N840MH
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2009-09-07 – 2009-09-07 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2009-09-07 – 2009-09-07 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
35F EMER LIGHT PATH COVER MISSING LIGHT REMAIN OPERATIVE. R/R LIGHT HOUSING ASSY ABD CLOSEOUT PER B767 CMM 25-21-58. (8716747) (AIRCRAFT GROUNDED)
SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. R & R LIGHT ASSEMBLY REF B767-400 AMM 52-73, OPS CK GOOD (1476657)
SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED 601 SLIDE LIGHT DOES NOT ILLUMINATE 1L DOOR. CORRECTIVE ACTION: RESECURRED 1L DOOR SLIDE LIGHT INDICATOR ASSY. OPS CHK GOOD. (8585992)
R1 DOOR SLIDE ARM LIGHT INOPERATIVE. R & R R1 DOOR SLIDE ARM LIGHT ASSY IAW AMM 52-73. (1353581)
LEFT STRUT FORWARD UPPER SPAR WEB CRACKED AT LT EQUIPMENT CUTOUT. REPAIRED AS PER PRI630407-14 REV 0. (1336211)
CRACKS WERE FOUND ON THE NR 1 PYLON FWD UPPER SPAR WEB. ACCOMPLISH ER/A 630407-14AD. (1335822)
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)
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)
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)
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)
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).
L1 SLIDE LIGHT INOP ON FAP. R/R L1 SLIDE LIGHT PER B767-400 AMM 33-51. OPS CHK GOOD. OK FOR SVC. (7377265)
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.
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).
SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED DOOR2L SLIDE LT NOT ILLU / INTERIOR. CORRECTIVE ACTION: COMPLIED WITH ER/A 626286-14. (0951868).
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)
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)
SHIP 1816 FOUND 1L DOOR SLIDE BURGING. CORRECTIVE ACTION: R/R 1L DOOR SLIDE PER B767-400 W/C 5200-4473. (6614888)
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)
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)
SHIP 1816 EXIT SIGN 3L DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED EXIT SIGN PER B767 AMM 25-36 CABIN IS OK SERVICE (6198252)
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)
SLIDE INDICATOR LIGHT ASSEMBLY MISSING & ALARM SIGNAL MODULE DAMAGED. REPLACED ALARM SIGNAL MODULE IAW B767-400 AMM 52-73.
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)
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.
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
SHIP 1816 AFT CREW REST ESCAPE HATCH DOOR DAMAGED. CORRECTIVE ACTION: REPLACED CREW REST ESCAPE HATCH DOOR REF ERA 14-480725-14MA (9906531)
SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: RESET C/B & ALL CKS GOOD REF B767 AMM 52-73 (2728536)
SHIP 1816 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: RESET C/B & ALL CKS GOOD REF B767 AMM 52-73 (2728539)
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)
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)
GREEN EMERGENCY EXIT SIGN FELL OFF AT 2L DOOR. INSTALLED THE MISSING EXIT SIGN COVER REF B767 AMM 33-51
SHIP 1816 L1 AND R1 EEPLS EXIT SIGNS INOP, CORRECTIVE ACTION: R&R BATTERY PACK AT M1208 PER B767 AMM 33-51. (8971540)
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)
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)
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)
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)
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)
SHIP 1816 SLIDE INDICATOR LIGHT INOPERATIVE. CORRECTIVE ACTION: 8-12 JFK CYCLED DOOR SEVERAL TIMES. SYSTEM OPERATION IS NORMAL (LP 1909495)
SHIP 1816 EMERGENCY LIGHTS INOPERATIVE ROW 50 TO 56AB. REPLACED BATTERY PACK AND PSU M379. SYSTEM OPERATION IS NORMAL. (LP 7835772)
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)
ACOUSTIC LINING NR 2 ENGINE DELAMINATING REPAIRED, PER ERA 469315-14MA.
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)
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)
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)
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)
- 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)
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)
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)
DURING INSPECTION FOUND 2 CRACKS ON THE #2 PYLON FORWARD UPPER SPAR WEB. C/W ERA 585196-14. (LP 1504978)
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)
-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)
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)
-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)
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)
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)
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)
-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)
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)
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)
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)
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
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)
EMERGENCY LIGHTS SEATS 24-27 LEFT SIDE ARE INOPERATIVE. RESEATED CONNECTOR SYSTEM OPERATION IS NORMAL.
EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
EMERGENCY LIGHTS ROW 38-45AB ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY AND CHARGER. SYSTEM OPERATION IS NORMAL.
EMERGENCY LIGHTS AT 38-45AB ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
EMERGENCY LIGHTS ARE INOPERATIVE AT SEAT 19-21FG. MAINTENANCE RECONNECTED C/P AT L3348. SYSTEM OPERATION IS NORMAL.
EMERGENCY LIGHTS AT SEATS 23-25 ABC WERE INOPERATIVE. FOUND THE CONNECTOR DISCONNECTED AT 23ABC. CONNECTED. THE SYSTEM OPS NORMAL.
EMERGENCY FLOOR LIGHTING INOPERATIVE AT 25G. MAINTENANCE FOUND LOOSE CONNECTOR AND RE-CONNECTED. SYSTEM OPERATION IS NORMAL.
CREW REST EMERGENCY LIGHT STRIP ON LADDER IS INOPERATIVE. REPLACED STRIP. MCO/PLAC REMOVED.
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.
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.
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.
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)
R1 DOOR SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED R1 DOOR SLIDE IAW WORK CARD 5200-4473. (9638011)
NR 2 ENGINE RT CORE COWL SKIN HAS A 10 INCH CRACK AT THE TE. REPLACED THE COWL ASSY IAW AMM 71-11-06.
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.
DURING WALK AROUND DENT FOUND BS 566 BETWEEN STRINGERS 17 - 18L. C/W PERMANENT REPAIR IAW PRI 541869-14, REV B.
EMERGENCY LIGHT BATTERIES FAILED 15 MINUTE CAPACITY CHECK. REPLACED BATTERIES IAW AMM 33-51. OPS CHECKED NORMAL.
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.
R3 DOOR SLIDE GROUND LIGHT ILLUMINATED INOPERATIVE. REPLACED FUSE ON POWER PACK M6760 IAW AMM 33-51, REPLACED LAMPS, AND SECURED CONNECTORS, CHECKED OK.
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.
LOWER CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. OP CHECKED NORMAL.
LOWER LOBE CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK, OPS OK.
EMERGENCY LIGHTS ROW 21GF-18GF ARE INOPERATIVE. MAINTNENACE FOUND THE CONNECTOR LOOSE AT 21FG AND REINSTALLED. SYSTEM OPERATION IS NORMAL.
DURING DRC FOUND LOWER DECK CREW REST EMERGENCY LIGHTS INOPERATIVE. CREW REST BATTERY PACK WAS BAD AND REPLACED. SYSTEM OPERATION IS NORMAL.
FOUND DURING PSV, CORRODED WEB CLOSURE PANEL AT BS 955 AND LBL 90. REPAIRED PER ERA 498107-14. (ERA 498107-14)
EMERGENCY LIGHTS AT SEATS 32-38 ARE INOPERATIVE. MAINTENANCE RE-SEATED THE PLUG AT 31AB. SYSTEM OPERATION IS NORMAL.
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.
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.
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.
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.
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)
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'.
STATUS MSG - APU CONTROL. REPLACED APU PER AMM, CHECKS GOOD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.
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.
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.
L RECIRC FAN MSG WITH SMOKE IN THE CABIN, FWD TO MCO AND PLACARD PER MEL 21-25-01A.
WXR RADAR FAILED. REPLACED ANTENNA, PERFORMED TEST OK .
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.
LOST CAPT FMC CDU UNABLE TO RECOVER DIVERTING TO SNN FOR REPAIRS. REMOVED AND REPLACED CENTER CDU CKS GOOD MCO AND PLACARD REMOVED.
REPLACED NR 1 ENG PER ROUTINE DECK.
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.
TCAS FAILED IN FLT. INSTALLED PROCESSOR FROM A/C 1821, CKS GOOD.
ENGINE FAILED BORO OPN 5003 COMBUSTION LINER DAMAGED. REPLACED NR 1 ENGINE.
ANTI-SKID OFF EICAS MSG. RESET PARKING BRAKE VALVE C/B. CHECKS OK
APU AUTO SHUTDOWN - FAULTED 49-94007 LOW OIL PRESSURE. REPLACED APU.
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.
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.
COFFEMAKER IN AREA 206, FIRST CLASS GALLEY, SPARKING FROM COLD WATER BUTTON. REPLACED SAME.
AT 23GF MID GALLEY AND AFT GALLEY HAS ONE EACH EMERGENCY CEILING LIGHT INOP. RELAMPED, OPS CHECK OK.
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.