N722TW

Part: CONTROL MODULE — FAULTED (SPOILER SYSTEM) · airframe 91,926 hrs · 23,144 cycles

OPS DECISION TO DIVERT TO IAD FOR LONGER RUNWAY DUE TO SPOILERS EICAS MESSAGE. REPLACED 1L SPOILER CONTROL MODULE.

Part: LIGHT — ODOR (ZONE 200) · airframe 90,995 hrs · 22,921 cycles

SHIP 6816 STRONG ELECTRICAL BURN SMELL IN AFT LAV. CORRECTIVE ACTION: FOUND L2 LIGHT COVER DAMAGED C/W SECTION I: TIME LIMITED ALTERATION PER ER/A 626912-14 REV ORIG, C/W ER/A62612-14 REV ORG SECTION 2 PERMANET RESTORATION. R/R LIGHT ASSY PER B757 AMM 33-26. LIGHT IS NOW WORKING AND NO BUR SMELL.

Part: LENS — MISSING (ZONE 200) · airframe 90,817 hrs · 22,878 cycles

SHIP 6816 CLEAR EMER LIGHTS LENSE MISSING ABOVE ROW 20 FED. CORRECTIVE ACTION: INSTALLED MISSING EMERGENCY CLEAR LENS ABOVE 20FED REF B757 AMM 33-51. (6980369)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 90,817 hrs · 22,878 cycles

SHIP 6816 EMER ESCAPE PATHS LIGHTS INOP AT ROWS 39,40,41,43 AND 44. CORRECTIVE ACTION: R/R BATTERY AND POWER SUPPLY FWD OF SEATS 36 FED PER B757 AMM 33 -51. OPS CHK NML. (6980370)

Part: GIRT BAR — FOD (ZONE 800) · airframe 90,657 hrs · 22,838 cycles

SHIP 6816 DOOR 4R PRIOR TO DEPARTURE WOULD NOT ARM. CORRECTIVE ACTION: FOUND GIRT BAR HOOK ATTACHMENT POINT WITH FOD CLAENED OPS CHECKED NORMAL AFTER CLEANED NO FURTHER FAULTS FOUND REFF B757-2 AMM 52-66. (648588)

Part: GUIDE ARM — OUT OF ADJUST (ZONE 800) · airframe 90,462 hrs · 22,750 cycles

SHIP 6816 L4 DOOR WILL NOT CLOSE FROM INSIDE AND HAS TO BE FORCED CLOSED FROM OUTSIDE. CORRECTIVE ACTION: ADJUSTED LOWER GUIDE ARM ON L4 DOOR PER B757 AMM 52-11, OPS NML. (6661274)

Part: TRANSMITTER — OUT OF ADJUST (ZONE 200) · airframe 90,330 hrs · 22,682 cycles

SHIP 6816 -MISC/DE- DUE TO TRAILING EDGE DISAGREE ON APPROACH. CORRECTIVE ACTION: REPLACED FLAP LEVER POSITION TRANSMITTER AND ADJUSTED. (LP 6661205)

Part: LANYARD — UNSECURE (ZONE 800) · airframe 90,062 hrs · 22,597 cycles

SHIP 6816 4R DOOR DIFFICULT TO ARM. CORRECTIVE ACTION: FOUND LIENARD CORD BIDING WITH ARMING GIRT BAR. REROUTED AND SECURED LIENARD CORD. OPS CHECK 4R DOOR PER B757 AMM 52-11 OPS CHECK GOOD. (6607964)

Part: SLIDE — MALFUNCTIONED (ZONE 800) · airframe 90,062 hrs · 22,597 cycles

SHIP 6816 LT PASS DR 1 SLIDE LT INOP. CORRECTIVE ACTION: R/R M731 IAW B757 AMM AND SSM 33-51. OP TEST PASS. (6607959)

Part: SLIDE — FOD (ZONE 800) · airframe 89,914 hrs · 22,523 cycles

SHIP 6816 4R DOOR SLIDE LIGHT WILL NOT ILLUMINATE WITH DOOR CLOSED AND ARMED. CORRECTIVE ACTION: REMOVED DEBRIS FROM BOTTOM OF DOOR SLIDE. LIGHT WORKS NORMAL. REFERENCE B757 AMM25-66. (6607906)

Part: INDICATION SYS — MALFUNCTIONED (ZONE 800) · airframe 89,825 hrs · 22,486 cycles

SHIP 6816 2R SLIDE LIGHT NOT ILLUMINATING WHEN ARMED. CORRECTIVE ACTION: R/R 2R SLIDE CAP ASSY PER B757 IPC 33-51, OPS CHK GOOD PER AMM 25-66. (6749656)

Part: DOOR — FOD (ZONE 800) · airframe 89,689 hrs · 22,435 cycles

SHIP 6816 4R DOOR WILL NOT ARM PROPERLY. CORRECTIVE ACTION: CLEANED DEBRIS OFF ARMING SLOT. OPS CHK'S NML. (6749616)

Part: LANYARD — UNSECURE (ZONE 800) · airframe 89,711 hrs · 22,443 cycles

SHIP 6816 4R DOOR DIFFICULT TO ARM. CORRECTIVE ACTION: T/S PER B757 FIM 52-11 TASK 815-813. INSPECTED GIRT BAR AND FITTINGS. FOUND MOORING LINE LOOSE AND FOUND DEBRIS IN THE LATCH. TUCKED THE MOORING LINE BACK AND CLEANED OUT DEBRIS. DOOR ARMS NORMAL. (0719815)

Part: SHEAR PLATE — DAMAGED (ZONE 100) · airframe 89,139 hrs · 22,262 cycles

SHIP 6816 DUE BLOWN SIDE, FUSELAGE AT S22R AR APPROX STA 1661 DMG. CORRECTIVE ACTION: REF SRM B757 53-00-0102R REPAIR 28 APPLICABLE TO DMG AREA. DMG CLEANED UP AS REQ. PERFORMED HFEC SURFACE INSPECTION OF CUTOUT PER B757 NDT MANUAL PT 651-00-19, NO DAMAGE FOUND. C/W REPAIR 28 PER SRM 53-00-01- 02R.(6378671)

Part: BOTTLE — LOW PRESSURE (SLIDE) · airframe 89,044 hrs · 22,241 cycles

SHIP 6816 L1 SLIDE INFLATION BOTTLE LOW IN THE RED. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SLIDE I.A.W. WORK CARD. (6378633)

Part: APU — FIRE (ZONE 100) · airframe 89,044 hrs · 22,241 cycles

SHIP 6816 -FIRE- RAMP REPORTED SPARKS AND FIRE COMING FROM APU TAILPIPE. CREW DISCHARGED FIRE BOTTLE. CORRECTIVE ACTION: INSPECTED APU NO DAMAGE FOUND. APU AND APU FIRE DETECTION SYSTEM PLACED ON MEL. APU WILL BE REPLACED.

Part: GIRT BAR — LACK OF LUBE (ZONE 800) · airframe 89,037 hrs · 22,238 cycles

SHIP 6816 2R SLIDE LIGHT MULTIPLE RELAMPS. CORRECTIVE ACTION: LUBRICATED AND OPERATED DOOR SLIDE 2R GIRT BAR PER B757 AMM 25- 66. 2R SLIDE LIGHT OPERATES NML. GIRT BAR ASSEMBLY OPS CHK NML. (0594356)

Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 88,580 hrs · 22,136 cycles

2R DOOR KNUCKLE KNOCKER WILL NOT EXTEND WHEN ARMING DOOR. CORRECTIVE ACTION: FOUND DOOR MID PANEL OBSTRUCTING KNUCKLE KNOCKER. ADJUST PANEL POSITION PER B757 AMM 52-11. ADJUSTED KNUCKLE KNOCKER STOP PER B757 AMM 52-11- 20-825-001 STEP K. CHECKS GOOD (5125304)

Part: SIGN — LOOSE (604) · airframe 88,456 hrs · 22,109 cycles

SHIP 6816 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:604. CORRECTIVE ACTION:RE-SECURED EXIT SIGN. OPS CHK NML. (0488251)

Part: HEATER — ODOR (ZONE 200) · airframe 88,295 hrs · 22,073 cycles

PLASTIC/ELECTRICAL SMELL REPORTED IN THE 2L DOOR AREA BY FLIGHT ATTN, SMELL WENT AWAY WITHIN 10MIN OF REPORT. REMOVED AND REPLACED NO.2 HEATER PER B757 AMM 21-45.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,147 hrs · 21,811 cycles

DOOR ENTRY LIGHT INOP. CORRECTIVE ACTION: REPLAMP, T/S PER WDM 52-71-11 PG 12. REMOVED E3-4 RACK AND FOUND PRE AA 4430-01019 WIRING STILL INSTALLED IN D40924J PIN 1. REMOVED PRE MOD WIRING AND CORRECTED ALL WIRING TO MATCH 52-71- 11. REINSTALLED E3-4 RACK AND PERFORM OPS CHECK OF ALL RACK COMPONENTS AND ENTRY DOOR LIGHT. ALL OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU FIRE) · airframe 86,911 hrs · 21,757 cycles

SHIP 6816 APU TAIL PIPE FIRE REPORTED. CORRECTIVE ACTION: PERFORMED TAIL PIPE INSPECTION PER AMM B757 TASK 49-81-01-202- 023 C/W WITH UP TO E3-E. MINO 257811. COMPLETED APU EXHAUST DUCT INSPECTION PER B757 AMM 49-81 & PERFORMED INSPECTION AFTER AN APU FIRE PER B757 AMM 49-11. NO DEFECTS NOTED (0236577)

Part: INDICATOR — INOPERATIVE (L2 DOOR) · airframe 86,457 hrs · 21,657 cycles

SHIP 6816 ESCAPE SLIDE ARMED CONDITION INDICATORS --2L DOOR KNUCKLE KNOCKER INOP. OPS CHK 2L DOOR REF B757 AMM 52-11. KNUCKLE KNOCKER OPERATES NML.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,026 hrs · 21,535 cycles

SHIP 6816 AISLE EMERGENCY LIGHTS FROM ROW 37 TO ROW 44 INOPERATIVE. CORRECTIVE ACTION: T/S PER 33-52. CHECKED FUSES ON EMERGENCY LIGHT BATTERY PACK POWER SUPPLY. ALL FUSES CHECK GOOD. INSPECTED WIRING FOR EXIT PATH LIGHTS, FOUND MULTIPLE CONNECTORS UNSECURE AND DISCONNECTED. RECONNECTED AND RESECURED CONNECTORS AND WIRE BUNDLES. ALL LIGHTS OP TEST GOOD. (4424862)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,892 hrs · 21,501 cycles

SHIP 6816 EXIT SIGN COVER FOR THE 2L DOOR IS DETACHED. CORRECTIVE ACTION: SECURED EXIT SIGN COVER IN REF. TO B757 AMM 33-51. (5364486)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON BODY FAIRING SETTLEMENT SUPPORTS (2 EA) STA 1240 BTW STR= 27LH / 27RH AT WING / BODY FAIRINGS. CORRECTIVE ACTION: SUMMARY OF NRC 00233: CORROSION ON BODY FAIRING SETTLEMENT SUPPORTS (2 EA) STA 1240 BTW STR= 27LH / 27RH AT WING WAS REPAIRED PER ERA 613095-14. (0053009)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 SECONDARY NRC IN REF. NRC: MON/6816/1960309: DURING INSPECTION DENT #20 WAS FOUND OUT OF LIMITS ON MAIN INBD FLAP UPPER SKIN AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00428: MAIN INBD FLAP UPPER SKIN AT RH WING WAS REPAIRED PER ERA 613096-14 REV. ORIG. SECTION I: PERMANENT REPAIR AND PRI 613096 REV. 2. (0052474)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON LOWER SILL FROM BS 1360 TO BS 1480 AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00189 CORROSION ON LOWER SILL FROM BS 1360 TO BS 1480 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B757-200 SRM 51-40. (0045096)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON FLOOR STRINGERS SUPPORTS 2.9LBL, 7.55LBL & 16.10LBL ALSO 2.9RBL, 7.55RBL & 16.10RBL ON BS 1470 AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00186 CORROSION ON FLOOR STRINGERS SUPPORTS ON BS1470 LBL2.9, LBL7.55, LBL16.10 AND RBL2.9 WERE REPAIRED PER. B757-200 SRM 53-00 AND FLOOR STRINGERS SUPPORTS RBL7.55 & RBL16.10 AT AFT CARGO COMPARTMENT WERE REPLACED PER B757-200 SRM 51-40. (0045360)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON SIDE PLATE (UPPER/LWR SURFACES) LH STA 1530 TO 1640 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00644. SIDE PLATE LH STA 1530 TO 1640 AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM 51-40. (0043591)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON RH SIDE PLATE (SEVERAL SPOTS) FROM BS 1200 TO BS 1310 IN AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00636. RH SIDE PLATE FROM BS 1200 TO BS 1310 IN AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B757-200 SRM 51-40. (0043946)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION DAMAGE WAS FOUND ON LH SIDE PLATE STA 1280 TO 1310 AND ADJACENT S-27L AT AFTER CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00656. LH SIDE PLATE STA 1200 TO 1310 WAS REPLACED PER B757-200 SRM 51-40. (0042134)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CRACK ON LH SIDE PLATE BTW BSTA= 736/740 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00154: CORROSION LH SIDE PLATE BTW BSTA = 736/740 AT FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM 51-40. (0040759)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON FLOOR STRINGER SUPPORT STA=1480 RBL 7.55 AND RBL 16.10 . STA=1498 LBL 2.90RH, LBL 7.55 AND RBL 7.55 ,RBL 10.45 . STA=1510 LBL 2.90 ,RBL 2.90 RBL 7.55(PREVIOUS REPAIR) , RBL 10.45(PREVIOUS REPAIR) C2. CORRECTIVE ACTION: SUMMARY OF NRC 00141 ON FLOOR STRINGER SUPPORT STA=1510 RBL 2.90, LBL2.90 WERE REPAIRED PER B757-200, SRM, PREVIOUS REPAIR ON RBL 7.55, RBL10.45 WERE REPLACED PER B757-200, SRM. SUPPORTS STA=1498 LBL 2.90RH, LBL 7.55 AND RBL 7.55 , RBL 10.45 WERE CLEANED PER DAL PS.900-1-2-1 NO. 01 PAR 4.C.(3), RE-INSPECTIONED PER B757-200 SRM AND NO DAMAGE WERE FOUND. SUPPORTS STA=1480 RBL7.55,RBL16.10 MUST BE REPLACED WITH NRC 00186.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 A.A. - A.D. DISBOND (3.500IN X 2.500IN) ON PRODUCTION DOUBLER AT OSS 305.5 LOWER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE. RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 0045: OSS 305.5 LOWER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE. RH WING WAS REPAIRED PER B757-200 S.R.M. 90035729)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON SIDE PLATE FROM STA 645 TO 764 IN REF NRC 00152. CORRECTIVE ACTION: SUMMARY OF NRC 00490: CORROSION ON RH SIDE PLATE FROM STA 645 TO 764 AT FWD CARGO COMPARTMENT WAS REPLACED PER B757- 200 SRM 51-40. (0034086).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON INTERCOSTAL (5 EAS) BTW STA 1380 AND 1440 LOWER SIDE AT AFT CARGO DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00051 CORROSION ON INTERCOSTAL (5 EAS) BTW STA 1380 AND 1440 LOWER SIDE AT AFT CARGO DOOR WERE REPLACED PER B757-200 SRM 51-40. (0032814)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON FLOOR STRINGERS SUPPORTS 2.90LBL, 7.55RBL AND 2.90RBL FROM BS 1320 TO BS 1340 AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00181 CORROSION ON FLOOR STRINGERS SUPPORTS LBL 2.90, RBL 2.90 FROM BS 1320 TO BS 1340 AT AFT CARGO COMPARTMENT WERE REPAIRED PER B757-200 SRM 53-00. (0032875)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON SIDE PLATE (UPPER/LWR SURFACES) RH STA 1440 TO 1530 PER ADJACENT STGR 27 C2. CORRECTIVE ACTION: SUMMARY OF NRC 00646 CORROSION ON RH SIDE PLATE BTW STA 1440 TO 1530 AT C2 WAS REPLACED PER B757-200SRM 51-40. (0031458)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON FLOOR SUPPORT UNDER ATTACH FITTING REMOVED (WIP #2) AT STA 680 APPROX. CORRECTIVE ACTION: SUMMARY OF NRC 00429. CORROSION ON FLOOR SUPPORT WAS REPLACED PER B757-200 SRM 51-40 (0030912)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON DECK PLATE AREA STA 1720-1681 AND RBL 52 TO LBL 52 AT FLOOR STRUCTURE (W4) (AREA OUT LIMITS). CORRECTIVE ACTION: SUMMARY OF NRC 00469 CORROSION ON DECK PLATE AREA STA 1720-1681 AND RBL 52 TO LBL 52 AT FLOOR STRUCTURE WAS REPAIRED PER B757-200 SRM 53-60-51. (0027253)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION FLOOR STRUCTURE SUPPORT BTW STA. 324 TO 333 AND RBL.40 AT PASSENGER CABIN W1 AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00378 NEW FLOOR STRUCTURE SUPPORT BTW STA. 324 TO 333 AND RBL.40 WAS FABRICATED AND REPLACED PER B757-200 SRM 51-40. (0027141)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 DENT ON FRAMES BSTA 1320 & BSTA 1380 BTW STGS 26LH & 27LH AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00178: FRAMES BSTA 1320 & BSTA 1380 BTW STGS 26LH & 27LH AT AFT CARGO COMPARTMENT WERE REPAIRED PER B757-200 SRM 53-00. (0026950)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 SECONDARY NRC IN REF AMDS 2751-2542 STEP# 9: CORROSION ON OUTBD BALLSCREW NUT OF OUTBD TE FLAP AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00396: OUTBD BALLSCREW OF OUTBD TE FLAP AT RH WING REMOVED AND SERVICEABLE BALLSCREW WAS INSTALLED PER B757-200 AMM: 27-51. OPERATIONAL TEST IS ACCOMPLISHED UNDER AMDS. (0014352)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 85,888 hrs · 21,499 cycles

SHIP 6816 CORROSION ON LEFT OUTBD PASSENGER SEAT TRACK BTW STA. 720-740 AND 760- 770. CORRECTIVE ACTION: SUMMARY OF NRC 00289 SEAT TRACK ON STA. Y= 700 TO STA Y= 788 AND LBL= 45.50 WAS REPLACED PER B757-200 SRM. (0014309)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,496 hrs · 21,416 cycles

SHIP 6816 EMERGENCY LIGHTS ON SEAT ROW 27 FED THRU 35 FED. CORRECTIVE ACTION: T/S REMOVED AND REPLACED BATTERY AND BATTERY CHARGER FOR EMERGENCY ISLE SEAT LIGHTS PER B757 AMM 33-51. FOUND WIRE W3632-9002-20 OPEN. FOUND SAME BROKEN ABOVE OVHD BIN AT SEAT 27DEF. REPAIRED WIRE REF B757 SWPM CH. 20. FOUND WIRE W3632-9002-20 PULLED FROM CONNECTOR AT FLOOR BELOW SEAT 26F. REPLACED PIN ON WIRE W3632-9002-20 PER BSWPM CHPT 20 ALL LIGHTS CK'S GOOD. (4689254)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,561 hrs · 21,196 cycles

SHIP 6816 EMERG EXIT SIGN LIGHTS INOP AFT R EMERG EXIT DOOR AND AFT LEFT SIDEWALL PANEL. CORRECTIVE ACTION: REMOVED AND REPLACED POWER SUPPLY (BATT CHARGER) ABOVE AFT R EMERGENCY EXIT DOOR. (4694739)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,986 hrs · 21,076 cycles

SHIP 6816 ON SVC CHK FOUND EMERGENCY LIGHTS ON ROWS 36-44 RT SIDE INOP. CORRECTIVE ACTION: R/R EMERGENCY LIGHT BATTERY PACK, NO HELP. R/R EMER LIGHT BATTERY CHARGER WITH ORIGINAL BATTERY INSTALLED LIGHTS OPS NML. REF B757 AMM 33-51. (4149451)

Part: NONE — NONE · airframe 83,615 hrs · 20,984 cycles

SHIP 6816 REF: N/R 001 - WHILE WORKING WORK CARD 5331-01232-02G TO REPAIR A CRACK COMMON TO THE L1 DOOR UPPER, FWD CORNER BEAR STRAP. CORRECTIVE ACTION: REF: N/R 001 - COMPLIED WITH ER/A 606813-14AD PRI REV. 0. (7354961)

Part: NONE — NONE · airframe 83,615 hrs · 20,984 cycles

SHIP 6816 WHILE WORKING WORK CARD # 5331-01232-02A L-1 DOOR CUT OUT FOUND CRACK INDICATION IN BEAR STRAP, CRACK LENGTH IS APPROX. 9/16". CORRECTIVE ACTION: COMPLIED WITH AMDS WORK CARD 5331-01232-02G PERMANENT REPAIR. (7354953)

Part: NONE — NONE · airframe 83,615 hrs · 20,984 cycles

SHIP 6816 DTE, ER/A 606813-14AD TRACKING. B757-200 / FUSELAGE / L1 DOOR SURROUND / UPPER FWD CORNER / CRACK. CORRECTIVE ACTION: REF ERA 606813-14AD. (2663210)

Part: ARMING LEVER — WILL NOT ARM · airframe 83,230 hrs · 20,894 cycles

SHIP 6816 FA NOTED ARMING LEVER AT 4R WOULD MOVE FULLY IN THE ARMED POSITION. CORRECTING ACTION: CHECKED DOOR OPERATION PER B757 AMM 52-11 OPS CK NML. (9452470)

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 83,098 hrs · 20,866 cycles

1R DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM THE GIRT BAR AND OPS GOOD IAW AMM 52-11. (9452428)

Part: LIGHT — MALFUNCTIONED (DOOR SLIDE) · airframe 82,287 hrs · 20,678 cycles

SHIP 6816 1R DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: CYCLED 1R DOOR GIRT BAR ENGAGEMENT WITH NO DISCREPANCIES NOTED. SLIDE LIGHT ILLUMINATES NORMALLY. (9434460)

Part: NONE — NONE · airframe 82,272 hrs · 20,675 cycles

SHIP 6816 PER W/C 3352-01042-01B DOOR 1L EXIT SIGN OUT OF CONFIGURATION. CORRECTIVE ACTION: REPLACED 1L FLOOR EXIT SIGN IAW SWPM 20-30-12. REF B757 AMM 33- 51-10. OPS NORMAL. (9434450)

Part: NONE — NONE · airframe 82,132 hrs · 20,642 cycles

SHIP 6816 DEVELOPING HISTORY OF 1R DOOR NOT ARMING/SLIDE LIGHT NOT ILLUMINATING. CORRECTIVE ACTION: R/R FWD PROX SWITCH (S10216) SWPM CH 20 AND B757 WDM 25-66-11 GAP CHECK OF PROX SWITCHES ACCOMPLISHED IAW B757 AMM 25-66 DOOR DISARMED & ARMED MULTIPLE TIMES, ALL OPS NORMAL. (2431043)

Part: NONE — NONE · airframe 81,934 hrs · 20,597 cycles

SHIP 6816 DOOR 1R WILL NOT ARM. CORRECTIVE ACTION: REMOVED BUSTLE. CLEARED SLIDE HOOK FROM UNDER GIRT BAR. REINSTALLED BUSTLE PER B757 AMM 52-11. SLIDE ARM & DISARMS NORMALLY. (9094908)

Part: SENSOR — INTERMITTENT · airframe 81,036 hrs · 20,375 cycles

SHIP 6816 4L DOOR EIAS LIGHT (OPEN) INTERMITTENT. CORRECTIVE ACTION: ADJUSTED SENSOR IAW B757 AMM 52-71 OP CHECKS GOOD. (8717584)

Part: NOT REPORTED — NOT REPORTED · airframe 80,559 hrs · 20,260 cycles

SHIP 6816 CAPTAIN #1 WINDOW SIGNS OF ARCING ON TOP BUS BAR. CORRECTIVE ACTION: INSTALLED L1 WINDOW PER B757 AMM 56-11. (8841599)

Part: NONE — NONE · airframe 79,987 hrs · 20,132 cycles

SHIP 6816 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:605. CORRECTIVE ACTION: R+R EMER. EXIT SIGN AT 3L PER B737 AMM 33-51. CHECK GOOD. (2085611)

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP, SECTION 4, AS FOLLOW: HOLE #2 CORROSION ON FITTING AND SKIN, BTW 2 AND 5 OCLOCK POSITION, HOLE #3 CORROSION ON SKIN AT 3 OCLOCK POSITION, HOLE #4 CORROSION ON FITTING AT 2 OCLOCK POSITION AND CORROSION ON SKIN AT 7 O?CLOCK POSITION, HOLE #5 CORROSION ON FITTING AT 2 OCLOCK POSITION AND CORROSION ON SKIN AT 7 OCLOCK POSITION AND HOLE #10 CORROSION ON SKIN, BTW 3 AND 5 OCLOCK POSITION, IN REF. CARD. (1989597)

Part: NOT REPORTED — NOT REPORTED · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 LH ENG DRAG FTG CLAMP UP SECTION 04 DAMAGES FOUND ON OPEN HOLES AS FOLLOWS: HOLE#1 CORROSION ON SKIN BTW 5 -7 HRS POSITION; HOLE #2 CORROSION ON SKIN/FITTING BTW 4 - 1 CLOCK POSITION, GOUGE ON SKIN BTW 7 - 10 CLOCK POS, GOUGE ON FITTING BTW 12 - 2 CLOCK POSITION ; HOLE #3 CORROSION ON SKIN BTW 9 - 4 CLOCK, CORROSION ON FITTING AT 10 CLOCK AND AT 6 CLOCK POS ; HOLE #4 CORROSION ON SKIN/FITTING BTW 9 - 5 CLOCK POS ; HOLE #5 CORROSION ON SKIN BTW 4 - 7 CLOCK POS AND BTW 8 - 10 CLOCK POS, SCRATCH ON 7 CLOCK POSITION ON SKIN/FITTING ; HOLE #6 CORROSION ON SKIN BTW 4 - 11 CLOCK POS, CORROSION ON FITTING BTW 4 - 6 CLOCK POS , SCRATCH ON SKIN/FITTING AT 11 CLOCK POS, SCRATCH ON SKIN/FITTING AT 10 CLOCK POS ; HOLE #7 CORROSION ON SKIN BTW 4 - 1 CLOCK POS , CORROSION ON FITTING BTW 4 - 11 CLOCK POS ; HOLE #8 CORROSION ON SKIN/FITTING ALL AROUND BORE HOLE ; HOLE #9 CORROSION ON SKIN BTW 11 - 1 CLOCK POSITION ; HOLE #10 CORROSION ON FITTING BTW 6 - 4 CLOCK POSITION (IN REF TASK CARD). CORRECTIVE ACTION: SUMMARY OF NRC00276 OPEN HOLES AT LH ENG DRAG FTG AS FOLLOW: HOLE #1, HOLE #2, HOLE #3, HOLE #4, HOLE #5, HOLE #6, HOLE #7, HOLE #8, HOLE #9 AND HOLE #10 WERE REPAIRED PER ER/A 594900-14AD REV:ORIGINAL; SECTION I: PERMANENT REPAIR AND ETI-57-21-509 REV 4. (1989604)

Part: NOT REPORTED — NOT REPORTED · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 594900-14. CORRECTIVE ACTION: REF ERA 594900-14. (1989145)

Part: NOT REPORTED — NOT REPORTED · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 594856-14. CORRECTIVE ACTION: REF ERA 594856-14. (1989156)

Part: NONE — NONE · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 DENT ON FUSELAGE SKIN BTW STA 480-500 BTW STRG 16L TO 17L (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00128: DENT ON FUSELAGE SKIN BTW STA 480-500 BTW STRG 16L TO 17L WAS EVALUATED IS WITHIN LIMITS PER ETI-57-21-510 REV 2 AND ERA 594520-14 REV ORIG. (1975389)

Part: NONE — NONE · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 LIFT SPRING DOES NOT HOLD THE GIRT BAR SLIDER OF THE R1 SLIDE EMERGENCY DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00001: NEW GIRT BAR OF R1 DOOR WAS INSTALLED PER B757-200 AMM 25-66. (1969555)

Part: NONE — NONE · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 INITIAL INSPECTION (A.A. 2560-01492-0201): MINIMUM ENGAGEMENT DIMENSION IS LESS THAN 0.37 INCH ON R2 SLIDE GIRT BAR. CORRECTIVE ACTION: SUMMARY OF NRC 00002: NEW GIRT BAR OF R2 DOOR WAS INSTALLED PER B757-200 AMM 25-66. (1969731)

Part: NONE — NONE · corrosion level 2 · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 CORROSION ON FITTINGS STA, 1400 AND 1420 AT DOOR LOWER SILL AREA AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00251 FITTINGS STA 1400 AND 1420 AT DOOR LOWER SILL AREA AFT CARGO COMPARTMENT WERE REPLACED PER B757-200 SRM. (1967688)

Part: NONE — NONE · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 CRACK ON FLOOR BEAM STABILIZATION STRAP BTW STA 365.25-377,7 AND APROX LBL 25 AT NLG LH TUNNEL.(E/E). CORRECTIVE ACTION: SUMMARY OF NRC 00082-FLOOR BEAM STABILIZATION STRAP BTW STA 365.25-377,7 AND APROX LBL 25 AT NLG LH TUNNEL, WAS REPAIRED PER B757-200 SRM. (1960455)

Part: NONE — NONE · airframe 79,304 hrs · 19,967 cycles

SHIP 6816 INITIAL INSPECTION (PER INSPECTION REQUEST): REMOVE ALL GIRT BARS ASSY FROM SLIDES OF R4, L1, L2, AND L4 TO CONFIRM THAT CORRECT P/N IS INSTALLED PER IPC IN REF. A.A. CORRECTIVE ACTION: SUMMARY OF NRC 00009 : ALL GIRT BARS ASSY FROM SLIDES OF R4, L1, L2, AND L4 WERE VERIFIED TO CONFIRM THAT CORRECT P/N IS INSTALLED PER IPC IN REF. A.A. 2560-01492-0201, AND ONLY L4 GIRT BAR ASSY MUST BE REPLACED UNDER NRC # 00296. (1957594)

Part: SIGN — DETACHED (L3 DOOR) · airframe 79,074 hrs · 19,919 cycles

SHIP 6816 3L DOOR EXIT SIGN FELL OFF. CORRECTIVE ACTION: SECURED DOOR EXIT SIGN. (7988207)

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 77,939 hrs · 19,673 cycles

SHIP 6816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:608. CORRECTIVE ACTION: LOC 608 SLIDE IND LIGHT OPS CKS OK. (1791607)

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 77,691 hrs · 19,614 cycles

SHIP 6816 L1 DOOR OUTSIDE EMERGENCY EXIT LIGHT INOP. CORRECTIVE ACTION: CLEANED CORROSION FROM SOCKET AND RE-LAMPED PER B757 AMM 33-51, OPS CHECK GOOD. (7427472)

Part: TRANSMITTER — MALFUNCTIONED (FLAP POSITION) · airframe 76,828 hrs · 19,422 cycles

SHIP 6816 - THE FLIGHT CREW DECLARED AN EMERGENCY WHILE ON APPROACH DUE TO A "TE FLAP DISAGREE" MESSAGE WHEN CHANGING FROM FLAPS 20 TO 25. THE FLAPS STAYED AT 20. COMPLIED WITH THE QRH AND USED ALTERNATE FLAPS. INITIAL CORRECTIVE ACTION: CONTRACT MAINTENANCE RAN THE FLAPS BOTH ELECTRICALLY AND HYDRAULICALLY. ALL CHECKS NORMAL AT EVENT STATION. FOLLOW UP CORRECTIVE ACTION: MAINTENANCE COMPLIED WITH NO GO PROGRAM. REPLACED FLAP POSITION TRANSMITTER. CHECKED TRANSMISSION FLUID & TORQUE INDICATORS. LUBRICATED FLAP TRANSMISSION AND CHECKED THE FLAP POSITION TRANSMITTERS ADJUSTMENT. VERIFIED NO BINDING IN DRIVE SYSTEM. OK FOR SERVICE. (LP #7621074)

Part: UNKNOWN — ODOR (CABIN) · airframe 75,272 hrs · 19,097 cycles

ON TAXI OUT WITH BOTH ENGINE RUNNING AND PACKS ON , FA REPORTED SMELL OF GASOLINE IN AFT OF CABIN. ON GATE RETURN, APU WAS USED FOR PACKS AND FOR PACKS AND SMELL WENT AWAY. TRIED EACH ENGINE INDIVIDUALLY AFTER THAT AND SMELL DID NOT RETURN.

Part: SLIDER — DEFECTIVE (GIRT BAR) · airframe 75,136 hrs · 19,069 cycles

4R DOOR DIFFICULT TO ARM. PERFORMED DVI OF DOOR 4 RT REF AMM 52-11, NO DISCREPANCIES NOTED. ARM/DISARM LEVER OPERATES SMOOTHLY. REMOVED AND REPLACED GIRT BAR SLIDERS REF AMM 25-66.

Part: LANYARD — OUT OF POSITION (R4 DOOR) · airframe 74,980 hrs · 19,035 cycles

ENTRY DOOR ARMING LEVER HARD TO OPERATE. FOUND 4R DOOR HARD TO ARM. REPOSITIONED LANYARD. NOW 4R DOOR ARMS / DISARMS NORMALLY IAW AMM 52-11.

Part: DOOR — FOD (R4) · airframe 74,957 hrs · 19,030 cycles

R4 DOOR WILL NOT ARM. FOUND DEBRIS IN DOOR AREA. REMOVED DEBRIS AND OPS CHECKED THE DOOR WAS OK IAW AMM 52-11.

Part: LIGHT — INOPERATIVE (SLIDE) · airframe 74,957 hrs · 19,030 cycles

SLIDE INDICATOR LIGHT INOPERATIVE. R & R IAW WDM 25-66-11.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 74,680 hrs · 18,970 cycles

SHIP 6816 R4 DOOR WILL NOT ARM PROPERLY RECYCLED DOOR SEVERAL TIMES. CORRECTIVE ACTION: FOUND FOD ON GIRT BAR ATTACHMENT. CLEARED FOD, OPS CHK NML. (6504380)

Part: SWITCH — NOT SEATED (R2 DOOR) · airframe 74,593 hrs · 18,950 cycles

(AIRCRAFT 6816, L/P 6504316) 2R DOOR SLIDE INDICATION INOP. CORRECTIVE ACTION: REMOVED AND RESEATED R2 DOOR "SLIDE" SWITCH (RESEATED).

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 73,779 hrs · 18,767 cycles

(AIRCRAFT 6816, L/P 6514694) 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: CLEARED OBSTRUCTION ON GIRT TRACK AS REQ'D.

Part: SENSOR — OBSTRUCTED (R1 DOOR SLIDE) · airframe 73,696 hrs · 18,748 cycles

PRIOR TO PUSHBACK, DOOR 1R SLIDE ARMED LIGHT WOULD NOT ILLUMINATE. REMOVED DEBRIS.

Part: LAMP — INOPERATIVE (ARMING LIGHT) · airframe 73,683 hrs · 18,745 cycles

1R DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE. RELAMPED 1R DOOR SLIDE PER B767 AMM CHP 33-51.

Part: LAMP — INOPERATIVE (GIRT BAR IND) · airframe 73,609 hrs · 18,732 cycles

(AIRCRAFT 6816, L/P 1405161) 1R DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOP. CORRECTIVE ACTION: CLEAR DEBRIS AT SENSOR AND RELAMP 1R DOOR SLIDE.

Part: ARMING LEVER — FOD (R4 DOOR) · airframe 73,243 hrs · 18,664 cycles

SHIP 6816 ARMING LEVER AT DOOR 4R DOES NOT COMPLETELY ENGAGE IN THE RED (ARMED) POSITION. CORRECTIVE ACTION: REMOVED DEBRIS FROM BENEATH GIRT / OPERATED ARM AND DISARM HANDLE WITH SUCCESSFUL LIGHT , ALONG WITH GIRTBAR ENGAGEMENT. (6349960)

Part: BEARING — WORN (PAX DOOR HINGE) · airframe 73,070 hrs · 18,629 cycles

SHIP 6816 UPPER AND LOWER DOOR HINGE BEARINGS SHOWING SIGNS OF WEAR. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 001 0148:2040 0191 1R 001 00364 REMOVED AND REINSTALLED R1 DOOR TO FOM PER B757 AMM 52 11. CARD COMPLETE ON AMDS. (1322824)

Part: SEAL — TORN (THRUST REVERSER) · airframe 73,070 hrs · 18,629 cycles

SHIP 6816 #2 ENGINE I/B T/R: UPPER FWD SECTION OF FIRE SEAL IS TORN. NOTE: JUST ABOVE FWD ENGINE MOUNT. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0233:2021-2122-02/018 00199 REPAIRED PER B757 AMM 78-31. (1323032)

Part: NONE — NONE · airframe 73,070 hrs · 18,629 cycles

(AIRCRAFT 6816, L/P 1321678) COMPLY WITH ERA 573400-14 REV B SECTION III. PERMANENT REPAIR. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE REPAIR REF ERA 573400-14 REV B SECTION III.

Part: BEARING — WORN (DOOR HINGE) · airframe 73,070 hrs · 18,629 cycles

SHIP 6816 UPPER AND LOWER DOOR HINGE BEARING SHOWING WEAR. CORRECTIVE ACTION: REMOVE AND REINSTALL R4 DOOR TO FOM PER B757 AMM 52-11-01. CARD COMPLETED ON AMDS CARD. (1321791)

Part: NONE — NONE (NONE) · airframe 73,070 hrs · 18,629 cycles

(AIRCRAFT 6816, L/P 1277371) REPLACE A SECTION OF FUSEALGE SKIN PANEL PER BOEING 757-200 SRM 53-30-01, REPAIR 2 TO ELIMINATE EXISTING REPAIR CORRECTIONS AND DTA REQUIREMENTS. ACCOMPLISH SECTION III OF ER/A 573400-14 REV. B AT NEXT C-CHECK OR WITHIN 60 DAYS WHICHEVER OCCURS FIRST. CORRECTIVE ACTION: C/W ERA 573400-14 REV B , ALL WORK DOCUMENTED ON NRC #154, LOGPAGE CREATED FOR REPETITIVE INSPECTION#1321306 AND LOG PAGE #1321678 CREATED FOR THE SRM AND SDR.

Part: ARMING LEVER — MALFUNCTIONED (DOOR) · airframe 72,821 hrs · 18,582 cycles

(AIRCRAFT 6816, L/P 1272533) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:603 / KNUCKLE KNOCKER IS NOTEXTENDED FULLY / INTERIOR. CYCLED ARMING LEVER SEVERAL TIMES KNUCKLE KNOCKER OPS NORMAL NOW.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 72,503 hrs · 18,523 cycles

R1 DOOR WILL NOT INDICATE PROPERLY WHEN IN ARM POSITION. FOUND DEBRIS IN GIRT BAR TRACK. CLEARED DEBRIS FROM TRACK, GIRT BAR ENGAGES & ARMED LIGHT ILLUMINATES.

Part: INDICATOR — OBSTRUCTED (L2 DOOR) · airframe 71,261 hrs · 18,295 cycles

(AIRCRAFT 6816, L/P 6284772) DOOR 2L KNUCKLE KNOCKER DOES NOT EXTEND WHEN DOOR IS ARMED. REMOVED DEBRIS FROM UPPER PART OF KNOCKER. OPS NML.

Part: TRACK — DIRTY (R2 DOOR) · airframe 70,749 hrs · 18,199 cycles

R2 DOOR WILL NOT CLOSE. REMOVED DEBRIS FROM 2R DOOR TRACK.B757 AMM 25-66.

Part: INDICATOR — DIRTY (DOOR) · airframe 70,344 hrs · 18,124 cycles

SHIP 6816 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:603. CORRECTIVE ACTION: CLEANED KNUCLE BUSTER. ARMED/DISARMED DOOR 10X OPS CHK NML. (0978647)

Part: INDICATOR — MALFUNCTIONED (DOOR) · airframe 70,330 hrs · 18,121 cycles

SHIP 6816 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:603. CORRECTIVE ACTION: OPERATED DOOR ARMED & DISARMED SLIDE , OPS CHK NML. (0978646)

Part: SKIN — DENTED (FUSELAGE) · airframe 69,252 hrs · 17,904 cycles

(AIRCRAFT 6816, L/P 0848093) ON PREFLIGHT, FOUND TWO DENTS IN AIRCRAFT FUSELAGE JUST FORWARD OF 2L DOOR. CORRECTIVE ACTION: FABRICATED DOUBLER AND PICKED UP FASTENER HOLES ON SKIN TO .189 PER PRI 573400-14, REV. 1. FINISHED DRILLING UP ALL DOUBLER AND COUNTERSUNK ALL HOLES. APPLIED PRIMER, SEAL AND INSTALLED DOUBLER PER ER/A 573400-14 REV ORIGINAL. OKAY TO RESTORE ACCESS. ACCESS RESTORED ON INTERIOR. REF: LP: 0845540 FOR FOLLOW UP ACTION. REPAIR COMPLETED PER ERA: 573400-14 REV A. EXTERIOR PAINT COMPLETED. REPAIR IDENTIFIED. JOB COMPLETE.

Part: FRAME — DAMAGED (BS 560) · airframe 69,252 hrs · 17,904 cycles

(AIRCRAFT 6816, L/P 0847507) STATION 560, DAMAGE TO FRAME AT SHEAR TIE ATTACH POINT AT STRINGER 16L. TIME LIMITED REPAIR ACCOMPLISHED PER ER/A 573441-14 REV ORIG. TIME STANDARDS ARE DRIVEN ON LOGS 0846705 AND 0846723. JOB COMPLETE RII INSPECTIONS COMPLETE.

Part: STRINGER — DAMAGED (BS 560) · airframe 69,252 hrs · 17,904 cycles

(AIRCRAFT 6816, L/P 0847499) STRINGER 16L IS DAMAGED 2" AFT OF FRAME 560 STA. CUT OUT DAMAGED STRINGER FROM BS546 -570.5. STARTED TO DRILL UP REPAIR PER PRI 573400-14 REV 1 (588392). FINISHED DRILLING UP STRINGER AND SPLICE PER PRI 573400-14 REV 1 (651509). INSTALLED STRINGER REPAIR PER PRI 573400-14 REV 1. STRINGER CLIP NEEDS TO BE INSTALLED AFTER SHEAR TIE REPAIR AT STA 560 IS COMPLETE. INSTALLED STRINGER CLIP; REPAIR COMPLETE PER ER/A 573400-14 REV O. RII COMPLETE.

Part: SHEAR TIE — DAMAGED (BS 560) · airframe 69,252 hrs · 17,904 cycles

(AIRCRAFT 6816, L/P 0847504) SHEAR TIE CLIP DAMAGED AT STATION 560 BETWEEN STRINGERS 15L & 16L. CORRECTIVE ACTION: TIME LIMITED REPAIR ACCOMPLISHED PER ER/A 573441-14 REV ORIG. TIME STANDARDS ARE DRIVEN ON LOGS 0846705 AND 0846723. JOB COMPLETE. RII INSPECTIONS COMPLETE.

Part: FRAME — DAMAGED (BS 580) · airframe 69,252 hrs · 17,904 cycles

(AIRCRAFT 6816, L/P 0847508) STATION 580, DAMAGE TO FRAME AT SHEAR TIE ATTACH POINT AT STRINGER 16L. TIME LIMITED REPAIR ACCOMPLISHED PER ER/A 573441-14 REV ORIG. CORRECTIVE ACTION: TIME STANDARDS ARE DRIVEN ON LOGS 0846705 AND 0846723. JOB COMPLETE RII INSPECTIONS COMPLETE.

Part: NONE — NONE (NONE) · airframe 73,070 hrs · 18,629 cycles

SHIP 6816 PER ERA 573400-14, SECTION II DTE IS REQUIRED ON THE FUSELAGE SKIN BETWEEN BS 560 & 587 AT STRINGER 16L. CORRECTIVE ACTION: C/W ERA 573400-14 REV B , ALL WORK DOCUMENTED ON NRC #154, LOG PAGE CREATED FOR REPETITIVE INSPECTION#1321306 AND LOG PAGE #1321678 CREATED FOR THE SRM AND SDR. (0845540)

Part: DOOR — OBSTRUCTED (R1) · airframe 68,892 hrs · 17,832 cycles

(AIRCRAFT 6816, L/P 4835240) 1R DOOR WONT ARM. REMOVED OBSTRUCTION FROM 1R DOOR, ACCOMPLISHED OPERATIONAL CHECK OF ARMING MECHANISM PER AMM 52-11, OKAY FOR SVC.

Part: INDICATOR — STICKS (DOOR) · airframe 68,753 hrs · 17,806 cycles

(AIRCRAFT 6816, L/P 0760468) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:DOO / DOOR ARMED KNUCKLE STICKS / INTERIOR. CLEARED DEBRIS AROUND OPENING- OP CKD OK.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 66,554 hrs · 17,400 cycles

AFTER THE ACFT WAS REPOSITIONED TO A REMOTE PAD, FOUND THE L1 DOOR SLIDE ASSY OFF MOUNT & STILL IN THE ARMED POSITION. REMOVED DOOR ASSIST BOTTLE & ESCAPE SLIDE PER B757 AMM 52-11 & WORKCARD 2566-9001-1L RESPECTIVELY. OK TO INSTALL IAW AMM 52-11 & WORKCARD 2566-900-1L. INSTALLED DOOR ASSIST BOTTLE & ESCAPE SLIDE. INSPECTED COMPLIED WITH IAW AMM 52-11 & AMDS WORKCARD 2566-900-1L.

Part: DOOR — DIRTY (R2) · airframe 66,544 hrs · 17,398 cycles

R2 DOOR WILL NOT DISARM. CLEARED DEBRIS FROM THE DOOR.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 65,470 hrs · 17,176 cycles

EMERGENCY EXIT LIGHT LENS UNSECURE. SECURED THE LENS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,874 hrs · 17,053 cycles

GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY FUSE IAW AMM 33-51-07. PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-00.

Part: SENSOR — OUT OF ADJUST (AFT PAX DOOR) · airframe 64,873 hrs · 17,052 cycles

LEFT AFT ENTRY DOOR UNSAFE INDICATION ON EICAS. ADJUSTED THE DOOR SENSOR IAW AMM 52-71-00. PRESSURIZED THE AIRCRAFT TO 7 PSI WITH NO INDICATION OF AN UNSAFE DOOR, NO FURTHER ACTION REQUIRED.

Part: SNUBBER — FAILED (R4 DOOR) · airframe 64,870 hrs · 17,049 cycles

R4 DOOR SNUBBER FAILED SERVICING INSPECTION. REMOVED AND REPLACED R4 DOOR SNUBBER. ADJUSTMENT /OPS CHECK PERFORMED ON AMDS CARD.

Part: FRAME — GOUGED (BS 1280) · airframe 64,869 hrs · 17,048 cycles

MAIN CABIN FRAME BS 1280, STRINGERS 10L TO 14L HAD SEVERAL GOUGED SPOTS. REPAIRED THE FRAME IAW ERA 556461-14AD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 64,869 hrs · 17,048 cycles

AFT CARGO COMP BS 1375-1380 BETWEEN STRINGERS 26 RT 27 RT INTERCOSTAL HAS CORROSION. FABRICATED NEW DIM 24"X 6" AND INSTALLED INTERCOSTAL IAW SRM 51-40-02 AND DWG 146N5212 REV - , 146N5213 REV - AND 146N5412 REV A.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 64,869 hrs · 17,048 cycles

SURFACE CORROSION FOUND AROUND NUT PLATE HOLES AT THE UPPER AND LOWER SURFACES OF THE CABIN FLOORBEAM, BS 365, BL 0 TO RBL 60. REMOVED THE CORROSION AND FOUND OUT OF ALLOWABLE LIMITS IAW SRM. REPAIRED THE FLOORBEAM IAW ERA 481634-14MA, REV A.

Part: CUSP WEB — CORRODED (BS 1349) · airframe 64,869 hrs · 17,048 cycles

AFT CARGO BAY BS 1349 RT LOWER CUSP WEB HAS CORROSION. REMOVED THE CORROSION AND EVALUATED THE CUSP WEB, FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-60-13. CUT OUT THE DAMAGED SECTION AND REPAIRED IAW SRM 51-70-13 FIG 1.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 64,869 hrs · 17,048 cycles

AFT CARGO BAY, BS 1510, LBL 2.9 FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-10-02,

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 61,027 hrs · 16,320 cycles

2R DOOR WONT ARM. CLEANED DEBRIS FROM GIRT BAR FITTING. OPS CK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 60,465 hrs · 16,211 cycles

EMERGENCY LIGHT LENS MISSING AT ROW 3 RIGHT OVERHEAD BIN. LIGHT OPS OK. INSTALLED A NEW LENS, OPS & SECURITY CHECKED OK, IAW AMM 33-51.

Part: SIGN — UNSECURE (CABIN) · airframe 59,183 hrs · 15,990 cycles

THE EXIT SIGN ABOVE THE 2L DOOR HAS FALLEN OFF. REINSTALLED EXIT SIGN ABOVE 2L DOOR.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 58,988 hrs · 15,954 cycles

EXIT SIGN FELL OFF BY DOOR 2L. REATTACHED EXIT LIGHT 2L DOOR.

Part: MOUNT — OUT OF POSITION (NR 1 ENGINE) · airframe 56,496 hrs · 15,436 cycles

FOUND NR 1 ENGINE FWD ENGINE MOUNT-TO- PYLON INSPECTION ARE NO GAPS BETWEEN THE STRUT FITTING AND ENGINE MOUNT ASSY, BUT THE TORQUE STRIP ON 1 OR MORE BOLTS WERE CRACKED. THE FWD ENGINE MOUNT BOLTS AND ASSOCIATED HARDWARE MUST BE REPLACED PRIOR TO FURTHER FLIGHT IAW THIS ORIGINATING CARD STEP 4 B. MAINTENANCE MUST CONTACT PLANNING TO ADD FORECAST NR 56-0571 -8-0011, WC 7121-01026-02C-01. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 066-0001: 7121-01026-01C-01/001-00146 ACCOMPLISHED AMDS WC 7121-01026-02C-01. REPLACED FWD ENGINE MOUNT BOLTS.

Part: FASTENER — LOOSE (NOT REPORTED) · airframe 56,496 hrs · 15,436 cycles

MISSING, LOOSE, CORRODED FASTENERS, SEEM JUST FORWARD OF LT & RT PAC BAYS. MARKED. REPLACED AND SECURED FASTENERS IAW SRM 51-10-02.

Part: SKIN — DENTED (NR 10 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 10 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 10 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST CW ON R/C 56-0557-8- 0072. NR 10 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED I/D TAG ON SLAT DAMAGED AREA.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 1 SLAT HAS NUMEROUS UNIDENTIFIED DENTS, SLAT UPPER T/E WEDGE. INSPECTED NR 1 SLAT FOUND NUMEROUS DENTS, ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON RC 56-0557-8-0072 . NR 1 SLAT NEEDS TO BE ADDED TO MONITOR INSP. INSTALLED I/D TAG ON NR 1 SLAT DAMAGED AREA.

Part: SKIN — DENTED (NR 8 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 8 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 8 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 8 SLAT NEEDS TO ADDED TO MONITOR INSPECTION, INSTALLED TAG ON SLAT DAMAGE AREA.

Part: SKIN — DENTED (NR 6 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 6 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 6 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 6 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION. INSTALLED ID TAG ON SLAT DAMAGED AREA.

Part: SKIN — DAMAGED (NR 2 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 2 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 2 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON RC 56-0557-8-0072. NR 2 SLAT NEEDS TO BE ADDED TO MONTOR INSPECTION INSTALLED ID TAG ON NR 2 SLAT DAMAGED AREA.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 5 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 5 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 5 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED I/D TAG ON SLAT DAMAGED AREA.

Part: SKIN — DENTED (NR 9 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 9 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 9 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 9 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED ID TAG ON SLAT DAMAGED AREA.

Part: SKIN — DENTED (NR 3 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 3 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 3 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072 . NR 3 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION. INSTALLED ID TAG ON NR 3 SLAT DAMAGED AREA.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 4 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER TE WEDGE. INSPECTED NR 4 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 4 SLAT NEEDS TO BE ADDED TO MONTOR INSPECTION. INSTALLED ID TAG ON NR 4 SLAT DAMAGED AREA.

Part: SKIN — DENTED (NR 7 SLAT) · airframe 56,496 hrs · 15,436 cycles

NR 7 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER TE WEDGE. INSPECTED NR 7 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 7 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED ID TAG ON SLAT DAMAGED AREA.

Part: LIGHT — UNSECURE (SEAT 18D) · airframe 55,970 hrs · 15,334 cycles

EMERGENCY AISLE LIGHT FIXTURE IS LOOSE/STICKING OUT AT SEAT 18D. RESECURED BRACKET. OPS NORMAL.

Part: INTERCOSTAL — MISSING (BS 395-418) · airframe 52,487 hrs · 14,649 cycles

OVERHEAD BIN INTERCOSTAL MISSING BS 395-418, STR 6L. INSTALLED REPLACEMENT INTERCOSTAL IAW B/E DN-B223240-001-001-03.

Part: SKIN — DENTED (BS 620) · airframe 52,487 hrs · 14,649 cycles

DENT ON FUSELAGE SKIN BS 620 BETWEEN STRINGERS 15 - 16L. FOUND DENT TO BE OUT OF LIMITS. CUT OUT AREA, FABRICATED REPAIR, AND INSTALLED IAW SRM AND ERA 530465-14, REV O.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 47,440 hrs · 13,646 cycles

SEAT ROW 41 RT SIDE EMERGENCY LIGHT CONNECTOR FROM SIDEWALL TO SEAT BROKEN. REPLACED CONTACT SOCKETS IAW SWPM 20-60. OPS CHECKED GOOD, OK FOR SERVICE.

Part: FRAME — DENTED (BS 231.25) · airframe 43,701 hrs · 12,906 cycles

BS 231.25 FRAME AT BL 0 DENTED.

Part: FRAME — DENTED (BS 540) · airframe 43,690 hrs · 12,903 cycles

BS 540 FRAME BETWEEN STRINGERS 24L AND 25L DENTED.

Part: SKIN — DENTED (BS 1590 S15L) · airframe 43,527 hrs · 12,871 cycles

DENT WAS FOUND ON THE FUSELAGE SKIN, SKIN PANEL AT STA1590, BELOW S15L. THE DENT DIMENSIONS ARE 1.75- DIA X 0.045- D. THE DENT WAS FREE FROM OIL CANNING, GOUGE AND LOOSE OR PULLED FASTENER. REPAIR WAS ACCOMPLISHED BY ERA 496643-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN SEAT TRACK GOUGED AND CORRODED ON CROWN & INSIDE STA 700-780 LBL 45.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN CUSP WEB CORRODED STA 1180-1200 LT. COMPLIED WITH ERA 497740-14 REV A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN SEAT TRACK CORRODED AND GOUGED ALL AREAS STA 1540-1640 RBL 24. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM STA 1540-1640 RBL 24 IAW B757 SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

FWD CARGO FRAME DENTED 2 PLACES STA 540 BETWEEN STR 24 AND 25L. SUBMITTED TO ENGINEERING AT SAA/SAT AND DOCUMENTED ON N/R 184385 W/O 89268380001. DURING HMV.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN SEAT TRACK CORRODED AND GOUGED ALL AREAS STA 1540-1640 LBL 45. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM 1540-1640 LBL 45 IAW B 757 SRM 51-40-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN FLOOR RT INNER CUSP CHORD CORRODED STA 700-757. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED RT CUSP CHORD STA 665-757 IAW B757 SRM 51-40-02.

Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

FWD ACCESSORY COMPARTMENT DOOR CUTOUT FWD SIDE STA 231 BL 0 FRAME TOP FLANGE, HAS DENT 77-46. MAPPED AND SUBMITTED TO ENGINEERING. DOCUMENTED ON N/R 186965 W/O 89267760001 AT SAA/SAT DURING HMV.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN FLOORBEAM HAS EXISTING SCRIBE LINE, HOLES WITH NO ED AND CORROSION STA 1640 RBL 60 LBL 60.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABN LT INNER CUSP CHORD CORRODED STA 377. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED INNER CUSP CHORD STA 377 LT IAW B757 SRM 51-40-02.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN SEAT TRACK GOUGED AND CORRODED ALL AREAS STA 1540-1640 RBL 45. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM 1540-1640 RBL 45 IAW B757 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN SEAT TRACK CORRODED AND GOUGED ALL AREAS STA STA 1540-1640 LBL 24. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM STA 1540-1640 LBL 24 IAW B757 SRM 51-40-02 PG 4.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

MAIN CABIN FLOOR RT INNER CUSP CHORD CORRODED STA 324-377.

Part: SKIN — CRACKED (L4 DOOR) · airframe 39,366 hrs · 12,038 cycles

L-4 DOOR INNER SKIN CRACKED/PUNCTURED JUST ABOVE ARM/DISARM BOX. COMPLIED WITH ERA 496637-14 REV ORG DURING HMV.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

ACCOMPLISH REPAIR PER ERA 468701-14 REV B "PERM RPR FUSELAGE SKIN AT FS 580/RT FWD RADIO ALTIMTER ANTENNA DENT. COMPLIED WITH ERA 496649-14 REV ORG.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

DENT ON FUSELAGE SKIN BETWEEN STA 580-600 BELOW STR 17L / MEASURED DENT, FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-01. COMPLIED WITH ERA 496642-14 REV ORG DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

DENT ON FUSELAGE SKIN AT ST 1590 BELOW STR 15L / MEASURED DENT, FOUND TO BE OUT OF LIMITS PER B757 53-00-01. COMPLIED WITH ERA 492243-14 REV ORG DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

DENT ON FUSELAGE SKIN AT STA 1648 BETWEEN STR 25L-26L / MEASURED DENT, FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-01. COMPLIED WITH ERA 496645-14 REV A DURING HMV.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,366 hrs · 12,038 cycles

DENT ON FUSELAGE SKIN AT STA 712 BETWEEN STR 18L AND 19L / MEASURED DENT FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-01. COMPLIED WITH ERA 496647-14 REV ORG DURING HMV.

Part: OVEN — DIRTY (FWD GALLEY) · airframe 30,429 hrs · 10,311 cycles

FIRST CLASS NR1 OVEN PRODUCED SMOKE IN FLIGHT. MX DEACTIVATED OVEN AND FORWARDED TO NEF ITEM.

Part: CIRCUIT BREAKER — POPPED · airframe 26,354 hrs · 9,485 cycles

APU DOOR STATUS MSG AFTER APU SHUTDOWN. RETURN TO GATE. FOUND APU BATT C/B POPPED. RESET SAME DOOR, OPN NOW NORMAL.

Part: SHUTOFF VALVE — FOD (FUEL SYSTEM) · airframe 26,196 hrs · 9,438 cycles

DURING PREFLT FOR FUEL CONTROL CHANGE HAD LOW AIR FROM NR 1 ENG AFTER REMOVING HPSOV FOUND METAL STRIPS INSIDE VALVE. CONSULTED ENGINE SHOP AND DETERMINED TO BE AIRSEAL FROM 12TH TO 13 STG COMPRESSOR SECTION. REPLACED NR 1 ENGINE PER TRANS 6T103.

Part: LIGHT — INOPERATIVE (EXTERIOR)

SEA - EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CABLE — DISCONNECTED (EMERGENCY LIGHT)

EMERGENCY FLOOR LIGHTING SYSTEM PLASTIC COVER BROKEN AND LIGHTING TRACK PULLED OUT AT ROW 12. REPLACED CONDUCTOR CABLE FROM ROW 7 TO ROW 16 FOR EMERGENCY FLOOR TRACK LIGHTING. ALSO REPLACED LIGHT ELEMENT AND SECURED COVER FOR EMERGENCY LIGHT AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,866 hrs · 4,340 cycles

THE FIRST CLASS CABIN EGRESS FLOOR LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND CABLE PN 6664-9.

Part: CARBON SEAL — FAILED (NR 1 & 2 ENGINE) · airframe 8,675 hrs · 2,765 cycles

JUST AFTER TAKEOFF SMOKE WAS REPORTED IN CABIN. FLIGHT RETURNED TO STL. FOUND THE NUMBER 2 AND 3 BEARING CARBON SEAL ASSEMBLY ON BOTH ENGINES HAD FAILED. THE AIRCRAFT WAS FERRIED TO ANOTHER STATION FOR REPLACEMENT OF THE CARBON SEAL ASSEMBLIES ON BOTH ENGINES. SERIAL NUMBER ON THE SECOND ENGINE WAS 4949, HOURS AND CYCLES THE SAME AS FIRST ENGINE.

Part: SMOKE — DETECTED (CABIN) · airframe 8,673 hrs · 2,763 cycles

SMOKE REPORTED IN CABIN RIGHT AFTER TAKEOFF. ACCOMPLISHED PACK BURN OUT, CHECKED L/E WING DUCTING, CHECKED MID CABIN BALLAST WIRING AND RESULTS NEGATIVE. INDICATIONS CAUSED SUSPICION OF CONDENSATION.

Part: FAN — FAILED (CABIN) · airframe 8,640 hrs · 2,751 cycles

IN CLIMB SMOKE APPEARED IN THE CABIN. FLIGHT RETURNED TO STL. CHANGED THE RT RECIRCULATION FAN, P/N 606772-3, AND BOTH RECIRC FILTERS, P/N P196555. ALSO ACCOMPLISHED CHECKS OF FAN CONNECTORS AND WIRING. PERFORMED TEST FLIGHT TO CONFIRM CORRECTIONS.

Part: FAN — FAILED (CABIN) · airframe 8,639 hrs · 2,750 cycles

SMOKE WAS REPORTED IN AIRCRAFT. FLIGHT RETURNED TO STL. CHANGED THE LT RECIRCULATION FAN 606772-3. ALSO ACCOMPLISHED PRECAUTIONARY CHECKS OF SYSTEM AND WIRING, RESULTS NEGATIVE.

Part: O-RING — WORN (RT WING) · airframe 3,992 hrs · 1,351 cycles

FUEL WAS LEAKING FROM THE RIGHT WING. FLIGHT RETURNED TO STL. REPLACED THE O-RING AT THE FUEL OVERFILL SENSOR. NO CHECK-C.

Part: FUEL CELL — LEAKING (RT WING) · airframe 3,991 hrs · 1,350 cycles

FUEL WAS REPORTED LEAKING FROM THE RIGHT WING. FLIGHT RETURNED TO STL. LEAK CHECKED ENTIRE AREA AND UNABLE TO FIND ANY LEAK. NO CHECK-C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,350 hrs · 795 cycles

DURING ROUTINE INSPECTION, FOUND L2 DOOR EMERGENCY LIGHT INOP. RELAMPED. 0004 4-28-00 JFK.