N867DA

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 79,553 hrs · 8,757 cycles

(AIRCRAFT 7008, L/P 1387470) EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:603 / INTERIOR. CORRECTIVE ACTION: NEW LENS INSTALLED.

Part: INDICATOR — MALFUNCTIONED (DOOR ARMING) · airframe 77,113 hrs · 8,512 cycles

F/A PANEL INDICATES ARMED DOOR BUT DOOR INDICATES SAFE. ARMED/DISARMED ALL ENTRY DOORS PER B777 AMM 52-71.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,058 hrs · 8,403 cycles

DURING C3 CHECK, INSPECTIONS ON THE SEC 47 FUSELAGE SKIN (P/N 147W2352-4) C/T 147W2312-211 SKIN PANEL ASSY, SEVERAL DAMAGES (BLENDOUTS + DENTS) WERE FOUND WITHIN CLOSE PROXIMITY FROM STA 2000  STA 2087, BETWEEN S-37R TO S-43R. BLENDED OUT DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER. LP 0978085.

Part: LENS — CRACKED (CABIN) · airframe 76,058 hrs · 8,403 cycles

DURING C3 CHECK, EMERGENCY LIGHT LENS ASSEMBLY CRACKED AT EXTERIOR OF OFCRE AND A4 GALLEY. REPLACED EMERGENCY LIGHT LENS ASSEMBLY. LP 0973670

Part: LIGHT — DETACHED (SEAT 55F) · airframe 75,477 hrs · 8,321 cycles

(AIRCRAFT 7008, L/P 5239321) EMERGENCY LIGHT AT SEAT 55F HANGING DOWN. INSTALLED LIGHT CKS OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 75,477 hrs · 8,321 cycles

(AIRCRAFT 7008, L/P 5239320) EMERGENCY LIGHT RED LENS COVER MISSING IN ISLE AT MID GALLEY. INSTALLED RED LENS COVER CKS OK.

Part: LIGHT — DAMAGED (CABIN) · airframe 75,383 hrs · 8,309 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:10B / INTERIOR. ESCAPE PATH LIGHTING AT SEAT 10B RELAMPED.

Part: ACTUATOR — FAULTY (R2 DOOR) · airframe 75,245 hrs · 8,292 cycles

(AIRCRAFT 7008, L/P 0797001) A/C AHM CONTINUES TO DOWN LINK ACTIVE MMSG 52-11310, 52-12120, AND 52-12130 PED 2R ACTUATOR HAS A FAULT OR OUT OF POSITION. REPLACED FLIGHT LOCK ACTUATOR PER AMM 52-11. TEST GOOD PER AMM 52-11. NO FAULTS FOUND.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,992 hrs · 8,166 cycles

EMERGENCY LIGHTS INOP ROW 10-12 SEATS. REMOVED AND REPLACED POWER SUPPLY M33098 PER AMM 33-51-06.

Part: LENS — DAMAGED (CABIN) · airframe 73,992 hrs · 8,166 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE, LOCATIONS:903. REPLACED LENS CKS GOOD.

Part: LENS — DAMAGED (CABIN) · airframe 73,992 hrs · 8,166 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE, LOCATIONS:901. REPLACED LENS CKS GOOD.

Part: LENS — MISSING (CABIN) · airframe 73,992 hrs · 8,166 cycles

RED LENS COVER MISSING ON FLOOR PROXIMITY LIGHT ON SIDE OF GALLEY NEXT TO THE 4R DOOR. REPLACED LENS COVER PER AMM 33-51-05.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,316 hrs · 8,097 cycles

ZONE 2 FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK M33404 IAW AMM 33-51-06.

Part: PACKING — DAMAGED (LT ENGINE) · airframe 73,274 hrs · 8,093 cycles

DIV TO KEF DUE TO LEFT ENGINE OIL QUANTITY DROPPING. MAINTENANCE FOUND 2 OIL LINES AT INTERMEDIATE GEARBOX LEAKING OIL, REPLACED PACKINGS ON BOTH OIL LINES. COMPLIED WITH OIL SYSTEM LEAK CHECK, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: COVER — MISSING (L1 DOOR) · airframe 70,353 hrs · 7,787 cycles

DOOR OR GIRT BAR PROXIMITY SENSOR COVER DAMAGE/MISSING. RE-ATTACHED 1L DOOR COVER. OPS SATIS.

Part: SWITCH — FAILED (RT BACK UP GEN) · airframe 70,149 hrs · 7,764 cycles

BACKUP GENERATOR RT LIGHT INOPERATIVE. R & R THE RT BACKUP GENERATOR SWITCH IAW AMM 33-13. OPS CHECKED GOOD.

Part: PANEL — CRACKED (LT WING) · airframe 70,251 hrs · 7,775 cycles

DURING A TURBULENCE INSPECTION OF THE LEFT WING UPPER SURFACE, FOUND A THREE INCH CRACK ON FIXED PANEL AFT OF THE NR 7 SLAT. 12 INCHES INBD OF OTBD EDGE ON AFT EDGE OF PANEL. NO DEFORMATION AROUND CRACKED AREA. REMOVED AND REPAIRED THE PANEL IAW SRM 51-70-05, REPAIR .

Part: LENS — MISSING (CABIN) · airframe 68,847 hrs · 7,611 cycles

COVER FOR EMERGENCY PATHWAY LIGHT AT DOOR 1L MISSING. INSTALLED RED LENS COVER.

Part: SPAR — CORRODED (NR 1 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02, ER/A 558254-14 PRI, REV 0, ER/A 558254-14, PRI REV 0, AND COMPAIRED IAW ER/A 558254-14AD, REV 0. FOUND IN COMPLIANCE.

Part: SPAR — CORRODED (NR 1 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 2 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 2 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 1 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 2 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 2 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 1 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 2 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 2 ENGINE PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 1 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 2 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 2 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (NR 1 NACELLE) · airframe 68,618 hrs · 7,589 cycles

NR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (BS 506) · airframe 68,617 hrs · 7,588 cycles

FWD CARGO DOOR LOWER MAIN SILL UPPER SURFACE FOUND CORRODED AT BS 506. REPAIRED IAW ER/A 552734-14, PRI REV 0.

Part: FLOOR SUPPORT — CHAFED (BS 1077-1287) · airframe 68,618 hrs · 7,589 cycles

FLOOR SUPPORT BS 1077 - 1287, RBL 33 FOUND CHAFED AROUND FLOOR PANEL ATTACHMENT HOLES. REPAIRED IAW ER/A 552736-14 PRI, REV 0.

Part: FLOOR SUPPORT — CHAFED (BS 1035-1297) · airframe 68,618 hrs · 7,589 cycles

FLOOR SUPPORT BS 1035 - 1297, LBL 11 FOUND CHAFED AROUND FLOOR PANEL ATTACHMENT HOLES. REPAIRED IAW ER/A 552735-14 PRI, REV 0.

Part: FLOOR SUPPORT — CHAFED (BS 1056-1287) · airframe 68,618 hrs · 7,589 cycles

FLOOR SUPPORT BS 1056 - 1287, LBL 11, FOUND CHAFED AROUND THE FLOOR PANEL ATTACHMENT HOLES. REPAIRED IAW ER/A 552735-14 PRI, REV 0.

Part: FLOOR SUPPORT — CHAFED (BS 1035-1287) · airframe 68,618 hrs · 7,589 cycles

BS 1035 - 1287, RBL 11 FLOOR SUPPORT FOUND CHAFED AROUND FLOOR PANEL ATTACHMENT HOLES. REPAIRED IAW ER/A 552735-14 PRI, REV 0.

Part: FLOOR SUPPORT — CHAFED (BS 1035-1225) · airframe 68,618 hrs · 7,589 cycles

FLOOR SUPPORT, BS 1035 - 1225, RBL 33 FOUND CHAFED AROUND FLOOR PANEL ATTACHMENT HOLES. REPAIRED IAW ER/A 552736-14 PRI, REV 0.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,573 hrs · 7,583 cycles

MULTIPLE EMERGENCY LIGHT LAMPS ARE INOPERATIVE AND MISSING COVERS. REPLACED THE LAMPS AND INSTALLED COVERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,477 hrs · 7,572 cycles

MULTIPLE EMERGENCE FLOOR LIGHTS INOP/MISSING COVERS. RE-LAMPED AND INSTALLED LENS COVERS AS REQUIRED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,379 hrs · 7,562 cycles

BOTH EMERGENCY "EXIT" SIGNS AT DOOR 3L INOP. REPLACED BATTERY PACK M33406 PER AMM 33-51-06.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 67,833 hrs · 7,513 cycles

EMERGENCY LIGHTS AT SEATS 3C AND 1B MISSING COVERS. REPLACED THE COVERS.

Part: LENS — MISSING (CABIN) · airframe 66,599 hrs · 7,405 cycles

AFT CABIN END BULKHEAD MISSING RED EPATH LENSES. REPLACED FLOOR PROX LIGHT LENS ON WALL.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 54,048 hrs · 6,102 cycles

LEFT & RIGHT SEAT AISLE EMERGENCY LIGHTS INOPERATIVE, ROWS 10 THRU 14. REPLACED FUSE IAW AMM 33-51-06 960-801. OPS CHECKED OK.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,800 hrs · 5,865 cycles

DURING CHECK, EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT IAW FIM 33-51-00 AND WDM 33-51-58. REPLACED FUSES IN M33404 POWER SUPPLY. OPS CHECKED GOOD. AMM 33-51-06. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 51,602 hrs · 5,847 cycles

R2 DOOR ASSIST BOTTLE PSI LOW. R & R BOTTLE IAW AMM 52-11. OPS CHECKED GOOD.

Part: PIN — NOT SEATED (CONNECTOR) · airframe 44,253 hrs · 5,186 cycles

DURING A MAINTENANCE VISIT, THE OVERHEAD EXIT EMERGENCY SIGN AT DOOR 1L WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE PUSH PIN AT THE CONNECTOR DISCONNECTED AND RESEATED IT. SYSTEM OPERATION WAS NORMAL AFTER THE PIN WAS RESEATED. (2011-D1392)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,371 hrs · 5,002 cycles

DURING THE WALK AROUND INSPECTION TWO EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT SEATS 10B AND 14B. MAINTENANCE REPLACEDTHE LIGHT ASSEMBLY AND A BLOWN FUSE FOUND AT BATTERY PACK M33098. OPERATION CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,201 hrs · 4,885 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY CABIN LIGHTS FROM BATTERY PACK M33400 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE CHARGER AND BATTERY PACKS M33400 AND M33405 AND INSTALLED CHARGER AND BATTERY SERIAL NUMBER 25185AT M33400 AND SERIAL NUMBER 589544 AT M33405. SYSTEM OPERATION WAS NORMAL AFTER CHARGER AND BATTERY WERE REPLACED.

Part: UNKNOWN — ODOR (GALLEY) · airframe 38,076 hrs · 4,560 cycles

ENROUTE F/A REPORTED ELECTRICAL ODOR IN AFT GALLEY. IT WAS UNKNOWN IF ANY PRECAUTIONARY ACTION WAS TAKEN. FLIGHT CONTINUED ON TO PVG WHERE MX DEFERRED THE OVEN AND WILL REPLACE IT AT A LATER TIME. (DL777101496)

Part: OVEN — ODOR (GALLEY) · airframe 38,062 hrs · 4,559 cycles

RTB FOR BURNING SMELL IN AFT CABIN T/S FOUND SMELL FROM CTR OVEN. PULL COLLAR C/B. FWD TO NEF PROGRAM 253.30. PLACARD INSTALLED. (DL777101468)

Part: OVEN — MALFUNCTIONED (FWD GALLEY) · airframe 36,310 hrs · 4,388 cycles

FLT CREW REPORTED 2 HALON BOTTLES USED ON FWD GALLEY OVEN AT POS NR 1 DUE TO HISSING ARCHING AND GLOW. C/B HAS ALSO BEEN PULLED TO ISLOATE OVEN. OVEN ISSUE ISLOATED AND OK NOW IAW CAPT. RPLCD OVEN IAW AMM. OPS CK GOOD MP/N 72077500. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: DISPLAY — INTERMITTENT (COCKPIT) · airframe 35,982 hrs · 4,357 cycles

UPPER DISPLAY UNIT FLICKERS OFF MORE THAN 7 SECONDS IN 10 SECONDS. REPLACED UPPER DISPLAY IAW AMM, CHECKS GOOD.

Part: PROBE — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 35,673 hrs · 4,326 cycles

AFTER ENGINE START - HEAT PITOT C EICAS MSG AND NO LAND 3 MSG. REMOVED AND REPLACED CTR PITOT/STATIC PROBE PER M/M. ALL OPS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 35,207 hrs · 4,282 cycles

FMC FUEL TOTALIZER DID NOT REDUCE DURING TAXI REMAINED FROZEN AT BLOCK OUT FUEL DISAGREED WITH EICAS AND FMC CALC BY 2000 LBS PLUS WHEN ENGINES SHUTDOWN FMC CALCULATED JUMPED UP TO MATCH FMC TOTALIZER VALUE WHICH LEFT ONLY EICAS AS ACCURATE. RESET ALL F/Q C/BS P320 D7 P310 G10 J8 J11 P210 L1 RAN ENG VERIFIED F/Q WORKING, NO FAULTS NOTED.

Part: ACTUATOR — MALFUNCTIONED (NLG STEERING) · airframe 34,641 hrs · 4,236 cycles

RTO/RTB DUE TO MLG STEERING WARNING. FWD TO MCO AND PLAC PER MEL 32-53-01. REPLACED LT MLG STEERING ACTUATOR PER M/M. OPS CK AND LEAK C GOOD. MCO/PLAC REMOVED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: START VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 34,009 hrs · 4,186 cycles

AFTER PUSHBACK ENG START VALVE R EICAS AND NO ENGINE ROTATION. ACTUATED R/START VALVE. CLEARED MSG OPS CHECK NORMAL.

Part: ENGINE — MAKING METAL (APU) · airframe 24,562 hrs · 3,389 cycles

APU GEN WOULD NOT COME ONLINE TS PER FIM ALL APU CHIP DETECTORS HAVE LARGE AMOUNT OF METAL REPLACED APU PER MM GEN, OPS CKS OK.

Part: TIRE — DAMAGED (NLG) · airframe 23,310 hrs · 3,267 cycles

LEFT NOSE TIRE SIDE WALL DAMAGE ON PUSH BACK. REPLACED LT NOSE WHEEL ASSY PER MM.

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 21,887 hrs · 3,109 cycles

AFTER T/O LT ENG RELATED MESSAGES, HIGH OIL PRESS EPR/N1/EGT/N3 EXCEEDANCES. AUTOTHROTTLES KICKED OFF. ENGINE RESPONDED NORMALLY. ENG CTLL/EEC C1L/ REPLACED L ENG EEC. UPDATED SOFTWARE. RAN ENG NO FAULTS NO MESSAGES.

Part: ENGINE — OIL CONSUMPTION (APU) · airframe 20,847 hrs · 2,995 cycles

APU REPLACED DUE TO HIGH OIL COMSUMPTION.

Part: OVEN — INOPERATIVE (GALLEY) · airframe 20,747 hrs · 2,983 cycles

OVEN 1 CIRCUIT BREAKER PULLED IN ASSOC WITH BURNING ELEC SMELL. ACTIVATED OVEN FWD TO MCO AND PLAC PER MEL 25-20-01G. REPLACED OVEN AND OPERATED OPS CKS OK MCO AND PLACARD REMOVED.

Part: STATUS MESSAGE — MULTIPLE FAIL (COCKPIT) · airframe 20,444 hrs · 2,949 cycles

NUMEROUS STATUS MSG AFTER ENGINE START. RETURNED TO GATE DOWN POWERED A/C AND AFTER POWER UP ALL STATUS MSGS CLEARED OK FOR SERVICE.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 18,996 hrs · 2,786 cycles

DUE TO TGT TREND SHIFTED BOROSCOPED NR 2 ENG HPC FOUND 6TH STG BLADES DAMAGED OUT OF AMM LIMITS. C/W AMM TASKS 600-804 AND 600-805 BOROSCOPE PER TABLE 305 942426. BORO INSP NR 2 ENG PER FIM 71-00-10. FOUND DAMAGE TO 6TH STG HPC BLADES OUT OF LIMITS PER 72-00-00-601. NR 2 ENG CHANGE S/N 051361 QC1321. REPLACED NR 2 ENG PER ENGINE CHANGE TRANSMITTAL 11T003 QC1440.

Part: SMOKE DETECTOR — MALADJUSTMENT (LAVATORY) · airframe 15,181 hrs · 2,334 cycles

LAV 204 SMOKE DETECTOR CHIRPS, REPLACED BATTERY.

Part: CONNECTOR — BURNED (NR 1 ENGINE) · airframe 12,368 hrs · 1,962 cycles

EICAS MESSAGE ENG FUEL FILTER L CAME ON ABOUT 2 HOURS INFLT. FOUND PIN 3 OF CONNECTOR OF DIFF PRESS SWITCH BURNT. REPLACED PIN, SWITCH AND FILTER.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 10,692 hrs · 1,678 cycles

EN ROUTE ATH CREW HEARD NOISE FROM WEATHER RADAR AREA AND LATER HAD WX SYSTEM MESSAGE. DIVERTED TO JFK. REPLACED RADAR ANTENNA AND DRIVE.