N833HK

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 35,061 hrs · 31,150 cycles

LANDING GEAR AIR GROUND FAIL ON TAKEOFF, GEAR WOULD NOT COME UP, RETURNED TO BLOCK. MAINTENANCE REPLACED NLG WOW PROXIMINTY SENSOR, OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 34,976 hrs · 31,068 cycles

LANDING GEAR FAILED TO RETRACT DURING CLIMB, FOLLOWED QRH, GEAR MOVED NORMAL, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED LANDING GEAR ELECTRONIC UNIT, OPS CHECK GOOD.

Part: ACM — FAILED (NR 1) · airframe 34,873 hrs · 30,966 cycles

ELECTRICAL SMOKE ODOR WITH VISIBLE SMOKE FROM F/O'S OTBD FLOORBOARD AREA, PLANE MADE AN UNSCHEDULED LANDING. MAINTENANCE INSPECTED AND FOUND NR 1 AIR CYCLE MACHINE LOCKED UP, REPLACED NR 1 AIR CYCLE MACHINE AND OPS CHECKED GOOD.

Part: DUCT — BLOWN (CABIN AIR) · airframe 34,570 hrs · 30,689 cycles

BRIEF ELECTRICAL SMOKE AND ODOR IN COCKPIT DURING CRUISE. MAINTENANCE INSPECTED AND FOUND A DUCT BLOWN UNDER CABIN. MAINTENANCE SECURED DUCT AND OPS, LEAK CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,800 hrs · 29,985 cycles

CEILING EMERGENCY EXIT LIGHTS ARE INOP AT ROWS 18 AND 23. MAINTENANCE REPLACED BULBS AND OPS CHECKED GOOD.

Part: COUPLING — DISCONNECTED (A/C PACK) · airframe 33,578 hrs · 29,792 cycles

DURING CLIMB AT AROUND 10000 FT, THERE WAS A LOUD POPPING NOISE FOLLOWED BY LOUD NOISE OF AIR RUSHING UNDER CABIN FLOOR AND DIFFICULTY MAINTAINING CABIN PRESSURIZATION FOLLOWED BY NR 2 A/C PACK OVERLOAD MESSAGE, ACFT RETRURNED. MAINTENANCE INSPECTED AND FOUND COUPLING ON COOLING PACK CAME OFF, ADJUSTED COUPLING AND SECURED, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAME 15) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

FWD DIGITAL IS CORRODED AT FRAME 15 AND LT OMEGA BEAM. MAINTENANCE REPLACED FWD DIGITAL.

Part: CHANNEL — CORRODED (THRESHOLD) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

CHANNEL AT PASSENGER DOOR THRESHOLD CORRODED. MAINTENANCE REPLACED CHANNEL.

Part: GUSSET — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

CENTER GUSSET BETWEEN FRAME 59 - 61 AT Y0.0 HAS CORROSION. MAINTENANCE REPLACED CENTER GUSSET.

Part: GUSSET — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

LEFT GUSSET BETWEEN FRAMES 59 AND 61 AT Y-479.0 CORRODED. MAINTENANCE REPLACED LEFT GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

RIGHT FLOOR SUPPORT AT FRAME 61 CORRODED. MAINTENANCE REPLACED FLOOR SUPPORT.

Part: GUSSET — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

RIGHT GUSSET BETWEEN FRAMES 59 AND 61 AT Y479.0 CORRODED. MAINTENANCE REPLACED RT GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

LEFT FLOOR SUPPORT AT FRAME 61 HAS CORROSION. MAINTENANCE REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-19) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

LOWER RAMP FLOORBOARD SUPPORT ON LT BEAM BETWEEN FR18 AND FR19 HAS LEVEL 2 CORROSION. MAINTENANCE REPLACED LOWER RAMP BOARD SUPPORT.

Part: SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

RAMP SUPPORT ON CENTER BEAM AT FRAME 19 HAS LEVEL 2 CORROSION. MAINTENANCE REPLACED RAMP SUPPORT AT FRAME 19.

Part: BEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

CENTER BEAM GUSSET HAS CORROSION AT FRAME 20. MAINTENANCE REPLACED CENTER BEAM GUSSET.

Part: CHANNEL — CORRODED (DOOR SILL) · corrosion level 2 · airframe 33,573 hrs · 29,787 cycles

CARGO DOOR BOTTOM SILL CHANNEL IS CORRODED. MAINTENANCE REPLACED CARGO DOOR BOTTOM CHANNEL.

Part: BRACKET — BENT (DOOR ROLLER) · airframe 32,963 hrs · 29,231 cycles

PASSENGER DOOR STAIRS DID NOT DEPLOY WHEN DOOR OPENED DURING POST FLIGHT. MAINTENANCE INSPECTED AND REPLACED PASSENGER DOOR ROLLER BRACKET, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,685 hrs · 28,990 cycles

LEFT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,500 hrs · 28,824 cycles

EMERGENCY LIGHT ON BULKHEAD AT 3C IS INOPERATIVE. MX REPLACED BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,339 hrs · 28,675 cycles

MX INSPECTED AND FOUND LT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. REPLACED FLOOD LIGHT, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,146 hrs · 28,509 cycles

SERVICE DOOR EXIT MARKER INOPERATIVE. MX REPLACED BULB AND OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,124 hrs · 28,490 cycles

LEFT EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. MX REPLACED BULB AND OPS CHECKED GOOD.

Part: SWITCH — BROKEN (COCKPIT) · airframe 31,404 hrs · 27,899 cycles

DURING PRE-FLIGHT INSPECTION, THE FLIGHT CREW FOUND THE EMERGENCY LIGHT SWITCH ON THE OVERHEAD PANEL BROKEN. MX INSPECTED AND R & R THE SWITCH. SYS OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,128 hrs · 27,650 cycles

DURING SCHEDULED MAINTENANCE FOUND THE RIGHT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACE THE BULB. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,128 hrs · 27,650 cycles

DURING SCHEDULED MAINTENANCE THE RIGHT AFT WING/FUSELAGE FARING EXTERIOR FLOOD LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT WING/FUSELAGE FARING EXTERIOR FLOOD LIGHT. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,302 hrs · 27,622 cycles

DURING SCHEDULED MAINTENANCE THE LEFT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT BULB. SYSTEM OPS CHECKED GOOD.

Part: CABLE — OUT OF ADJUST (CABIN DOOR) · airframe 30,300 hrs · 26,927 cycles

FLT 3395 - CMH - THE FLIGHT ATTENDANT REPORTED THAT THE MAIN CABIN DOOR COULD NOT BE OPENED. MAINTENANCE INSPECTED THE MAIN CABIN DOOR AND ADJUSTED THE INNER HANDLE CONNECTION CABLE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL INSTRUCTIONS. FOLLOW-ON OPERATIONAL CHECK OF THE DOOR WAS GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 29,515 hrs · 26,214 cycles

CREW REPORTED, A/C FILLED WITH SMOKE ON GROUND AT GATE. MAINTENANCE INSPECTED A/C AND PERFORMED OPS CHECK AND COULD NOT DUPLICATE, OPS CHECK GOOD.

Part: SUPPORT — DEFECTIVE (PAX DOOR) · airframe 29,499 hrs · 26,198 cycles

CREW REPORTED THAT THE PASSENGER DOOR AIRSTAIR STEPS DO NOT DEPLOY WHEN OPENED DURING POST FLIGHT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED PASSENGER DOOR SUPPORT AND OPS CHECK GOOD.

Part: SEAL — OBSTRUCTED (CABIN DOOR) · airframe 29,410 hrs · 26,113 cycles

A/C WOULD NOT PRESSURIZE DURING CLIMBOUT OF KSTL, CREW RETURNED A/C TO KSTL FOR UNSCHEDULED LANDING. MAINTENANCE INSPECTED MAIN DOOR SEAL AND REMOVED DEBRIS, OPS CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,981 hrs · 25,726 cycles

UPON INSPECTION, QA FOUND 2 LEVEL 2 CORROSION DAMAGE AREAS BETWEEN SKIN SPLICE JUN 02 TO FR14, STR 18R & STR 21R ON LOWER RIGHT CENTER FUSELAGE I. DAMAGE 1 AREA: 2.7"X1.5", DAMAGE 2 AREA: 5"X4.3". MAINTENANCE REPAIRED THE 2 DAMAGE AREAS BY FILLERS AND DOUBLERS MADE OUT OF AL 2024-T3, 0.050" (1.3MM) THICK, AL 2024-T3, 0.040" (1.0MM) THICK.

Part: ACCUMULATOR — CRACKED (HYDRAULIC SYS) · airframe 28,979 hrs · 25,725 cycles

HYD FLUID LEAKING IN FWD HYD COMPARTMENT. MAINTENANCE FOUND CRACK IN ACCUMULATOR, CAPPED ASSOCIATED HYD LINE, DEFERRED PASSENGER DOOR HYD ACTION, FERRIED A/C FROM MDT TO STL. MAINTENANCE THEN REPLACED ACCUMULATOR HAVING P/N 2704-0001-003 AND OPS AND LEAK CHECK GOOD.

Part: GENERATOR — MALFUNCTIONED (APU) · airframe 28,636 hrs · 25,387 cycles

DURING PREFLIGHT INSPECTION THE FLIGHT CREW REPORTED THE APU GENERATOR WENT OFF LINE AND THEN THEY SMELLED SMOKE AND BURNT WIRES. MAINTENANCE INSPECTED THE APU AND FOUND NO EVIDENCE OF BURNT WIRING OR SMOKE. DEFERRED APU GENERATOR PER MEL 24-34-01-2.

Part: VALVE — LEAKING (BLEED AIR SYS) · airframe 28,428 hrs · 25,187 cycles

DURING CLIMB THE FLIGHT CREW GOT A HIGH STAGE BLEED VALVE FAIL MESSAGE FOLLOWED BY A BLEED 1 OVERTEMP. AIRCRAFT RETURNED TO IAD. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 HIGH STAGE VALVE. SYSTEM OPS AND LEAK CHECKED GOOD.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 27,675 hrs · 24,514 cycles

RAMP PERSONNEL MOVED AIRCRAFT TO A REMOTE PAD AND WHEN THEY WENT TO CLOSE THE PASSENGER DOOR THE HANDLE BROKE. MAINTENANCE INSPECTED THE DOOR AND REMOVED AND REPLACED THE PASSENGER DOOR HANDLE. SYSTEM OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 26,653 hrs · 23,563 cycles

DURING LANDING THE FLIGHT CREW GOT A BRAKE DEGRADE EICAS MESSAGE WHEN LANDING GEAR WAS SELECTED AND DEPLOYED INTO THE DOWN AND LOCKED POSITION. CREW REPORTED THAT BRAKING ACTION FEELS DIMINISHED UPON TOUCHDOWN. MAINTENANCE INSPECTED AND OPS TESTED THE BRAKES AT THE GATE. ALL CHECKS WERE GOOD. MAINTENANCE ALSO CHECKED NUMBER 4 TRANSDUCER, HUB CAP AND CLIP. ALL CHECKS WERE GOOD. CREW TAXIED AND TESTED THE BRAKES AND BRAKES FELT NORMAL. NO MESSAGE ON EICAS. OPS CHECKED GOOD.

Part: LINKAGE — LACK OF LUBE (SERVICE DOOR) · airframe 26,639 hrs · 23,547 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THAT THE GALLEY SERVICE DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND LUBRICATED THE GALLEY SERVICE DOOR. DOOR OPS CHECKED GOOD.

Part: ROLLER — BENT (PAX DOOR) · airframe 26,504 hrs · 23,418 cycles

DURING PRE-FLIGHT THE FLIGHT CREW FOUND A ROLLER AT THE BASE OF THE PASSENGER DOOR BENT. MAINTENANCE INSPECTED AND THE AIRCRAFT WAS FERRIED TO IAD. MAINTENANCE REMOVED AND REPLACE THE PASSENGER DOOR STEP FOLD OUT BACK STOP. DOOR OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,149 hrs · 23,073 cycles

DURING CLIMB AIRCRAFT MAY HAVE HAD A POSSIBLE LIGHTNING STRIKE. CREW REPORTED A STRONG O-ZONE SMELL IN CABIN WITH NO VISIBLE SMOKE. MAINTENANCE INSPECTED AND PERFORMED A LIGHTNING STRIKE INSPECTION. NO DEFECTS WERE NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,825 hrs · 22,782 cycles

DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 7, 9, 11,13, 15, AND 16 WERE INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND INVERTER. SYSTEM OPS CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CARGO FLOOR PANEL 272AF IS DELAMINATED. R & R CARGO PANEL. W/C 2197

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CENTER SEAT TRACK B-5 HAS CORROSION AROUND FASTENER HOLES. R & R SEAT TRACK. W/C 2126

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT CTR SEAT TRACK B-3 HAD CORROSION AROUND FASTENER HOLES BETWEEN FRAME 30-35. R & R LT SEAT TRACK. W/C 2126

Part: SUPPORT — BROKEN (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CABLE GUIDE SUPPORTS BROKEN. R & R CABLE GUIDE SUPPORTS. W/C 2200

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RIGHT CENTER SEAT TRACK C-4 BETWEEN FRAME 47-52 HAS CORROSION AROUND FASTENER HOLES. R & R SEAT TRACK. W/C 2129

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT CTR SEAT TRACK C-2 HAD CORROSION AROUND FASTENER HOLES BETWEEN FRAME 30-35. R & R RT SEAT TRACK. W/C 2128

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RIGHT CENTER SEAT TRACK C-2 BETWEEN FRAME 30-35 HAS CORROSION AROUND FASTENER HOLES. R & R SEAT TRACK. W/C 2128

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT CTR SEAT TRACK B-1 HAD CORROSION AROUND FASTENER HOLES. R & R LT SEAT TRACK. W/C 2124

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT CTR SEAT TRACK C-5 BETWEEN FRAME 52-60 HAS CORROSION AROUND FASTENER HOLES. R & R SEAT TRACK. W/C 2130

Part: SUPPORT — BROKEN (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) SUPPORTS BROKEN AT FRAME 34. R & R SUPPORTS. W/C 1154

Part: ATTACH ANGLE — DELAMINATED (LT WING) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT FWD BOTTOM WING-FAIRING ATTACHMENT ANGLE IS CRACKED. R & R ANGLE. W/C 5069

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LEFT SEAT TRACK A-5 HAS CORROSION AROUND FASTENER HOLES. R & R SEAT TRACK. W/C 2123

Part: TRACK — WORN (TE FLAP) · airframe 25,762 hrs · 22,733 cycles

LEFT WING OTBD FLAP CENTER TORQUE BOX TRACK WORN. R & R TRACK ASSY. W/C 5072

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT OMEGA BEAM AT FRAME 48 IS CORRODED BEYOND LIMITS. R & R DAMAGED AREA ON OMEGA BEAM. W/C 1110

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RIGHT FLOOR SILL AT FRAME 36-41 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1091

Part: ATTACH FITTING — DAMAGED (RT WING) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT INBD L/E WING-FAIRING ATTACHMENT STRIP CRACKED. R & R STRIP. W/C 6017

Part: PARTITION — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT PARTITIAN AT FRAME 61 IS CORRODED BEYOND LIMITS. R & R LT PARTITIAN. W/C 2089

Part: PROFILE — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT OTBD PROFILE AT FRAME 61 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 2172

Part: GUSSET — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CTR GUSSET AT FRAME 29-35 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET. W/C 1144

Part: SILL — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SILL AT FRAME 29-35 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1146

Part: ATTACH FITTING — DAMAGED (RT WING) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT TOP WING-FAIRING ATTACHMENT STRIP CRACKED. R & R STRIP. W/C 6018

Part: ATTACH FITTING — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT TOP WING-FAIRING ATTACHMENT STRIP CRACKED. R & R STRIP. W/C 6020

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LEFT SEAT TRACK A-1 AROUND FASTENER IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 2119

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CTR GUSSET AT FRAME 39-46 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET. W/C 1094

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

SILL AT FRAME 48-52 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1093

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) FLOOR SUPPORT BEAM DAMAGED BEYOND LIMITS. R & R BEAM. W/C 1112

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) SILL AT FRAME 42-48L IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1096

Part: GUSSET — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT GUSSET AT FRAME 29-35 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1145

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SEAT TRACK D-2 AT FRAME 30-35 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2132

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 25,762 hrs · 22,733 cycles

(V0XR) COCKPIT FLOOR PANEL 221GF IS DAMAGED BEYOND LIMITS. R & R FLOOR PANEL. W/C 2157

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SEAT TRACK D-1 AT FRAME 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2131

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SILL AT FRAME 60-65 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 2107

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

LEFT FLOOR GUSSET AT FRAME 36-3948-52 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1089

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT FWD BOTTOM WING-FAIRING ATTACHMENT ANGLE IS CRACKED. R & R ANGLE. W/C 5068

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SEAT TRACK A-4 AT FRAME 35-47 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2122

Part: BEAM — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT BEAM AT FRAME 58-61 IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 2079

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SEAT TRACK D-4 AT FRAME 47-52 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2134

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT GUSSET AT FRAME 53-59 IS CORRODED BEYOND LIMITS. R & R BEAM, GUSSET WAS PRE-INSTALLED ON BEAM. W/C 2086

Part: PARTITION — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT PARTITIAN AT FRAME 61 IS CORRODED BEYOND LIMITS. R & R PARTITIAN. W/C 2078

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) SILL AT FRAME 48-52 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1097

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT GUSSET AT FRAME 53-59 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2083

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SEAT TRACK A-2 AT FRAME 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2120

Part: SEAL — WORN (HORIZONTAL STAB) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT HORIZONTAL INBD L/E SEAL PANEL 333DL IS WORN BEYOND LIMITS. R & R SEAL. W/C 3063

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) GUSSET AT FRAME 24-29 Y0.0 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1113

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

LEFT GUSSET AT FRAME 36-39 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1089

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SEAT TRACK D-3 AT FRAME 35-47 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2133

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CTR GUSSET AT FRAME 53-59 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2082

Part: PROFILE — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT OTBD PROFILE AT FRAME 65 HAS NUMEROUS HOLES DRILLED AROUND NUTPLATE. R & R PROFILE W/C 1129

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SEAT TRACK D-5 AT FRAME 52-60 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2135

Part: BUSHING — CORRODED (RUDDER) · airframe 25,762 hrs · 22,733 cycles

(V0XR) BUSHINGS AT FWD RUDDER AT PCU-2 CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 3059

Part: ANGLE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT PROFILE ANGLE BEAM AT FR 66-67 IS CRACKED UNDER BAGGAGE COMPARTMENT. R & R BEAM. W/C 1136

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) SILL AT SERVICE DOOR IS CORRODED OUT OF LIMITS. R & R SILL. W/C 1085

Part: ANGLE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) GUSSET AT LY-479.0 AT FR 18-23 IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1087

Part: GUSSET — DAMAGED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CO-PILOTS LOWER AFT SIDEWALL PANEL IS DAMAGED. R & R SIDEWALL. W/C 2117

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RIGHT SEAT TRACK D-3 IS CORRODED BEYOND LIMITS. R & R RT SEAT TRACK. W/C 2133

Part: PROFILE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) SILL AT FR 41-48R IS CORRODED OUT OF LIMITS. R & R SILL. W/C 1092

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) FLOOR GUSSET AT FR 46-52 IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1098

Part: ANGLE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) SCALLOPED ANGLE AT FR 18 IS CORRODED OUT OF LIMITS. R & R ANGLE. W/C 1086

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CTR GUSSET AT YO.O FR 20-23 IS CORRODED OUT OF LIMITS. R & R CTR GUSSET. W/C 1073

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SEAT TRACK D-2 BETWEEN 30-35 IS CORRODED BEYOND LIMITS. R & R RT SEAT TRACK. W/C 2132

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SILL FWD OF SERVICE DOOR AT FR 19-20 IS CORRODED OUT OF LIMITS. R & R SILL. W/C 1076

Part: ANGLE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT PROFILE ANGLE BEAM AT FR 66-67 IS CRACKED UNDER BAGGAGE COMPARTMENT. R & R BEAM. W/C 1136

Part: PROFILE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) GUSSET AT FR 36-39 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2073

Part: ANGLE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT PROFILE ANGLE BEAM AT FR 66-67 IS CRACKED UNDER BAGGAGE COMPARTMENT. R & R BEAM. W/C 1136

Part: PROFILE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT PROFILE ANGLE BEAM AT FR 66-67 IS CRACKED UNDER BAGGAGE COMPARTMENT. R & R BEAM. W/C 1136

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT FLOOR GUSSET AT FR 23-29 IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1105

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SILL AFT OF SERVICE DOOR FR 22-23 IS CORRODED OUT OF LIMITS. R & R RT SILL. W/C 1075

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LEFT SEAT TRACK A-3 IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 2121

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SEAT TRACK A-4 BETWEEN 35-47 IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 2122

Part: DOUBLER — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) DOUBLER AT RY 479.0 FR 20-22 IS CORRODED OUT OF LIMITS. R & R DOUBLER. W/C 1082

Part: PROFILE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT PROFILE AT FR 61 IS CORRODED OUT OF LIMITS. R & R LT PROFILE. W/C 1063

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT OMEGA BEAM AT FR 45 IS CORRODED OUT OF LIMITS. R & R BEAM. W/C 1111

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) FLOOR SUPPORT AT YO.O FR 19-20 IS CORRODED OUT OF LIMITS. R & R FLOOR SUPPORT. W/C 1077

Part: PROFILE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) PROFILE AT FR 20 IS CORRODED OUT OF LIMITS. R & R PROFILE. W/C 1078

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SILL AT FR 53-59 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2080

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) FLOOR GUSSET AT FR 39-46L IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1095

Part: CHANNEL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CTR HAT BEAM AT YO.O FR 19-20 IS CORRODED OUT OF LIMITS. R & R CTR HAT BEAM. W/C 1080

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) CTR GUSSET AT FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2087

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT FLOOR GUSSET AT FR 46-52R IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1099

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SILL AT FR 29-35 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2112

Part: PROFILE — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) PROFILE AT FR 17-18 OTBD OF LY 479.0 IS CORRODED OUT OF LIMITS. R & R PROFILE. W/C 1088

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT GUSSET AT FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2088

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) PAX DOOR THRESHOLD SUPPORT BRACKETS CORRODED OUT OF LIMITS. R & R ANGLES IAW SRM 51-20-03. W/C 1084

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SILL AT FR 23-29 IS CORRODED OUT OF LIMITS. R & R SILL AT FR 23-29 IAW SRM 51-40-02. W/C 1106

Part: GUSSET — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) GUSSET AT FR 17-18, Y0.0, LY-479.0 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED GUSSET IAW EMB145 SRM 51-10-02, 51-10-03, AND 51-40-02. W/C 1074

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SILL AT FR 59-60 IS CORRODED OUT OF LIMITS. R & R LT SILL AT FR 59-60 IAW SRM 51-40-02, 51-10-02, 51-20-02, AND CPM 51-21-05. W/C 2085

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SILL AR FR 23-29 IS CORRODED OUT OF LIMITS. R & R RT SILL AT FR 23-29 IAW SRM 51-10-02, 51-20-03, 51-40-02, CMP 51-21-04. W/C 1114

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SILL AT FR 18-23 IS CORRODED OUT OF LIMITS. R & R LT SILL FROM FR 18-23 IAW SRM 51-40-02. W/C 1081

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) LT SILL AT FR 53-59 IS CORRODED OUT OF LIMITS. R & R SILL IAW SRM 53-24-10, 51-10-02, 51-20-03, 51-40-02, CMP 51-21-04. W/C 2081

Part: SILL — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT SILL AT FRAME 59-60 IS CORRODED OUT OF LIMITS. R & R RT SILL AT FR 59-60 IAW SRM 51-40-02, 51-10-02, 51-10-01, CPM 51-21-05. W/C 2084

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,762 hrs · 22,733 cycles

(V0XR) RT HAT BEAM AT RY 479.0, FR 19-25 IS CORRODED OUT OF LIMITS. R & R RT OMEGA BEAM FROM FR 19-25 IAW SRM 51-40-00 AND 51-20-03. W/C 1079.

Part: MECHANISM — BINDING (PAX DOOR) · airframe 24,477 hrs · 21,567 cycles

DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE INTERNAL HANDLE LOCKING MECHANISM. PASSENGER DOOR OPS CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 24,151 hrs · 21,269 cycles

DURING GROUND HANDLING, THE CREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE MAIN DOOR LATCHING MECHANISM PRIOR TO FLIGHT. FOLLOW-ON OPERATIONAL CHECK OF THE DOOR WAS SATISFACTORY.

Part: CONNECTOR — DIRTY (CABIN) · airframe 23,879 hrs · 21,006 cycles

DURING THE PRE FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL OF THE EMERGENCY LIGHTS WERE INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE AS MAINTENANCE CLEANED THE CONNECTOR AT THE NR 2 EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPS CHECKED GOOD FOLLOWING REPAIR. AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 22,995 hrs · 20,263 cycles

CREW REPORTED THAT THE MAIN PASSENGER DOOR AS BEING DIFFICULT TO OPEN. MAINTENANCE ADJUSTED THE MAIN DOOR CABLES. OPERATIONALLY CHECKED GOOD AFTER ADJUSTMENT.

Part: MECHANISM — OUT OF ADJUST (PAX DOOR) · airframe 22,988 hrs · 20,256 cycles

CREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE DOOR OPERATING MECHANISM. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,797 hrs · 20,070 cycles

DURING THE PREFLIGHT INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER CONTROLLING THE RIGHT OVERWING EXIT LIGHT. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 22,728 hrs · 20,000 cycles

CREW REPORTED A STRONG ELECTRICAL SMELL IN THE CABIN NEAR ROW 16 AND THAT THE LIGHT LENS AT THE SAME ROW WAS WARPED. MAINTENANCE INSPECTED THE CABIN LIGHTING SYSTEM AND DEFERRED THE CEILING LIGHT AT ROW 16 IAW THE EMB145 MEL.

Part: WARNING SYSTEM — ACTIVATED (FUEL SYSTEM)

FLT 7896 - DEN - ABORTED TAKEOFF - EI FUEL IMPENDING BYPASS EICAS MESSAGE. MAINTENANCE INSPECTED AND DEFERRED PER MEL. (S)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,267 hrs · 16,856 cycles

PRE FLT 7882 - STL - VARIOUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER. LIGHT OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 19,242 hrs · 16,832 cycles

PRE FLT 7884 -ORD- EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESECURED THE CONNECTION TO THE AFFECTED LIGHT STRIP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,854 hrs · 16,471 cycles

PRE FLT 7987 - RIC - SEVERAL EMERGENCY LIGHTS IN CABIN WILL NOT SHUT OFF. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: LIGHT — BURNED OUT (CABIN) · airframe 18,106 hrs · 15,808 cycles

PRE FLT NR 7979 - MLI - EMERGENCY EXIT LIGHT LEFTHAND OVERWING EXIT MARKER INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT, OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 18,099 hrs · 15,799 cycles

PRE FLT NR 7967 - ORD - EMERGENCY LIGHT BEHIND OVERWING EXIT LEFT SIDE INOP. MAINTENANCE RE-SECURED LIGHT SIGN CONNECTOR AND ACCOMPLISHED EMERGENCY LIGHT TEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,954 hrs · 15,677 cycles

PRE FLT NR 7928- ALB - LEFTHAND OVERWING EXIT MARKER EMERGENCY LIGHT INOP. MAINTENANCE RESET POWER, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 17,893 hrs · 15,627 cycles

POST FLT NR 7883 - IAD - EMERGENCY LIGHT GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE RESET EMERGENCY LIGHT SWITCH AND SECURED LIGHT CONNECTOR, OPS NORMAL.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 17,882 hrs · 15,617 cycles

POST FLT NR 7901 - ORD - EMERGENCY LIGHT AT LEFT OVERWING INOP. MAINTENANCE CLEANED CONNECTOR, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 17,766 hrs · 15,503 cycles

PRE FLT NR 7947 - ORD - EMERGENCY LIGHT LEFTHAND OVERWING EXIT IDENTIFIER IS INOP. MAINTENANCE CLEANED CONNECTOR. OPS CHECKS GOOD ON GROUND.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 17,760 hrs · 15,497 cycles

POST FLT NR 7903 - MKE - GALLEY WALL EXIT LOCATOR LIGHT INOP. MAINTENANCE REMOVED GALLEY WALL EMERGENCY LIGHT CLEANED CONNECTOR REINSTALLED, OPS CHECKS GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 17,558 hrs · 15,299 cycles

PRE FLT NR 8011 - MLI - EMERGENCY LIGHT AT LEFT WING EXIT INOP. MAINTENANCE SECURED CONNECTOR CHECKS GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 17,558 hrs · 15,299 cycles

PRE FLT NR 8015 - ORD - EMERGENCY LIGHT LEFT OVERWING EXIT IDENTIFIER IS OUT. MAINTENANCE RE-SEATED BATTERY CONNECTOR EMERGENCY LIGHTS TEST OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 17,393 hrs · 15,145 cycles

PRE FLT NR 8023 - TYS - EMERGENCY LIGHT GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE RESECURED CONNECTION GALLEY WALL EXIT LOCATOR, OPS CHECK GOOD.

Part: CONTACT — DIRTY (EXIT LIGHT) · airframe 17,265 hrs · 15,023 cycles

PRE FLT 7979 - OMA - LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE CLEANED THE CONTACTS AT THE SUBJECT LIGHT. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,242 hrs · 14,999 cycles

POST FLT NR 8025 - IAD - CEILING LIGHT INOP, EMERGENCY LIGHT AT ROW 16A. MAINTENANCE RELAMPED, OPS CHECK GOOD.

Part: SEAL — WORN (NR 2 ENGINE) · airframe 17,209 hrs · 14,968 cycles

FLT NR 7916 - ORD - E2 LOW OIL PRESSURE MESSAGE- QTY AT 3 QTS. MAINTENANCE REPLACED SEAL AT STARTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,003 hrs · 14,764 cycles

PRE FLT NR 8018 - STL - EMERGENCY LIGHT LEFTHAND OVERWING EXIT MARKER INOP. MAINTENANCE CYCLED POWER SYSTEM CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,872 hrs · 14,642 cycles

POST FLT NR 7961 - IAD - EMERGENCY LIGHT AISLE FLOOD LIGHTS AFT INOP. MAINTENANCE REMOVED AND REPLACED BULBS SYSTEM, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (SPOILER SYS) · airframe 16,810 hrs · 14,584 cycles

FLT NR 8000 - IAD - SPOILER FAIL & INTERMITTENT UNCOMMANDED SPOILER DEPLOYMENT DURING TAXI. MAINTENANCE CLEANED CONNECTOR ON SPOILERS AND WHEEL SPEED TRANSDUCER, ALL CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,795 hrs · 14,568 cycles

PRE FLT NR 7922 - DAY - EMERGENCY LIGHT FLOOR PROXIMITY AND AFT CEILING EXIT LOCATOR BOTH OVERWING EXIT IDENTIFIER ARE INOP. MAINTENANCE REMOVED AND REPLACED NR 3 BATTERY PACK SYSTEM, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,729 hrs · 14,503 cycles

PRE FLT NR 7900 - MKE - ALL EMERGENCY LIGHTS ARE INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,572 hrs · 14,347 cycles

PRE FLT NR 8018 - STL - EMERGENCY LIGHT INOP AT RIGHT ROW SIDE WALL POSITION. MAINTENANCE RESECURED CONNECTORS, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (CABIN) · airframe 16,568 hrs · 14,343 cycles

PRE FLT NR 8008 - IAD - LEFTHAND SIDE EXIT EMERGENCY LIGHT OVERWING EXIT MARKER INOP. MAINTENANCE CLEANED CONNECTOR AT INVERTER 4 & 5 SYSTEM, OPERATIONAL NORMAL.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 16,509 hrs · 14,285 cycles

POST FLT 7922 - IAD - EMERGENCY LIGHT LEFT HAND OVERWING EXIT MARKER INOP. MAINTENANCE RESET CONNECTION BEHIND EXIT LIGHTED SIGN, RETURN TO NORMAL OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 16,458 hrs · 14,231 cycles

PRE FLT NR 8010 - STL - EMERGENCY LIGHT AT LEFTHAND OVERWING EXIT MARKER IS INOP. MAINTENANCE CLEANED ELECTRICAL CONNECTION AND OPS CHECK GOOD AT THIS TIME.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 16,325 hrs · 14,102 cycles

PRE FLT NR 8022 - STL - LEFT EMERGENCY OVERWING EXIT MARKER LIGHT INOP. MAINTENANCE RESCURED LEFT EMERGENCY LIGHT CONNECTOR, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 19,809 hrs · 17,512 cycles

PRE FLIGHT NR 5505-STL-EMERGENCY LIGHT ON FLOOR NEAR EXIT INOP. MAINTENANCE CLEANED THE CONNECTION ON THE FLOOR PATH LIGHTING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,930 hrs · 12,750 cycles

PRE FLIGHT 8022 - STL - ROWS 1 THROUGH 5 FLOOR TRACK EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK.

Part: WIRE — LOOSE (CABIN) · airframe 14,780 hrs · 12,601 cycles

MX - RIC - EMERGENCY PATH LIGHTS INOP. RE-SECURED LOOSE WIRE TO PATH LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,651 hrs · 12,474 cycles

PRE FLIGHT 8043 - RIC - AFT CABIN EMERGENCY LIGHTS DO NOT COME ON. MAINTENANCE CYCLED THE POWER TO THE EMERGENCY LIGHTING SYSTEM. OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 14,221 hrs · 12,085 cycles

FLT - 8039 - ORD - BAGGAGE DOOR OPEN INDICATION DURING T/O RUN. MAINTENANCE DEFERRED BAGGAGE DOOR WARNING SYSTEM PER MEL.

Part: BULB — LOOSE (CABIN LIGHTS) · airframe 13,546 hrs · 11,439 cycles

FLT 8068 - ORD - F/A REPORTED BURNING WIRE SMELL AND HEARD POPPING NOISE OVER SEAT 1A. MAINTENANCE INSPECTED AND RESECURED LOOSE BULB AT SEAT 1A.

Part: LIGHT — MALFUNCTIONED (OVERWING) · airframe 13,282 hrs · 11,180 cycles

PRE FLT 7966 - IAD - OVERWING EMERGENCY LIGHTS ON INSIDE OF AIRCRAFT AS WELL AS OUTSIDE OVERWING EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN ALL POWER IS REMOVED FROM THE AIRCRAFT AND TOGGLE SWITCH IS IN THE OFF POSITION. MAINTENANCE OPS CHECKED THE SYSTEM WITH NO DEFECTS NOTED.

Part: CONTROL HANDLE — INOPERATIVE (NLG STEERING) · airframe 12,343 hrs · 10,269 cycles

FLT NR 8018 - STL- WHILE MAKING LEFT TURN, STEERING INOP MESSAGE DISPLAYED ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE STEERING CONTROL HANDLE. OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG) · airframe 10,901 hrs · 8,913 cycles

8003- ORD- NOSE WHEEL STEERING PULLED HARD RIGHT. REMOVED AND REPLACED 7 DEGREE PROX SWITCH.

Part: SOLENOID — DEFECTIVE (RUDDER GUST LOCK) · airframe 8,948 hrs · 7,137 cycles

GUST LOCK WILL NOT DISENGAGE. MAINTENANCE DEFERRED SYSTEM IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE RUDDER GUST LOCK SOLENOID.