N938UW

Part: SOCKET — NOT SEATED (R4 DOOR) · airframe 78,946 hrs · 27,933 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE LIGHT DISAGREES WITH DOOR SLIDE ARM. MAINTENANCE FOUND R4 LIGHT SOCKET NOT SEATED AND REINSTALLED LIGHT SOCKET AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 78,898 hrs · 27,920 cycles

AIRCRAFT NOT GROUNDED: EMERGENCY PATH SAT-T-GLO STRIP INOP FROM R1 DOOR TO R2 DOOR. REPLACED EMERGENCY PATH SAT-T-GLO FROM R1 DOOR TO R2 DOOR REF DWG #19P33D1256.

Part: COLLAR — BROKEN (L2 GUST LOCK) · airframe 78,800 hrs · 27,892 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS 2L GUST LOCK EXTREMELY STICKY. MAINTENANCE REPLACED HOLD-OPEN LOCK COLLAR ON 2L DOOR IAW AMM 52-11-08. OPS CHECK GOOD.

Part: BLEED VALVE — FAULTY (LT ENGINE) · airframe 78,105 hrs · 27,733 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF LEFT ENGINE BLEED FAULT INDICATION. FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PRSOV IAW AMM 36-11-09, WHILE TROUBLESHOOTING BLEED ISSUE FOUND FWD DUCT OF PRSOV DAMAGED AND LEAKING, REMOVED AND REPLACED FLEX JOINT DUCT ASSEMBLY IAW AMM 36-11-01. NEW JOINT DUCT ASSEMBLY WAS NOT COMPLETE ORDERED NEW PARTS FOR ASSEMBLY AND INSTALLED PRESSURE TAP ASSEMBLY IAW AMM 36-11-01. REMOVED AND REPLACED PNEUMATIC OVERTEMP LIMITING SENSOR IAW AMM 36-11-13-004. PERFORMED IDLE LEAK CHECK- NO LEAKS. PERFORMED TAKE OFF POWER TEST #13, NO FAULTS AT THIS TIME. PERFORMED TAKE OFF POWER WITH BLEEDS ON AND NO FAULTS.

Part: CONTROL VALVE — FAILED (LT BLEED SYS) · airframe 78,071 hrs · 27,726 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF PRESSURIZATION ISSUE. LEFT ENGINE BLEED FAILURE AFTER RH BLEED ON MEL. MAINTENANCE REPLACED FAN AIR VALVE IAW AMM 36-11-16-404-096-001. OPS AND LEAK CHECK GOOD.

Part: TRANSITION PANEL — CORRODED (BS 1480-1520) · corrosion level 2 · airframe 77,866 hrs · 27,673 cycles

CORROSION WAS FOUND ON THE TRANSITION PANEL, BS 1480 - 1520, LBL 16 IN THE AFT CARGO BAY. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R-2, 51-40-02, & 51-20-10.

Part: PANEL — DELAMINATED (ZONE 100) · airframe 77,537 hrs · 27,592 cycles

DELAMINATED PANEL 611BB AT THE CORNER. REPAIRED THE PANEL IAW SRM 57-41-01AND B757 SRM 51-70-03.

Part: BOTTLE — LOW PRESSURE (R4 DOOR SLIDE) · airframe 77,537 hrs · 27,592 cycles

R4 DOOR SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE SLIDE IAW JC 19L80025002.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 76,442 hrs · 27,347 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR SLIDE PRESSURE LOW. MAINTENANCE REPLACED R4 DOOR SLIDE/RAFT PER JOB CARD 19L80025002 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — FAILED (CABIN) · airframe 76,407 hrs · 27,337 cycles

THE AIRCRAFT WAS NOT GROUNDED. PHOTOLUMINESCENT TEST COUPON FAILED. DUE TO REPORT TO ENGINEERING THAT THE PHOTOLUMINESCENT TEST COUPON HAS FAILED ACCOMPLISH LIGHT PATH REPAIRS PER EA 280866. REPLACED FIRST CLASS RIGHT SIDE STRIPS AND BUSINESS CLASS RIGHT SIDE STRIPS TO R2 DOOR PER EA 280866. ALL PATH LIGHTING OPERATIONS CHECK GOOD.

Part: WINDOW — CRACKED (L4 DOOR) · airframe 76,097 hrs · 27,271 cycles

AIRCRAFT WAS GROUNDED. DOOR L4 WINDOW PRISM CRACKED. REPLACED DOOR L4 WINDOW PRISM PER AMM 56-31-02.

Part: STRUCTURE — CRACKED (ZONE 400) · airframe 75,975 hrs · 27,241 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND PYLON STRUT HAS CRACK INDICATIONS AT THE INBOARD THRUST REVERSER AFT MOUNT BOTH UPPER AND LOWER FASTENER HOLES. REPAIRED RIGHT HAND PYLON STRUT PER EA 278784.

Part: COOLING FAN — BURNED OUT (E&E BAY) · airframe 74,522 hrs · 26,905 cycles

AIRCRAFT WAS NOT GROUNDED. ELECTRICAL ODOR IN BOTH THE COCKPIT AND CABIN DURING CRUISE. TURNED OFF THE ENTERTAINMENT SYSTEM AND LEFT RECIRCULATION FAN AND ODOR WENT AWAY. REMOVED AND REPLACED BURNED OUT #1 FORWARD EQUIPMENT COOLING SUPPLY FAN PER AMM 21-58-06. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 74,333 hrs · 26,864 cycles

R1 DOOR WILL NOT ARM. REINSTALLED GIRT BAR IAW AMM 52-11-00-862-007. OPERATIONAL CHECK GOOD.

Part: RESERVOIR — LOW PRESSURE (R2 DOOR SLIDE) · airframe 74,043 hrs · 26,809 cycles

AIRCRAFT WAS GROUNDED. R2 DOOR EMERGENCY EVACUATION SLIDE RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSEMBLY. OPS CHECKED GOOD.

Part: GIRT BAR — DAMAGED (R1 DOOR SLIDE) · airframe 74,032 hrs · 26,807 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR IS DISLODGED AND FOOT REMOVED. FOUND GIRT BAR SPRINGS FLAT ON ONE END. REMOVED AND REPLACED GIRT BAR. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: GUARD — OUT OF ADJUST (LIGHT SWITCH) · airframe 73,966 hrs · 26,795 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS SWITCH GUARD TURNS SWITCH TO OFF POSITION WHEN IT IS DOWN. ADJUSTED GUARD. OPS CHECKED GOOD.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 73,645 hrs · 26,732 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR EMERGENCY EVACUATION SLIDE RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED SLIDE/RAFT IAW JOB CARD 19L80025002. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,468 hrs · 26,693 cycles

AIRCRAFT WAS NOT GROUNDED. CORROSION ON AFT CARGO PIT INTERCOSTAL, LOWER FORWARD CORNER, AT FUSELAGE STATION 1620, S29R. REPAIRED INTERCOSTAL IAW SRM 51-70-11-0G AND SRM 51-40-02.

Part: PIN — BROKEN (ESCAPE SLIDE) · airframe 73,008 hrs · 26,588 cycles

RIGHT EMERGENCY EXIT DOOR ESCAPE SLIDE, AFT RELEASE CABLE PIN, SAFETY STRING BROKEN. REPLACED THE PIN BREAKAWAY TIE IAW CMM 25-61-28.

Part: SKIN — CORRODED (BS 1672) · airframe 73,008 hrs · 26,588 cycles

CORROSION ON FUSELAGE SKIN UNDER AFT DRAIN MAST BETWEEN STRINGERS 25 - 26R. REPAIRED THE SKIN IAW SRM 53-00-01 AND SRM 51-40-02.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR SLIDE) · airframe 72,715 hrs · 26,516 cycles

THE R1 DOOR SLIDE LIGHT FOUND INOPERATIVE. MAINTENANCE FOUND AND REMOVED A SMALL ALCOHOL BOTTLE STUCK UNDER THE GIRT BAR AND ACCOMPLISHED SATISFACTORY OPS CHECK.

Part: WIRE — BROKEN (HANDLE SWITCH) · airframe 72,616 hrs · 26,489 cycles

SETTING TAKEOFF POWER WE GOT SPOILERS CAUTION AND CONFIGURATION WARNING WITH HORN. ABORTED TAKEOFF, WENT TO RUNUP AREA AND GOT THE SAME SYMPTONS WHEN THRUST IS ABOVE 1.5 EPR. AIRCRAFT WAS GROUNDED. MAINTENANCE FIXED A BROKEN WIRE AT TBL190 FOR SPOILER HANDLE SWITCH S493 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 31-51-00.

Part: APU — SPARKS · airframe 72,471 hrs · 26,458 cycles

SEVERAL GROUND CREW MEMBERS OBSERVED SPARKS COMING OUT OF APU EXHAUST. AIRCRAFT WAS GROUNDED. REPLACED APU.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 72,456 hrs · 26,453 cycles

R1 DOOR SLIDE BELOW MINIMUM PRESSURE REQUIREMENTS. REPLACED DOOR R1 EVACUATION SLIDE.

Part: CONNECTOR — SHORTED (ZONE 700) · airframe 72,351 hrs · 26,419 cycles

NLG EMERGENCY EXTERIOR LIGHT TEST SWITCH INOP FOR L3 AND R3 DOORS. FLIGHT DECK AND FAP TEST CORRECTLY. REMOVED AND REPLACED CONN D40488P IAW STANDARD WIRING PRACTICES 20-60-03. OP'S CK'S GOOD. THE AIRCRAFT WAS NOT GROUNDED.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 72,053 hrs · 26,325 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR WOULD NOT ARM. FOUND DEBRIS INTERFERING WITH THE 1R GIRT BAR REMOVED DEBRIS AT 1R TRACK AND PERFORMED OPERATIONAL CHECK PER AMM 52-11-00-201 ARMED WITH NO ISSUES.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 72,001 hrs · 26,310 cycles

AIRCRAFT WAS GROUNDED. DOOR R4 SLIDE PRESSURE BOTTLE BELOW LIMITS. REPLACED R4 DOOR SLIDE RAFT ASSEMBLY PER JOB CARD 19L80025002.

Part: GUST LOCK — INOPERATIVE (L2 DOOR) · airframe 71,975 hrs · 26,299 cycles

GATE AGENT INFORMED MTC L2 DOOR GUST LOCK INOPERATIVE. REMOVED AND REPLACED L2 DOOR LOCK COLLAR IAW AMM 52-11-08-358-001. OPS CK GOOD. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 71,929 hrs · 26,281 cycles

FLIGHT ATTENDANT`S FLASHLIGHT WAS FOUND INOPERATIVE AT POSITION 4L. REPLACED THE BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 71,920 hrs · 26,279 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1R SLIDE LIGHT DOES NOT LIGHT UP WHEN DOOR IS ARMED. REMOVED OBSTRUCTION FROM GIRT BAR.

Part: STOP PIN — OUT OF ADJUST (SERVICE DOOR) · airframe 71,854 hrs · 26,265 cycles

AIRCRAFT WAS GROUNDED: LEFT AFT SERVICE DOOR INDICATOR LIGHT EICAS SHOWED OPEN.HANDLE INSIDE DRIFTS UP POSITION.LIGHT OUT WHILE WEIGHT IS APPLIED TO HANDLE.UNEVENTFUL.MAINTENANCE FOUND STOP PINS OUT OF ADJUSTMENT AND PROPERLY ADJUSTED THE STOP PINS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: MONITOR — FAILED (CABIN) · airframe 71,354 hrs · 26,148 cycles

WHILE AT CRUISE, THE FLIGHT CREW REPORTED AN ACRID ODOR THROUGH OUT CABIN THAT LASTED ABOUT 5 MINUTES. FLIGHT ATTENDANT REPORTED THAT THE OVERHEAD MONITOR SMOKED WHICH RESULTED IN THE CREW TURNING OFF THE VIDEO. THE ODOR DISSIPATED. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE MONITORS AT ROW 9 AND 15 IAW AMM 23-32-00-800-802.

Part: SPRING — BINDING (R1 DOOR) · airframe 71,281 hrs · 26,128 cycles

R1 DOOR COVER OFF AND SLIDE WOULD NOT DISARM. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE AFT LEAF SPRING BINDING, STRAGHTENED SPRING AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-66-01. MAINTENANCE INSTALLED SLIDE COVER.

Part: STRAP — OUT OF ADJUST (R1 DOOR) · airframe 71,026 hrs · 26,063 cycles

DOOR 1 RT UNABLE TO ARM. FOUND SLIDE STRAP UNDER THE GIRT BAR. STRAP WAS ADJUSTED AND A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 70,689 hrs · 25,971 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR GIRT BAR APPEARS LOOSE. REATTACHED R1 DOOR GIRT BAR IN THE DOOR FITTINGS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-66-10-201.

Part: SLAT — DEBONDED (LT WING) · airframe 70,255 hrs · 25,855 cycles

AIRCRAFT WAS GNDED. LT WING NR 5 SLAT HAS AREA OF DISBOND 4" FROM THE UPPER INBD EDGE. REPLACED SLAT IAW AMM 27-81-01 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — MISSING (ZONE 800) · airframe 70,034 hrs · 25,790 cycles

AIRCRAFT WAS NOT GNDED. DOOR 1L SLIDE LIGHT MISSING. INSTALLED MISSING DOOR SLIDE LENS AT THE 1L DOOR.

Part: ACTUATOR — DEFECTIVE (R4 DOOR) · airframe 69,859 hrs · 25,747 cycles

AIRCRAFT WAS NOT GNDED. R4 DOOR SLIDE LIGHT INOPERATIVE. INSTALLED GIRT BAR SLIDER PROXIMITY TARGET, ACTUATOR, IAW AMM TR 25-017AW. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (L1 DOOR) · airframe 69,612 hrs · 25,689 cycles

AIRCRAFT WAS NOT GNDED. LENS COVER MISSING ON SLIDE ARMED INDICATOR AT DOOR 1L. REPLACED L1 SLIDE ARMED INDICATOR LIGHT LENS, OPERATIONAL CHECKED GOOD.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 69,175 hrs · 25,582 cycles

AIRCRAFT WAS NOT GNDED. WHEN 1R DOOR IS OPEN A LANYARD HANGS BELOW SLIDE. REPOSITIONED SLIDE LANYARD & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GOVERNOR — DEFECTIVE (RT ENGINE) · airframe 68,837 hrs · 25,486 cycles

NUMBER 2 ENG FAILED & SHUTDOWN ON TAKEOFF ROLL. STATUS MSG RT ENG LOW PRESS PUMP. REPLACED THE RT ENGINE FUEL FLOW GOVERNOR & HIGH PRESS FUEL PUMP. ACCOMPLISHED SATISFACTORY LEAK & OPERATIONAL CHECKS. SEE AALA201511109028 FOR ADDITIONAL PART INFORMATION.

Part: PUMP — DEFECTIVE (NR 2 ENGINE) · airframe 68,837 hrs · 25,486 cycles

NUMBER 2 ENG FAILED & SHUTDOWN ON TAKEOFF ROLL. STATUS MSG, RT ENG LOW PRESS PUMP. REPLACED THE RT ENG FUEL FLOW GOVERNOR & HIGH PRESS FUEL PUMP. ACCOMPLISHED SATISFACTORY LEAK & OPERATIONAL CHECKS. SEE AALA201511109005 FOR ADDITIONAL PART INFORMATION.

Part: FITTING — DETACHED (GIRT BAR) · airframe 68,622 hrs · 25,415 cycles

R1 DOOR, FITTING CAME OFF GIRT BAR. RE-INSTALLED GIRT BAR FITTING. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 26-66-10-202-039.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 68,442 hrs · 25,379 cycles

1R DOOR DOES NOT ARM & DISARM PROPERLY. REMOVED DEBRIS & CLEANED GIRT BAR. DOOR ARM OPERATION TESTED SATISFACTORY.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 68,306 hrs · 25,342 cycles

DOOR 1R WILL NOT CLOSE & CANNOT ARM. REMOVED DEBRIS FROM FLOOR & GIRT BAR RETAINER. NO FURTHER DEFECTS NOTED AMM 52-11-00-862-077.

Part: STRAP — UNSECURE (R1 DOOR) · airframe 68,094 hrs · 25,293 cycles

TOWER FOREMAN REPORTED R1 DOOR HAS SOMETHING HANGING. SECURED BUSTLE STRAP WHEN R1 SLIDE WAS REPLACED. OK FOR SERVICE.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 68,094 hrs · 25,293 cycles

FLIGHT 837 EN-ROUTE, ALL CREW NOTICED STRONG ODOR ESPECIALLY IN COCKPIT & NEAR 2L DOOR. FLIGHT ATTENDANT DISABLED INFLIGHT ENTERTAINMENT & SMELL DISSIPATED. COMPLIED WITH JC 19L00021001. R & R RT CABIN RECIRCULATION FAN IAW AMM 21-25-01-404-094 & 21-25-01-004-092. OPERATIONS CHECKED GOOD, NO ODOR NOTED.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 67,941 hrs · 25,255 cycles

C1 CHECK, CORROSION ON FORWARD CARGO LEFT SIDE PANEL BETWEEN STATION 510 & 645 AT LBL 22. REPAIRED SIDE PANEL IAW SRM 53-00-53-2R-2.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,941 hrs · 25,255 cycles

C1 CHECK, CORROSION ON FORWARD CARGO LEFT SIDE PANEL BETWEEN STATION 645 & 705 AT LBL 22. REPAIRED SIDE PANEL IAW SRM 53-00-53-2R-2.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,941 hrs · 25,255 cycles

C1 CHECK, CORROSION ON SIDE PANEL BETWEEN STATION 620 & 645 AT RBL 22. REPLACED SIDE PANEL IAW SRM 53-00-53-1A-1 FIG 101 DET 1 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,941 hrs · 25,255 cycles

C1 CHECK, CORROSION ON FLOOR SUPPORT ANGLE AT STATION 845 BETWEEN LBL 25 & RBL 25. REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-10-02 & 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,941 hrs · 25,255 cycles

C1 CHECK, CORROSION ON FLOOR STRINGER BETWEEN STATION 640 & 660 AT RBL 2.9. REPLACED FLOOR STRINGER IAW SRM 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,941 hrs · 25,255 cycles

C1 CHECK, CORROSION ON SIDE PANEL BETWEEN STATION 645 & 705, RBL 19 & RBL 26. REPLACED SIDE PANEL IAW SRM 51-40-02.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,941 hrs · 25,255 cycles

C1 CHECK, CORROSION ON STRINGER SPLICE AT STATION 630 & RBL 7.55. REPLACED STRINGER SPLICE IAW SRM 51-40-02.

Part: BUSHING — WORN (R1 GIRT BAR)

R1 DOOR FWD GIRT BAR SLIDER ASSEMBLY HAS EXCESSIVE PLAY. REPLACED BUSHING ON R1 DOOR FWD GIRT BAR SLIDER ASSEMBLY IAW SOPM 20-50-03.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

FLASHLIGHT BATTERY AT L1 DOOR ATTENDANT SEAT REQUIRES REPLACEMENT. R & R FLASHLIGHT BATTERY IAW AMM 25-64-00-902-037.

Part: CABLE — OUT OF ADJUST (R1 DOOR)

C1 CHECK, R1 DOOR ASSIST BOTTLE CABLE TRAVEL TO SHORT, FAILED TEST. ADJUSTED CABLES TRAVEL IAW AMM 52-11-32-404. OPERATIONS CHECKED GOOD .940 TRAVEL.

Part: GIRT BAR — FAULTY (R1 DOOR) · airframe 65,901 hrs · 24,658 cycles

DOOR R1 SLIDE BAR LOCK CAME OFF. REINSTALLED BAR LOCK. DOOR ARMS & DISARMS NORMAL. UPON FURTHER REVIEW, MX CONTROL REQUESTED FURTHER INSPECTION. COMPLETED THE INSPECTION & REPLACED THE GIRT BAR FOR THE DOOR R1 ESCAPE SLIDE.

Part: GIRT BAR — DETACHED (R1 DOOR) · airframe 65,896 hrs · 24,656 cycles

NOTIFIED BY CLEANERS THAT THE GIRT BAR ON THE 1R DOOR BECAME DETACHED. FOUND GIRT BAR LOCK KNOCKED OFF GIRT BAR. RE-INSTALLED LOCK.

Part: GIRT BAR — DEFECTIVE (R1 DOOR) · airframe 65,654 hrs · 24,569 cycles

R1 GIRT BAR END DISENGAGED AS FROM BAR AS DOOR IS OPENED. REPLACED GIRT BAR.

Part: FLAP — DELAMINATED (RT WING) · airframe 65,251 hrs · 24,468 cycles

RON VISIT RT INBD TE FLAP IS DELAMINATED BEHIND NR 2 ENG APPROX 9.5 INCHES FROM OTBD EDGE, 29 INCHES LONG & 7 INCHES FROM TE TO LE AT WS 369.5, BBL 70.50. REPLACED IAW JOB CARD 19L50027003.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 63,094 hrs · 23,902 cycles

SJU R1 DOOR GIRT BAR FWD END LOOSE. SECURED R1 DOOR GIRT BAR, R1 DOOR ARMS & DISARMS SLIDE AS REQUIRED.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAP)

FLT 1796, ENROUTE EICAS MESSAGE. TE FLAP DISAGREE WHEN FLAP 1 POSITION SELECTED. FLAPS FAILED TO MOVE TO SELECTED POSITION. ACCOMPLISHED QRH PROCEDURE. R & R FLAP LEVER POSITION TRANSMITTER. NO UNUSUAL CONDITIONS NOTED, PASSED BENCH TEST. CONTAMINATED, CLEANED & TESTED IAW MANUFACTURER`S SPECS.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 62,999 hrs · 23,870 cycles

PHL - FLT 1804 EN-ROUTE PHX TO PHL. FLAPS FAILED TO MOVE. TE LIGHT ON & EICAS MESSAGE TE FLAP DISAGREE DISPLAYED. FLAPS ALSO INOPERATIVE ON TE ALTN SYS. ACCOMPLISHED OPERATIONAL TEST OF THE TE EDGE FLAPS, COULD NOT DUPLICATE, INSPECTED FLAPS & NO FAULTS FOUND.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON SERVO STAND BOX SUPPORT LOWER CHORD AT BS 1860, BL 0. REPAIRED SERVO STAND BOX SUPPORT LOWER CHORD AT BS 1860, B L0 IAW EA 505777 & 505775 & B757 SRM 51-40-02-0G.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON L4 DOOR CUT OUT LOWER FWD SUPPORT ANGLE AT BS 1642, LBL 63. REPLACED L4 DOOR CUT OUT LOWER FWD SUPPORT ANGLE AT BS 1642, LBL 63 IAW B757 SRM 51-10-02, 53-60-15-1A-1, 51-40-02 & DRAWING 146N8769.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,781 hrs · 23,794 cycles

C4 CHECK CRACK ON INTERCOSTAL BETWEEN BS 345 TO BS 365, RBL 44. REPLACED INTERCOSTAL BETWEEN BS 345 TO BS 365, RBL 44 IAW B757 SRM 51-40-02.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 62,781 hrs · 23,794 cycles

C4 CHECK DELAMINATION ON NR 7 SLAT TE WEDGE INBD END LOWER SURFACE AT OSS305. REPAIRED NR 7 SLAT TE WEDGE IAW B757 SRM 51-70-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,781 hrs · 23,794 cycles

C4 CHECK CRACK ON INTERCOSTAL UPPER T CHORD BETWEEN BS 324 TO BS 345, RBL 25. REPAIRED INTERCOSTAL BETWEEN BS 324 TO BS 345, RBL 25 IAW B757 SRM 51-40-02 & DRAWING 141N5150.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

C4 CHECK LEVEL 2 INTERGRANULAR CORROSION ON INTERCOSTAL AT BS 684 BETWEEN LBL 34 TO LBL 44. REPLACED INTERCOSTAL AT BS 684 BETWEEN LBL 34 TO LBL 44 IAW B757 SRM 51-40-02.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN CREASEBEAM CORRODED BETWEEN BS 754 AND 763 AT LBL 64. REPAIRED CREASE BEAM IAW SRM 51-10-02, 53-30-13, 51-40-02, 51-70-12 & 51-20-21.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 3 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 377.7 AND LBL 62. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 720 AND 740 AT RBL 55. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 AND DWG 143N5410.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1655 AND LBL 62. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-60-15-1A-1, 51-40-02, 51-30-01 AND 51-20-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN SEAT TRACK CORRODED AT BS 377.7 AND LBL 44. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 53-00-51-1A & 51-40-02 AND DRAWING 141N5130 & 141N5131.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 397 AND BL 0. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN SEAT TRACK CORRODED AT BS 377.7 AND LBL 24. FABRICTED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 53-00-51-1A & 51-40-02-0G AND DWG 141N5130 & 141N5131.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 395 AND 418 AT RBL 60. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOORBEAM CORRODED AT BS 377.7 AND LBL 62. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-2R-10.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOORBEAM CORRODED BS 365 FROM BL 0 TO RBL 64. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A, 51-40-02-0G & 53-00-51-2R-10.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CREASE BEAM CORRODED BETWEEN BS 680 AND 740 AT RBL 56. R & R CREASE BEAM IAW SRM 51-10-02, 53-00-51-1A & 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 680 AND 700 LBL 56. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02 & 53-00-51-1A AND DWG 143N540.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 72 AND 740 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, FLOOR SUPPORT CORRODED BETWEEN BS 333.45 AND 365.25 RBL 62. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1315 AND LBL 25. R & R SUPPORT IAW SRM 51-40-02, 53-00-51-1A & 51-30-01.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CREASEBEAM CORRODED AT BS 750 AND LBL 55. R & R CREASE BEAM IAW SRM 51-10-02, 51-40-02 & 53-30-13-1A AND DWG 143N8322.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 397 RBL 44. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 AND DWG 141N5162.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1300 AND 1350 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 CORROSION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,781 hrs · 23,794 cycles

C4 CHECK CABIN FLOOR STRUCTURE CLIP CRACKED AT BS 1320 & LBL 25. R & R CLIP IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT ANGLE CRACKED BETWEEN BS 1420 AND 1440 AT BL 0. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT ANGLE IAW DWG 140N2505 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 700 AND 720 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, FLOOR SUPPORT ANGLE CORRODED AT BS 728 AND LBL 67. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT ANGLE IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 AND DWG 143N8322.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1675 AND LBL 62. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-60-15-1A-1 & 51-40-02 AND DWG NR 146N8016.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR SUPPORT WEB CORRODED BETWEEN BS 1300 AND 1320 AT RBL 55. R & R FLOOR SUPPORT WEB IAW SRM 53-60-15-1A, 51-10-02 & 51-40-02 AND DWG 146N8322.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, CORROSION AT CUSP WEB BETWEEN BS 1620 TO 1640, LBL 62. REPLACED CUSP WEB IAW SRM 51-10-02-OG, 53-00-51-1A, 51-30-01, 51-40-02 & DWG 146N8722.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR STIFFENER CRACKED AT BS 1320 AND LBL 50. R & R STIFFENER IAW SRM 51-40-02, CRACK, .5".

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED AT BS 1660 AND RBL 56. R & R FLOOR SUPPORT IAW SRM 53-60-15, 51-40-02 & 51-30-01.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON R4 DOOR LOWER CUT OUT AREA FWD SILL FITTING AT BS 1650, RBL 62. REPLACED FWD SILL FITTING AT BS 1650, RBL 62 IAW B757 SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1640 AND 1682 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-60-15-1A-1, 51-40-02 & 51-40-05.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. FLOORBEAM ANGLE CORRODED AT BS 1678 AND BLB 56. R & R FLOORBEAM ANGLE IAW SRM 51-40-02, 51-40-05 & 53-00-01.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1660 AND 1682 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-10-02, 51-40-02, 51-40-05 & 53-00-51-1A-1.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON L4 DOOR LOWER CUT OUT AREA FWD SILL FITTING AT BS 1670, LBL 62. REPLACED FWD SILL FITTING AT BS 1670, LBL 62 IAW B757 SRM 51-10-02, 53-60-15-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1640 AND 1660 AT BL 0. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON L4 DOOR LOWER CUT OUT AREA FWD SILL FITTING AT BS 1670, LBL 62. REPLACED FWD SILL FITTING AT BS 1670, LBL 62 IAW B757 SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK, FLOOR SUPPORT CORRODED BETWEEN BS 1660 AND 1680 AT BL 0. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1660 AND 1680 AT RBL 9.5. R & R FLOOR SUPPORT IAW SRM 51-30-01 & 51-40-02 AND DWG 146N5191.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,781 hrs · 23,794 cycles

DURING C4 CHECK. CABIN SEAT TRACK CORRODED AT BS 1640 AND LBL 45.5. REPAIRED SEAT TRACK IAW SRM 51-10-02, 53-00-52-1A & 53-00-52-2R-3.

Part: GOVERNOR — MALFUNCTIONED (FUEL FLOW) · airframe 62,776 hrs · 23,792 cycles

ENROUTE, WHEN STARTING A CLIMB FROM 36000 TO 38000, RT ENGINE ROLLED BACK TO IDLE. SEVERAL ATTEMPTS MADE TO RECOVER POWER UNSUCCESSFULLY. ENGINE DID NOT FLAME OUT. CONTINUED FLIGHT AT IDLE POWER, AT LOWER ALTITUDE. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AT 4000 FT, THERE WAS SOME RECOVERY. MAINTENANCE REPLACED RT ENGINE FUEL FLOW GOVERNOR.

Part: LIGHT — LOOSE (ZONE 200) · airframe 62,651 hrs · 23,755 cycles

EMERGENCY LIGHT AT ROW 13 LT SIDE, LOOSE. SECURED EMERGENCY LIGHT AT ROW 13.

Part: LIGHT — LOOSE (CABIN) · airframe 61,446 hrs · 23,435 cycles

EMERGENCY EXIT LIGHTING STRIP ON FLOOR AT ROW 10 IS LOOSE AND STICKING UP. RESECURED STRIP TO FLOOR.

Part: TRACK — LOOSE (CABIN) · airframe 60,792 hrs · 23,275 cycles

CLT - EMERGENCY FLOOR MOUNTED TRACK LIGHTS LOOSE AT ROW 11-12. SECURED FLOOR TRACK LIGHT STRIP AT ROW 11-12.

Part: LENS — DETACHED (CABIN)

PHX - L2 DOOR EMERGENCY EXIT LENS COVER FELL OFF (LENS IN FLT DECK). RE-ATTATCHED EMERGENCY EXIT LENS COVER AT L2 DOOR.

Part: PLACARD — MISSING (R2 DOOR) · airframe 59,729 hrs · 22,929 cycles

ESCAPE PATH MARKING MISSING AT R2 DOOR. MAINTENANCE INSTALLED ESCAPE PATH EXIT ARROW AND STRIPS AS REQUIRED.

Part: COLLAR — BROKEN (L2 DOOR) · airframe 58,506 hrs · 22,544 cycles

L2 DOOR WON'T CLOSE, MAKES LOUD NOISE WHEN TRYING TO CLOSE. MAINTENANCE REMOVED AND REPLACED BROKEN HOLD-OPEN LOCK COLLAR.

Part: SENSOR — LEAKING (COMPRESSOR) · airframe 57,734 hrs · 22,306 cycles

FLT 1579, ON DESCENT, AS POWER WAS ADVANCED TO LEVEL OFF AT 12,000, ALL 3 COCKPIT OCCUPANTS NOTICED A DIRTY SOCK ODOR. AFTER ABOUT 1 MINUTE TURNED OFF RIGHT PACK. ODOR PERSISTED. TURNED OFF LEFT PACK AND ODOR DISAPPEARED QUICKLY. ODOR NOT NOTICED IN CABIN. MAINTENANCE SEALED LEFT ENGINE IP COMPRESSOR CASE SPEED SENSOR TERMINAL BLOCKS IN 3 AND 12 POSITIONS. ALSO, ACCOMPLISHED TASK TO REMOVE OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEM. RAN ENGINES AND PACKS, NO ODOR DETECTED.

Part: WIRE HARNESS — SPARKS (CABIN) · airframe 57,558 hrs · 22,246 cycles

FLT 1560 EN ROUTE. ENTERTAINMENT SYS WIRING SPARKING AT SEAT 12F. REMOVED & INSTALLED NEW AUDIO SYSTEM CABLE AT ROW 12DEF.

Part: RESERVOIR — FAULTY (R1 DOOR) · airframe 57,433 hrs · 22,197 cycles

CLT - R1 DOOR EMERGENCY POWER ASSIST RESEVOIR NEEDS REMOVED AND REPLACED. REPLACED RESERVOIR.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,211 hrs · 22,130 cycles

C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON HAT CHANNEL BETWEEN BS 1380 TO BS 1400, S23R. REPLACED HAT CHANNEL BETWEEN BS 1380 TO BS 1400, S23R IAW B757 SRM 51-40-03.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,211 hrs · 22,130 cycles

C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB AT BS 1400, S27R. REPLACED WEB AT BS 1400, S27R IAW B757 SRM 51-40-02 & BOEING DRAWING 145N5401.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,211 hrs · 22,130 cycles

C3 CHECK - CRACK IN FAIL SAFE STABILIZER STRAP AT BS 365.25, LBL 20. REPAIRED FAIL SAFE STABILIZER STRAP AT BS 365.25, LBL 20 IAW EA 103639.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,211 hrs · 22,130 cycles

C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORTS AT BS 1470 BETWEEN LBL 14 TO RBL 14. REPLACED FLOOR SUPPORTS AT BS 1470 BETWEEN LBL 14 TO RBL 14 IAW B757 SRM 51-70-11.

Part: WEDGE — DEBONDED (TE FLAP) · airframe 57,211 hrs · 22,130 cycles

C3 CHECK - AREA OF DISBOND ON RIGHT INBOARD MAIN FLAP, OUTBOARD TRAILING EDGE WEDGE LOWER SURFACE APPROX 13 INCHES FROM INBOARD END & 6 INCHES FORWARD OF AFT TRAILING EDGE. REPAIRED RIGHT INBOARD MAIN FLAP, OUTBOARD TRAILING EDGE WEDGE LOWER SURFACE IAW B757 57-53-01-01 & SRM 51-70-10.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 56,839 hrs · 22,012 cycles

L1 DOOR ASSIST BOTTLE LOW PRESSURE. REPLACED DOOR ASSIST BOTTLE.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 56,648 hrs · 21,947 cycles

PHL - FLASHLIGHT NOT CHARGING L2 DOOR INBD. REMOVED AND REPLACED BATTERY PACK, F/A FLASHLIGHT L2 INBD POS CHARGING NORM.

Part: PANEL — BROKEN (CABIN) · airframe 56,343 hrs · 21,858 cycles

PHL - EMERGENCY LIGHT UNARMED LIGHT ASSY BROKEN. REPLACED LIGHT PANEL ASSY CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,202 hrs · 21,811 cycles

RON CHECK - CORROSION ON LOWER SECTION OF INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, RBL 3. REPLACED INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, RBL 3 IAW BOEING DRAWING 146N5399 & B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,202 hrs · 21,811 cycles

RON CHECK - CORROSION ON LOWER SECTION OF INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, LBL 3. REPLACED INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, LBL 3 IAW BOEING DRAWING 146N5399 & B757 SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,202 hrs · 21,811 cycles

RON CHECK - CORROSION ON FRAME AT BS 1460 BETWEEN BBL 0 TO RBL 6 & BETWEEN S29R TO S30. REPAIRED FRAME AT BS 1460 BETWEEN BBL 0 TO RBL 6 & BETWEEN S29R TO S30 IAW EA 200659 & 103312.

Part: SEAL — LEAKING (RT ENGINE)

FLT 1043 ENROUTE, RIGHT ENGINE OVERHEATING. THE CREW POWERED BACK THE RIGHT ENGINE AND DECLARED AN EMERGENCY. THE FLIGHT DIVERTED TO PLS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND RING SEAL CLAMP LOOSE ON HP2 DUCT OFF TAKE. REPLACED RING SEAL. OPS CHECKED OK.

Part: FASTENER — SHEARED (NACELLE) · airframe 52,432 hrs · 20,805 cycles

CLT - C2 - MAJOR REPAIR - FASTENER SHEARED AT RIGHT PYLON OUTBOARD UPPER VERTICAL FLANGE FOR STRUT TO DIAGONAL BRACE FITTING AT PPS209.5. REPLACED DAMAGED FASTENER IAW EA 102029A.

Part: SKIN PANEL — DELAMINATED (TAILCONE) · airframe 52,432 hrs · 20,805 cycles

CLT - C2 - MAJOR REPAIR - DELAMINATION ON APU TAIL CONE INTERIOR SKIN PANEL AT BS1990, BL 0. REPAIRED APU TAIL CONE INTERIOR SKIN PANEL AT BS 1990, BL 0 IAW EA 132039.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,432 hrs · 20,805 cycles

CLT - C2 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF CREASE BEAM WEB & T-ANGLE BETWEEN BS 1330 TO BS 1335, S17R, RBL 65. REPLACED CREASE BEAM CHORD BETWEEN BS 1330 TO BS 1335, S17R, RBL 65 IAW B757 DRAWING 146N8322.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,432 hrs · 20,805 cycles

CLT - C2 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF CREASE BEAM WEB AT BS 1330, S17R, RBL 65. REPLACED CREASE BEAM WEB AT BS 1330, S17R, RBL 65 IAW BOEING DRAWING 143N8322.

Part: SLIDE — LOW PRESSURE (R3 DOOR)

PHL - THE R3 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE AT DOOR R3. OK FOR SERVICE.

Part: SLIDE — LOW PRESSURE (R3 DOOR)

PHL - THE EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE AT DOOR R3 WAS LOW. MAINTENANCE REPLACED THE R3 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.

Part: LIGHT — FAILED (ZONE 200) · airframe 45,255 hrs · 18,602 cycles

FLL - EMERGENCY EXIT SIGN AT LEFT AFT DOOR INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY.

Part: SILL — CORRODED (BS 1660-1680) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

RIGHT AFT DOOR SILL STA 1660-1680 CORRODED. REMOVED & REPLACED WITH NEW WEB PER SRM 51-40-00; CORR TASK JL-90-0900; LEVEL 1, DEFECT SIZE: 9 X 1.5 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,627 hrs · 41,627 cycles

FWD END SEAT TRACK LBL 45.5 AT STA 377.7 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER DWG 141N5131 & SRM 51-70-12, DEFECT SIZE: 1.5 INCH X 5 FEET.

Part: CREASE BEAM — CORRODED (BS 324-327) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

BETWEEN STA 324-327 RBL 60 CORRODED. REMOVED & REPLACED 2 CREASE BEAMS PER SRM 51-40-02; CORR TASK JL-46-53500, LEVEL 1, DEFECT SIZE: 120 SQ INCHES.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

SPORADIC CORROSION BETWEEN STA 1681 & 1720 AND FROM LBL 51 - RBL 51 CORRODED. MANUFACTURED FLOOR WEB PER DWG 146N5300; CORR TASK C53-251-03; LEVEL 1, DEFECT SIZE: 5 SQ INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,627 hrs · 41,627 cycles

STA 1661 LBL 4 TOP SIDE OF BEAM AROUND HOLE CORRODED. REPLACED CAP OF FLOORBEAM PER TR 53-15-01, DEFECT SIZE: 1 X 2 INCHES.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

RIGHT CREASE BEAM BETWEEN CHORD & WEB AT STA 1636 CORRODED. REMOVED & REPLACED WEB PER SRM 51-40-02. CORR TASK JA-58-53516, LEVEL 1, DEFECT SIZE: 1 X 3 INCHES.

Part: PANEL — CRACKED (SLAT) · airframe 41,627 hrs · 41,627 cycles

OUTBOARD END OF SLAT COVE PANEL CRACKED. FABRICATED NEW COVE PANEL ABOUT 27 INCHES LONG PER BOEING DWG 114N4003, DEFECT SIZE: 1 INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

NUMEROUS AREAS AROUND SCREW HOLES, TOP OF FLOORBEAM STA 377.7 CORRODED. INSTALLED T-CAP & SPLICE ANGLES PER SRM 53-00-51; CORR TASK JL-46-53500; LEVEL 1 DEFECT SIZE: 2.75 INCHES.

Part: SKIN — CHAFED (I/B FOREFLAP) · airframe 41,627 hrs · 41,627 cycles

INBOARD FOREFLAP, TRAILING EDGE, BOTTOM SIDE, 12 INCHES OUTBOARD OF AFT FLAP CUTOUT CHAFED. CUT OUT DAMAGE, HONEYCOMB REPAIR WITH DOUBLERS PER SRM 51-70-10, DEFECT SIZE: 1 INCH.

Part: ANGLE — CORRODED (BS 300-377) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

ANGLE AT STA 300-377 RBL 61 CORRODED. FABRICATED & INSTALLED NEW ANGLE PER BAC DWG 141N8322; CORR TASK JL-43-53501; LEVEL 1, DEFECT SIZE: 1.5 X 9 INCHES.

Part: CHANNEL — CORRODED (BS 1640-1660) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

INBOARD OF AFT LEFT DOOR SILL BETWEEN STA 1640-1660 OF FLOOR STRUCTURE CORRODED. REMOVED & REPLACED PART PER SRM 51-40-01, DEFECT SIZE: 2 X 2 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,332 hrs · 20,332 cycles

LOCATION: BETWEEN FR 16 AND 17 AND -Y50 REMOVED AND REPLACED FLOORBEAM AND BRACE IAW SRM 51-72-00; CORR TASK JA-220-53500; LEVEL 1 DEFECT SIZE: 5 SQ. IN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

TOP CHORD OF FLOOR FRAME 1640 AT LBL 57 CORRODED; CORR TASK JL-58-53516L LEVEL 1. SPLICED IN NEW UPPER T-CAP CHORD & ANGLE DOUBLERS PER TYP REP 53-15-01; SRM 51-40-02; DEFECT SIZE: 2 X 2 INCHES.

Part: WEB — CORRODED (BS 1660-1681) · corrosion level 1 · airframe 41,627 hrs · 41,627 cycles

LEFT DOOR SILL AFT WEB & SUPPORT CLIP, BETWEEN STA 1660-1681 CORRODED. REMOVED CORROSON PER SRM 53-60-15, TREATED & PRIMED, FAB'D NEW SUPPORT CLIP. CORR TASK JL-58-53516, DEFECT SIZE: 1 X 1 INCH.