N671DN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,122 hrs · 42,150 cycles

SHIP 0671 R1 DOOR ASSIST RESERVOIR AT 0 PSI. CORRECTIVE ACTION: REMOVED AND REPLACED R1 DOOR ASSIST RESERVOIR IN REF W/B757 AMM 52-11. AC OK FOR SERVICE. (4324256)

Part: SLIDE — PARTIAL DEPLOY (UNKNOWN) · airframe 93,101 hrs · 42,133 cycles

SHIP 671 DOOR R1 SLIDE PARTIALLY DEPLOYED WHEN CATERING OPENED DOOR. CORRECTIVE ACTION: DOOR NO. 1 RIGHT SLIDE INSTALLATION ONLY. C/W JOB CARD 2566-9001. (4324242)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,677 hrs · 41,872 cycles

SHIP 671 2L DOOR EMER EXIT LENS FELL OFF INSIDE CABIN DURING CLIMBOUT. CORRECTIVE ACTION: RESECURED SAME. (4476056)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,677 hrs · 41,872 cycles

SHIP 671 ON WAKE UP FOUND R2 DOOR EMER EXIT LENS MISSING. CORRECTIVE ACTION: REPLACED LENS. (4476054)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,584 hrs · 41,812 cycles

SHIP 0671 L2 DOOR OVERHEAD EXIT SIGN LENS DAMAGED. CORRECTIVE ACTION REMOVED AND REPLACED L2 DOOR EMERGENCY EXIT LIGHT LENS. REF B757 CMM 33-51-31. OK FOR SVC. (2990942)

Part: UNKNOWN — UNKNOWN (UNKNKOWN) · airframe 91,611 hrs · 41,227 cycles

SHIP 671 ER/A 599012-14 / SECTION III ONE-TIME INSPECTION. CORRECTIVE ACTION: REF ERA 599012-14 REV A. (2759091)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,561 hrs · 41,194 cycles

SHIP 671 RT OVERWING EMERGENCY EXIT SLIDE FAILED DEPLOYMENT TEST. CORRECTIVE ACTION: COMPLIED WITH STEP 4 OF WORKCARD 2566-2003-RT. (4142576/2743428)

Part: UNKNOWN — UNKNOWN · airframe 91,187 hrs · 40,982 cycles

SHIP 0671 -ATB- DUE TO RIGHT WING ANTI-ICE LIGHT ILLUMINATED. CORRECTIVE ACTION: REPLACED RIGHT WING ANTI-ICE VALVE. OPS CHECKS GOOD.

Part: NONE — NONE · airframe 91,091 hrs · 40,928 cycles

SHIP 671 ON WALK AROUND FOUND CRACK AT STA. 440 STRINGER. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:0514-2001/001 00001 C/W FUSELAGE SKIN DAMAGE REPAIR PER ERA 606367-14 REV ORIG. (2644342)

Part: NONE — NONE · airframe 91,091 hrs · 40,928 cycles

SHIP 671 ON WALK AROUND FOUND CRACK AT STA 440 STRINGER 26R ON RIGHT SIDE. SKIN CRACKED AT BUTT JOINT. CORRECTIVE ACTION: REF ELECTRONIC NR 00001. C/W FUSELAGE SKIN DAMAGE REPAIR PER ERA 606367-14 REV ORIG PRI 606367-14 REV 0AND 1 MATCH. ERA 606367-14 REV 0RIG. (4049907)

Part: SKIN — CRACKED (BS 439 S25R) · airframe 93,963 hrs · 42,652 cycles

SHIP 671 DTE 606367-14 - B757-200 / FUSELAGE SKIN / STA 439 & S-25R / CRACK PERMANENT REPAIR. CORRECTIVE ACTION: REF ERA 606367-14. (2644141)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 90,978 hrs · 40,849 cycles

SHIP 671 CA SIDE WINDSHIED ARCING AND CRACKED. UPPER LEFT CORNER. CORRECTIVE ACTION: R/R CAPT SIDE WINDSHIELD L1 PER B757 AMM 56-11. REF LOG 9613522 FOR WHC R/R DUE TO ARCING. NO LEAKS NOTED AND OPS TEST GOOD. (9613521)

Part: PROXIMITY SENSOR — FAULTED (LT WING SLIDE) · airframe 90,359 hrs · 40,454 cycles

ON APPROACH AND CONFIGURED TO LAND HAD EICAS MESSAGE LEFT WING SLIDE FOR 1-2 MINUTS WENT OUT ON IT'S OWN. R & R LT WING SLIDE PROX SENSOR REF B757 WIRING DIAGRAM 527111 AND 527121. ADJUSTMENT REF B757 AMM 52-71. DISARM AND ARM OFF WING ESCAPE SYS REF B757 AMM 25-65. OPS CKS GOOD.

Part: RELAY — INOPERATIVE (LT WING SLIDE) · airframe 90,267 hrs · 40,398 cycles

SHIP 671 LT WING SLIDE WARN LIGHT INOP. CORRECTIVE ACTION: R/R SLIDE TEST RELAY (K10486) PER B757 IPC 25-65. WARNING LIGHT EXTINGUISHED. NO FAULTS NOTED. (9104202)

Part: NONE — NONE · airframe 90,236 hrs · 40,367 cycles

SHIP 671 ON FINAL, L OVERWING SLIDE CAUTION ILLUMINATED. HAD F/A'S CHECK VISUALLY WITH NO INDICATION SLIDE DEPLOYED. YELLOW CAUTION WENT OUT AND QRH COMPLETED. CORRECTIVE ACTION: ADJUSTED LFT WING OVERWING SLIDE DOOR SENSOR PER B757 AMM 52-71- 00-501-825-211 DOOR TEST SENSOR TEST CHECKS GOOD. (8919524)

Part: NONE — NONE · airframe 90,236 hrs · 40,367 cycles

'SUPPLIMENTAL INFORMATION' SHIP 671 LT WING SLIDE CTN MSG ILLUM SEVERAL TIMES ON APPROACH. CORRECTIVE ACTION: RPLCD PSEU PER B757 AMM 32-09 TEST GOOD. TARGET NEAR. NO MSG. (9062676)

Part: AXLE — DEPARTED · airframe 89,624 hrs · 39,878 cycles

SHIP 671 -TIRE- LEFT NOSE WHEEL ASSEMBLY CAME OFF AFTER LANDING. CORRECTIVE ACTION: REMOVED AND REPLACED NLG AXLE. REMOVED AND REPLACED NOSE WHEEL ASSEMBLIES PER B757 AMM 32-45.

Part: NONE — NONE · airframe 89,491 hrs · 39,799 cycles

SHIP 671 DURING LATCHING & UNLATCHING OF LH OVERWING SLIDE DOOR FOUND LATCH FITTING STUDS ON LATCH TUBE ONLY PARTIALLY ENGAGED IN LATCH FITTINGS ON THE DOOR. CORRECTIVE ACTION: REMOVED DOOR LATCH TUBE IAW B757 AMM 25-65. INSTALLED DOOR LATCH TUBE PER B757 AMM 25-65. FOUND DOOR LATCH FITTINGS PARTIALY ENGAGED. REPOSITIONED DOOR LATCH FITTINGS PER B757 AMM 25-65. LATCH FITTING STUD ENGAGMENT TO DOOR LATCH FITTINGS SATISFACTORY. CONT LOG # 8666935 ALL RII'S C/W. (8666932)

Part: NONE — NONE · airframe 89,491 hrs · 39,799 cycles

SHIP 671 L WING SLIDE EICAS MSG. CORRECTIVE ACTION: INSPECTED LT OFF WING SLIDE SYSTEM FOUND SLIDE DOOR OPEN BUT NO OTHER DEFECTS. CLOSE LT OFF WING SLIDE DOOR PER B757 AMM 25-65. REACTIVATED LT OFF WING SLIDE SYSTEM PER B757 AMM 25-65. (8666920)

Part: DRAG FITTING — INSTALLED · airframe 89,485 hrs · 39,796 cycles

SHIP 671 AWR TRANSFERRED FROM LOG 2202742: REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENTS REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588953-14AD REV A. CORRECTIVE ACTION: SUMMARY OF NRC00146:REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING WAS PERFORMED PER ER/A 588953-14AD REV:B SECTION VI: REPAIR INSTRUCTIONS (QRO MAY 2022) AND UNDER LOG PAGE NUMBER: 2238487. (2238657)

Part: NONE — NONE · airframe 89,474 hrs · 39,791 cycles

SHIP 671 [AD / AA] LH ENG DRAG FTG HOLES NBR 1 TO 10 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #2, CORROSION ON SKIN AND FITTING BTW 8 TO 10 CLOCK POS ; HOLE #4, CORROSION ON SKIN AND FITTING BTW 3 TO 6 CLOCK POS ; HOLE #5, CORROSION ON SKIN BTW 10 AND 11 CLOCK POS ; HOLE #9, CORROSION ON FITTING BTW 3 TO 5 CLOCK POS. IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00148:HOLE #2, HOLE #4, HOLE #5 AND HOLE #9 WERE REPAIRED PER ER/A 588953-14AD REV:B; SECTION VI. (2238487)

Part: NONE — NONE · airframe 89,474 hrs · 39,791 cycles

SHIP 671 AMOC, ER/A 501945-14AD REV. A; FUSELAGE / SKIN / STA. 620, S-26L & S-27L / PREVIOUS REPAIR / CORROSION. CORRECTIVE ACTION: REF ERA 501945-14AD REV A. (2237921)

Part: NONE — NONE · airframe 89,474 hrs · 39,791 cycles

SHIP 671 AWR. AD. A.A 5311-01227-01B. "EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1300 BTW S-24R AND S-27R. CORRECTIVE ACTION: SUMMARY OF NRC 00143: "EXISTING REPAIR ON FRAME STA 1300 BTW S- 24R AND S-27R. WAS REPAIRED PER PRI 501941-14 REV 2 AND ER/A 501941-14AD REV. A SECTION II (PERMANENT REPAIR). (2238319)

Part: NONE — NONE · airframe 89,474 hrs · 39,791 cycles

SHIP 671 DENT ON FUSELAGE SKIN BTW STA 1500 TO STA 1505 AND BTW S30 AND S29 LH AT LOWER FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00059: DENT ON FUSELAJE SKIN BTW STA 1500 TO STA 1505 AND BTW S30 AND S29 LH AT LOWER FUSELAJE WAS REPAIRED PER PRI 599012-14 REV 0 AND ERA 599012-14 REV. ORIG. SECTION I: PERMANENT REPAIR. (2237908)

Part: NONE — NONE · corrosion level 2 · airframe 89,474 hrs · 39,791 cycles

SHIP 671 CORROSION ON REPAIR DOUBLER BTW STA 620 TO STA 630 AND S26 AND S27 LH AT LOWER FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00053: FUSELAGE SKIN BTW STA 620 TO STA 630 AND S26 AND S27 LH WAS REPAIRED PER PRI 501945-14 REV. 0 AND ER/A 501945-14AD REV. (2238175)

Part: SKIN — CORRODED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 DTE, ER/A 599124-14; FUSELAGE / SKIN / STA. 455 TO 470 BETWEEN S27L TO S27R / CORROSION. CORRECTIVE ACTION: REF ERA 599124-14. (2234183)

Part: SKIN — DENTED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 ER/A 599012-14; FUSELAGE / SKIN / STA. 1500 TO 1503 BETWEEN S29L TO S30 / DENTS. CORRECTIVE ACTION: REF ERA 599012-14. (2234637)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,657 hrs · 41,245 cycles

SHIP 671 DTE, ER/A 599012-14; FUSELAGE / SKIN / STA. 1500 TO 1503 BETWEEN S29L TO S30 / DENTS. CORRECTIVE ACTION: REF ERA 599012-14 REV A. (2234642)

Part: ACCESS DOOR — CORRODED · corrosion level 2 · airframe 89,455 hrs · 39,784 cycles

SHIP 671 CORROSION ON E&E ACCESS DOOR CUT OUT AT LOWER FUSELAJE (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00065: CORROSION ON E&E ACCESS DOOR CUT OUT AT LOWER FUSELAJE WAS REPAIRED PER ER/A 599124-14 REV. ORIGINAL SECTION I (PERMANENT REPAIR). (2234779)

Part: ACCESS PANEL — SCRATCHED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 DURING OK TO CLOSE OF ACCESS PANEL 532 HZ , SCRATCHES WERE FOUND ON CUT OUT PANEL (IN REF TO NRC: 00282). CORRECTIVE ACTION: SUMMARY OF NRC 00326: SCRATCHES ON CUT OUT PANEL WERE REPAIRED PER ER/A 599305-14 REV. ORIGINAL SECTION 1. (2234555)

Part: REPAIR — INSTALLED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 SECTION I REPAIR TO LH WING DRY BAY BARRIER AT WSTA 285.65 TO 313.5 REQUIRES SECTION II REPAIR WITHIN 24 MONTHS PER ERA 599305 -14. CORRECTIVE ACTION: REF ERA 599305-14. (2234231)

Part: SKIN — CORRODED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 [AD / AA] RH ENG DRAG FTG HOLES NBR 1 TO 10 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #3, CORROSION ON SKIN AND FITTING BTW 4 TO 7 CLOCK POS ; HOLE #4, CORROSION ON SKIN AND FITTING BTW 3 TO 6 CLOCK POS ; HOLE #9, CORROSION ON FITTING AT 12 CLOCK POS. IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00244: A.A: HOLES #3,#4 AND #9 WERE REAMED TO FIRST OVERSIZE PER AMDS 5720-01100-04B STEP 14 (C). (VT)VISUAL INSPECTION & (ET)HFEC ON OPEN-HOLES, INSPECTION WERE PERFORMED PER AMDS AND B757 NDT MANUAL PART 6, 51-00-16, NO DAMAGE FOUND. (2233217)

Part: NONE — NONE · airframe 89,455 hrs · 39,784 cycles

SHIP 671 DURING THE ENABLING ACTIVITIES OF W.O 5725- 010006-01B, WEAR WAS FOUND IN THE AREA OF THE LOWER AFT WING SKIN, AFT EDGE AT THE FLAP TRACK NBR 7, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00254:WEAR IN THE AREA OF THE LOWER AFT WING SKIN , AFT EDGE AT THE FLAP TRACK NBR 7, RH WING WAS REPAIRED PER PRI 5599088-14 REV 1 AND ERA 599088-14 REV.ORIGINAL. (2230805)

Part: SKIN — WORN · airframe 89,455 hrs · 39,784 cycles

SHIP 671 DURING THE ENABLING ACTIVITIES OF W.O 5725- 010006-01A, WEAR WAS FOUND IN THE AREA OF THE LOWER AFT WING SKIN, AFT EDGE AT THE FLAP TRACK NBR 2, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00255:WEAR IN THE AREA OF THE LOWER AFT WING SKIN , AFT EDGE AT THE FLAP TRACK NBR 2 WAS REPAIRED PER PRI 5599087- 14 REV. 1 AND ERA 599087-14 REV.ORIGINAL. (2229696)

Part: SLAT — DEBONDED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 A.A. 2 DEBONDS AS FOLLOW: 1) OSS 414 (1.900IN X 1.400IN) UPPER SURFACE & 2) OSS 306 (4.200IN X 2.400IN) ON LOWER SURFACE SLAT 4 TRAILING EDGE WEDGE (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC: 00098 SLAT 4 TRAILING EDGE WEDGE 1) OSS 414 UPPER SURFACE & 2) OSS 306 ON LOWER SURFACE WAS REPAIRED PER B757-200 SRM. (2227962)

Part: NONE — NONE · airframe 89,455 hrs · 39,784 cycles

SHIP 671 DURING THE INSTALLATION OF EMERGENCY POWER RESERVOIR WAS FOUND WITH LOW PRESS. CORRECTIVE ACTION: SUMMARY OF NRC 00291: EMERGENCY POWER RESERVOIR AT DOOR 4 L WAS REMOVED AND INSTALLED PER B757-200 AMM 52-11-30. (2227302)

Part: SLAT — DEBONDED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 A.A : 1 DEBOND LOCATED AT OSS 723 (2.100IN X 1.300IN) ON UPPER SURFACE SLAT 10 TRAILING EDGE WEDGE (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00099: AREA (OSS 723) ON UPPER SURFACE SLAT 10 TRAILING EDGE WEDGE WAS REPAIRED PER B757-200 SRM. (2226099)

Part: DOUBLER — DAMAGED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 AWR WORN PREVIOUS REPAIR ON OUTBD WEB AT NCA STA 100 APRROX AT LH PYLON IN REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00300: PREVIOUS REPAIR DOUBLER ON OUTBD WEB AT NCA STA 100 APRROX AT LH PYLON WAS REPLACED PER ER/A 567740-14 REV ORIGINAL SECTION I PERMANENT REPAIR. (2225572)

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 89,455 hrs · 39,784 cycles

SHIP 671 CORROSION TYPE EXFOLATION ON AFT LAVATORY SHROUD INTERNAL STRUCTURE AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00223: DOUBLER INTERNAL ON AFT LAVATORY AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 S.R.M. (2224375)

Part: SKIN — DAMAGED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 PERFORM REPAIR ON FWD CARGO COMPARTMENT SKIN, APROX 16 IN AFT OF DOOR HANDLE. CORRECTIVE ACTION: SUMMARY OF NRC 00109: FWD CARGO COMPARTMENT SKIN, APROX 16 IN AFT OF DOOR HANDLE WAS REPAIRED B757-200 SRM 52-30-01-2R. (2224494)

Part: WEDGE — DEBONDED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 A.A : 1 DEBONDED LOCATED AT OSS 306 ON LOWER SURFACE SLAT 7 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF NRC 00100: LOWER SURFACE SLAT 7 TRAILING EDGE WEDGE WAS REPAIRED PER B757-200 SRM. (2224150)

Part: SKIN — DAMAGED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 PERFORM REPAIR ON FWD CARGO COMPARTMENT SKIN, APROX 16 IN AFT OF DOOR HANDLE. CORRECTIVE ACTION: SUMMARY OF NRC 00109: FWD CARGO COMPARTMENT SKIN, APROX 16 IN AFT OF DOOR HANDLE WAS REPAIRED B757-200 SRM. (2224502)

Part: SLAT — DEBONDED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 A.A AD : DEBONDED ON SLAT 7 LOWER SURFACE OSS 310. CORRECTIVE ACTION: SUMMARY OF NRC 00031: LOWER SURFACE SLAT 7 TRAILING EDGE WEDGE WAS REPAIRED PER B757-200 SRM. (2224140)

Part: SKIN — CRACKED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 CRACK ON DENT BTW STA 530 TO STA 540 AND BTW S27 AND 28 LH AT LOWER FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00049:CRACK ON DENT BTW STA 530 TO STA 540 AND BTW S27 AND 28 LH AT LOWER FUSELAGE SKIN WAS REPAIRED PER B757- 200 SRM 53-00-01-2R REPAIR 29. (2200550)

Part: SKIN — UNKNOWN · airframe 89,455 hrs · 39,784 cycles

SHIP 671 AD, AA, IN REF AMDS 5331-01282-03 STEP 2. TWO REPAIRS WERE FOUND ON LAP SPLICE STR-14L STA 610 AND 620 AT FUSELAGE SKIN (LOG 1140915 AND ERA 513144-14 REV ORIG). CORRECTIVE ACTION: SUMMARY OF NRC 0021 AND REF ERA 503144AD REV A. (2219801)

Part: PUSHROD — CORRODED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 CORROSION ROD END OF SLIDE ARMED PUSHROD AT R4 DOOR. PTAS. CORRECTIVE ACTION: SUMMARY OF NRC 00041: ROD END OF SLIDE ARMED PUSHROD AT R4 DOOR WAS REPLACED AND ADJUSTED PER B757-200 AMM 52-11-20. (2216791)

Part: SKIN — DENTED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 DENT ON FUSELAJE SKIN AT STA 1540 BTW S26 AND S27 RH AT LOWER FUSELAJE (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00062: DENT ON FUSELAGE SKIN AT STA 1540 BTW S26 AND S27 RH AT LOWER FUSELAGE WAS REPAIRED PER PRI 599086-14 REV .0 AND ERA 599086-14 REV. ORIGINAL. (2216787)

Part: SKIN — DENTED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 DENT ON FUSELAJE SKIN AT STA 1500 BTW S28 AND S29 RH AT LOWER FUSELAJE (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00061: DENT WAS REPAIRED PER PRI 599078-14 REV. 0 AND ERA 599078-14 REV. ORIGINAL. (2215285)

Part: SKIN — CRACKED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 CRACK ON DENT BTW STA 530 TO STA 540 AND BTW S27 AND 28 LH AT LOWER FUSELAJE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00049:CRACK ON DENT BTW STA 530 TO STA 540 AND BTW S27 AND 28 LH AT LOWER FUSELAJE SKIN WAS REPAIRED PER B757- 200 SRM 53-00-01. (2214153)

Part: STRAP — CRACKED · airframe 89,455 hrs · 39,784 cycles

SHIP 671 CRACKED STABILIZER STRAP STA 377.7 AT NLG LEFT TUNNEL (NLG). CORRECTIVE ACTION: SUMMARY OF NRC 00171: STABILIZER STRAP STA 377.7 AT NLG LEFT TUNNEL (NLG) WAS REPAIR PER ER/A:384483-14MA REV. D. (2214040)

Part: NONE — NONE · airframe 89,418 hrs · 39,762 cycles

SHIP 671 -DIV- IN TO CLE DUE TO DUAL LOOP FAILURE ON #2 ENG. CORRECTIVE ACTION: REPAIRED WIRING HARNESS LOOP #2 AND REPLACED FIRE DETECTOR LOOP #4.

Part: NOT REPORTED — NOT REPORTED · airframe 89,295 hrs · 39,679 cycles

SHIP 671 2L ENTRY DOOR GUST LOCK WILL NOT ENGAGE. CORRECTIVE ACTION: CYCLED DOOR OPEN AND CLOSED RELEASE GUST LOCK OPS CHECK NORMAL REF B757 AMM 52-11. (8831210)

Part: NONE — NONE · airframe 89,276 hrs · 39,666 cycles

SHIP 671 FOUND DURING WAKE UP 2L PAX DOOR FWD UPPER STOP FITTING MISSING. CORRECTIVE ACTION: INSTALLED STOP PLATE FITTING IAW B757 AMM 52-11-00. (8831203)

Part: NONE — NONE · airframe 89,276 hrs · 39,666 cycles

SHIP 671 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:03R. CORRECTIVE ACTION: FOUND WATER BOTTLE CAP AT 3R DOOR GRIT BAR CHANNEL. CLEANED GIRT BAR CHANNEL AT 3R DOOR. DOOR ARM AND DISARM FUNCTION CHECK NORM, PER 757 AMM 52-21. (2157354)

Part: NONE — NONE · airframe 88,834 hrs · 39,395 cycles

SHIP 671 R AFT ENT DOOR EICAS MSG WITH DOOR CLOSED AND ARMED PROPERLY. CORRECTIVE ACTION: RPLCD PROX SENSOR REF B757 AMM 52-71 AND SPWM CHAPT 20. TEST GOOD. (8247628)

Part: NONE — NONE · airframe 88,590 hrs · 39,265 cycles

SHIP 671 DURING WAKE UP CHK FOUND OVER WING EXIT SIGN FWD MISSING. CORRECTIVE ACTION: INSTALLED LENS AS REQ. OK FOR SVC. (8175106)

Part: NONE — NONE · airframe 88,494 hrs · 39,214 cycles

SHIP 671 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS 1R INOP. CORRECTIVE ACTION: RELAMPED, REMOVED DEBRIS FROM GIRT BAR AND PROX SENSORS. OPS CK GOOD. (2015012)

Part: NONE — NONE · airframe 88,328 hrs · 39,105 cycles

SHIP 671 FWD RAFT PRESSURE FOUND BELOW LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED FWD RAFT PER B757 AMM 25-64. (8053874)

Part: NONE — NONE · airframe 88,159 hrs · 38,999 cycles

SHIP 671 LOWER EMERGENCY EXIT SIGN INOP AT SEAT 26A. CORRECTIVE ACTION: REPLACED BLOWN FUSE #4 ON POWER SUPPLY SLED M10567 IAW B757 AMM 33-51. (7765484)

Part: SCREW — MISSING (L2 DOOR LEVER) · airframe 87,844 hrs · 38,876 cycles

SHIP 671 ARMING LEVER ON DOOR 2L MISSING A SCREW. CORRECTIVE ACTION: RE-SECURED L2 DOOR ARMING LEVER SCREW PER B757 AMM 52-11 CHK NML. (7457172)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 86,217 hrs · 38,216 cycles

DURING INSPECTION MAINTENANCE FOUND A CRACK INDICATION RT BS1640 LOWER HOLES AT S-14R INTERCOSTAL. REPARIED PER ERA 588944-14.

Part: FRAME — CRACKED (BS 1640 S14R) · airframe 93,459 hrs · 42,351 cycles

SHIP 671 FUSELAGE / FRAME / RHS - BS1640 - STR-14R / LOWER HOLES / CRACK. CORRECTIVE ACTION: REF ERA 588944-14. (1685878)

Part: DRAG FITTING — DAMAGED (RT ENGINE) · airframe 86,217 hrs · 38,216 cycles

DURING PROBE INSPECTION OF RT ENGINE DRAG FITTING HOLES NR 1-10 MAINTENANCE FOUND HOLE NR 2 HAS CRACK LIKE INDICATION IN TOP SKIN AT 9 O`CLOCK POSITION FACING AFT. C/W ERA 588956-14.

Part: DRAG FITTING — DAMAGED (LT ENGINE) · airframe 86,217 hrs · 38,216 cycles

MAINTENANCE DISCOVERED INDICATION OF DEFECT NOTED ON THE LT ENGINE DRAG FITTING NR 3 HOLE AT THE 10 O`CLOCK POSITION LOOKING AFT. INDICATION IS IN THE FITTING. REPAIRED PER ERA 588953-14.

Part: DRAG FITTING — DAMAGED (LT ENGINE) · airframe 86,217 hrs · 38,216 cycles

INDICATION OF DEFECTS NOTED ON THE LT ENGINE DRAG FITTING NR 8 HOLE AT THE 11 AND 6 O`CLOCK POSITIONS LOOKING AFT BOTH INDICATIONS ARE LOCATED IN THE FITTING. C/W ERA 588953-14.

Part: NONE — NONE · airframe 88,932 hrs · 39,454 cycles

SHIP 671 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588956-14. CORRECTIVE ACTION: REF ERA 588956-14. (1683719)

Part: NONE — NONE · airframe 88,839 hrs · 39,400 cycles

SHIP 671 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588953-14. CORRECTIVE ACTION: REF ERA 588953-14. (1683696)

Part: WIRE — BROKEN (CABIN) · airframe 84,197 hrs · 37,344 cycles

(AIRCRAFT 671, L/P 5965233) CEILING EMER LIGHT INOP AT 5A. FOUND BROKEN WIRE ON LIGHT CONNECTOR. REPLACED CONNECTOR A/C SIDE OF AISLE EMERGENCY LIGHT AT 5A PER SWPM 20-30 AND RECONNECTED LIGHT. PERFORMED OP CHECK PER AMM 33-51-05 CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 83,147 hrs · 36,910 cycles

SHIP 671 DOOR 1R EMERGENCY EXIT IDENTIFIER LIGHT INOP. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY M730 PER AMM 33-51. OPS CK GOOD. (3009641)

Part: WIRE — CHAFED (L4 DOOR) · airframe 83,136 hrs · 36,906 cycles

SHIP 671 4L DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: FOUND WIRING AT SWITCH S10222 CHAFED THROUGH AND BARE. REPAIRED WIRING. REF SWPM 20-30 AND SSM 25-66-01. FOUND SWITCH S10223 INTERMITTENTLY FAILING. REPLACED SWITCH PER AMM 25-66. (0996175)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 81,013 hrs · 35,942 cycles

TE FLAP DISAGREE AT 2500 ASL DURING APPROACH. PERFORMED A GO AROUND, RAN THE TE FLAP DISAGREE CHECKLIST AND LANDED FLAPS 20 DEG UNEVENTFULL. PERFORMED A BITE TEST OF BOTH FSEUS IAW TSM 27-51, NO FAULTS. RAN SLATS AND FLAPS THRU 2 FULL CYCLES. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (L4 DOOR) · airframe 80,937 hrs · 35,918 cycles

L4 DOOR ICAS MESSAGE ILLUMINATED AT 3000 FT MSG DURING APPROACH. ADJUSTED THE PROXIMITY SWITCH S10097 IAW AMM 52-71.

Part: LAMP — INOPERATIVE (SLIDE LIGHT) · airframe 80,767 hrs · 35,856 cycles

SLIDE INDICATOR LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 25-56, CHECKED OK.

Part: DOOR — OUT OF ADJUST (L4) · airframe 80,635 hrs · 35,814 cycles

DURING FUNCTIONAL CHECK FLIGHT LT AFT ENTRY DOOR LIGHT ILLUMINATED. ADJUSTED L4 PASSENGER DOOR IAW AMM 52-11-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,635 hrs · 35,814 cycles

FWD LOWER WTB STRUCTURE HAS CORROSION STA 900 BETWEEN LBL 12 & RBL 12. CUT OUT DAMAGE DIM 51 1/2 AND REPAIRED AS REQ IAW DWG 149N7132 REV G AND A, SRM 51-40-02 AND 51-70-12 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,635 hrs · 35,814 cycles

FWD LOWER WTB AREA CRACK NOTICED BETWEEN TWO FASTENERS AFT SIDE OF FRAME STA 900 LBL10. REPAIRED AREA AS REQ AT FWD LOWER WTB AREA AFT SIDE OF FRAME STA 900 LBL 10 IAW ERA 567747-14 REV A.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,635 hrs · 35,814 cycles

AFT CARGO STA BETWEEN 1681-1701 STR 22L HAS CORROSION. REPAIRED AFT CARGO STRINGER IAW ERA 567741-14 REV ORIGINAL.

Part: REPAIR — GOUGED (NR 1 ENGINE) · airframe 80,635 hrs · 35,814 cycles

NR 1 ENGINE OUTBD FIREWALL STA 102.0 HAS AN EXISTING REPAIR GOUGED. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR ON 31 ENGINE O/B FIREWALL STA 102.0 IAW ERA 567740-14 REV ORIGINAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,633 hrs · 35,812 cycles

BULK CARGO COMPT FS 1681 FRAME FWD FACE IS CORRODED BETWEEN STR 29L & STR 29R. FABRICATED, LOCATED, DRILLED & INSTALLED SHEAR TIE IAW SRM 51-40-02 & SRM 51-40-05.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,633 hrs · 35,812 cycles

AFT CARGO STA BETWEEN 1681-1701 STR 24L IS CORRODED. REMOVED CORROSION AND EVALUATED AFT CARGO STRINGER 24 LEFT BETWEEN STA 1681-1701. CUT OUT DAMAGED SECTION AND REPAIRED STRINGER 24L IAW SRM 53-00-53 REPAIR 1.

Part: PUSHROD — CORRODED (L4 DOOR) · airframe 80,633 hrs · 35,812 cycles

4L DOOR LWR GATE PUSH ROD FOR GIRT BAR CRANK IS CORRODED. REMOVED AND REPLACED L-4 DOOR LOWER GATE GIRT BAR PUSH ROD IAW SRM -51-40-02 ADJUSTMENT/OPS CHECK TO BE PERFORMED ON AMDS 2040-0057-4L.

Part: FRAME SPLICE — CORRODED (BS 1420) · corrosion level 2 · airframe 80,633 hrs · 35,812 cycles

AFT CARGO BAY BS 1420, STRINGER 24, THE FRAME DOUBLER HAS CORROSION AT FASTENER. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME SPLICE IAW SRM 51-40-02, AND DWG 146N1011, REV A.

Part: WEB — CORRODED (BS 1717) · corrosion level 2 · airframe 80,633 hrs · 35,812 cycles

PASSENGER CABIN HAD THREE AREAS OF CORROSION BS 1717 ON THE FLOOR WEB LBL 40 TO LBL 50. CUT OUT THE DAMAGED SECTION AND REPAIRED THE FLOOR WEB IAW IAW SRM 53-60-51, REPAIR 18.

Part: CUSP WEB — CRACKED (BS 418) · airframe 80,633 hrs · 35,812 cycles

PASSENGER CABIN HAS A CRACKED CUSP WEB BS 418, LBL 53. REMOVED, FABRICATED AND INSTALLED A NEW CUSP WEB IAW SRM 51-40-02, 51-30-01, AND DWG 141N8322, REV.F, & REV V.

Part: ATTACH ANGLE — CRACKED (BS 660) · airframe 80,633 hrs · 35,812 cycles

MAIN DECK FLOORBEAM HAS A CRACKED VERTICAL INTERCOSTAL ATTACH ANGLE AT BS 660, RBL 48. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, 51-30-01, AND DWG 143N5140, REV PL, REV BJ.

Part: CREASE BEAM — CORRODED (BS 900) · corrosion level 2 · airframe 80,633 hrs · 35,812 cycles

RIGHT SIDE CREASE BEAM ANGLE AT BS 900 HAD EXFOLIATED CORROSION. FABRICATED, LOCATED, & DRILLED A NEW SECTION OF THE CREASE BEAM, REPAIR STRAP & CHANNEL. INSTALLED IAW SRM 51-40-02, AND SRM 53-00-13, REPAIR 1 41.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,385 hrs · 35,709 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE AT THE L1 DOOR. REPLACED THE LAMPS IAW AMM 33-51.

Part: SUPPORT ANGLE — DAMAGED (BS 1520-1540) · airframe 78,981 hrs · 35,212 cycles

THE BS 1520 TO 1540 GILLINER SUPPORT ANGLE DAMAGED. PERFORMED THE SPLICE REPAIR IAW SRM 51-70-11, AND SRM 51-70-11.

Part: FRAME — CRACKED (BS 620) · airframe 78,981 hrs · 35,212 cycles

FRAME, BS 620 CENTER BRACKET HOLE INDICATES A CRACK. THE FRAME HOLE WAS BROUGHT .216 TO REMOVE THE CRACK INDICATION. PERFORMED HFEC IAW NDT MANUAL PARTS 6, 51-00-16, NO CRACK INDICATED. DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05, INSTALLED THE NEW STRINGER CLIP IAW SRM 51-40-02, AND ENGINEERING DEVATION AUTHORIZATION DWG 005W0900, & ER/A 560343-14.

Part: UNKNOWN — MALFUNCTIONED (LE SLAT) · airframe 77,779 hrs · 34,816 cycles

DURING FLAP EXTENSION 225 KTS; LEADING EDGE SLANT DISAGREE" LIGHT AND FLAP INDICATOR BETWEEN UP AND 1. RAN QRH CHECKLIST FOR SLAT DISAGREE & LE SLAT ASYMMETRY. OPS NORMAL, FLAP 20 LDG. REPLACED FSEU 3 AMM 27-51-01. FOUND RT LE POS XMITTER READING 9.64 DEGREES. ADJUSTED TO 8.90 DEGREES PER AMM 27-58. INSTALLED NEW SOLENOID VALVE ASSY ON NEW FLAP + SLAT MODULE. REINSTALLED FLAP+ SLAT MODULE + ORIGINAL LT PRESS/SENSITIVE FLOW LIMITER AS PER AMM 27-51. REPLACED PRESSURE - SENSITIVE FLOW LIMITER FOR LEFT HYD SYS PER AMM 27-51. T/S PER AMM 27-81-00. FOUND LE PDU INPUT CABLES LESA + LESB CABLE TENSION LOW. TENSION CABLE PER AMM 27-81. OPS CHECKS NORMAL. RII REQUIRED INSPECTION C/W

Part: FLOOR SUPPORT — BROKEN (BS 760-780) · airframe 77,303 hrs · 34,661 cycles

FLOOR SUPPORT UPPER ANGLE BETWEEN BS 760 AND 780 BL 0 WAS FOUND BROKEN IN SEVERAL PLACES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG.

Part: LENS — DAMAGED (CABIN) · airframe 77,294 hrs · 34,656 cycles

EMERGENCY ISLE LIGHTS DAMAGE AT SEATS 3,6,26,27. REMOVED AND REPLACED LENS FOR EMERGENCY ISLE LIGHTS AT SEATS 3,6,26,27 PER MM 33-52.

Part: SKIN — CORRODED · corrosion level 2 · airframe 75,516 hrs · 33,829 cycles

FUSELAGE LOWER SURFACE HAS SURFACE CORROSION BETWEEN FORWARD LAV . SERVICE DOOR, MEC ACCESS DOOR, AND THE ANTENNA FWD OF THE MEC ACCESS DOOR. C/W ERA 545967-14. REFINISHED IAW PS 900-3-6, 36.

Part: BALL SCREW — CORRODED (TE FLAPS) · airframe 75,486 hrs · 33,815 cycles

NR 2 FLAP DRIVE BALLSCREW, HAS CORROSION, PITTING ON FWD END ATTACH POINT TO UNIVERSAL. REPLACED BALLSCREW IAW AMM 27-51-21.

Part: ACCESS DOOR — CORRODED · airframe 75,486 hrs · 33,815 cycles

LOWER SURFACE OF THE MEC ACCESS DOOR HAS SURFACE CORROSION. REMOVED MEC DOOR FOR SHOP VISIT.

Part: BALL SCREW — CORRODED (NR 7 FLAP) · airframe 75,486 hrs · 33,815 cycles

NR 7 FLAP TRACK BALL SCREW HAS CORROSION IN PINS. R & R NR 7 BALLSCREW IAW R/C.

Part: BALL SCREW — CORRODED (NR 2 TE FLAP) · airframe 75,486 hrs · 33,815 cycles

NR 2 FLAP DRIVE BALLSCREW HAS CORROSION ON FWD END ATTACH POINT TO UNIVERSAL. REMOVED NR 2 BALLSCREW FOR SHOP REPAIR. REPLACED NR 2 BALLSCREW IAW MM 27-51-21.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 73,534 hrs · 33,030 cycles

EMERGENCY LIGHTS CAME ON STEADY DURING FLIGHT. CYCLING EMERGENCY LIGHTS, SWITCHED TO OFF AND ARMED, LIGHTS EXTINGUISHED. FOUND RT NLG CONTROL PANEL SWITCH PIN 2 GROUNDING, REPLACED THE SWITCH, OPS NORMAL IAW AMM 33-51.

Part: INTERCOSTAL — CORRODED (BS 1212) · airframe 71,899 hrs · 32,355 cycles

CORROSION ON INTERCOSTAL BS 1212 BETWEEN LONGERON 29-30R AT AFT CARGO BAY. CORROSION REMOVED, WITHIN LIMITS IAW SRM 51-30-2, 51-10-3, PAR 26, 21, 14, 38 AND ERA NR 511165-14 MA, REV B.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,290 hrs · 32,094 cycles

FIRST CLASS EMERGENCY AISLE LIGHTS WILL NOT LIGHT UP. R & R EMERGENCY LIGHTS POWER SUPPLY CHARGER TRAY AT POSITION M9101 IAW AMM 33-51. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (ROW CD) · airframe 71,290 hrs · 32,094 cycles

EMERGENCY AISLE LIGHT AT ROW 1CD INOPERATIVE. R & R EMERGENCY AISLE LIGHT ASSY IAW AMM 33-51. OPS CHECKED GOOD.

Part: DUCT — DETACHED (CABIN PRESSURE) · airframe 70,696 hrs · 31,799 cycles

PRESSURE AT FL380, AUTO 1 PRESSURE FAIL. CABIN WENT TO 10K AND ALT WARNING. DESCENDED TO FL10 AND CONTINUING TO DESTINATION. NO MASKS DROPPED. DISCOVERED BLOWN DUCT. REPAIRED DUCT, COUPLINGS & CLAMPS. PACK LEAK CHECK GOOD.

Part: SLIDE — MALFUNCTIONED (RT OVERWING) · airframe 70,609 hrs · 31,755 cycles

SCHEDULED TEST DEPLOYMENT OF RT OFFWING ESCAPE SLIDE TOOK EXTENDED AMOUNT OF TIME. R & R SLIDE.

Part: SLIDE — NO TEST (RT OVERWING) · airframe 70,574 hrs · 31,741 cycles

RIGHT OFF-WING ESCAPE SLIDE FAILED TO DEPLOY WITHIN THE MAX ALLOTED TIME. R & R SLIDE.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 69,539 hrs · 31,332 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 19DEF FOUND WIRES AT SEAT TO SEAT CONNECTOR PULLED LOOSE OF CONNECTOR. TERMINATED SEAT TO SEAT CONNECTOR AT 19D, OPS CHECKED NORMAL.

Part: SKIN — DENTED (BS 1720) · airframe 69,471 hrs · 31,309 cycles

SKIN DENTED BS 1720, STRINGER 28L. REPAIRED IAW ERA 501946-14, REV A.

Part: SNUBBER — OUT OF TOLERANCE (L2 DOOR) · airframe 69,249 hrs · 31,211 cycles

SNUBBER FOR L2 DOOR, PIN IS BELOW FLUSH. REPLACED SNUBBER ON L2 DOOR IAW AMM 52-11-10.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 69,191 hrs · 31,177 cycles

FLOOR EMERGENCY PATH LIGHTS 28DEF TO 45DEF INOPERATIVE. SECURED SEAT TRACK WIRING AT ROW 40DEF, IAW SWPM 20.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,965 hrs · 31,066 cycles

DURING SERVICE CHECK, FOUND EMERGENCY ESCAPE LIGHTS ROW 38-45 INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51, & WDM 33-51-16.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,965 hrs · 31,066 cycles

DURING SERVICE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS VERY DIM ROWS 27-37. REPLACED BATTERY PACK, LIGHTS CHECKED GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 68,877 hrs · 31,036 cycles

FOUND EMERGENCY LIGHTS DIMMER AFT OF EMERGNCY EXIT ROW. TOTALLY INOPERATIVE AFT OF ROW 36. REPLACED TWO BATTERY PACKS. FOUND WIRE SHORTED IN FLOOR TRACK AT SEAT 38DEF. REPAIRED. CHECKED NORMAL.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 66,651 hrs · 30,168 cycles

DURING EMERGENCY LIGHT TEST, FOUND SEATS 40D-45D OUT. SEATED EMERGENCY POWER BATTERY SUPPLY. OPS CK GOOD.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 66,258 hrs · 29,993 cycles

DAMAGE WAS FOUND ON THE UPPER HINGE CUTOUT OF THE FORWARD FRAME ON THE SUBJECT R2 DOOR. REF ERA 06-498709-14, REV A.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 64,918 hrs · 29,456 cycles

MX DISCOVERED THE EMERGENCY LIGHT AT SEAT 3C INOPERATIVE. FOUND BROKEN WIRE UNDER SEAT INTHE MIDDLE OF RUN. REPAIRED BROKEN WIRE IAW WSPM 20-30. LIGHT CHECKS OK.

Part: SKIN — DAMAGED (BS 1180 S28-29R) · airframe 63,793 hrs · 28,946 cycles

ELONGATED FASTENER HOLE IN SKIN AT BS 1180, BETWEEN STR 28 AND 29R, RBL 15 AND WL 140. REPAIRED IAW ERA 503142-14 REV ORIG.

Part: SHEAR TIE — CORRODED (BS 1460 S29-30R) · airframe 63,793 hrs · 28,946 cycles

AFT PIT BILGE SHEAR TIE CORRODED BS 1460, BETWEEN STR 29R AND 30 C/L. REPAIRED IAW ERA 503139-14 REV ORIG.

Part: SHEAR TIE — CRACKED (BS 1701 S2R) · airframe 63,793 hrs · 28,946 cycles

MAIN CABIN, CEILING AREA SHEAR TIE CRACKED AT BS 1701 AT STRINGER 2R. REPAIRED IAW ERA 503154-14 REV ORIG.

Part: FRAME — DENTED (BS 1300 S26R) · airframe 63,793 hrs · 28,946 cycles

AFT CARGO BAY FRAME DENTED BS 1300, STRINGER 26R. REPAIRED IAW ERA 501941-14 REV ORIG.

Part: SKIN — CHAFED (BS 1855-1875) · airframe 63,793 hrs · 28,946 cycles

AFT FUSELAGE, EXTERNAL SKIN WORN LT SIDE HORIZONTAL STAB CUTOUT AREA, BS 1855-1875 STR 16L- STR 15L. REPAIRED IAW ERA 501944-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 617 S27L) · airframe 63,793 hrs · 28,946 cycles

DENT AT BS 617 AT SKIN LAP IS OUT OF LIMITS IAW SRM 53-00-01. REPAIRED PER ERA 501945-14.

Part: SKIN — DENTED (BS 655 S18L) · airframe 63,793 hrs · 28,946 cycles

DENT AT BS 655 WAS FOUND TO BE OUT OF LIMITS. REPAIRED PER ERA 503145-14.

Part: SKIN — DENTED (BS 738-761) · airframe 63,793 hrs · 28,946 cycles

THREE DENTS AT BS 738, BS 757 AND BS 761, OUT OF LIMITS, REPAIRED PER ERA 503141-14.

Part: SKIN — DENTED (BS 1720 S29-30L) · airframe 63,793 hrs · 28,946 cycles

DENT AT BS 1720 STR 29 - 30L, OUT OF LIMITS. REPAIRED PER ER/A 501964-14.

Part: FRAME — CORRODED (BS 1460) · corrosion level 2 · airframe 69,539 hrs · 31,332 cycles

FUSELAGE FRAME BS 1460, S29-30R CORRODED.

Part: SKIN — DENTED (BS 635-660) · airframe 63,793 hrs · 28,946 cycles

LEFT SIDE OF THE FUSELAGE FWD OF THE L2 DOOR FIVE DENTS LOCATED BETWEEN BS 635-660 STRINGERS 14L AND 19L. REPAIRED PER ERA 503144-14.

Part: BULKHEAD — WORN (NR 1 PYLON) · airframe 63,793 hrs · 28,946 cycles

NR 1 PYLON AFT BULKHEAD OUTBOARD LOWER CORNER IS WORN. REPAIRED IAW ERA 501947-14AD REV ORIGINAL.

Part: FRAME — DENTED (BS 1320 S26R) · airframe 63,793 hrs · 28,946 cycles

AFT CARGO BAY FRAME DENTED, BS 1320, S26R. REPAIRED IAW SRM 53-00-07.

Part: FRAME — DENTED (BS 1500 S26L) · airframe 63,793 hrs · 28,946 cycles

AFT CARGO LEFT FRAME DENTED BS 1500 STR 26L. REPAIRED FRAME IAW SRM 53-00-07 FIG 201.

Part: SHEAR TIE — CRACKED (FS 839 S13R) · airframe 63,793 hrs · 28,946 cycles

MAIN CABIN, FS 839, S13R, SHEAR TIE CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 680-740) · airframe 63,793 hrs · 28,946 cycles

MAIN CABIN FLOOR SUPPORT ANGLE CORRODED UNDER DRAIN PAN, BS 680 - 740, LBL 65. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02.

Part: SKIN — DENTED (BS 428 S23L) · airframe 63,793 hrs · 28,946 cycles

SKIN DENT AT BS 428 AT S23L . DAMAGE CUT OUT AND DOUBLER FABRICATED AND INSTALLED PER SRM 53-00-01 FIG 201.

Part: FRAME — DENTED (BS 580 S25L) · airframe 63,793 hrs · 28,946 cycles

FORWARD CARGO BAY LEFT FRAME DENTED AT BS 580, S25L. REPAIRED IAW SRM 53-00-07 REPAIR 5 FIG 201 DETAIL 3.

Part: FRAME — DENTED (BS 600 S25L) · airframe 63,793 hrs · 28,946 cycles

FWD CARGO BAY FRAME DENTED AT BS 600, STR 25L. REPAIRED IAW SRM 53-00-07.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 63,209 hrs · 28,741 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE RECONNECTED THE LIGHT. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 61,685 hrs · 28,060 cycles

DURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHT AT SEAT 6C INOPERATIVE. MX REPAIRED THE SEAT WIRES. OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,485 hrs · 27,089 cycles

LIGHTNING STRIKES ON FUSELAGE AT STA 834 AND 854 AT STRINGER 9R. REPAIR ACCOMPLISHED PER ERA 482199-14. WORKED ON NR CARD 33 AT PSV 16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,485 hrs · 27,089 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN STA 875 STR 9R. REF NR 33 PSV16 - REPAIRED PER ERA 482199-14 REV ORIG. TIME LIMITED REPAIR.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 59,175 hrs · 26,930 cycles

DURING LAYOVER CHECK THE EMERGENCY PATH LIGHT AT ROW 24DEF WAS FOUND TO BE INOPERATIVE. MAINT REPLACED THE EMERGENCY PATH LIGHT WIRE HARNESS AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,042 hrs · 26,860 cycles

SEVERAL EMERGENCY PATH LIGHTS OUT. RECONNECTED AND RELAMPED.

Part: SKIN — CRACKED (BS 395)

FOUND STA 395-17 BETWEEN STR 16R AND 17R SKIN DENTED. SKIN DENTED OUT OF LIMITS AND STRINGER 16R CRACKED. CUT OUT DENTED SKIN AND CRACKED SECTION OF STRINGER. FABRICATED SKIN AND STRINGER REPAIR IAW B757 SRM 53-00-01 FIG 101 AND B757 SRM 53-00-03 FIG 201. SKIN REPAIR IS CLASS B AND HAS REINSPECT THRESHOLD AS REQUIRED IN B757 SRM 53-00-01 FIG 203 DETAIL II.

Part: TIRE — FAILED (MLG) · airframe 44,251 hrs · 20,571 cycles

TOWER REPORTED BLOWN TIRE ON LANDING NR 5 POSITION. REPLACED NR 5 AND NR 6 MAIN TIRES. WHEEL ASSYS IAW M/M.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 40,780 hrs · 19,313 cycles

ON INSPECTION FOUND EMERGENCY LIGHTS FWD OF 1R AND 1L DOOR INOP. REPLACED FUSE AT AFFECTED POWER SUPPLY PER MM. OPN OF LIGHTS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 40,780 hrs · 19,313 cycles

ON INSPECTION FOUND EMERGENCY LIGHTS INOP ON AFT RIGHT LAVATORY. REPAIRED THREE BROKEN WIRES UNDER AISLE CARPET AT RT AFT LAVATORY PER WSPM. OPN OF LIGHTS NORMAL.

Part: FRAME — BUCKLED (FUSELAGE) · airframe 27,938 hrs · 13,520 cycles

THE FS 395 BULKHEAD AND ADJACENT LT SKIN PANEL SUFFERED LOCAL BUCKLING FAILURE DUE TO A HARD NOSE LANDING INCIDENT. THE LOWER CAP OF THE BULKHEAD WAS REPLACED AS WELL AS THE LT SKIN PANEL. FRAMES AND STRINGERS IN THE BUCKLING AREA WERE REPAIRED PER THE B727 SRM. THE REPAIRS WERE DOCUMENTED PER ER/A 369396-14, REV A.

Part: EXTINGUISHER — LEAKING (CABIN)

FWD H2O EXTINGUISHER USED, SEAL BROKEN. FOUND SEAL BROKEN ON H2O EXTINGUISHER AND EXTINGUISHER LEAKING. BOTTLE WAS NOT USED. REPLACED H2O EXTINGUISHER. (P/N 267701883) (S/N DL2591) OFF, (S/N DL2207).

Part: UNKNOWN — ODOR (COCKPIT)

STRONG ELECTRICAL ODOR IN COCKPIT. DECLARED EMERGENCY, ACCOMP SMOKE IDENTIFICATION/REMOVEL CHECKLIST. UNABLE TO DETERMINE CAUSE OF ODOR. ISOLATED TO COCKPIT, ODOR DID NOT GO AWAY. REMOVED ALL CAPT AND F/O INSTRUMENTS, INSPECTED BEHIND PANEL, INSPECTED LOWER E/E COMPARTMENTS, NTF RAN ENGINES AND ALL SYS OPN CHECKED NORMAL WITH NO ELECTRICAL ODORS FOUND. CLEANED COFFEE SPILL AT F/O BRIEF CASE AREA.

Part: LANYARD — BROKEN (L 4 DOOR SLIDE)

L-4 SLIDE SAFETY LANYARD FOUND BROKEN DURING ACCOMPLISHMENT OF EO 6-71325-3AD. REPLACED SLIDE ASSY.

Part: BATTERY — DISCHARGED (CABIN)

F/C EMERG SEAT TRACK LIGHTS INOP. REPLACED POWER SUPPLY FUSE AND BATTERY. CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

ESCAPE PATH LIGHTING INOP IN TEST ALL OF FIRST CLASS. REPLACED BATTERY PACK.

Part: MEGAPHONE — DAMAGED (CABIN)

F/A REPORTS, AFT MEGAPHONE BROKEN. REPLACED MEGAPHONE.

Part: EEL WIRE — LOOSE WIRE (CABIN)

ON PREFLIGHT, FWD CABIN FLOOR TRACK EMERGENCY LIGHTS ARE INOP. FOUND LOOSE WIRES IN TRACK AT SEAT ROWS 1 TO 2. REPAIRED WIRES, OPERATION NORMAL.