N27957

Part: LIGHT — BROKEN (ZONE 200) · airframe 41,352 hrs · 3,953 cycles

BROKEN 12F SEAT PROXIMITY EMER LT. REPLACED EMER LT ASSY, OPS CHK OK.

Part: ENGINE — FLAMED OUT (LEFT) · airframe 39,401 hrs · 3,766 cycles

ENG FAIL L CAUTION THE LEFT ENGINE HAS FLAMED OUT AND RUN DOWN BELOW IDLE SPEED. FIM TASK REF : G73-90-F8-01A-421B-A CMC MSG# 7332901 FLIGHT STATUS: A INTERMITTENCE CODE: M PH: CLIMB NARRATIVE: ELECTRONIC ENGINE CONTROL CHAN-B (LEFT ENG) SDR FLAGGED.

Part: SLAT — DAMAGED (LEFT WING) · airframe 38,313 hrs · 3,665 cycles

DURING MARSHELLING OF THE A/C. JET BRIDGE STATIONED AT B66 COLLIDES WITH THE LEADING EDGE OF LEFT WING CAUSING SERIOUS DAMAGE. ATTACHED ADDITIONAL PICTURES OF LEFT WING LEADING EDGE DAMAGE SLAT # 2 & #3 M&E # SEE LOG PAGES 6164370 & 6164494 FOR WORK PERFORMED.

Part: GEAR — INOPERATIVE (NLG) · airframe 30,299 hrs · 2,933 cycles

AFTER TAKEOFF GEAR DISAGREE SOUND LIKE NOSEGEAR DOWN DOES NOT FOLLOW COMMAND W/ MX MSG 32-51001, MSG ACTIVE WENT TO INACTIVE WITH GEAR HANDLE DOWN. CREW DEBRIEF: CREW STATED GEAR HANDLE UP, GEAR DISAGREE SOUNDED LIKE GEAR DID NOT RETRACT & DOORS DID NOT CLOSE, PLACED GEAR HANDLE DOWN PER QRH & LANDING GEAR INDICATION NORMAL AND FAULTS CLEARED. AHM CONFIRMS FAULT MX "GEARS DOORS" LANDING GEAR DOORS DUE TO REPEAT FAILURE AND BOEING DIRECTION PLEASE REF. L/P''S 8409606, 8409594, 8409583 FOR COMPONENENT REPLACEMENT DIRECTION. REF LP 8416075. NOSE GEAR RETRACTION WAS PERFORMED AFTER PARTS REPLACEMENT. CLOSED LOG

Part: DOOR — WARNING MESSAGE (UNKNOWN) · airframe 30,265 hrs · 2,926 cycles

GEAR DISAGREE EICAS MSG. GEAR DOOR CAUTION MSG. WITH NOSE GEAR INDICATION SHOWING HASHED. MAINTENANCE MESSAGE 32-51001. FLIGHT CREW BELIVE NLG DID NOT RETRACT WHEN COMMANDED. AIRCRAFT SUBSEQUENTLY DUMPED FUEL AND RETURNED TO LHR.

Part: CONNECTOR — LOOSE (DOOR 2L) · airframe 29,922 hrs · 2,883 cycles

L2 DOOR EMERGENCY EXIT SIGN ABOVE DOOR INOP REF HAECO NON-ROUTIN E NO.9481658 - ORIGINATED BY EMP AS PER N27957(0957) HANGAR NON-ROUTINE PICK UP SHEET (07 MAR 2022) ITEM 1. PERFORMED BY EMP REINSTALLED THE ELECTRICAL CONNECTOR TO DR 2L EXIT MARKING SIGN L3351003 AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LT FOUND NORMAL REF TO AMM 33-51-02-00A-72 0A REV 158 & AMM 33-51-00-00C-320A REV 158. IDT BY

Part: CABLE — NONE (PAX SEAT 31DF) · airframe 29,922 hrs · 2,883 cycles

DURING PERFORM EMERGENCY LIGHT SYSTEM FULL TEST FOUND PAX SEAT 30DF TO 35DF EMERGENCY LIGHT NOT COME ON REF HAECO NON-ROUTINE NO.9479642 - ORIGINATED BY EMP EA 4400-01112 REV A OP001 . PERFORMED BY EMP REFER FIM 33-50-F1-W5A-421A-A REV 140 AND SSM 33-51-11-0A-054A-D REV 136 PERFORMED T/S FOUND PAX SEAT 31DF INSEAT WIRE HARNESS FAULTY. THAT HARNESS CONNECTOR J,PIN 02 PUSHED BACK DUE TO THE LOCK BROKEN. REPLACED THE WIRE HARNESS AND PERFORMED EMERGENCY LIGHT SYS FULL TEST. THE RESULT FOUND "PASSED". PAX SEAT 30DF TO 35DF EMERGENCY LIGHT COME ON REFER AMM 33-51-00-07A-343A-A REV 157. SDR SHOULD BE CHANGE TO Y.

Part: NONE — INOPERATIVE (LH AND RH) · airframe 29,281 hrs · 2,809 cycles

LEFT HF INOP MAINT MESSAGES 42-59471 AND 23-19401. MESSAGES NOT ACTIVE UPON AND AMM 23-11-05. HF OPERATIONAL TEST CHECKS GOOD. ARRIVAL. REPLACED LEFT HF TRANSCEIVER PRECAUTIONARY. RESET ROTABLE PARTS CHANGE WAS INDICATED - TT # 1195254 SN OFF 8018 CROWN DOOR 4L CCS REMOTE DATA CONCENTRATOR 17. REF FIM TASKS DMC-B787-A-42-40-F1-AVA-421A-A. DMC-B787-A-23-10-F1-38A-421A-A. TRANSCEIVER, HF OFF 78-2311-9-0001 8018 ON 78-2311-9-0001 4002

Part: BEAM — CORRODED (MID LAVATORY) · airframe 25,792 hrs · 2,423 cycles

M LAV UNDER SCUFF PLATE BEAM AND FRAME CORROSION REF NON-ROUTINE NR.9426069. SPEC NO.B787-25-3-0069. M LAV UNDER SCUFF PLATE BEAM AND FRAME REPLACED AS PER ECRA 2541 -01547 REV. ORIG.

Part: LIGHT — CRACKED (G9B GALLEY) · airframe 25,792 hrs · 2,423 cycles

THE LEFT FLOOR PROXIMITY LIGHT AT DOOR 3 GALLEY G9B FND CRACKED REF NON-ROUTINE NO.9426063. REPLACED DOOR 3 G9B GALLEY LT 2 EA FLOOR PROXIMITY LIGHT. PERFORMED OP TEST OF EMERGENCY LT FOUND NORMAL REF AMM 33-51-06- 00A-720A REV.144.

Part: LIGHT — CRACKED (DOOR 1 OFCR PNL) · airframe 25,792 hrs · 2,423 cycles

THE LEFT AFT, RIGHT FWD AND RIGHT AFT FLOOR PROXIMITY LIGHT AT DOOR 1 OFCR PANEL FOUND CRACKED REF NON-ROUTINE NO.9426059 - SPEC NO. B787-33-3-0002. THE LEFT AFT, RIGHT FWD AND RIGHT AFT FLOOR PROXIMITY LIGHT AT DOOR 1 OFCR HAD BEEN REPLACED, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT, THE RESULT WAS ''SATIS'' REF TO AMM 33-51-06-00A- 720A-A REV.144.

Part: LIGHT — CRACKED (G5 GALLEY) · airframe 25,792 hrs · 2,423 cycles

THE LEFT FWD, LEFT AFT, RIGHT FWD AND RIGHT AFT FLOOR PROXIMITY LIGHT AT GALLEY G5 FOUND CRACKED REF NON-ROUTINE NO.9426061. REPLACED G5 GALLEY LT FWD, LT AFT, RT FWD, RT AFT FLOOR PROXIMITY LIGHT. PERFORMED OP TEST OF EMERGENCY LT, FOUND NORMAL REF AMM 33-51-06-00A-720A REV.144.

Part: LIGHT — CRACKED (GALLEY G9B) · airframe 25,792 hrs · 2,423 cycles

THE RIGHT FLOOR PROXIMITY LIGHT AT DOOR 3 GALLEY G9B FOUND CRACKED REF NON-ROUTINE NO.9426065. REPLACED DOOR 3 G9B GALLEY RT 2 EA FLOOR PROXIMITY LIGHT. PERFORMED OP TEST OF EMERGENCY LT FOUND NORMAL REF AMM 33-51-06- 00A-720A REV.144.

Part: LIGHT — CRACKED (G4 GALLEY) · airframe 25,792 hrs · 2,423 cycles

THE LEFT FWD, RIGHT FWD AND RIGHT AFT FLOOR PROXIMITY LIGHT AT GALLEY G4 FOUND CRACKED REF NON-ROUTINE NO.9426060 - ORIGINATED BY, SPEC NR.B787-33-3-0002. REPLACED G4 GALLEY LT FWD, RT FWD, RT AFT FLOOR PROXIMITY LIGHT, PERFORMED OP TEST OF EMERGENCY LT, FOUND NORMAL REF AMM 33-51- 06-00A-720A REV.144.

Part: LIGHT — CRACKED (DOOR 3 GALLEY) · airframe 25,792 hrs · 2,423 cycles

THE LEFT AND RIGHT FLOOR PROXIMITY LIGHT AT DOOR 3 GALLEY G9A FND CRACKED REF NON-ROUTINE NO.9426066. REPLACED DOOR 3 GALLEY G9A LT AND RT TOTAL 4 EA FLOOR PROXIMITY LIGHT. PERFORMED OP TEST OF EMERGENCY LT, FOUND NORMAL REF AMM 33 -51-06-00A-720A REV.144.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 24,672 hrs · 2,290 cycles

WINDOW HEAT RT FWD ADVISORY LOSS OF RIGHT FORWARD WINDOW HEAT (PRIMARY). FIM TASK REF: 31-90-F8-01A-421B-A CMC MESSAGE 3032413. FLIGHT STATUS: LT INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: 24 PDHM OPS (GPM L8) CMC MESSAGE 3032413 FLIGHT STATUS: LT INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: 24 PDHM OPS (GPM L8) CMC MESSAGE 3032413 FLIGHT STATUS: LT INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: REF B787 MM TASK DMC-B787-A-56-11-01-00A-52A-A STARTED REMOVAL OF FO'S WINDSHIELD. WINDOW IS DISCONNECTED AND READY TO BE REMOVED FROM WINDOW FRAME. REMOVED DAMAGED WINDOW. STARTED WINDOW INSTALLATION, REF DMC-B787-A-56-11-01-00A-720A-A, STOPPED AT STEP 4E, INSTALLED BOLTS LOOSELY ON TOP SIL. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1067244 SN OFF 1246 WINDSHIELD, NR 1 OFF 78-5610-9-9002 1246 ON 79-5611-9-0002 4168. REPLACED RIGHT FWD WINDSHIELD, REF DMC-B787-A-56-11-01-00A-520A-A, HEAT TEST PASS. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1212125 SN OFF 4168 WINDSHIELD, ASSEMBLY OFF 79-5611-9-0002 4168 ON 79-5611-9-0002 3250, REF AMM FLIGHT COMPARTMENT NR 1 WINDOW-INSTALLATION, REFERENCE: DMC-B787-A-56-11-01-00A-720A-A.

Part: ENGINE — VIBRATION (LEFT) · airframe 15,846 hrs · 1,477 cycles

LEFT ENG HIGH VIBRATION 7.0. OPERATED AT 66 N1 VIB 2.0. REVIEW OF CMC NIL EXCEEDANCES RECORDED REF CREW REPORT AIRCAFT WAS OPERATING IN ICING CONDITIONS. REF.FTD 71-13002. NIL MSG NOTED HI VIBRATION NOTED. INSPECTION CARRIED OUT AS PER AMM G71-00-00-3A-280A NIL DEFECTS NOTED ENGINE GRD RUN CARRIED OUT L & R ENGINES ALL PARAMETERS AND INDICATIONS NORMAL NIL VIBRATION.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 11,399 hrs · 1,077 cycles

FIRST OFFICER'S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAULTY (EMERGENCY LIGHTS) · airframe 9,501 hrs · 910 cycles

DURING EMERGENCY LIGHT TEST, FOUND FLOOR LIGHTING AT ROWS 1 & 2 INOPERATIVE. R & R WCU AT SEAT 1F, OPS CHECKED GOOD. WORK IAW AMM 33-51-00-00C-320A.