N961TW

Part: LIGHT — INOPERATIVE (AFT STAIR) · airframe 52,759 hrs · 26,427 cycles

FORWARD LOWER AFT STAIR PANEL EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIR LEFT SIDE EMERGENCY LIGHT ASSEMBLY PER AMM 33-53-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,383 hrs · 26,197 cycles

THE AIRCRAFT WAS IN BASE MAINTENANCE. RIGHT HAND SHEAR TIE CRACKED AT STATION 1380 L13R. REPAIRED SHEAR TIE PER 53-10-00-20.

Part: RELAY — OVERHEATED (ZONE 100) · airframe 51,753 hrs · 25,807 cycles

THE AIRCRAFT WAS GROUNDED. FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL BURNING SMELL AT APPROXIMATELY ROW 7. SMELL REPORTED COINCIDENT WITH A/P. FOUND AIRCRAFT NOSE UP BRAKE CONTROL RELAY OVERHEATED. REPLACED RELAY R20-18. OPERATIONS CHECK OK PER AMM 27-40-03.

Part: FLASHLIGHT — INOPERATIVE (GALLEY) · airframe 50,801 hrs · 25,177 cycles

GALLEY FLASH LIGHT WAS NOT BLINKING. REMOVED AND REPLACED THE FLASHLIGHT AND OPS CHECKED NORMAL IAW GPM 25-60-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 50,347 hrs · 24,898 cycles

THE AIRCRAFT WAS NOT GROUNDED. L1 F/A FLASHLIGHT NEAREST TO AISLE DOES NOT INDICATE FROM LED LIGHT. REMOVED AND REPLACED FWD ENTRY FLASHLIGHT IAW AMM 25-60-00 OPS CHECK NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,044 hrs · 24,079 cycles

EMERGENCY EXIT LIGHTS BATTERY B5-101 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,044 hrs · 24,079 cycles

EMERGENCY EXIT LIGHTS BATTERY B5-107 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: FITTING — CRACKED (LT WING) · airframe 49,044 hrs · 24,079 cycles

CRACK ON LEFT WING GROUND SPOILER FITTING FORWARD SUPPORT LEG AND INBOARD TRAILING EDGE AT WING STATION 91.01 TO 99.01. REMOVED AND REPLACED GROUND SPOILER FITTING IAW AARD 51-11-05 AND SRM 51-30-02.

Part: FITTING — CRACKED (RT WING) · airframe 49,044 hrs · 24,079 cycles

CRACK ON RIGHT WING GROUND SPOILER ACTUATOR SUPPORT AT FORWARD INBOARD CORNER AT WING STATION 99.01 TO 91.15. REMOVED AND REPLACED GROUND SPOILER FITTING IAW 51-00-05 AND SRM 51-30-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,559 hrs · 23,128 cycles

AIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER ESCAPE PATH LIGHTING, BETWEEN ROWS 3 & 19 IS INOPERATIVE. R & R BATTERY ASSEMBLY AT FWD CABIN X LOCATION IAW AMM 33-60-98. SYS CHECKED NORMAL. SEE ALSO AALA 20160421008.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,559 hrs · 23,128 cycles

AIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER ESCAPE PATH LIGHTING, BETWEEN ROWS 3 & 19 IS INOPERATIVE. R & R BATTERY ASSEMBLY AT MID-CABIN W LOCATION IAW AMM 33-60-98. SYS CHECKED NORMAL. SEE ALSO AALA 20160421007.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 47,031 hrs · 22,831 cycles

EMER LIGHTS FROM ROW 28 - 32 FAILED TO TEST. REPLACED B5-107 EMER LIGHT BATTERY PACK IAW AMM 33-53-00. TESTED OK. THE ACFT WAS NOT GNDED.

Part: UFI — FAULTY (FUEL SYSTEM) · airframe 46,667 hrs · 22,613 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB THE CTR FUEL PRESS LOW LIGHT ILLUMINATED WITH 6,400 LBS OF FUEL IN THE CTR. R & R THE CTR UFI TOP ASSEMBLY & RAM CTR TOP ASSEMBLY IAW AMM 28-20-28. SYS CHECKED NORMAL. SEE ALSO AALA20111005.

Part: FUEL SYS — FAULTY (ZONE 100) · airframe 46,667 hrs · 22,613 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMERGENCY NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB THE CTR FUEL PRESS LOW LIGHT ILLUMINATED WITH 6,400 LBS OF FUEL IN THE CTR. R & R THE CTR UFI TOP ASSEMBLY & RAM CTR TOP ASSEMBLY IAW AMM 28-20-28. SYS CHECKED NORMAL. SEE ALSO AALA20151210008.

Part: UFI — TRIPPED (ZONE 100) · airframe 46,120 hrs · 22,273 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, CTR FUEL PRESS LOW LIGHT ILLUMINATED. COMPLETED QRH PROCEDURE. CTR FUEL WOULD NOT FEED. FOUND CTR AFT BOOST PUMP UFI TRIPPED, STATUS CODE 35. ACCOMPLISHED UFI FAULT ISOLATION PROCEDURE IAW AMM 28-20-28-201 & TROUBLE SHOOTING 28-20-07. BOOST PUMP & WIRING CHECKED OKAY. UFI RESET OKAY. CTR BOOST PUMPS OPERATIONAL CHECKED OKAY.

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM) · airframe 45,946 hrs · 22,168 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB CTR PRESS LOW LIGHT CAME ON WITH 5900 LBS OF FUEL IN CTR TANK. ACCOMPLISHED ADJUSTMENT TEST RESET ON UNIVERSAL FAULT INTERRUPTER FOR CTR TANK IAW AMM 28-20-28. OPERATIONAL CHECKED GOOD.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,818 hrs · 22,077 cycles

FORWARD CARGO DOOR PAN IS CORRODED ON VERTICAL & HORIZONTAL FLANGES AT STRINGER 26R BETWEEN FUSELAGE STATINS 370 & 427. SPLICED IN NEW SECTION OF PAN IAW SRM 53-05-00 & EA 253062.

Part: FLOORBEAM — WORN (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

FLOORBEAM AT STATION 389 & RBL 1 HAS WORN AREA DUE TO CONTACT WITH BARRIER DOOR. REPAIRED FLOORBEAM IAW AARD 53-20-00-21.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON RT CUSP SHEET BETWEEN 389 & 503. REPLACED RT CUSP SHEET BETWEEN 389 & 503.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON G1 GALLEY MOUNT AT STATION 160. REPLACED G1 GALLEY MOUNT AT STATION 160.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON NR 4 SEAT TRACK BETWEEN STATION 200 & 265. REPLACED NR 4 SEAT TRACK BETWEEN STATION 200 & 265.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON NR 5 SEAT TRACK BETWEEN STATION 200 & 265. REPLACED NR 5 SEAT TRACK BETWEEN STATION 200 & 265.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON NR 6 SEAT TRACK, BETWEEN STATION 218 & 588. REPLACED NR 6 SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON NR 6 SEAT TRACK, BETWEEN STATION 797 & 1088. REPLACED NR 6 SEAT TRACK.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,818 hrs · 22,077 cycles

CORROSION ON AFT CARGO TIE DOWN TRACK, BETWEEN STATION 1250 & 1322 AT STRINGER 27 LT. REPLACED AFT CARGO TIE DOWN TRACK.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON RT CUSP SHEET BETWEEN STATION 1163 & 1164. REPAIRED RT CUSP SHEET BETWEEN STATION 1163 & 1164 IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

CORROSION ON RT CUSP SHEET BETWEEN STATION 360 & 389. REPAIRED RT CUSP SHEET BETWEEN STATION 360 & 389 IAW AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,818 hrs · 22,077 cycles

AFT CARGO COMPARTMENT RT TIE DOWN TRACK AT LONGERON 27R IS CORRODED AT FS 1220. R & R TIE DOWN TRACK SECTION BETWEEN STATIONS 1212 & 1322 IAW SRM 51-30-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

FUSELAGE SKIN CRACK AT CANT FRAME STATION 1474, LT SIDE, 15" BELOW RAIN GUTTER. INSTALLED DOUBLER REPAIR IAW AARD 53-30-00-4 & SRM 53-01-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

LONGERON 20R CRACKED OTBD OF RT WW, FUSELAGE STATION 993. INSTALLED DOUBLER ON LONGERON 20R IAW AARD 53-10-00-18.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

RIGHT CUSP CORRODED BETWEEN FS 200 & 207. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,818 hrs · 22,077 cycles

CORROSION ON RT CUSP AT STATION 218. REPLACED RT CUSP BETWEEN STATION 218 & 237.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

SKIN CRACK AT FS 1474 RT SIDE, 15" BELOW RAIN GUTTER. ACCOMPLISHED DOUBLER REPAIR IAW AARD 53-30-00-4 & SRM 53-01-00-001.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

LEFT CUSP CORRODED BETWEEN FS 473 & 477. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

RIGHT CUSP OTBD OF NR 6 SEAT TRACK CORRODED & CRACKED AT FS 1125 TO 1126 AT LIGHTING HOLE. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

LEFT CUSP IS CORRODED AT FS 840. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,818 hrs · 22,077 cycles

FUSELAGE SKIN CRACKED AT STATION 1380 & LONGERON 14L. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW SRM 53-01-00-001.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,396 hrs · 20,707 cycles

CRACK IN FUSELAGE SKIN AT STATION 1474 LT SIDE 7 O CLOCK POSITION LOOKING FWD. STOP DRILLED CRACK & INSTALLED DOUBLER IAW SRM 53-01-00-001 FIGURE 2 SHEET 3.

Part: FORMER — CRACKED (LT WING) · airframe 43,041 hrs · 20,520 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-05 & EA MD80-57-035064.

Part: FORMER — CRACKED (RT WING) · airframe 43,041 hrs · 20,520 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMED IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-06 & EA MD80-57-035064.

Part: WIRE — DAMAGED (CABIN) · airframe 41,387 hrs · 19,624 cycles

POWER SUPPLY AB5-1 WILL NOT POWER FORWARD SEAT EGRESS LIGHTS. REPAIRED WIRING WITH SPLICE AT SIDEWALL FEED THROUGH AT SEAT 4DEF. OPERATIONS CHECKED NORMAL.

Part: LANYARD — FRAYED (GIRT BAR) · airframe 41,387 hrs · 19,624 cycles

LT NR 1 DOOR SLIDE GIRT BAR LANYARD FRAYED. REPLACED LANYARD.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,387 hrs · 19,624 cycles

FWD OVERWING INTERIOR EXIT LIGHTS INOPERATIVE. REPLACED B5-103 BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: PORTABLE LIGHT — FAILED (CABIN) · airframe 41,387 hrs · 19,624 cycles

LT NR 1 DOOR PORTABLE EMERGENCY LIGHT FLICKERS DURING TEST. REPLACED LT NR 1 DOOR PORTABLE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 39,147 hrs · 18,448 cycles

LONGERON 2 RIGHT CRACKED AFT OF STATION 1418. INSTALLED DOUBLER REPAIR PER SRM 53-02-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,147 hrs · 18,448 cycles

SKIN CRACKED AT SHEAR TIE FASTENER AT STATION 1380 BETWEEN LONGERONS 13 AND 14 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 35,595 hrs · 16,610 cycles

DFW - CREW REPORTED RIGHT ENGINE GENERATOR FAILED AND UNABLE TO START AUXILIARY POWER UNIT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 35,260 hrs · 16,419 cycles

CRACK IN RIGHT CUSP AT STATION 1234. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,260 hrs · 16,419 cycles

RIGHT CUSP STATION 1064 CORRODED BEYOND LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,260 hrs · 16,419 cycles

CRACK IN RIGHT CUSP AT STATION 1293. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,260 hrs · 16,419 cycles

AFT ACCS 1463 CANT FRAME WEB CRACKED ABOVE LEFT LOUVER BOX. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIGURE 38 AND EA MD80-53-018063 DATED 7-14-2011.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 35,260 hrs · 16,419 cycles

DENT AT APPROXIMATE STATION 340 AND LONGERON 23 LEFT. INSTALLED DOUBLER REPAIR PER SG09530002 CLASS I REPAIR.

Part: LONGERON — BENT (FUSELAGE) · airframe 35,260 hrs · 16,419 cycles

LONGERON 24 LEFT STATION 320 BENT IN RADIUS. REPAIRED LONGERON 24 LEFT STATION 320 PER SRM 53-02-00 FIGURE 18.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,260 hrs · 16,419 cycles

RIGHT CUSP STATION 1064 CORRODED BEYOND LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,260 hrs · 16,419 cycles

SEAT TRACK LUG CORROSION OUT OF LIMITS AT STATIONS 1195 TO 1196. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,260 hrs · 16,419 cycles

CORROSION ON RIGHT CUSP, BOTTOM SIDE, STATIONS 753 TO 757. CUT OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,260 hrs · 16,419 cycles

CORROSION LEFT CUSP BOTTOM SIDE STATIONS 608 TO 613. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,260 hrs · 16,419 cycles

FORWARD CARGO AT STATION 450 RIGHT CUSP HAS CORROSION. REMOVED CORROSION AND INSTALLED FABRICATED DOUBLER PER AARD 53-20-00-16. TREATED AND PRIMED PER SRM 51-10-3.

Part: PAN — CRACKED (WINDOW) · airframe 35,260 hrs · 16,419 cycles

LEFT HAND, STATION 1022 LOWER AFT WINDOW PAN EAR IS CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,260 hrs · 16,419 cycles

WEB CRACKED STATION 207, LONGERON 15 LEFT. INSTALLED STRAP AT STATION 207 LONGERON 15 PER AARD 53-10-00-11.

Part: PAN — CRACKED (WINDOW) · airframe 35,260 hrs · 16,419 cycles

RIGHT STATION 826 UPPER AFT WINDOW PAN EAR IS CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,260 hrs · 16,419 cycles

CORROSION AT SUB-FLOOR, STATIONS 184 TO 191 AT FORWARD ENTRY THRESHOLD AREA. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DUCT — CRACKED (AC BAY) · airframe 34,987 hrs · 16,266 cycles

DEN - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PNEUMATIC DUCT ON RIGHT SIDE OF TAIL COMPARTMENT CRACKED. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — FAULTY (OUTFLOW VALVE) · airframe 33,137 hrs · 15,359 cycles

DFW - CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. AT 8000 FEET AFT GALLEY DOOR LIGHT ILLUMINATED. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OUTFLOW VALVE ACTUATOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DIRTY (CABIN) · airframe 32,695 hrs · 15,156 cycles

ON OVERNIGHT INSPECTION OF EMERGENCY LIGHT SYSTEM, IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 28 AFT TO TAIL CONE COMPARTMENT. CLEANED AND RE-SEATED BATTERY PACKS AT ROW 31 AND IN RIGHT AFT LAVATORY. OPS CHECKED NORMAL.

Part: CABLE — FRAYED (TAILCONE) · airframe 31,483 hrs · 14,576 cycles

LEFT LOWER TAIL CONE LATCH LEVER CABLE FRAYED. REMOVED AND REPLACED AND RIGGED CABLE PER AMM 53-53-00-5 6 AND PATTERN CARD AD 5918 MPN 3913359-545 PER IPC 53-50-00-25A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,483 hrs · 14,576 cycles

CRACKED SHEAR TIE AT STATION 1401 LONGERON 15 LEFT. REPLACED SHEAR TIE PER SRM 53-01.

Part: FAN BLADE — DAMAGED (RT ENGINE) · airframe 29,943 hrs · 13,926 cycles

AT 1100" AGL BIRD STRIKE RIGHT ENGINE. INITIAL EPR DROP OF .60, RECOVERED AFTER DELAY OF 10 SECONDS (COMPRESSOR STALL). SMOOTH OVERWEIGHT LANDING AT 152,500. ENGINE WAS OPERATED AT IDLE. PRELIMINARY VISUAL 13 FAN BLADES BENT/DAMAGED. INSPECTION TO COMPLETE BORESCOPES TO EVALUATE ENGINE STATUS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,491 hrs

ORD - EMERGENCY LIGHTS FAIL TO OPERATE FROM THE FLIGHT DECK. REPLACED BATTERY PACK.

Part: BATTERY — UNSECURE (CABIN) · airframe 29,475 hrs

LGA - OVERHEAD EMERGENCY LIGHTS FROM SEAT 4 TO 6 INOPERATIVE. RESECURED BATTERIES IN BATTERY PACK AT ROW 4.

Part: BATTERY — LOOSE (CABIN) · airframe 29,475 hrs

LGA - CEILING EMERGENCY LIGHTS FROM ROW 28 TO AFT VENTRAL DOOR INOPERATIVE. RESECURED LOOSE BATTERIES AT ROW 29 FOR EMERGENCY LIGHTS.

Part: BATTERY — UNSECURE (CABIN) · airframe 29,475 hrs

LGA - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESECURED BATTERIES IN BATTERY PACKS.

Part: REGULATOR VALVE — FAILED (CABIN PRESSURE) · airframe 28,382 hrs · 13,268 cycles

ORD INFLIGHT - CREW REPORTED INTENSE BURNING SMELL THROUGHOUT CABIN AT START OF DESCENT AND FOR ABOUT 10 MINUTES. NO VISIBLE SMOKE. CREW WAS UNABLE TO IDENTIFY ORIGIN. LANDED WITHOUT INCIDENT. REPLACED RIGHT PRESSURE REGULATOR VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · 27,134 cycles

BOS EMERGENCY EXIT SIGN AT OVERHEAD FORWARD OVERWING DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT OVERHEAD FORWARD OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 26,881 hrs

SLC INFLIGHT T327/27JUL. CREW REPORTED NOSE LANDING GEAR UNSAFE LIGHT ON APPROACH. LANDED SLC WITHOUT INCIDENT. CLEANED NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR. RESEATED PROXIMITY SENSOR ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 26,881 hrs

DFW INFLIGHT T472/27 JUL (REPEAT). CREW REPORTED NOSE LANDING GEAR WARNING INDICATION AND LANDING GEAR AURAL WARNING ON APPROACH. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,199 hrs

DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 14D) · airframe 25,199 hrs

DFW - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,199 hrs

DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 8 TO 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 8 TO 13. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 25,199 hrs

DFW - EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 23 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS) · airframe 25,199 hrs

DFW - EMERGENCY LIGHT AT SEAT 17D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANDING GEAR — MALFUNCTIONED (NOSE)

ORD - INFLIGHT NOSE GEAR FAILED TO EXTEND. LANDED AT ORD WITH NOSE GEAR UP. AIRCRAFT OUT OF SERVICE FOR EVALUATION AND REPAIRS. ACCOMPLISHED PRE FERRY BILL OF WORK AND INSPECTION. FERRIED ORD TO TUL PER AUTHORIZATION SM6090 FOR REPAIRS.

Part: STRUT — INOPERATIVE (NLG)

ORD - THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED NOSE LANDING GEAR STRUT SEALS AND SERVICED NOSE LANDING GEAR STRUT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COALESCER BAG — CONTAMINATED (A/C PACK)

DFW - INFLIGHT T368/18 THE CABIN WAS FULL OF SMOKE ON LANDING. INSPECTED APU INLET AND AIRCRAFT TAIL SECTION. FOUND NO OIL OR HYDRAULIC FLUID LEAKS. RAN AIR CONDITIONING PACKS WITH APU AIR AND ENGINE AIR WITH NO SMOKE NOTED. AS PRECAUTIONARY REPLACED WATER SEPARATOR BAGS AND PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS DRIVEN BY B5-106 AND B5-107 EMERGENCY LIGHT BATTERIES INOPERATIVE. REPLACED BOTH B5-106 AND B5-107 BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERY FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: BOOT — OUT OF POSITION (A/C BAY)

LAS - FLT 1306 - EN ROUTE LAS-STL, AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON. DECLARED EMERGENCY AND RETURNED TO LAS WITHOUT FURTHER INCIDENT. REINSTALLED DISLOCATED BOOT AND CLAMP IN BETWEEN AIR CYCLE MACHINE AND HEAT EXCHANGER ON LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK · airframe 8,252 hrs · 4,097 cycles

EMERGENCY LIGHTS ON OVERHEAD AT ROWS 28 & 29 ARE INOP. REPLACED BATTERY POWER SUPPLY AND OPS CHECK PER MM33-53-00. ---CLOSED---