N717TW

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 91,056 hrs · 22,550 cycles

SHIP 6812 DURING SVC CHECK FOUND EMERGENCY LIGHTS @ 19-26ABC INOP. CORRECTIVE ACTION: R/R M733 BATTERY PACK AT L2 DOOR REF B757 AMM 33-51. OPS CHECK GOOD. (6689198)

Part: SKIN — DENTED (ZONE 800) · airframe 93,503 hrs · 23,237 cycles

RAMP REPORTED A DENT ON FWD CARGO DOOR OUTER SKIN. REPAIRED PREVIOUSLY REPORTED DENT IAW SRM 52-30-01-212- 4. REPAIR IS CATEGORY B. (5447494)

Part: SWITCH — INOPERATIVE (SLIDE LIGHT) · airframe 89,607 hrs · 22,163 cycles

SHIP 6812 DOOR 2L SLIDE CAUTION INOP. CORRECTIVE ACTION: R/R 2L SLIDE LIGHT SWITCH PER 757 AMM 33-00. OPS OK. (6148912)

Part: CONTROL PANEL — BROKEN (EMERGENCY LIGHTS) · airframe 89,535 hrs · 22,142 cycles

SHIP 6812 EMER LIGHTS UNARMED LIGHT ASSY BROKEN. CORRECTIVE ACTION: R/R EMER LIGHT O/H PNL. CKS GOOD. B757 AMM 33-51. (5612470)

Part: INDICATOR — NONE (DOOR SLIDE) · airframe 89,324 hrs · 22,094 cycles

SHIP 6812 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:608. CORRECTIVE ACTION: ALL OPS NML. NTF. (0394493)

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 88,247 hrs · 21,880 cycles

SHIP 6812 PLASTIC COVER FOR EMERGENCY EXIT SIGN OVER DOOR 2L CAME OFF. CORRECTIVE ACTION: REATTACHED EXIT EMERGENCY COVER PERR B757 AMM 33-51 OK FOR SVC (5739688)

Part: SIGN — DETACHED (CABIN) · airframe 88,171 hrs · 21,860 cycles

SHIP 6812 EMERGENCY EXIT SIGN AT 2R FELL DOWN 2ND WRITEUP TODAY. CORRECTIVE ACTION: RE INSTALLED IAW B757 AMM 33-51 NOW SECURE. (5739652)

Part: SIGN — DETACHED (CAIBN) · airframe 88,171 hrs · 21,860 cycles

SHIP 6812 EXIT SIGN FELL OFF DOOR R2. CORRECTIVE ACTION: REATTACHED EXIT SIGN IAW 33-51 IN B757 AMM. (5739650)

Part: ACTUATOR — TRIPPED (LE SLAT SYS) · airframe 88,110 hrs · 21,843 cycles

SHIP 6812 -FCNT/DE- LE SLAT DISAGREE ON APPROACH. CORRECTIVE ACTION: T/S REPLACED ROTARY ACTUATORS, PERFORMED LUBE, OPS / ADJ SATISFACTORY.

Part: TRANSMITTER — MALFUNCTIONED (LE SLAT SYS) · airframe 88,101 hrs · 21,841 cycles

SHIP 6812 -ATB/FCNT/DE- LE SLAT DISAGREE AFTER TAKEOFF. CORRECTIVE ACTION: RIG CK OF LAT PDU MODULE C/W. REPLACE BOTH TRANSMITTERS AS PER MD LOG. REMOVED AND REPLACED FLAP/SLAT VALVE DUE TO LEAKING. PERFORMED FLAP AND SLAT LUBE.

Part: SLAT SYSTEM — LACK OF LUBE · airframe 88,100 hrs · 21,840 cycles

SHIP 6812 -FCNT/DE- LE SLAT DISAGREE MESSAGE. CORRECTIVE ACTION: T/S PER FIM. PERFORMED SLAT LUBE. SLATS OPERATE NORMAL.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 87,895 hrs · 21,780 cycles

SHIP 6812 EMERGENCY EXIT LIGHT COVER OVER L2 BOARDING DOOR FELL OFF AFTER CLOSING THE DOOR. CORRECTIVE ACTION: RESECURED EXIT LIGHT COVER AS REQUIRED. (5373196)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,657 hrs · 21,723 cycles

SHIP 6812 OBSERVED ROWS 1-4 SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION: REMOVED AND REPLACED M731 CHARGER. INSTALLED NEW BATTERY PER B757 AMM 33-51. T/S PER B757 WDM 33-51-21. FOUND CONNECTOR D9333P DISCONNECTED FROM J1. RECONNECTED AND PERFORMED CONTINUITY CHK. OPS CHK GOOD. (4287078)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,351 hrs · 21,647 cycles

SHIP 6812 SCRATCH ON RH HORIZONTAL STABILIZER UPPER SKIN BTW. STAB STA. 115 TO 128 AND NEXT TO 20.IN OF STAB. LEADING EDGE. CORRECTIVE ACTION: SUMMARY OF NRC 00043: SCRATCH ON RH HORIZONTAL STABILIZAER UPPER SKIN WAS REPAIRED PRI 613818-14. (0077844)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,351 hrs · 21,647 cycles

SHIP 6812 LEAF SPRING ON AFT SLIDERS DOES NOT RETAINS THE SLIDER AT L1 DOOR. SUMMARY OF NRC 00029: LEAF SPRINGS FROM GIRT BAR WERE REPLACED PER BOEING CMM 25-66-14. (0077466)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,336 hrs · 21,640 cycles

SHIP 6812 DISBOND WAS FOUND ON LE SLAT 5 TRAILING EDGE WEDGE UPPER SKIN ISS 106.3+14.5 APPROX. OF 1.500IN LENGTH AND 0.813IN WIDTH, IN REF. TASK CARD 5740-01145-05E JOB#114-0001. CORRECTIVE ACTION: SUMMARY OF NRC 00055: DISBOND ON LE SLAT 5 TRAILING EDGE WEDGE UPPER SKIN ISS 106.3+14.5 APPROX. OF 1.500IN LENGTH AND 0.813IN WIDTH WAS REPAIRED PER BOEING 757-200 S.R.M. 51-70. (0067959)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,336 hrs · 21,640 cycles

SHIP 6812 AD - A.A. DISBOND WAS FOUND ON LE SLAT 8 TRAILING EDGE WEDGE UPPER SKIN OSS 438.1 OF 8.687IN LENGTH AND 3.875IN WIDTH. CORRECTIVE ACTION: SUMMARY OF NRC 00056: DISBOND FOUND ON LE SLAT 8 TRAILING EDGE WEDGE UPPER SKIN OSS 438.1 OF 8.687IN LENGTH AND 3.875IN WAS REPAIRED PER B757-200 S.R.M. 51-70. (0068220)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,336 hrs · 21,640 cycles

SHIP 6812 DENT ON FUSELAGE SKIN ON BS 705 BTW STRINGERS 25LH & 26LH SIDE. CORRECTIVE ACTION: THE DENT WAS EVALUATED AND FOUND OUT OF LIMITS. SUMMARY OF NRC 00033: DENT ON FUSELAGE SKIN ON BS 705 BTW STRINGERS 25LH & 26LH SIDE WAS REPAIRED PER ERA 613647-14. (0066803)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,336 hrs · 21,640 cycles

SHIP 6812 CRACKED STABILIZER STRAP STA 377 LBL AT NLG TUNNEL INTERNAL AREA THROUGH ACCESS 119BL. CORRECTIVE ACTION: SUMMARY OF NRC 00119: STABILIZER STRAP STA 377 LBL AT NLG TUNNEL INTERNAL AREA THROUGH ACCESS 119BL. WAS REPAIRED PER ERA 384483-14MA. (0063308)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,742 hrs · 21,502 cycles

SHIP 6812 FOUND AFT EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION REMOVED AND REPLACED EMERGENCY BATTERY M734 PER B757 AMM 33-51. REPAIR & RESECURE WIRES. OPS CHECK GOOD. (4614412)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,723 hrs · 21,498 cycles

SHIP 6812 EXIT SIGN AT 2R DOOR FELL OFF. CORRECTIVE ACTION: RESECURED EXIT SIGN AT 2R DOOR OK FOR SVC. (4614408)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,493 hrs · 21,447 cycles

SHIP 6812 EMERGENCY SEAT MOUNTED LIGHTNING DAMAGED / INOPERATIVE / LOCATIONS:21D. CORRECTIVE ACTION: RESECURED LIGHT AS NECESSARY. OPS CHK GOOD, PER B757 AMM 33-51. A/C FOR SVC. (2926476)

Part: GIRT BAR — DIRTY · airframe 82,290 hrs · 20,483 cycles

SHIP 6812 4R DOOR WOULD NOT ARM FOR DEPARTURE. CORRECTIVE ACTION: RE-SECURED 4R GIRT BAR AND CLEANED FITTINGS. (9264100)

Part: NONE — NONE · airframe 81,735 hrs · 20,352 cycles

SHIP 6812 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT AT 2R INOP. CORRECTIVE ACTION: REMOVED AND REPLACED 2R DOOR SLIDE ARM LIGHT ASSMBLY IAW B757 AMM 25-66. OPS CHK GOOD. (2180824)

Part: NONE — NONE · airframe 80,707 hrs · 20,121 cycles

SHIP 6812 GOUGE AT LWR EXTERNAL FUSELAGE SKIN, STA. 1400-1420, BTW S-30 AND S-29R. CORRECTIVE ACTION: SUMMARY OF NRC 00023: GOUGE AT LWR EXTERNAL FUSELAGE SKIN, STA.1400-1420, BTW S-30 AND S-29R WAS REPAIR PER ETI-57-21-566 REV. 2 AND ER/A 595654-14 REV. ORIGINAL. (2032566)

Part: NONE — NONE · airframe 80,705 hrs · 20,120 cycles

SHIP 6812 INITIAL INSPECTION: OUT OF LIMITS ROTARY SNUBBER PIN EXTENSION AT 1L DOOR OF CABIN PAX IN REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00147 AT 1L DOOR ROTARY SNUBBER WAS REMOVED PER B757-200 AMM 52-11 AND SERVICEABLE ROTARY SNUBBER WAS INSTALLED PER B757-200 AMM 52-11. (2030648)

Part: NONE — NONE · airframe 80,705 hrs · 20,120 cycles

SHIP 6812 INITIAL INSPECTION: OUT OF LIMITS ROTARY SNUBBER PIN EXTENSION AT 4L DOOR OF CABIN PAX IN REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC:148 ROTARY SNUBBER WAS REMOVED PER B757-200 AMM 52-11 AND WAS INSTALLED SERVICEABLE ROTARY SNUBBER PER B757-200 AMM 52-11. (2030643)

Part: NONE — NONE · airframe 80,705 hrs · 20,120 cycles

SHIP 6812 INITIAL INSPECTION (A.A. 2560-01492-0201): INCORRECT P/N ASSY ON GIRT BAR INSTALLED ON L4 SLIDE IN REF. A.A. WORKCARD. CORRECTIVE ACTION: SUMMARY OF NRC 00053: GIRT BAR L4 DOOR WAS REPLACED PER B757-200 AMM 25-66. (2027181)

Part: NONE — NONE · airframe 80,705 hrs · 20,120 cycles

SHIP 6812 INITIAL INSPECTION (A.A. 2560-01492-0201): SPRING ON L2 DOOR GIRT BAR DOES NOT RETAIN THE SLIDER. CORRECTIVE ACTION: SUMMARY OF NRC 00037: L2 DOOR GIRT BAR WAS REPLACED PER B757-200 AMM 25-66. (2026957)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 80,067 hrs · 19,982 cycles

SHIP 6812 OXYGEN PANEL MASK DEPLOYED / LOCATIONS:201. CORRECTIVE ACTION: RE-STOWED OXYGEN MASK ON THE FWD F/C LAVATORY, IN REF B757 AMM 35-21. (1946887)

Part: NONE — NONE · airframe 80,705 hrs · 20,120 cycles

SHIP 6812 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 582894-14 REV A. CORRECTIVE ACTION: REF ERA 582894-14 REV A. (1931107)

Part: NONE — NONE · airframe 80,705 hrs · 20,120 cycles

SHIP 6812 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 582897-14 REV A. CORRECTIVE ACTION: REF ERA 582897-14 REV A.

Part: UNKNOWN — ODOR (CABIN) · airframe 79,783 hrs · 19,921 cycles

SHIP 6812- SMOKE/DIV- TO LAX DUE TO LEFT ENGINE HIGH OIL TEMPERATURE FOLLOWED BY SMOKE IN THE CABIN. CORRECTIVE ACTION: FOUND GEARBOX FULL OF OIL. R/R NBR 1 ENGINE LUBE SCAVENGE OIL PUMP AND ENGINE GEARBOX OIL SCAVENGE PUMP ASSY PER PW 2000 EM 72-00 AND AMM 79-21. IDLE LEAK CHECK GOOD. C/W ODI CHECKLIST PER AMDS CARD. REPLACED L&R RECIRC FILTERS IAW B757 AMM 21-58.

Part: LIGHT — INOPERATIVE (SEAT 36 FED) · airframe 78,823 hrs · 19,722 cycles

SHIP 6812 ROW 36 FED FOUND RED EMERGENCY SEAT LIGHT INOP. CORRECTIVE ACTION: R/R RED EMERGENCY SEAT LIGHT PER CMM 25-21-52 B757. (7606737)

Part: WIRE — DAMAGED (NR 1 FSEU) · airframe 77,603 hrs · 19,444 cycles

THE FLIGHT CREW DECLARED AN EMERGENCY FOR LANDING AT SLC DUE TO A "LE FLAP ASSYM" EICAS MESSAGE AND LEADING EDGE DISAGREE LIGHT DURING CLIMB AT FL210 AND 300 KTS. NO ROLL OR FLIGHT CONTROL PROBLEMS. THE QRH WAS COMPLIED WITH AND THE LANDING IN SLC WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE FSEU-1 FAULTS THE RIGHT SLAT TRANSMIT WIRE (CODE 323). THE FSEU-1 WAS REPLACED, PER B757 AMM 27-51. ALSO FOUND BROKEN WIRES AT PINS 6 AND 7 OF CONNECTOR D40404P. THAT CONNECTOR WAS REPLACED, PER ESPM 20- 61-11. SYSTEM CHECKS WERE GOOD. VERIFIED FLAPS AND SLATS OPERATED NORMALLY WITHOUT ANY FAULT MESSAGES. AIRCRAFT IS OK FOR SERVICE.

Part: CONNECTOR — FAILED (TE FLAP SYSTEM) · airframe 77,603 hrs · 19,444 cycles

THE FLIGHT CREW DECLARED AN EMERGENCY FOR LANDING AT SLC DUE TO A "LE FLAP ASSYM" EICAS MESSAGE AND LEADING EDGE LIGHT WHEN APPROACHING CRUISE ALTITUDE OF FL300. NO OTHER FLIGHT CONTROL ISSUES NOTED. COMPLIED WITH THE QRH AND LANDED UNEVENTFULLY. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE PLUG D41654J PIN 12 HAD FAILED AND REPLACED THE PLUG, PER BOEING SWPM 20-61-11. VERIFIED FLAPS AND SLATS OPERATED NORMALLY WITHOUT ANY FAULTS. OK FOR SERVICE.

Part: TRANSMITTER — MALFUNCTIONED (LE FLAPS) · airframe 77,608 hrs · 19,447 cycles

DURING THE CLIMB, WHEN PASSING FL220 AND AT 300 KTS, THE CREW NOTICED THE "LE FLAP ASYM" EICAS MESSAGE ALONG WITH THE "LEADING EDGE" LIGHT. THE QRH WAS COMPLIED WITH AND A VISUAL INSPECTION REVEALED BOTH OF THE SLATS WERE UP. THE FLIGHT CONTINUED TO AN UNEVENTFUL SCHEDULED LANDING. CORRECTIVE ACTION: MAINTENANCE FOUND HIGH ELECTRICAL RESISTANCE IN SOME CONNECTIONS AND REPLACED THE SLAT POSITION TRANSMITTER. OPERATIONAL CHECK WAS GOOD, PER B757 AMM 27-51.

Part: TRANSMITTER — MALFUNCTIONED (RT SLAT SYSTEM) · airframe 77,382 hrs · 19,393 cycles

THE CREW HAS DECLARED AN EMERGENCY DUE TO AN EICAS MESSAGE ILLUMINATING FOR LEADING EDGE SLAT ASYMMETRY WHILE ON FINAL APPROACH. FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE RIGHT SLAT POSITION TRANSMITTER, PER B757 AMM 27-88. FUNCTIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,392 hrs · 19,183 cycles

EMERGENCY LIGHTS AT L3, R3 AND CENTER AISLE SIGN, SEATS 27-35 ARE INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY ABOVE 36ABC (M735), BATTERY AND CHARGER AT 35 DEF M10699) SYSTEM OPERATION IS NORMAL.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR SLIDE) · airframe 74,643 hrs · 18,835 cycles

(AIRCRAFT 6812, L/P 1371658) R4 DOOR WILL NOT ARM. CORRECTIVE ACTION: GIRT BAR MECHANISM ADJUSTMENT WAS PERFORMED PER B757-200 AMM 52-11-25-825-001 STEP F (1). SYSTEM TEST WAS PERFORMED PER B757-200 AMM 52-11-25-735-024 AND ARMED IS OK.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1368412) BROKEN EMERGENCY LIGHT LENS OF NO. 2 LEFT PASSENGER DOOR AT CABIN PAX. CORRECTIVE ACTION: EMERGENCY LIGHT LENS OF NO. 2 LH PASSENGER DOOR AT CABIN PAX WAS REPLACED PER B757-200 AMM 33-51-01 AND EFFECTIVITY WAS VERIFIED PER B757-200 IPC 33-51-01-07.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1367917) BROKEN CAGE AND LENS AT RH FWD LAVATORY EMERGENCY EXIT LIGHT. CORRECTIVE ACTION: CAGE AND LENS AT RH FWD LAVATORY EMERGENCY EXIT LIGHT (2E/A) WERE REPLACED PER B757-200 AMM 33-51-10 AND EFFECTIVITY WAS VERIFIED PER B757-200 AIPC 33-50-02-03 ITEM 15.

Part: SKIN — DENTED (BS 1600-1620) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1367012) DENTS ON EXTERNAL FUSELAGE REPAIR DOUBLER BTW STA: 1600-1620 AND STGR: 18L-19L. CORRECTIVE ACTION: EXTERNAL FUSELAGE REPAIR DOUBLER BTW STA: 1600-1620 AND STGR: 18L-19L WAS REPLACED PER ERA 583144-14 REV. ORIGINAL AND ETI-57-19-163 REV.1 AND UPDATE AND CLOSE LOG PAGE 2598230 PER ERA 583144-14 REV. ORIGINAL STEP 21.

Part: BUSHING — CORRODED (RT PYLON) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1366155) CORROSION ON UPPER SPAR FITTING BUSHING INBD SIDE AT RH PYLON. AMDS 5720-01100-0101B. CORRECTIVE ACTION: SUMMARY OF NRC S/N:00398, UPPER SPAR FITTING BUSHING INBD SIDE AT RH PYLON WAS REPLACED PER B757-200 SRM 54-51-90 REPAIR 3 PROCEDURE IX.

Part: SKIN — DENTED (BS 600) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1364514) 2 DENT WERE DONE ON NEW SECTION SKIN STA 600 BTW STRINGER 18LH-19LH, PROTUBERANCE WAS DONE ON NEW SECTION SKIN STA 620 ABOVE STRINGER 18LH AND TOOL MARKS WERE DONE ON SPLICE REPAIR DOUBLER STA 589-596 STRINGER 17LH. CORRECTIVE ACTION: PROTUBERANCE ON NEW SECTION SKIN STA 620 ABOVE STRINGER 18LH AND TOOL MARKS ON SPLICE REPAIR DOUBLER STA 589-596 STRINGER 17LH WERE REPAIR PER ERA 574571-14AD REV. A, SECTION V.

Part: SKIN — CORRODED (RT WING) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1364510) WINGS / OUTER WING / UPPER SURFACE / RHS SKIN / HOLES #1, #2, #3, #5, #6, #7, #8 AND #16 / CORROSION. REMOVE AND INSTALL BOLTS #11 TO #15 AND # 17-18 ON RH OUTER WING SKIN UPPER SURFACE. CORRECTIVE ACTION: SB 57A0073 R1 WAS ACCOMPLISHED. BOLTS #11 TO #15 AND #17-18 ON RH OUTER WING SKIN UPPER SURFACE WERE REMOVED AND INSTALLED PER ER/A 582897-14AD REV. ORIGINAL AND ETI 57-19-151 REV 10.

Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1360188) DURING NDT INSPECTION, CORROSION INDICATIONS WERE FOUND ON OPEN HOLES 1, 2, 3, 5, 6, 7, 8 AND 16 ON DRAG FITTING RH WING. CORRECTIVE ACTION: (CORROSION LEVEL 2) CORROSION ON OPEN HOLES 1, 2, 3, 5, 6, 7, 8 AND 16 ON DRAG FITTING RH WING. WERE REPAIRED PER ER/A 582897-14AD REV.ORIGINAL. AND ETI 57-19-151 REV 10.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1360054) DURING NDT INSPECTION, CORROSION INDICATIONS WERE FOUND ON OPEN HOLES 5, 8 AND 10 ON DRAG FITTING LH WING. CORRECTIVE ACTION: (CORROSION LEVEL 2) CORROSION ON OPEN HOLES 5, 8 AND 10 ON DRAG FITTING LH WING WERE REPAIRED PER ER/A 582894-14AD REV. ORIGINAL AND ETI 57-19-150 REV. 9.

Part: FRAME — DENTED (BS 1480) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1357401) DENT ON FRAME STA 1480 AND S-26L AT AFT CARGO COMPARTMENT. (CCT). CORRECTIVE ACTION: DENT ON FRAME STA 1480 AND S-26L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM 53-00- 07-2R-5 MAINTENANCE REQUERIMENTS WERE VERIFIED AND FOLLOWING ACTIONS ARE NEEDED: INSPECTION THRESHOLD 37,500 FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 50000 AIRFRAME FLIGHT CYCLES. PERFORM REPETITIVE DETAILED INSPECTION AND HFEC EVERY 12000 FLIGHT CYCLES AFTER REPAIR WAS INSTALLED PER B757-200 SRM 53-00-07 REPAIR 5 TABLE II.

Part: WEDGE — DEBONDED (LT WING SLAT) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1355359) DISBOND OF 1.250" X 1" BTW SS 137 TO 145 AT UPPER SKIN ON WEDGE SLAT # 5 LH WING. (REF. CARD 5740-01145-05E). CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO. 00085: DISBOND CLASS 3 SS 137 TO 145 AT UPPER SKIN ON WEDGE SLAT # 5 WAS REPAIRED PER B-757-200 S.R.M. 57-43-02-2R-1 (DISBOND CLASS PER TABLE 202) AND REPAIR PER B757-200 S.R.M. 51-70-10-2R-4. AND PERFORM A DECAL CONDITION INSPECTION EVERY "L" CHECK PER TOPP MANUAL 30-10-70 PAR. I PAGE 14.

Part: WEDGE — DEBONDED (RT WIND SLAT) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1355347) DISBOND (2.1" X 1.7") ON RH WING LEADING EDGE SLAT 9 TRAILING EDGE WEDGE SS 600. CORRECTIVE ACTION: DISBOND (CLASS 3 ) ON RH WING LEADING EDGE SLAT 9 TRAILING EDGE WEDGE SS 600 WAS REPAIRED PER B-757-200 S.R.M. 57-43-02-2R-1 (DISBOND CLASS PER TABLE 202) AND REPAIR PER B-757-200 S.R.M. 51-70-10-2R-4. PERFORM A DECAL CONDITION INSPECTION EVERY "L" CHECK PER TOPP MANUAL 30-10-70 PAR. I PAGE 14.

Part: TEE FITTING — DAMAGED · airframe 74,628 hrs · 18,831 cycles

SHIP 6812 PER CARD 5310-01371-0201 DOOR 4 INTERCOSTAL TEE CLIP 757-TERMINATING MOD, STEP 4. CORRECTIVE ACTION: DOOR 4 TEE CLIP REPAIR WAS COMPLETED PER CARD. (1350358)

Part: FLOOR SUPPORT — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

SHIP 6812 CORROSION ON FLOOR CHANNEL BTW STA 1661 AND 1681 LBL 55 , AT PASSENGER FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00424 FLOOR CHANNEL BTW STA 1661 AND 1681 LBL 55, AT PASSENGER FLOOR STRUCTURE WAS REPLACED PER B757-200 SRM.(1349036)

Part: BUSHING — CORRODED (RT PYLON) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

SHIP 6812 CORROSION ON UPPER LINK BUSHING (FWD SIDE) AT RH PYLON. CORRECTIVE ACTION:SUMMARY OF NRC 400: BUSHING OF UPPER LINK (FWD SIDE) AT RH PYLON WAS REPLACED PER B757-200 CMM 54-50; SOPM 20-50-03 AND DWG. (1348480)

Part: SNUBBER — OUT OF TOLERANCE (L1 DOOR) · airframe 74,628 hrs · 18,831 cycles

SHIP 6812 ROTARY SNUBBER PIN EXTENSION DOES NOT MEET REQUIREMENTS ON LEFT DOOR #1. CORRECTIVE ACTION: SUMMARY OF NRC 00596: SNUBBER ON #1 LEFT PASSENGER DOOR WAS REPLACED PER B757-200 AMM 52-11. (1345326)

Part: SNUBBER — OUT OF TOLERANCE (L2 DOOR) · airframe 74,628 hrs · 18,831 cycles

SHIP 6812 THE ROTARY SNUBBER PIN , IS LESS THAN THE MINIMUM EXTENSION PERMITED VALUE, AT NBR 2 LEFT DOOR REF AMDS. CORRECTIVE ACTION: SNUBBER ON #2 PASSENGER DOOR WAS REPLACED PER B757-200 AMM 52-11. (1343936)

Part: SNUBBER — OUT OF TOLERANCE (L4 DOOR) · airframe 74,628 hrs · 18,831 cycles

SHIP 6812 THE ROTARY SNUBBER PIN , IS LESS THAN THE MINIMUM EXTENSION PERMITED VALUE , AT NO 4 LEFT DOOR REF. AMDS. CORRECTIVE ACTION: SNUBBER ON #4 PASSENGER DOOR WAS REPLACED. (1343943)

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1344390) CORROSION ON FLOOR CHANNEL BTW STA 1661 AND 1681, BL 0, AT PASSENGER FLOOR STRUCTURE (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2: FLOOR CHANNEL BTW STA 1661 AND 1681, BL 0, AT PASSENGER FLOOR STRUCTURE WAS REPLACED PER B757-200 SRM 51-40-02 PAR. 4 AND 7.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1342843) CORROSION ON CHANNEL BTW STA 345 AND 365 RBL 62 , AT PASSENGER CABIN FLOOR STRUCTURE (CPAX). CORRECTIVE ACTION: SUMMARY OF NRC00411 CORROSION LEVEL 2; FOR EXCESSIVE CORROSION ON CHANNEL BTW STA 345 AND 365 RBL 62, AT PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED PER B757-200 SRM 51-40-02 PAR.7 AND DWG141N5160-79 REV.CD.

Part: ACCESS PANEL — DENTED (VERTICAL STAB) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1342743) SEVERAL DENTS ON VERTICAL L.E. ACCESS PANEL 321DL (LH SIDE), (EHV). CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO. 00138: DENTS ON VERTICAL L.E. ACCESS PANEL 321DL (LH SIDE) AND OUT OF LIMITS PER B-757-200 SRM 55-30-01 FIG. 101. THESE DENTS WERE REPAIRED PER ERA 582658-14 REV. ORIG. AND PER ETI-57-19-154 REV. 2.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1342024) CORROSION ON CHANNEL BTW STA 324 AND 345 RBL 62, AT PASSENGER CABIN FLOOR STRUCTURE (CPAX). CORRECTIVE ACTION: SUMMARY OF NRC00412 CORROSION LEVEL 2; FOR EXCESSIVE CORROSION ON CHANNEL BTW STA 324 AND 345 RBL 62, AT PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED PER B757-200 SRM 51-40-02 PAR.7 AND DWG141N5160-78 REV. CD.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1341889) CORROSION ON SUPPORT FITTING , STA 1315 RBL 25 , AT PASSENGER FLOOR STRUCTURE (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, EXCCESIVE CORROSION ON SUPPORT FITTING , STA 1315 RBL 25 , AT PASSENGER FLOOR STRUCTURE REPLACE PER B757-200 SRM 51-40-02 PAR. 7.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1340254) CORROSION OUT OF LIMITS ON WEB BTW STA: 1681-1689 AND RBL:54 AT CABIN PAX. CORRECTIVE ACTION: (CORROSION LEVEL 2), (AREA CUTTED OUT IS 1.00) WEB BTW STA 1681-1689 AND RBL 54 AT CABIN PAX WAS REPAIRED PER B757-200 SRM 53-60-51 REPAIR 2 ALTERNATIVE II AND 51-40-02 PAR. 4. AND 7.

Part: FRAME — DAMAGED (BS 1280) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 1339382) TOOL MARK ON PREVIOUS REPAIR ON FRAME STA 1280 STGR 10R. (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00308: PREVIOUS REPAIR DOUBLER ON FRAME STA 1280 STGR 10R AT PAX CABIN WAS REPLACED PER ER/A 519273-14 REV ORIGINAL; SECTION I. REPAIR APPROVAL IS LIMITED TO A THRESHOLD OF 29,100 TOTAL AIRFRAME FLIGHT CYCLES ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR AFTER 29,100 FLIGHT CYCLES.

Part: INDICATOR — OBSTRUCTED (DOOR) · airframe 74,247 hrs · 18,759 cycles

(AIRCRAFT 6812, L/P 1263343) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:602 / ACARS TEXT: FRC521207602 / INTERIOR. CLEARED OBSCTRUCTION. OK FOR SVC.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 72,121 hrs · 18,367 cycles

SHIP 6812 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:606. LOCATED EXIT COVER LENS LOC. 606. REINSTALLED SAME. (1008291)

Part: ANTI-ICE VALVE — FAILED (LT WING) · airframe 71,695 hrs · 18,283 cycles

SHIP 6812 WING AIR CB POPPED WHEN SELECTED. RESET CB ONCE AND IT POPPED A SECOND TIME. C/W NO GO ODI CHECKLIST STEP 1 AND STEP 2. ALL WORKING CHKS OK AT P37 PANEL. FOUND LT ANTI ICE VALVE WITH HIGH RESISTANCE. REMOVED LT WING ANTI ICE VALVE PER B757 AMM 30-11. INSTALLED LT WING ANTI ICE VALVE PER B757 AMM 30-11-02. OPS CHK GOOD. (5562650)

Part: SKIN — DENTED (BS 640) · airframe 74,628 hrs · 18,831 cycles

(AIRCRAFT 6812, L/P 0907974) COMPLY WITH SECTIONS IV AND V AS REQUIRED PER ER/A 574571-14-14, REV ORIGINAL FOR DENT FWD OF DOOR 2L REF LOG 4386025. CORRECTIVE ACTION: PERMANENT REPAIR ON FUSELAGE SKIN STA 640 STR 17L-18L WAS PERFORMED PER ER/A 574571-14AD REV.A SECTION V. PERMANENT REPAIR UNDER LP 1367422.

Part: BEARING — OUT OF POSITION (R1 DOOR) · airframe 68,767 hrs · 17,728 cycles

R1 DOOR HARD TO CLOSE, WONT LOCK. FOUND LATCH ROLLER BEARING ON AFT PART OF DOOR UPPER AND LOWER CONTACTING LATCH FITTING ON FRAME DAMAGING BOTH UPPER AND LOWER LATCH FITTINGS AFT SIDE AND LATCH BEARINGS ON DOOR AFT SIDE. CHECKED AND RIGGED R1 DOOR PER AMM 523-11 DOOR OPERATED OK. REPLACED UPPER AFT AND LOWER AFT LATCH FITTINGS AND UPPER AFT LOWER AFT ROLLERS. APPLIED GREASE AND OPS CHK NML. ROLLERS CONTACTING LATCH FITTINGS PROPERLY. ALL DONE IAW AMM 52-11 AND 52-13.

Part: D-RING — DISLODGED (R1 DOOR SLIDE) · airframe 68,762 hrs · 17,727 cycles

D-RING ON THE R1 ESCAPE SLIDE WAS DISLODGED. SECURED THE D-RING. ACFT OK FOR SERVICE IAW AMM 25-66.

Part: FITTING — WORN (R1 DOOR) · airframe 68,279 hrs · 17,635 cycles

WHILE PERFORMING MTC, R1 DOOR HARD TO LOCK. FOUND UPPER AFT LATCH FITTING SEVERELY WORN. REMOVED WORN FITTING AND INSTALLED FITTING PER AMM 52-11.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 68,085 hrs · 17,595 cycles

RED EMERGENCY LIGHT LENS LOOSE. SECURED THE LENS IAW AMM 33-51. OK FOR SERVICE.

Part: SWITCH — DAMAGED (SLIDE LIGHT) · airframe 67,351 hrs · 17,446 cycles

L1 DOOR SLIDE LIGHT INOPERATIVE. FOUND THE SWITCH JAMMED INWARD. SECURED THE SWITCH. OPS NORMAL.

Part: GIRT BAR — DETACHED (R4 DOOR) · airframe 67,278 hrs · 17,429 cycles

R4 DOOR WILL NOT ARM. ATTACHED THE GIRT BAR. R4 DOOR OPS CHECKED OK IAW AMM 52-11.

Part: COVER — MISSING (R1 DOOR HANDLE) · airframe 66,915 hrs · 17,357 cycles

DURING A CABIN WALKTHROUGH, FOUND THE R1 DOOR HANDLE COVER MISSING. REPLACED THE HANDLE COVER.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 66,667 hrs · 17,308 cycles

(AIRCRAFT 6812, L/P 3877952) R1 SLIDE LANYARD HANGING DOWN WHEN DOOR OPEN DURING CATERING. RESTOWED SLIDE LANYARD PER B757 AMM 52-11.

Part: DOOR — OUT OF ADJUST (R4) · airframe 66,325 hrs · 17,226 cycles

R4 DOOR SLIDE LIGHT DOES NOT COME ON WHEN ARMING DOOR. ADJUSTED THE R4 DOOR IAW AMM 52-11-25.

Part: THRESHOLD — CORRODED (LAVATORY) · airframe 66,323 hrs · 17,225 cycles

AFT LT LAVATORY DOOR THRESHOLD CORRODED. COMPLIED WITH ERA 562697-14.

Part: ROD END — DAMAGED (L1 DOOR) · airframe 66,323 hrs · 17,225 cycles

ROD END DAMAGED ON PUSH ROD OF THE L1 DOOR. REPLACED THE ROD END AND CHECKED ADJUSTMENT IAW AMM 52-11-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,601 hrs · 17,087 cycles

DURING PDC, FOUND EXIT LIGHT LENS AT THE R1 DOOR MISSING. THE LENS WAS REPLACED. OPS CHECKED OK.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 63,897 hrs · 16,766 cycles

L2 DOOR WOULD NOT ARM. INVESTIGATED AND FOUND SALT SHAKER IN GIRT BAR AREA. REMOVED AND OPS CHECKED GOOD. OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 63,154 hrs · 16,587 cycles

E-PATH LIGHT INOP BY SEAT 18D. FOUND CONNECTOR UNDER SEAT DISCONNECTED. RE-CONNECTED CONNECTOR AND PERFORMED EMERGENCY LT TEST CHKS OK PER ER AMM 33-51.

Part: STRUT — CORRODED (NLG) · airframe 57,617 hrs · 15,504 cycles

RUST EMANATING FROM NLG LOWER DRAG STRUT ATTACH PIN AT STRUT ATRH ATTACHMENT TO OUTER CYLINDER. REPLACED NLG LOWER DRAG STRUT ATTACH PIN IAW AMM 32-21-03. UNSERVICE AND SERVICE STRUT IAW AMM 12-15-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,500 hrs · 16,667 cycles

FUSELAGE SKIN REPAIR AT FS 293, BETWEEN S-18R AND S-19R. REF ERA 540714-14 FOR REPAIR.

Part: BALL SCREW — CORRODED (RT WING TE FLAP) · airframe 57,617 hrs · 15,504 cycles

WHILE WORKING AN INSPECTION, RT INBD T/E FLAP BALLSCREW RT INBD T/E FLAP INBD BALLSCREW FOUND CORRODED. REMOVED RT INBD FLAP INBD BALLSCREW IAW AMM 27-51-11 . OFF PN, OFF SN 5467, OK TO INSTALL BALLSCREW ASSY IAW AMM 27- 51-11, PN 7821344, SN DL 15. REPLACED BALLSCREW ASSY IAW AMM 27-51-11. OPS TEST ON BALLSCREWS C/W ON R/C 2751-2542, STEP 18.

Part: BALL SCREW — CORRODED (LT WING TE FLAP) · airframe 57,617 hrs · 15,504 cycles

LT INBD T/E FLAP BALLSCREW CORROSION FOUND. SUMMARY, NR FOR ADDITIONAL INFORMATION 001-0067:2751-2539-LT/001 00195. REPLACED BALLSCREW ASSY IAW AMM 27-51-11. OPS TEST C/W ON R/C 2751-2538, STEP 18.

Part: GCU — ODOR (RIGHT) · airframe 56,856 hrs · 15,359 cycles

FUMES AFTER STARTING LT ENGINE START CREW NOTED EICAS RT AC BUS OFF WITH CIRCUIT BREAKER ON P6-1 PANEL ROW G5 POPPED. F/A ALSO SMELLED AN ELECTRICAL ODOR IN AFT CABIN. AFTER APU WAS RESTARTED THE RT AC BUS CAME BACK ON LINE. RETURNED TO THE GATE. REPLACED RT GCU IAW AMM 24-22-02-404-004. INSPECTED P33, P54, P51 P50, P32, P31, P34 AND P37 PANEL IN THE E/E COMPARTMENT, ALSO INSPECTED COCKPIT P6-1, P6-2, P6-3 AND P6-4 PANELS NO DISCREPANCIES FOUND AND NO EVIDENCE OF ELECTRICAL ODOR. THE C905 AUX POWER BREAKER INSPECTED. ALL GALLEYS OVENS CHILLERS COFFEEMAKERS AND RECIRCULATING FAN INSPECTED NO TROUBLE FOUND. RAN BOTH ENGINES WITH APU GENERATOR FOUND ALL ELECTRICAL GENERATIONS SYSTEMS WORKING NORMALLY.

Part: SKIN — DAMAGED (BS 293) · airframe 57,679 hrs · 15,518 cycles

FWD OR R1 DOOR BS 293, RAMP REPORTS NICK ON SKIN. REPAIRED IAW ERA 540714-14, REV ORIGINAL.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 53,649 hrs · 14,725 cycles

DIVERTED DUE TO AN INFLIGHT OVEN FIRE IN THE AFT GALLEY. CREW COMPLIED WITH QRH PROCEDURES. MAINTENANCE FOUND BURNED RESIDUE ON THE OVEN HEATING COIL. REPLACED AFT GALLEY LT OVEN IAW AMM.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 53,368 hrs · 14,657 cycles

EXECUTED AN AIR TURN BACK DUE TO A BURNING ELECTRICAL ODOR AFTER TURNING ON THE WEATHER RADAR. CREW TURNED THE RADAR OFF AND PULLED ASSOCIATED CIRCUIT BREAKERS. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER, WEATHER RADAR MODE PANEL AND LT & RT RECIRCULATION FILTERS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,895 hrs · 14,196 cycles

EXIT LIGHT ABOVE R4 DOOR INOPERATIVE. R & R EMERGENCY BATTERY PACK AND CHARGER ASSY IN AFT CABIN OVERHEAD CEILING PANEL IAW AMM 33-51.

Part: FRAME — GOUGED (BS 1280) · airframe 49,435 hrs · 13,898 cycles

BS 1280, FRAME WAS FOUND GOUGED AT SEVERAL LOCATIONS BETWEEN S9-15R. A NEW FRAME SEGMENT WAS SPLICED IN BETWEEN S9-10R IAW ER/A 519273-14.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

FLOORBEAM AT BS 365 HAS CORROSION ON UPPER SURFACE AND LWR SURFACE FROM RBL 2-63. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REPAIRED IAW SRM 53-00-51, REPAIR 8.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

FLOORBEAM AT BS 324 HAS CORROSION ON UPPER SURFACE FROM RBL 52-62, FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-10-08, REPAIR 1.

Part: FLOOR SUPPORT — CRACKED (BS 365-377) · airframe 49,435 hrs · 13,898 cycles

CABIN UNDER FLOOR STRAP BETWEEN FLOOR SUPPORT BS 365 AND 377 HAVE CRACKED, LBL 25. REPAIRED IAW ER/A384483-14MA, REV B, PERMANENT REPAIR BY REMOVING DAMAGED PORTION OF STRAP FROM BS 345 TO 385 & INSTALLED A NEW SECTION IAW ER/A 384483-14MA, REV B.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 49,435 hrs · 13,898 cycles

FLOORBEAM HAS CORROSION AROUND LOWER NUTPLATE HOLES, BS 1640, RBL 3-LBL8. REMOVED DAMAGED SECTION OF CABIN FLOORBEAM AT BS 1640 FROM LBL 11 TO RBL 17 & INSTALLED A NEW SECTION PERMANENT REPAIR IAW SRM 53-00-51, REPAIR 10.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1460-1480 LBL 2 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 53-00-53. R & R FLOOR SUPPORT IAW SRM 51-40-02, PG 7 AND ER/A 491157-14 MA.

Part: SKIN — DENTED (BS 1620) · airframe 49,435 hrs · 13,898 cycles

DENT ON FUSELAGE SKIN JUST AFT OF LAST WINDOW RT SIDE, ON BUTT SPLICE AT BS 1620. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN JUST AFT OF LAST WINDOW RT SIDE, ON BUTT SPLICE AT STA 1620 IAW ER/A 519272-14, REV ORIG DENTED AREA MEASURE 2.15"X0.7"X.013" MAX DEPTH, A/Y =53.85, BLENDOUT COMMON TO DENTED AREA MEASURE 2" X 1" X .076" MIN REM MATERIAL THICKNESS. FWD SKIN ORIG THICKNESS:.090", AFT SKIN ORIG. THICKNESS: .080".DISCREPANT DENT AND BLENDOUT FOUND TO BE OUT OF LIMTS DUE TO PROXIMITY TO SKIN JOINT & WINDOW CUTOUT REF SRM 53-00-01. REPAIRED IAW ERA 14-519272.

Part: SEAT TRACK — GOUGED (BS 866) · airframe 49,435 hrs · 13,898 cycles

MAIN CABIN SEAT TRACK BS 866, RBL 24 HAS DEEP GOUGED. R & R DAMAGED SECTION OF SEAT TRACK FROM BS 842-880 IAW SRM 53-00-52, FIG 201, REPAIR 3. REPAIRED IAW SRM 53-00-52, REPAIR 3, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1500-1520, RBL 7 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 53-00-53. REPAIRED IAW ER/A 332525-14MA REV D.

Part: SEAT TRACK — DAMAGED (BS 1540-1640) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

AFT CABIN, SEAT TRACK BS 1540-1640, RBL 24.75 CHAFED AND AFT 8 INCHES EXFOLIATED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE I, DETAIL I, REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5130.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1500-1520, LBL 11.4 HAS CORROSION. REPAIRED IAW ER/A 332525-14MA, REV D.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1500-1520, RBL 2 HAS CORROSION. REPAIRED2 IAW ER/A 332525-14MA, REV D.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1500-1520 LBL 2 HAS CORROSION UPPER & LOWER SURFACES. REPAIRED IAW ER/A 332525-14MA, REV D.

Part: SEAT TRACK — GOUGED (BS 866) · airframe 49,435 hrs · 13,898 cycles

MAIN CABIN SEAT TRACK, BS 866, RBL 45 HAS DEEP GOUGED. R & R DAMAGED SECTION OF SEAT TRACK FROM STA 848 TO 880, INSTALLED REPAIR IAW SRM 53-00-52, REPAIR 3, FIG 201.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 49,435 hrs · 13,898 cycles

CORROSION ON AFT CARGO DOOR REPAIR DOUBLER AT INTERCOSTAL WEB. R & R IAW SRM-51-40-02.

Part: FRAME — GOUGED (BS 1520) · airframe 49,435 hrs · 13,898 cycles

FUSELAGE FRAME UPPER FLANGE IS GOUGED, STA 1520, BETWEEN S23R AND S26R ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE FRAME STA 1520 BET. S23R AND S26R IAW SRM 53-00-07, FIG 201, REPAIR 5, DETAIL III. REPAIR ON FRAME STA 1520 BET S 23R AND S26R IS A CAT "B".

Part: SEAT TRACK — DAMAGED (BS 1390) · airframe 49,435 hrs · 13,898 cycles

AFT CABIN, SEAT TRACK BS 1390 LBL 45.5 HAS A BROKEN LUG. REMOVED DAMAGED SECTION OF SEAT TRACK & INSTALLED REPLACEMENT SECTION IAW SRM 53-00-52, REPAIR 3, FIG 201.

Part: FRAME — DENTED (BS 1400) · airframe 49,435 hrs · 13,898 cycles

DENT ON FUSELAGE FRAME UPPER FLANGE IN AFT CARGO BAY BS 1400 BETWEEN STRINGERS 26-27L. TRIMMED DAMAGE IAW SRM 53-00-07, REPAIR 5, FIG 201. REPAIRED IAW SRM 53-00-07, REPAIR 5, FIG 201.

Part: SEAT TRACK — CORRODED (BS 635) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

CORROSION ON MAIN CABIN SEAT TRACK AT BS 635, RBL 45.5, FOUND OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-00-52, FIG 201, REPAIR 3.

Part: FRAME — DENTED (BS 1420) · airframe 49,435 hrs · 13,898 cycles

FRAME UPPER ANGLE IS DENTED AT AFT CARGO BAY BS 1420 BETWEEN S26-27L. TRIMMED -OUT DENTED AREA ON FRAME. REPAIRED IAW SRM 53-00-07, REPAIR 5, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1460-1480, RBL 2 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE DETAIL V & ER/A 491157-14MA, REV ORIG ACCOMPLISHED.

Part: SEAT TRACK — DAMAGED (BS 1320-1420) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

AFT CABIN, SEAT TRACK BS 1320-1420, RBL 24.75 CHAFED AND FWD 15 INCHES CORRODED. BLENDED SEAT TRACK AND FOUND TO BE OUT OF LIMITS IN SRM 53-00-52, REP 3. REPAIRED SEAT TRACK IAW SRM 53-00-52, REP 3, PAGE 201, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1320-1340) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO FLOOR SUPPORT CORRODED BS 1320-1340, RBL 2. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE 1, DETAIL V & ER/A 491157-14MA, REV ORIG. REPAIRED IAW AMM 53-87-01-801.

Part: FLOOR SUPPORT — CORRODED (BS 640-660) · airframe 49,435 hrs · 13,898 cycles

LIGHT CORROSION ON FLOOR SUPPORT BS 640-660. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53, DET V FIG 101 AND ER/A 491157-14MA.

Part: SEAT TRACK — CHAFED (BS 1540-1640) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

AFT CABIN, SEAT TRACK BS 1540-1640, RBL-45.5 CHAFED, REMOVED DAMAGE AND FOUND OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-02.

Part: FRAME — DENTED (BS 600) · airframe 49,435 hrs · 13,898 cycles

FRAME IS DENTED, UPPER FLANGE AT BS 600 IN FWD CARGO ABOVE STRINGER 24L. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (BS 740-765) · airframe 49,435 hrs · 13,898 cycles

LIGHT CORROSION ON TOP AND BOTTOM SURFACE OF FLOOR SUPPORTS BS 740-765, BETWEEN LT AND RT TRANSITION PANEL'S AT NUTPLATES. REMOVED CORROSION FROM FLOOR SUPPORTS IAW SRM 53-00-53, FIG 101. FOUND TO BE WITHIN LIMITS. BLENDED IAW ER/491157-14MA.

Part: SEAT TRACK — DAMAGED (BS 1540-1640) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

AFT CABIN, SEAT TRACK BS 1540-1640 LBL 45.5 CHAFED AND AFT 7 INCHES EXFOLIATED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, DETAIL 1. R & R SEAT TRACK IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1500-1520, RBL 11.4 HAS CORROSION. REMOVED CORROSION IAW SRM 51-40-02, 53-0053, 53-60-53, ER/A 491157-14MA, REV ORIG.

Part: SEAT TRACK — CHAFED (BS 1540-1640) · corrosion level 2 · airframe 49,435 hrs · 13,898 cycles

AFT CABIN, SEAT TRACK BS 1540-1640, LBL-24.75 HAS CHAFING DOWN INSIDE, DAMAGED AREAS ON CROWN, AND AFT 8" IS EXFOLIATED. REMOVED CORROSION AT MAIN CABIN SEAT TRACK BETWEEN STA 1640 TO 1560, LBL 24.75. FOUND OUT OF LIMITS MAXIMUM ALLOWABLE DIAMETER 0.84" AFTER BLENDOUT 0.98 IN REF SRM 53-00-52, ALLOWABLE DAMAGE 1 DETAIL I R & R SEAT TRACK AT MAIN CABIN BETWEEN STA 154 TO 1640, LBL 24.75 IN REF SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1320-1340) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO FLOOR SUPPORT HAS CORROSION UPPER/LOWER SURFACE STA 1320-1340, RBL 7.5. REMOVED CORROSION ON AFT CARGO STR UPPER/LOWER SURFACE STA 1320-1340, RBL 7.5, ORIG MAT THICKNESS 0.063" AND MAT. LOSS 0.004" FOUND TO BE WITH IN LIMITS IAW SRM 53-00-53, ALLOWABLE DAMAGE 1.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO, FLOOR SUPPORT BS 1460 -1480, RBL 10 HAS CORROSION UPPER/LOWER SURFACES (111-74). REMOVED CORROSION ON AFT CARGO, FLOOR STR STA 1460-1480 UPPER/LOWER SURFACES, RBL10, ORIG MAT THICKNESS 0.063 AND MAT. LOSS 0.003" FOUND TO BE WITH IN LIMITS IAW SRM 53-00-53 ALLOWABLE.

Part: FLOOR SUPPORT — CORRODED (BS 1320-1340) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO FLOOR SUPPORT HAS CORROSION UPPER SURFACE STA 1320-1340, LBL 7.5 (111-60). REMOVED CORROSION ON AFT CARGO STR, UPPER/LOWER SURFACE STA 1320-1340, LBL 7.5, ORIG. MAT. 0.063" AND MAT. LOSS 0.005" FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE 1.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 49,447 hrs · 13,902 cycles

CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 345 FROM LBL 21 TO RBL 42. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II. REPAIRED IAW E/RA 488913-14MA, REV B.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 49,447 hrs · 13,902 cycles

CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 345 FROM LBL 21 TO RBL 42. REMOVED CORROSION , FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REPAIRED IAW ER/A 488913-14MA, REV B.

Part: FLOORBEAM — CORRODED (BS 377) · airframe 49,447 hrs · 13,902 cycles

FLOORBEAM AT BS 377 HAS CORROSION ON EDGE AND UPPER SURFACE FROM LBL 7 TO RBL 6. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III, REPAIRED IAW SRM 53-00-51, REPAIR 10.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO FLOOR SUPPORT BS 1500-1520, LBL 7 HAS CORROSION UPPER & LOWER SURFACES. REPAIRED FLOOR SUPPORT IAW ER/A 332525-14MA.

Part: FLOOR SUPPORT — CORRODED (BS 1320-1340) · airframe 49,435 hrs · 13,898 cycles

AFT CARGO FLOOR SUPPORT HAS BROKEN NUTPLATE AND CORROSION UPPER & LOWER SURFACE BS 1320-1340 LBL 16. REMOVED NUT PLATES IAW SRM 51-40-02, PG 3, PARA 5C, AND AFT CARGO FLOOR STRINGER, STA 1320-1340, LBL 16. REMOVED CORROSION IAW SRM 53-00-53, ALLOWABLE DAMAGE 1, DETAIL V, AND E/RA 491157-14MA, REV ORIG. ORIGINAL MATERIAL THICKNESS .063", IAW SRM 53-60-53, FIG 1, DETAIL VII, WITH .046" REMAINING, OUT OF LIMITS IAW SRM 53-00-53. PERMANENT REPAIR INSTALLED IAW AMM 53-87-01-801.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 43,989 hrs · 12,840 cycles

DURING LETTER CHECK IN ATL, MAINTENANCE FOUND CORROSION ON THE C2 DOOR LOWER SILL OUTBOARD CHORD RUNNING THE LENGTH OF THE DOORWAY. THE CORROSION IS CONFINED TO THE .140- THICK VERTICAL FLANGE OF THE TEE CHORD AND HAS BEEN REMOVED BY BLENDING. THE DEPTH OF THE CORROSION RANGES FROM .004-. REMOVED TO .052- MAXIMUM. REPAIR MAJOR.

Part: SIGN — DAMAGED (CABIN) · airframe 42,579 hrs · 12,561 cycles

LINE MAINTENANCE FOUND 3L ENTRY DOOR EMERGENCY EXIT SIGN DAMAGED. REPLACED SIGN, OPERATION NORMAL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 33,680 hrs · 10,863 cycles

CTR HYD SYS RESVR DROPPED TO 0.24 AFTER T/O SYS PRESS STAYED NORMAL. FOUND 2 HYD LINES CHAFED AND LEAKING FROM CI PUMP, REF IPC 29-11-51-20A ITEMS 130 AND 605. INSTALLED 2 TEMP LINES. SCVD HYD AND LEAK CKS OK.

Part: FMC — FAILED (E/E BAY) · airframe 32,308 hrs · 10,594 cycles

BOTH LT AND RT FMC WILL NOT HOLD ROUTE DATA T/S IN WORK. R & R CAPTS FMS COMPUTER IAW MM AND UPDATED NAV AND OP PROGRAM DATABASE IAW MM. ALSO RELOADED RT FMS NAV DATABASE IAW MM ALL OPS NML. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: COMPUTER — FAULTED (FMC) · airframe 32,308 hrs · 10,594 cycles

BOTH FMCS WOULD NOT DISPLAY SPEED/ALTITUDE ETSS/ FUEL. COULD NOT MANUALLY ENTER DATA CA-R/R CAPTS FMS COMPUTER IAW MM AND UPDATED NAV AND OP PROGRAM DATABASE IAW MM. ALSO RELOADED RT FMS NAV DATABASE IAW MM, ALL OPS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: ACTUATOR — MALFUNCTIONED (THRUST REVERSER) · airframe 28,963 hrs · 9,969 cycles

RT ENG SEC CONTROL MSG DISPLAYED ON STATUS PAGE. FWD TO MCO AND PLACARD PER MEL 73-21-01A RT T/R IS DEACTIVATED. T/S FIM FOUND MESSAGE PCVA/EEC/EVA/EEC 300-25 FOUND INBD T/R LVDT BAD R SING 503656, P/N DAL 781702948. REMOVED AND REPLACED LEFT SLEEVE CENTER LOCKING ACTUATOR PER AMM. CLEARED MSG AND RAN T/R. MSG DID NOT RETURN. MCO AND PLACARD REMOVED.

Part: LIGHT — DAMAGED (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 7D INOP WITH TRACK LIGHT END PLUG MISSING. REPLACED PATH FLOOR EMERGENCY LIGHTING AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COVER — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH FLOOR TRACK LIGHT AT SEAT 25C HAS MISSING COVER. REPLACED PATH FLOOR EMERGENCY LIGHTING COVER AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN)

DFW - EMERGENCY LIGHT AT LAVATORY D INOP WITH BOTH ENDS TRACK LIGHT MISSING. REPLACED PATH FLOOR EMERGENCY LIGHTING AT LAVATORY D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COVER — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH TRACK LIGHT AT SEAT 33C HAS MISSING COVER. REPLACED PATH FLOOR EMERGENCY LIGHTING COVER AT SEAT 33C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT ROWS 7 TO AFT OF LAVATORY D DOOR INOP. REPLACED PATH FLOOR EMERGENCY LIGHTING CABLE FEED AT SEAT ROW 24 FOR EMERGENCY LIGHTING AT SEAT ROWS 7 TO AFT OF LAVATORY D DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 24D INOP WITH TRACK LIGHT END PLUG MISSING. REPLACED PATH FLOOR EMERGENCY LIGHTING AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

SEA - EMERGENCY LIGHT AT LEFT NR 4 DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW - EXTERIOR EMERGENCY LIGHT AT DOOR L4 INOPERATIVE. CLEANED LIGHT BULB BASE FOR EXTERIOR EMERGENCY LIGHT AT DOOR L4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY FLOOR TRACK LIGHTING FROM ROW 18 AFT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT NUMBER 3 LEFT DOOR FOR EMERGENCY FLOOR TRACK LIGHTING FROM ROW 18 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN INOPERATIVE. REPLACED AFT FLOOR LIGHT POWER STRIP FOR EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - AISLE EMERGENCY LIGHT ON RIGHT HAND SIDE SECOND FROM AFT INOPERATIVE. REPLACED LIGHT ASSEMBLY AND BATTERY PACK FOR AISLE EMERGENCY LIGHT ON RIGHT HAND SIDE SECOND FROM AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

MCO EGRESS LIGHT AT ROW 31 AFT INOPERATIVE. SPLICED WIRING FOR CONNECTOR FOR EGRESS LIGHT AT ROW 31 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — LOOSE (CABIN) · airframe 8,192 hrs · 2,661 cycles

THE EGRESS LIGHT IN FRONT OF THE D-LAVATORY WAS INOPERATIVE. TIGHTENED A LOOSE CONNECTOR. CHECK-C 9-6-00 LAX.

Part: FAIRING — DAMAGED (LT WING TE FLAP) · airframe 5,615 hrs · 1,883 cycles

DURING CHECK-C MAINT, FOUND LEFT WING O/B FLAP O/B CANOE AFT FAIRING LOWER O/B CORNER WITH A HOLE. DRESSED OUT DAMAGED AREA AND POTTED WITH 934 EPOXY. INSTALLED HOT BOND FIBERGLASS WET LAYUP 3 INCH DIAMETER PER SRM 51-70-03.

Part: LIGHT — INOPERATIVE (PAX DOOR)

THE RIGHT SIDE NUMBER 4 CABIN DOOR EMERGENCY SLIDE LIGHT WAS INOPERATIVE. FOUND SOLDER FLUX ON THE SOLDERED CONNECTION OF THE LIGHT ASSEMBLY. CLEANED THE CONNECTION ON LIGHT ASSY AND RESOLDERED CONTACT ON THE LAMP. CHECK-C 3-14-99 LAX.

Part: SKIN — PUNCTURED (FUSELAGE)

PUNCTURE IN FUSELAGE, 3 IN BY 5 IN, LOCATED 3 FT FWD OF THE NUMBER 4 DOOR ON LT SIDE, AND 6 IN BELOW THE DOOR. REPAIRED PER SRM 53-00-01, FIG 204, SHEET 3.