N659AA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
78 reports on file, 1995-11-27 – 2014-11-28.
Part: TACH GENERATOR — DEFECTIVE (LT ENGINE) · airframe 70,740 hrs · 24,682 cycles
AIRCRAFT RETURNED, EMER NOT DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. LT ENG N3 FLUCTUATION ALONG WITH LT ENG BLEED OFF & LT ENG SPEED CARD STATUS MSG. ACCOMPLISHED WIRING CHECK OF LT ENG N3 TACH GEN IAW WDM 71-51-22 WITH NO FAULTS FOUND. R & R LT ENG TACH GEN IAW AMM 77-12-02. PERFORMED LEAK & OPERATIONAL CHECKS. SYS CHECKED NORMAL.
Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 70,158 hrs · 24,451 cycles
WEATHER RADAR FAILED. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RADAR ANTENNA & ANTENNA HARNESS. SYS GND CHECKED NORMAL OPERATION CLOSED.
Part: COOLING DUCT — BLOCKED (WEATHER RADAR) · airframe 69,761 hrs · 24,296 cycles
THE WEATHER RADAR WAS TURNED ON & THE RADAR SCREENS WERE COVERED WITH STATIC. FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED THE RADAR ANTENNA ASSEMBLY, NO HELP. REMOVED BLOCKAGE INSIDE EQUIPMENT COOLING DUCT. SYS GND CHECKED NORMAL OPERATION CLOSED.
Part: SKIN — GOUGED (FUSELAGE) · airframe 69,729 hrs · 24,285 cycles
GOUGE FOUND AT STATION 1380 & STRINGER 30. DOUBLER WAS FABRICATED & INSTALLED IAW SRM 53-00-01-2R-2.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,729 hrs · 24,285 cycles
KEEL BEAM T CHORD CORRODED AT LEVELING PLATE STATION 1150 IN RT WW. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-53-035364.
Part: PRESSURE DECK — CORRODED (RT MLG WW) · corrosion level 3 · airframe 69,729 hrs · 24,285 cycles
RIGHT WW PRESS DECK CORROSION. REMOVED CORRODED AREA & ACCOMPLISHED REPAIR IAW EA B757-53-035591.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,729 hrs · 24,285 cycles
BODY STATION 1480 BOTTOM FRAME SECTION CORRODED. INSTALLED DOUBLER IAW EA B757-53-035281.
Part: SKIN — GOUGED (FUSELAGE) · airframe 69,729 hrs · 24,285 cycles
DOUBLER AT STATION 288 & STRINGER 23 RT GOUGED. REPLACED DOUBLER IAW ENGINEERING AUTHORIZATION B757-53-035169 & SRM 53-00-01 FIGURE 201, REPAIR 3.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,230 hrs · 24,096 cycles
LEFT AFT AREA WING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT AFT AREA WING EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: SKIN — CRACKED (NR 1 PYLON) · airframe 69,124 hrs · 24,049 cycles
NR 1 PYLON, THE INBD UPPER AFT HOLE THROUGH THE PYLON SKIN AT THE THRUST REVERSER AFT HINGE FITTING WAS FOUND TO HAVE A CRACK INDICATION DURING HFEC INSPECTION. REMOVED CRACK BY REAMING THE OUTER SKIN ONLY TO .640 & INSTALLED A FREEZE PLUG IAW EA B757-54-033849.
Earlier reports · 1995–2012 · 68 reports
2012
Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 64,392 hrs · 22,347 cycles
FLAP SUPPORT FITTING AT STATION 1180 CORRODED. REPLACED FLAP SUPPORT FITTING PER AARD 51-00-05-1 AND IPC 53-43-52-01. MRT 038028
Part: FILTER — DIRTY (CABIN) · airframe 63,811 hrs · 22,137 cycles
MIA - CREW REPORTED ELECTRICAL SMOKE SMELL THROUGHOUT THE CABIN. EMERGENCY DECLARED, FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RECIRCULATION FAN FILTERS AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,911 hrs · 21,449 cycles
NUMBER 2 SLAT SKIN CORRODED TOP ABOVE OUTBOARD SLAT TRACK AROUND 3 EACH FASTENERS. REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,911 hrs · 21,449 cycles
RIGHT WING CORROSION NUMBER 7 SLAT LOWER SKIN FORWARD OF INBOARD MAIN TRACK. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,911 hrs · 21,449 cycles
NUMBER 7 SLAT CORROSION ON LEADING EDGE SKIN 33 INCHES INBOARD FROM OUTBOARD END 20 INCHES FORWARD FROM UPPER TRAILING EDGE. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 57-43-00-1.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,911 hrs · 21,449 cycles
NUMBER 7 SLAT LEADING EDGE CORROSION AROUND FASTENERS 37 INCHES OUTBOARD FROM INBOARD END. REMOVED CORROSION 37 INCHES OUTBOARD FROM INBOARD END AND FABRICATED DOUBLERS PER ESO 57-43-00-1.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,911 hrs · 21,449 cycles
RIGHT WING CORROSION NUMBER 9 SLAT LOWER SKIN, FORWARD OF OUTBOARD MAIN TRACK. REMOVED DAMAGE AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,911 hrs · 21,449 cycles
RIGHT NUMBER 2 DOOR INNER CREASE BEAM (STR 17) IS CORRODED FROM STATIONS 680 TO 760. RE-INSTALLED INNER CHORD OF CREASE BEAM FROM STATIONS 680 TO 760 PER AARD 51-10-05-1.
Part: TACH GENERATOR — INOPERATIVE (RT ENGINE) · airframe 61,212 hrs · 21,194 cycles
DFW - CREW REPORTED DURING TAKEOFF RIGHT N3 GAUGE BECAME ERRATIC WITH ALL OTHER RIGHT ENGINE GAUGES NORMAL. ALSO HAD RIGHT ENGINE BLEED "OFF" LIGHT, RIGHT CENTER FUEL PUMP PRESS LIGHT AND RIGHT ENGINE SPEED CARD STATUS MESSAGE DISPLAYED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TACHOMETER GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LENS — DAMAGED (CABIN) · airframe 60,842 hrs · 21,073 cycles
LEFT FORWARD OVERWING SIDEWALL EXIT LIGHT LENS DAMAGED. INSTALLED SERVICEABLE PLACARD. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 60,842 hrs · 21,073 cycles
RIGHT FORWARD OVERWING SIDEWALL EXIT LIGHT LENS MISSING. INSTALLED SERVICEABLE PLACARD. OPS CHECK NORMAL.
Part: LENS — DAMAGED (CABIN) · airframe 60,842 hrs · 21,073 cycles
LEFT AFT OVERWING SIDEWALL EXIT LIGHT LENS DAMAGED. INSTALLED SERVICEABLE PLACARD. OPS CHECK NORMAL.
Part: LIGHT — DAMAGED (CABIN) · airframe 60,842 hrs · 21,073 cycles
RIGHT AFT OVERWING SIDEWALL EXIT LIGHT DAMAGED. REPLACED LIGHT ASSEMBLY FOR RIGHT AFT OVERWING EXIT LIGHT. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 60,599 hrs · 20,987 cycles
SEAT 9D EMERGENCY EXIT LIGHT LENS MISSING. REPLACED CLEAR LENS FOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.
Part: LAMP — MISSING (CABIN) · airframe 60,599 hrs · 20,987 cycles
SEAT 9D EMERGENCY EXIT LIGHT MISSING LAMP. REPLACED LAMP FOR SEAT 9D EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.
2010
Part: ACM — FAULTY (AC BAY) · airframe 60,219 hrs · 20,852 cycles
SFO - CREW REPORTED LEFT PACK FAILED WITH RIGHT PACK ON PLACARD. CAPTAIN INITIATED EMERGENCY DESCENT. NO OXYGEN MASKS WERE DEPLOYED. EMERGENCY DECLARED LANDED SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,033 hrs · 20,786 cycles
FIRST CLASS EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK. OPS CHECKS NORMAL.
Part: GENERATOR — FAULTY (RT ENGINE) · airframe 59,761 hrs · 20,689 cycles
IAD - INFLIGHT JFK-SJO. CREW REPORTED RIGHT ENGINE GENERATOR FAILED. AUXILIARY POWER UNIT WAS STARTED AND TRIP CONTINUED. AUXILIARY POWER UNIT AUTO SHUTDOWN. EMERGENCY DECLARED DIVERTED IAD LANDED WITHOUT INCIDENT. FOUND INTERNAL DIODE FAULT ON RIGHT INTEGRATED DRIVE GENERATOR. REPLACED RIGHT HAND INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — BROKEN (CABIN) · airframe 59,569 hrs · 20,627 cycles
RIGHT AFT LAVATORY SIDEWALL EMERGENCY LIGHT INOPERATIVE. INSTALLED SERVICEABLE LIGHT ASSEMBLY. NO HELP. FOUND BROKEN WIRE AT SIDEWALL. REPAIRED WIRE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,115 hrs · 20,459 cycles
FORWARD SECTION OF COACH SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,115 hrs · 20,459 cycles
AFT SECTION OF COACH SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED NORMAL.
Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 59,029 hrs · 20,426 cycles
LANDED MSY ACCT RT PACK ON MEL, LT PACK WOULD NOT HOLD PRESSURIZATION. REPLACED LT ACM. REPLACE RT FLOW CONTROL VALVE.
Part: CONTACT — BROKEN (INTERPHONE JACK) · airframe 58,799 hrs · 20,341 cycles
DFW - DURING CLIMBOUT INTERPHONE CAUSED EXTREME AUDIO STATIC. CAPTAIN WAS UNABLE TO TRANSMIT OR HEAR USING HIS AUDIO SELECT PANEL. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND EXTERNAL FLIGHT INTERPHONE JACK CONTACTS BROKEN AND SHORTED TOGETHER. REPLACED INTERPHONE JACK. SYSTEM GROUND CHECKED NORMAL OPERATION.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,437 hrs · 19,855 cycles
EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. REPLACED LAMP.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,807 hrs · 19,619 cycles
EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK, OPS OK.
2008
Part: LENS — BROKEN (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — BROKEN (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT ROW 24 DEF LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 24DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 51,988 hrs
DFW - EMERGENCY LIGHT AT AFT SEAT 6E HAS A BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT AFT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHROUD — BROKEN (EMERGENCY LIGHTS) · airframe 51,988 hrs
DFW - EMERGENCY LIGHT AT AFT SEAT 14D HAS A BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT AFT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN) · airframe 51,988 hrs
DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT AFT OF LEFT AFT PASSENGER DOOR AT L00760 IS BROKEN. REPLACED LIGHT FOR EMERGENCY EXIT IDENTIFIER LIGHT AT AFT OF LEFT AFT PASSENGER DOOR AT L00760. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — WRONG PART (CABIN) · airframe 51,688 hrs
DFW - EMERGENCY LIGHT AT AFT RIGHT LAVATORY DOOR NEAR FLOOR AT L09007 HAS WRONG LIGHT. REPLACED LIGHT FOR EMERGENCY LIGHT AT AFT RIGHT LAVATORY DOOR NEAR FLOOR AT L09007. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN) · airframe 51,988 hrs
DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT AFT OF RIGHT AFT PASSENGER DOOR AT L00762 IS BROKEN. REPLACED LIGHT FOR EMERGENCY EXIT IDENTIFIER LIGHT AT AFT OF RIGHT AFT PASSENGER DOOR AT L00762. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN) · airframe 51,988 hrs
DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT AFT RIGHT NUMBER ONE DOOR BROKEN. REPLACED LIGHT FOR EMERGENCY EXIT IDENTIFIER LIGHT AT AFT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN) · airframe 51,988 hrs
DFW - EMERGENCY LIGHT AT AFT SEAT 9D HAS A BROKEN BACK PLATE. REPLACED BACK PLATE FOR EMERGENCY LIGHT AT AFT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,988 hrs
DFW - EMERGENCY LIGHTS AT FORWARD CABIN SEATS AND EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN SEATS AND EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,988 hrs
DFW - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LENS — MISSING (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHROUD — MISSING (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BEZEL — BROKEN (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT 17D HAS BROKEN BEZEL. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: CONTROLLER — INOPERATIVE (COCKPIT)
PLA INFLIGHT T882/25DEC SDQ TO MIA FIRST OFFICERS FORWARD WINDSHIELD BEGAN ARCHING FOLLOWED BY THE OUTER WINDSHIELD SHATTERING BUT REMAINING INTACT. LANDED PLA WITHOUT INCIDENT. REPLACED FIRST OFFICERS FORWARD WINDSHIELD AND REPLACED RIGHT HAND WINDOW HEAT CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
DFW EMERGENCY AISLE FLOOD LIGHT HAS MISSING LENS. REPLACED LENS FOR EMERGENCY AISLE FLOOD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.(CLOSED)
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
EMERGENCY LIGHT AT SEAT 5E BULLNOSE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 5E BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
2004
Part: CONNECTOR — LOOSE (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 9 TO 15 INOPERATIVE. REPLACED SOCKET AT ROW 9 FOR EMERGENCY ESCAPE PATH LIGHTING FOR ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: COUPLING — SPLIT (HYD SYSTEM)
ENROUTE KIN-MIA LOST LEFT HYDRAULIC SYSTEM QUANTITY. DECLARED EMERGENCY AND LANDED MIA WITHOUT INCIDENT. REPLACED LT PUMPS AND FILTERS AS WELL AS SPLIT HYDRAULIC COUPLING AT TOP OF LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (SW21200401055)
2002
Part: FSEU — MALFUNCTIONED (E/E BAY)
CUN - FLT 1671 - EN ROUTE JFK-CUN, ON FINAL APPROACH, LEADING EDGE SLAT DISAGREE MESSAGE APPEARED UPON FLAP EXTENSION. UTILIZING ALTERNATE LEADING EDGE/TRAILING EDGE FLAP SWITCHES, EXTINGUISHED MESSAGE. LANDED AT CUN WITHOUT INCIDENT. REPLACED ROTARY ACTUATOR BEHIND NR 5 SLAT PANEL AND REPLACED THE NR 1 FLAP SLAT ELECTRIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PRESSURE SWITCH — FAILED (HYD SYSTEM)
MIA - FLT 971 - EN ROUTE MIA-MGA AT 35,000 FEET, LEFT HYDRAULIC SYSTEM FAILED. EMERGENCY DECLARED. AIRCRAFT RETURNED AND LANDED AT MIA WITHOUT INCIDENT. TROUBLESHOT AND FOUND TO BE AN INDICATION FAULT. REPLACED PRESSURE SWITCH ON LEFT ENGINE DRIVEN PUMP. ALSO, REPLACED PRESSURE SWITCH ON POWER TURBINE UNIT AS A PRECAUTION. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT ON SEAT 6E INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FAN — MALFUNCTIONED (CABIN)
PTY - FLT 2110 - EN ROUTE LIM-MIA - ACRID ELECTRICAL SMELL IN COCKPIT AND CABIN. RECIRCULATING FAN ALREADY TRIPPED OFF. SMELLS STOPPED WHEN RIGHT PACK TURNED OFF. AIR INTERRUPTED AND LANDED PTY WITHOUT INCIDENT. ACCOMPLISHED RECIRCULATION SYSTEM OPERATIONAL TEST FOR BOTH LEFT AND RIGHT RECIRCULATION FANS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: TIRE — SEPARATED (RT MLG)
ORD - FLT 181 - EN ROUTE ORD-LAX, DURING TAKEOFF NR 4 TIRE TREAD SEPARATED. CONTINUED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 4 TIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. RIGHT MLG DOOR AND FLAP FAIRING DAMAGED BY RUBBER DEBRIS, BOTH COMPONENTS REMOVED PER CDL. (M)
2000
Part: CONNECTOR — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF EMERGENCY EXIT ESCAPE PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP LOCATED FORWARD OF COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP FORWARD OF COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, FORWARD EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FORWARD EMERGENCY EXIT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: MODULE — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, L2 DOOR EMERGENCY EXIT LIGHT OVERHEAD INOPERATIVE. RESEATED L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, MID-GALLEY EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPAIRED WIRING ON EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT CHECK, L1 AND R1 FORWARD EMERGENCY EXIT DOOR LIGHT SIGN INOPERATIVE. REPAIRED BROKEN/SHORTED WIRE TO L1 AND R1 FORWARD EMERGENCY EXIT DOOR LIGHT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: ENGINE — DEFECTIVE (LEFT)
LGA - FLT 1129 - AFTER TAKEOFF LGA DURING CLIMB-OUT, SMOKE NOTED IN CABIN AND COCKPIT. AIRCRAFT RETURNED TO LGA AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED LT ENGINE. ACCOMPLISHED LEAK AND GROUND ENGINE RUN CHECK WITH NO DEFECTS FOUND. ACCOMPLISHED PACK BURNOUT PROCEDURE. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE NOTED IN CABIN OR COCKPIT. (M)
1996
Part: FLOOR — CORRODED (BS 405)
AFW - FOUND FLOOR AT STATION 405, RBL 12 HAD CORROSION BLENDED BEYOND LIMITS. REPAIRED PER MRB 757-968. (M)
Part: FRAME — CRACKED (BS 780)
AFW - FOUND FRAME AT STATION 780 NEAR STRINGER 24L HAD A SMALL CRACK INBOARD FLANGE. REPAIRED PER MRB 757-963. (M)
Part: FRAME — GOUGED (BS 1340)
AFW - FOUND FRAME AT STATION 1340 BETWEEN STRINGER 25L AND STRINGER 26L HAD SMALL GOUGE BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-964. (M)
Part: FLOOR — CORRODED (BS 405)
AFW - FOUND FLOOR AT STATION 405, RBL 59, HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-960. (M)
Part: FLOOR BEAM — CORRODED (BS 377)
AFW - FOUND FLOOR BEAM AT STATION 377 LBL 48 HAD CORROSION REMOVED BEYOND SRM LIMITS. REPAIRED PER MRB 757-962. (M)
Part: FLOOR — CORRODED (BS 372)
AFW - FOUND FLOOR AT STATION 405 RBL 12 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-967. (M)
Part: FLOOR BEAM — CORRODED (BS 1640)
AFW - FOUND FLOOR BEAM STATION 1640 RBL 30 HAD CORROSION REMOVED BEYOND SRM LIMITS. REPAIRED PER MRB 757-958. (M)
Part: ANGLE — CORRODED (BS 374)
AFW - FOUND FLOOR STRUCTURE ANGLE AT L-1 DOOR STATION 374 LBL 63 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-961. (M)
Part: SILL — CORRODED (BS 1382-1441)
AFW - FOUND AFT CARGO CUT OUT LOWER SILL INNER CHORD HAS CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-965. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 18F AND AFT INOPERATIVE. RESEATED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 18F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: CONDUCTOR — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 9 THROUGH 17 AND SIDEWALL DIRECTIONAL ARROW LIGHTS AT L2 AND R2 DOORS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT FLAT CONDUCTOR WIRE BY CENTER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)