N693AA

Part: BRACKET — CRACKED (RT MLG WW) · airframe 60,728 hrs · 20,983 cycles

RT MAIN WW, LOWER FAIRING SUPPORT STRUCTURE UPLOCK SWITCH BRACKET CRACKED BS 1060, RBL 66.0. R & R IAW AA B757 SRM 51-40-02.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 58,671 hrs · 20,262 cycles

PUNCTURE TO THE LOWER AFT FUSELAGE SKIN JUST ABOVE AFT DRAIN MAST. INSTALLED DOUBLER REPAIR PER SRM 53-00-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,594 hrs · 20,236 cycles

LEFT AFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT HAND AFT DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON FLOORBOARD SUPPORT FROM STATIONS 1661 TO 1680. REPLACED SUPPORT SRM 51-10-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON TOP OF LATERAL FLOORBEAM STATIONS 1660 TO 1662, LEFT BUTTLINE 59 TO 61, INBOARD OF LEFT NUMBER 4 DOOR. INSTALLED T-CAP AND REPAIR ANGLES PER EA B757-53-022922

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

FLOORBEAM SUPPORT CORRODED, BETWEEN FRAME STATIONS 1640 AND 1661 LATERAL "I" BEAMS. REPLACED FLOORBOARD SUPPORT BEAM BETWEEN FRAME STATIONS 1640 AND 1661 AT CENTER LINE 0 WITH NEW FLOORBEAM PER SRM 51-1-02-0G, AND AARD 51-00-05-1, REPAIR 1.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON LATERAL I-BEAM AT STATION 1640 LEFT BUTTLINES 49 TO 59. PERFORMED T-CAP REPAIR PER EA B757-53-022900.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

FLOORBEAM SUPPORT CORRODED BETWEEN STATIONS 1640 AND 1661 AT BUTTLINE 0. INSTALLED NEW SUPPORT PER SRM 51-1-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON TOP OF LATERAL FLOOR BEAM AT STATION 1660, BUTTLINE 0. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-00-51-2R 5.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

RIGHT NUMBER 4 DOOR FORWARD DRAIN SUPPORT CORRODED BETWEEN STATIONS 1640 AND 1661. REPLACED DRAIN SUPPORT PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 56,777 hrs · 19,571 cycles

FLOOR SUPPORT AT LEFT BUTTLINE 20, STATIONS 1620 TO 1640, NICKED WHEN CUTTING T-CAP ON 1640 BEAM. REMOVED AND REPLACED FLOOR SUPPORT PER AARD 51-00-05-1, REPAIR 1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON AFT OUTBOARD GALLEY MOUNT 52 INCHES RIGHT OF BUTTLINE 0 AT STATION 1715. REPLACED RIGHT AFT G4 FLOOR MOUNT PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON AFT DECK Z-ANGLE 51 INCHES RIGHT OF BUTTLINE 0 AT STATION 1716. INSTALLED NEW RIGHT Z-ANGLE PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

STATION 1720 T-CHORD HAS TWO SPOTS OF CORROSION AT LEFT BUTTLINES 2 TO 5 AND 20 TO 24. REPLACED CHORD ANGLE PER SRM 51-10-02-0G.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

GUSSET PLATE HAS LIGHT CORROSION ON UPPER SURFACE AT BUTTLINE 0 STATION 1680. INSTALLED GUSSET PLATE PER SRM 51-10-02-0G.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

HAT CHANNEL CORRODED AT BUTTLINE 0 STATION 1716 TOP OF AFT DECK. REPLACED AFT HAT CHANNEL PER AARD 51-00-05-1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON FORWARD OUTBOARD GALLEY MOUNT 52 INCHES RIGHT OF BUTTLINE 0 AT STATION 1687. REPLACED RIGHT FORWARD G4 FLOOR MOUNT PER AARD 51-00-05-1.

Part: DECK PLATE — DAMAGED (FUSELAGE) · airframe 56,777 hrs · 19,571 cycles

DOUBLERS AT STATION 1720 ON THE AFT DECK DO NOT GO UNDER THE T-CHORD. REPLACED AFT DECK PLATE PER AARD 51-00-05-01 REPAIR 1.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

HAT CHANNEL CORRODED AT BUTTLINE 0 STATION 1684 TOP OF AFT DECK. REPLACED NEW FORWARD HAT CHANNEL PER AARD 51-00-05-1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

RIGHT NUMBER 4 DOOR AFT DRAIN SUPPORT CORRODED BETWEEEN STATIONS 1661 AND 1680. REPLACED RIGHT AFT DRAIN SUPPORT FROM STATIONS 1661 TO 1681 PER AARD 51-00-05-1.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 56,777 hrs · 19,571 cycles

PUNCTURE IN LOWER FUSELAGE SKIN FRAME STATION 321, 3 INCHES BELOW STRINGER 17 LEFT. INSTALLED BLIND RIVET PER SRM 53-00-01-2 REPAIR 6 SECTION 1 AND SRM 51-40-02-0G.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,777 hrs · 19,571 cycles

TEMPORARY REPAIR, BLIND FASTENER INSTALLED AT FRAME STATION 360, STRINGER 4 LEFT. INSTALLED OF A SOLID RIVET AT FRAME STATION 360, STRINGER 4 LEFT PER SRM 53-00-01-2R 6.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON SEAT TRACK A FORWARD END STATION 377. INSTALLED NEW SEAT TRACK A STATIONS 377 TO 438 PER AARD 51-10-05 - 1, REPAIR 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON SEAT TRACK B FORWARD END STATION 377. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: SKIN — CORRODED (NR 1 SLAT) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

NUMBER 1 LEFT OUTBOARD SLAT CORRODED 30 INCHES FROM INBOARD END TOP SKIN. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

CORROSION ON LATERAL I BEAM AT STATION 1681 LEFT BUTTLINE 40. REPLACED I BEAM.

Part: SKIN — CORRODED (NR 1 SLAT) · corrosion level 2 · airframe 56,777 hrs · 19,571 cycles

DEEP BLEND ON NUMBER 1 SLAT UPPER SKIN AT OUTBOARD DRIVE TRACK. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 56,777 hrs · 19,571 cycles

DEEP BLEND WITH BLIND FASTENER ON NUMBER 3 SLAT UPPER SKIN AT INBOARD DRIVE TRACK. INSTALLED DOUBLER REPAIR PER AARD 57-43-00-1.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 56,777 hrs · 19,571 cycles

INTERCOSTAL CRACKED BETWEEN BS 1200 TO 1220 BUTTLINE 0 FORWARD TOP CORNER 3/4 INCHES LONG. INSTALLED WEB AND UPPER ANGLE PER SRM 51-10-02-0G.

Part: SERVICE DOOR — DISLODGED (HYD SYSTEM) · airframe 56,776 hrs · 19,570 cycles

CREW REPORTED VIBRATION FELT IN CLIMB OUT FOLLOWED BY LOSS OF CENTER HYDRAULIC SYSTEM. EMERGENCY DECLARED FLIGHT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. DISCOVERED THE LEFT HYDRAULIC SERVICE DOOR HAD BECOME LOOSE AND LODGED UP INTO THE SERVICE BAY BREAKING THE ACCUMULATOR LINE ON BOTTOM OF ACCUMULATOR. UPDATE: FURTHER INVESTIGATION DISCOVERED THE POSSIBILITY OF THE PANEL BEING IMPACTED FROM THE INSIDE CAUSING THE PANEL TO HAVE BEEN PUSHED INTO THE AIRSTREAM. THE BROKEN RESERVOIR LINE DOES NOT INDICATE ANY EXTERNAL MARKINGS REMOVING THE LIKELIHOOD OF AN EXTERNAL IMPACT CAUSING THE BROKEN LINE. (SUPPLEMENTAL STILL OPEN)

Part: DUCT — BLOWN (LT WING) · airframe 55,055 hrs · 18,912 cycles

MIA - CREW REPORTED DURING CLIMB OUT "L BLEED DUCT LEAK" ANNUNCIATED ON EICAS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED Y-DUCT ON TOP OF LEFT WING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,621 hrs · 18,759 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,685 hrs · 18,431 cycles

LEFT NUMBER 3 DOOR EXTERIOR EMERGENCY LIGHT OUT. REPLACED LAMP FOR LEFT NUMBER 3 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: GUARD — DAMAGED (CABIN) · airframe 53,685 hrs · 18,431 cycles

SEAT 13D EMERGENCY LIGHT GUARD DAMAGED. REPLACED GUARD FOR SEAT 13D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 52,784 hrs · 18,104 cycles

RIGHT WING HAS PREVIOUS BLENDOUT AT THE OUTBOARD END NUMBER 9 SLAT. RIGHT WING NUMBER 9 SLAT BLENDED AREA EXCEEDED LIMITS PER AARD 57-43-00-3. REMOVED DAMAGED CORRODED SKIN AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,784 hrs · 18,104 cycles

RIGHT WING CRACK IN NUMBER 9 SLAT COVE SKIN AT THE INBOARD TRACK. RIGHT WING NUMBER 9 SLAT INSTALLED EXTERIOR DOUBLER REPAIR PER AARD 57-43-0064.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,203 hrs · 17,905 cycles

PART OF COACH CABIN SEAT EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER 2 DOOR. OP CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,203 hrs · 17,905 cycles

FORWARD PART OF COACH CABIN SEAT EMERGENCY LIGHTS DIM. REPLACED POWER SUPPLY FOR EMERGENCY LIGHTS AT RIGHT NUMBER 2 DOOR. OP CHECKED NORMAL.

Part: ACCELEROMETER — INOPERATIVE (VIBRATION SYS) · airframe 50,838 hrs · 17,432 cycles

RDU - INFLIGHT MIA-LGA. CREW REPORTED RIGHT ENGINE VIBRATION. ENGINE WAS PLACED TO IDLE. EMERGENCY DECLARED FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PIECE OF ROPE INGESTED IN RIGHT ENGINE. ACCOMPLISHED BOROSCOPE NO DAMAGE FOUND. REPLACED AIRBORNE VIBRATION MONITORING ACCELEROMETER AND AVM SIGNAL CONDITIONER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,597 hrs · 17,343 cycles

EMERGENCY PATH LIGHT AT SEAT AT 13D INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATH LIGHT AT SEAT 13D, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,597 hrs · 17,343 cycles

EMERGENCY EXIT LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT LEFT NUMBER FOUR DOOR. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,597 hrs · 17,343 cycles

EMERGENCY PATH LIGHTING AT SEAT 13D INOPERATIVE. REMOVED AND REPLACED LAMP FOR EMERGENCY PATH LIGHTING AT SEAT 13D. OPS CHECKS GOOD.

Part: LIGHT — BROKEN (CABIN)

DFW - BULL NOSE EMERGENCY LIGHT ASSEMBLY AT SEAT 31ABC BROKEN. INSTALLED SERVICEABLE LIGHT ASSEMBLY AT SEAT 31ABC.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,819 hrs · 16,702 cycles

FLOOR STIFFENER CORRODED AFT CARGO. REPAIRED IAW SRM 51-10-02-0G.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 28,574 hrs · 1,629 cycles

FLOOR STIFFENER INBD OF AFT CARGO TRANSITION PANEL CORRODED STA 1400 TO STA 1420. REPAIRED IAW SRM 51-10-02-0G. REPLACED PART 146N5390.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 28,574 hrs · 1,629 cycles

NR 3 SLAT HAS CRACK IN THE BACK SKIN 1.25 INCH LONG AT THE INBD DRIVE TRACK. REPAIRED IAW AARD 57-43-04. INSTALLED DOUBLER.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,819 hrs · 16,702 cycles

EXTERNAL FUSELAGE SKIN CORRODED. REPAIRED IAW EA B757-53-00516.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 28,574 hrs · 1,629 cycles

NR 9 SLAT HAS AN APPARENT CRACK ON THE BACK SIDE AT OTBD TRACK. REPAIRED IAW SRM 57-43-00-4. INSTALLED DOUBLER.

Part: SLAT — DAMAGED (WING) · airframe 48,819 hrs · 16,702 cycles

NR 9 SLAT HAS INTERIM REPAIR. REPAIRED IAW SRM 57-43-01-2R2 FLUSH DOUBLER.

Part: SLAT — CRACKED (WING) · airframe 48,819 hrs · 16,702 cycles

NR 9 SLAT CRACKED AT AFT SIDE AT OUTBOARD TRACK. REPAIRED IAW AARD 57-43-00-4 EXTERNAL DOUBLER.

Part: SKIN — CORRODED (NR 9 SLAT) · corrosion level 2 · airframe 28,574 hrs · 1,629 cycles

NR 9 SLAT HAS BLENDED AREA WITH FILLER MATERIAL OVER BLIND FASTENER. REPAIRED IAW SRM 57-43-01-2R2. INSTALLED DOUBLER.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 28,574 hrs · 1,629 cycles

NR 2 SLAT BACK SKIN CRACKED THROUGH FASTENER HOLE AT INBD DRIVE TRACK AREA.

Part: SKIN — CORRODED (NR 3 SLAT) · corrosion level 2 · airframe 28,574 hrs · 1,629 cycles

NR 3 SLAT HAS LOCAL BLEND AND BLIND FASTENER 61 INCH FROM INBD END - FWD OF THE AFT END OF UPPER SKIN. REPAIRED IAW SRM 57-43-01. INSTALLED DOUBLER.

Part: SKIN — DAMAGED (NR 2 SLAT) · corrosion level 2 · airframe 28,574 hrs · 1,629 cycles

NR 2 SLAT HAS LOCAL BLEND AREA WITH BLIND FASTENER INSTALLED AT THE LOCATION 30 INCH OTBD OF INBD END AND 17 INCHES FWD OF AFT END ON LEADING EDGE NOSE SKIN.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 28,574 hrs · 1,629 cycles

NR 3 SLAT CRACKED AT BACK SKIN 1.25 INCH LONG AT THE INBD DRIVE TRACK AREA.

Part: SLAT — DAMAGED (WING) · airframe 48,816 hrs · 16,701 cycles

NR 3 SLAT HAS INTERIM REPAIR. REPAIRED IAW SRM 57-43-01. (INSTALLED FLUSH DOUBLER)

Part: SLAT TRACK — CRACKED (LE SLAT) · airframe 48,816 hrs · 16,701 cycles

NR 2 SLAT CRACKED AT INBOARD DRIVE TRACK. REPAIRED IAW AARD 57-43-00-4. (INSTALLED EXTERNAL DOUBLER).

Part: SKIN — CORRODED (NR 3 SLAT) · corrosion level 2 · airframe 28,574 hrs · 1,629 cycles

NR 3 SLAT HAS LOCAL BLEND AND BLIND FASTENER AT LOCATION 43 INCHES FROM INBD END AT THE AFT LWR END NOSE SKIN. REPAIRED IAW SRM 57-43-01. INSTALLED DOUBLER.

Part: SLAT — DAMAGED (WING) · airframe 48,819 hrs · 16,702 cycles

NR 2 SLAT HAS INTERIM REPAIR. REPAIRED IAW SRM 5743-01.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 28,574 hrs · 1,629 cycles

NR 2 SLAT BACK SKIN CRACKED THROUGH FASTENER HOLE AT INBD DRIVE TRACK AREA.

Part: SKIN — CORRODED (NR 3 SLAT) · corrosion level 2 · airframe 28,574 hrs · 1,629 cycles

NR 3 SLAT HAS LOCAL BLEND AND BLIND FASTENER AT LOCATION 31 INCH INBD OF THE OTBD EDGE - 105 INCH FWD OF THE AFT END. REPAIRED IAW SRM 57-43-01. INSTALLED DOUBLER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,814 hrs · 16,700 cycles

FLOOR SUPPORT CORRODED. REPAIRED IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,814 hrs · 16,700 cycles

FLOOR WEB CORRODED. REPAIRED IAW SRM.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 48,819 hrs · 16,702 cycles

NR 8 SLAT TOP SKIN CORRODED. REPAIRED IAW AARD 57-43-01.

Part: SKIN — CORRODED (NR 8 SLAT) · corrosion level 2 · airframe 28,574 hrs · 1,629 cycles

NR 8 SLAT HAS TWO CORROSION BLISTERS IN TOP SKIN ON 33 INCH FROM THE INBD END. REPAIRED IAW AARD 57-43-0. INSTALLED DOUBLER.

Part: LIGHT — BROKEN (SEAT 23D)

DFW EMERGENCY LIGHT AT SEAT 23D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: A/C PACK — DIRTY (A/C BAY) · airframe 45,971 hrs

MIA INFLIGHT T2107/19JUN. CREW REPORTED FUMES IN CABIN. FLIGHT ATTENDANTS REQUIRED OXYGEN. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED AIR CONDITIONING PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,746 hrs

JFK - EMERGENCY LIGHT AT SEAT ROW 15DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: SHROUD — MISSING (EMERGENCY LIGHT) · airframe 45,746 hrs

JFK - EMERGENCY LIGHT AT SEAT ROW 15DEF MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,746 hrs

JFK - EMERGENCY LIGHT AT SEAT ROW 15DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BRACKET — DISCONNECTED (EMERGENCY LIGHT)

TPA - EAT MOUNTED EMERGENCY LIGHT AT ROW 31 BRACKET DISCONNECTED. REPLACED BRACKET FOR SEAT MOUNTED EMERGENCY LIGHT AT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SQUAT SWITCH — INOPERATIVE (MLG)

SJU INFLIGHT T0815/28MAR - AFTER TAKEOFF FROM JFK, EICAS MESSAGE NOSE AIR GROUND DISAGREE. LANDED SJU WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR COMPRESSED PROXIMITY SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SAN - SEAT MOUNTED AISLE EMERGENCY LIGHTS IN COACH INOPERATIVE. REPLACED THREE BATTERY PACKS IN COACH CABIN FOR SEAT MOUNTED AISLE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSMITTER — DEFECTIVE (T/E FLAP)

AIR INTERRUPTED INTO IAD DUE TO TRAILING EDGE FLAP DISAGREE MESSAGE WHEN FLAPS SELECTED. FLAPS STUCK AT 1 DEGREE. REPLACED LEFT FLAP TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (SW21200401056)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)

EMERGENCY LIGHTS WERE VERY DIM IN THE FIRST CLASS CABIN. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPRING — OUT OF ADJUST (GIRT BAR)

JFK - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND LOWER FUSELAGE SKIN CORRODED AT SKIN SPLICE, STATION 1400 BETWEEN STRINGER 29L AND 29R. REMOVED CORRODED SECTION OF SKIN AND REPAIRED AREAS AFFECTED IAW ESO 90309 DATED 02/25/2003. REPAIR NR 26-536012-2570 AND REPAIR NR 26536012-257 DATED 02-27-03. (M)

Part: SMOKE — DETECTED (CABIN)

MIA - FLT 2415 - FLIGHT ATTENDANT REPORTED SMOKE AND BURNING SMELL IN THE VICINITY OF 2L AND R DOORS. LANDED MIA WITHOUT INCIDENT. PERFORMED HIGH POWER RUN-UP, CLOSED AND OPEN AND ISOLATED BLEEDS. NO SMOKE NOTICED OR BURN SMELL OR HOT AIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — DIRTY (EXTERIOR)

MIA - FOUND AFT LEFT FUSELAGE EMERGENCY LIGHT NEXT TO PRESSURE RELIEF VALVE IS INOPERATIVE. CLEANED BULB ASSEMBLY CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31D INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — MISSING (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23D MISSING. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (AFT BLKHD DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, AFT BULKHEAD DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED AFT BULKHEAD DOOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (ROW 32D)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT 32D EMERGENCY EXIT PATH LIGHTING INOPERATIVE. REPLACED SEAT 32D EMERGENCY EXIT PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHT IN FORWARD CABIN INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE AT FORWARD CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STRIP — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT BY PASSENGER SEAT 4E FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PASSENGER SEAT 4E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: MEC — MALFUNCTIONED (NR 2 ENGINE)

AT 35,000 FT, CREW EXPERIENCED NUMBER 2 ENGINE FLAME-OUT. SUCCESSFULLY RESTARTED ENGINE AT 15,000 FT. AIRCRAFT DIVERTED TO ELP AND MADE A NORMAL LANDING. TROUBLESHOT AND BORESCOPED ENGINE, NO DEFECTS NOTED. REPLACED ENGINE FUEL SHUTOFF VALVE, ENGINE MEC AND FUEL PUMP. CHECKED START LEVER SWICTH, CDP LINE AND ALL LINES ON ENGINE. FUEL S/O VALVE: P/N 61163, S/N 128 MEC: P/N 8063208, S/N 60 FUEL PUMP P/N 7086002, S/N 18348.