N602AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
64 reports on file, 1996-01-11 – 2017-07-22.
Part: PROXIMITY SENSOR — FAULTY (R1 DOOR) · airframe 67,203 hrs · 23,586 cycles
AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR ENGAGEMENT LIGHT DISAGREES WITH ARMED STATUS. REMOVED AND REPLACED GIRT BAR PROXIMITY SENSOR S10216 PER WDM 25-66-11. OPERATIONAL CHECK GOOD.
Part: SUPPORT BRACKET — DAMAGED (LT WING TE FLAP) · airframe 66,947 hrs · 23,477 cycles
DURING TROUBLESHOTING OF THE FLAP ISOLATION VALVE EICAS MESSAGE, THE LEFT INBOARD FLAP TRACK FORWARD SUPPORT FITTING HAS FOUND TO HAVE LOOSE OR BROKEN HARDWARE. REMOVED AND REPLACED THE LEFT INBOARD TRAILING EDGE FLAP TRACK SUPPORT BRACKET IAW AMM 27-51-03. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.
Part: SENSOR — FAULTY (MLG)
EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A MAIN LANDING GEAR INDICATION. UNEVENTFUL LANDING. REMOVED AND REPLACED MAIN LANDING GEAR DOOR CLOSED SENSORS; S10241 RIGHT MLG SYSTEM 1, S10242 LEFT MLG SYSTEM 1, AND S10072 RIGHT MLG SYSTEM 2 IAW AMM 32-61-02. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: SENSOR — FAULTY (MLG)
EMERGENCY DECLARED. MIA-UVF FLIGHT RETURNED TO MIA ACCOUNT MAIN LANDING GEAR INDICATION. UNEVENTFUL LANDING. REMOVED AND REPLACED MAIN LANDING GEAR DOOR CLOSED SENSORS; S10241 RIGHT MLG SYSTEM, S10242 LEFT MLG SYSTEM 1, AND S10072 RIGHT MLG SYSTEM 2 IAW AMM 32-61-02. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: SENSOR — FAULTY (MLG) · airframe 66,937 hrs · 23,471 cycles
EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A MAIN LANDING GEAR INDICATION. UNEVENTFUL LANDING. REMOVED AND REPLACED MAIN LANDING GEAR DOOR CLOSED SENSORS S10241, RIGHT MLG SYSTEM 1, S10242 LEFT MLG SYSTEM 1, AND S10072 RIGHT MLG SYSTEM 2, IAW AMM 32-61-02. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: CEILING PANEL — BROKEN (CABIN) · airframe 66,928 hrs · 23,468 cycles
CEILING PANEL WITH ATTACHED EMERGENCY EXIT SIGN IN AFT GALLEY AISLE IS BROKEN. REMOVED AND REPLACED THE CEILING PANEL ASSEMBLY IAW AMM 25-22-02. OPERATIONAL CHECKED GOOD.
Part: SLAT — DELAMINATED (RT WING) · airframe 66,899 hrs · 23,455 cycles
AIRCRAFT WAS GROUNDED. RIGHT WING LEADING EDGE INBOARD NR 6 SLAT IS DELAMINATED, 25.5 INCHES BY 8 INCHES. REMOVED AND REPLACED SLAT IAW MCM CARD 27-94-16 AND DRAWING 114N30001. OPERATIONAL AND RIG CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 66,896 hrs · 23,454 cycles
AIRCRAFT WAS NOT GROUNDED. UPON ADVANCING POWER FOR TAKEOFF, THE MASTER WARNING, CONFIGURATION WARNING, AND SPOILER MESSAGE DISPLAYED. ABORTED TAKEOFF AT APPROXIMATELY 30-40 KNOTS. ACCOMPLISHED FIM 27-61-00, NO FAULTS FOUND. OPERATIONAL CHECK GOOD.
Part: INDICATOR — FAULTY (AIRSPEED) · airframe 66,512 hrs · 23,290 cycles
DURING TAKEOFF ROLL, CAPTAIN`S AIRSPEED INDICATOR FAILED. ABORTED TAKEOFF AT 100 KNOTS. REMOVED AND REPLACED THE MACH AIRSPEED INDICATOR IAW AMM 34-13-02. OPS CHECKED GOOD.
Part: BATTERY — FAILED (FLASHLIGHT) · airframe 66,384 hrs · 23,235 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IN FIRST CLASS LEFT INBOARD SEAT FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00-902-037. OPS CHECKED GOOD.
Earlier reports · 1996–2016 · 54 reports
2016
Part: BEARING — BROKEN (L1 DOOR) · airframe 65,693 hrs · 22,946 cycles
AFTER GATE ARRIVAL THE CREW WAS UNABLE TO OPEN THE L1 DOOR. MAINTENANCE FOUND BROKEN BEARINGS IN THE SLIDE ARMING MECHANISM AFT LINKAGE. REMOVED AND REPLACED BEARINGS AND ADJUSTMENT LINKAGE IAW AMM 52-11-20. OPERATIONAL AND LEAK CHECKS NORMAL. GROUNDED.
Part: BEARING — BROKEN (L1 DOOR) · airframe 65,693 hrs · 22,946 cycles
AFTER GATE ARRIVAL THE CREW WAS UNABLE TO OPEN THE L1 DOOR. MAINTENANCE FOUND BROKEN BEARINGS IN THE SLIDE ARMING MECHANISM AFT LINKAGE. REMOVED AND REPLACED BEARINGS AND ADJUSTMENT LINKAGE IAW AMM 52-11-20. OPERATIONAL AND LEAK CHECKS NORMAL. AIRCRAFT WAS GROUNDED.
Part: GIRT BAR — DIRTY (ZONE 800) · airframe 65,674 hrs · 22,936 cycles
AIRCRAFT NOT GROUNDED. R4 DOOR EMERGENCY EXIT SLIDE WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.
Part: KEELBEAM — CORRODED (BS 1176) · corrosion level 2 · airframe 65,062 hrs · 22,691 cycles
CORROSION WAS FOUND ON THE LEFT SIDE OF THE KEEL REAM WEB AROUND A HYDRAULIC FITTING AT BS 1176 APPROXIMATELY 27 INCHES ABOVE THE LOWER HORIZONTAL OF THE KEEL BEAM. REPAIRED THE KEEL BEAM IAW EA 260548 AND SRM 51-10-02.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,062 hrs · 22,691 cycles
AIRCRAFT WAS IN BASE MX. RT WING UPPER SKIN INNER & OUTER SURFACES ARE CORRODED AT THE OVERWING FUEL FILL PORT ADAPTER LANDING. REPAIRED SKIN IAW EA 260450.
Part: ANTENNA — FAULTY (WEATHER RADAR) · airframe 65,023 hrs · 22,671 cycles
AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB THE WEATHER RADAR FAILED. R & R THE WEATHER RADAR ANTENNA IAW AMM 34-43-05 & ACCOMPLISHED OPERATIONAL TEST IAW AMM 34-43-05. SYS CHECKED NORMAL.
2015
Part: UNKNOWN — ODOR (CABIN) · airframe 64,252 hrs · 22,359 cycles
AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB A STRONG ELEC ODOR WAS REPORTED THROUGHOUT THE CABIN. ACCOMPLISHED MCM 05-96-12 & 05-96-70 WITH NO ODORS NOTED.
Part: FILTER — DIRTY (CABIN) · airframe 64,155 hrs · 22,321 cycles
AFTER ENG START FOR TAXI, FLIGHT ATTENDANT REPORTED A STRONG ELEC SMELL THROUGHOUT THE ENTIRE CABIN. ACCOMPLISHED MCM CARD 05-96-70, TROUBLESHOOT CABIN AIR QUALITY, & CARD 05-96-70, RB 211 CABIN ODOR TROUBLESHOOTING. R & R RECIRCULATION AIR FILTER.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,773 hrs · 21,849 cycles
MAIN CABIN AFT DECK PLATE IS CORRODED BETWEEN FS 1680 - 1720 FROM LBL 54 TO RBL 54. R & R AFT DECK PLATE IAW AARD 51-00-05-1.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,612 hrs · 21,784 cycles
L749 1L DOOR EXIT IDENTIFIER LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33-51-10 WITH GOOD OPERATIONAL CHECK.
2014
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 61,660 hrs · 21,426 cycles
EMERGENCY PATH LIGHTS AT SEAT 28D INOPERATIVE. RECONNECTED SEAT 28D EMER PATH LIGHT CONNECTOR. SYS CHECKED NORMAL IAW 33-51-05.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,909 hrs · 21,141 cycles
EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 36D. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,909 hrs · 21,141 cycles
EMERGENCY LIGHT AT SEAT 17A INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 17A. OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 60,909 hrs · 21,141 cycles
FORWARD GALLEY FLOOD LIGHT INTERMITTENT. SECURED CONNECTOR FOR FWD GALLEY FLOOD LIGHT L9005. OPERATIONS CHECKED NORMAL.
2013
Part: ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 59,056 hrs · 20,438 cycles
MIA CREW REPORTED LE SLAT DISAGREE MESSAGE. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 6 LE ROTARY ACTUATOR. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.
Part: ADC — FAULTY (LEFT) · airframe 56,365 hrs · 19,449 cycles
MIA - CREW REPORTED EICAS MESSAGE FOR TRAILING EDGE FLAP DISAGREE. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.
2012
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,915 hrs · 18,932 cycles
CABIN SEAT MOUNTED ESCAPE PATH LIGHTS ARE DIM. REPLACED BATTERY PACK. OPS CHECK NORMAL.
Part: PLATE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 54,914 hrs · 18,931 cycles
CORROSION ON LEFT AND RIGHT HORIZONTAL STABILIZER STIFFENER PLATE FOWARD OF PIVOT BEARING. REPLACED STIFFENER PLATE EA B757-53-024849.
Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 54,914 hrs · 18,931 cycles
RIGHT NUMBER 2 DOOR UPPER HINGE CUTOUT IS CRACKED. INSTALLED DOUBLER PER SRM 52-10-02-2R 1.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,914 hrs · 18,931 cycles
CORROSION AROUND FASTENERS AT TOP OF KEEL BEAM STATION 1153 LEFT MAIN LANDING GEAR WHEEL WELL. REPAIRED LEFT WHEEL WELL KEEL BEAM INNER CHORD AT STATION 1153 PER EA B757-53-024632.
Part: WIRE — DAMAGED (CABIN) · airframe 54,086 hrs · 18,616 cycles
MID FORWARD CEILING EXIT MARKER LIGHT AFT AT RIGHT AND LEFT NUMBER 2 DOORS INOPERATIVE. REPAIRED WIRE. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,086 hrs · 18,616 cycles
RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
2011
Part: SKIN — DENTED (FUSELAGE) · airframe 52,832 hrs · 18,145 cycles
FOREIGN OBJECT DAMAGE AT STATION 512 AT APPROXIMATE STRINGER 28 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER ECO F1937AA.
2010
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 50,883 hrs · 17,445 cycles
NUMBER 1 SLAT SKIN INBOARD MAIN TRACK ATTACH FITTING AREA CORRODED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER AARD 57-43-00-1.
Part: PAN — GOUGED (L1 DOOR) · airframe 50,883 hrs · 17,445 cycles
LEFT NUMBER 1 DOOR HANDLE PAN GOUGED. REMOVED AND REPLACED HANDLE PAN PER ESO 90108.
Part: SKIN — CRACKED (LE SLAT) · airframe 48,500 hrs · 16,588 cycles
COVE SKIN CRACKED NUMBER 9 SLAT AT INBOARD DRIVE TRACK FITTING. REPAIRED DAMAGE AND INSTALLED EXTERNAL DOUBLER ON INBOARD COVE SKIN PER AARD 57-43-00-4.
Part: SKIN — CRACKED (LE SLAT) · airframe 48,500 hrs · 16,588 cycles
COVE SKIN CRACKED ON SLAT NUMBER 10 AT OUTBOARD DRIVE TRACK FITTING. REPAIRED DAMAGE AND INSTALLED EXTERNAL DOUBLER PER AARD 57-43-00-4.
2009
Part: LENS — MISSING (CABIN) · airframe 47,681 hrs · 16,284 cycles
AFT LAV EMERGENCY FLOOD LIGHT MISSING LENS. INSTALLED NEW LENS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,681 hrs · 16,284 cycles
RIGHT NUMBER ONE DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT.
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW- EMERGENCY LIGHTS IN AFT GALLEY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT GALLEY AREA.
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW- EMERGENCY PATH LIGHTS FROM SEAT 1E TO 6E INOPERATIVE. REPLACED BATTERY PACKS FOR SEAT 1E TO 6E.
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW- EMERGENCY LIGHTS IN ENTIRE FORWARD GALLEY AREA INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY AREA.
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW- EMERGENCY PATH LIGHTS FROM SEAT 26D TO SEAT 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM 26D TO 36D
2008
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 44,046 cycles
SFO EMERGENCY LIGHT AT SEAT ROWS 16 TO 23 INOPERATIVE. REPLACED BATTERY PACK AT SECTION 3 FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 23. SYSTEM GROUND CHECKED NORMAL OPS.
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT 33 INOPERATIVE. REPAIRED CONNECTOR AT WALL DISCONNECT FOR EMERGENCY LIGHT AT SEAT 33. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)
2007
Part: MONITOR — SHORTED (CABIN)
SXM INFLIGHT T1738/09MAY - AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. RETURNED TO SXM AND LANDED WITHOUT INCIDENT. FOUND NUMBER FIVE MONITOR WITH SHORT THAT CAUSED MONITOR TO SMOKE WHEN POWERED ON. REPLACED MONITORS NUMBER THREE AND FIVE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 30D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LENS — MISSING (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT SEAT 19D HAS LENS MISSING. REPLACED LENS AND LAMP FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT CENTER AISLE FORWARD GALLEY FLOOR LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT CENTER AISLE FORWARD GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - FORWARD LEFT MOUNTED EMERGENCY LIGHT AT FORWARD GALLEY WALL DAMAGED. REPLACED FORWARD LEFT MOUNTED EMERGENCY LIGHT AT FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SOCKET — INOPERATIVE (EMERG;ENCY LIGHT)
LGA - EMERGENCY LIGHT AT SEAT ROW 19DEF INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT SEAT ROW 19DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (CABIN)
SFO EMERGENCY LIGHTS AFT OF SEAT 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AFT OF SEAT 28. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
2004
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY LIGHTS ON SEATS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON SEATS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SENSOR — MALFUNCTIONED (RT ENGINE)
ORD - INFLIGHT T2252/01 ON FINAL RIGHT ENGINE FIRE INDICATION SHUT ENGINE DOWN AND FIRED BOTH BOTTLES. REPLACED BOTH ENGINE FIRE BOTTLES AND SQUIBS PER MM 26 21 01 4 FOR RIGHT HAND ENGINE AND REPLACED NR 1 TS5031 FIRE LOOP AND REPLACED NUMBER TWO CARD M684. SYSTEM GROUND CHECKED NORMAL OPERATION.
2002
Part: BATTERY — DISCHARGED (CABIN)
LAX - FOUND EMERGENCY SEAT MOUNTED LIGHTS RIGHT SIDE FROM ROWS 15 TO 23 ARE INOPERATIVE. REPLACED BATTERY AND CHARGED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EXIT SIGN DIM. REPLACED LAMPS IN RIGHT VOERWING EXIT SIGN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: PIN — INOPERATIVE (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. RE-SECURED EMERGENCY EXIT CONNECTOR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LGHT AT DOOR 3L INOPERATIVE. RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS AT SEAT 23D INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE FLOOR PATH LIGHT ASSEMBLY AT SEAT 23D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1996
Part: SKIN — GOUGED (LT TE FLAP)
AFW - FOUND LEFT WING OUTBOARD MAIN FLAP UPPER SKIN PANEL HAS GOUGES BLENDED AS SHOWN ON SKETCH. GOUGES ARE FROM CONTACT WITH FASTENERS ON NR 3 SPOILER. PER MRB 757-768. (M)
Part: LIGHT STRIP — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT MID-GALLEY AREA FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT MID-GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: STRIP — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT MID-GALLEY FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT MID-GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)