PER WDM 33-51-21. FOUND DAMAGED WIRE W3532-9122, REPAIRED SAME PER B757 WDM 33-51-21 IAW SWPM 20. EMER LTS OPS NORM, (6366164)

Part: ESCAPE ROPE — OUT OF POSITION (L2 DOOR) · airframe 85,473 hrs · 22,700 cycles

SHIP 6806 FA UNABLE TO ARM DOOR 2L. CORRECTIVE ACTION: RE-STOWED GREEN ROPE ON SLIDE. NO 2L DOOR ARMS OK. REF B757 AMM 52-11. (5132752)

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 85,237 hrs · 22,646 cycles

SHIP 6806 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:603 EXIT SIGN FELL OFF. CORRECTIVE ACTION: RE-ATTACHED EXIT SIGN AT 2L. (0509517)

Part: PAN — CORRODED (ZONE 100) · corrosion level 2 · airframe 85,229 hrs · 22,644 cycles

SHIP 6806 REMOVED FWD LAV SVC PAN AND LAV PAN SUPPORT PER B757 SRM 51-40. FOUND SURFACE CORROSION ON SKIN UNDER LAV SVC PAN. CORRECTIVE ACTION: CLEANED AND EVALUATED, DRILLED NEW SUPPORT UPPER AND INSTLLED PAN AND SUPPORT, C/W PER B757 SRM. (0499169)

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 84,894 hrs · 22,567 cycles

SHIP 6806 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. CORRECTIVE ACTION: RESECURED EXIT SIGN. (0432283)

Part: CONTROL PANEL — FAILED (ILS) · airframe 84,862 hrs · 22,561 cycles

SHIP 6806 -DIV- TO ONT DUE TO ILS GLIDESLOPE FAILED. CORRECTIVE ACTION: REPLACED ILS CONTROL PANEL.

Part: DRAG FITTING — CORRODED (LT ENGINE) · airframe 84,846 hrs · 22,556 cycles

DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON FITTING AT 8 O CLOCK POSITION, HOLE #2 CORROSION ON FITTING-SKIN AND BTW TO 1-2 O CLOCK POSITION,AND GOUGE ON FITTING-SKIN BTW TO 1-2 O CLOCK POSITION AND BTW TO 9-10 O CLOCK POSITION; HOLE #3 CORROSION ON FITING-SKIN BTW TO 9-10 O CLOCK POSITION AND GOUGE ON FITTING BTW TO 7-8 O CLOCK POSITION . HOLE #4 CORROSION AND GOUGE ON FITTING-SKIN BTW 3-4 O CLOCK POSITION , HOLE #5 CORROSION ON SKIN-FITTING BTW TO 9-10 O CLOCK POSITION, AND GOUGE ON SKIN BTW TO 12-1 O CLOCK POSITION . HOLE #6 GOUGE ON SKIN 7 O CLOCK POSITION. HOLE #7 CORROSION AND GOUGE ON FITTING-SKIN BTW TO 8-9 O CLOCK POSITION. HOLE #8 CORROSION ON FITTING-SKIN BTW 8-9 O CLOCK POSITION AND GOUGE ON FITTING BTW TO 5-6 O CLOCK POSITION , HOLE #9 CORROSION-GOUGE ON FITTING AND SKIN BTW TO 10-11 O CLOCK POSITION, GOUGE ON FITTING AT 7 O CLOCK POSITION. HOLE #10 CORROSION ON SKIN BTW TO 7-8 O CLOCK POSITION AND GOUGE ON FITTING BTW TO 8-9 O CLOCK POSITION IN REF . CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00347: HOLES #1, #2, #3, #4, #5, #6, #7, #8, #9 & #10 WERE REPAIRED PER PRI 618107-14 REV. 5 & ER/A 618107-14AD REV. ORIG.

Part: FRAME — DENTED (BS 540 S24-25L) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 AMOC, ERA 618543-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME AT STA 540, BETWEEN S-24L & S-25L WAS FOUND DENTED. CORRECTIVE ACTION:REF ERA 618543-14. (0399211)

Part: FRAME — DENTED (BS 540 S24-26L) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 DENTS ON FRAME STA. 540, BTW S-24L TO S-26L AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00802: FRAME STA. 540, BTW S-24L TO S-26L AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 618543-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (0400438)

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 STUCK EMERGENCY HANDLE OF ARMING/DISARM SLIDE MECHANISM AT 4R PASSENGER DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00816: SYSTEM TEST GIRT BAR MECHANISM WAS PERFORMED AND DISCREPANCE WAS CORRECTED PER B 757-200 AMM 52-11.

Part: SKIN — NONE (LT WING) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 618107-14AD. CORRECTIVE ACTION: REF ERA 618107-14AD. (0399401)

Part: SKIN — DAMAGED (BS 560 & 620) · airframe 84,846 hrs · 22,556 cycles

FUSELAGE / EXTERNAL SKIN / FWD CARGO DOOR CUTOUT/ BTW BS 560 & 620 AT S-26R, ELONGATED HOLES. REF ERA 618195-14.

Part: FLOOR SUPPORT — CORRODED (BS 1470-1510) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

AIRCRAFT 6806, CORROSION LEVEL 2 ON FLOOR STRINGERS (8 EAS) LBL/RBL: 2, 7,10 AND 16 STA. 1470 ALSO (5 EAS) LBL/RBL: 2, 7, (10 RBL) STA. 1510 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: STRINGER IN AFT CARGO COMPARTMENT REPAIRED PER REPAIR PER B757-200 SRM 53-00-53-2R PROCEDURE 1 REP. 1. (LP 0368549)

Part: FLOORBEAM — CORRODED (BS 1280 RBL 24) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON FLOOR BEAM AT STA 1280 RBL 24 AT CPAX. CORRECTIVE ACTION: SUMMARY OF NRC 00478: FLOOR BEAM AT STA 1280 RBL 24 AT CPAX. WAS REPAIRED PER B757-200 S.R.M. (0367369)

Part: SNUBBER — OUT OF LIMITS (L4 DOOR) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF. AMDS 5211-3001-4L STEP 3 : ROTARY SNUBBER PIN EXTENSION OUT OF LIMITS AT 4L DOOR. CORRECTIVE ACTION: WAS REPLACED BY SERVICEABLE SNUBBER PER B757-200 AMM 52-11-10 AND SAME 4L PASSENGER DOOR WAS INSTALLED PER B757-200 AMM 52-11-01, ADJUST THE SAME DOOR WILL BE PERFORM ON AMDS. (0366261)

Part: INTERCOSTAL — CORRODED (BS 1300-1320) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF. TO NRC 00165: CORROSION ON INTERCOSTAL 30 BTW STA 1300 AND 1320 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 744: INTERCOSTAL 30 BTW STA 1300 AND 1320 AT AFT CARGO COMPARTMENT. WAS REPLACED" PER B757-200 SRM. (0364846)

Part: PLATE — CORRODED (BS 1380-1440) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF. NRC 0168: CORROSION ON RH SIDE PLATE (UPPER AND LOWER SURFACE) 1380 TO 1440 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00654. RH SIDE PLATE (UPPER AND LOWER SURFACE) 1380 TO 1440 AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (0364848)

Part: FLOOR SUPPORT — CORRODED (BS 1328-1331) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF TO NRC S/N 00162: CORROSION OUT LIMITS ON FLOOR SUPPORTS (JOOGLE AREA) BTW STA 1328 TO 1331 AND LBL 16.10, LBL 10.45, RBL 2.90 RBL 7.55 RBL 10.45 RBL 16.10 AT AFT CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 724: CHANNELS 6 (E/AS) WERE REPLACED PER B757-200 SRM. (0364740)

Part: SKIN — DENTED (FUSELAGE) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF TO MON 0953076, FOUND 2 DENTS ABOUT 5 FEET AFT OF C1. DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00203. AREA WAS REPAIRED PER B757-200 S.R.M. 53- 00-01-2R REPAIR 29. (0363644)

Part: SKIN — DENTED (LT SIDE) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF TO MON 0953076, FOUND 2 DENTS ABOUT 5 FEET AFT OF C1. DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00203. AREA WAS REPAIRED PER B757-200 S.R.M. 53- 00-01-2R REPAIR 29. (0363621)

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON FLOOR BEAM STA 1640 RBL 55 TO LBL 55 AT FLOOR STRUCUTRE CABIN PAX. CORRECTIVE ACTION: SUMMARY OF NRC 00471. CORROSION ON FLOOR BEAM STA 1640 RBL 55 TO LBL 55 AT FLOOR STRUCUTRE CABIN PAX.WAS REPAIRED PER B757-200 SRM 53-00-51-2R REPAIR 9. (0359120)

Part: ANGLE — CORRODED (AFT CRGO THSHOLD) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON FWD ANGLE OF SILL FITTING TO ATTACH THRESHOLD (LOWER SIDE) AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00433, FITTING TO ATTACH THRESHOLD (LOWER SIDE) AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (0358244)

Part: FLOORBEAM — CORRODED (BS 377 LBL 59) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON FLOOR BEAM BTW. STA.377 AND LBL .59 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY, OF NRC 00552 FLOOR BEAM BTW. STA.377 AND LBL.59 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER B757-200 SRM 53-00-51-2R-8 REPAIR 8. (0358427)

Part: FLOORBEAM — CORRODED (BS 345 BL0-LBL25) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON FLOOR BEAM BTW LBL 0. AND LBL 25 STA 345.0 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00547. CORROSION LEVEL 2. AREA WAS REPAIRED PER B757-200 SRM 53-00-51-2R REPAIR 10. (0358572)

Part: FLOORBEAM — CORRODED (BS 324 RBL 40) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON FLOOR BEAM RBL 40 STA 324.0AT PAX CABIN. CORRECTIVE ACTION: SUMMARY, OF NRC 00545, FLOOR BEAM RBL 40 STA 324.0AT PAX CABIN WAS REPAIRED PER B757-200 S.R.M. 53-10-08. (0358357)

Part: WEB — CORRODED (BS 1380-1400) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON WEB BTW STA 1400 AND 1380 AT RH PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00558, WEB ON BTW STA 1400 TO 1380 AT RH PAX CABIN WAS FABRICATED PER B757-200 SRM. (0358247)

Part: FRAME — GOUGED (BS 1280 S11-12L) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 GOUGES ON REPAIR DOUBLER ON FRAME AT STA 1280 BTW S-11L TO S-12L AT CPAX. CORRECTIVE ACTION: SUMMARY, OF NRC 00441: REPAIR DOUBLER ON FRAME AT STA 1280 BTW S -11L TO S-12L AT CPAX WAS REPLACED PER B757-200 S.R.M. (0358262)

Part: SNUBBER — OUT OF TOLERANCE (L1 DOOR) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF. ROTARY SNUBBER PIN EXTENSION OUT OF LIMITS AT 1L DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00426: SNUBBER WAS REMOVED AND REPLACED BY A SERVICEABLE SNUBBER PER B757-200 IPC 52-11-01-03 AND WILL BE INSTALL PER NRC 556. (0355768)

Part: SEAT TRACK — CORRODED (BS 1572-1640) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CORROSION ON OUTBOARD SEAT TRACK RH SIDE STA . 1572,1600 TO 1605,1633 TO 1640 AT PAX CABIN. CORRECTIVE ACITON: SUMMARY OF NRC 00232. SEAT TRACK BTW STA 1540 TO STA 1640 AND RBL 45.50 WAS REPLACED PER B757-200 SRM. (0353589)

Part: DECK PLATE — CORRODED (BS 1718 RBL11-16) · corrosion level 2 · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 IN REF TO NRC 00469: CORROSION ON DECK PLATE STA 1718 RBL 11 TO 16. CORRECTIVE ACTION: SUMMARY OF NRC 00566: CORROSION LEVEL 2. CORROSION ON DECK PLATE STA 1718 RBL 11 TO 16..WAS REPAIRED PER B757-200 SRM 53-60-51- 2R PROCEDURE 2 REPAIR 2. (0353167)

Part: STRAP — CRACKED (BS 365-377 LBL24) · airframe 84,846 hrs · 22,556 cycles

SHIP 6806 CRACK ON STABILIZATION STRAP BTW STA. 365 TO 377 AND LBL. 24 AT LOWER SIDE OF PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00650:AREA WAS PREVIOUSLY REPAIR PER B757-200 SRM 53-10-51. (0346915)

Part: BLANKING PLATE — NONE (NONE) · airframe 84,846 hrs · 22,556 cycles

AIRCRAFT 6806, THIS ALTERATION REMOVES THE LOWER FORWARD ATG4 ANTENNA BLANKING PLATE AND INTERNAL STRUCTURE ORIGINALLY INSTALLED BY AA 2330-01298 AND 2330-01322. THIS ANTENNA IS NO LONGER USED AND HAS ICA INSPECTIONS THAT CANNOT BE COMPLETED. CORRECTIVE ACTION: THE ANTENNA BLANKING PLATE IS REMOVED AND REPLACED WITH A NEW PERMANENT PLATE. REMAINING INTERNAL STRUCTURE IS REMOVED OR TRIMMED PER ER/A 616999-14. (LP 0272603)

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 84,837 hrs · 22,553 cycles

SHIP 6806 OXYGEN PANEL MASK DEPLOYED / LOCATIONS:204. CORRECTIVE ACTION: RESECURED O2 MASK PER B757 AMM 35-21. (1535128)

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 84,773 hrs · 22,537 cycles

SHIP 6806 O2 MASK @ 3L LAV DROPPED ON TAKE OFF. CORRECTIVE ACTION: RESECURRED 3L LAV O2 MASK REF B757 AMM 35-20. (7053827)

Part: LIGHT — UNSECURE (SEAT 22D) · airframe 83,879 hrs · 22,350 cycles

SEAT 22D MOUNTED EMERGENCY LIGHT UNSECURE. SECURED THE LIGHT AND PANEL OVER SEAT 22D. CHECKED NORMAL IAW AMM 33-51.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 83,619 hrs · 22,298 cycles

(AIRCRAFT 6806, L/P 6241939) O2 MASK 3R BATHROOM DROPPED. CORRECTIVE ACTION: SECURED 3R LAV 02 MASK PANEL PER B757 AMM 35-21.

Part: OXYGEN MASK — UNWANTED DEPLOY (RT LAVATORY) · airframe 83,570 hrs · 22,288 cycles

(AIRCRAFT 6806, L/P 6241912) ON TAKEOFF AFT R LAV O2 MASKS DROPPED. CORRECTIVE ACTION: FA WAS ABLE TO SECURE. / VERIFY FUNCTIONALITY. INSP AFT RT LAV O2 MASK PER B757 AMM 35-21. NO DISCREPENCIES NOTED. ITEM CLEARED.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY R3) · airframe 83,549 hrs · 22,283 cycles

(AIRCRAFT 6806, L/P 6241902) LAV 3R OXYGEN DEPLOYED. CORRECTIVE ACTION: INSPECTED OXYGEN GENERATOR. AND RE-INSTALLED MASKS PER B757 AMM 35-21.

Part: OXYGEN MASK — UNWANTED DEPLOY · airframe 83,533 hrs · 22,280 cycles

(AIRCRAFT 6806, L/P 1367824) OXYGEN PANEL MASK DEPLOYED / OXYGEN PANEL OPENMASK DROPPED / INTERIOR. CORRECTIVE ACTION: RE-SECURED O2 MASK AND DOOR AT LOCATION 204 AS NECESSARY. VERIFIED O2 GEN WAS NOT ACTIVATED. OK FOR SVC.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 83,308 hrs · 22,237 cycles

SHIP 6806 EXIT SIGN OVER 2L DOOR FALLING OFF. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT LENSE ABOVE L2 DOOR. (1332344)

Part: SIGN — DETACHED (CABIN) · airframe 83,297 hrs · 22,235 cycles

(AIRCRAFT 6806, L/P 5757274) EXIT SIGN OVER 2L DOOR FELL OFF. CORRECTIVE ACTION: RESECURED EXIT SIGN OVER 2L.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 83,295 hrs · 22,234 cycles

SHIP 6806 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. CORRECTIVE ACTION: RESECURED LENS. CHKS GOOD. (1330179)

Part: SIGN — DETACHED (CABIN) · airframe 83,254 hrs · 22,226 cycles

(AIRCRAFT 6806, L/P 5757262) DOOR 2L EXIT LT FELL DURING TAXI WILL NOT STAY IN PLACE. CORRECTIVE ACTION: REINSTALLED L2 EXIT SIGN PER B757 AMM 33-51.

Part: WATER SEPARATOR — ODOR (CABIN AIR) · airframe 82,522 hrs · 22,087 cycles

FA'S AND PASSENGERS REPORT AN ACRID/DEAD ANIMAL SMELL FROM 2-3 ROWS FWD OF AFT LAC TO 2-3 ROWS AFTE OF AFT LAV. SMELL STARTED JUST AFTER TAKEOFF. INTIALLY THE SMELL WAS VERY STRONG. IT SUBSIDED TO MANAGEABLE FOR THE REMAINDER OF FLIGHT. REPLACED WATER SEPARATOR AND SECURED FILL LINE CLAMP. SERVICED LAV. CKS OK.

Part: ARM — FOD (R1 DOOR) · airframe 82,312 hrs · 22,046 cycles

R1 DOOR WON'T ARM. REMOVED DEBRIS FROM 1R DOOR ARMS OK PER AMM 52-11.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 82,204 hrs · 22,027 cycles

ESCAPE SLIDE ARMED COND IND 1L DOOR KNUCKLE KNOCKER INOP. PERFORMED OPERATIONAL CHECK OF DOOR 1L ESCAPE SLIDE INDICATION CHKS GOOD IAW AMM 25-66.

Part: LANYARD — UNSECURE (EVAC SLIDE) · airframe 81,884 hrs · 21,968 cycles

SHIP 6806 ON PREFLIGHT WALKAROUND, STRAPS FROM SLIDE ON 1R DOOR UNSECURED AND HANGING OUTSIDE OF AIRCRAFT BETWEEN BOTTOM OF 1R DOOR AND DOOR SILL. CORRECTIVE ACTION: TUCKED LANYARD BACK INTO SECURE LOCATION. DOOR ARMS & DISARMS PROPERLY. (5980612)

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 44 ABC) · airframe 80,270 hrs · 21,662 cycles

SHIP 6806 ROW 44 ABC OXY MASKSDEPLOYED ON TAKEOFF.COMPARTMENT LATCH INOP. CORRECTIVE ACTION: RESTOWED MASKS IAW B757 AMM 35-21. (0953029)

Part: GIRT BAR — FOD (R1 DOOR) · airframe 79,566 hrs · 21,523 cycles

SHIP 6806 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS: 1R ARMING LEVER MOVES ONTAKE OFFSLIDE LIGHT GOES OUTON CRUSEARMING LEVERMOVES BACK TO POSIONLIGHT COMES BACKON / INTERIOR. CORRECTIVE ACTION: FOUND DEBRIS ON GIRT BAR COVERS AT 1R DOOR, REMOVED AS REQ. C/W OPS CK OF IND. AS PER B757 AMM 52-70, OPS CK GOOD. (0874784)

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 24C) · airframe 79,509 hrs · 21,510 cycles

(AIRCRAFT 6806, L/P 0867011) OXYGEN PANEL MASK DEPLOYED / LOCATIONS:24C / INTERIOR. CORRECTIVE ACTION: REFERENCE: LOGPAGE 0867009). STOWED MASKS & PANEL PER B757 AMM 35-21. PANEL IS SECURE.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 24B) · airframe 79,509 hrs · 21,510 cycles

(AIRCRAFT 6806, L/P 0867010) OXYGEN PANEL MASK DEPLOYED / LOCATIONS:24B / INTERIOR. REFERENCE LOGPAGE 0867009. STOWED MASKS & PANEL PER B757 AMM 35-21. PANEL IS SECURE.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 24A) · airframe 79,509 hrs · 21,510 cycles

(AIRCRAFT 6806, L/P 0867009) OXYGEN PANEL MASK DEPLOYED / LOCATIONS:24A / INTERIOR. STOWED MASKS & PANEL PER B757 AMM 35-21. PANEL IS SECURE.

Part: GIRT BAR — MISSING (L1 DOOR SLIDE) · airframe 79,454 hrs · 21,499 cycles

(AIRCRAFT 6806, L/P 0855536) L1 DOOR GIRT BAR MISSING ON NEW SLIDE. INSTALLED NEW GIRT BAR REF AMDS CARD 2040-0191-1L JOB# 131-0002.

Part: LIGHT — BURNED (ROW 44) · airframe 79,265 hrs · 21,460 cycles

(AIRCRAFT 6806, L/P 4732492) READING LIGHT CAPT SIDE ROW 36-44 WENT OUT. BURNING SMELL REPORTED BY F.A'S. SMELL DISSIPATED OUT . F/A/ STATED PUTTING NOSE NEAR OVERHEAD LIGHTS OF ROW 44 THAT SLIGHT ODOR DETECTED. WHILE PERFORMING NO-GO ODI FOR SMOKE/FUMES REPORTED IN THE CABIN FROM SPECIFIC ARES. FOUND LED READING LIGHT ASSEM AT 44A BURNING AND SMOKING DURING OPERATION. REPLACED LED ASSEM PER B757 M/M 33-23. ALSO REPLACED TRANSFORMER T10014 PER B757 SWPM.

Part: INDICATOR — LACK OF LUBE (L2 DOOR) · airframe 79,068 hrs · 21,424 cycles

(AIRCRAFT 6806, L/P 0789934) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:02L / KNUCKLE KNOCKER STICKS WHEN ARMING THE 2L DOOR / INTERIOR. LUBRICATED KNUCKLE KNOCKER MECHANISM.

Part: INDICATOR — INOPERATIVE (DOOR ARMING) · airframe 78,724 hrs · 21,362 cycles

(AIRCRAFT 6806, L/P 0758023) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:601 / ACARS TEXT: FRC521207601 KNUCKLE KNOCKER INOP / INTERIOR. ADJUSTED DOOR BUSTLE. OPS NML.

Part: LIGHT — MISSING (SEAT 43DEF) · airframe 78,342 hrs · 21,293 cycles

DURING AN OVERNIGHT CHECK, FOUND THE SEAT MOUNTED EMERGENCY LIGHT MISSING AT ROW 43DEF. INSTALLED A NEW EMERGENCY LIGHT AT IAW AMM 33-51.

Part: GIRT BAR — LACK OF LUBE (L4 DOOR) · airframe 77,393 hrs · 21,123 cycles

L4 ARMING HANDLE HAS TO BE CLOSED MORE THAN NORMAL TO FORCE INDICATE ARMED. LUBRICATED THE L4 DOOR GIRT BAR, OPS CHECKED NORMAL IAW AMM 25-61. ACFT OK FOR SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 76,864 hrs · 21,023 cycles

READING LIGHT AT 38B FLICKERED THEN BURNED OUT. GAVE AN ELECTRICAL ODOR. INITIALLY A LITTLE SMOKE THEN DISSIPATED QUICKLY. ODOR LINGERED BUT DID NOT INTENSIFY. FOUND PAX SEAT 37C READING LIGHT AT FAULT. REPLACED LIGHT ASSY AND BOARD PER CMM 25-23. ALSO READING LIGHT 38ABC INOP. REPLACED 38ABC READING LIGHT PER CMM 25-23. ALL PARTS ODI QUARANTINE.

Part: INDICATOR — DAMAGED (L1 DOOR) · airframe 76,341 hrs · 20,918 cycles

L1 DOOR ARMED INDICATOR STICKER IN POOR CONDITION PREVENTING INDICATOR FROM EXTENDING WHEN DOOR IS ARMED. REPLACED THE STICKER, CHECKED OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 76,036 hrs · 20,848 cycles

SHORTLY AFTER TAKEOFF AND DURING INITIAL CLIMB, A STRONG MUSTY ODOR AND SLIGHT HAZE IN CABIN REPORTED BY FA'S. DISSIPATED AFTER ABOUT 10 MINUTES, ALL NORMAL SINCE. ODI WORK SCOPE C/W 705535. NO CONTAMINATION FOUND. ALL COMPONENTS AND SYSTEMS CHECKED NORMAL.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 75,949 hrs · 20,830 cycles

L1 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. ADJUSTED THE KNUCKLE KNOCKER. OPS NORMAL.

Part: GIRT BAR — DAMAGED (R2 DOOR) · airframe 75,515 hrs · 20,744 cycles

DURING A SERVICE CHECK, FOUND THE R2 DOOR NOT DISARMING PROPERLY. INSTALLED SAFETY PINS IN THE SLIDE AND DOOR ASSIST BOTTLE. FOUND THE R2 DOOR GIRT BAR AFT ENGAGEMENT SENSOR RETENTION SPRING BENT. REPLACED SLIDE PACK GIRT BAR IAW AMM 25-66-01.

Part: DOOR — UNKNOWN (R2) · airframe 75,515 hrs · 20,744 cycles

UNABLE TO DISARM THE R2 DOOR. DOOR DISARMED OK.

Part: INDICATOR — OUT OF ADJUST (L1 DOOR) · airframe 75,249 hrs · 20,692 cycles

(AIRCRAFT 6806, L/P 3676578) 1L DOOR KNUCKLE KNOCKER INOP. ADJ AS REQUIRED.

Part: GIRT BAR — DETACHED (R1 DOOR) · airframe 74,283 hrs · 20,491 cycles

R1 DOOR WOULD NOT ARM SLIDE LIGHT WOULD NOT COME ON. ATTACHED THE GIRT BAR MECHANISM. OPS NORMAL.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 74,184 hrs · 20,470 cycles

R1 DOOR 1R WILL NOT ARM. REMOVED DEBRIS FROM THE GIRT BAR AREA. THE R1 DOOR ARMS NORMALLY.

Part: STRUCTURE — OUT OF ADJUST (DOOR) · airframe 74,134 hrs · 20,461 cycles

DOOR ARMED HANDLE INOPERATIVE ADJUSTED THE TRIM ON DOOR. ALL CHECKED OK IAW AMM 52-11-02.

Part: GIRT BAR — DAMAGED (PAX DOOR) · airframe 73,480 hrs · 20,340 cycles

AFT RT ENTRY DOOR BOTTOM AFT GIRT BAR DAMAGED. REPAIRED IAW ERA 532494-14MA AND ERA 532494-14 MA, REV B.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 71,418 hrs · 19,889 cycles

FUSELAGE SKIN HAS A PREVIOUS DOUBLER ON LT SIDE OF A/C WITH ADENT AT THE AFT END OF THE DOUBLER, APPROX STA 646 ABOVE STRINGER 16. (96-17) WITH DENT TO BE ALSO ON FUSELAGE SKIN ADJACENT TO DENT ON DOUBLER. ACCOMPLISHED TIME-LIMITED REPAIR ON FUS SKIN ON LT SIDE OF A/C AT BETWEEN STA 620-650 STR 16L IAW ER/A 547325-14 REV A.

Part: LINER — OUT OF ADJUST (L4 DOOR) · airframe 69,212 hrs · 19,494 cycles

L4 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. L4 DOOR KNUCKLE KNOCKER DOES NOT EXTEND WHEN DOOR IS ARMED. ADJUSTED DOOR LINING AROUND KNOCKER. OPS NORMAL.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 66,120 hrs · 18,866 cycles

RAM-1 1R DOOR HARD TO ARM. DURING DOOR INSPECTION WITH BUSTLE REMOVED, FOUND SLIDE SURVIVAL PACK GREEN ROPE CHORD ON FWD SIDE OF SLIDE HAD COME OUT FROM STOWED POSITION AND WRAPPED AROUND GIRT BAR MECHANISM AND GIRT BAR SLIDER CAUSING INTERFERENCE WITH GIRT BAR SLIDER. REROUTED CHORD BACK TO ORIGINAL POSITION AND RESTOWED INSIDE PACK. DOOR OPS CHECK NORMAL.

Part: ENGINE — MAKING METAL (RIGHT) · airframe 65,170 hrs · 18,690 cycles

DIVERTED DUE TO A RT ENGINE OIL FILTER CAUTION EICAS MESSAGE. FOLLOWED THE QRH AND THE ENGINE WAS SHUTDOWN. EMERGENCY WAS DECLARED. TROUBLESHOT IAW FIM 79-21-00-815-803-P00. FOUND MAGNETIC CHIP DETECTOR CONTAMINATED IN EXCESS OF INSPECTION LIMITS AMM 79-21-00. R & R NR 2 ENGINE IAW 71-00-9902E-02. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 64,087 hrs · 18,503 cycles

MAINTENANCE FOUND R1 DOOR EMERGENCY POWER RESERVOIR PRESSURE LOW. THE EMERGENCY POWER RESERVOIR FOR THE R1 DOOR WAS REPLACED.

Part: FUEL — LEAKING (WING) · airframe 63,645 hrs · 18,414 cycles

AT DEPARTURE, FUEL LEAK REPORTED FROM NR 6 SLAT TRACK HOUSING. PHYSCIAL DAMAGE NOTED ON NR 6 SLAT BOX. REMOVED SLAT 6 INBD BOX. INSTALLED BOX IAW PRI 535438-14AD. REPAIR ACCOMPLISHED IAW ERA 535438-14AD.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 62,780 hrs · 18,217 cycles

FOUND DURING INSPECTION, FOUND L2 DOOR EXIT SIGN BROKEN. REINSTALLED EXIT SIGN COVER. CHECKED GOOD.

Part: WEB — CORRODED (BS 1681-1720) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BETWEEN BS 1681-1720, BL 0 - RBL 30, FLOOR WEB CORRODED. REPAIRED IAW ERA 531463-14 REV.O.

Part: SKIN — CORRODED (RT WING SLAT) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

RT WING SLAT 7 UPPER SURFACE INBD SIDE CORRODED AROUND FASTENER. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: TRIGGER — FRACTURED (R4 DOOR) · airframe 62,778 hrs · 18,215 cycles

TRIGGER ON R4 DOOR IS FRACTURED AT EMERGENCY ASSIST ARM ON TOP HINGE. R & R TRIGGER ON R4 DOOR AT EMERGENCY ASSIST ARM OR TOP HINGE IAW AMM.

Part: MOUNT — CORRODED (BS 446) · airframe 62,778 hrs · 18,215 cycles

BS 446.5, T-CAS ANTENNA MOUNT AREA CORRODED. ACCOMPLISHED CORROSION REMOVAL FROM T-CAS ANTENNA MOUNT PLATE IAW ERA 531462-14, REV O.

Part: WEB — CORRODED (BS 1681-1720) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BETWEEN BS 1681-1720, BL 0 - LBL 52 FLOOR WEB CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM AND ERA 531463-14.

Part: FRAME — DAMAGED (BS 580) · airframe 62,778 hrs · 18,215 cycles

FWD BILGE FUSELAGE FRAME DENTED AND CRUSHED, BS 580 BETWEEN STRINGERS 24-25L. REMOVED DAMAGE, AND INSTALLED A REPAIR IAW SRM.

Part: FRAME — GOUGED (BS 720) · airframe 62,778 hrs · 18,215 cycles

FWD CARGO BAY BS 720, STR 22R FOUND FRAME GOUGED. REMOVED DAMAGED AND FABRICATED REPAIR. INSTALLED REPAIR IAW SRM.

Part: FRAME — DENTED (BS 600) · airframe 62,778 hrs · 18,215 cycles

FWD CARGO BAY FRAME BS 600 BETWEEN STR 24-25 LT IS DENTED BETWEEN STR 24-25LT. REMOVED DAMAGE BY TRIMMED OUT FRAME FLANGE IAW SRM, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BS 365 FLOORBEAM CORRODED, RBL 12. REPAIRED IAW ERA 531459-14.

Part: FLOOR SUPPORT — CORRODED (BS 324-365) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

FLOOR SUPPORT INBD OF R2 DOOR THRESHOLD CORRODED. BS 324-365. RBL 60. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 1320) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BS 1320, RBL 21 HAS CORROSION AROUND NUT PLATE ON INTERCOSTAL. REMOVED CORROSION AND FOUND OUT OF LIMITS. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1640) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

FLOOR SUPPORT CORRODED AT BS 1640. LBL-52 INBD. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED REF SRM.

Part: FLOOR SUPPORT — CORRODED (BS 345) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BS 345, LBL 19 FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R NEW FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1671) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

FLOOR SUPPORT CORRODED AT BS 1671, -52 INBD. FOUND OUT OF LIMITS IAW SRM. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN FLOORBEAM TEE. BS 1640 CORROSION FROM BL 0 - RBL 60. REMOVED CORROSION AND FOUND OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1560-1640) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 1560-1640 LBL 45. R & R THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1632-1640) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN SEAT TRACK AT RBL 22 BS 1632-1640 HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS. R & R THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1632-1640) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN SEAT TRACK AT RBL 22 BS 1632-1640 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM. R & R THE SEAT TRACK.

Part: WEB — CORRODED (BS 1681-1720) · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BETWEEN BS 1681- 1720, BL 0 - RBL 52 WEB CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1632-1640) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN SEAT TRACK AT RBL 44 BS 1632-1640 HAS CORROSION. FOUND AREA OUT OF LIMITS. R & R SEAT TRACK SECTION REF DWG & SRM.

Part: INTERCOSTAL — CORRODED (BS 1300-1320) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BETWEEN BS 1300-1320 LBL 21 INTERCOASTAL HAS CORROSION AROUND NOT PLATE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED, LOCATED, DRILLED AND INSTALLED REF SRM.

Part: SEAT TRACK — CORRODED (BS 700-780) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

SEAT TRACK, RBL 24.75, BS 700 - 780 FOUND EXFOLIATED. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — GOUGED (BS 1450) · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN SEAT TRACK AT RBL 44 BS 1450 HAS A GOUGE. FOUND OUT OF LIMITS. FABRICATED SEAT TRACK SECTION AND INSTALLED.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN BS 345 FLOORBEAM CORRODED LBL 12 TO BL 0. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1560-1640) · corrosion level 2 · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 1560- 1640 LBL 24. R & R SEAT TRCK SECTION IAW SRM.

Part: FRAME — DAMAGED (BS 1280) · airframe 62,778 hrs · 18,215 cycles

MAIN CABIN FRAME BS 1280 HAS MECHANICAL DAMAGE BETWEEN S10-14L. CUT OUT DAMAGE AND INSTALLED A REPAIR IAW SRM.

Part: RESERVOIR — NO TEST (PAX DOOR) · airframe 58,748 hrs · 17,417 cycles

DOOR EMERGENCY POWER RESERVOIRS FAILED INSPECTION. REPLACED RESERVOIR IAW MM 52-11-30.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,419 hrs · 17,157 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51 OP CKS GOOD.

Part: GIRT BAR — DAMAGED (R4 DOOR) · airframe 56,738 hrs · 17,030 cycles

R4 DOOR EMERGENCY POWER RESERVOIR EMPTY. GIRT BAR FOUND IN PIECES ON FLOOR. GIRT BAR MOUNTED AND RESERVOIR POWER ASSY REPLACED, AMM 52-11-30-404-013.

Part: LINER — PUNCTURED (RT ENGINE) · airframe 62,610 hrs · 18,174 cycles

DURING WALK-AROUND, FOUND PUNCTURE TO RT ENGINE INLET ACCOUSTIC LINING AT 8 O`CLOCK POSITION, APPROXIMATELY 2 FT AFT OF INLET LIP, APPROXIMATELY .5" X .2500" PUNCTURE. RT INLET COWL PUNCTURE REPAIRED IAW SRM 54-01-01, FIG 201.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,080 hrs · 16,914 cycles

RT MID GALLEY EMERGENCY LIGHTS INOPERATIVE AND AFT RED LENS MISSING. REPLACED EMERGENCY BATTERY LIGHT TRAY IAW AMM 33-51. OPS CHECK GOOD. OK FOR SERVICE.

Part: FITTING — CRACKED (AFT CARGO FRAME) · airframe 55,460 hrs · 16,802 cycles

AFT CARGO DOOR FRAME UPPER FWD FITTING STA 1400 AT DOOR LOCKED SWITCH CRACKED. R & R UPPER FWD DOOR FRAME FITTING NEAR DOOR LOCKED SWITCH IAW SRM 53-30.

Part: SKIN — BURNED (LT PACK DOOR) · airframe 53,486 hrs · 16,391 cycles

FOUND LIGHTNING STRIKE DAMAGE ON LT PACK DOOR, REPAIRED DAMAGE IAW SRM 52-40-02.

Part: SKIN — DENTED (BS 686) · airframe 62,610 hrs · 18,174 cycles

DENT FOUND IN FUSELAGE BS 686 BETWEEN STRINGERS 23 - 24R. INSPECTED AND REPAIRED IAW SRM 53-00-01.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 51,599 hrs · 16,031 cycles

AFTER TAKEOFF AT APPROXIMATELY 800AGL AIRCRAFT INGESTED BIRDS INTO NR 2 ENGINE, WHICH RESULTED IN MULTIPLE ENGINE STALLS. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED AIRPORT WITH NO FURTHER INCIDENTS REPORTED. REMOVED AND REPLACED ENGINE AND REPAIRED OR REPLACED DAMAGED COWLING AND RELATED COMPONENTS. RELATED AIRWORTHINESS INSPECTIONS COMPLETED, AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 51,380 hrs · 15,987 cycles

FUSELAGE SKIN PUNCTURED AT FS 690 BETWEEN S-24L AND S-25L. DOUBLER INSTALLED BY ER/A 501914-14 AND SRM 53-00-01 R3.

Part: UNKNOWN — UNKNOWN · airframe 42,444 hrs · 14,246 cycles

WHEN ADVANCING THROTTLES BOTH BLEEDS TRIPPED OFF AND LT BOOST PUMP STARTED FLASHING.

Part: RELIEF VALVE — LEAKING (FUEL SYSTEM) · airframe 41,306 hrs · 14,018 cycles

RAMP REPORTS FUEL LEAKING FROM RT WING. FOUND FUEL LEAKING FROM RT WING TANK FUEL PRESSURE RELIEF VALVE. RESET PRESSURE RELIEF VALVE. NO LEAKS NOTED. OK FOR SERVICE. ETOPS CATEGORY 'E'.

Part: COFFEEMAKER — SPARKS (F/C GALLEY) · airframe 39,741 hrs · 13,742 cycles

F/A REPORTED SPARKS COMING FROM LOW WATER BUTTON FROM AFT NR 2 COFFEEMAKER 1ST CLASS GALLET/ REMOVED AND REPLACED F/C COFFEEMAKER OPS CHECKS NORMAL.

Part: SKIN — DENTED (BS 1681-1701) · airframe 39,056 hrs · 13,611 cycles

ACCOMPLISHED PERMANENT REPAIR SRM 53-00-01 FIG 101 TO DENT AFT OF L4 DOOR 16IN AFT OF DOOR CUTOUT STA 1681-1701. ACCOMPLISHED PERMANENT REPAIR ON NON ROUTINE 120354 AT SAA IN SAT DURING HMV VISIT WORKING OFF THE OMI LIST CN U04148254.

Part: SKIN — DAMAGED (BS 610) · airframe 39,056 hrs · 13,611 cycles

ACCOMPLISH PERM REPAIR PER ERA 469215-14 REV A ACTL LONE 2300 FUSELAGE SKIN STR L16 APPROX STA 610 SKIN DENT (REF OMI LOG W/CN U06308025) C/W AT SAA - SAT ON N/R 120353 JOB 82594490001.

Part: STRUCTURE — CORRODED (BS 710) · airframe 39,056 hrs · 13,611 cycles

LAV SERVICE BOX CORRODED ON UPPER SIDE AT PLUMBING CONNECTION IN FWD CARGO COMPARTMENT AT FS 710 S21L. FABRICATED REPAIR DOUBLER ON NR 134068 AT SAA IN SAT DURING HMV VISIT.

Part: PAN — CORRODED (BS 425) · airframe 39,056 hrs · 13,611 cycles

LAV A PAN STRUCTURE CORRODED (EXFOLIATED) AROUND DRAIN DUCT STA 425 BL10L. INSTALLED NEW LAV PAN ON NR 126522 WHILE AT HMV IN SAT AT SAA.

Part: FRAME — BENT (BS 1400 S26L) · airframe 39,054 hrs · 13,609 cycles

FRAME BENT DENTED IN AFT CARGO AT STA 1400 ABOVE STR 26L AT SAA - SAT ON N/R 126358 JOB 8259770001.

Part: FLOORBEAM — CORRODED (BS 740) · airframe 39,054 hrs · 13,609 cycles

MAIN CABIN FLOOR INNER CUSP CHORD CORRODED IN MULTIPLE AREAS STA 740-14 -800 RT C/W AT SAA - SAT ON N/R 126437 JOB 82600270001.

Part: SEAT TRACK — CORRODED (BS 1080-1180) · airframe 39,054 hrs · 13,609 cycles

CABIN SEAT TRACK GOUGED SEVERAL PLACES STA 1080-1180 RBL 45 C/W AT SAA - SAT ON N/R 126470 JOB 82601390001.

Part: SEAT TRACK — GOUGED (BS 1540-1640) · airframe 39,054 hrs · 13,609 cycles

CABIN SEAT TRACK GOUGED SEVERAL PLACES STA 1540-1640 RBL 24 CORROSION AT STA 1640 C/W AT SAA - SAT ON N/R 136452 JOB 82601340001.

Part: FRAME — DENTED (BS 1480 S25-26L) · airframe 39,054 hrs · 13,609 cycles

AFT CARGO FS 1480 S26L-25L FRAME UPPER FLANGE DENTED AT SAA - SAT ON N/R 129452 JOB 8259850001.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 39,054 hrs · 13,609 cycles

MAIN CABIN FLOORBEAM STA 1660, RB0, UPPER SURFACE CORRODED AROUND FASTNERS AR SAA - SAT ON N/R 129491 JOB 82598990001.

Part: INTERCOSTAL — CRACKED (BS 1320) · airframe 39,054 hrs · 13,609 cycles

AFT CARGO STATION 1320 LBL 24 VERTICAL INTERCOSTAL CRACKED 3 INCHES LONG. REPAIRED PER SRM 53-60-51 AT SAT/SAA ON NR 133776 JOB NUMBER 82602350001.

Part: FRAME — DENTED (BS 1440 S26L) · airframe 39,054 hrs · 13,609 cycles

AFT CARGO FS 1440 S26L FRAME UPPER FLANGE DENTED. C/W AT SAA, SAT ON N/R 129450 JOB 82598480001.

Part: SEAT TRACK — CORRODED (BS 440-640) · airframe 39,054 hrs · 13,609 cycles

MAIN CABIN SEAT TRACK GOUGED AND CORRODED AT STA 440-640 RT RBL 45. C/W AT SAA, SAT ON N/R 126444 JOB 82600260001.

Part: SEAT TRACK — CORRODED (BS 440-640) · airframe 39,054 hrs · 13,609 cycles

MAIN CABIN SEAT TRACK GOUGED AND CORRODED AT STA 440-640 RT RBL 24/ AR SAA - SAT ON N/R 126443 JOB 82600280001.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 35,516 hrs · 12,929 cycles

COULD NOT GET CABIN TEMP BELOW 87 USING THE RIGHT PACK. STANDBY WAS NO USE. PERFORMED BITE RT PACK CONTROLLER FAULTS RT TEMP CONTROL VALVE NIS JFK FWD TO MCO PER MEL 21-51-04B.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 34,122 hrs · 12,500 cycles

LEFT ENGINE GEN DRIVE LIGHT ILLUM AFTER T/O DISCONNECTED AND RETURNED TO LAS. REMOVED AND REPLACED NR 1 ENGINE IDG ASSY SERVICED W/OIL AWAITING ENGINE RUN SAURIN 256438. PERF OPERATIONAL TEST/AND BITE TEST OPS LK CK OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY BULL NOSE LIGHT AT ROW 16 RIGHT SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY BULL NOSE LIGHT AT ROW 16 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT STRIP ON FLOOR BETWEEN SEATS 1AB AND 2AB INOPERATIVE. REPLACED LIGHT STRIP ON FLOOR BETWEEN SEATS 1AB AND 2AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IDG — INOPERATIVE (RIGHT)

RIGHT ENGINE DRIVE ILLUMINATED ON CLIMB-OUT. APU FLAMED OUT TWICE AFTER INFLIGHT START. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE INTEGRATED DRIVE GENERATOR AND P2 SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN — INOPERATIVE (CABIN)

STL INFLIGHT T1727/11NOV - FLIGHT ATTENDANTS AND PASSENGERS REPORTED STRONG AND DISTINCT ODOR OF BURNING ELECTRICAL OR INSULATION IN THE CABIN. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT)

DFW - EMEREGNCY EXIT FLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

LAS - SECTION OF EMERGENCY FLOOR TRACK LIGHTING AT SEAT 1B BROKEN. REPLACED FORWARD EMERGENCY FLOOR TRACK LIGHTING AT SEAT 1B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLADE — DAMAGED (COMPRESSOR)

EWR T785/15 EN ROUTE, ON CLIMBOUT AT 20,000 FT EXPERIENCED TWO COMPRESSOR STALLS FROM RT ENGINE. RT ENGINE LT AT IDLE AND LANDED EWR WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. ON BOROSCOPE OF 6TH STAGE COMPRESSOR BLADES FOUND 18 DAMAGED BLADES AND 1/4 OF 1 BLADE MISSING. NINTH STAGE 30 DAMAGED BLADES AND 1/4 OF 1 BLADE MISSING. FIFTEENTH STAGE ALL BLADES DAMAGED. RT ENGINE REPLACED PER WORKCARD M577101. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED--

Part: BATTERY PACK — DISCHARGED (CABIN)

SNA SEVERAL AFT GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR SEVERAL AFT GALLEY AREA EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN · airframe 18,739 hrs · 6,250 cycles

OILY SMOKE WAS REPORTED THROUGHOUT THE CABIN DURING TAKEOFF. THE LH AIR CONDITIONING PACK WAS SHUT OFF AND SMOKE DISSIPATED. THE LH PACK WAS PLACARDED INOPERATIVE PER MEL AND THE AIRCRAFT WAS OPERATED TO ANOTHER STATION WHERE THE LH RECIRCULATION FAN WAS REPLACED. CHECK-C 9-18-01 LAX. --CLOSED--

Part: SKIN — CRACKED (FUSELAGE) · airframe 17,327 hrs · 5,736 cycles

DURING CHECK-C MAINT THE WINDOW BELT LOWER LAP SEAM AT STA 1618, BELOW STRINGER 14R, HAD SKIN DAMAGE. THE LOWER INNER SKIN WAS CRACKED. REPAIRED PER ARA 17863, PAGE 1 THRU 6.

Part: FLAP — PUNCTURED (LT WING) · airframe 16,728 hrs · 5,530 cycles

DURING CHECK-C MAINT ON LT WING THE LOWER SURFACE OF THE INBD FOREFLAP, MIDDLE SECTION, HAD .25 INCH WIDE PUNCTURE AND 1 INCH LONG DENT, LOCATED JUST OTBD AND AFT OF THE INBD CANOE FAIRING. INSTALLED HOT BOND REPAIR AND PRIMED AND PAINTED PER SRM 51-70-10.

Part: DOUBLER — DELAMINATED (HORIZ STAB) · airframe 16,728 hrs · 5,530 cycles

DURING CHECK-C MAINT THE TOP SURFACE JUST AFT OF L/E AND 6 FT OTBD OF FUSELAGE, FOUND PATCH DELAMINATED WITH RAGGED EXPOSED EDGE. INSTALLED 4 .5 INCH DIAMETER METAL TO METAL HOT BOND REPAIR ON UPPER LEFT HORIZONTAL STABILIZER PANEL PER SRM 55-10-01, PAGE 1, AND 51-70-10 PAGE 52. PRIMER, SANDED, AND MATCHED PAINT.

Part: BAR — WORN (NR 1 PYLON) · airframe 16,728 hrs · 5,530 cycles

DURING CHECK-C MAINT ON THE NUMBER 1 INBD PYLON, THE EQUALIZER BAR HOLE IN THE PYLON FWD OF AFT REVERSER MOUNT, THE FWD EDGE OF THE HOLE WAS WORN. CLEANED AND SMOOTHED OUT AREA PER SRM 54-5-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 16,728 hrs · 5,530 cycles

DURING CHECK-C MAINT FOUND AT STA 1365 AND STRINGER 23L, 2 DAMAGE AREAS WITHIN 6 INCHES OF STATIC PORT. GOUGE AND DENT ABOVE PORT. SHOWS EDDY CURRENT CRACK. INSTALLED 1 INCH ROUND REPAIR, FLUSH TYPE, PER SRM 53-00-01, FIG 208 PAGE 225.

Part: SKIN — WORN (NR 1 PYLON) · airframe 16,728 hrs · 5,530 cycles

DURING CHECK-C MAINT ON THE NUMBER 1 PYLON, THE AFT REVERSER EQUALIZER BAR HAD WEAR SPOT AT CONTACT POINT WITH INBOARD SKIN. CLEANED UP AND SMOOTHED OUT AREA PER SRM 54-51-01.

Part: SIGN — MISSING (CABIN) · airframe 14,250 hrs · 4,798 cycles

THE EMERGENCY EXIT SIGN WAS MISSING FROM THE CEILING BY THE OVERWING EXITS. RE-INSTALLED LIGHT ASSEMBLY. CHECK-C 5-3-00 LAX.

Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 11,525 hrs · 3,922 cycles

AT THE GATE THE R4 DOOR EVACUATION SLIDE WAS INADVERTANTLY DEPLOYED BY AN OUTSIDE VENDOR. REPLACED SLIDE ASSEMBLY PER M57-25-09 AND M57-52-01. AC12 04-25-00 LAX.

Part: PANEL — GOUGED (HORIZONTAL STAB) · airframe 11,313 hrs · 3,852 cycles

DURING CHECK-C MAINT, THE LT HORIZ STAB L/E REMOVABLE PANEL 3320L, TOP SIDE HAD A 3.5 FOOT BY. 125 INCH WIDE BY.0625 INCH DEEP GOUGE. REMOVED GOUGE PER SRM 55-10-01, PAGE 103 DETAIL II AND BLENDED AND ALODINED.

Part: LIGHT — INOPERATIVE (SEAT 23, 24, 27) · airframe 11,140 hrs · 3,805 cycles

THE EMERGENCY LIGHTS OVER SEATS 23L, 24R, AND 27R WERE INOPERATIVE. REPLACED THE LAMP AT EACH LOCATION. CHECK-C 10-24-98 LAX.

Part: POWER SUPPLY — OVERHEATED (VIDEO PLAYER) · airframe 10,758 hrs · 3,688 cycles

VIDE O PLAYER INOP. RED FAIL LIGHT ON BOTTOM UNIT ILLUMINATED. SMELLS OF ELECTRICAL. REMOVED AND REPLACED VTR1 AND VTR2. AC09 12-01-99 LAX.

Part: LIGHT — INOPERATIVE (CABIN)

THE EMERGENCY LIGHT AT THE FORWARD LEFT CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-24-8 LAX.

Part: WIRE — BROKEN (ROW 5)

THE EGRESS LIGHTS WERE INOPERATIVE AT THE MID LAVATORY AND AT ROW 5. REPAIRED BROKEN WIRES AT THE MID LAV, AND REPLACED TWO LAMPS AT ROW 5. CHECK-C 10-24-98 LAX.

Part: ACM — FAILED (CABIN)

BWI - FLT 176 - DURING APPROACH, LT AIR CYCLE MACHINE MADE A BURNED SMELL IN THE CABIN. REPLACED THE LT AIR CYCLE MACHINE MFG PN 680640-4-3. OP-15. 5-14-97. NEW. (X)