N840MH

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 99,838 hrs · 17,176 cycles

R1 DOOR SLIDE ARM LIGHT INOPERATIVE. R & R R1 DOOR SLIDE ARM LIGHT ASSY IAW AMM 52-73. (1353581)

Part: SPAR — CRACKED (ZONE 400) · airframe 99,744 hrs · 17,159 cycles

LEFT STRUT FORWARD UPPER SPAR WEB CRACKED AT LT EQUIPMENT CUTOUT. REPAIRED AS PER PRI630407-14 REV 0. (1336211)

Part: SPAR — CRACKED (ZONE 400) · airframe 99,744 hrs · 17,159 cycles

CRACKS WERE FOUND ON THE NR 1 PYLON FWD UPPER SPAR WEB. ACCOMPLISH ER/A 630407-14AD. (1335822)

Part: SPAR — CRACKED (ZONE 400) · airframe 99,744 hrs · 17,159 cycles

LEFT STRUT, LT FORWARD UPPER SPAR VERTICAL FLANGE CRACKED NSTA 221.25. ABRICATED THE UPPER SPAR AND REMOVED AND REPLACED THE UPPER SPAR CHORD IAW ER/A 630536-14. (1331241)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 99,740 hrs · 17,157 cycles

FOUND SEAT TRACK CORROSION AT STA 1307 TO STA 1329 RBL 88.5 REFER TO CPCP TASK 53-646-00. THE SEAT TRACK REWORKED AREA REPAIRED AS PER PRI 630383-14 (1320320)

Part: INTERFACE UNIT — WORN · airframe 99,740 hrs · 17,157 cycles

NR 8 SLAT INTERFACE T/E 49IN FROM OTBD FOUND WORN. NR 8 SLAT INTERFACE T/E 49IN FROM O/B REPAIRED AS PER SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-4 FIGURE 202 AND SRM 51-70-10-2R-0. REV.76.00, DATE: AUG-29-2025. (LP 1318949)

Part: STRUT — CRACKED (ZONE 400) · airframe 99,740 hrs · 17,157 cycles

NR 2 NAC STRUT STA 204.50 I/B FITTING FOUND CRACK. CORRECTIVE ACTION: THE FITTING REMOVED AND REPLACED AS PER B767-400 SRM51-40-02 (1314415)

Part: SKIN — CRACKED (ZONE 200) · airframe 99,740 hrs · 17,157 cycles

FOUND ONE CRACK BELOW THE NR 7 FASTENER HOLE, COUNTING FROM FRONT TO THE BACK, BETWEEN FRAMES 1654 - 1678, STRINGER 13AL. REPAIED IAW SRM 53-80 -01-2R-7 (1308025).

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 99,550 hrs · 17,129 cycles

L1 SLIDE LIGHT INOP ON FAP. R/R L1 SLIDE LIGHT PER B767-400 AMM 33-51. OPS CHK GOOD. OK FOR SVC. (7377265)

Part: LIGHT — NO TEST (ZONE 200) · airframe 98,633 hrs · 16,991 cycles

EMERGENCY LIGHT FROM SET 50 TO 56 INOP DURING SERVICE CHECK. REMOVED AND REPLACED POWER SUPPLY BATTERY AS PER AMM 33- 51 OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 98,157 hrs · 16,919 cycles

SHIP 1816 RECEIVED FLASH MASTER WARNING AND ALL DOOR EICAS MESSAGES THREE TIMES IN FLIGHT. EMERGENCY LIGHTS CAME ON DURING FLASHES. CORRECTIVE ACTION: CLEARED MSG AND PSEU BITE TEST C/O IAW B764 AMM 32-09-04-704-013. (7069175).

Part: INDICATOR — INOPERATIVE (ZONE 200) · airframe 97,974 hrs · 16,895 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED DOOR2L SLIDE LT NOT ILLU / INTERIOR. CORRECTIVE ACTION: COMPLIED WITH ER/A 626286-14. (0951868).

Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 95,999 hrs · 16,608 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:606. CORRECTIVE ACTION: FOUND BROKEN TAB AND SOLDER JOINT. R/R DOOR 2R ARMED LIGHT ASSY (FAP PANEL) REF B767-400 WDM 52-73-11, AIPC 52-11-46-07D, SWPM 20-84. OPS CK NRML. (0734572)

Part: LIGHT — ODOR (ZONE 200) · airframe 95,914 hrs · 16,598 cycles

SHIP 1816 ODOR EMITTED FROM LED SIDEWALK LIGHT AT ROW 52 FHG BREIFLY. CORRECTIVE ACTION: R/R LIGHT ASSY AT 53FG IAW B767-400 AMM 33-21. R/R GASPER FAN PER B767-400 AMM 21-24. (6614566)

Part: SLIDE — BULGED (1L DOOR SLIDE) · airframe 95,510 hrs · 16,538 cycles

SHIP 1816 FOUND 1L DOOR SLIDE BURGING. CORRECTIVE ACTION: R/R 1L DOOR SLIDE PER B767-400 W/C 5200-4473. (6614888)

Part: DOOR — FOD (L4) · airframe 95,034 hrs · 16,474 cycles

SHIP 1816 4L DOOR WOULD NOT ARM BEFORE DEPATURE. CORRECTIVE ACTION: REMOVED DEBRIS FROM 4L DOOR. ARMS NORMAL. OK FOR SVC. REF B767 AMM 52-22 (6369060)

Part: BULB — INOPERATIVE (R2 DOOR) · airframe 94,963 hrs · 16,465 cycles

SHIP 1816 2R DOOR ARM LIGHT AT 1L PANEL WILL NOT ILLUMINATE. CORRECTIVE ACTION: FOUND ONE OF TWO ELEMENTS BROKEN IN BULB. R/R 2R PUSH SWITCH BULB IN 1LT DOOR PANEL P21. OPS TEST GOOD IN REF TO B767-4 AMM 52-73. MEL/PLACARD REMOVED. (6369054)

Part: SIGN — DAMAGED (ZONE 200) · airframe 94,268 hrs · 16,378 cycles

SHIP 1816 EXIT SIGN 3L DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED EXIT SIGN PER B767 AMM 25-36 CABIN IS OK SERVICE (6198252)

Part: INDICATOR — MISSING (R4 DOOR SLIDE) · airframe 94,058 hrs · 16,351 cycles

SHIP 1816 ENTRY DOOR INOPERATIVE ELECTRICALLY / LOCATIONS:608. CORRECTIVE ACTION: PER CABIN CREW COMMENTS 4R LED SLIDE LIGHT MISSING COMPLETELY. REINSTALLED SLIDE LIGHT LENS. CHECKS GOOD. (0470748)

Part: MODULE — FAULTED (SLIDE INDICATOR) · airframe 93,692 hrs · 16,306 cycles

SLIDE INDICATOR LIGHT ASSEMBLY MISSING & ALARM SIGNAL MODULE DAMAGED. REPLACED ALARM SIGNAL MODULE IAW B767-400 AMM 52-73.

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 93,544 hrs · 16,288 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: REILLUMINATED 601 FA PLANE R1 DOOR SLIDE INDICATOR LIGHT IAW B 767-400 AMM 33-22 OPS CHECK GOOD. (0412636)

Part: O-RING — LEAKING (NR 12 SPOILER) · airframe 93,324 hrs · 16,261 cycles

SHIP 1816 -MISC/DE- CREW ELECTED DE DUE TO LT HYD QTY INDICATION DECREASE DURING FLIGHT. C/W QRH AND LANDED AND TAXIED IN NORMALLY. CORRECTIVE ACTION: REPLACED O-RING ON NUMBER 12 SPOILER EHSV CAP.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 92,711 hrs · 16,186 cycles

SHIP 1816 EMERG LIGHTS ROW 38A AFT CEILING LIGHTS AND AISLE LIGHTS INOP. CORRECTIVE ACTION: BATTERY PACK ROW 53A REPLACED IAW B767-400 AMM 33-51-07 OPS NOW OK. (5808411)

Part: LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 92,711 hrs · 16,186 cycles

SHIP 1816 SLIDE LIGHT AT DOOR 1L IS INOP. CORRECTIVE ACTION: DOOR ARM IND LIGHT R/R IAW B767-400 AMM 52-73 OPS CHECKED GOOD (5844482)

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 92,480 hrs · 16,154 cycles

SHIP 1816 DURING SVC CHECK FOUND EMERGENCY LIHTS INOP AT SEAT 50 AB THROUGH 56AB, CORRECTIVE ACTION: R+R EMERGENCY LIGHT BATTERY 2 EACH AT LOCATIONS 53AB AND 54AB PER B767-400ER AMM 33-51 (5844790)

Part: LIGHT — INOPERATIVE (SLIDE) · airframe 92,445 hrs · 16,150 cycles

SHIP 1816 4L SLIDE LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED 4L SLIDE LIGHT ASSY IAW B767 AMM 52-73. OPC NML A/C OK FOR CONT SVC. NO OTHER DEFECTS NOTED. MEL AND PLACARD REMOVED (5844760)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 92,153 hrs · 16,112 cycles

SHIP 1816 O/H EMERGENCY LIGHT AT 21CD INOP. TRIED NEW LAMP. NO HELP. PLAC INST. CORRECTIVE ACTION: TROUBLESHOT FOUND CONNECTOR D22464 ABOVE RT SIDE CEILING PANEL AT ROW21 WIRING MIS-PINNED. RE-PINNED PER B767 WDM 33-51-12 AND SWPM 20-61-00. EMERGENCY LIGHTS OPS CHECK GOOD PER B767 AMM 33- 51. MEL AND PLACARD REMOVED. NO "M" PROCEDURES. (5728766)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,811 hrs · 16,067 cycles

SHIP 1816 F/C EMERGENCY LIGHTS IN SEAT OUT ON RT SIDEROWS 1-5. CORRECTIVE ACTION: R/R'D EMERGENCY BATTERY PACK M6756 PER B767-400 AMM 33-51 OPS CKS GOOD (5079728)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,748 hrs · 16,055 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED. CORRECTIVE ACTION: C/W RE-SECURED OF SLIDE LIGHT INDICATOR LENS AT R2 DOOR IAW B767 -400 52-73. OPS NML AT THIS TIME. (0149919)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,588 hrs · 16,033 cycles

SHIP 1816 2L DOOR SLIDE ARMED INDICATING LIGHT ON THE 1L F/A PANEL IS INOP. CORRECTIVE ACTION: T/S PER B767-400 SSM 52-73. FOUND PSEU BAD. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS UNIT PER B767-400 AMM 32-09. 02L ARM LIGHT CHECKS GOOD. (0133284)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,955 hrs · 15,947 cycles

SHIP 1816 ON WALK AROUND CHECK FOUND 1 DIVERTER STRIP MISSING AT 0600 POSITION ON RADOME. CORRECTIVE ACTION: 1 DIVIDER STRIP ALLOWED TO BE MISSING IAW B767-400 AMM 53-12-03- 308-023, A/C OK FOR SVC. (5072088)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,498 hrs · 15,886 cycles

SHIP 1816 -ATB- DURING CLIMB CREW REPORTED LEFT ENGINE VIBRATIONS UP TO 4.3 AND BEING FELT IN THE CABIN. AT LEVEL OFF, ENGINE VIBRATIONS REDUCED TO 1.0. CORRECTIVE ACTION: PERFORMED NUMBER 1 FAN BALANCE AND VIBRATION SURVEY. OPS CHECK GOOD. (4614772)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,102 hrs · 15,831 cycles

SHIP 1816 -ATB- RT FWD WINDOW HEAT INOP. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSPECTION. REPLACED J3 CONNECTER AND LEFT WINDOW HEAT CONTROLLER. RESISTANCE VALUE WITHIN LIMIT. (4515134)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,845 hrs · 15,795 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:603. CORRECTIVE ACTION: REPLACED DOOR WARNING LIGHT ASSY AT 2L, STOCK # 09-5200-3-1243, PER B767-400 WDM 52-73 AND PERFORMED SUCCESSFUL TEST PER B767- 400 AMM 52-73 THIS CLEARS MEL 52-11-01, PLACARD REMOVED. (2911933)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,969 hrs · 15,678 cycles

SHIP 1816 DOOR ARM LIGHT AT 1L DOOR INOP. CORRECTIVE ACTION: ARMED DOOR & ARM LIGHT CKS NORMAL. OK FOR SVC. REF B767 AMM 52- 73 (9412602)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,520 hrs · 15,616 cycles

SHIP 1816 FOUND SEAT ROW 50 AB TO 56 AB EMERGENCY LIGHTS INOP ON SVC CK WALK AROUND. CORRECTIVE ACTION: R/R POWER PACK (M738) PER B767-400 AMM 33-51. OPS CK GOOD. OK FOR SVC. (9906556)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,429 hrs · 15,602 cycles

SHIP 1816 AFT CREW REST ESCAPE HATCH DOOR DAMAGED. CORRECTIVE ACTION: REPLACED CREW REST ESCAPE HATCH DOOR REF ERA 14-480725-14MA (9906531)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,301 hrs · 15,582 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: RESET C/B & ALL CKS GOOD REF B767 AMM 52-73 (2728539)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,315 hrs · 15,584 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: RESET C/B & ALL CKS GOOD REF B767 AMM 52-73 (2728536)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,133 hrs · 15,560 cycles

SHIP 1816 DURING CRV LOCATED EMERGENCY EXIT SIGN @ 3R DOOR DAMAGED. CORRECTIVE ACTION: R/R EMERGENCY EXIT SIGN @ 3R DOOR PER B767 AMM 33-51. EMERGENCY EXIT SIGN COMPLETED PER SWPM 20-62-23. NEF REMOVED. OK FOR SVC. (2699167)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,056 hrs · 15,547 cycles

SHIP 1816 R3 EXERIOR EMERGENCY LIGHT INOP, CORRECTIVE ACTION: FOUD NO POWER AT LIGHT. REMOVED AND REPLACED CHARGER AND BATTERY PER B767 AMM 33-51 AT LOCATION M6760. OPS CHECK GOOD. (4164664)

Part: SIGN — DETACHED (EMERGENCY EXIT) · airframe 87,206 hrs · 15,428 cycles

GREEN EMERGENCY EXIT SIGN FELL OFF AT 2L DOOR. INSTALLED THE MISSING EXIT SIGN COVER REF B767 AMM 33-51

Part: NONE — NONE · airframe 85,674 hrs · 15,196 cycles

SHIP 1816 L1 AND R1 EEPLS EXIT SIGNS INOP, CORRECTIVE ACTION: R&R BATTERY PACK AT M1208 PER B767 AMM 33-51. (8971540)

Part: NONE — NONE · airframe 85,546 hrs · 15,172 cycles

SHIP 1816 FOUND CREW REST EMERGENCY LIGHT INDICATOR INOP. CORRECTIVE ACTION: R/R CREW REST EMERGENCY LIGHT INDICATOR. REF B767-400 AMM 33-90- 03-900-801C1. OK SVC. (9187646)

Part: NONE — NONE · airframe 85,177 hrs · 15,114 cycles

SHIP 1816 ON SVC FOUND AFT LT SEAT EMERGENCY LIGHTS AND CEILING LIGHTS OUT, CORRECTIVE ACTION: R/R M738 BATTERY PACK IN REF TO B767-400 AMM 33-51, LIGHT TEST GOOD. (7303680)

Part: HYDRAULIC LINE — LEAKING · airframe 85,032 hrs · 15,094 cycles

SHIP 1816 - DE - INTO ATL DUE TO THE LOSS OF QTY AND PRESSURE FROM THE LEFT HYDRAULIC SYSTEM. CORRECTIVE ACTION: FOUND PRESSURE HYDRAULIC LINE IN THE PYLON LEAKING. REPLACED ALL THE FILTERS WITHIN THE SYSTEM AND THE LEFT EDP. PERFORMED A FLUSH OF THE ENTIRE SYSTEM. (7303606)

Part: NONE — NONE · airframe 84,541 hrs · 15,008 cycles

SHIP 1816 -ATO- DUE TO "UNSCHEDULED STAB TRIM" EICAS MESSAGE DISPLAYED AT THROTTLE UP. CORRECTIVE ACTION: T/S PER B767-400 FIM. TEST 65 C/W NO FAULTS. RT FSPM CHANGED ON FOLLOW UP LOG. (8517190)

Part: NONE — NONE · airframe 84,124 hrs · 14,934 cycles

SHIP 1816 ON SVC CHK FOUND R3 DOOR EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REMOVED OLD SEALANT UNDER BULB, REINSTALLED BULB PER B767 AMM 33 -51. OPS CHECKED GOOD. (8407107)

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 82,451 hrs · 14,589 cycles

SHIP 1816 SLIDE INDICATOR LIGHT INOPERATIVE. CORRECTIVE ACTION: 8-12 JFK CYCLED DOOR SEVERAL TIMES. SYSTEM OPERATION IS NORMAL (LP 1909495)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,211 hrs · 14,532 cycles

SHIP 1816 EMERGENCY LIGHTS INOPERATIVE ROW 50 TO 56AB. REPLACED BATTERY PACK AND PSU M379. SYSTEM OPERATION IS NORMAL. (LP 7835772)

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 80,719 hrs · 14,172 cycles

SHIP 1816 CEILING EMERGENCY LIGHTS ABOVE SEAT 43FG ARE INOPERATIVE. MAINTENANCE SECURED CANNON PLUG ON THE LIGHT ASSEMBLY L3300. SYSTEM OPERATION IS NORMAL. (LP 7486741)

Part: ACOUSTIC LINER — DELAMINATED (NR 2 NACELLE) · airframe 80,233 hrs · 14,028 cycles

ACOUSTIC LINING NR 2 ENGINE DELAMINATING REPAIRED, PER ERA 469315-14MA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 79,925 hrs · 13,957 cycles

AD/EM-EO TASK -OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT ABOUT 10 O'CLOCK POSITION (LOOKING FROM I/B )ON THE LOWER OF THE THREE FASTENER HOLES IN THE RH STA 955 FAIL-SAFE STRAP AS MARK PER W/C 5312-01170-06 STEP 10 .AND TO REPAIR THE FAIL SAFE STRAP IN ACCORDANCE WITH EM 5312-01170 SECTION 10B PRIOR TO FURTHER FLIGHT . AD/EM-EO TASK -OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT ABOUT 10 O'CLOCK POSITION (LOOKING FROM I/B )ON THE LOWER OF THE THREE FASTENER HOLES IN THE RH STA 955 FAIL-SAFE STRAP AS MARK PER W/C 5312-01170-06 STEP 10 .AND TO REPAIR THE FAIL SAFE STRAP IN ACCORDANCE WITH EM 5312-01170 SECTION 10B PRIOR TO FURTHER FLIGHT . THE CRACK ON THE FAIL SAFE STRAP REPAIRED IN ACCCORDANCE WITH EM5312-01170 SECTION 10B. (1518248)

Part: STRAP — CRACKED (FUSELAGE) · airframe 79,925 hrs · 13,957 cycles

AD/EM-EO TASK -OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT ABOUT 5 O'CLOCK POSITION (LOOKING FROM I/B ) ON THE LOWER OF THE THREE FASTENER HOLES IN THE LH STA955 FAIL -SAFE STRAP AS MARK PER W/C 5312-01170-05 STEP 10 .AND TO REPAIR THE FAIL SAFE STRAP IN ACCORDANCE WITH EM 5312-01170 SECTION 10A PRIOR TO FURTHER FLIGHT . THE CRACK ON THE FAIL SAFE STRAP REPAIRED IN ACCORDANCE WITH EM5312-01170 SECTION 10A. (1518337)

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,925 hrs · 13,957 cycles

HFEC INSPECTION FOUND 01 EA CRACK APPROX 0.300 INCH IN LENGTH ON THE FUSELAGE SKIN BELOW THE 9TH STRINGER -ATTACH RIVET ALONG S-13 AR .AFT OF FRAME 1654.5 AS MARK PER W/C 5330- 01229-01B STEP 4. THE 01 EA CRACK ON FUSELAGE SKIN BELOW THE 9TH STRINGER -ATTACH RIVET ALONG S-13AR .AFT OF FRAME 1654.5 REPAIRED AS PER B767-400 SRM 53-80-01-2R REPAIR 7 .RELEASE 59.00 DATE 12/19/19. INSPECTION THRESHOLD :WITHIN 7500 FLIGHT CYCLES FROM THE REPAIR INSTALL.METHOD :EXTERNAL DETAILED INSPECTION AND EXTERNAL -LOW FREQUENCY EDDY CURRENT INSPECTION .INTERVAL :7500 FLIGHT CYCLES LOG-PAGE UPDATED (1511519)

Part: STRUCTURE — DENTED (L3 DOOR) · airframe 79,925 hrs · 13,957 cycles

DURING W/A NOTICED A DENT AT DOOR L3 ENTRY DOOR FWD LOWER CORNER. THE DENT (LOG#0647929) IS CLOSE TO ANOTHER DENT (LOG#0649568) CONSIDERED AS ONE REPAIR .THE 02 DENTS REPAIRED AS PER B767-400 SRM52-10-01-2R-6 RELEASE :59.00 DATE:12/19/19 .DETAIL SEE NRC 100-122 PLS CLOSE THE LOG#0647929 LOG-PAGE UPDATED @ 25FEB20 (0647929)

Part: SKIN — DENTED (SERVICE DOOR) · airframe 79,925 hrs · 13,957 cycles

- ACS REPORTS SMALL DENT IN AFT LEFT SERVICE DOOR SKIN THE DENT IN THE AFT ENTRY DOOR SKIN REF TO LOG #0649568 AND ANOTHER DENT REF TO LOG #0647929 CONSIDERED AS ONE REPAIR .THE 02 EA DENTS REPAIRED AS PER B767-400 SRM 52-10-01-2R-6.RELEASE 59.00 DATE:19DEC19.CATEGORY B REPAIR INSPECTION REQUIREMENT : BEGIN EXTERNAL LFEC INSPECTION OF THE SKIN AT 6000 DOOR FLIGHT CYCLES AFT REPAIR INSTALL .INTERVAL:6000 DOOR FLIGHT CYCLES . BEGIN EXTERNAL LFEC INSPECTION OF THE BEAM CHORD AT 12000 DOOR FLIGHT CYCLES AFT REPAIR INSTALL .INTERVAL :12000 DOOR FLIGHT CYCLES . LOG-PAGE UPDATED @ 25FEB20 (0649568)

Part: SKIN — CRACKED (LT NACELLE) · airframe 79,925 hrs · 13,957 cycles

MTC TASK-RH PYLON LEFT UPPER SKIN BTW NAC STA221 AND 237 FOUND FASTENER HOLE CRACK. RH PYLON LEFT UPPER SKIN BETWEEN NAC STA221 AND 237 FASTENER HOLE CRACKED AREA REPAIRED AS PER PRI585196-14AD REV.0. PRI585196-14AD REV.0 COMPARED AND COMPLIED WITH ER/A585196-14AD SECTION I REV.ORIGINAL. THE SECTION II OF ER/A585196-14AD REV.ORIGINAL REFER TO LOG PAGE#1504978 FOR INSPECTION DETAIL. ASSOCIATED ER/A 14-585196 ADDED FOR AC 1816 (1505614)

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 82,816 hrs · 14,664 cycles

DURING INSPECTION FOUND 2 CRACKS ON THE #2 PYLON FORWARD UPPER SPAR WEB. C/W ERA 585196-14. (LP 1504978)

Part: TEE FITTING — DAMAGED · airframe 79,925 hrs · 13,957 cycles

AD/MTC TASK -DURING PERFORM WORK CARD 5312-01170-10B-02 FOUND 2 EXISTING FASTENER HOLES SHORT EDGE MARGIN ON "T"FITTING (P/N: 145T1929U10) REPAIRED AS PER PRI585419-14 REV O.THE PRI 585419-14 REV O COMPAIRED AND COMPLIED WITH ER/A 585419-14 REV ORIGINAL . ASSOCIATED ER/A 14-585419 ADDED FOR AC 1816 (1503920)

Part: STRUCTURE — CRACKED (NR 1 NACELLE) · airframe 79,925 hrs · 13,957 cycles

MTC TASK-NO.1 STRUT MID SPAR CUTOUT AREA AT NAC STA221.25 FOUND CRACK. NO.1 STRUT MID SPAR WEB CUTOUT AT NAC STA221.25 CRACKED AREA REPAIRED AS PER PRI585200-14 REV.0. PRI585200-14 REV.0 COMPARED AND COMPLIED WITH ER/A585200-14 REV.ORIGINAL. ASSOCIATED ER/A 14-585200 ADDED FOR AC 1816 (1502572)

Part: PRESSURE DECK — CORRODED (BS 961) · corrosion level 2 · airframe 79,925 hrs · 13,957 cycles

-MLG WHEEL WELL PRESSURE DECK UPPER SURFACE AT STA961 BETWEEN RBL 88 AREA FOUND CORROSION .REF TO CPCP TASK :53-508-00 LOG-PAGE UPDATED THE CORROSION ON MLG WHEEL WELL PRESSURE DECK UPPER SURFACE AT STA961 BETWEEN RBL88 REMOVED AND REPAIRED AS PER PRI585126-14 REV O.THE PRI585126-14 REV O COMPAIRED AND COMPLIED WITH ER/A 585126 -14 REV ORIGINAL .ER/A SECTION II DAT DTE IS DUE AT OR BEFORE 30000 TOTAL FLIGHT CYCLES ON THE AIRCRAFT REFER THE LOG #1500666 ASSOCIATED ER/A 14-585126 ADDED FOR AC 1816 LOG-PAGE UPDATED (1501374)

Part: FRAME — CRACKED (BULKHEAD) · corrosion level 2 · airframe 79,925 hrs · 13,957 cycles

R/H MLG WHEEL WELL REAR SPAR BULKHEAD AT STA955 RBL78.5 WL178.02 FOUND CORROSION .REFET TO CPCP TASK 53-524-00 THE CORROSION AT R/H MLG WHEEL WELL REAR SPAR BULKHEAD AT STA955 RBL78.5 WL 178.02 REMOVED AND REPAIRED AS PER PRI 585024-14 REV O .THE ER/A 585024-14 REV ORIGINAL COMPAIRED AND COMPLETED WITH THE PRI585024-14 REV O. ASSOCIATED ER/A 14-585024 ADDED FOR AC 1816 (1498673)

Part: FAILSAFE — CRACKED (BS 955) · airframe 79,925 hrs · 13,957 cycles

-OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT ABOUT 5 O'CLOCK POSITION (LOOKING FROM I/B )ON THE LOWER OF THE THREE FASTENER HOLES IN THE LH STA955 FAIL SAFE STRAP AS MARK LOG-PAGE UPDATED THE CRACK AT ABOUT 5 O'CLOCK POSITION (LOOKING FROM I/B )ON THE LOWER OF THE THREE FASTENER HOLE IN THE LH STA955 FAIL SAFE STRAP REPAIRED AS PER W/C 5312-01170-10A-02. (1498599)

Part: FAILSAFE — CRACKED (BS 955) · airframe 79,925 hrs · 13,957 cycles

AD/EM-EO TASK -OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT ABOUT 10 O'CLOCK POSITION (LOOKING FROM I/B ) ON THE LOWER OF THE THREE FASTENER HOLES IN THE RH STA955 FAIL SAFE STRAP AS MARK . LOG-PAGE UPDATED THE CRACK AT ABOUT 10 O'CLOCK POSITION (LOOKING FROM I/B ) ON THE LOWER OF THE THREE FASTENER HOLES IN RH STA955 FAIL SAFE STRAP REPAIRED AS PER W/C 5312-01170-10B-02 AND NRC 130-016 (1498929)

Part: FAILSAFE — CRACKED (BS 955) · airframe 79,925 hrs · 13,957 cycles

AD/ MTC TASK -THERE EXISTED INDICATIONS OF POSSIBLE CRACK IN THE RH STA955 FAIL -SAFE STRAP DURING UT INSP. LOG-PAGE UPDATED THE CRACK IN THE R/H STA955 FAIL -SAFE STRAP REPAIRED AS PER W/C 5312-01170-10B-02 AND NRC 130-016 (1498965)

Part: FAILSAFE — CRACKED (BS 955) · airframe 79,925 hrs · 13,957 cycles

THERE EXISTED INDICATIONS OF POSSIBLE CRACK IN THE LH STA955 FAIL -SAFE STRAP DURING UT INSP. THE CRACK IN THE LH STA955 FAIL-SAFE STRAP REPAIRED AS PER W/ C5312-01170-10A-02. (1498617)

Part: STIFFENER — CRACKED (NLG WW) · airframe 79,925 hrs · 13,957 cycles

-MFEC INSPECTION FOUND 01 CRACK APPROX 0.210 INCH ON NOSE WHEEL WELL RH VERTICAL STIFFENER FROM WL 159.00 TO WL 185.00 AS MARK PER W/C 5312-01186-01B STEP 7 THE CRACK ON NOSE WHEEL WELL RH VERTICAL STIFFENER FROM WL 159.00 TO WL 185.00 REPAIRED AS PER CARD 5312-01186-02B. LOG-PAGE UPDATED (1496156)

Part: SEAT TRACK — CORRODED (BS 753-1098) · corrosion level 2 · airframe 79,925 hrs · 13,957 cycles

SEAT TRACK -SEAT TRACK AT STA753.45 TO STA1098.45 BETWEEN RBL 88.5 FOUND CORROSION .REF TO CPCP TASK 53-646-00 LOG-PAGE UPDATED THE CORROSION REMOVED AND REPAIRED AS PER B767-400 PRI585201 REV 0 .THE PRI585201-14 REV0 COMPAIRED AND COMPLETED WITH THE ER/A 585201-14 REV ORIGINAL . ASSOCIATED ER/A 14-585201 ADDED FOR AC 1816 LOG-PAGE UPDATED (1494487)

Part: SEAT TRACK — CORRODED (BS 1480) · corrosion level 2 · airframe 79,925 hrs · 13,957 cycles

MTC TASK -CABIN SEAT TRACK AT STA1480 BETWEEN LBL 54.75 FOUND CORROSION .REF TO CPCP TASK 53-646-00 N ENTR 00174272 W THE CORROSION AT CABIN SEAT TRACK AT STA 1480 BETWEEN LBL54.75 REMOVED AS PER B767-400 SRM 51-10-02 .RELEASE :59.00 .19DEC2019 .THE DAMAGE AREA MEASURED THE LENGTH IS:3" .WIDTH IS 1" .DEPTH ON THE FLANGE IS 0.043".FOUND OUT OF ALLOWABLE DAMAGE LIMIT AS PER B767-400 SRM53-00-52 FIG101 .RELEASE :59.00.19 DEC 2019 . REPLACED THE SEAT TRACK AT STA1360 TO STA1480 .LBL54.75. AS PER B767-400 SRM51-40-02 RELEASE 59.00 19DEC 2019 .THE NEW SEAT TRACK FABRICATED AS PER BOEING DRAWING 146T5213 AND PO G20SL00466. LOG-PAGE UPDATED (1489027)

Part: DOOR SILL — CORRODED (R1 DOORWAY) · corrosion level 2 · airframe 79,925 hrs · 13,957 cycles

MTC TASK-PASSENGER CABIN SERVICE DOOR R1 LOWER SILL TEE SUPPORT FOUND CORROSION .REFER TO CPCP TASK 53-674-00 LOG-PAGE UPDATED PASSENGER CABIN SERVICE DOOR R1 LOWER SILL CORROSION TEE SUPPORT REMOVED AND REPLACED AS PER B767-400 SRM51-40-02RELEASE (1489040)

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 79,176 hrs · 13,868 cycles

DURING CLIMBOUT ABOUT 1500' LEFT AFT CM STARTED TO SMOKE FROM CORNER OF HOT PLATE. COFFEEMAKER WAS SHUT DOWN AND CB 607 AND 608 PULLED & COLLARD, SMOKE DISAPPEARED WITHIN 5 MIN.REMOVED BOTH CM AND CLEANED CM TRAY. NO EVIDENCE OF FIRE MARKS. REPLACED BOTH COFFEE MAKERS AND CLEARD CLOGGED DRAIN LIN COFFEE MAKER A608. SYSTEM OPERAITON IS NORMAL

Part: OUTLET — SPARKS (LAVATORY) · airframe 78,560 hrs · 13,790 cycles

LAV 4L FLT ATTEND OBSERVED SPARK FROM ELEC OUTLET.LAV SECURED. COULD NOT DUPLICATE.R/R PLUG AS PRECAUTION PER B767-400 AMM 25- 29.OPS CK GOOD.OK FOR SERVICE. (LP6555724)

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 76,219 hrs · 13,470 cycles

EMERGENCY LIGHTS SEATS 24-27 LEFT SIDE ARE INOPERATIVE. RESEATED CONNECTOR SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,886 hrs · 13,427 cycles

EMERGENCY LIGHTS ROW 38-45AB ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY AND CHARGER. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,922 hrs · 13,432 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 75,819 hrs · 13,417 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT SEAT 19-21FG. MAINTENANCE RECONNECTED C/P AT L3348. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,819 hrs · 13,417 cycles

EMERGENCY LIGHTS AT 38-45AB ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 73,159 hrs · 13,026 cycles

EMERGENCY LIGHTS AT SEATS 23-25 ABC WERE INOPERATIVE. FOUND THE CONNECTOR DISCONNECTED AT 23ABC. CONNECTED. THE SYSTEM OPS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 72,985 hrs · 13,004 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE AT 25G. MAINTENANCE FOUND LOOSE CONNECTOR AND RE-CONNECTED. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CREW REST) · airframe 71,802 hrs · 12,845 cycles

CREW REST EMERGENCY LIGHT STRIP ON LADDER IS INOPERATIVE. REPLACED STRIP. MCO/PLAC REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WIND SHEAR) · airframe 71,152 hrs · 12,744 cycles

RECIEVED PREDICTIVE WINDSHEAR WARNINGS, FOLLOWED BY A REJECTED TAKEOFF TWO TIMES IN GUSTY WIND CONDITIONS. TAXIED CLEAR OF THE RUNWAY, THE WARNING CLEARED, AND THE CREW REVIEWED POST REJECT CONSIDERATIONS. THE AIRCRAFT HAD NO HOT BRAKE OR FUSE PLUG ISSUES AFTER THE RTO. ALL STANDARD DEBRIEF ITEMS COMPLETE, THE CREW ATTEMPTED ANOTHER TAKEOFF, WHICH ENDED WITH AN RTO AT 101 KNOTS FOR WINDSHEAR WARNING. TROUBLESHOT IAW FIM, FAULT CODE INDEX 34-90-68-00. NO FAULT NOTED. IAW ODI REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-43. BITE TESTED GOOD. ACFT OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (BOOST PUMP) · airframe 70,484 hrs · 12,644 cycles

UNABLE TO TURN OFF LEFT FWD FUEL PUMP DURING CROSSFEED OPERATION. NO PUMP DURING SWITCH OR EICAS ILLUMINATED. CROSSFEED WAS NORMAL. CHECKED OPERATION OF LT FWD BOOST PUMP , EICAS AND PUMP INDICATION OPS NORMAL, OK FOR SERVICC IAW AMM 28-22.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 67,378 hrs · 12,238 cycles

DURING PDC, FOUND THE R1 SLIDE LOOSE ON AFT SIDE. SLIDE PACK DISCONNECTED FROM AFT SIDE HOLDER, UNABLE TO RECONNECT. REPLACED THE R1 DOOR SLIDE IAW W/C 5200-4473. OPS CHECKED GOOD. REACTIVATED EMERGENCY EVACUATION SYSTEM AND SEAT 1-5 A THRU D.

Part: ENGINE — LEAKING (LEFT) · airframe 66,532 hrs · 12,124 cycles

DIVERTED DUE TO APPROXIMATELY ONE HOUR INTO FLIGHT, THE LEFT ENGINE OIL QUANTITY DROPPED TO ZERO. OIL PRESSURE ALSO DROPPED. CREW CONSULTED QRH, AND CONTACTED DISPATCH AND MC AND DECISION WAS MADE TO DIVERT TO AMS. EMERGENCY WAS DECLARED WHEN REQUEST TO DUMP FUEL WAS MADE. ARFF REPORTED A BRAKE FIRE AND FOLLOWED THE AIRCRAFT TO THE GATE. RIGHT INBOARD REAR FUSE PLUG MELTED. ENGINE WAS PULLED BACK TO IDLE. A/C LANDED WITH LEFT ENGINE ON WITH 9 PSI OIL PRESSURE. MTC FOUND OIL STREAKING FROM RECOUP DUCTS IN TAILPIPE. CORRECTIVE ACTION: ENGINE CHANGE. (9638068)

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 66,399 hrs · 12,104 cycles

R1 DOOR SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED R1 DOOR SLIDE IAW WORK CARD 5200-4473. (9638011)

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 66,134 hrs · 12,064 cycles

NR 2 ENGINE RT CORE COWL SKIN HAS A 10 INCH CRACK AT THE TE. REPLACED THE COWL ASSY IAW AMM 71-11-06.

Part: SKIN — GOUGED (FUSELAGE) · airframe 62,855 hrs · 11,652 cycles

FUSELAGE SKIN IS GOUGED FWD EDGE OF C-1 DOOR BETWEEN DOOR CUT-OUT AND ALT STATIC PORT. REPAIRED AREA IAW SRM 53-00-01.

Part: SKIN — DENTED (BS 566) · airframe 62,855 hrs · 11,652 cycles

DURING WALK AROUND DENT FOUND BS 566 BETWEEN STRINGERS 17 - 18L. C/W PERMANENT REPAIR IAW PRI 541869-14, REV B.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,047 hrs · 10,310 cycles

EMERGENCY LIGHT BATTERIES FAILED 15 MINUTE CAPACITY CHECK. REPLACED BATTERIES IAW AMM 33-51. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,019 hrs · 10,180 cycles

SEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE, FOUND BATTERY PACK LOOSE. R & R POWER SUPPLY & BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (R3 DOOR SLIDE) · airframe 49,812 hrs · 10,023 cycles

R3 DOOR SLIDE GROUND LIGHT ILLUMINATED INOPERATIVE. REPLACED FUSE ON POWER PACK M6760 IAW AMM 33-51, REPLACED LAMPS, AND SECURED CONNECTORS, CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,185 hrs · 9,946 cycles

DURING A CHECK FOUND ROW'S 15-22 AND 2L EXIT LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-52, OPS CHECK NORMAL, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,439 hrs · 9,731 cycles

LOWER CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. OP CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 47,121 hrs · 9,691 cycles

LOWER LOBE CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK, OPS OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 44,502 hrs · 9,366 cycles

EMERGENCY LIGHTS ROW 21GF-18GF ARE INOPERATIVE. MAINTNENACE FOUND THE CONNECTOR LOOSE AT 21FG AND REINSTALLED. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — DISCHARGED (CREW REST) · airframe 43,265 hrs · 9,213 cycles

DURING DRC FOUND LOWER DECK CREW REST EMERGENCY LIGHTS INOPERATIVE. CREW REST BATTERY PACK WAS BAD AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: PANEL — CORRODED (FUSELAGE) · airframe 41,815 hrs · 9,035 cycles

FOUND DURING PSV, CORRODED WEB CLOSURE PANEL AT BS 955 AND LBL 90. REPAIRED PER ERA 498107-14. (ERA 498107-14)

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 41,580 hrs · 9,008 cycles

EMERGENCY LIGHTS AT SEATS 32-38 ARE INOPERATIVE. MAINTENANCE RE-SEATED THE PLUG AT 31AB. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 40,792 hrs · 8,915 cycles

DURING DRC, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM SEAT ROWS 38AB TO 42AB. MAINTENANCE FOUND PLUG AT 37B DISCONNECTED AND RE-CONNECTED IT. OPERATIONAL CHECK WAS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 40,087 hrs · 8,830 cycles

MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEATS 19FG - 22FG. MAINTENANCE FOUND CONNECTOR OUT AT SEAT 18FG AND RE-SECURED IT. OPERATIONAL CHECK WAS OK.

Part: ACM — SEIZED (LEFT) · airframe 37,012 hrs · 8,443 cycles

SULFER TYPE ODOR THOUGHOUT CABIN AND FLIGHT DECK/ SMOKE/ HAZE OBSERVED BY F/A. ON LANDING HAD EICAS MESSAGE LT ACM. FOUND LT ACM SEIZED.

Part: ACM — SEIZED (LEFT) · airframe 37,012 hrs · 8,443 cycles

SULFUR TYPE SMELL THROUGHOUT CABIN AND FLIGHT DECK, SMOKE, HAZE OBSERVED BY F/A ON LANDING AN EICAS MESSAGE ABOUT THE LT ACM SHOWED UP. MX FOUND THE LT ACM SEIZED.

Part: MODULE — MALFUNCTIONED (AIR DATA) · airframe 35,357 hrs · 8,238 cycles

AFTER T/O, ON CLIMB OUT, TAS DISAGREES AND ALT DISAGREES. EICAS MESSAGES WITH F/O SIDE FLUCTUATING ON AIRSPEED AND ALTITUDE CA-R/R RT STATIC AIR DATA MODULE M11264 IAW MM 34-26-03-401. RT AIR DATA SYS CKS OK. MPN C17001BA01 INSTALLED. (DL764101437)

Part: OVEN — FAILED (GALLEY) · airframe 32,929 hrs · 7,936 cycles

AFT GALLEY OVEN C/B POPPED CB AND SMOKE. REMOVED FOOD DEBRIS FROM OVEN RESET C/B OPERATED OVEN 30 MINS OPS NORMAL ETOPS CATEGORY 'F'.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 32,765 hrs · 7,913 cycles

STATUS MSG - APU CONTROL. REPLACED APU PER AMM, CHECKS GOOD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: WIRE — SHORTED (CABIN) · airframe 32,435 hrs · 7,875 cycles

A/C 1816 DIVERTED TO ATL BECAUSE OF PASSENGER O2 MASK DEPLOYED. FLIGHT CREW NOTICED A LOUD SCRATCHING NOISE IN THE P/A AND NUMEROUS C/B'S POPPED. T/S FOUND WIRE BUNDLE ARC BURNED OVER LAV L1. ALSO FOUND LA SYS H1 C/B POPPED ON P37 LAV FLUSH SYS N10 P34 AND LAV SHO D4 ON P36 ALSO POPPED. 704304 RE PACKED O2 MASKS ON L/S O A/C 6887480, DISCONNECTED C/P D 3881 D3879 AND D5160 ABOVE LAV. REMOVED HARNESS W0220 FOR REPLACEMENT. 878465 FABRICATED NEW HARNESS W0820 PER WSPM AND WDM. 684597 INSTALLED NEW HARNESS WO820 FROM D5160 TOD3881 AND D3879.

Part: ADIRU — MALFUNCTIONED (LEFT) · airframe 30,353 hrs · 7,619 cycles

INTERMITTENT - ALT DISAGREE - CAUTION MESSAGE DURING FLIGHT. CAPT AND F/O ALTIMETERS AS MUCH AS 250 FT DIFFERENCE AT FL310. SEEMED TO IMPROVE SLIGHTLY DURING FLIGHT. MCDP SHOWED LAST FLT LEG, L-V NAV FAIL AD SYS L IRMP. SHOWED LT SYS FAULT CODE 34-21050. SWAPPED LT AND CTR IDIRUS. PERFORMED OPS CK OK PER FIM 34-26-00-101.

Part: FAN — SMOKE (LEFT) · airframe 29,853 hrs · 7,556 cycles

L RECIRC FAN MSG WITH SMOKE IN THE CABIN, FWD TO MCO AND PLACARD PER MEL 21-25-01A.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 27,335 hrs · 7,263 cycles

WXR RADAR FAILED. REPLACED ANTENNA, PERFORMED TEST OK .

Part: MONITOR — MALFUNCTIONED (HYD QTY) · airframe 24,500 hrs · 6,932 cycles

RTO DUE AT 60 KTS LT HYD QTY INDICATION DROPPED TO ZERO. MTC FOUND LT QTY IND AT TANK FULL. FWD LT QTY IND TO MCO AND PLACARD. INSPECTED AND SHOOK DOWN WIRING AND CP AT TRANSMITTER. NTF. CO NOT DUPLICATE REPLACED HYD QTY MONITOR M122 AS PRECAUTION DUE TO PREV. REINSTALLED PTU SIGNAL WIRE PER MEL. OPS CK GOOD, REMOVED MCO AND PLACARD.

Part: COMPUTER — MALFUNCTIONED (LT FMC) · airframe 22,929 hrs · 6,727 cycles

LOST CAPT FMC CDU UNABLE TO RECOVER DIVERTING TO SNN FOR REPAIRS. REMOVED AND REPLACED CENTER CDU CKS GOOD MCO AND PLACARD REMOVED.

Part: ENGINE — FAILED (NR 1) · airframe 22,283 hrs · 6,641 cycles

REPLACED NR 1 ENG PER ROUTINE DECK.

Part: DETECTOR — MALFUNCTIONED (AIRFLOW) · airframe 21,943 hrs · 6,597 cycles

AT 240 INTO FLT FWD EQ OVHT EICAS ILLUMINATED WENT TO STDBY PER QRH. AFTER 5 MIN THE OVHT LT RE-ILLUM. WENT TO OVRD PER QRH. FWD EQ COOLING LT ILLUM ON OVRD ON SHORT FINAL INSP CONICAL SCREEN AT EQ COOLING SUPPLY FAN. NO DEFECTS NOTED. REMOVED TS104 FLOW DETECTOR. STRONG AIRFLOW IN AUTO AND STDBY. REPLACED TS104 FLOW DETECTOR. ALSO, REPLACED EQ COOLING IND CARD M867. CKS OK.

Part: COMPUTER — MALFUNCTIONED (TCAS) · airframe 20,076 hrs · 6,365 cycles

TCAS FAILED IN FLT. INSTALLED PROCESSOR FROM A/C 1821, CKS GOOD.

Part: COMBUSTION LINER — DAMAGED (NR 1 ENGINE) · airframe 20,049 hrs · 6,361 cycles

ENGINE FAILED BORO OPN 5003 COMBUSTION LINER DAMAGED. REPLACED NR 1 ENGINE.

Part: WARNING MESSAGE — ILLUMINATED (PARKING BRAKE) · airframe 19,353 hrs · 6,200 cycles

ANTI-SKID OFF EICAS MSG. RESET PARKING BRAKE VALVE C/B. CHECKS OK

Part: ENGINE — SHUTDOWN (APU) · airframe 18,672 hrs · 6,019 cycles

APU AUTO SHUTDOWN - FAULTED 49-94007 LOW OIL PRESSURE. REPLACED APU.

Part: METERING VALVE — FAILED (NLG STEERING) · airframe 17,175 hrs · 5,734 cycles

AFTER PUSHBACK AND ENG START, HEARD A WARNING HORN AT L1 DOOR AREA. FOUND SOUND FROM NOSE WHEEL STEERING METERING VALVE MODULE W HYD SYS PRESSURIZED. REPLACED STEERING METERING VALVE MODULE PE AMM 32-51-04. OPS CKD NORMAL.

Part: ACTUATOR — LEAKING (APU) · airframe 16,028 hrs · 5,480 cycles

FUEL LEAK FROM APU DRAIN MAST. FORWARD TO FLIGHT CREW PLACARD PER MEL 49-11-01B. AIRCRAFT FLOWN TO HNL TO MTC REPAIR APU. REPLACE IGV ACTUATOR PER M/M.

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 10,296 hrs · 3,864 cycles

COFFEMAKER IN AREA 206, FIRST CLASS GALLEY, SPARKING FROM COLD WATER BUTTON. REPLACED SAME.

Part: LAMP — INOPERATIVE (EMERGENC LIGHT) · airframe 9,704 hrs · 3,720 cycles

AT 23GF MID GALLEY AND AFT GALLEY HAS ONE EACH EMERGENCY CEILING LIGHT INOP. RELAMPED, OPS CHECK OK.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 8,285 hrs · 3,261 cycles

AFTER TAKEOFF GOT EICAS MSGS TAILSKID AND TCAS DURING CLIMB. TAILSKID MSG WENT OUT AND GOT GEAR DISAGREE EICAS MSG ACCOMPANIED BY GEAR SYNOPTIC NOSE UP AND MAIN GEAR INTRANSIT. RETURNED TO LAX. CHECKED OUT WIRING AND GEAR HANDLE SWITCHES THROUGH TO PSEU PROBLEMS FOUND. REPLACED R33 DIODE, PRECAUTIONARY REPLACED PSEU-JAC A/C SWUNG GEAR CHECKED OK, NO FAULT MSGS. REPLACED SYSTEM 1 S 244 NOSE GEAR NOT COMPRESSED SWITCH. RETRACT AND EXTEND LANDING GEAR, OPS CHECKED NORMAL.