N692AA

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 87,804 hrs · 24,559 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AFT WOULD NOT TEST ON PREFLIGHT. MAINTENANCE REPLACED AFT FLASHLIGHT BATTERY PER AMM 25-60-00.

Part: WEB — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT DOOR LOWER FORWARD WEB SIDE FRAME CRACKED AND CORRODED. REPAIRED WEB PER EA 297540.

Part: LATCH — UNKNOWN (L2 WINDOW) · airframe 87,185 hrs · 24,362 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS AFTER LANDING L-2 WINDOW VERY DIFFICULT TO UNLOCK. MAINTENANCE ACCOMPLISHED LATCH SYSTEM TEST IAW AMM 56-11-02, OPERATION NORMAL.

Part: FLOOR SUPPORT — CORRODED (BS 1440-1500) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRINGER BETWEEN BS 1440 AND BS 1500 AND RBL 7.55. REPLACED FLOOR STRINGER PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERCOSTAL FROM FR 1400 TO FR 1420, LBL10. REPLACED INTERCOSTAL PER 51-00-05-1.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON U CHANNEL FROM FR 1640 TO FR 1660. REPLACED U CHANNEL PER SRM 51-00-01.

Part: ANGLE — CRACKED (BS 1330) · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL UPPER CHORD ANGLE, BS 1330. REPLACED CHORD ANGLE PER SRM 53-00-51.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LAVATORY MOUNT FROM FR 330 TO FR 335, LBL20. REPLACED LAVATORY MOUNT PER SRM 51-00-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN INNER SURFACE BETWEEN BS 1680 AND BS 1701, BETWEEN S29L AND S26R. REPAIRED SKIN PER EA 297530 AND SRM 53-00-01.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FRAME AT BS 1460 BETWEEN RBL 23 AND RBL 26. REPLACED FRAME PER 51-00-05-1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT INTERCOSTAL WEB BETWEEN BS 1412 AND BS 1420 AT RBL 9. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND FORWARD GALLEY MOUNT AT FR 1687, RBL-51. REPLACED MOUNT PER 51-00-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z ANGLE AT FR 1715, RBL-50. REPLACED Z ANGLE PER SRM 51-00-05.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GALLEY MOUNT AT FR 1713, RBL-51. REPLACED GALLEY MOUNT PER 51-00-05.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT DECK AT FR 1718, LBL23. REPLACED AFT DECK PER 51-00-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON G5 CENTER GALLEY FITTING AT FR 1687. REPLACED FITTING PER 51-00-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,184 hrs · 24,361 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON G5 LEFT HAND AFT GALLEY FITTING AT FR 1713, LBL51. REPLACED FITTING PER 51-00-05.

Part: PUMP — WEAK (HP FUEL) · airframe 85,636 hrs · 23,928 cycles

RIGHT ENGINE FLUCTUATED, N1+/- 2% +/-2%; F/F +/- #200 LBS; EGT+/- 50C. REPLACED THE HIGH PRESSURE FUEL PUMP IAW 73-11-03-404-016. LEAK CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 85,613 hrs · 23,920 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED FORWARD ENTRY DOOR WAS EXTREMELY DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED MAIN CABIN ENTRY DOOR 1L MECHANISM PER FIM 52-11-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 84,863 hrs · 23,681 cycles

AIRCRAFT WAS NOT GROUNDED. COACH CLASS SEAT MOUNTED EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERIES FOR COACH CLASS PER MM 33-51-07.

Part: BATTERY — DISCHARGED (CABIN) · airframe 84,863 hrs · 23,681 cycles

AIRCRAFT WAS NOT GROUNDED. FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERIES FOR FIRST CLASS PER MM 33-51-07.

Part: ACTUATOR — FAULTY (RT OVRWG EXIT) · airframe 84,800 hrs · 23,666 cycles

WHILE ACCOMPLISHING SIC 2905, RIGHT OVERWING SLIDE DEPLOYMENT, THE RIGHT OVERWING SLIDE DID NOT DEPLOY WITHIN THE 10 SECONDS AS REQUIRED IAW MM 25-65-00-705-035. REPLACED THE ACTUATOR IAW ITEM #2. ACCOMPLISHED OPERATIONAL TEST OF SLIDE IAW AMM 25-65-00. THE AIRCRAFT WAS GROUNDED.

Part: ACTUATOR — MALFUNCTIONED (EVAC SLIDE) · airframe 84,797 hrs · 23,665 cycles

JFK - AIRCRAFT WAS GROUNDED. WHILE ACCOMPLISHING MCM 2905 RIGHT OVERWING SLIDE DID NOT DEPLOY WITHIN 10 SECOND AS REQUIRED BY AMM 25-65-00-705-035 STEP D7. MAINTENANCE REPLACED THE R OFF WING ESCAPE SLIDE ACTUATOR PER AMM 25-65-05.

Part: PIN — UNSECURE (EICAS COMPUTER) · airframe 84,437 hrs · 23,579 cycles

AIRCRAFT WAS GROUNDED. FLIGHT CREW ABORTED TAKEOFF BETWEEN 120 TO 130 KNOTS FOR AN EICAS ENGINE SHUTDOWN MESSAGE. AIRCRAFT WAS DISABLED DUE TO A BRAKE MALFUNCTION. REJECTED TAKEOFF AFTER EICAS LEFT ENGINE SHUTDOWN MESSAGE DISABLED. DURING EICAS BITE TEST OF LEFT HAND EICAS COMPUTER IT WOULD NOT GO TO FAULT HISTORY USING AUTO SELECTION ON P61 PANEL. SUSPECT BAD EICAS COMPUTERS. REPLACEMENT OF BOTH LEFT HAND AND RIGHT HAND EICAS COMPUTERS PER AMM 31-41-02, OPERATIONS CHECKS GOOD. FOUND TWO LOCK PINS WERE PUSHED BACK ON RIGHT HAND EICAS RACK. REINSERTED AND LOCKED PINS (D321D-H1 AND D321A-A1) PER WDM 73-31-11 AND WDM 31-41-21. HIGH POWER RUNS WERE ACCOMPLISHED ALONG WITH FUNCTIONAL CHECKS OF ALL BRAKES. THIS SDR IS FOR THE RIGHT HAND EICAS PINS. (SEE CONTROL AALA201809069036 AND AALA201809069037)

Part: COMPUTER — DEFECTIVE (ZONE 100) · airframe 84,437 hrs · 23,579 cycles

AIRCRAFT WAS GROUNDED. FLIGHT CREW ABORTED TAKEOFF BETWEEN 120 TO 130 KNOTS FOR AN EICAS ENGINE SHUTDOWN MESSAGE. AIRCRAFT WAS DISABLED DUE TO A BRAKE MALFUNCTION. REJECTED TAKEOFF AFTER EICAS LEFT ENGINE SHUTDOWN MESSAGE DISABLED. DURING EICAS BITE TEST OF LEFT HAND EICAS COMPUTER IT WOULD NOT GO TO FAULT HISTORY USING AUTO SELECTION ON P61 PANEL. SUSPECT BAD EICAS COMPUTERS. REPLACEMENT OF BOTH LEFT HAND AND RIGHT HAND EICAS COMPUTERS PER AMM 31-41-02, OPERATIONS CHECKS GOOD. FOUND TWO LOCK PINS WERE PUSHED BACK ON RIGHT HAND EICAS RACK. REINSERTED AND LOCKED PINS (D321D-H1 AND D321A-A1) PER WDM 73-31-11 AND WDM 31-41-21. HIGH POWER RUNS WERE ACCOMPLISHED ALONG WITH FUNCTIONAL CHECKS OF ALL BRAKES. THIS SDR IS FOR THE LEFT HAND EICAS COMPUTER. (SEE CONTROL AALA201809069037 AND AALA201809069038)

Part: COMPUTER — DEFECTIVE (ZONE 100) · airframe 84,437 hrs · 23,579 cycles

AIRCRAFT WAS GROUNDED. FLIGHT CREW ABORTED TAKEOFF BETWEEN 120 TO 130 KNOTS FOR AN EICAS ENGINE SHUTDOWN MESSAGE. AIRCRAFT WAS DISABLED DUE TO A BRAKE MALFUNCTION. REJECTED TAKEOFF AFTER EICAS LEFT ENGINE SHUTDOWN MESSAGE DISABLED. DURING EICAS BITE TEST OF LEFT HAND EICAS COMPUTER IT WOULD NOT GO TO FAULT HISTORY USING AUTO SELECTION ON P61 PANEL. SUSPECT BAD EICAS COMPUTERS. REPLACEMENT OF BOTH LEFT HAND AND RIGHT HAND EICAS COMPUTERS PER AMM 31-41-02, OPERATIONS CHECKS GOOD. FOUND TWO LOCK PINS WERE PUSHED BACK ON RIGHT HAND EICAS RACK. REINSERTED AND LOCKED PINS (D321D-H1 AND D321A-A1) PER WDM 73-31-11 AND WDM 31-41-21. HIGH POWER RUNS WERE ACCOMPLISHED ALONG WITH FUNCTIONAL CHECKS OF ALL BRAKES. THIS SDR IS FOR THE RIGHT HAND EICAS COMPUTER. (SEE CONTROL AALA201809069036 AND AALA201809069038)

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 83,659 hrs · 23,393 cycles

THREE AREAS OF CONDENSATION ON THE RT OUTBOARD TRAILING EDGE FLAP. ALL THREE LOCATIONS ARE 6.5 INCHES FWD OF THE TRAILING EDGE OF THE FLAP. THE DIMENSIONS FROM INBOARD TO OUTBOARD ARE AS FOLLOWS: 3.0 INCHES BY 4 INCHES AT WBL 539.5, 2.0 INCHES BY 2.0 INCHES AT WBL 553.5, 1.0 INCH BY 1.0 INCH AT WBL 578. A TAP TEST OF THE AFFECTED AREAS CONFIRMED THERE IS NO DISBONDING PRESENT AND REPAIRED IAW EA 281530. THE AIRCRAFT WAS GROUNDED.

Part: FLOW VALVE — FAULTY (FUEL) · airframe 83,362 hrs · 23,325 cycles

CABIN ALTITUDE WARNING AT FL380. EMERGENCY WAS DELCARED AND DIVERTED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE FLOW CONTROL VALVE IAW AMM 21-51-00. AIRCRAFT WAS GROUNDED.

Part: SENSOR — INOPERATIVE (GIRT BAR) · airframe 82,378 hrs · 23,040 cycles

AIRCRAFT NOT GROUNDED. L2 DOOR SLIDE GIRT BAR ENGAGED DOES NOT SHOW ARMED, AIRCRAFT GROUNDED. NOTIFIED FLT CREW. REPLACED BOTH GIRT BAR SENSORS TO 2L DOOR SLIDE ESCAPE GIRT BAR, NOW READS ARMED, LIGHT OKAY.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 81,080 hrs · 22,682 cycles

EMERGENCY EXIT LIGHT AT THE R1 DOOR EXTERIOR SLIDE IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND BATTERY IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 81,080 hrs · 22,682 cycles

EMERGENCY EXIT LIGHT AT THE R1 DOOR EXTERIOR SLIDE IS INOPERATIVE. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.

Part: BATTERY — CORRODED (MEGAPHONE) · airframe 81,002 hrs · 22,658 cycles

THE AIRCRAFT WAS NOT GROUNDED. F/C MEGAPHONE BATTERIES SHOW SIGNS OF CORROSION. REPLACED F/C MEGAPHONE BATTERIES REF MM 25-64-00.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 80,711 hrs · 22,584 cycles

EMERGENCY EXIT SIGN AT L2 DOOR IS DETACHED. INSTALLED EXIT SIGN IAW AMM 33-50-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,595 hrs · 22,562 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FIRST CLASS EMERGENCY PATH LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY AND CONTROL MODULE (AALA201705059053) IAW AMM 33-51-07. ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-00. SYSTEM CHECKS NORMAL

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 80,595 hrs · 22,562 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FIRST CLASS EMERGENCY PATH LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY (AALA20170505002) AND CONTROL MODULE IAW AMM 33-51-07. ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-00. SYSTEM CHECKS NORMAL.

Part: SKIN — CORRODED (LT NACELLE) · corrosion level 2 · airframe 80,595 hrs · 22,562 cycles

LEFT PYLON CORRODED ON THE RIGHT SIDE OF THE PRESSURE REGULATING AND SHUTOFF VALVE ACCESS PANEL LANDING. REPAIRED IAW SRM 51-10-02-0G AND EA 268826.

Part: SKIN — CORRODED (LT NACELLE) · corrosion level 3 · airframe 80,595 hrs · 22,562 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT ENGINE PYLON INBOARD SKIN CORRODED AFT OF THE LOWER CHORD FLANGE. REPAIRED IAW EA 268963.

Part: CHAIN — MISSING (L2 DOOR SLIDE) · airframe 80,526 hrs · 22,535 cycles

AIRCRAFT WAS NOT GROUNDED. L2 DOOR SLIDE HARNESS LATCH RELEASE STRAP IS MISSING CHAIN LINKS AND SPACER. REPLACED CHAIN LINKS AND SPACER IAW AMM 25-66-01. OPS CHECKED GOOD.

Part: SPACER — MISSING (L2 DOOR SLIDE) · airframe 80,526 hrs · 22,535 cycles

L2 DOOR SLIDE HARNESS LATCH RELEASE STRAP IS MISSING CHAIN LINKS AND SPACER. REPLACED CHAIN LINKS AND SPACER IAW AMM 25-66-01. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 80,441 hrs · 22,508 cycles

EMERGENCY EXIT LIGHT ON BULLNOSE BY SEAT 1B HAS A MISSING LENS. REPLACED THE LENS IAW AMM 33-51-05. OPERATIONAL CHECKED GOOD.

Part: COVER — LOOSE (R4 DOOR SLIDE) · airframe 80,438 hrs · 22,507 cycles

R4 DOOR SLIDE COVER IS LOOSE AND OBSTRUCTING DOOR OPENING. SECURED THE SLIDE COVER IAW AMM 52-11-02. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,423 hrs · 22,500 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS IN THE AFT CABIN FAILED TEST. REMOVED AND REPLACED BATTERY PACK M10953 IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: MODULE — FAILED (CABIN) · airframe 80,423 hrs · 22,500 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS IN FIRST CLASS, L1/R1 DOOR EMERGENCY EXIT LIGHTS AND OVERHEAD BIN LIGHTS FAILED TEST. REMOVED AND REPLACED CONTROL MODULE M10798 AND BATTERY PACK M10798 (AALA20170222002) IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,423 hrs · 22,500 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS IN FIRST CLASS, L1/R1 DOOR EMERGENCY EXIT LIGHTS AND OVERHEAD BIN LIGHTS FAILED TEST. REMOVED AND REPLACED CONTROL MODULE M10798 (AALA20170222001) AND BATTERY PACK M10798 IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,423 hrs · 22,500 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS IN MID CABIN, L2/R2 DOOR EMERGENCY EXIT LIGHTS AND OVERHEAD BIN LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY M733 (AALA20170223018) AND BATTERY PACK M10952 IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 80,423 hrs · 22,500 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS IN MID CABIN, L2/R2 DOOR EMERGENCY EXIT LIGHTS AND OVERHEAD BIN LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY M733 AND BATTERY PACK M10952 (AALA20170223019) IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: LOCK — DIRTY (GIRT BAR) · airframe 79,999 hrs · 22,379 cycles

L4 DOOR EMERGENCY ESCAPE SLIDE DIFFICULT TO ARM & DISARM. CLEANED THE GIRT BAR LOCK ASSEMBLY IAW AMM 52-11-00-862-077. OPS CHECKED GOOD.

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 79,703 hrs · 22,264 cycles

EMERGENCY EXIT LIGHTS IN THE AFT RIGHT CABIN IS INOPERATIVE DURING TEST. MAINTENANCE FOUND CHAFED WIRES IN THE AFT RIGHT LAVATORY. REMOVED AND REPLACED WIRES IAW WDM 33-51-22. OPERATIONAL CHECK NORMAL IAW MCM CARD 2866.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,703 hrs · 22,264 cycles

RIGHT AFT EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. SYSYTEM CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 79,703 hrs · 22,264 cycles

CABIN FLOORBEAM AT BS 324 IS CORRODED BETWEEN RBL 33 AND 58. REPAIRED THE FLOORBEAM IAW SRM 53-10-08-2R-1 REPAIR 1 DETAIL II.

Part: CONTROL MODULE — FAULTY (EMERGENCY LIGHTS) · airframe 79,703 hrs · 22,264 cycles

RIGHT AFT EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL MODULE IAW AMM 33-51-07. SYSYTEM CHECKED NORMAL.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 79,703 hrs · 22,264 cycles

CORROSION ON THE RIGHT WING LEADING EDGE SPAR WEB FORWARD FACE AT FSS 627. REPAIRED WEB IAW EA 263556 AND SRM 51-10-02.

Part: PLATE — CORRODED (ZONE 300) · corrosion level 2 · airframe 79,703 hrs · 22,264 cycles

RIGHT LOWER STABILIZER TORQUE BOX INNER PLATE CORRODED AT APPROXIMATELY BS 1830. REMOVED AND REPLACED INNER PLATE IAW 51-00-05-1 AND DRAWING 182N1601.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,815 hrs · 21,902 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS AT SEATS BETWEEN ROWS 26 & 36, AT R4 & L4 DOORS ARE INOPERATIVE. R & R CONTROL MODULE & BATTERY AT AFT GALLEY AREA & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-07. SEE ALSO AALA 20160426004.

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 78,815 hrs · 21,902 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS AT SEATS BETWEEN ROWS 26 & 36 & AT R4 & L4 DOORS ARE INOPERATIVE. R & R CONTROL MODULE & BATTERY AT AFT GALLEY AREA & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-07. SEE ALSO AALA 20160429012.

Part: OVERHEAT SENSOR — FAULTY (RT NACELLE) · airframe 76,756 hrs · 21,235 cycles

AIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RT ENG OVHT OCCURRED WITH RT ENG OVHT AMBER ANNUNCIATION LIGHT ON PEDESTAL. R & R RT NACELLE LP1 & LP2 OVHT SENSOR IAW AMM 26-11-01. PERFORMED LEAK & ENG OPERATIONAL CHECK IAW 71-00-00. SYS CHECKED NORMAL. SEE ALSO AALA20150708014.

Part: DUCT — DEFECTIVE (RT ENGINE) · airframe 76,756 hrs · 21,235 cycles

AIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RT ENG OVERHEAT OCCURRED WITH RT ENG OVHT AMBER ANNUNCIATION LIGHT ON PEDESTAL. R & R RT ENG HIGH PRESSURE OUTLET DUCT. SEE ALSO AALA20150709008.

Part: FMC — FAULTY (RIGHT) · airframe 76,018 hrs · 21,058 cycles

ALL THREE AUTOPILOTS FAILED ALONG WITH RT FMC. ACCOMPLISHED BITE OF FMC BITE IAW FIM 34-61-00, AUTO FLIGHT IAW FIM 22-02 TASK 815-818, BPCU IAW FIM 24-20 TASK 815-801 & EEC IAW FIM 73-21-00-902. EMERGENCY DECLARED, RETURNED TO DEPARTURE, AND LANDING WAS UNEVENTFUL. R & R RT FMC IAW AMM 34-61-01 & 34-61-01-424-005-002. PERFORMED FMC SOFTWARE CROSS LOAD IAW AMM 34-61-00-342-009-004. ALL OPERATIONAL CHECKED GOOD.

Part: CONTROL PANEL — FAULTY (AUTOPILOT SYS) · airframe 76,024 hrs · 21,060 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. ALL THREE AUTOPILOTS FAILED ALONG WITH RT FMC. ACCOMPLISHED FMC BITE IAW FIM 34-61-00, AUTO FLIGHT BITE IAW FIM 22-02 TASK 815-818, BPCU BITE IAW FIM 24-20 TASK 815-801 & EEC BITE IAW FIM 73-21-00-902. R & R AUTO FLIGHT MODE CONTROL PANEL IAW AMM 22-11-02. PERFORMED FMC SOFTWARE CROSS LOAD IAW AMM 34-61-00-342-009-004. ALL OPERATIONAL CHECKS GOOD.

Part: PRESSURE DECK — CORRODED (RT MLG WW) · corrosion level 2 · airframe 75,791 hrs · 21,001 cycles

RIGHT MAIN WW PRESS DECK CORRODED AT APPROX FS 1170 & RBL 60 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA 53-039083 DATED 03 20 2015.

Part: PRESSURE DECK — CORRODED (LT MLG WW) · corrosion level 2 · airframe 75,791 hrs · 21,001 cycles

LEFT MAIN WW PRESS DECK HAS CORROSION AT APPROX FS 1170 & LBL 68 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA 53-038994 DATED 03 20 2015.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,791 hrs · 21,001 cycles

RIGHT MAIN WW PRESS DECK CORRODED AT APPROX FS 1165 & RBL 49 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA B757-53-039083 DATED 03 20 2015.

Part: PRESSURE DECK — CORRODED (RT MLG WW) · corrosion level 2 · airframe 75,791 hrs · 21,001 cycles

RIGHT MAIN WW PRESS DECK CORRODED AT APPROX FS 1151 & RBL 51 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA 53-039083 DATED 03 20 2015.

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 71,722 hrs · 20,036 cycles

MIA CREW REPORTED BOTH CTR TANK FUEL PUMP INOPERATIVE IN FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT & RT HAND CTR TANK FUEL PUMP PRESS SWITCH. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — CRACKED (R1 DOOR) · airframe 71,194 hrs · 19,885 cycles

RT NR 1 DOOR FWD INNER SKIN CRACKED AT LIGHTNING HOLE 9 INCHES FROM FWD EDGE. REPAIRED INNER SKIN IAW EA COMP-52-032485 & REO-G16859 REV A.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,194 hrs · 19,885 cycles

ATTACH CLIP AT STATION 970, BELOW LT HAND FWD OVERWING EXIT IS CORRODED. REMOVED AND INSTALLED CLIP IAW EA B757-53-032498 & REO-G16858 REV A.

Part: HINGE FITTING — CRACKED (THRUST REVERSER) · airframe 71,194 hrs · 19,885 cycles

NR 1 ENG THRUST REVERSER HINGE FITTING, INBD UPPER AFT ATTACH HOLE IS CRACKED. ACCOMPLISHED REPAIR IAW AA EA B757-54-032610 & REO-G16877 REV A.

Part: TAIL CONE — CRACKED (FUSELAGE) · airframe 71,194 hrs · 19,885 cycles

AFT FUSELAGE TAIL CONE CRACKED AT STATION 1960 BL 0. REPAIRED TAIL CONE IAW EA B757-53-032633.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,194 hrs · 19,885 cycles

LT SIDE OF AFT FUSELAGE 4 INCHES FWD OF STATION 1720 PROTRUDING DENT BETWEEN STRINGER 25 & 26 LT. REPAIRED FUSELAGE SKIN IAW EA B757-53-032377.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,194 hrs · 19,885 cycles

FS 1460 FRAME CLIP CORRODED BETWEEN STRINGERS 28 & 29 LEFT. REMOVED CORRODED SHEAR TIE & INSTALLED NEW SHEAR TIE IAW SRM 51-40-05-0G, SRM 51-40-02-0G & SRM 51-10-02 PARA 9.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,194 hrs · 19,885 cycles

BULK CARGO COMPARTMENT, BODY STATION 1600, STRINGER 25RT. FRAME UPPER CAP DENTED. REPAIRED FRAME AT STATION 1600 IAW SRM 53-00-07-2R-5 FIGURE 201, DETAIL II.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,194 hrs · 19,885 cycles

INSIDE MAIN CABIN FLOOR ATTACH ANGLE IS CORRODED AT STATION 897 & LBL 64. INSTALLED REPAIR ANGLE IAW AARD 53-30-13-1.

Part: INDICATOR — INOPERATIVE (CABIN PRESSURE) · airframe 67,653 hrs · 19,000 cycles

HNL - CREW REPORTED PRESSURIZATION FAULT. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE CABIN PRESSURE INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — INOPERATIVE (RT ENGINE) · airframe 67,586 hrs · 18,982 cycles

HNL - INFLIGHT OGG-LAX CREW REPORTED RIGHT ENGINE N3 INDICATION FLUCUATION AND SPEED CARD MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE N3 GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — DAMAGED (NLG) · airframe 66,441 hrs · 18,710 cycles

LAX - CREW REPORTED EICAS MESSAGE "NOSE AIR/GROUND DISAGREE". EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT NOSE GEAR NOT COMPRESSED SENSOR S10067 DAMAGED. REPLACED SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 65,646 hrs · 18,466 cycles

CREASE BEAM WEB STATIONS 1620 TO 1640 RIGHT HAS DAMAGED FASTENER HOLES. INSTALLED NEW WEB AND WEB SUPPORT BRACKET PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

RIGHT CREASE ANGLE STATIONS 1570 TO 1630 CORRODED. REPLACED RIGHT CREASE ANGLE PER AARD 53-60-13-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

CORROSION ON CABIN FLOORBEAM STATION 365 RIGHT BUTTLINES 2 TO 16. REMOVED CORROSION BY SECTION REMOVAL AND INSTALLED FILLER AND DOUBLERS PER SRM 53-00-51-2R AND EA B757-53-022776.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 1640 AND 1661 AT BUTTLINE 0. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

NUMEROUS AREAS OF CORROSION ALONG ENTIRE LENGTH OF STATION 1681 FLOORBEAM TEE CAP. REPLACED UPPER TEE PER EA B757-53-022818.

Part: SUPPORT — DAMAGED (ZONE 200) · airframe 65,646 hrs · 18,466 cycles

WATER TANK SUPPORT HAS DAMAGED HOLES BETWEEN BS 1640 AND 1660. REMOVED AND REPLACED SUPPORT PER SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

NUMEROUS AREAS OF CORROSION ALONG ENTIRE LENGTH OF BS 1640 FLOORBEAM. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-05 AND EA B757-53-022812.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

FLOOR SUPPORT AT LEFT NUMBER 4 DOOR IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

FLOOR SUPPORT AT LEFT NUMBER 4 DOOR IS CORRODED. REMOVED AND REPLACED LEFT NUMBER 4 FLOOR SUPPORT PER SRM 51-10-02.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

CORROSION ON CHORD ANGLE IN LEFT SIDE OF NOSE LANDING GEAR WHEEL WELL. REPLACED CHORD ANGLE PER AARD 51-10-05.

Part: TEE FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

TEE FITTING AT STATION 1720 AT BUTTLINE 59 RIGHT HAS CORROSION. REPLACED TEE FITTING PER SRM 51-10-02.

Part: RING — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

CORROSION ON BREAK RING AT STATION 1720 RIGHT AT STRINGER 17 RIGHT. REWORKED CORROSION PER EA B757-53-022696.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

LEFT CREASE ANGLE CORRODED FROM STATIONS 1620 TO 1610 LEFT BUTTLINE 60. REMOVED AND REPLACED LEFT CREASE ANGLE FROM STATIONS 1620 TO 1610 LEFT BUTTLINE 60 PER AARD 53-60-13-1.

Part: SKIN — DAMAGED (ZONE 200) · airframe 65,646 hrs · 18,466 cycles

LIGHTNING STRIKE ON UPPER FUSELAGE STATION 581 STRINGER 7 LEFT. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER PER EA B757-53-022701.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 65,646 hrs · 18,466 cycles

AFT CARGO FORWARD DOOR FRAME AT BS 1380 WAS CORRODED. INSTALLED DOUBLER PER 53-00-07 2R2.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,646 hrs · 18,466 cycles

CORROSION ON FORWARD SIDE OF AFT CARGO DOOR FRAME WEB. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-07-2R 2.

Part: INTERCOSTAL — DAMAGED (CARGO DOOR) · airframe 65,646 hrs · 18,466 cycles

AFT CARGO DOOR, 3RD INTERCOSTAL FROM AFT AT BOTTOM OF DOOR HAS OVERSIZED HOLE IN CHORD AND DOUBLE DRILLED HOLE IN WEB FLANGE. INSTALLED NEW CORD ANGLE AND WEB PER ESO 90121.

Part: ANGLE — DAMAGED (CARGO DOOR) · airframe 65,646 hrs · 18,466 cycles

AFT CARGO DOOR, 2ND INTERCOSTAL FROM AFT AT BOTTOM OF DOOR HAS OVERSIZED HOLE IN CHORD ANGLE. INSTALLED NEW CHORD ANGLE PER ESO 90121.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,646 hrs · 18,466 cycles

NUMBER 2 SLAT JUST FORWARD OF INBOARD DRIVE TRACK, SKIN HAS TWO CRACKS AT FASTENERS. INSTALLED REPAIR DOUBLER ON NUMBER 4 COVE SKIN ON NUMBER 2 LEFT SLAT PER AARD 57-43-00-4.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 65,011 hrs · 18,280 cycles

LAX - CREW REPORTED TRAILING EDGE FLAP DISAGREE LIGHT AT FLAP SELECTION 20. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. FOUND FLAP POSITION INDICATOR INOPERTAIVE AND NUMBER 1 FLAP TRANSMITTER INDICATOR OUT. REPLACED FLAP POSITION INDICATOR AND RESET FLAP TRANSMITTER INDICATION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,902 hrs · 18,252 cycles

CENTER AISLE EMERGENCY LIGHTS ON RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR CENTER AISLE EMERGENCY LIGHTS ON RIGHT SIDE. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,331 hrs · 17,886 cycles

BATTERY PACK FOR MID CABIN EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK FOR MID CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 62,873 hrs · 17,779 cycles

HNL - CREW REPORTED DURING CLIMBOUT THE LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. INDICATIONS ON OVERHEAD AND EICAS. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED LEFT ENGINE DRIVEN PUMP, CASE, PRESSURE AND RETURN FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 62,561 hrs · 17,696 cycles

LAX - CREW REPORTED WHILE AT CRUISE A PRESSURIZATION WARNING AND UNCOMMANDED DEPRESSURIZATION. EMERGENCY DESCENT TO 10000 FT AND O2 MASKS WERE DEPLOYED MANUALLY. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 CABIN PRESSURE CONTROLLER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,459 hrs · 17,177 cycles

RIGHT NUMBER 10 OUTBOARD SLAT CORROSION ON UPPER SKIN AT INBOARD DRIVE TRACK AREA. RIGHT NUMBER 10 OUTBOARD SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: LIGHT — BROKEN (CABIN) · airframe 60,144 hrs · 17,097 cycles

SEAT 11D SEAT-MOUNTED EMERGENCY LIGHT IS BROKEN, MISSING LENS AND LAMPS. REMOVED AND REPLACED SEAT 11D SEAT-MOUNTED EMERGENCY LIGHT ASSEMBLY. OPS CHECKED NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 60,144 hrs · 17,097 cycles

SEAT 16D AFT SEAT-MOUNTED RED EMERGENCY LIGHT IS BROKEN, MISSING LENS AND LAMPS. REMOVED AND REPLACED SEAT 16D AFT SEAT-MOUNTED RED EMERGENCY LIGHT ASSEMBLY. OPS CHECKED NORMAL.

Part: LAMP — MISSING (CABIN) · airframe 59,535 hrs · 16,965 cycles

THE 16 DEF EMERGENCY LIGHT MISSING ONE LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT 16 DEF. OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 59,535 hrs · 16,965 cycles

THE 16DEF EMERGENCY LIGHT MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT 16DEF. OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 57,589 hrs · 16,465 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D HAS LENS MISSING. REPLACED MISSING CLEAR LENS AT SEAT 16D.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 57,311 hrs · 16,400 cycles

FLIGHT CREW REPORTED, COULD NOT CONTROL THE CABIN PRESSURIZATION. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED THE OUTFLOW VALVE ACTUATOR. SYSTEM CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16D.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 28D.

Part: LIGHT — BROKEN (CABIN)

DFW EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 11D.

Part: CLAMP — LOOSE (NR 1 ENGINE) · 53,476 cycles

TUL INFLIGHT T9677/14SEP. CREW REPORTED LT STRUT OVERHEAT STATUS IN FLIGHT. CREW TURNED OFF NR 1 ENGINE BLEED. LANDED TUL WITHOUT INCIDENT. FOUND CLAMP LEAKING AT HIGH PRESSURE DUCT FORWARD OF PRECOOLER. TIGHTENED CLAMP AT HIGH PRESSURE DUCT FORWARD OF PRECOOLER. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN) · airframe 50,625 hrs

DFW - EMERGENCY LIGHT AT SEAT 25D BROKEN OFF OF SEAT. REPLACED LIGHT ASSEMBLY AND NUT PLATE FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 50,551 hrs

MCO INFLIGHT T1034/15DEC - RIGHT MAIN LANDING GEAR DOOR AMBER LIGHT ILLUMINATED DURING APPROACH. CAPTAIN FLEW BY TOWER FOR COMFIRMATION. LANDED MCO WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING HEAR DOOR INBOARD EXTENSION/RETRACTION RETURN HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,210 hrs

SFO - EMERGENCY LIGHTS FROM SEAT ROW 26 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT FROM SEAT ROW 26 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (SPOILERS)

HNL INFLIGHT T297 - SPOILER LIGHT ILLUMINATED ON EICAS AND OVERHEAD WARNING PANEL. LANDED HNL WITHOUT INCIDENT. REPLACED POWER CONTROL ACTUATOR NUMBER 6. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GEARBOX — CONTAMINATED (LEFT ENGINE)

DEN INFLIGHT T844/07AUG SNA TO ORD - LEFT ENGINE VIBRATION FOLLOWED BY LOW ENGINE GAS TEMPERATURE AND LOW OIL PRESSURE INDICATIONS. SHUT DOWN LEFT ENGINE AND LANDED DEN WITHOUT INCIDENT. SINGLE ENGINE TIME 19 MINUTES. FOUND GEARBOX CHIP DETECTORS CONTAMINATED WITH METAL. REPLACED NUMBER ONE ENGINE ON 07 AUGUST AT DEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: EEC — FAILED (LEFT ENGINE)

ORD INFLIGHT T9653/10JUL - ON TAKE OFF LEFT BLEED, LEFT ELECTRONIC ENGINE CONTROL, AND LEFT ELECTRICAL LOAD CONTROL FAILED. LEFT ENGINE FAILED ON APPROACH. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 12 JUL AT ORD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - FOUND EMERGENCY LIGHT AT RIGHT NUMBER ONE SLIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: EEC — INOPERATIVE (LT ENGINE)

MIA - LEFT ENGINE ELECTRONIC ENGINE CONTROL AND LEFT ENGINE LIMITER FAULTED DURING FLIGHT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED POWER CONDITIONING AND CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TACH GENERATOR — INOPERATIVE (RT ENGINE)

RIGHT HAND FUEL FLOW INDICATED 0 TEMPORARILY. WHEN N3 INDICATED 0 EICAS INDICATIONS CENTER RIGHT FUEL PUMP AND RIGHT ENGINE BLEED OFF CENTER PUMP PRESSURE LIGHT AND RIGHT ENGINE BLEED OFF. RIGHT DUCT PRESSURE INDICATED 5 PSI. STANDBY ENGINE INSTRUMENTS INDICATED N3 AT 0 AS WELL. LANDED SJU WITHOUT INCIDENT. REPLACED RIGHT ENGINE N3 TACHOMETER GENERATOR AND SPEED CARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT FIRST CLASS SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT)

SJU - DURING OVERNIGHT CHECK FOUND EMERGENCY FLOOR LIGHTING SYSTEM AT ROWS 15 TO 25 INOPERATIVE. FOUND BROKEN CONNECTOR AT ROW 16. REPAIRED BROKEN CONNECTOR AT ROW 16 FOR EMERGENCY FLOOR LIGHTING AT ROWS 15 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - AISLE EMERGENCY EXIT LIGHTS AT 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY ON SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - AFT LEFT HAND OVERWING EMERGENCY EXIT LIGHT AND FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR AFT LEFT HAND OVERWING EMERGENCY EXIT LIGHT AND FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - EMERGENCY LIGHTS AT SEAT ROWS 16D THROUGH 25D AND EMERGENCY EXIT LIGHT OVER RIGHT AND LEFT HAND WING INOPERATIVE. REPLACED BATTERY PACK M10953 FOR EMERGENCY LIGHTS AT SEAT ROWS 16D THROUGH 25D AND EMERGENCY EXIT LIGHTS OVER RIGHT AND LEFT HAND WING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 25DEF)

JFK - EMERGENCY ESCAPE PATH LIGHTING AT ROW 25DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY ESCAPE PATH LIGHTING AT ROW 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY)

LAX - ON CLIMB-OUT FROM LAX FLIGHT ATTENDANTS REPORTED A BURNING SMELL IN THE FORWARD GALLEY SMOKE WAS THEN REPORTED RETURNED TO LAX. FOUND BAKED ON DEBRIS IN FORWARD OVEN. DEBRIS REMOVED AND OVEN CLEANED BY CABIN SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 16 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 AND L2 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (LT EMER EXIT)

SFO - DURING OVERNIGHT MAINTENANCE, AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)

Part: SIGN — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, RIGHT AFT OVERWING DOOR EMERGENCY EXIT SIGN FOUND INOPERATIVE. REPLACED AFT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT EXIT LIGHT AT RIGHT MID DOOR INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT EXIT CONNECTOR AT RIGHT MID CABIN DOOR CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)