N348AN

Part: CONTROL CABLE — OUT OF ADJUST (VSV FEED BACK) · airframe 61,239 hrs · 10,280 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT ENGINE VERY SLOW TO SPOOL UP ON T/O. ALSO , AT IDLE AT ALTITUDE ON DESCENT LEAVING FL 240, RIGHT FUEL FLOW WAS 0.6 LEFT WAS 1.1. TOOK ONE AND A HALF KNOBS ON THROTTLES TO MATCH F.F. N1 44.1/34.7. MAINTENANCE ACCOMPLISHED R/H ENGINE VSV FEEDBACK CABLE ADJUSTMENT TEST IAW JOB CARD 4455. FOUND NORMAL NO ADJUSTMENTS NEEDED. ACCOMPLISHED ENGINE RUN IAW AMM 71-00-00. FOUND ALL PARAMETERS NORMAL.

Part: LATCH — UNLATCHED (PAX DOOR) · airframe 61,097 hrs · 10,253 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS FWD ENTRY DOOR WILL NOT OPEN FULLY OR COVER FOR INSIDE OF DOOR LOWER THAN NORMAL. FOUND ONE OF BUSTLE LATCH UNDONE. RE-LATCHED BUSTLE OPEN/CLOSES ELECTRICALLY NORMAL IAW AMM 52-11-00.

Part: MODULE — UNRELIABLE (FLAP/STAB) · airframe 60,984 hrs · 10,232 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO PHL ON ACCOUNT OF LEADING EDGE, FLAP AND SLAT DISAGREE. EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED FIM TASK 27-51-00-815-811 AND 809, REPLACED FLAP POSITION TRANSMITTER #1 M473 IAW AMM 27-51-45 AND THE LEFT FLAP/STABILIZER POSITION MODULE IAW AMM 27-58-01. OPS CHECK GOOD. (SEE SDR # AALA201912049038)

Part: TRANSMITTER — MALFUNCTIONED (LT WING FLAPS) · airframe 60,984 hrs · 10,232 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO PHL ON ACCOUNT OF LEADING EDGE, FLAP AND SLAT DISAGREE. EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED FIM TASK 27-51-00-815-811 AND 809, REPLACED FLAP POSITION TRANSMITTER #1 M473 IAW AMM 27-51-45 AND THE LEFT FLAP/STABILIZER POSITION MODULE IAW AMM 27-58-01. OPS CHECK GOOD. (SEE SDR # AALA201912029021)

Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 60,537 hrs · 10,126 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT MEGAPHONE WAS INOPERABLE. MAINTENANCE REPLACED MEGAPHONE PER STANDARD PRACTICES.

Part: FLASHLIGHT — NO TEST (CABIN) · airframe 60,359 hrs · 10,081 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS FIRST CLASS FLIGHT ATTENDANT SEAT LEFT HAND FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,359 hrs · 10,081 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR TIE AT BS 1562 BETWEEN S38L AND S38R. REPLACED SHEAR TIE PER EA 297934.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,359 hrs · 10,081 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME FAILSAFE CHORD FLANGE AT BS 1562 BETWEEN S38L AND S38R. REPAIRED FRAME FAILSAFE CHORD PER EA 297934.

Part: O-RING — DAMAGED (ZONE 300) · airframe 60,047 hrs · 10,021 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO PHL ON ACCOUNT OF HYDRAULIC LEAK. AFTER 2 HRS OF FLIGHT THE LEFT HYDRAULIC SYSTEM SHOWED .75 RF. WENT DOWN TO .73.. EMERGENCY DECLARED. MAINTENANCE FOUND LEAK AT VERT. STAB. HYDR. MANIFOLD. REPLACED 2 O RINGS. LEAK CHECK GOOD. SERVICED LT HYDR SYS AS REQUIRED.

Part: TRANSMITTER — FAULTY (LT WING) · airframe 58,957 hrs · 9,788 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS THAT ON BASE TO FINAL WHILE EXTENDING FLAPS, RECEIVED TRAILING EDGE FLAP ASYM MESSAGE. COMPLIED WITH QRH WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LH OUTBOARD #2 FLAP TRNASMITTOR IAW AMM 27-51-45. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,617 hrs · 9,712 cycles

FOUND THE EMERGENCY LIGHT INOPERATIVE ON THE RT CLOSET, AFT OF ROW 17. REPLACED THE LIGHT ASSY IAW AMM 33-60-98. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 58,494 hrs · 9,691 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT EMERGENCY LIGHT WOULD NOT TEST WHEN SWITCH WAS IN THE ARM POSITION. MAINTENANCE REPLACED COCKPIT EMERGENCY LIGHT EXIT SIGN ASSEMBLY PER MM 33-51-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 58,493 hrs · 9,691 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT EMERGENCY LIGHT WOULD NOT TEST WHEN SWITCH WAS IN THE ARM POSITION. MAINTENANCE REPLACED COCKPIT EMERGENCY LIGHT EXIT SIGN ASSEMBLY PER MM 33-51-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — PARTIAL DEPLOY (R1 DOOR) · airframe 58,491 hrs · 9,690 cycles

AIRCRAFT WAS GROUNDED: SLIDE PARTIALLY DEPLOYED WHEN DOOR WAS PARTIALLY OPENED. R1 DOOR WAS UNABLE TO CLOSE NORMALLY. MAINTENANCE REPLACED R1 DOOR SLIDE PER AMM 25-66-01 AND WORK CARD 12L80025001 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WINDOW — DELAMINATED (R3) · airframe 58,396 hrs · 9,665 cycles

MOISTURE INGRESS AND DELAMINATION AROUND THE COCKPIT R3 WINDOW PERIMETER. THE AIRCRAFT WAS GROUNDED. REPLACED THE WINDOW IAW AMM 56-11-10.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 58,294 hrs · 9,650 cycles

FLASHLIGHT LOCATED AT THE L4 DOOR SEAL WAS BROKEN. MAINTENANCE REPLACED THE SEAL AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: EXHAUST VALVE — FAULTY (CABIN PRESSURE) · airframe 57,821 hrs · 9,540 cycles

AIRCRAFT WAS GROUNDED. AIRPLANE WOULD NOT PRESSURIZE. A/C RETURNED TO MIA ON ACCOUNT OF A PRESSURIZATION ISSUE. AN EMERGENCY WAS DECLARED, FLIGHT LANDED OVERWEIGHT AND WITHOUT INCIDENT. REPLACED ELECTRONIC EQUIPMENT OVERBOARD EXHAUST VALVE PER AMM 21-58-05. OPERATIONS AND LEAK CHECK OK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 57,672 hrs · 9,511 cycles

MID GALLEY FLIGHT ATTENDANT FLASHLIGHT RIGHT SIDE INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-25-00.

Part: SQUIB — BLOWN (RIGHT) · airframe 56,216 hrs · 9,244 cycles

WHILE DEACTIVATING THE OVERWING ESCAPE SLIDE SYSTEM, FOUND THE RIGHT OVERRIDE SPOILER BLOWN DOWN, ACTUATOR SQUIB ASSEMBLY PINS BENT. REPLACED THE SQUIB ASSEMBLY IAW MM 25-65-19. AIRCRAFT OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,424 hrs · 9,072 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT SIDE EMERGENCY SEAT LIGHTS FROM SEAT 5J TO SEAT 23HJ FAILED 10 MINUTE TEST. MAINTENANCE REPLACED BATTERY (M1209) AT STA873 AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER MM 33-51-07.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,424 hrs · 9,072 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. LEFT EMERGENCY OVERHEAD LIGHTS FROM SEAT 23AB TO ROW 34AB, FAILED 10 MINUTE TEST. REPLACED BATTERY AT STATION 988 AND PERFORMED OPERATIONS CHECK PER AMM 33-51-07. OPERATIONS CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,424 hrs · 9,072 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. RIGHT EMERGENCY CEILING LIGHTS ARE INOPERATIVE FROM ROW 17HJ TO ROW 32HJ AND EPL ON SEATS 21HJ TO 23HJ. REPLACED BATTERY AT STATION 1010. OPERATIONS CHECK GOOD PER AMM 33-51-00.

Part: WINDOW — FAILED (COCKPIT) · airframe 55,106 hrs · 9,016 cycles

AT FL 340, TWO HOURS INTO THE FLIGHT, LEFT FWD WINDOW EICAS MESSAGE. WINDOW ARCHED AND OUTER PANE COMPLETELY CRACKED, INNER PANE OK. REMOVED AND REPLACED THE LT FWD WINDOW IAW WC 56-94-01.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 54,285 hrs · 8,861 cycles

AIRCRAFT WAS NOT GROUNDED. PER FAA FINDINGS, FLIGHT ATTENDANT STATION MID RIGHT HAND AISLE OPPOSITE LAV FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERY PACK IN FLASHLIGHT ASSEMBLY IAW MM 25-60-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 53,825 hrs · 8,774 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE L1 JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.

Part: IDG — FAILED (RT ENGINE) · airframe 53,588 hrs · 8,730 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. ORD-DUB FLIGHT RETURNED TO ORD ACCOUNT RIGHT ENGINE INTEGRATED DRIVE GENERATOR WARNING INDICATION. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED IDG PER AMM 24-11-01. OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,702 hrs · 8,564 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 29H IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 52,427 hrs · 8,513 cycles

DURING TEST, LEFT AFT GROUND SCAN EMERGENCY LIGHT CHARGER FAILED. REPLACED EMERGENCY LIGHT POWER SUPPLY MODULE (M00738) IAW AMM 33-51-00 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: FILTER — CONTAMINATED (ZONE 400) · airframe 49,376 hrs · 7,981 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RECEIVED LT FUEL FILTER EICAS MSG. FOUND LT ENG FUEL FILTER CONTAMINATED. R & R FILTER IAW AMM 73-11-02. ACCOMPLISHED TAKEOFF POWER ENG RUN WITH NO FURTHER DISCREPANCIES NOTED.

Part: PIN — MISSING (NLG) · airframe 46,746 hrs · 7,532 cycles

DURING CLIMB CONFIGURATION WARNING ALERT WAS RECEIVED DURING FLAP RETRACTION. EMERGENCY DECLARED, LANDED WITHOUT EVENT. FOUND NOSE GEAR CENTERING PINS MISSING UPPER CAM. INSTALLED MISSING PINS & REPACKED THE NOSE STRUCT IAW CARD 776A. PERFORMED OPERATIONAL TEST OF NLG EXTENSION & RETRACTION SYS IAW AMM 32-34-00-715. SYS CHECKED NORMAL.

Part: CIRCUIT CARD — FAULTY (ZONE 100) · airframe 46,597 hrs · 7,508 cycles

AIR INTERRUPT, DURING CLIMB AT GEAR RETRACTION NOSE WHEELS SPUN MUCH LONGER THAN NORMAL WITH EXCESSIVE AIRFRAME VIBRATION. AS FLAPS RETRACTED TO ZERO A CONFIGURATION WARNING OCCURRED. BOTH AURAL & RED LIGHTS. FOUND EXCESSIVE PLAY IN NLG LT TIRE. R & R BOTH NOSE WHEELS IAW AMM 32-45-02 & CARD 32-96-51. CONFIGURATION FAULT REPEATED ON TEST FLIGHT. R & R TAKEOFF & LANDING CONFIGURATION CARD IAW AMM 31-51-04. SYS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,570 hrs · 7,501 cycles

CABIN FLOORBEAM UPPER CHORD AT FS 325 IS CORRODED BETWEEN RBL 60 & 85. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1 FIGURE 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,570 hrs · 7,501 cycles

CABIN FLOORBEAM UPPER CHORD AT FS 287 IS CORRODED BETWEEN RBL 58 & 82. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1 FIGURE 301.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,570 hrs · 7,501 cycles

CABIN FLOORBEAM AT FUSELAGE 303 UPPER CHORD IS CORRODED BETWEEN RBL 53 & RBL 85. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1 FIGURE 201.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,570 hrs · 7,501 cycles

R1 DOOR LOWER SILL UPPER SURFACE PLATE ASSEMBLY UNDER AFT GIRT BAR FITTING CORRODED. R & R PLATE ASSEMBLY IAW SRM 51-40-02-0G.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,570 hrs · 7,501 cycles

GUSSET CORRODED AT RBL 88.5 STATION 342. R & R GUSSET IAW SRM 51-40-02-0G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,570 hrs · 7,501 cycles

UPPER CABIN SEAT TRACK 10 IS CORRODED AT RBL 88.5 & FS 345. R & R NR 10 SEAT TRACK IAW SRM 51-40-02-0G.

Part: INTERCOSTAL — DEFORMED (FUSELAGE) · airframe 46,570 hrs · 7,501 cycles

AFT CARGO COMPARTMENT CEILING ALONG ENTRANCE AREA BETWEEN BS 1329 & 1351, RBL 81 INTERCOSTAL HAS DEFORMATION. R & R INTERCOSTAL IAW SRM 51-40-02-OG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,297 hrs · 7,459 cycles

SEAT 17H EMER LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-10. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,060 hrs · 7,422 cycles

RIGHT FUSELAGE EMER GND ILLUMINATION LIGHT FWD OF AFT CARGO IS INOPERATIVE. RELAMPED RT FUSELAGE ILLUMINATION LIGHT FWD OF AFT CARGO IAW AMM 33-51-03. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,060 hrs · 7,422 cycles

L4 DOOR EXTERNAL EMER LIGHT IS INOPERATIVE. RELAMPED L4 DOOR EXTERNAL EMER LIGHT IAW AMM 33-51-03. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,052 hrs · 7,274 cycles

ROW 23B EMER LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-10. SYS CHECKED NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,052 hrs · 7,274 cycles

EMERGENCY LIGHT LENS MISSING, FWD SEAT 2A ON COMPARTMENT WALL. REPLACED THE MISSING LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,052 hrs · 7,274 cycles

EMERGENCY LIGHT LENS MISSING, FWD OF SEAT 2J ON COMPARTMENT WALL. REPLACED THE LENS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,052 hrs · 7,274 cycles

LEFT SIDE FUSELAGE EMER ESCAPE LIGHT AFT OF WING BODY FAIRING INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,052 hrs · 7,274 cycles

RIGHT FUSELAGE EMER ESCAPE LIGHT AFT OF WING BODY FAIRING INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,052 hrs · 7,274 cycles

L4 DOOR EXTERNAL EMER LIGHT INOPERATIVE. RELAMPED L4 EXTERIOR EMER LIGHT IAW AMM 33-51-03.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,926 hrs · 7,253 cycles

EXTERIOR EMER LIGHT R1 DOOR IS INOPERATIVE. REPLACED LAMP IAW 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,645 hrs · 7,217 cycles

RIGHT NR 1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,235 hrs · 7,161 cycles

LEFT NR 2 DOOR EXTERNAL EMER LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: ACTUATOR — LEAKING (NR 5 SPOILER) · airframe 44,080 hrs · 7,141 cycles

LOSS OF CTR HYD QTY. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 5 SPOILER ACTUATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,988 hrs · 7,121 cycles

OVERHEAD EMER LIGHT AT 40JH INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMER LIGHT AT 40HJ. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,988 hrs · 7,121 cycles

LEFT NR 4 EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 43,783 hrs · 7,093 cycles

EMERGENCY LIGHT AT SEAT 5B INOPERATIVE. RESEATED CONNECTOR FOR EMER LIGHT AT SEAT 5B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 43,783 hrs · 7,093 cycles

RIGHT AFT OVERWING EMER EXIT SIGN INOPERATIVE. REPLACED LAMPS FOR RT AFT OVERWING EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,783 hrs · 7,093 cycles

EMERGENCY LIGHT AT SEAT 41H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 41H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,783 hrs · 7,093 cycles

SEAT 32G OVERHEAD AISLE EMER LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 32G OVERHEAD AISLE EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 43,783 hrs · 7,093 cycles

EMERGENCY EXIT SIGN AT LT NR 1 DOOR, LOWER FWD LAMPS INOPERATIVE. REPLACED LOWER FWD LAMPS FOR EMER EXIT SIGN AT LT NR 1 DOOR. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,783 hrs · 7,093 cycles

EMERGENCY LIGHT ACROSS FROM M2 LAVATORY INOPERATIVE. REPLACED LAMP FOR EMER LIGHT ACROSS FROM M2 LAVATORY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,308 hrs · 7,023 cycles

M2 LAVATORY LOWER EMER LIGHT INOPERATIVE. REPLACED LAMP FOR M2 LAVATORY LOWER EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,308 hrs · 7,023 cycles

LEFT NR 1 DOOR LOWER INTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR LOWER INTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 43,308 hrs · 7,023 cycles

RIGHT FWD OVERWING EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT FWD OVERWING EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,541 hrs · 6,719 cycles

LT AFT EMERGENCY EXIT SIGNS & CEILING LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M739.

Part: SIGN — BROKEN (CABIN) · airframe 41,541 hrs · 6,719 cycles

RT NR 2 DOOR LT HAND EMERGENCY EXIT IDENTIFIER SIGN BROKEN. R & R EXIT SIGN, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,541 hrs · 6,719 cycles

LT HAND EMERGENCY EXIT EXTERIOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK M738, OPERATIONS CHECKED NORMAL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,440 hrs · 6,701 cycles

SEAT 5AB EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 5AB EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,440 hrs · 6,701 cycles

RT SIDE OF FS AFT OF FLAP EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT SIDE OF FS OF AFT FLAP EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: FMC — INOPERATIVE (COCKPIT) · airframe 40,146 hrs · 6,487 cycles

RT FLIGHT MANAGEMENT COMPUTER FAILED. REPLACED RT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,750 hrs · 6,266 cycles

ESCAPE PATH LIGHT AT M1 LAVATORY CEILING ENTRY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT M1 LAVATORY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 38,750 hrs · 6,266 cycles

RIGHT NUMBER 2 DOOR EMEGRENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY SLIDE LIGHT. OPS CHECK NORMAL

Part: FAN — MALFUNCTIONED (CABIN) · airframe 38,335 hrs · 6,190 cycles

HNL INFLIGHT OGG-DFW. CREW REPORTED ELECTRICAL ODOR IN MID GALLEY. EMERGENCY DECLARED FLIGHT DIVERTED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARD RIGHT RECIRCULATION FAN PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED RIGHT RECIRCULATION FAN AT MIA ON 01/05/2013. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,913 hrs · 5,836 cycles

EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 2 DOOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,913 hrs · 5,836 cycles

EMERGENCY LIGHT AT SEAT 11B DIM. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11B. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 34,934 hrs · 5,662 cycles

OVERHEAD EMERGENCY LIGHT AT AISLE 5B INOPERATIVE. SECURED LOOSE CONNECTOR ABOVE SEAT 5B. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 34,934 hrs · 5,662 cycles

OVERHEAD EMERGENCY LIGHT AT 3B INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 3B. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,934 hrs · 5,662 cycles

AFT LOWER FUSELAGE RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE RIGHT. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT LOWER FUSELAGE EXTERIOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,934 hrs · 5,662 cycles

FORWARD LOWER FUSELAGE LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD LOWER FUSELAGE LEFT EXTERIOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,523 hrs · 5,588 cycles

RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CONTROL VALVE — FAILED (AC BAY) · airframe 34,272 hrs · 5,540 cycles

MIA - CREW REPORTED LEFT PACK FAILED DURING CRUISE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT TEMPERATURE CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RELAY — INOPERATIVE (ZONE 200) · airframe 32,880 hrs · 5,329 cycles

LAX - INFLIGHT DFW-OGG. CREW REPORTED BATTERY BUSS CIRCUIT BREAKER POPPED OUT. NO EICAS OR STATUS MESSAGES. FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. REPLACED C898 BATTERY BUSS POWER CIRCUIT BREAKER AND MAIN BATTERY RELAY K104. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PSEU — INOPERATIVE (LE SLAT) · airframe 32,502 hrs · 5,272 cycles

DFW - CREW REPORTED LEADING EDGE SLAT ASYMMETRY INDICATION. FLIGHT EXECUTED MISSED APPROACH. EMERGENCY DECLARED FLIGHT LANDED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PROXIMITY SWITCH ELECTRINIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,659 hrs · 5,143 cycles

SEAT 40HJ EMERGENCY LIGHTS INOPERATIVE. RE-SECURED LOOSE CONNECTOR FOR SEAT 40HJ EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,659 hrs · 5,143 cycles

SEAT 41HJ EMERGENCY LIGHTS INOPERATIVE. RE-SECURED LOOSE CONNECTOR FOR SEAT 41HJ EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 31,604 hrs · 5,134 cycles

MIA - CREW REPORTED AFTER TAKEOFF RIGHT ENGINE COMPRESSOR STALLED. EXHAUST GAS TEMPERATURE IN RED, AIRCRAFT VIBRATIONS AND FLAMES NOTED OUT OF RIGHT ENGINE. RETARDED RIGHT THROTTLE TO KEEP EGT IN LIMITS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT MIA ON 06/02/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — OUT OF POSITION (AC BAY) · airframe 30,946 hrs · 5,035 cycles

SCL - CREW REPORTED RIGHT PACK FAILED WITH LEFT PACK ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED SCL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND AIR LEAK TO LEFT DUCT ASSEMBLY TURBINE INLET. REPOSITIONED CLAMP. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: INDICATOR — FAILED (COCKPIT) · airframe 29,370 hrs · 4,771 cycles

MAO - INFLIGHT GRU-MIA. CREW REPORTED INTEGRATED STANDBY FLIGHT DISPLAY FAILED AND CIRCUIT BREAKER POPPED IN FLIGHT. FLIGHT DIVERTED MAO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED INTEGRATED STANDBY/AIRSPEED ALTIMETER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,251 hrs · 4,548 cycles

EMERGENCY LIGHT LEFT SIDE EXTERIOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,251 hrs · 4,548 cycles

EMERGENCY LIGHT RIGHT SIDE EXTERIOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,595 hrs · 4,429 cycles

RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LAMP INOPERATIVE. REPLACED LAMP FOR RIGHT AFT SERVICE, DOOR EXTERIOR EMERGENCY EXIT. OPS CHECKS NORMAL.

Part: SIGN — LOOSE (CABIN) · airframe 25,344 hrs · 4,056 cycles

EMERGENCY EXIT SIGN ABOVE ROW 20H NOT SECURE. SECURED EMERGENCY EXIT SIGN AS REQUIRED.

Part: COMPUTER — FAILED (LT ADC) · airframe 24,194 hrs · 3,830 cycles

CAPT ALTIMETER INOPERATIVE. CLIMBING THRU 3000 FEET RECEIVED ORANGE OFF FLAG. WORKS OK IN ALTERNATE AIR DATA. REPLACED LEFT AIR DATA COMPUTER PER MM 34-12-01-4, ALL REQD CHECKS OK. REPLACED CAPTAINS ALTIMETER PER MM 34-13-01-4. ALL REQD CHECKS OK.

Part: FUEL FILTER — INOPERATIVE (RIGHT) · airframe 23,047 hrs · 3,639 cycles

ORD - CREW REPORTED A FEW MINUTES AFTER TAKEOFF RIGHT FUEL FILTER MESSAGE CAME ON THEN WENT OUT A FEW TIMES. EMERGENCY DECLARED RETURNED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH LEFT AND RIGHT ENGINE FUEL SYSTEM FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · 20,945 cycles

MIA EMERGENCY LIGHT AT SEAT 4H AFT POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 4H AFT POSITION. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 29H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,534 hrs

SFO - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — MISSING (CABIN)

DFW - EMERGENCY EXIT PLACARD AT LEFT NUMBER FOUR DOOR MISSING. REPLACED PLACARD FOR EMERGENCY EXIT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT RIGHT AFT OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

SFO - EMERGENCY LIGHT EXIT SIGN AT RIGHT NUMBER ONE DOOR HAS BROKEN BASE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR EXIT SIGN AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

SFO RIGHT AFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

SFO - FLT 1994 - EMERGENCY EXIT LIGHTS INOPERATIVE AT LEFT FUSELAGE. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ALTIMETER — FAILED (COCKPIT)

CAPTAIN ALTIMETER IS STUCK AT 100, AFTER TAKEOFF FLAG WAS DISPLAYED OFF FLAGG NOT DISPLAYED ON GROUND. REPLACED CAPTAINS BARO ALTIMETER PER MM 34-13-01, SYSTEM CHECKS NORMAL. (M)