N583NW

Part: LANYARD — UNSECURE (ZONE 800) · airframe 78,082 hrs · 25,709 cycles

L4 DOOR NOT ARMING. LANYARD HANGING OUT OF DOOR. RESTOWED LANYARD & BUSTLE AT 4L DOOR. DOOR ARMS NORMALLY. (6789006)

Part: BRACKET — CORRODED (ZONE 800) · airframe 78,060 hrs · 25,701 cycles

IN REF AMDS 5200-8346, STEP NR 9: CORROSION ON BRACKET INSIDE STORAGE COMPARTMENT AT RIGHT SLIDE PACK. PIN OF THE ACTUATOR ROD TO THE SLIDE PACK CARRIER WAS REMOVED AND INSTALLED PER AMM 25-65-05 AND BRACKET (FITTING) INSIDE STORAGE COMPARTMENT AT RIGHT SLIDE PACK WAS REPLACED PER SRM 51-40-02-0G. (1307494)

Part: GIRT BAR — DAMAGED (ZONE 800) · airframe 78,060 hrs · 25,701 cycles

DURING INSPECTION OF 4L DOOR GIRT BAR, MEASURE OF ENGAGEMENT ON AFT/FWD FLOOR FITTINGS IS LESS THAN 0.37 INCH. GIRT BAR 4L WAS REPAIRED PER PRI 630301-14 REV 1 AND ERA 630301-14AD REV ORIGINAL SECTION I. (1306015)

Part: GIRT BAR — DAMAGED (ZONE 800) · airframe 78,060 hrs · 25,701 cycles

GIRT BAR LEAF SPRING DOES NOT RETAIN THE SLIDER RIDES OVER THE FWD SPRING ON 4R PASSENGER DOOR. GIRT BAR 4R WAS REPAIRED PER PRI 630301-14 REV 1 AND ERA 630301-14AD REV ORIGINAL SECTION I.(1306022)

Part: GIRT BAR — DAMAGED (ZONE 800) · airframe 78,060 hrs · 25,701 cycles

SHIP 5803 AA. AD. INITIAL INSPECTION: AFT FLOOR FITTING DOES NOT GET THE MINIMUM ENGAGEMENT DIMENSION FOR THE GIRT BAR SLIDER AT L1 DOOR IN REF. AMDS 2561-01257-01A STEP 14 B. CORRECTIVE ACTION. GIRT BAR 1L, 4L & 4R WERE REPAIR PER PRI 630301-14 REV 1 AND ERA 630301-14AD REV ORIGINAL SECTION I. (1305706)

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,060 hrs · 25,701 cycles

SHIP 5803 IN REF NRC 00234: CORROSION OUT OF LIMITS ON SIDE PLATE LT SIDE BTW STA 1390 TO STA 1410 PER B757-300 SRM 53-00-53- 1A PROCEDURE.1 AD.1 FIGURE 101 (SHEET 4 OF 9) NOTE. C DETAIL. 9 38757 NDT MANUAL PART. 4 51-00-10 PROCEDURE 2. CORROSION LEVEL 2. SIDE PLATE LT SIDE BTW STA 1390 TO STA 1410 WAS REPAIRED PER B757-300 SRM 53-00-53-2R PROCEDURE 2 REPAIR 2. (1305699)

Part: FRAME — DENTED (ZONE 100) · airframe 78,060 hrs · 25,701 cycles

DENT IN FRAME STA 1520 BTW S-25L TO S-26L AT AFT CARGO COMPARTMENT. FRAME STA 1520 BTW S-25L TO S-26L AT AFT CARGO COMPARTMENT WAS REPAIRED PER PRI 630331-14 REV. 0 AND ER/A 630331-14AD REV ORIGINAL SECTION I. (1302961)

Part: FRAME — DENTED (ZONE 100) · airframe 78,060 hrs · 25,701 cycles

DTA MONITOR INSPECTION LOG REF ERA 630331-14 FUSELAGE FRAME BS 1520. UPPER FRAME FLANGE, S-25L - S-26L. DENTS. REF ERA 630331-14AD.

Part: RESERVOIR — OUT OF TOLERANCE (ZONE 800) · airframe 78,060 hrs · 25,701 cycles

IN REFERENCE TO AMDS 5211-3001-1L: POWER RESERVOIR OF 1L DOOR WAS FOUND WITH LOWER PRESSURE. RESERVOIR ASSY OF L1 DOOR WAS REMOVED AND SERVICEABLE RESERVOIR ASSY WAS INSTALLED PER B757-300 AMM 52-11-30. (1300018)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,060 hrs · 25,701 cycles

IN REF NRC 00273: CORROSION OUT OF LIMITS ON FLOOR SUPPORTS STA 1470 RBL 2.9. PER B757-300 SRM 53-00-53-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 FIGURA 101 NOTE C DETAIL IX AND B757 NDT MANUAL PART 4, 51-00-10 PROCEDURE 2. CORROSION LEVEL 2: FLOOR SUPPORTS STA 1470 RBL 2.9 WAS REPAIRED PER B757-300 SRM 53-00-53-2R PROCEDURE 1 REPAIR 1. (1301215)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,060 hrs · 25,701 cycles

CORROSION IN INTERCOSTAL BTW STA 1520 TO STA 1540 RBL2.9 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2: INTERCOSTAL BTW STA 1520 TO STA 1540 RBL2.9 AT AFT CARGO COMPARTMENT.WAS FABRICATED PER B757-300 DWG 146N8401 REV. B. AND REPLACED PER B757-300 SRM 51-40-02-0G. (1296544)

Part: STRAP — CRACKED (ZONE 200) · airframe 78,060 hrs · 25,701 cycles

CRACKED STABILIZATION STRAP IN STA 1380 RBL 48 AT AFT CARGO COMPARTMENT. STABILIZATION STRAP IN STA 1380 RBL 48 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-300 SRM 53-00-51-2R PROCEDURE 12 REPAIR 12. (1290744)

Part: STRAP — CRACKED (ZONE 100) · airframe 78,060 hrs · 25,701 cycles

CRACKED STABILIZATION STRAP BS 1660, RBL 48 IN THE AFT CARGO COMPARTMENT. STABILIZATION STRAP STA 1660 RBL 48 AT AFT CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-51-2R, PROCEDURE 12, REPAIR 12. (1287003)

Part: STRAP — CRACKED (ZONE 100) · airframe 78,060 hrs · 25,701 cycles

CRACK STABILIZER STRAPS (2 E/AS) ON BS 780+ 120 & 45 RBL/LBL AT CEILING STRUCTURE OF FWD CARGO COMPARTMENT. THE STABILIZER STRAPS (2 E/AS) ON BS 780+120 & 45 RBL/LBL AT CEILING STRUCTURE OF FWD CARGO COMPARTMENT WERE REPAIRED IAW SRM 53-00-51-2R, PROCEDURE 12, REPAIR 12. (1287029)

Part: STRAP — CRACKED (ZONE 100) · airframe 78,060 hrs · 25,701 cycles

CRACKED STABILIZATION STRAP STA 1660 RBL 24 AT AFT CARGO COMPARTMENT. THE STABILIZATION STRAP BS 1660 RBL 24 AT AFT CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-51-2R, PROCEDURE 12, REPAIR 12. (1287152)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,060 hrs · 25,701 cycles

CORROSION ON INBOARD SEAT TRACK RH SIDE STA 365 TO 418 AT PAX CABIN IS OUT LIMITS IAW SRM 53-00-52-1A PROCEDURE 1, ALLOWABLE DAMAGE 1, FIG 101, DETAIL 1. CORROSION LEVEL 2. INBOARD SEAT TRACK RT SIDE BS 365 TO 418 AT PAX CABIN WAS REPLACED IAW SRM 51-40-02-0G, PAR 7. (1286766)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,060 hrs · 25,701 cycles

CORROSION ON OTBD SEAT TRACK RT SIDE BS 365 TO 418 AT PAX CABIN IS OUT LIMITS IAW SRM 53-00-52-1A, PROCEDURE 1, ALLOWABLE DAMAAGE 1, FIG 101, DETAIL 1. CORROSION LEVEL 2 OTBD SEAT TRACK RT SIDE BTW BS 365 TO 418 WAS REPLACED IAW SRM 51-40-02- 0G, PARA 7, AND 9. (1286376)

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,060 hrs · 25,701 cycles

CORROSION ON ANGLE STA 1020 TO 1040 RBL 65 AT WINGBOX. SUMMARY OF NRC 00511. CORROSION LEVEL 2. ANGLE STA 1020 TO 1040 RBL 65 AT WINGBOX WAS REPLACED PER B757-300 SRM 53-00-13-2R PROCEDURE 2 REPAIR 2. (1282343)

Part: PUMP — FAILED (HYD SYSTEM) · airframe 77,735 hrs · 25,607 cycles

DE/MISC- DUE TO LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP. (LP 7189964)

Part: COVER — DETACHED (ZONE 200) · airframe 77,682 hrs · 25,591 cycles

FOUND OVERWING EXIT LIGHT COVER FELL OFF. SECURED EXIT LIGHT COVER AS REQUIRED. (1191128)

Part: ROLLER — MISINSTALLED (ZONE 800) · airframe 76,808 hrs · 25,287 cycles

SHIP 5803 R CTR ENTRY DOOR EICAS MESSAGE ON LANDING. CORRECTIVE ACTION: FOUND 2R DOOR PROX SWITCH ROLLER ON DOOR SIDE INCORRECTLY SHIMMED AND BARELY MAKING CONTACT WITH PROX SENSOR PADDLE SWITCH. ADJUSTED ROLLER PER B757 AMM 52-71. ALL OPS GOOD. (7516166)

Part: JAM-NUT — LOOSE (ZONE 800) · airframe 76,808 hrs · 25,287 cycles

SHIP 5803 R CTR ENT DOOR ADVISORY MESSAGE ON TOUCHDOWN. CORRECTIVE ACTION: FOUND JAM NUT LOOSE UNDERNEATH SWITCH SENSOR AT UPPER LATCH FITTING. TIGHTENED JAM NUT REF B757 AMM 52-11. CYCLED 2R DOOR NUMEROUS TIMES. MESSAGE EXTINGUISHED WHEN DOOR CLOSED. (7516160)

Part: TARGET — LOOSE (ZONE 800) · airframe 76,718 hrs · 25,242 cycles

SHIP 5803 R CTR ENTRY DOOR EICAS MESSAGE DISPLAYED AFTER LANDING. CORRECTIVE ACTION: REMOVED PLUNGER COVER AT 2R DOOR. FOUND TARGET LOOSE ON THREADED PLUNGER ROD. JAM NUT WAS BACKED OFF. TIGHTENED JAM NUT ONTO TARGET. OPERATED DOOR SEVERAL TIMES, OPS NORMAL. CHECKED CLEARANCES REF. B757 AMM 52-71. REINSTALLED COVER. 2R DOOR OK. (7516122)

Part: CAM — DIRTY (DOOR LATCH) · airframe 76,710 hrs · 25,239 cycles

SHIP 5803 ON TAXI IN RT CTR ENTRY DOOR EICAS MSG DISPLAYED WITH ENTRY DOOR LIGHT ON O/H PANEL. CORRECTIVE ACTION: CLEANED AND INSPECTED DOOR 2R DOOR LATCH CAM, PLUNGER AND CONFIRMED THE SENSOR IS CORRECTLY ADJUSTED PER B757 AMM 52-71

Part: LIGHT — DAMAGED (ZONE 200) · airframe 76,121 hrs · 25,013 cycles

SHIP 5803 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:404 FWD RT SEAT MOUNTED OVERWING EXIT PATH LIGHT, SEAT 27/28D. (0817613)

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 76,121 hrs · 25,013 cycles

SHIP 5803 ON LNDG, "R CTR ENT DOOR" EICAS MESSAGE. CORRECTIVE ACTION: R/R R2 DOOR WARNING PROXIMITY SENSOR PER B 757 AMM 52-71. LOOSE SPLICE FOUND ON PREVIOUS INSTALL. DOOR WARNING CKS OK. (6678511)

Part: GIRT BAR — CONTAMINATED (ZONE 800) · airframe 75,878 hrs · 24,915 cycles

SHIP 5803 R CTR ENT DOOR EICAS MSG ON LANDING ROLLOUT. CORRECTIVE ACTION: CLEAN EXCESS GREASE FROM GIRT BAR FITTING CLEAN DEBRI FROM DOOR OPS CHECK NML IAW B757 AMM 52 -71. (5382990)

Part: SLIDER — DETACHED (ZONE 800) · airframe 75,393 hrs · 24,723 cycles

SHIP 5803 L-2 DOOR GIRT BAR AFT SLIDER FELL OFF. CORRECTIVE ACTION: REINSTALLED SLIDER.GIRT BAR ARM/DISARM OPS NML. (6748748)

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 75,303 hrs · 24,684 cycles

SHIP 5803 EMERGENCY LIGHTS OUT AT ROWS 36-40. CORRECTIVE ACTION: FOUND BATTERY PACK M11081 DISCHARGED. RMVD AND RPLCD BATTERY PACK WITH REF TO B757 AMM 33-51. OPS CHK GOOD. (6748717)

Part: LANYARD — OUT OF POSITION (GIRT BAR) · airframe 75,246 hrs · 24,661 cycles

SHIP 5803 L4 DOOR SURVIVAL LANYARD BLOCKED GIRT BAR FROM ARMING. CORRECTIVE ACTION: SECURED SURVIVAL LANYARD DOOR NOW ARMS NML IAW B757 AMM 25-64. (6731186)

Part: GIRT BAR — FOD (ZONE 800) · airframe 75,246 hrs · 24,661 cycles

SHIP 5803 4L DOOR WILL NOT ARM. CORRECTIVE ACTION: OPEN AND CLOSED 4L DOOR REF B757 AMM 52-11. FOUND DEBRIS IN GIRT BAR FITTING. REMOVED TRASH, DOOR ARMS. (6731180)

Part: EMER LIGHT SYS — INOPERATIVE (ROW 27-31) · airframe 74,491 hrs · 24,406 cycles

SHIP 5803 DURING SERVICE CHECK FOUND ROW 27-31 EMERGENCY LIGHTS OFF. CORRECTIVE ACTION: REMOVED AND REPLACED M11488 BATT CHARGER NOT WORKING R/R AS PER B757 AMM 33-50 OPS CHECK GOOD. (6062080)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 74,474 hrs · 24,402 cycles

SHIP 5803 EMERGENCY LIGHTS ROW 27-31 INOP. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PACK M11488 AS PER B757 AMM 33-50 OPS CHECK GOOD. (6062074)

Part: LIGHT SYS — INOPERATIVE (SEAT 27-32) · airframe 74,474 hrs · 24,402 cycles

SHIP 5803 EMERGENCY LIGHTS AT SEAT 27-32 INOP. CORRECTIVE ACTION: REPLACED BATTERY PACK PER B757 AMM 33-51. OPS CHECK GOOD, OK FOR SERVICE. (6062064)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 74,474 hrs · 24,402 cycles

SHIP 5803 EMERGENCY LIGHTS AT DOOR 2L + 2R INOP. CORRECTIVE ACTION: R + R BATTERY AND POWER PACK PER B717 AMM 33-51. OPS CK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,369 hrs · 24,367 cycles

SHIP 5803 EMERGENCY LIGHTS INOP AT 27DEF. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT BATTERY AT 27DEF OP CHECKS GOOD B757 AMM 33-51. (6062020)

Part: UNKNOWN — UNKNOWN (L2 DOOR) · airframe 74,086 hrs · 24,277 cycles

SHIP 5803 2L DOOR NOT ARMING. CORRECTIVE ACTION: OPS CK 2L PASS DOOR PER B757 AMM 25-63. CK GOOD. (5990152)

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT CNTER DOOR) · airframe 73,739 hrs · 24,163 cycles

SHIP 5803 ON LANDING WE GOT R CENTER ENT DOOR CAUTION MSG ON EICAS & " ENTRY DOORS" ANNUNCITION ON OVERHEAD PANEL. CORRECTIVE ACTION: ADJUST PROX SENSOR PER B757 AMM 52-00 OPS CHECK NORMAL. (5270004)

Part: LATCH — FAULTED (CENTER DOOR) · airframe 73,739 hrs · 24,163 cycles

SHIP 5803 REPEAT RT CTR ENT DOOR EICAS MSG. CORRECTIVE ACTION: R/R UPPER RT LATCH FITTING IAW B757 AMM 52-11-37. PERFORMED PRESSURIZATION CHECK OF 3PSI IAW B757 AMM 05-51-24. ALL OPS CK & LEAK CHECK GOOD. (0329485)

Part: SENSOR — OUT OF ADJUST (RT DOOR) · airframe 73,728 hrs · 24,159 cycles

SHIP 5803 ON SHORT FINAL EICAS MSG R CTR ENT DOOR REMAINED ON AFTER LANDING. CORRECTIVE ACTION: ADJUSTED SENSOR PER 52-71-00 MSG CLEARED OPERATED DOOR SEVERAL TIMES, DID A SHAKE TEST AS WELL NO RETURN OF MESS. (4868774)

Part: SWITCH — FAULTED (RT CENTER DOOR) · airframe 73,673 hrs · 24,130 cycles

SHIP 5803 ON LANDING R CTR ENT DOOR MESSAGE. CORRECTIVE ACTION: REMOVED AND REPLACED SWITCH S10091 WITH SERVICEABLE REF AMM 52-71-00 ADJUSTED AND OPS CHECKED GOOD. (4868734)

Part: DOOR — WARNING MESSAGE (CABIN) · airframe 73,573 hrs · 24,092 cycles

ON LANDING R CENT ENT DOOR EICAS. DOOR VERIFIED CLOSED. CORRECTIVE ACTION: T/S PER B757 FIM 52-71, ADJUSTED PROX TARGET & ADJUSTMENT ROD PER B757 AMM 52-71. OPS CHECK GOOD. DOOR INDICATION WORKS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (DOOR) · airframe 73,540 hrs · 24,080 cycles

RIGHT CTR ENTRY DOOR ADVISORY MSG ON LANDING ROLL OUT. FA REPORTS NOTHING UNUSUAL. TROUBLESHOT IAW FIM 52-71-00-815-804. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (DOOR) · airframe 73,484 hrs · 24,059 cycles

SHIP 5803 R CTR ENT DOOR EICAS MSG. CORRECTIVE ACTION: NO MSG ON ARRIVAL TO FLT DECK.. INSPECTED RIGHT CTR ENT DOOR AND SENSOR/ ALL OK. CYCLED DOOR / INDICATION NORMAL B757 AMM 52-71 RIGHT CENTER ENTRY DOOR OPS NORMAL. (5477918)

Part: SKIN — CORRODED (BS 1787-1864) · airframe 73,484 hrs · 24,059 cycles

SHIP 5803 SECONDARY NRC IN REF NRC #00137: CORROSION ON INTERNAL SKIN BTW STA 1787.45 AND 1864 AND STGRS 25L TO 27L AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00193: CORROSION INTERNAL SKIN BTW STA 1787.45- 1825 AND STA. 1850-1864 AND STGRS 25L-27L AT AFT ACCESORY COMPARTMENT WAS REMOVED PER B757-300 SRM. MEASUREMENT THICKNESS WAS ACCOMPLISHED ON INTERNAL SKIN BTW STA 1787.45-1825 AND STA. 1850-1864 AND STGRS 25L-27L AT AFT ACCESORY COMPARTMENT. ORIGINAL THICKNESS AREA IS WITHIN LIMITS PER B757-300 SRM, AND INTERNAL SKIN BTW STA 1825-1850 AND STGRS 25L-27L AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER ER/A 617034-14 REV. ORIGINAL SECTION I PERMANENT REPAIR AND PRI 617034-14 REV. 2.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 73,476 hrs · 24,057 cycles

SHIP 5803 DTE, 616927-14; STABILIZER / RH HORIZONTAL / LWR SKIN / BETWEEN STAB STA. 342 TO 364 AND FRONT TO REAR SPAR / DENTS. CORRECTIVE ACTION: REF ERA 616927-14. (0279139)

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 73,476 hrs · 24,057 cycles

SHIP 5803 SECONDARY NRC: IN REF. NRC # 00079 DENT (01 EA) ON LOWER SKY BTW RIB 14 /15 AT RH HORIZONTAL STABILIZER WAS FOUND OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00196: DENT (01 EA) ON LOWER SKY BTW RIB 14 /15 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER ER/A 616927-14 REV. ORIGINAL SECTION I PERMANENT REPAIR AND PRI 616927-14. REV. 2. (0279296)

Part: SLIDE — DISLODGED (LT OVERWING) · airframe 73,473 hrs · 24,056 cycles

SHIP 5803 DISJOINTED OVERWING EMERGENCY SLIDE PACK AT LH WING. CORRECTIVE ACTION: SUMMARY OFF NRC: 00117 LEFT OVER-WING ESCAPE SLIDE PACK WAS REPLACED BY SERVICEABLE OVER-WING ESCAPE SLIDE PACK PER AMDS. (0266828)

Part: LEAF SPRING — FAILED (L4 GIRT BAR) · airframe 73,473 hrs · 24,056 cycles

SHIP 5803 FWD LEAF SPRINGS DOES NOT RETAIN THE SLIDER ON GIRT BAR OF L4 DOOR SLIDE. CORRECTIVE ACTION: SUMMARY OF NRC 00035 UNSERVICEABLE GIRT BAR WAS REPLACED BY SERVICEABLE GIRT BAR AND LEAF SPRING ENGAGEMENT TEST WAS PERFORMED PER AMDS:2561-01257-01E. TEST OK. (0262048)

Part: GIRT BAR — OUT OF LIMITS (DOOR SLIDE) · airframe 73,473 hrs · 24,056 cycles

SHIP 5803 DURING CHECK MEASURE ON GIRT BAR TO VERIFY A MINIMUM ENGAGEMENT OF 0.37 INCH. DURING ATTEMPT TO INSERT GO/NO GO GAUGE, THE MEASURE IS OUT OF LIMIT AT 2L DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00034 UNSERVICEABLE GIRT BAR WAS REPLACED BY SERVICEABLE GIRT BAR AND MEASURE ENGAGEMENT TEST WAS PERFORMED PER AMDS:2561-01257-01C, TEST OK. (0262045)

Part: LEAF SPRING — FAILED (GIRT BAR) · airframe 73,473 hrs · 24,056 cycles

SHIP 5803 A.A. INITIAL INSPECTION: AFT LEAF SPRINGS DOES NOT RETAIN THE SLIDER ON GIRT BAR OF L1 DOOR SLIDE. CORRECTIVE ACTION: SUMMARY OF NRC 00033 UNSERVICEABLE GIRT BAR WAS REPLACED BY SERVICEABLE GIRT BAR AND LEAF SPRING ENGAGEMENT TEST WAS PERFORMED PER AMDS:2561-01257-01A, TEST OK. (0262092)

Part: CHANNEL — CRACKED (BS 366 BL 0) · airframe 73,473 hrs · 24,056 cycles

SHIP 5803 CRACK ON CHANNEL STA 366 AND BL 0 AT E/E COMPARTMENT. CHANNEL STA 366 AND BL 0 AT E/E COMPARTMENT WAS REPAIRED PER B757-300 SRM. (0258897)

Part: DOOR SILL — CORRODED (BS 1380-1440) · airframe 73,473 hrs · 24,056 cycles

SHIP 5803 FUSELAGE / OPENING FRAMES / #2 CARGO DOOR SURROUND STRUCTURE / LOWER SILL OUTBOARD CHORD / STA 1380 TO 1440 / CORROSION. CORRECTIVE ACTION: REF ERA 598161-14. (0251129)

Part: COVER — DAMAGED (L2 DOOR INDICATO) · airframe 73,438 hrs · 24,043 cycles

SHIP 5803 DUE TO ERA 560980-14TR REV. B ON LOG 5251118, DEFER ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT @2L. CORRECTIVE ACTION: COMPLETED SEC V, PERMANENT REPAIR OF 2L LIGHT/COVER PER ER/A 560980 14 REV B. (5251119)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,936 hrs · 23,867 cycles

SHIP 5803 AISLE EMERGENCY LIGHTS SEATS 24-26 INOP. CORRECTIVE ACTION: SPLICED WIRES IAW SWPM 20-30. OPS CK NO GOOD. FOUND POWER SUPPLY BAD. R&R POWER SUPPLY IAW B757 AMM 33-51. OPS CK GOOD. (573832)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,812 hrs · 23,818 cycles

SHIP 5803 R CTR ENTRY DOOR MESSAGE ON EICAS AFTER LANDING AND TAXI CLEAR OF RUNWAY, APPEARED TO BE CLOSED WHEN VIEWING FROM THE CABIN. CORRECTIVE ACTION: INSPECTED 2R DOOR AND OPERATED SEVERAL TIMES W/ CORRECT INDICATIONS PER B757 AMM 52-71. (4419192)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,804 hrs · 23,815 cycles

SHIP 5803 CIRCUIT BREAKER -EMER CHGR- POPPED ON GROUND AT GATE. CORRECTIVE ACTION: CYCLED BOTH LEFT AND RIGHT EMER BATTERY CHARGER C/B'S AND PERFORMED OPS CHECK PER B757 AMM 33-51. OPS CHECK NORMAL. (4419182)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,791 hrs · 23,811 cycles

SHIP 5803 R4 DOOR ARMED CONDITION INDICATOR NOT EXTENDED. CORRECTIVE ACTION: KNUCKLE KNOCKER AT DOOR 4R TRAPPED BY THE DOOR LINER. ADJUSTED DOOR LINER REF. B757 AMM 52-11. OPS NORMAL. (0120383)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,615 hrs · 23,742 cycles

SHIP 5803 R CTR ENT DOOR EICAS UPON LANDING. CORRECTIVE ACTION: T/S AS PER FIM TASK 52-71 FOUND DOOR 2R SENSOR OUT OF LIMITS. ADJUSTED DOOR SENSOR AS PER B757 AMM 52 -71. SENSOR WITHIN LIMITS AND OPS CHK GOOD. (4419110)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,464 hrs · 23,686 cycles

SHIP 5803 RED/WHITE SEAT MOUNT EMERGENCY LIGHTS INOP ROW 41-45. CORRECTIVE ACTION: T/S PER B757 FIM 33-51-00-815-802. REMOVED AND REPLACED (M737) RT EMERGENCY LIGHT POWER SUPPLY PER B757 AMM 33-51. OPS CK GOOD. (8945437)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,929 hrs · 23,518 cycles

SHIP 5803 EXIT ROW LIGHT ON SEAT 28D CAME OFF AND NEEDS TO BE REMOUNTED. CORRECTIVE ACTION: RE-INSTALLED 28D EXIT LGT. (4430212)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,912 hrs · 23,514 cycles

SHIP 5803 SEATS 1DC-3DC AND L1 DOOR EMERFENCY LIGHTS ON IN ARM POSITION. CORRECTIVE ACTION: T/S PER B757 FIM 33-51. REMOVED AND REPLACED CHARGER AND BATTERY PER B757 AMM 33-51. OPS CK GOOD. EMERGENCY LIGHTS TOGGLE SW WONT SW TO OFF. REMOVED AND REPLACED PER B757 33-51 OPS CKS GOOD. (4430206)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,791 hrs · 23,479 cycles

SHIP 5803 R CTR ENT DOOR EICAS INDICATION ON LANDING. CORRECTIVE ACTION: OPENED DOOR & CLEANED SENSOR, MSG CLEARED PER B757 AMM 52-11. OK FOR SVC. (8987034)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,216 hrs · 23,321 cycles

SHIP 5803 EICAS MESSAGE DISPLAYED "R CTR ENT DOOR". CORRECTIVE ACTION: READJUSTED DOOR PROX SENSOR TARGET PER B757 AMM 52-71. (4054684)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,106 hrs · 23,289 cycles

SHIP 5803 R CTR ENT DOOR ILLUM IN FLIGHT. PRESSURIZATION WAS GOOD. CORRECTIVE ACTION: REMOVED AND INSTALLED NO 2 PASSENGER DOOR WARNING SENSOR S10091 REF B757 AMM 52-71-00. TEST OK (4054634)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,051 hrs · 23,272 cycles

SHIP 5803 PATH LIGHT AT 17 D HANGING DOWN. CORRECTIVE ACTION: RESECURED ESCAPE PATH LIGHT PER B757 AMM 33-51. OPS TEST GOOD. (4054622)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,051 hrs · 23,272 cycles

SHIP 5803 R4 DOOR IS DISARMED BUT "ARMED" LIGHT STAYS ILLUMINATED. CORRECTIVE ACTION: R4 DOOR SLIDE PINNED. R/R GIRT BAR PER B757 AMM 25-66. PINNED REMOVED RII INSPECTIONS C/W. VARIFIED R-4 DOOR SLIDE PIN REMOVED PER B757 AMM 25-66. (4054616)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,051 hrs · 23,272 cycles

SHIP 5803 AFTER CHOCKING IN DURING DISARMING THE DOORS AFT 4R DOOR SLIDE LIGHT REMAINED ILLUMINATED. CORRECTIVE ACTION: FOUND DEBRIS AND ICE IN GRIT BAR FITTING AREA, LUBED AND INSURED FLOOR DRAIN ARE DRAINING. ARMED AND DISARMED SLIDE MECHANISM NO FURTHER ISSUES IAW B757 AMM 52-11. (4054618)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,001 hrs · 23,260 cycles

SHIP 5803 UPON LANDING, EICAS MESSAGE " R CTR ENT DOOR". CORRECTIVE ACTION: CLEANED SENOR ON "R CTR ENT DOOR" EICAS MSG CLEARD. (4054612)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,990 hrs · 23,257 cycles

SHIP 5803 UPON LANDING ECIAS MSG " R CTR ENT DOOR". CORRECTIVE ACTION: OPEN #2R DOOR AND REMOVE DEBRIS AND GREASE,, PER B757 AMM 52-11. OPS CHK GOOD. (4054604)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,582 hrs · 23,129 cycles

SHIP 5803 SEAT ROW 37-40 EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: T/S PER B757 WDM 33-51. FOUND DAMAGED WIRES AT SEAT ROW 40D-E-F. REPAIRED WIRES PER BOEING SWPM 20-10. OPS CHECKED GOOD. (9959622)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,320 hrs · 23,036 cycles

SHIP 5803 RT CENTER DOOR EICAS MESSAGE ON. CORRECTIVE ACTION: INSP OF DOOR 2R PROX SWITCH PLUNGER FOUND LOCKING JAM NUTS BACKED OFF AND OUT OF ADJUSTMENT. ADJUSTED PER B757 AMM 52-71. OPS CK GOOD. (9950618)

Part: UNKNOWN — UNKNOWN · airframe 70,166 hrs · 22,983 cycles

SHIP 5803 R CTR ENT DOOR EICAS MSG ON LANDING. CORRECTIVE ACTION: FOUND RT CTR ENT DOOR SENSOR (S10091) OUT OF ADJUSTMENT. ADJUSTED PER B757 AMM 52-71. SYSTEM TEST OK. (2663703)

Part: NONE — NONE · airframe 70,127 hrs · 22,967 cycles

SHIP 5803 ON FINAL @1000' AGL THE "R CTR ENT DOOR" SHOWED ON THE EICAS. CORRECTIVE ACTION: NO FAULTS AT THIS TIME, DOOR OPS NORMAL. (4114058)

Part: NONE — NONE · airframe 70,102 hrs · 22,959 cycles

SHIP 5803 R CTR ENT DOOR EICAS AFTER LANDING. CORRECTIVE ACTION: NO MSG ON ARRIVAL. OPENED DOOR 2R. R CTR ENT DOOR EICAS MESSAGE APPEARS. INSPECTED S10091 REF B757AMM 52-71-00. NO TROUBLE FOUND. (4114036)

Part: LATCH — WORN (L2 DOOR) · airframe 69,843 hrs · 22,846 cycles

SHIP 5803 DURING SERVICE CHECK FOUND L2 DOOR UPPER FWD LATCH FITTING HAS WEAR DAMAGE. CORRECTIVE ACTION: BLENDED DAMAGE. ACCOMPLISHED HEFEC IAW B757 NJM PART 651-10-01- NO CRACKS. DAMAGE BEYOND ENGINEERING LIMITS. R&R LATCH PER B757 AMM 52-11. (9630982)

Part: PLATE — MISSING (R2 DOOR) · airframe 69,843 hrs · 22,846 cycles

SHIP 5803 DURING SERVICE CHECK FOUND R2 DOOR LOWER AFT STOP BEARING PLATE MISSING. CORRECTIVE ACTION: REPLACED MISSING STOP FITTING BEARING PLATE PER B757 AMM 52-11. (9630983)

Part: TRANSDUCER — FAULTED (ANTI-SKID) · airframe 69,731 hrs · 22,804 cycles

CREW DECLARED EMERGENCY DURING APPROACH DUE TO NML AND ALTN ANTISKID EICAS MESSAGES AND ASSOCIATED ANTISKID DISCREET LIGHT ILLUMINATED. R & R NR 4 & 8 TRANSDUCER WIRING FROM TRANSDUCERS TO LG JUNCTION BOX. R & R NR 8 TRANSDUCER AND ANTISKID - AUTO BRAKE CONTROL UNIT. R & R RELAYS K10323 AND K10233.

Part: WARNING MESSAGE — FALSE ACTIVATION (DOOR) · airframe 69,710 hrs · 22,796 cycles

SHIP 5803 R CTR ENT DOOR EICAS IN FLT WITH GEAR DOWN FLAPS 20. CORRECTIVE ACTION: CYCLED DOOR. OPS CK GOOD INDICATION IS CLEARED PER B757 AMM 52- 11. (9630928)

Part: DOOR — FOD (R1) · airframe 69,579 hrs · 22,743 cycles

R1 DOOR WILL NOT ARM. REMOVED DEBRIS. DOOR ARMS/DISARMS NORMAL.

Part: INDICATOR — OUT OF ADJUST · airframe 69,299 hrs · 22,622 cycles

SHIP 5803 HISTORY OF 4R DOOR KNUCKLE KNOCKER NOT EXTENDING. CORRECTIVE ACTION: ADJUSTED LOWER DOOR LINING PER B757 AMM 52-11-02-904-007. DOOR KNUCKLE BUSTER NOW OPS NORMAL. (2505553)

Part: INDICATOR — OUT OF ADJUST · airframe 69,299 hrs · 22,622 cycles

SHIP 5803 DOOR 4R KNUCKLE KNOCKER WILL NOT EXTEND WHEN IN ARMED POSITION. CORRECTIVE ACTION: ADJ/TEST 4R DOOR MECHANISM PER B757 AMM 52-11. (9438826)

Part: INDICATOR — INOPERATIVE (R4 DOOR) · airframe 69,292 hrs · 22,619 cycles

SHIP 5803 DOOR 4R KNUCKLE KNOCKER WILL NOT EXTEND WHEN IN ARMED POSITION. CORRECTIVE ACTION: RECYCLED ARM/DISARM LEVER. OPS CKS GOOD AT THIS TIME. OK FOR SVC. REF B757 AMM 52-11. (9438824)

Part: PLATE — MISSING (L4 DOOR BEARING) · airframe 69,067 hrs · 22,550 cycles

L4 DOOR MISSING AFT MIDDLE BEARING PLATE. INSTALLED BEARING PLATE REF B757 AMM 52-11. (9358130)

Part: LENS — MISSING · airframe 68,016 hrs · 22,218 cycles

SHIP 5803 EMERGENCY LIGHT ABOVE DOOR 4R MISSING LENS. CORRECTIVE ACTION: REPLACED LENS COVER. (8512164)

Part: NONE — NONE · airframe 67,847 hrs · 22,160 cycles

SHIP 5803 EMERGENCY EXIT SIGN COVER LOOSE. CORRECTIVE ACTION: RESECURE EXIT SIGN AT 2L AS REQUIRED. (2241125)

Part: SWITCH — DIRTY · airframe 67,650 hrs · 22,085 cycles

SHIP 5803 R CTR ENT DOOR EICAS MSG. AIRCRAFT MAINTAINED NORMAL. CORRECTIVE ACTION: CLEANED DOOR INDICATION SWITCH OPS CHECKED AND INDICATION GOOD PER B757 AMM. 52-11. (8808452)

Part: NONE — NONE · airframe 67,626 hrs · 22,076 cycles

SHIP 5803 -HYD- INBOUND TO MSP LOSS LEFT HYD PRESSURE AND QTY AND ALTERNATE GEAR EXTENSION REQUIRED. CORRECTIVE ACTION: FOUND HYD FLEX LINE LEAKING ON TOP OF RIGHT GEAR. REPLACED LINE, ACMP, LEFT ENG EDP, LT SYSTEM ACMP PRESSURE FILTERS, RETURN FILTER AND PTU. REPLACED CASE DRAIN LINE DUE TO FOUND CRACK ON B NUT. PERFORMED LEAK CHECK, NO LEAKS NOTED.

Part: COVER — MISSING · airframe 67,602 hrs · 22,068 cycles

SHIP 5803 MID CABIN OVHD EMERGENCY LIGHT MISSING COVER. CORRECTIVE ACTION: REINSTALLED EMGY LIGHT COVER. (8808415)

Part: SKIN — CORRODED · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 CORROSION ON FUSELAGE SKIN BELLOW TOP ATC ANNTENA BTW STA 520 TO STA 540 IN REF NRC 00049. CORRECTIVE ACTION:SUMMARY OF NRC 00225; CORROSION ON FUSELAGE SKIN BELLOW TOP ATC ANNTENA BTW STA 520 TO STA 540 WAS REPAIRED PER PRI 598292-14 REV 0 AND ER/A NO.598292-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2174412)

Part: FASTENER — LOOSE · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 LOOSE FASTENERS NBR 3 AND 8 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT LH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00136:FASTENERS #3 AND #8 WERE REPLACED PER AMDS 5720-01100-04A AND ERA 586129-14AD REV A. SECTION II. (2174109)

Part: PIN — OUT OF POSITION · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 DAMAGE T: OUT OF PLACE SAFETY PIN ON LH OVERWING EMERGENCY SLIDE. CORRECTIVE ACTION: SUMMARY OF NRC 00104:OVERWING EMERGENCY SLIDE LH WAS REPLACED PER B757-300 AMM 25-65-01 AND UNDER AMDS. (2174118)

Part: FASTENER — LOOSE · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 AWR, AD, A.A.: LOOSE FASTENERS NBR 14 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT LH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00137:FASTENER #14 WAS REPLACED PER AMDS 5720- 01100-05A AND ERA 586129-14AD REV A. (2174125)

Part: DRAG FITTING — DAMAGED · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 LOOSE FASTENERS NBR 12 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00071:FASTENER NBR 12 AT RH WING UPPER SKIN DRAG FITTING WAS REPLACED PER AMDS 5720-01100-05B AND ERA 586153-14AD REV B.SECTION V. (2172771)

Part: FASTENER — LOOSE · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 LOOSE FASTENERS NBR 2,3,4,7 AND 8 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00070:FASTENERS NBR 2,3,4,7 AND 8 AT RH WING UPPER SKIN DRAG FITTING WERE REPLACED PER AMDS 5720-01100-04B AND ERA 586153-14AD REV B.SECTION V. (2172797)

Part: FITTING — CORRODED · corrosion level 2 · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 CORROSION FITTINGS (4 EAS) ON GIRT BAR 4L, 4R, 1R AND 1L. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00170: CORROSION LEVEL 2, FITTINGS (4 EAS) ON GIRT BAR 4L, 4R, 1R AND 1L. WERE REPLACED PER B-757-300 AMM 25- 66-10. (2170948)

Part: SKIN — NONE (RT WING) · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 586153-14 REV B. CORRECTIVE ACTION: REF ERA586153-14 REV B. (2170983)

Part: SKIN — NONE (LT WING) · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 586129-14 REV A. CORRECTIVE ACTION: REF ERA 586129-14 REV A. (2170938)

Part: DOOR SILL — CORRODED · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 CORRODED OUTER CHORD ON AFT CARGO DOOR LWR SILL. CORRECTIVE ACTION: SUMMARY OF NRC 00103. OUTER CHORD ON AFT CARGO DOOR LWR SILL WAS REPAIRED PER PRI 598161-14 REV 0 AND ER/A 59861-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (2171802)

Part: GIRT BAR — MALFUNCTIONED (R1 DOOR) · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 AA. DURING INSPECTION OF THE GIRT BAR AT DOOR 1R, MEASURE OF ENGAGEMENT IS LESS THAN 0.37 INCH AT FWD FLOOR FITTINGS IN REFERENCE AMDS AD. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00106:GIRT BAR WAS REPLACED PER B757-300 AMM 25-66-10 AND AMDS. (2169922)

Part: GIRT BAR — MALFUNCTIONED (L4 DOOR) · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 AA. DURING INSPECTION OF THE GIRT BAR AT DOOR 4L , MEASURE OF ENGAGEMENT IS LESS THAN 0.37 INCH AT FWD FLOOR FITTINGS IN REFERENCE AMDS AD. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00105: GIRT BAR WAS REPLACED PER B757-300 AMM 25-66-10 AND AMDS. (2169803)

Part: DOOR FRAME — CORRODED · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 DTE, ER/A598161-14 FUSELAGE / OPENING FRAMES / #2 CARGO DOOR SURROUND STRUCTURE / LOWER SILL OUTBOARD CHORD / STA 1380 TO 1440 / CORROSION. CORRECTIVE ACTION: REF ERA 598161-14. (2170565)

Part: SKIN — DENTED (BS 620-640) · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 INITIAL INSPECTION: DENT ON FUS SKIN BTW STA 620 TO STA 640 AND BTW S-27R TO S-28R. CORRECTIVE ACTION: SUMMARY OF NRC 00045. DENT ON FUS SKIN BTW STA 620 TO STA 640 AND BTW S-27R TO S-28R WAS MEASURED AND EVALUATED PER PRI 598100 REV 0 AND ER/A 598100-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (2169422)

Part: UNKNOWN — UNKNOWN · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 DTE, ER/A598100-14 FUSELAGE / SKIN STA 620-640, S-27R TO S-28R / DENT TIME LIMITED. CORRECTIVE ACTON: REF ERA 598100-14. (2167791)

Part: NOT REPORTED — NOT REPORTED · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 INITIAL INSPECTION: CRACK ON STABILIZATION STRAP BTW FRAME STA 365.25 AND STA 377.7 LBL 23 AREA ABOVE OF NLG W/W (FYT). CORRECTIVE ACTION: SUMMARY OF NRC 00195; CRACK ON STABILIZATION STRAP BTW FRAME STA 365.25 AND STA 377.7 LBL 23 AREA ABOVE OF NLG W/W WAS REPAIRED PER B757-300 SRM. (2164294)

Part: NONE — NONE · airframe 67,319 hrs · 21,970 cycles

SHIP 5803 AFTER DISARMING 2L DOOR SLIDE LIGHT REMAINED ILLUMINATED. CORRECTIVE ACTION: RESET GIRT BAR ARM SWITCHES. CYCLED ARM LEVER. OPS CKS NORMAL. (8870676)

Part: NONE — NONE · airframe 66,950 hrs · 21,842 cycles

SHIP 5803 R1 DOOR EMER SLIDE LOW PSI. CORRECTIVE ACTION: REMOVED R1 BUSTLE. ACCOMPLISH R1 DOOR SLIDE CHANGE PER WORKCARD. (7892794)

Part: NONE — NONE · airframe 66,962 hrs · 21,846 cycles

SHIP 5803 ROW 41 SEAT RED EMER LIGHT INOP. CORRECTIVE ACTION: REMOVED & REPLACED SEAT MOUNTED ASSY. OPS CHECK GOOD. (7892792)

Part: NONE — NONE · airframe 66,182 hrs · 21,610 cycles

SHIP 5803 ON POWER UP AND ENGAGING WINDOW HEAT SAW TWO SPARKS FROM THE R FWD WINDOW CONNECTOR. CORRECTIVE ACTION: FOUND WINDOW HEAT PLUG D3274 LOOSE AND BURNT REPLACED WINDOW HEAT PLUG B7578 AMM 30-41. TEST WINDOW HEAT B757 AMM 30-41 CKS GOOD. (8189388)

Part: NOT REPORTED — NOT REPORTED · airframe 66,149 hrs · 21,602 cycles

SHIP 5803 EMERGENCY EXIT SIGN COVER LOOSE. CORRECTIVE ACTION: SECURED EMERGENCY EXIT SIGN. (1990556)

Part: NOT REPORTED — NOT REPORTED · airframe 66,149 hrs · 21,602 cycles

SHIP 5803 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:605. CORRECTIVE ACTION: SECURED EMERGENCY EXIT SIGN. (1990557)

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,454 hrs · 21,420 cycles

SHIP 5803 EMERGENCY EXIT SIGN COVER LOOSE. CORRECTIVE ACTION: SECURED LOC 605 EMERGENCY EXIT SIGN COVER. (1907537)

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,373 hrs · 21,397 cycles

SHIP 5803 EMERGENCY EXIT SIGN COVER LOOSE. CORRECTIVE ACTION: REINSTALLED AND SECURED EXIT SIGN COVER OPS CHECKED GOOD. (1900285)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,306 hrs · 21,379 cycles

SHIP 5803 DOOR 2R EXIT SIGN COVER MISSING. CORRECTIVE ACTION: INSTALLED CURRENT LENS PER ER-A 593217-14 SECTION III PERMANENT REPAIR. (7983022)

Part: INDICATOR — INOPERATIVE (R4 DOOR SLIDE) · airframe 64,856 hrs · 21,248 cycles

SHIP 5803 4R DOOR KNUCKLE KNOCKER DID NOT EXTEND. CORRECTIVE ACTION: ADJUSTED TRIM PANEL AROUND KNUCKLE KNOCKER - DOOR OPERATES NORMAL. (7573612)

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 64,507 hrs · 21,134 cycles

SHIP 5803 L1 DOOR ASSIT BOTTLE PRESSURE LOW. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 006-0001:2020-2367-1L/001 00005 REPLACED DOOR ASSIST BOTTLE PER B757 AMM 52-11. (1806625)

Part: SKIN — DELAMINATED (NR 3 SLAT LE) · airframe 64,245 hrs · 21,015 cycles

SHIP 5803 FIXED LE DELAMANATED AT #3 SLAT. CORRECTIVE ACTION: REMOVED PANEL AND ACCOMPLISHED PERMANENT REPAIR PER ER/A 590906-14 REV. ORIGINAL, INSTALLED PANEL. (1771486)

Part: NONE — NONE · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 ERA 590906-14 SECTION I ISSUED FOR LH WING FIXED LEADING SKIN REPAIR AT OSS 440 TO OSS 452. SECTION I ACCOMPLISHED DURING PAINT VISIT AT CWF ON N.R. 001. CORRECTIVE ACTION: GVI AND TAP TEST WERE PERFORMED PER ERA 590906-14 REV.ORIG. SECT.II AND DISBONDS WERE FOUND. AREA WAS REPAIRED PER ERA 590906-14 REV.A SEC.III (PERMANENT REPAIR). (1770434)

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 63,959 hrs · 20,875 cycles

SHIP 5803 CENTER ISLE EMERGENCY EXIT SIGN ADJACENT TO L3 DOOR FOUND MISSING. CORRECTIVE ACTION: REPLACED EXIT COVER. SYSTEM OPERATION IS NORMAL. (LP7661609)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 63,722 hrs · 20,717 cycles

R3 EMERGENCY EXIT LIGHTS ARE INOPERATIVE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE BATTERY AND CHARGER. SYSTEM OPERATION IS NORMAL.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 62,734 hrs · 20,344 cycles

L1 DOOR SLIDE PARTIALLY DEPLOYED. CORRECTIVE ACTION: FOUND L1 DOOR SLIDE ASSIST BOTTLE BLOWN. REPLACED L1 SLIDE. SYSTEM OPERATION IS NORMAL.

Part: SUPPORT — CORRODED (FAIRING) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON LH/RH BODY FAIRING FRAME SUPPORT LOWER AREA AT STA 860 (FUS). CORRECTIVE ACTION: SUMMARY OF NRC S/N 00682, LH/RH BODY FAIRING FRAME SUPPORT LOWER AREA AT STA 860 (FUS), WERE REPAIRED PER ER/A 586288-14 REV ORIG SECTION 1, PERMANENT REPAIR AND ETI. (1543517)

Part: GIRT BAR — UNSERVICEABLE (R4 DOOR) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 R4 DOOR DOES NOT RETAIN THE SLIDER. CORRECTIVE ACTION: SUMMARY OF NRC 0004:R4 DOOR GIRT BAR WAS REMOVED AND SERVICIABLE GIRT BAR WAS INSTALLED. (1542909)

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 ELECTRICAL ARC ON RH WINDSHIELD (UPPER AREA ) AT COCKPIT. CORRECTIVE ACTION: NRC S/N: 00070 RH WINDSHIELD AT COCKPIT WAS REPLACED PER B 757-300 AMM 56-11 AND OPERATIONAL TEST WAS PERFORMED. TEST OK. (1542472)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON FLOOR SUPPORTS PREVIOUSLY REPAIRED, STA. 654. LBL/RBL 16, LBL/RBL11, RBL 7, AND LBL/RBL 3, AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00250, CORROSION LEVEL 2. PREVIOUS REPAIRS OF FLOOR SUPPORTS FROM STA. 654. LBL/RBL 16, LBL/RBL11, RBL 7, AND LBL/RBL 3, AT FWD CARGO COMPARTMENT WERE REPLACED PER. B757-300 SRM AND ER/A 586291-14 REV. ORIGINAL SECTION I. (1540385)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON FLOOR SUPPORTS STA. 780+65 FROM LBL/RBL 16, LBL/RBL11, LBL/RBL 7, AND LBL/RBL 3, AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY: OF NRC00243 CORROSION LEVEL 2; FLOOR SUPPORTS STA. 780+65 FROM LBL/RBL 16, LBL/RBL11, LBL/RBL 7, AND LBL/RBL 3, AT FWD CARGO COMPARTMENT. (C1) WERE REPAIRED PER B757-300 SRM. (1539643)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON FLOOR SUPPORT STA. 654. LBL 7 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION:SUMMARY OF NRC S/N 00377, CORROSION LEVEL 2, FLOOR SUPPORT STA. 654. LBL 7 AT FWD CARGO COMPARTMENT. (C1) WAS REPAIRED PER. B757-300 SRM, REPAIR.1. (1540226)

Part: FASTENER — LOOSE (WING) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 AWR: AD: LOOSE FASTENERS NBR 1,2,3,4,5,6,7,8,9 AND 10 OF LH DRAG FITTING REF AMDS. CORRECTIVE ACTION: SUMMARY 1,2,3,4,5,6,7,8,9 AND 10 AT LHS UPPER SKIN & DRAG FITTINGS WAS PERFORMED PER ETI-57-20-052 REV. 4 AND ER/A 586129-14AD REV. ORG. SECTION I. (1540067)

Part: FASTENER — LOOSE (WING) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 AWR: AD: LOOSE FASTENERS NBR 11,12,13,15,16 AND 17 OF LH DRAG FITTING REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00428: TEMPORARY REPAIR FOR LOOSE FASTENERS NBR 11, 12, 13, 15, 16, AND 17 AT LHS UPPER SKIN & DRAG FITTINGS WAS PERFORMED PER ETI-57-20-052 REV. 4 AND ER/A 586129-14AD REV. ORG. SECTION I. (1540055)

Part: FASTENER — LOOSE (RT WING) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 AWR, AD, A.A.: LOOSE FASTENER NBR 1, 2, 3, 4, 5, 6, 8, 9 AND 10 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00465: PERMANENT REPAIR ON LOOSE FASTENER NBR 1, 2, 3, 4, 5, 6, 8, 9 AND 10 AT RH WING UPPER SKIN & DRAG FITTINGS WAS PERFORMED PER ETI-57-20-048 REV. 5 AND ER/A 586153-14AD REV. (1539404) . ORG. SECTION I.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON INTERCOSTAL BTW STA 1400 TO 1420 AND BTW ST 29LH AND 30 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION:SUMMARY OF NRC. 00671. CORROSION OUT OF LIMITS. ON INTERCOSTAL BTW STA 1400 TO 1420 AND BTW ST 29LH AND 30, WAS REPAIRED PER. ETI-57-20-073 REV. 1 AND ER/A 586448-14 REV ORIG. SECTION: I. (1539423)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 DURING WASTE PAN FASTENER REMOTION, INTERCOSTAL WAS FOUND WITH CORROSION. IN REF. NRC 00060. CORRECTIVE ACTION: SUMMARY OF NRC. 00547. CORROSION LEVEL 2. CORROSION OUT OF LIMITS ON INTERCOSTAL WAS REPAIRED PER. ER/A 586353-14 REV. ORIG. SECTION: I. (1539328)

Part: FASTENER — LOOSE (RT WING) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 AWR, AD, A.A.: LOOSE FASTENER NBR 12, 13, 14, 15, 16 AND 18 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00466 PERMANENT REPAIR ON LOOSE FASTENER NBR 12, 13, 14, 15, 16 AND 18 AT RH WING UPPER SKIN & DRAG FITTINGS WAS PERFORMED PER ETI-57-20-048 REV. 5 AND ER/A 586153-14AD REV. ORG. SECTION I. (1539459)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION OUT OF LIMITS WAS FOUND ON STRINGERS SUPPORT FROM STA 1328 TO 1331 AT RBL 2.90 TO RBL 16.10; FROM STA 1321 TO 1324 AT RBL 7.55 AND RBL 2.90; FROM STA 1397 TO 1399 RBL 16.10 ALSO FROM STA 1404 TO 1405 RBL 16.10 IN REF. NRC 00171. CORRECTIVE ACTION: SUMMARY: OF NRC S/N 00647 WERE REPAIRED PER B757-300 SRM (1538209)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION OUT OF LIMITS WAS FOUND ON STRINGERS SUPPORTS FROM STA 1508 TO STA 1511 AT LBL 7.55, LBL 10.45 AND LBL 2.90 AND STRINGER SUPPORTS FROM STA 1468 TO STA 1471 AT LBL 16.10 AND LBL 2.90 AT AFT CARGO COMPARTMENT IN REF. NRC 00193. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00649, CORROSION LEVEL 2, STRINGERS SUPPORTS FROM STA 1508 TO STA 1511 AT LBL 7.55, LBL 10.45 AND LBL 2.90 AND STRINGER SUPPORTS FROM STA 1468 TO STA 1471 AT LBL 16.10 AND LBL 2.90 AT AFT CARGO COMPARTMENT (C2) WERE REPAIRED PER B757-300 SRM. (1538836)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON FLOOR SUPPORT FROM STA 1380 TO STA 1440 RBL 20 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00173, FLOOR SUPPORT FROM STA 1380 TO STA 1440 RBL 20 AT AFT CARGO COMPARTMENT, C2 WAS REPLACED PER DWG REV B AND B757-300 SRM. (1538238)

Part: WEB — CRACKED (FUSELAGE) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CRACK ON WEB UNDER LOWER DOOR SILL AT STA 377 AND LBL 66 AT L1 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00683: PERMANENT REPAIR WAS PERFORMED ON WEB UNDER LOWER DOOR SILL AT STA 377 AND LBL 66 PER ER/A 586397-14 REV. ORG SECTION I AND B757-300 SRM. (1538666)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION WAS FOUND OUT OF LIMITS ON STRINGERS SUPPORTS FROM STA 1508 TO STA 1511 AT RBL 7.55, RBL 2.90, (IN REF NRC 00193.) CORRECTIVE ACTION: SUMMARY OF NRC. 00648. STRINGERS SUPPORTS FROM STA 1508 TO STA 1511 AT RBL 7.55, RBL 2.90, WERE REPAIRED PER. B757-300 SRM. (1538835)

Part: NOT REPORTED — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 NRC # 00474. CORROSION OUT OF LIMITS ON STA 365 RBL 15.5 TO RBL 25 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00553 PERMANENT REPAIR WAS PERFORMED ON STA 365 RBL 15.5 TO RBL 25 AT PAX CABIN. PER B757-300 SRM. (1538672)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON FRAME STA 1460 BTW STR 27 LH TO 28 RH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00188 FRAME STA 1460 BTW STR 27 LH TO 28 RH AT AFT CARGO COMPARTMENT C2, WAS REPAIRED PER ER/A 586386-14AD REV ORIGINAL SECTION 1 AS PERMANENT REPAIR. (1538560)

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON RIGHT SIDE PLATE FROM STA 1310 TO 1380 AT AFT CARGO COMPARTMENT. CORRECTIVE AVCTION: SUMMARY OF NRC 00156, CORROSION LEVEL 2, SIDE PLATE WAS REPLACED PER B757-300 SRM AND DWG. (1536782)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON FLOOR SUPPORTS STA. 750 LBL/RBL 16, LBL/RBL11, LBL/RBL 7, AND LBL/RBL 3, AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00245 CORROSION LEVEL 2, FLOOR SUPPORTS WERE REPAIRED PER B757-300 SRM. (1536653)

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION OUT OF LIMITS WAS FOUND ON RH SIDE PLATE FROM STA 1231 TO 1234 IN REF. NRC 00168. CORRECTIVE ACTION: SUMMARY OF NRC 00645: CORROSION LEVEL 2 WAS REPAIRED ON RH SIDE PLATE FROM STA 1231 TO 1234 PER B757-300 SRM. (1536544)

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON RH SIDE PLATE UPPER AND LOWER SURFACE FROM STA 1440 TO 1520.AFT CARGO COMPARTMENT. AMDS 2020-2379. C2. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00199, CORROSION LEVEL 2, RH SIDE PLATE FROM STA 1440 TO 1520.AFT CARGO COMPARTMENT. C2, WAS REPLACED PER B757-300 SRM AND DWG. (1536657)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION OUT OF LIMIT ON ANGLE FLOOR SUPPORT FROM STA 413 TO 428 RBL 66 AT PAX CABIN. W1. IN REF NRC 00460. CORRECTIVE ACTION:SUMMARY OF NRC. 00595 PERMANENT REPAIR: ANGLE FLOOR SUPPORT FROM STA 413 TO 428 RBL 66 AT PAX CABIN. WAS REPAIRED PER. ER/A. 586310-14 REV. ORIG. SECTION I, ETI-57-20-068 REV. ORG. AND B757 -300 SRM. (1536471)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION OUT OF LIMITS WAS FOUND ON STRINGERS SUPPORT FROM STA 1328 TO 1331 AT LBL 2.90 TO LBL 16.10 IN REF. NRC 00171. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00646, STRINGERS SUPPORT FROM STA 1328 TO 1331 AT LBL 2.90 TO LBL 16.10 (C2) WERE REPAIRED PER B757-300 SRM. (1535265)

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 AWR, OUT OF LIMITS: CORROSION ALONG RH SIDE PLANEL BTW STA 780+51 TO 780+69 AT FWD CARGO COMPARTMENT. ( IN REF. NRC S/N 00230). CORRECTIVE ACTION: SUMMARY OF NRC 00677: CORROSION LEVEL 2 ON SIDE PANEL BTW STA 780+51 TO 780+69 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B757-300 SRM. (1535071)

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION PREVIOUS REPAIR ON LH SIDE PLATE STA 1480 LBL 22 AT AFT CARGO COMPARTMENT. AMDS 2020-2379. C2. CORRECTIVE ACTION: SUMMARY OF NRC 00197 CORROSION LEVEL 2: SIDE PANEL WAS REPLACED PER DWG REV. ORG. AND B757-300 SRM. (1534998)

Part: NONE — NONE · airframe 67,435 hrs · 22,005 cycles

SHIP 5803 SECTION I TEMPORARY REPAIR TO LH WING UPPER SKIN AT DRAG FITTING ATTACHMENTS REQUIRES SECTION II PERMANENT REPAIR. CORRECTIVE ACTION: REF ERA 586129-14AD REV A. (1533796)

Part: NONE — NONE · airframe 67,424 hrs · 21,998 cycles

SHIP 5803 REF ERA 586153-14, ACCOMPLISH SECTION II REPETITIVE INSPECTIONS EVERY 2100 CYCLES AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR. CORRECTIVE ACTION: ERA 586153-14 UPDATED TO REV. A. (1533903)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 IN REF. TO NRC # 00474. CORROSION OUT OF LIMITS ON STA 377 LBL 11.5 TO LBL 13 AND LBL 54 TO LBL 55. AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00552 CORROSION LEVEL 2 ON STA 377 LBL 11.5 TO LBL 13 AND LBL 54 TO LBL 55. AT PAX CABIN. W1. WAS REPAIRED PERMANENTLY PER B757-300 SRM PROCEDURE 8 AND ER/A 585911-14 REV. ORG SECTION I. (1532874)

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION OUT OF LIMITS WAS FOUND ON LH SIDE PANEL FROM STA 600 TO 637 IN REF. NRC 00228. CORRECTIVE ACTION: SUMMARY OF NRC 00629: CORROSION LEVEL 2 ON LH SIDE PANEL FROM STA 600 TO 637 WAS REPAIRED PER B757-300 SRM. (1532991)

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CRACK ON METALLIC STRAP ADJACET TO FLOOR BEAM, STA. 720, RBL 26 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00213: METALIC STRAP ADJACET TO FLOOR BEAM, STA. 720, RBL 26 WAS REPAIRED PER B757-300 SRM. (1530682)

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION OUT OF LIMITS WAS FOUND ON LH SIDE PANEL AT STA 780+63 FWD CARGO COMPARTMENT (C1). (IN REF NRC 00243). CORRECTIVE ACTION: SUMMARY OF NRC 00630: CORROSION LEVEL 2 WAS REPAIRED ON LH SIDE PANEL AT STA 780+49 TO 780+69 PER B757-300 SRM. (1530638)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON RH INBD SEAT TRACK, FROM STA. 365.25 TO STA. 443, RBL 25 AT PASSENGER CABIN. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00442, CORROSION LEVEL 2, RH INBD SEAT TRACK, FROM STA. 365.25 TO STA. 443, RBL 25 AT PASSENGER CABIN. (CPAX) WAS REPLACED PER B757-300 SRM PAR 4 AND 7, AND DWG. (1528596)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CORROSION ON SEAT TRACK SUPPORT, STA. 365.25, RBL 44 AT PASSENGER CABIN. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00439, CORROSION LEVEL 2, SEAT TRACK SUPPORT, STA. 365.25, RBL 44 AT PASSENGER CABIN. (CPAX) WAS REPLACED PER B757-300 SRM AND DWG 141N5131 REV U. (1528598)

Part: WINDOW — DAMAGED (COCKPIT) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 INITIAL INSPECTION: ELECTRICAL ARC DAMAGE ON RH WINDOW NBR 3 AT COCKPIT. CORRECTIVE ACTION: SUMMARY OF NRC 00013: RH WINDOW NBR 3 AT COCKPIT WAS REMOVED AND THEN NEW WINDOW AT #3 RH POSITION WAS INSTALLED PER B757-300 AMM 56-11. OPERATIONAL TEST OK. (1528367)

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,219 hrs · 20,164 cycles

SHIP 5803 CRACK STIFFENER UNDER FLOOR BEAM STA 370 TO 377 LBL 15 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC. 00470 CRACK STIFFENER (STRAP) UNDER FLOOR BEAM STA 370 TO 377 LBL 15 WAS REPAIRED PER. B757-300 SRM. (1526957)

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1524887) CORRODION OUT OF LIMITS ON DECK PLATE STA Y=1681 BTW RBL 42 TO RBL 44 AT PASSENGER CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2. PERMANENT REPAIR WAS PERFORMED ON DECK PLATE PER B757-300 SRM 53-60-51-2R.

Part: STRUCTURE — CRACKED (L4 DOOR) · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1525756) CRACK ON INNER STRUCTURE OF L4 PASSENGER DOOR. CORRECTIVE ACTION: REPAIRED PER ERA 585897-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND ETI-57-20-055 REVISION ORIGINAL.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1524923) DECK PLATE OUT OF LIMITS ON STA. Y=1717 BTW LBL 2 TO LBL 3, STA Y=1708 BTW BL 0 TO RBL 2 AND STA Y=1681 BTW RBL 42 TO RBL 44 AT PASSENGER CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2, DECK PLATE OUT OF LIMITS REPAIRED PER ER/A 585970-14, REV: ORIGINAL, SECTION I, AND STA 1681 BTW RBL 42 TO RBL 44 WAS REPAIRED UNDER LOG PAGE 1524887.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1521725) ORIGINAL THICKNESS ON SETTLEMENT SEAT TRACKS STA 377 LBL 23-26 AT PAX CABIN IS 0.070 AND REMAINING THICKNESS ON SETTLEMENT SEAT TRACK IS 0.040". THEREFORE IS OUT OF LIMITS PER B757-300 SRM 53-00-52-1A FIG. 101 DETAIL VIII. CORRECTIVE ACTION: CORROSION LEVEL 2. CORROSION OUT OF LIMITS SEAT TRACKS SUPPORT AT STA 377 TO STA 418 LBL 23-26 WAS REPLACED PER. B757-300 SRM. 51-40-02-0G PAR. 4 AND 7 AND BAC1508-237.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1518056) CORROSION ON SEAT TRACK FROM STA 1640 BTW RBL 46 AT PAX CABIN. CORRECTIVE ACTION: REPLACED PER. B757-300 SRM. 51-40-02 PAR. 4 AND 7 AND 51-10-02 PAR. 15.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1517728) CORROSION SECOND TIER IN REF. NRC S/N 00435: CORROSION ON GUTTER SUPPORT FROM STA 1661 TO STA 1681 BTW LBL 54 AT PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PER B757-300 SRM 51-40-02 PAR 7 AND DWG 146N5230 REV. A.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1516046) ELECTRICAL ARC DAMAGE ON LH WINDSHIELD NBR 1 AT COCKPIT. CORRECTIVE ACTION: LH WINDSHIELD NBR 1 WAS REPLACED AT COCKPIT PER B757-300 AMM 56-11-01-424-015.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,219 hrs · 20,164 cycles

(AIRCRAFT 5803, L/P 1516479) CORROSION OUT OF LIMIT ON ANGLE STA 1023 TO 1034, RBL 64 AT PAX CABIN. CORRECTIVE ACTION: REPAIRED PER. B757-300 SRM. 53-00-13-2R.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,891 hrs · 20,055 cycles

5 BATTERY PACKS DID NOT ILLUMINATE THEIR GROUP OF EMERGENCY LIGHT FOR 15 MIN PER JOB CARD 3351-7004. CORRECTIVE ACTION: R/R'D BATTERY PACKS PER AMM 33-51.

Part: COVER — LOOSE (EXIT SIGN) · airframe 61,800 hrs · 20,027 cycles

(AIRCRAFT 5803, L/P 1424850) EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 3R / INTERIOR. CORRECTIVE ACTION: RESECURED EXIT SIGN.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 61,517 hrs · 19,943 cycles

(AIRCRAFT 5803, L/P 6560476) FOUND 3R AND 3L EXIT LENS DAMAGED. CORRECTIVE ACTION:REPLACED DAMAGED LENS.

Part: STRAP — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 61,117 hrs · 19,814 cycles

SHIP 5803 AT PUSHBACK L2 DOOR WOULD NOT ARM. CORRECTIVE ACTION: ADJUSTED BUSTLE STRAP. NOW OPS NML. REF B757 AMM 25-66. (6361050)

Part: COVER — UNSECURE (L2 GIRT BAR) · airframe 60,942 hrs · 19,763 cycles

COULD NOT ARM /DISARM DOOR. SECURED FWD L2 DOOR GIRT BAR COVER, ARM LIGHT OPS CK GOOD IAW B757 25-66.

Part: INDICATOR — STUCK (DOOR) · airframe 59,604 hrs · 19,399 cycles

2L AND 2R DOOR KNUCKLE KNOCKERS STICKING IN. DOORS ARMED. T/S DOOR 2L & 2R KNUCKLE KNOCKER TEST IAW B757 AMM 52-11. CYCLED HANDLE MULTIPLE TIMES, OPS CHECK GOOD. NI RIGGING DISTURBED. OK FOR SVC.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,807 hrs · 19,185 cycles

SHIP 5803 EMERGENCY EXIT SIGNS INOP AT DOORS 2L & R. CORRECTIVE ACTION: R&R BATTERY PACK. (5780547)

Part: SIGN — INOPERATIVE (CABIN) · airframe 58,786 hrs · 19,179 cycles

SHIP 5803 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS: 37. CORRECTIVE ACTION: RE ATTACHED EXIT SIGN AT 37. (0996290)

Part: LENS — UNSECURE (CABIN) · airframe 58,242 hrs · 19,009 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:206. RESECURED LENS.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 57,982 hrs · 18,927 cycles

SHIP 5803 DURING PUSHBACK PREP NR 4 RT DOOR WOULD NOT ARM. CORRECTIVE ACTION: RMVD DEBRIS FROM GIRT BAR. (3749864)

Part: WINGLET — DAMAGED (RT WING) · airframe 57,908 hrs · 18,909 cycles

SHIP 5803 RT WINGLET TIP TRAILING EDGE DAMAGE. CORRECTIVE ACTION: C/W ER/A 574215-14 REV ORIG, SEC I PERMAMANT REPAIR. (0882472)

Part: SHOE — NOT SEATED (GIRT BAR) · airframe 57,450 hrs · 18,788 cycles

(AIRCRAFT 5803, L/P 5012486) 4R DOOR ARMED INDICATIONS INOP. HANDLE JAMMED HALFWAY. RESEATED FWD GIRT BAR SHOE AND PERFORMED OP CK PER B757 AMM 25-66.

Part: LIGHT — INOPERATIVE (SEAT 28D) · airframe 57,364 hrs · 18,759 cycles

(AIRCRAFT 5803, L/P 0816546) EMERGENCY PATH LIGHT INOP AT SEAT 28D. REPLACED SEAT LIGHT AT 28D. OPS CHECKS NORMAL.

Part: DOOR — OBSTRUCTED (R1) · airframe 57,097 hrs · 18,684 cycles

DOOR 1 RT WILL NOT ARM. REMOVED DEBRIS FROM SILL AREA DOOR 1RT.

Part: SIGN — UNSECURE (MID CABIN) · airframe 55,556 hrs · 18,297 cycles

EXIT SIGN, MID SHIP WAS NOT SECURE. SECURED THE EXIT SIGN.

Part: SIGN — MISSING (ROW 38) · airframe 55,368 hrs · 18,241 cycles

EXIT SIGN AT ROW 38 WAS MISSING. REPLACED THE SIGN.

Part: DOOR — OUT OF ADJUST (L2) · airframe 55,275 hrs · 18,216 cycles

DOOR ARMED KNUCKLE KNOCKER INOPERATIVE, LOCATIONS:603 INTERIOR. ADJUSTED 2L KNUCKLE KNOCKER.

Part: SIGN — INOPERATIVE (CABIN) · airframe 55,287 hrs · 18,219 cycles

EMERGENCY EXIT SIGNS INOPERATIVE, LOCATIONS:37C INTERIOR. REINSTALLED EXIT SIGN COVER UP RIGHT.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 55,167 hrs · 18,177 cycles

DURING A SERVICE CHECK, FOUND ROW 27 LEFT EXIT SIGN DAMAGED. REPLACED THE EXIT SIGN IAW WDM 33-51-13.

Part: SKIN — DENTED (BS 610) · airframe 54,698 hrs · 18,035 cycles

FOUND TWO DENTS IN THE LT FUSELAGE SKIN, BS 610 BETWEEN STRINGERS 15L & 16L. OPEN

Part: NOT REPORTED — DIRTY (R1 DOOR) · airframe 54,691 hrs · 18,032 cycles

R1 DOOR WOULD NOT ARM. REMOVED DEBRIS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,529 hrs · 17,979 cycles

EXIT SIGN ABOVE THE R2 DOOR INOPERATIVE. FOUND THE BATTERY PACK FAILED, INSTALLED A NEW BATTERY PACK, OPS CHECKED GOOD IAW MM 33-51-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,375 hrs · 17,931 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 33 - 36. REPLACED THE POWER SUPPLY AND BATTERY PACK IAW AMM 33-51. CHECKED OK.

Part: UNKNOWN — UNKNOWN (L2 DOOR) · airframe 54,250 hrs · 17,892 cycles

L2 PAX ENTRY DOOR WON'T ARM. INSPECTED THE DOOR CYCLE ARM & DISARM LEVER, NO FAULT FOUND.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,162 hrs · 17,865 cycles

CABIN SEAT EMERGENCY LIGHTS INOPERATIVE AT ROWS 14 - 20. FOUND THE POWER SUPPLY INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY AT M11613 IAW AMM 33-51-07.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,162 hrs · 17,865 cycles

DURING SERVICE CHECK, FOUND THE EMERG LIGHTS AT THE L2 DOOR, CTR AISLE OVERHEAD, & SEATS 15 DEF- 20 DEF INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSY M11613 IAW AMM 33-51-07.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 53,106 hrs · 17,543 cycles

EMERGENCY LIGHT AT 28D, FOUND SHROUD BROKEN. REPLACED THE EMERGENCY LIGHT SHROUD. OPS GOOD IAW AMM 33-51.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 52,229 hrs · 17,317 cycles

EMERGENCY EXIT LIGHT COVER DAMAGED, ROW 40. REPLACED EMERGENCY EXIT COVER.

Part: SPRING — DEFECTIVE (R4 DOOR) · airframe 50,952 hrs · 16,882 cycles

R-4 DOOR WILL NOT OPEN. R&R GIRT BAR TARGET SPRING ALL CHECK NORMAL PER AMM 25-66.

Part: GUARD — DEFECTIVE (LIGHT SWITCH) · airframe 50,825 hrs · 16,835 cycles

EMERGENCY LIGHT SWITCH TURNS OFF WHEN GUARD IS LOWERED. REPLACED EMERGENCY LIGHT PANEL PER AMM33-51 CKS GOOD.

Part: FILTER — ODOR (CABIN) · airframe 49,982 hrs · 16,547 cycles

DURING CRUISE, 3 DIFFERENT F/A'S REPORTED SMELLING ELECTRICAL SMOKE FUMES WITH NO VISIBLE SMOKE AT SEAT 40 A,B,C. INSTRUCTED F/A TO TURN OFF IFE SYSTEM AND ODOR SUBSIDED AND STOPPED COMPLETELY. R & R THE FAN FILTERS. AIR FLOW NORMAL. CHECKED OVERHEAD LIGHTS, PSU'S, IFE MONITORS AND OUTLETS. NO TROUBLE FOUND. CHECKED IFE RACK IN AFT BAG BIN. SEEMED TO HAVE AN ELECTRICAL ODOR. CHANGED FAN FILTERS IN COMPARTMENT AND ODOR HAD DISSIPATED.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 49,197 hrs · 16,291 cycles

EXIT SIGN MISSING ABOVE AISLE ABOUT ROW 38. INSTALLED A NEW EMERGENCY EXIT SIGN, OK FOR SERVICE.

Part: LIGHT — BROKEN (ROW 6C) · airframe 49,117 hrs · 16,268 cycles

EMERGENCY LIGHT AT 6C BROKEN. REPLACED THE EMERGENCY LIGHT AND OPS CHECKED NORMAL.

Part: SKIN — DENTED (BS 640) · airframe 47,490 hrs · 15,715 cycles

FUSELAGE, SKIN, BS 640, S-17L DENT. AN EXISTING SRM REPAIR WAS REMOVED AND A PERMANENT REPAIR INSTALLED IAW ER/A 522511-14. DTA MONITOR INSPECTION LOG REF EA 58-522511. SECTION II REQUIRES DTA PRIOR TO 24 MONTHS FROM FAA FORM 8100-9 APPROVAL. ACCOMPLISHED PERMANENT REPAIR AT BS 640, STR-17L, FWD OF L2 DOOR IAW ER/A 522511-14, REV ORIGINAL. OK TO CLOSE LOG PAGE REFNEW LOG PAGE NR 1348700 CREATED FOR REPEAT INSPECTION IAW ER/A 522511-14, REV ORIGINAL SECTION I. SDR REPORTABLE ITEM. ER/A 522511-14 HAS BEEN REVISED, CURRENT REVISION IS A. SCHEDULING HAS BEEN CHANGED. REFER TO LOGPAGE 2339492 FOR ALL FOLLOW ON ACTION ASSOCIATED WITH ERA 522511-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,589 hrs · 15,411 cycles

LIGHTNING STRIKE IN NOSE AREA. FOUND EVIDENCE OF DISCHARGE APPROXIMATELY 3" AFT OF DOOR 1R, 12" FROM TOP EDGE. REF SRM 53-00-01, REPAIR 6 + 53-00-01, REMOVED FASTENER + CLEANED UP AREA. NEEDS NDT EDDY CURRENT, WIP 715288, MEASURED BLEND TO BE WITHIN ACCEPTABLE LIMITS IAW SRM 53-00-01, FIG 101. PERFORMED HFEC INSP IAW NDT PT6, 51-00-01, NO DEFECTS NOTED. COMPLETED REPAIR IAW SRM 53-00- 01.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 46,589 hrs · 15,411 cycles

LIGHTNING STRIKE DAMAGE FOUND ON LT ELEVATOR BOTTOM SIDE AND T/E. BURN MARKS ARE CLUSTERED IN A 6" X 8" AREA, 6" AFT OF THE FWD EDGE OF THE ELEVATOR AND CENTERED AT N ELEV, BS 257. DAMAGE FALLS IN ZONE II REF SRM 55- 20-01 P101. COMPLETED DETAILED PROCEDURE IAW AMM 05-51-19E, 1,(D) 3. TEST OK. APPLIED REPAIRS AT 6" X 8" AREA, 5 MINOR SURFACE DELAMINATIONS IAW SRM 51-70-17.

Part: SLIDE — DAMAGED (RT OVERWING) · airframe 41,035 hrs · 13,540 cycles

RT OVERWING ESCAPE SLIDE SAFTY CABLE FOUND LACING LOOSE. R & R ESCAPE SLIDE IAW AMM 25-65-01-004-001 AND AMM 25-65-01-404-002. INSTALLATION OF ESCAPE SLIDE COMPLETED.

Part: SEAT TRACK — CORRODED (BS 720-740) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

MAIN CABIN SEAT TRACK AT RBL 45.5 HAS CORROSION ON INBD AND OTBD FLANGES AT BS 720 AND 740. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. INSTALLED SEAT TRACK IAW SRM.

Part: GIRT BAR — BROKEN (R1 DOOR) · airframe 41,035 hrs · 13,540 cycles

R1 DOOR GIRT BAR, AFT LEAF SPRING IS BROKEN OFF. R & R SERVICEABLE GIRT BAR. SPRING CK C/W.

Part: GIRT BAR — BROKEN (L1 DOORWAY) · airframe 41,035 hrs · 13,540 cycles

L1 DOOR GIRT BAR FWD LEAF SPRING FAILED CHECK, DOES NOT RETAIN SLIDER, SLIDER RIDES OVER SPRING. R & R GIRT BAR AND SPRING CHECK C/W.

Part: SEAT TRACK — CORRODED (BS 1320) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

MAIN CABIN SEAT TRACK, LBL 24.75, BS 1320 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED IAW SRM 53-00-52.

Part: DOOR FRAME — GOUGED (R4 DOORWAY) · airframe 41,035 hrs · 13,540 cycles

R4 DOOR FRAME UPPER FUSELAGE CUT-OUT GOUGED. BLENDED GOUGE ON R4 DOOR SEAL DEPRESSOR, FRAME UPPER FUSELAGE CUTOUT, REF DWG 146N6123. FOUND TO BE OUT OF LIMIT IAW SRM. R & R WITH NEW SEAL DEPRESSOR REF SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1300-1320) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

MAIN CABIN SEAT TRACK, RBL 24.75 BS 1300-1320 CORRODED ON BOTH SIDES OF THE FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED IAW SRM 53-00-52.

Part: FLOORBEAM — CRACKED (BS 365) · airframe 41,035 hrs · 13,540 cycles

STABILIZER STRAP IS CRACKED, BOTTOM SIDE OF FLOORBEAM AT BS 365.25, LBL 45.50. ACCOMPLISHED WORK IAW ER/A 384483-14MA, REV D STABILIZER STRAP REPAIR AT BOTTOM SIDE OF FLOORBEAM STA 365.25, LBL-45.5 ASSOCIATED ER/A 14-384483.

Part: SEAT TRACK — CORRODED (BS 1320) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

MAIN CABIN SEAT TRACK, RBL 24.75 JUST AFT OF BS 1320 BOTH SIDES OF FLANGE ARE CORRODED. BLENDED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. R & R SEAT TRACK SECTION BS 1320-1350 IAW SRM 53-00-52.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · airframe 41,035 hrs · 13,540 cycles

LEFT CREASE BEAM INNER CHORD ANGLE HAS AREAS OF LIGHT CORROSION BETWEEN BS 1020 AND 1040. R & R CREASE BEAM INNER CHORD ANGLE AT BS 900-1040 MAIN CABIN LT SIDE IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1320) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

MAIN CABIN SEAT TRACK LBL 24.75 JUST FORWARD OF BS 1320 IS CORRODED. REPAIRED FROM BS 1270 TO 1320 IAW SRM 53-00-52.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

RIGHT CREASE BEAM INNER ANGLE HAS AREAS OF LIGHT CORROSION FROM BS 1020 TO 1040. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW IAW SRM 53-30-13. REMOVED AND FABRICATED CREASE BEAM INNER ANGLE BS 900-1040 IAW SRM 51-40-02, 51-40-05, INSTALLED CREASE BEAM ANGLE IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

CORROSION AROUND RIVET HEADS AT OTBD END OF FLOORBEAM APPROX RBL 56, BS 1640. REPAIRED IAW ER/A 481634-14MA, REV A.

Part: STRUCTURE — GOUGED (THRUST REVERSER) · airframe 41,035 hrs · 13,540 cycles

NR 2 ENGINE, INBD THRUST REVERSER FWD UPPER INBD CORNER HAS LARGE GOUGE. REPAIRED IAW ERA 522505-14, REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

FLOORBEAM AT BS 377.7 IN MAIN CABIN HAS CORROSION ON UPPER CAP FROM BL 0-LBL 62. BLENDED OUT CORROSION, ACCOMPLISHED REPAIR IAW ER/A 481634-14MA. THE REST OF THE FLOORBEAM BETWEEN BL 0-LBL 5.5 AND LBL 5.5-LBL 62 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-51.

Part: STRINGER CLIP — BENT (R3 DOOR) · airframe 41,035 hrs · 13,540 cycles

AT S2 THE FWD AND AFT STRINGER CLIPS ARE BENT ON R3 DOOR. REMOVED, FABRICATED, AND INSTALLED FWD STRINGER CLIPS, NEW, ON R-3 DOOR AT S-2 LOCATION WITH SHT 7075 -0 -0.040" BATCH NR. HEAT TREATED TO T6 IAW DWG 146N6346-2 IAW SRM 51-40-02, PG 38, FIG 12, DETAIL II. REFORMED AFT STRINGER CLIP AT R-3 DOOR S-2 LOCATION IAW BAC 5300, NDT VERIFIED, NO CRACKS NOTED AT REWORKED AREA.

Part: SEAT TRACK — CORRODED (BS 1280-1320) · corrosion level 2 · airframe 41,035 hrs · 13,540 cycles

MAIN CABIN SEAT TRACK BS 1280-1320, LBL 24.75 CORRODED INSIDE SCALLOP AREA. SEAT TRACK REPAIRED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,083 hrs · 13,159 cycles

SKIN GOUGED FWD OF L2 DOOR. GOUGE CUT OUT, BLENDED AREA AND NOW IS BEYOND 15 PERCENT. PERFORMED UT MEASUREMENT IAW NDT SPM 51-00-10 FOUND UPPER BLEND AREA WITH.053 MATERIAL REMAINING CUT OUT DAMAGED AREA ACCOMPLISHED HFEC INSPECTION NTM 757, PART 651-00-01, NO CRACKS FOUND FABRICATED AND DRILLED DOUBLER AND FILLER IAW SRM 53-00-01. INSTALLED REPAIR IAW SRM 53-00-01, FIG 201.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,911 hrs · 13,086 cycles

EMERGENCY AISLE LIGHTS AT ROWS 47 15 AND 01 INOPERATIVE OVERHEAD. REPLACED LAMP IAW AMM 33-51. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,092 hrs · 12,459 cycles

FOUND SEVEN EMERGENCY ESCAPE PATH BULBS INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,973 hrs · 12,061 cycles

EMERGENCY LIGHTS AT SEATS ROW 37, 38, 39 AND SIGN AT 37 INOPERATIVE. TROUBLESHOT EMERGENCY LIGHT AT ROW 37,38 AND 39. R AND R BATTERY PACK AND CHARGER ABOVE SEAT ROW 40. SEATS 37,38,39 OPERATE NORMAL. INSTALLED NEW C/P AT EXIT ROW SIGN 37. EMERGENCY LIGHTS TESTED OK.

Part: CABLE — OUT OF TOLERANCE (R4 DOOR) · airframe 6,578 hrs · 2,278 cycles

DURING L CHECK, MAINTENANCE FOUND R4 DOOR EMERGENCY POWER ACTUATION CABLE FAILED STEP 3 ON CARD 5211-7001. CABLE WAS LESS THEN .9 INCH. MAINTENANCE ADJUSTED THE STUD ON THE R4 DOOR EMERGENCY POWER ACTUATION TRIGGER PER AMM 52-11. CABLE TRAVEL NOW IN ALLOWABLE LIMITS.

Part: CABLE — OUT OF TOLERANCE (L4 DOOR) · airframe 6,578 hrs · 2,278 cycles

DURING L CHECK, MAINTENANCE FOUND L4 DOOR EMERGENCY POWER ACTUATION CABLE FAILED STEP 3 ON CARD 5211-7001-4L. CABLE WAS LESS THEN .8 INCH. MAINTENANCE ADJUSTED STUD ON THE L4 DOOR EMERGENCY POWER ACTUATION TRIGGER PER AMM 52-11. CABLE TRAVEL NOW IN ALLOWABLE LIMITS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 6,081 hrs · 2,103 cycles

DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS OUT AT 4AB THRU 6AB. MAINTENANCE REPLACED BATTERY CHARGER FOR SEAT ROW 4-6 AB PER AMM 33-50. OPERATION OF LIGHT NOW CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 5,910 hrs · 2,029 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT PATH AT LAST 5 ROWS AND L4 EXIT SIGN INOP. OPERATION OF LIGHT NOW CHECKS OK. MAINTENANCE REPLACED BATTERY PACK AT M737 PER AMM 33-51-07. LIGHTS NOW CHECK OK.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 32,875 hrs · 10,518 cycles

DURING FLIGHT, CREW REPORTED AN ACRID ODOR IN THE COCKPIT AND CABIN. ODOR CAUSED BURNING IN THE EYES. MAINTENANCE CHECKED PACKS, CARGO, AND AVIONICS AREAS WITH NO SMELLS. ENGINE RUN WITH PACKS ON DID NOT DUPLICATE THE ODOR.

Part: COOLING FAN — SEIZED (NR 1) · airframe 31,168 hrs · 9,899 cycles

DURING FLIGHT, CREW NOTED A BURNING SMELL FOLLOWED BY 'EQPT OVHT' EICAS WITH 'OVHT'. FOLLOWED QRH AND MOVED THE EQUIPMENT COOLING SWITCH TO ALTERNATE. SMELL DISSIPATED AND MESSAGES EXTINGUISHED. MAINTENANCE FOUND THE FORWARD EQUIPMENT COOLING FAN 1 SEIZED AND REPLACED IT. ALL CHECKS WERE GOOD. (2011-00100)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,147 hrs · 9,887 cycles

DURING A LINE CHECK, MX FOUND THE DOOR 1R EXTERIOR EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE POWER SUPPLY. OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 757,351 hrs · 9,646 cycles

DURING A LINE CHECK, MX FOUND AN EMERGENCY EXTERIOR SLIDE LIGHT INOPERATIVE. MX REPAIRED THE LIGHT ASSY. OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (BS 540) · airframe 36,457 hrs · 11,853 cycles

DURING LIGHTNING STRIKE INSPECTION MX DISCOVERED STATIC DISCHARGE AT 3D RIVET ABOVE STRINGER 27C BS 540. REMOVED TEMP FASTENER AND COMPLETED BHEC -NO FAULTS NOTED. INSTALLED BRILES RIVET, TREATED, PRIMED AND PAINTED AREA IAW SRM 53-00-01.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 28,448 hrs · 9,037 cycles

DURING L-CHECK, FOUND PUNCTURE IN INBD MAIN FLAP LOWER SURFACE AT STA 130. REPAIRED IAW SRM 57-53-01, SRM 51-70-07, SRM 51-70-17.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,177 hrs · 8,635 cycles

EXTERNAL EMERGENCY LIGHTS AT DOORS 1R, 2R, 2L, AND 4L INOPERATIVE. RELAMPED DOOR 1R LIGHT. REMOVED, CLEANED, AND RESOLDERED CENTER POST IN REMAINING 3 SOCKETS. REINSTALLED LIGHTS AND OPS CHECK NORMAL. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 21,210 hrs · 6,832 cycles

BATTERY PACK ASSOCIATED WITH ESCAPE PATH LIGHTING AT ROWS 26 THROUGH 30 FAILED DURING EMERGENCY LIGHT BATTERY PACK CHECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,210 hrs · 6,832 cycles

BATTERY PACK ASSOCIATED WITH THE ESCAPE PATH LIGHTING AT ROWS FOUR THROUGH SIX FAILED DURING EMERGENCY LIGHT BATTERY PACK CHECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,210 hrs · 6,832 cycles

BATTERY PACK ASSOCIATED WITH THE ESCAPE PATH LIGHTING AT ROWS 40 THROUGH 44 FAILED DURING EMERGENCY LIGHT BATTERY PACK CHECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 21,210 hrs · 6,832 cycles

BATTERY PACK ASSOCIATED WITH THE ESCAPE PATH LIGHTING AT ROWS 14 THROUGH 20 FAILED DURING EMERGENCY LIGHT BATTERY PACK CHECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD.

Part: LINE — CHAFED (FUEL SYSTEM) · airframe 6,367 hrs · 2,204 cycles

THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD.

Part: LINE — CRACKED (HYDRAULIC SYS) · airframe 6,028 hrs · 2,097 cycles

IN CRUISE AT FL 37,000 FT RECEIVED R HYD SYS PRESS AND R HYD SYS QTY MESSAGES. QUANTITY SHOWED ZERO IN RT SYSTEM. DECISION WAS MADE TO DIVERT TO DTW. LANDING UNEVENTFUL, MAINTENANCE FOUND THE RETURN LINE FROM THE RT (ALTERNATING CURRENT MOTOR PUMP (ACMP) CRACKED AT B-NUT. VERIFIED SYSTEM WAS EMPTY AND INSTALLED TEMPORARY FLEX LINE (P/N 00255030499). AFTER SERVICING SYSTEM FOUND RT ACMP WITH CAVITATIONS AT 1230 PSI. REMOVED AND REPLACED AC HYDRAULIC PUMP 55-2911-9-0013 S/N OFF 56289 AND ENGINE DRIVEN PUMP 55-2911-9-0016 S/N OFF 58288.