N816AA

Part: STRAP — MISSING (ZONE 200) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN OFCR MISSING ESCAPE PANEL STRAP. INSTALLED CABIN OFCR ESCAPE PANEL STRAP. PER BOEING SRM B787-A-51-43-01-01A-010A-A.

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING #6 SLAT IN BOARD MAIN TRACK HAS PITTING. REPLACED #6 SLAT IN BOARD MAIN TRACK PER AMM DMC B787-A-27-81-47-00A-520A-A AND DMC B787-A-27-81-47-00A-720A-A.

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING #6 SLAT OUT BOARD MAIN TRACK HAS PITTING. REPLACED #6 SLAT OUT BOARD MAIN TRACK PER AMM B787-A-27-81-47-00A-520A-A AND AMM B787-A-27-81-47-00A-720A-A.

Part: FITTING — CORRODED (ZONE 100) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON KEEL BEAM LATTICE FITTING AT STA 910. REPLACED KEEL BEAM LATTICE FITTING PER SRM B787-A-51-41-05-03A-010A-A.

Part: STIFFENER — CRACKED (ZONE 400) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT PYLON OUTBD CUTOUT FRAME IS CRACKED AT UPPER MIDDLE SECTION. REPLACED STIFFENER ASSEMBLY PER SRM B787-A-51-43-05-03A-010A-A.

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING SLAT NUMBER 6 MIDDLE SLAT TRACK HAS PITTING. REPLACED SLAT TRACK PER DMC-B-787-A-27-81-47-010-941A-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR PANEL AT SEAT 30D IS DELAMINATEDD. ACCOMPLISHED PERMANENT REPAIR PER SRM B787-A-53-00-50-03A-663A-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED PASSENGER CABIN FLOOR PANEL FROM SEAT 25A TO SEAT 27A. REPLACED FLOOR PANEL PER AMM B787 A-53-01-01-02A-520A-A / 720A-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED PASSENGER CABIN FLOOR PANEL FROM SEAT 4L TO SEAT 5L. REPAIRED FLOOR PANEL PER SRM B787-A-53-00-50-03A-663A-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CAMIN FLOOR PANEL AT MID GALLEY IS DELAMINATED. ACCOMPLISHED PERMANENT REPAIR TO DELAMINATION PER SRM B787-A-53-00-50-03A-663A-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 32,997 hrs · 4,478 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED PASSENGER CABIN FLOOR PANEL AT SEAT 20H. REPLACED FLOOR PANEL PER AMM B787-A-563-01-01-02-520A-A/720A-A.

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 32,722 hrs · 4,439 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING W/C: 78T21033001 FOUND FAULT: MAINT MSG: 33-11311. MAINTENANCE REPLACED WIRELESS EMERGENCY LIGHTING SYSTEM CONTROL UNIT BATTERY WBU 11 W/ HARDWARE SERIAL NUMBER ST19120607 IAW AMM'33-51-07.

Part: DISPLAY — INTERMITTENT (ZONE 200) · airframe 32,612 hrs · 4,422 cycles

AIRCRAFT WAS NOT GROUNDED: APPROX ZERO INTO FLIGHT FO/'S SCREENS STARTED BLINKING OFF THENBACK ON. AT APPROX 3 HOURS AND BEFORE ENTERING OCEANIC AIRSPACESTATUS MDG AHRU R APPEARED. NEXT ''EFIS/DSP PANELR'' CHECK LISTSPEARED AS WELL AS '' EFIS/DSP PANEL R THEN '' WEATHER RADAR SYSL'' MSG APEARED - RAN & COMPELETED CHECK LIST'S. TURNED AIRPLANE AROUND AND RETURNED TO ORD. PFMD PRIMARY DISPLAY SYS OPS TEST AMM 31-61-00. PFMD ISS WXR OPSTEST AMM 34-42-00. PFMD EARTH REF SYS OPS TEST AMM 34-21-00. ALL OPS TESTS PASSED. FAULTS CLEARED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,601 hrs · 4,159 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK STEP C, WBU 11, HARDWARE P/N 100-2602-01. S/N : ST19120607,NEEDS TO BE REPLACED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 30,601 hrs · 4,159 cycles

AIRCRAFT WAS NOT GROUNDED: PER W/C : 78T21033001 : EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK STEP C, WBU 03, NEEDS TO BE REPLACED. **SUPPLEMENTAL SDR FOR AALA202405038003** (CLOSED) MAINTENANCE REPLACED, WELS BATTERY WCU03, PER TASK CARD 78C20033001.

Part: LIGHT — INOPERATIVE (SEAT 2D) · airframe 30,574 hrs · 4,155 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT CENTER AISLE 2D INOP. MAINTENANCE REMOVED AND REPLACED LUMINATOR LIGHT AT SEAT 2D, IAW 33-51-06.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,601 hrs · 4,159 cycles

AIRCRAFT WAS NOT GROUNDED: PER W/C : 78T21033001 : EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK STEP C, WBU 03, NEEDS TO BE REPLACED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 30,601 hrs · 4,159 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK STEP C, WBU 11, HARDWARE P/N 100-2602-01. S/N : ST19120607,NEEDS TO BE REPLACED. **SUPPLEMENTAL REPORT FOR SDR AALA202405032269.** (CLOSED) MAINTENANCE REPLACED WIRELESS EMERGENCY LIGHTING SYSTEM CONTROL UNIT BATTERY WBU 11 W/ HARDWARE SERIAL NUMBER ST19120607 IAW AMM'33-51-07.

Part: CHANNEL — CRACKED (ZONE 200 - FUSE) · airframe 28,917 hrs · 3,942 cycles

AIRCRAFT IN BASE MAINTENANCE: MOP SEAL NEXT TO SEAT 11A IS CRACKED. PERFORMED MOPSIL REPAIR AT SEAT 11A. PER AARD 25-21-01-2.

Part: CHANNEL — CRACKED (ZONE 200 - FUSE) · airframe 28,917 hrs · 3,942 cycles

AIRCRAFT IN BASE MAINTENANCE: MOPSIL CRACKED AT SEAT 12A. PERFORMED MOPSIL REPAIR AT SEAT 12A. PER AARD 25-21-01-2.

Part: CHANNEL — CRACKED (ZONE 200 - FUSE) · airframe 28,917 hrs · 3,942 cycles

AIRCRAFT IN BASE MAINTENANCE: MOP SEAL CRACKED NEXT TO SEAT 15L. INSTALLED DOUBLER. PER AARD 25-21-01-2.

Part: CHANNEL — CRACKED (ZONE 200 - FUSE) · airframe 28,917 hrs · 3,942 cycles

AIRCRAFT IN BASE MAINTENANCE: MOP SEAL CRACKED NEXT TO SEAT 13. INSTALLED DOUBLER REPAIR. PER AARD 25-21-01-2.

Part: CHANNEL — CRACKED (ZONE 200 - FUSE) · airframe 28,917 hrs · 3,942 cycles

AIRCRAFT IN BASE MAINTENANCE: MOP SEAL CRACKED NEXT TO SEAT 10L. INSTALLED DOUBLER. PER AARD 25-21-01-2

Part: STABILIZER — WARNING MESSAGE (ZONE 300 - STABS) · airframe 28,784 hrs · 3,921 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED ON ARRIVAL INTO PHL DUE A STABILZER L2 EICAS MESSAGE. THE AIRCRAFT LANDED SAFELY AT PHL AND TAXIED TO THE GATE. MAINTENANCE ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE STABILZERS PER FIM TASK 27-401F-11A-412A-A WITH NO DEFECTS NOTED.

Part: DUCT — DAMAGED (ZONE 100 - FUSE) · airframe 28,286 hrs · 3,856 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO RAISING CABIN PRESSURIZATION ISSUES, EMERGENCY DESCENT TO FLT 100 AIRCRAFT LANDED SAFELY AT SCL WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LEFT LOWER RECIRCULATION FAN (AALA202310102827) AND LEFT INNER RECIRCULATION DUCT (AALA202310106591). PER AMM 21-25-17.

Part: FAN — DAMAGED (ZONE 100 - FUSE) · airframe 28,286 hrs · 3,856 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO RAISING CABIN PRESSURIZATION ISSUES, EMERGENCY DESCENT TO FLT 100 AIRCRAFT LANDED SAFELY AT SCL WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LEFT LOWER RECIRCULATION FAN (AALA202310102827) AND LEFT INNER RECIRCULATION DUCT (AALA202310106591). PER AMM 21-25-17.

Part: SLIDER — BINDING (LAVATORY DOOR) · airframe 25,058 hrs · 3,430 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY 3F-12C, DOOR GETS STUCK. RE-INSTALLED SLIDER ON TOP OF LAVATORY DOOR THAT FELL ON FLOOR AS REQUIRED.

Part: DOOR — BROKEN (ZONE 900 - LAV/G) · airframe 20,905 hrs · 2,813 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY 3L DOOR BROKEN. REINSTALLED 3L LAVATORY DOOR IAW AMM 25-41-00, OPS CHECK GOOD.

Part: BUSTLE — INOPERATIVE (R2 DOOR SLIDE) · airframe 19,638 hrs · 2,563 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR R2 BUSTLE ON SLIDE COVER NOT GRABBING. REPLACED/ADJUSTED BUSTLE AT DOOR R2 PER AMM 52-11-24-03A-720A.

Part: BUSTLE — OUT OF ADJUST (R3 DOOR SLIDE) · airframe 19,638 hrs · 2,563 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR SLIDE COVER BUSTLE NOT GRABBING. ADJUSTED SLIDE BUSTLE IAW AMM 52-11-24-03A-720A, OPS CHECK GOOD.

Part: HINGE — INOPERATIVE (ESCAPE REEL DOOR) · airframe 18,887 hrs · 2,415 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE REEL STOWAGE DOOR DOES NOT OPEN PROPERLY. REPLACED HINGE FOR EMERGENCY ESCAPE REAL STOWAGE DOOR PER AMM 25-15-06.

Part: SLIDE — UNSERVICEABLE (R4 DOOR) · airframe 18,401 hrs · 2,313 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 4R SLIDE REQUIRES REPLACEMENT. REPLACED 4R SLIDE PER 78L80025001.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 16,328 hrs · 2,006 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS IN OAFR DO NOT COME ON. REPLACED WBU 31 BATTERY, PER AMM 33-51-07.

Part: MODULE — CONTAMINATED (FLT CONTROLS) · airframe 16,280 hrs · 1,995 cycles

AIRCRFT WAS GROUNDED: AIR RETURNED TO DFW ACCOUNT FLIGHT CONTROL INDICATION MESSAGE. FLIGHT DECLARED EMERGENCY AND AIRCRAFT LANDED OVERWEIGHT. FCE-R CABINET, ACE MODULE HAS EVIDENCE OF MOISTURE EGRESS. REPLACED FCE-R CABINET ACE MODULE IN THE AFT E/E COMPARTMENT. AMM 27-02-17.

Part: AIR DATA MODULE — FAULTED · airframe 16,255 hrs · 1,991 cycles

AIRCRAFT WAS GROUNDED: DIVERTED TO ORD ACCOUNT OF SPOILER/STABILIZER FAULT MESSAGES (STABILIZER R2, SPOILER PAIRS, NO, AUTOLAND AND AUTO SPEED BRAKE, ACES R INOP.). FLIGHT DECLARED EMERGENCY. FOUND MSG 27-23032 . REPLACED R ACE 2 MODULE IAW 787 MM 27-02-17 RAN LRU REPLACEMENT TEST, OPS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 16,170 hrs · 1,973 cycles

AIRCRAFT NOT GROUNDED - EICAS MESSAGE: LAVATORY SMOKE; CREW HEARD AND SAW ALARM OUTSIDE LAV 3F-1LC, NO SIGN OF ANYONE SMOKING IN LAV. PERFORMED LAV SMOKE DETECTION SYSTEM OPERATIONAL CHECK PER BOEING AMM DMC-B787-A-26-13-00-00A-300B-A, NO DEFECTS NOTED.

Part: VHF COMM — MALFUNCTIONED · airframe 15,661 hrs · 1,863 cycles

AIRCRAFT WAS GROUNDED: DURING CLIMBOUT SAT VOICE LOST DATALINK, LOST VHF DATALINK, LOST HF DATALINK LOST APPEARED RTB DFW. EMERGENCY WAS DELCARED.***SUPPLEMENTAL ACTION SECT 4: RE-LOADED SOFTWARE, OPERATIONAL CHECKED GOOD IAW AMM 45-13-00 .

Part: B-NUT — LOOSE (SCAV PUMP) · airframe 13,942 hrs · 1,607 cycles

AIRCRAFT WAS GROUNDED: FLIGHT AIR RETURNED TO DFW ON ACCOUNT OF NUMBER ONE ENGINE OIL OUANTITY ISSUE. EMERGENCY DECLARED. MAINTENANCE FOUND OIL SCAVENGE LINE B-NUT LOOSE AT AFT HOT SECTION, 5 OCLOCK POSITION. TIGHTENED B-NUT IAW AMM 79-21-00 AND AMM 70-21-00. LEAK CHECK GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 12,540 hrs · 1,418 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT IN FLIGHT CREW COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED BATTERY FOR FLASHLIGHT PER AMM 7-25-64-00.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 12,540 hrs · 1,418 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT DOOR 3R INOPERATIVE. MAINTENANCE REPLACED BATTERY FOR FLASHLIGHT PER AMM 77-25-64-00.

Part: BOTTLE — LEAKING (L1 DOOR) · airframe 11,128 hrs · 1,181 cycles

EICAS MESSAGE, L1 DOOR EPISODE SQUIB AND DOOR EPISODE SENSORS. REPLACED L1 DOOR EPAS PRESSURE BOTTLE AND PERFORMED SATISFACTORY OPERATIONAL CHECKED IAW AMM 52-11-22.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 10,824 hrs · 1,144 cycles

R1 FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00-00B-921A, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 10,608 hrs · 1,120 cycles

FOUND WIRE BROKEN ON BACK OF LIGHT ASSEMBLY OF MAIN AISLE MONUMENT MOUNTED PROXIMITY LIGHTS. REPAIRED THE WIRE.

Part: OVEN — SMOKE (AFT GALLEY) · airframe 9,432 hrs · 983 cycles

FLIGHT ATTENDANT REPORTED THE OVEN IN THE AFT GALLEY SMOKES WHEN IN USE. TURNED OFF THE OVEN. REPLACED THE AFT GALLEY OVEN IAW CMM 25-37-39, CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 9,265 hrs · 965 cycles

R3 FLIGHT ATTENDANTS FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW DMC-B787-A-25-64-00-00B-921A-A.

Part: MODULE — MALFUNCTIONED · airframe 8,220 hrs · 835 cycles

REMOTE DATA CONCENTRATOR FAILED DURING CRUISE, AT FL360. RT FUEL PUMP AFT AND AUTO SPEEDBRAKE EICAS CAUTIONS APPEARED WITH A TOTAL OF 17 STATUS MESSAGES INCLUDING SPAR VALVE R AND AHRVR. FUEL PUMP RIGHT AFT FAILED AND PRESSURE LIGHT ILLUMINATED. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO ORD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. INVESTIGATED MAINTENANCE MESSAGE 42-59500 FOR RDC-10. GROUND TEST PASSED TO RESET MODULE IAW FIM 42-40-F2. MESSAGES CLEARED BY GROUND TEST. OK FOR SERVICE.

Part: ACTUATOR — FAILED (DEFLECTOR DOOR) · airframe 5,851 hrs · 590 cycles

EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A LEFT AIR CONDITIONING PACK WARNING INDICATION. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT CABIN AIR COMPRESSOR INLET DEFLECTOR DOOR ACTUATOR IAW AMM DMC-B787-A-21-51-16-00A. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BOTTLE — FAILED (L1 DOOR) · airframe 4,907 hrs · 492 cycles

L1 DOOR EMERGENCY POWER ASSIST SYSTEM SQUIB MAINTENANCE MESSAGE RECEIVED. REMOVED AND REPLACED EPAS RESERVOIR BOTTLE ASSEMBLY IAW AMM DMC-B787-A-52-11-22. OPS CHECKED GOOD.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 4,169 hrs · 416 cycles

EMERGENCY EXIT LIGHT BY G5 GALLEY LEFT SIDE HAS AN UNSECURE LENS COVER. SECURED THE LENS COVER IAW AMM 25-00-00. OPS CHECKED GOOD.

Part: BOTTLE — FAULTY (L1 DOOR) · airframe 3,947 hrs · 392 cycles

AIRCRAFT WAS GROUNDED. L1 SQUIB DOOR MAINTENANCE MESSAGE 52-10933. REMOVED AND REPLACED L1 DOOR EMERGENCY POWER ASSIST SYSTEM PRESSURE BOTTLE ASSEMBLY IAW DMC-B787-A-52-11-22-080-941A-D. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 3,813 hrs · 378 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L4 STATION FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LEAKING (L1 DOOR) · airframe 3,720 hrs · 368 cycles

WHILE EXITING L1 DOOR, A HISSING SOUND WAS COMING FROM THE DOOR. REMOVED AND REPLACED EMERGENCY POWER ASSIST SYSTEM RESERVOIR BOTTLE ASSEMBLY IAW AMM 52-11-22. OPERATONAL CHECK GOOD.

Part: BOTTLE — UNSERVICEABLE (L1 DOOR) · airframe 3,544 hrs · 352 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY POWER ASSIST SYSTEM EICAS MESSAGE. REMOVED AND REPLACED EPAS RESERVOIR BOTTLE IAW AMM 52-11-22. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 3,410 hrs · 338 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L4 DOOR CENTER SEAT FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: ATTACH FITTING — DIRTY (ZONE 800) · airframe 3,080 hrs · 307 cycles

AIRCRAFT WAS NOT GROUNDED. L2 DOOR EMERGENCY EVACUATION SLIDE LEVER IS DIFFICULT TO PLACE IN ARMED POSITION. CLEANED DEBRIS FROM GIRT BAR ATTACH FITTING IAW AMM B767-A-52-11-00. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 2,926 hrs · 290 cycles

AIRCRAFT WAS NOT GROUNDED. DURING MIDFLIGHT, THE SMOKE DETECTOR IN LAVATORY 3F-1RC EMITTED A WARNING INDICATION. NO SMOKE OR FIRE WAS NOTED. TESTED THE SMOKE DETECTOR IAW AMM DMC-B787-A-26-13-00-00B-320A-A. OPERATIONAL CHECK GOOD.

Part: BOTTLE — FAULTY (L1 DOOR) · airframe 2,562 hrs · 253 cycles

L1 DOOR EMERGENCY POWER ASSIST SYSTEM PRESSURE BOTTLE ASSEMBLY STATUS MESSAGE. REMOVED AND REPLACED EPAS BOTTLE ASSEMBLY IAW 52-11-22. OPERATIONAL CHECK GOOD.

Part: BRAKE ASSY — FAULTY (MLG) · airframe 2,562 hrs · 253 cycles

MAIN LANDING GEAR BRAKE THREE ACTUATOR MESSAGE DISPLAYED AFTER SHUTDOWN. REMOVED AND REPLACED BRAKE ASSEMBLY IAW AMM 32-45-07. OPERATIONAL CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 756 hrs · 84 cycles

L2 DOOR FORWARD AND AFT AISLE MOUNTED EMERGENCY EXIT LOCATORS ARE INOPERATIVE. REMOVED AND REPLACED THE CONTROL UNIT BATTERY IAW AMM 33-50-07. OPS CHECKED NORMAL.

Part: LINE — LEAKING (NR 1 ENG OIL)

AFTER DEPARTING, ON CLIMB OUT, PASSING 12,500 FT, NR 1 OIL PRESSURE LIGHT CAME ON AND NR 1 OIL PRESSURE INDICATED ZERO. REDUCED NR 1 ENGINE TO IDLE AND FOLLOWED ENGINE SHUTDOWN PROCEDURES IN MFG OPERATING HANDBOOK. DECLARED EMERGENCY AND RETURNED TO DEPARTURE WITH NR 1 ENGINE SHUTDOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINT SENT, REMOVED AND REPLACED OIL TUBE LOCATED AT 3 OCLOCK POSITION AFT WITH SERVICEABLE TUBE IAW MM. OPS AND LEAKED CHECK GOOD, DURING ENGINE RUN UP IAW SEI-189. NO OTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE)

DURING RVSM FLT TESTING, IN LEVEL FLT AT FL375, NR 1 ENG FLAMED OUT. CREW DECLARED EMERGENCY, DRIFTED DOWN & ENGINE RE-STARTED AT FL290 USING AIRSTAT CHECKLIST. A/C RETURNED TO YIP & LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED NR 1 ENG TO DETERMINE CAUSE OF FLAME OUT. COMPRESSOR WAS BORESCOPED & FOD DAMAGE FOUND IN 6TH STAGE. DAMAGE BLENDED IAW GE SEI-187 MM 72-32-0. NR 1 ENG ANTI-ICE LINE FOUND TO BE CRACKED & REPAIR WELDED IAW THE USA JET GMM VOL 3, CHP 51, PAGE 5. ENG GIVEN A COMPRESSOR WASH & RUN TO CHECK PARAMETERS & FOR LEAKS. ENG RUN & CHECKED GOOD. A/C TEST FLOWN & A 'MAXIMUM ALTITUDE ACCELERATOIN TEST' PERFORMED IAW GE SEI-187 MM. TEST FLT SATISFACTORY & A/C RETURNED TO SERVICE. (M)

Part: ENGINE — FLAME OUT (LEFT)

PILOT REPORTED WHILE IN A STEADY STATE CLIMB-OUT OF FL 310, LT ENG FLAMED OUT AT 31,400 FEET. ACFT FLYING AT .68 MACH. THERE WERE NO CLOUDS AND NO TURBULENCE. CREW DESCENDED AND TRIED RESTARTS AT FL 290, FL 250, AND FL 150 WITHOUT SUCCESS. ENG RELIGHT FINALLY ACHIEVED AT 11,000 FEET. ACFT CONTINUED TO DESTINATION WITHOUT INCIDENT. ENG GIVEN A THOROUGH INSPECTION OF INLET AND EXHAUST FOR EVIDENCE OF FOD, BUT NONE FOUND. FUEL SYS CHECKED. A FULL GRND POWER RUN PERFORMED ON ENG IAW GE MM AND ALL PARAMETERS CHECKED WITHIN LIMITS. NO MECHANICAL CAUSE COULD BE FOUND FOR FLAME-OUT. THIS SAME FLIGHT CREW SUFFERED A FLAME-OUT OF LT ENG ON ANOTHER ACFT WITHIN PREVIOUS 24 HRS. ENG RETURNED TO SERVICE. (X)