N577AA

Part: SENSOR — INOPERATIVE (STALL WARNING) · airframe 61,509 hrs · 31,732 cycles

DFW - CREW REPORTED DURING TAKEOFF V1 STALL INDICATION FAILURE LIGHT, SLAT DISAGREE LIGHT AND WARNING HORN CAME ON. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ANGLE OF ATTACK VANE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PUMP — FAILED (LT ENGINE) · airframe 61,216 hrs · 31,560 cycles

DFW - CREW REPORTED LEFT HYDRAULIC HIGH TEMPERATURE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,085 hrs · 30,400 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. REPLACED EMERGENCY BATTERY PACK AT ROW 7DEF. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,529 hrs · 30,088 cycles

EMERGENCY LIGHTS FROM ROWS 28 TO 30 AND IN THE TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERIES FOR AFT CABIN AND TAIL COMPARTMENT AREA EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

AFT CARGO CORROSION LEFT TIE DOWN TRACK STATIONS 1007 TO 1212. INSTALLED TRACK SPLICE PER AARD 51-10-0-5.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CORROSION AFT SIDE FRAME STATION 1250 LONGERON 29 LEFT TO 29 RIGHT. INSTALLED FRAME SPLICE PER EA MD80-53-014022.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,728 hrs · 29,077 cycles

STATION 1418 FRAME CRACKED BETWEEN LONGERON 2 RIGHT AND LEFT. ACCOMPLISHED SPLICE REPAIR PER EA MD80-53-011681.

Part: ATTACH FITTING — DAMAGED (FUSELAGE) · airframe 56,728 hrs · 29,077 cycles

FLOORBEAM ATTACH FITTING (CASTING) AT STATION 294 LEFT UNDER NUMBER 1 SEAT FLOORBEAM ATTACH FITTING (CASTING) AT STATION 294 LEFT UNDER NUMBER 1 SEAT TRACK HAS DAMAGE ON UPPER AFT SIDE FLANGE. INSTALLED FLOORBEAM FITTING AT STATION 294 LEFT SRM 51-30-05 AND EA MD80-53-014038.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,728 hrs · 29,077 cycles

AFT CARGO - INTERCOSTAL CRACKED, BELOW CABIN FLOOR ON CENTER LINE, STATION 1271 TO 1287. REPLACED INTERCOSTAL PER AARD 51-10-00-5.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,728 hrs · 29,077 cycles

HOLE IN LEFT CUSP STATION 294. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CORROSION ON LEFT CUSP AT NUMBER 1 SEAT TRACK, STATIONS 1174 TO 1178. INSTALLED NEW CUSP SHEET, LEFT SIDE, BETWEEN NUMBER 1 AND NUMBER 2 SEAT TRACKS, STATIONS 1174 TO 1250 PER AARD 53-20-00-16 AND AARD 51-10-00-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,728 hrs · 29,077 cycles

AFT CARGO - INTERCOSTAL CRACKED, BELOW CABIN FLOOR ON CENTER LINE, STATION 1287 TO 1309. REPLACED INTERCOSTAL PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CORROSION ON THE LEFT CUSP UNDER THE AFT SERVICE DOOR AFT GIRT BAR SUPPORT BRACKET AT STATION 1168. LEFT CUSP UNDER AFT SERVICE DOOR AFT GIRT BAR SUPPORT BRACKET AT STATION 1168 WAS REPAIRED WITH DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CORROSION ON LEFT CUSP UNDER AFT SERVICE DOOR, FORWARD GIRT BAR BRACKET, STATION 1140. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

LOWER SUPPORT ANGLE AT STATION 1155 OUTBOARD OF DOOR BEAM IS CORRODED. BLENDED AND REMOVED CORROSION PER SRM 51-10-03. CORROSION OUT OF LIMITS PER SRM 53-01-00. REMOVED DAMAGED ANGLE AND INSTALLED A NEW ONE PER AARD 51-10-00-5. TREATED AND PRIMED PER SRM 51-10-03.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

AFT CARGO HAS CORROSION ON VERTICAL CORNER BRACKET IN DOOR OPENING AT STATION 1155 NEXT TO LOWER BEAM. BLENDED AND REMOVED CORROSION PER SRM 51-10-03 FOUND TO BE OUT OF LIMITS PER SRM 53-01-00. REMOVED DAMAGED CLIP AND REPLACED WITH A NEW ONE PER AARD 51-10-00-5. TREATED AND PRIMED PER SRM 51-10-03.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 56,728 hrs · 29,077 cycles

AFT CARGO DOOR FORWARD LOWER SUPPORT STRAP INTERCOSTAL IS CRACKED. DWMS NR1440044, MRT 028756, INSTALLED NEW SUPPORT STRAP INTERCOSTAL PER ESO 80174.

Part: SKIN — DENTED (CARGO DOOR) · airframe 56,728 hrs · 29,077 cycles

OUTER SKIN ON AFT CARGO DOOR (AAID BBDPZCR) HAS DENT APPROXIMATELY 10 INCHES FROM AFT EDGE BETWEEN NUMBER 3 AND 4 BEAMS. BLENDED AREA OF DENT TO REMOVE SHARP EDGES. DYE CHECKED DENTED AREA AND FOUND NO CRACK INDICATIONS. FABRICATED AND INSTALLED INTERNAL REPAIR DOUBLER WET WITH B-1422 SEALANT MADE FROM .032 2024-T3 MATERIAL PER SRM 53-04-00 FIGURE 38 SHEET 21.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,728 hrs · 29,077 cycles

CUSP SHEET CRACKED AT RIGHT HAND STATIONS 218 TO 223 UNDER SEAT TRACK NUMBER 6. INSTALLED SERVICEABLE CUSP SHEET FROM STATIONS 218 TO 237 RIGHT PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

STATIONS 512 TO 513 LEFT CUSP HAS CORROSION. DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

STATION 460 RIGHT CUSP HAS CORROSION. DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

LEFT CUSP STATIONS 488 TO 500 CORROSION OUT OF LIMITS. CUT OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CORROSION ON LEFT CUSP STATIONS 989 TO 992. ROUTED OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CORROSION ON UPPER SURFACE OF SUBFLOOR, STATIONS 160 TO 162, RIGHT BUTTLINES 10 TO 12. CUT OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,728 hrs · 29,077 cycles

LEFT WINDOW PAN CRACKED AT AFT UPPER CORNER STATION 845. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,728 hrs · 29,077 cycles

CABIN LEFT WINDOW PAN CRACKED AT AFT UPPER CORNER STATION 946. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,728 hrs · 29,077 cycles

CABIN LEFT WINDOW PAN CRACKED AT FORWARD UPPER CORNER STATION 1079. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,728 hrs · 29,077 cycles

LEFT WINDOW PAN CRACKED AFT LOWER CORNER STATION 984. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CABIN - SUBFLOOR CORRODED STATIONS 200 TO 202 FORWARD OF NUMBER 6 SEAT TRACK. INSTALLED SUBFLOOR DOUBLER FROM STATIONS 200 TO 218 RIGHT PER AARD 53-20-00-16.

Part: DOOR — BENT (ENTRY DOOR) · airframe 56,728 hrs · 29,077 cycles

FORWARD ENTRY DOOR PAN IS BENT AT UPPER HINGE CUTOUT. RELACED DOOR PAN FRAME PER ESO 80172.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

CABIN - SUBFLOOR CORRODED STATIONS 205 TO 213 FORWARD OF NUMBER 6 SEAT TRACK. INSTALLED SUBFLOOR DOUBLER FROM STATIONS 200 TO 213 RIGHT PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,728 hrs · 29,077 cycles

LEFT WINDOW PAN CRACKED FORWARD LOWER CORNER STATION 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,728 hrs · 29,077 cycles

SUBFLOOR BELOW G-1 GALLEY DRAIN PAN CORRODED AROUND DRAIN LINE ATTACH AREA. INSTALLED DOUBLER UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,429 hrs · 28,915 cycles

FRAME CRACKED AFT SIDE 1418 LONGERON 2 RIGHT. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-15.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 56,401 hrs · 28,903 cycles

DFW - DURING CLIMBOUT WITH ENGINE PRESSURE RATIO AT 1.8 LEFT ENGINE POWER FELL OFF AND TEMPERATURE SPIKED. WHILE PERFORMING QHR PROCEDURE POWER SUDDENLY CAME BACK UP AND TEMPERATURE DROPPED TO NORMAL. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT HAND ENGINE AT DFW ON 09/13/10. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,337 hrs · 27,789 cycles

EMERGENCY LIGHTS AT SEAT ROWS 3 TO 15 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: SWITCH — FAILED (COCKPIT) · airframe 54,325 hrs · 27,781 cycles

CREW REPORTED RED NOSE LIGHT STAYED ON DURING CLIMB. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. THREE GREEN LIGHTS FOR LANDING. REPLACED LANDING GEAR HANDLE SWITCH 51-89.

Part: UPLOCK SENSOR — FAULTY (NLG) · airframe 54,324 hrs · 27,780 cycles

CREW REPORTED GEAR HANDLE UP NOSE GEAR RED LIGHT INDICATION AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED THE LOCK SENSOR ON NOSE LANDING GEAR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,150 hrs · 27,141 cycles

THE J-BEAM AT LEFT SIDE STATION 46 LONGERON 26 LEFT IS CRACKED AT FASTENER HOLE IN DOUBLER. REMOVED AND REPLACED J-ANGLE DOUBLER AT STATION 46 LONGERON 26 LEFT PER AARD 53-10-00-4.

Part: SELECTOR — INOPERATIVE (CABIN PRESSURE) · airframe 52,867 hrs

CREW REPORTED CABIN LOST PRESSURIZTION. LANDED STL WITHOUT INCIDENT. FOUND NR 1 PRESSURE CONTROL INOPERATIVE. REPLACED NUMBER ONE CABIN PRESSURE CONTROLLER AND NR 1 AND 2 CABIN PRESSURE SELECTOR. MPN 1304768. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: SEAL — FAILED (NLG STRUT) · airframe 52,793 hrs

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. HAD A RED NOSE GEAR LIGHT AND A FLUSH INDICATOR. RETURNED SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STRUT SEALS AND SERVICED NOSE LANDING GEAR STRUT. REMOVED AND REPLACED D1-31 NOSE GEAR POSITION UP SENSOR AND P1-1156 CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: CONTROL BOX — INOPERATIVE (ANTI-SKID SYS) · airframe 52,712 hrs · 26,895 cycles

ONT - ANTI-SKID LIGHT ILLUMINATED. EMERGENCY DECLARED LANDED ONT WITHOUT INCIDENT. REMOVED AIRCRAFT FROM SERVICE. REPLACED ANTI SKID CONTROL BOX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 52,501 hrs

LGA - CEILING EMERGENCY LIGHTS FOR ROWS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18 TO 21.

Part: TIE BOLT — BROKEN (MLG WHEEL)

DFW INFLIGHT - AFTER TAKEOFF AT MEM FLIGHT ATTENDANT REPORTED STRONGER THAN NORMAL RUBBER ODOR AND UNUSUAL VIBRATION COMING FROM THE LEFT MAIN TIRE AND WHEEL WELL AREA. CREW REPORTED NO INDICATIONS IN COCKPIT. ALL BRAKE TEMPERATURES NORMAL. LANDED DFW WITHOUT INCIDENT. TAXIED TO GATE. FOUND BROKEN TIE BOLT ON NUMBER ONE MAIN WHEEL. REPLACED NUMBER ONE TIRE WHEEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS) · airframe 49,422 hrs

DFW - EMERGENCY LIGHT AT SEAT 8D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS) · airframe 49,422 hrs

DFW - EMERGENCY LIGHT AT SEAT 30D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE SWITCH — INOPERATIVE (RT ENGINE OIL)

DFW - INFLIGHT ON APPROACH RIGHT ENGINE CLOGGED STRAINER INDICATION ILLUMINATED. CREW PERFORMED IN FLIGHT SHUTDOWN. LANDED DFW WITHOUT INCIDENT. ALL CHECKS NORMAL. INSTALLED NEW FILTER AND OIL FILTER DIFFERENTIAL PRESSURE SWITCH. DRAINED AND REPLENISHED OIL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FUEL CONTROL — INOPERATIVE (LT ENGINE)

ORD - LEFT ENGINE SHUT DOWN ON APPROACH APPROXIMATELY 30 DEGREES BANK, 1.5 DEGREES NOSE DOWN, FLIGHT IDLE POWER, 160 KNOTS. REPLACED LEFT ENGINE FUEL CONTROL AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - EMERGENCY LIGHT IN CEILING AT ROWS 23 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR EMERGENCY LIGHT IN CEILING AT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - CEILING EMERGENCY LIGHTS AT STATION 1209L INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-107 FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HARNESS — DAMAGED (ESCAPE SLIDE)

DFW SECURITY ISSUE. AIRCRAFT RETURNED TO STATION. UPON LANDING TAIL CONE WAS DROPPED BUT EMERGENCY EVACUATION SLIDE DID NOT DEPLOY. FOUND SLIDE PROPERLY CONNECTED TO COVER. TAB SNAP BUTTON ON TAIL CONE LANYARD DAMAGED. WOULD NOT SNAP TO COVER. LANYARD ATTACHED TO COVER BY VELCRO ONLY. REPLACED SLIDE, TAIL CONE AND LANYARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DFW FORWARD ENTRY AISLE GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD ENTRY AISLE GALLEY OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (COCKPIT)

DFW COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY FOR COCKPIT OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (A/C BAY)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — FAILED (RT ENGINE)

DFW - FLT 389 - DFW-ABQ - EN ROUTE RT HYD PRESSURE LIGHT ILLUMINATED AND RIGHT HYD PRESSURE INDICATOR WENT TO ZERO. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT TAIL OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED AFT TAIL OVERHEAD EMERGENCY EXIT ILGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MOUNT — CORRODED (FUSELAGE)

TUL - FOUND STATION 218 G2 INBOARD FLOOR TIEDOWN HAS CORROSION. REPAIRED G2 INBOARD FLOOR TIEDOWN PER AARD 53-00-00-02. (M)

Part: MOUNT — CORRODED (FUSELAGE)

TUL - FOUND STATION 212, G2 INBOARD FLOOR TIE DOWN HAS CORROSION. REMOVED AND REPLACED G2 FLOOR TIE DOWN STATION 212. (M)

Part: PAN — CRACKED (FUSELAGE)

TUL - FOUND FLOOR PAN CRACKED. INSTALLED DOUBLER PER SRM 51-10-3. (M)

Part: BRACKET — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, G1 FORWARD CENTER FLOOR TIE DOWN. REMOVED AND REPLACED TIE DOWN BRACKET. (M)

Part: MOUNT — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, G1 FORWARD INBOARD FLOOR TIE DOWN. REMOVED AND REPLACED TIE DOWN. (M)

Part: BELTFRAME — WORN (FUSELAGE)

TUL - FOUND GROOVE WORN INTO BELTFRAME, STATION 1418 AT L18R. BLENDED OUT DAMAGE PER SRM 53-01. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-14. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED AFT STATION 1287 INBOARD OF NR 1 SEAT TRACK. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - AFT CARGO DOOR BEAM HAS CORROSION ON HORIZONTAL AND VERTICAL LEGS FROM STATION 1155-1212. BLENDED OUT CORROSION PER SRM 51-10-03. INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-16. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK AFT STATION 1250 CORRODED TOP SIDE OUTBOARD FLANGE. INSTALLED STRAP ON NR 1 SEAT TRACK AFT STATION 1250 PER AARD 53-20-00-13. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AT FASTENER HOLE STATION 1338. INSTALLED DOUBLER AND FILLER SRM 53-05 FIG 20A. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND WINDOW PANEL FRAME CRACKED AT FORWARD LOWER CORNER. TRIMMED OUT CRACK. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: WEB — TORN (FUSELAGE)

TUL - FOUND CUSP TORN STATION 218 FORWARD OF NR 4 SLAT IN CABIN. REPLACED CUSP DIAPHRAGM PER 53-00-00-13. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND SUBFLOOR UNDER G1 GALLEY HAS CORROSION. SUBFLOOR UNDER G1 GALLEY IS SCRATCHED, GOUGED, AND DENTED. REMOVED CORROSION. FABRICATED AND INSTALLED DOUBLER PER AARD 53-00-00-02. BLENDED OUT DAMAGE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND CORROSION RIGHT WINDOW PANEL FRAME CRACKED FS 1041 AT FORWARD LOWER CORNER. TRIMMED OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT PATH LIGHT FROM SEAT 20D AFT INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: O-RING — FAILED (APU)

BOS - FLT 1835 - EN ROUTE BOS-DFW, AFTER TAKEOFF A HOT MISTY ODOR WAS PRESENT IN COCKPIT FOLLOWED BY FLIGHT ATTENDANTS REPORTING SMOKE FILLING THE CABIN, SOME IN COCKPIT, FLIGHT ATTENDANTS REPORTED SMOKE WAS ORIGINATING AROUND ROWS 17 AND 18. DECLARED EMERGENCY, RETURNED TO TO BOS AND LANDED WITHOUT INCIDENT. SMOKE DISSIPATED DURING DESCENT AND LANDING. TAXI TO GATE WAS UNEVENTFUL. REPLACED APU O-RING AT MAGNETIC DRAIN PLUG. REPLACED LEFT COALESCERS BAG. ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — OUT OF ADJUST (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 22 THROUGH 26 INOPERATIVE. ADJUSTED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN SIDEWALL OF TAIL STAIRS INOPERATIVE. REPAIRED WIRE FOR EMERGENCY LIGHTS IN SIDEWALL OF TAIL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 8 INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT LIGHT AT ROW 8. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: STRUT — LOW (NLG)

DFW - FLT 865 - EN ROUTE DFW-SJD - DURING GEAR RETRACTION AFTER TAKEOFF NOSE GEAR RED LIGHT REMAINED ON AND AMBER DOOR OPEN LIGHT REMAINED ILLUMINATED. RECYCLED GEAR WITH NO RESULT. RETURNED DFW LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR WITH HYDRAULIC FLUID AND NITROGEN. PERFORMED RETRACTION AND EXTENSION CHECK. ALL CHECKS NORMAL WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 10D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 2D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 11D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 14D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPEATION. (M)

Part: SENSOR — DEFECTIVE (NLG)

DFW - FLT 0641 - EN ROUTE EWR/DFW, RED NOSE GEAR LIGHT ILLUMINATED IN CLIMB PASSING 18,000 FEET. ACCOMPLISHED ABNORMAL PROCEDURES WITH NO EFFECT. LIGHT EXTINGUISHED 15 MINUTES LATER AT 28,000 FEET. LANDED DFW WITHOUT INCIDENT. REPLACED UP/DOWNLOCK SENSOR ON NOSE GEAR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FRAME — BENT (CARGO DOORWAY)

TUL - FOUND ON THE AFT CARGO DOOR APPROX 7 O'CLOCK POSITION FUSELAGE SKIN OUTER FRAME BENT. INSTALLED DOUBLER PER SRM 53-05 AND ESO80559. (M)

Part: EEL CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 30 AND 33 INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)