N253AY

Part: FAN — INOPERATIVE (CABIN) · airframe 94,697 hrs · 17,841 cycles

LEFT RECIRCULATION FAN, EICAS C, LIGHT ELEC SMELL IN COCKPIT & CABIN, ENDED WHEN RECYCLING FAILED. R & R FAN CABIN AIR CIRCULATION. OPS CHECKED GOOD.

Part: CHARGER — MALFUNCTIONED (CABIN) · airframe 94,464 hrs · 17,801 cycles

PHL THREE AFT LT EMERGENCY GND ILLUMINATION LIGHTS DID NOT COME ON DURING TEST. R & R EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER AT M738 POSITION. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 94,245 hrs · 17,753 cycles

EMERGENCY FLASHLIGHT AT AFT RT F/A POS INOPERATIVE. R & R BATTERY. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 94,108 hrs · 17,718 cycles

EMERGENCY LENS MISSING AT MID CABIN CEILING LIGHT. REPLACED MISSING EMERGENCY LIGHT LENS.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 93,760 hrs · 17,668 cycles

AFT LT T/E INBD FLAP ASSY SPLIT AND DELAMINATED BETWEEN WBL 97.9566 TO WBL 289.45. REPLACED LT T/E INBD FLAP ASSY IAW AMM 27-51-06-022-035 & 27-51-06-422-059.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 93,614 hrs · 17,647 cycles

FLASHLIGHT UNDER JUMPSEAT 1L IS INOP. REPLACED FLASHLIGHT BATTERY. CHECKS OK.

Part: COVER — FAULTY (L1 DOOR SLIDE) · airframe 92,542 hrs · 17,487 cycles

L1 DOOR SLIDE COVER LOOSE. DOOR ALSO DOES NOT OPEN FULLY. REMOVED AND INSTALLED L1 DOOR SLIDE.

Part: SHUTOFF VALVE — FAULTY (RT ENGINE) · airframe 91,194 hrs · 17,207 cycles

FLT 805 EN ROUTE. AFTER STARTING THE RIGHT ENGINE & IT WAS STABILIZED BOTH THE ENGINE VALVE & SPAR VALVE LIGHT ILLUMINATED & THE RIGHT ENGINE SHUTDOWN. REMOVED AND REPLACED RT ENGINE FUEL SHUT-OFF VALVE. RAN NR 2 ENGINE. OPS CHECKED NORMAL.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 91,174 hrs · 17,201 cycles

C3 CHECK - DELAMINATION ON NR 1 SLAT UPPER SURFACE 5 INCHES FROM INBOARD EDGE & 2 INCHES FROM TRAILING EDGE. REPAIRED NR 1 SLAT UPPER SURFACE IAW EA 104574.

Part: FLAP — DELAMINATED (RT WING) · airframe 90,727 hrs · 17,098 cycles

RON VISIT - 19 INCH BY 4 INCH WIDE AREA OF DELAMINATION ON LEADING EDGE OF RIGHT OUTBOARD FLAP AT WS 746. REPLACED RIGHT OUTBOARD FLAP LEADING EDGE PANEL IAW B767 AMM 27-51-20-401 & JOB CARD 12L66027001.

Part: DOOR — NOT CLOSED (OVERWING EXIT) · airframe 89,613 hrs · 16,903 cycles

CLT - FOUND RT OVERWING DOOR AJAR. MAINTENANCE REPLACED THE RIGHT SIDE OFF WING SLIDE COMPARTMENT DOOR FORWARD DOOR OPENING ACTUATOR. VENDOR SHOP FINDINGS: INSPECTED AND TESTED UNIT, NO FAULTS FOUND.

Part: DOOR — NOT CLOSED (OVERWING EXIT) · airframe 89,613 hrs · 16,903 cycles

CLT - FOUND RIGHT OVERWING DOOR AJAR. MAINTENANCE REPLACED THE RIGHT SIDE OFF WING SLIDE COMPARTMENT DOOR AFT DOOR OPENING ACTUATOR. VENDOR SHOP FINDINGS: INSPECTED AND TESTED ACTUATOR, FOUND OK.

Part: DOOR — NOT CLOSED (OVERWING EXIT) · airframe 89,613 hrs · 16,903 cycles

CLT - FOUND RT OVERWING DOOR AJAR. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY ESCAPE SLIDE. VENDOR SHOP FINDINGS: INSPECTED & TESTED UNIT WITH NO FAULTS FOUND.

Part: LAMP SOCKET — BROKEN (COCKPIT) · airframe 89,503 hrs · 16,884 cycles

CLT - EMERGENCY LIGHT SOCKET FELL OUT OF OVERHEAD PANEL IN COCKPIT. REPLACED SOCKET, OPS NORMAL.

Part: COVER — OUT OF ADJUST (ZONE 200) · airframe 87,748 hrs · 16,626 cycles

F/A REPORTS AT AFT FLIGHT ATTENDANT SEAT UNABLE TO ACCESS FLASHLIGHT BECAUSE COVER WILL NOT RELEASE. ADJUSTED DOOR, DOOR OPENS ALRIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 87,440 hrs · 16,562 cycles

CLT - EMERGENCY FLASHLIGHT CHARGE LIGHT OUT AT FWD CTR STATION. REPLACED BATTERY. LIGHT CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT)

PHL FLT 751 EN ROUTE BRU TO PHL. DIRTY SOCKS SMELL NOTED IN COCKPIT AND CABIN 5 MINUTES BEFORE TOUCHDOWN, WHICH LASTED APPROXIMATELY 2 MINUTES, THEN DISSIPATED. MAINTENANCE REPLACED THE RIGHT ENGINE ASSEMBLY. HPC STAGE 5 BORESCOPE - ORGANIC DEPOSIT FOUND, POSSIBLE ODOR CONTRIBUTOR. OTHERWISE, NO FAULTS FOUND.

Part: FASTENER — SHEARED (NR 1 PYLON) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - NR 1 PYLON INBOARD MIDSPAR FITTING TENSION FASTENER SHEARED. REPLACED NR 1 PYLON INBOARD MIDSPAR FITTING TENSION FASTENER IAW EA 103598.

Part: RESERVOIR — LEAKING (THRUST REVERSER)

FLT 1250, THE CREW REPORTED AN ODOR IN THE CABIN DURING DESCENT. MAINTENANCE FOUND THE RIGHT ENGINE THRUST REVERSER RESERVOIR ASSEMBLY TOP LEAKING OIL ONTO THE RT ENGINE. REPLACED THE RT ENGINE THRUST REVERSER AUX RESERVOIR ASSEMBLY.

Part: CONVERTER — MALFUNCTIONED (ENTERTAIN SYS) · airframe 87,139 hrs · 16,501 cycles

BRU FLT 750 EN ROUTE PHL TO BRU. VIDEO EQUIPMENT IN MOST FORWRD COMPARTMENT (ACROSS FROM FWD LAV) HAD ELECTRICAL ODOR. ALL EQUIPMENT TURNED OFF. REMOVED AND REPLACED VIDEO SYS CONTROL UNIT. OPS GOOD AT THIS TIME. UNABLE TO CONFIRM REPORTED SNAG. OPENED UNIT AND INSPECTED ALL PC BOARDS, ALL CONNECTORS, FOR ELECTRICAL ODORS OR TRACE OF BURNS. NIL FOUND. REPLACED DC CONVERTER. REASON - DEFECTIVE.

Part: SIGN — BROKEN (CABIN) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - LEFT LOWER OVERWING EMERGENCY EXIT SIGN BROKEN. REPLACED LEFT LOWER OVERWING EMERGENCY EXIT SIGN IAW B767 AMM 33-51-09-022-041 AND 33-51-09-422-042.

Part: LENS — CRACKED (CABIN) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - CRACKED LEFT UPPER EMERGENCY EXIT LIGHT LENS. REPLACED LEFT UPPER EMERGENCY EXIT LIGHT LENS IAW B767 AMM 33-51-01-962-01.

Part: CABLE — BURNED (APU) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - APU BATTERY DC CABLE BURNT AT ATTACH POINT. REPLACED APU GROUND BRACKET ASSEMBLY IAW B767 SRM 51-90-02-06 PAR 4 PG8.

Part: LENS — CRACKED (CABIN) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - L2 DOOR UPPER EXIT LIGHT LENS IS CRACKED. REPLACED L2 DOOR UPPER EXIT LIGHT LENS IAW B767 AMM 33-51-01-962-001.

Part: LENS — CRACKED (CABIN) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - AFT LEFT & RIGHT CEILING EXIT LIGHT LENSES ARE CRACKED. REPLACED LEFT & RIGHT CEILING EXIT LIGHT LENSES IAW B767 AMM 33-51-09-022-041 & 33-51-09-422-042.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - DISBONDED ON THE NR 4 SLAT TRAILING EDGE WEDGE BETWEEN OSS575.275 TO OSS586.625. REPAIRED NR 4 SLAT IAW B767 SRM 51-70-10-2R-4, REPAIR 4 FIG 202.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - DELAMINATION ON SLAT 11 TRAILING EDGE WEDGE BETWEEN OSS982 TO OSS984. REPAIRED SLAT 11 IAW B767-200 SRM 51-70-10-2R4, REPAIR 4, FIGURE 202.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - CRACK ON STIFFENER BETWEEN BS 966 TO BS 977 LBL 97.42. REPLACED STIFFENER BETWEEN BS 966 TO BS 977 LBL 97.42 IAW B767-200 SRM 51-40-05-0G FIGURE 4 AND BOEING DRAWING 145T8752.

Part: FLAP — DEBONDED (RT WING) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - DISBONDED RIGHT WING OUTBOARD FLAP TRAILING EDGE BETWEEN WS 309.125 TO WS 311.625, 64 INCHES FROM OUTBOARD EDGE. REPAIRED RIGHT WING OUTBOARD FLAP TRAILING EDGE BETWEEN WS 309.125 TO WS 311.625, 64 INCHES FROM OUTBOARD EDGE IAW B767 SRM 51-70-05-0G PARAGRAPH A FIGURE 5.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - DISBONDED ON THE NR 11 SLAT TRAILING EDGE WEDGE 28 INCHES FROM INBOARD EDGE BETWEEN OSS857.74 TO OSS865.74. REPAIRED NR 11 SLAT IAW B767 SRM 51-70-10-2R, REPAIR 4, FIG 201.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 87,034 hrs · 16,479 cycles

C2 CHECK - AREA OF DISBOND ON NR 12 SLAT TRAILING EDGE WEDGE BETWEEN OSS984.73 TO OSS989.73. REPAIRED NR 12 SLAT TRAILING EDGE WEDGE BETWEEN OSS984.73 TO OSS989.73 IAW B767 SRM 51-70-2R-4 REPAIR 4 FIG 202.

Part: LENS — OUT OF POSITION (CABIN) · airframe 86,533 hrs · 16,394 cycles

FRA - LENS FELL OFF OF READING LIGHT LAMP AT ROW 22AB. FOUND EMER LIGHT AT 22AB COVER MISSING. RE-INSTALLED COVER. LIGHT OPS OK.

Part: SERVICE CART — OVERHEATED (GALLEY) · airframe 85,624 hrs · 16,247 cycles

CLT - HEATED CART AT AFT 2 GALLEY CART DEFECTIVE - ELECTRIC BURNING SMELL. PLUG TOO HOT TO TOUCH. ELECTED TO PULL BREAKER AND SHUT OFF AT SWITCH. MAINTENANCE COULD NOT DUPLICATE DEFECTIVE CART. NOTIFIED CATERING TO CHANGE OUT AFT 2 GALLEY CARTS. A/C OK FOR SERVICE (A/C LEFT SIDE CARTS).

Part: FAN — FAULTY (CABIN) · airframe 85,487 hrs · 16,224 cycles

GLA FLT 768 EN ROUTE PHL TO GLA. AT CRUISE GOT A STRONG ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN (SMELL ONLY, NO SMOKE) DID SMOKE AND FUMES QRH, SMELL DISSIPATED IN BOTH COCKPIT AND CABIN. TROUBLESHOT PER 767 CABIN AIR QUALITY PROCEDURE. NIL RELEVANT SMELLS APPARENT. AIRCRAFT RESTRICTED FROM ETOPS FLIGHT. SUBSEQUENT TO THIS ACTION, WHILE AT THE GATE, A STRONG ELECTRICAL BURNING SMELL WAS NOTICED IN COCKPIT & CABIN, AFTER WINDOW HEAT AND CARGO HEAT WAS TURNED ON, WITH BOTH RECIRC FAN SWITCHES ON. RIGHT RECIRC FAN 'INOP' LIGHT / ANNUNCIATED. THE RIGHT RECIRCULATION FAN WAS PLACED ON MEL. AFTERWARDS, AFTER PUSH BACK, THE FLIGHT ATTENDANTS COMPLAINED OF FUMES IN THE CABIN. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE RIGHT RECIRCULATION FAN AND FILTER. RAN AIRCRAFT ENGINES AT IDLE WITH AIRCRAFT IN FLIGHT CONFIGURATION. NIL RELEVANT SMELLS APPARENT.

Part: FAN — INOPERATIVE (CABIN) · airframe 85,135 hrs · 16,166 cycles

ELECTRICAL SMOKE NOTED FOLLOWED (30 SECS APPROX) EICAS MSGR RECIRC FAN. SMOKE SLOWLY DISSIPATED. MAINTENANCE REMOVED AND REPLACED RIGHT RECIRC FAN AND HEPA FILTER.

Part: TRIM PANEL — LOOSE (CABIN DOOR)

PHL - RIGHT FORWARD DOOR DIFFICULT TO CLOSE. MAINTENANCE FOUND UPPER DOOR LINING PANEL WAS LOOSE AND FALLING OUT OF TRACK. SECURED PANEL. OPS CHECKS GOOD. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

GIG - THE FLASHLIGHT AT FLIGHT ATTENDANT POSITION L2 WAS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY.

Part: MODULATING VALVE — FAULTY (AC BAY)

CLT - FLT 1106 EN ROUTE CLT TO PHF. THE AFT CABIN TEMP AT 17,000 FEET BECAME UNBEARABLE. HOT AIR WAS REPORTED TO BE COMING OUT INTO THE REAR CABIN. THE FLIGHT CREW DECLARED AN EMERGENCY, AND RETURNED TO THE FIELD IN CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE TRIM AIR MODULATING VALVE. ACTUATOR BINDING, SWITCHES OUT OF SPEC, RESISTOR ERRATIC.

Part: WIRE — LOOSE (CABIN)

ZRH - FOUND THE LEFT EMERGENCY DOOR WITH BOTH SIGNS NOT ILLUMINATED. REPAIRED LOOSE SUPPLY WIRE TO EMERGENCY LIGHT ASSEMBLY.

Part: POWER SUPPLY — FAULTY (RIGHT)

CLT - THE RIGHT SPOILER SQUIB WILL NOT TEST IN POS 2. REMOVED AND REPLACED THE RIGHT OFF-WING BATTERY AND POWER SUPPLY.

Part: MEGAPHONE — INOPERATIVE (CABIN)

PHL - AFT MEGAPHONE INOP. REPLACED AFT MEGAPHONE WITH NEW.

Part: SWITCH — FAULTY (CABIN)

CLT - THE EMERGENCY LIGHTS ON WITH SWITCH IN OFF POSITION. REPLACED FORWARD ATTENDANT PANEL EMERGENCY LIGHT SWITCH S1.

Part: HSI — ARCED (COCKPIT)

CLT FLT 968 SJU - CLT. THE FIRST OFFICER'S LOWER CRT (MAP SCREEN) HAS BRIGHT LIGHT SPIKES WITH INTERMITTENT INTERNAL ARCING. THE CREW SELECTED EFI, BUT THE PROBLEM PERSISTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT EHSI.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT REQUIRES A NEW BATTERY. MAINTENANCE REPLACED THE BATTERY FOR THE REAR FACING, AIRCRAFT LEFT AISLE, AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK CROWN & INBOARD FLANGE AT BS 347, LBL 54.75. REPAIRED SEAT TRACK AT BS 347, LBL 54.75 IAW B767 SRM 51-10-02.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - EEL - FORWARD FLIGHT ATTENDANT POSITION EMERGENCY FLASHLIGHT INOP. REPLACED FORWARD FLIGHT ATTENDANT POSITION EMERGENCY FLASHLIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - EEL - EMERGENCY CEILING LIGHT WIRE BROKEN AT SEAT ROW 25AB. REPAIRED BROKEN WIRE IAW B757 SWPM 20-30-12.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - EEL - EMERGENCY CEILING LIGHT BATTERY AT SEAT 29G IS INOP. REPLACED EMERGENCY LIGHT BATTERY IAW B767 AMM 33-51-07.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - EEL - BATTERY PACK ASSEMBLY UNDER THE FORWARD ATTENDANT SEAT INOP. REPLACED M1206 EMERGENCY LIGHT POWER SUPPLY FUSE IAW B767 WDM 33-51-21 & AMM 33-51-07.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - MAJOR REPAIR - FLOOR SUPPORT ANGLES CRACKED AT BS 246, LBL 7 TO RBL 19 (8EA). REPLACED (8EA) FLOOR SUPPORT ANGLES AT BS 246, LBL 7 TO RBL 19 IAW B767 SRM 51-70-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM UPPER CHORD AT BS 1480, LBL 43 TO LBL 27. REPAIRED FLOORBEAM UPPER CHORD AT BS 1480, LBL 43 TO LBL 27 IAW B767 SRM 51-20-01 & 53-00-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,746 hrs · 14,364 cycles

BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT BS 325, RBL 14 THRU RBL 20. REPAIRED FLOORBEAM AT BS 325, RBL 14 THRU RBL 20 IAW B767 SRM 53-00-51 & 51-40-02.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - MAJOR REPAIR - CABIN FLOORBEAM SUPPORT ANGLE IS CRACKED AT BS 246, LBL 36. REPAIRED FLOORBEAM SUPPORT ANGLE IS AT BS 246, LBL 36 IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,746 hrs · 24,894 cycles

BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON CREASE BEAM AT BS 858, RBL 88, WL 200. REPLACED CREASE BEAM AT BS 858, RBL 88, WL 200 IAW B767 SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - MAJOR REPAIR - FLOORBEAM SUPPORT ANGLE CRACKED AT BS 287, LBL 82. REPAIRED FLOORBEAM SUPPORT ANGLE AT BS 287, LBL 82 IAW B767 SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 75,746 hrs · 14,364 cycles

BFM - C4 - MAJOR REPAIR - CABIN FLOOR SUPPORT INBOARD ANGLE IS CRACKED IN HALF AT BS 303, RBL 54.75. REPAIRED CABIN FLOOR SUPPORT INBOARD ANGLE AT BS 303, RBL 54.75 IAW B737 SRM 51-40-02 & 51-21-01.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FLASHLIGHT AT D POSITION WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AT D POSITION. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (L/E SLAT)

MAD - FLT 730 PHL TO MAD. DURING APPROACH, THE FLAPS AUTOMATICALLY LOCKED AT 20 DEGREES DUE TO A LEADING EDGE SLAT ASYMMETRY WARNING. THE CREW DECLARED AN EMERGENCY, ACCOMPLISHED QRH PROCEDURES, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A BITE CHECK OF THE FSEU, AND OPERATED THE SLATS/FLAPS OVER A FULL RANGE. NO DEFECTS WERE NOTED. ALSO, THE PHYSICAL INSPECTION OF THE SLATS IN THE DEPLOYED POSITION REVEALED NO DEFECTS. OK FOR SERVICE.

Part: WEDGE — DELAMINATED (ZONE 500) · airframe 72,678 hrs · 13,907 cycles

BFM - MAJOR REPAIR - C3 CHECK, LEFT WING NR 2 SLAT WEDGE DELAMINATED, WS 852.9 AND WS 879.2. REPAIRED LEFT WING NR 2 SLAT WEDGE, WS 852.9 AND WS 879.2 IAW B767 SRM 57-43-02.

Part: FMC — FAILED (LEFT) · airframe 71,891 hrs · 13,764 cycles

FLT 798 PHL - AMS RETF - CREW REPORTED, "FMC WON'T ENTER THE IRS (3) DME MODE. PROGRESS PAGE 2 INDICATES BLANK. MAINTENANCE REMOVED AND REPLACED LT FMC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,318 hrs · 13,502 cycles

L1 DOOR FLOOR LEVEL LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 70,204 hrs · 13,485 cycles

FLIGHT 253, PHL-ATH: AIRCRAFT RETURNED TO PHL DUE TO A RECIRCULATION FAN MESSAGE AND SMOKE IN THE CABIN. MAINTENANCE PLACED THE RECIRC FAN ON MEL AND RETURNED THE A/C TO SERVICE. 08/07/07 UPDATE: MAINTENANCE REPLACED THE RECIRC FAN.

Part: CHARGER — FAILED (CABIN) · airframe 69,877 hrs · 13,438 cycles

MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE ON CABIN LEFT SIDE, ROW 18 AND AFT. REPLACED BATTERY CHARGER. NO FURTHER FAULTS.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 69,335 hrs · 13,361 cycles

FLIGHT 748, PHL-AMS: FLIGHT DIVERTED TO CLT DUE TO A NUMBER 2 ENGINE DRIVEN PUMP LOW PRESSURE LIGHT. PRESSURE INDICATION REMAINED NORMAL. MAINTENANCE REPLACED PRESSURE SWITCH S31. NO FURTHER FAULTS.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 67,672 hrs · 12,929 cycles

MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS BETWEEN ROWS 13-15 ON THE RIGHT SIDE INOPERATIVE. RECONNECTED WIRING. NO FURTHER DIFFICULTIES.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 67,440 hrs · 12,861 cycles

MAINTENANCE FOUND 1 EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRING TO LIGHT ASSEMBLY. NO FURTHER FAULTS.