N438AA

Part: DUCT — DISCONNECTED (A C BAY) · airframe 89,532 hrs · 42,418 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT, IND-DFW. EMERGENCY NOT DECLARED. LANDING UNEVENTFUL. DURING CLIMB THE PRESSURIZATION FLOW LIGHT ILLUMINATED AND AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE DUCT DISCONNECTED. RECONNECTED DUCT IAW AMM 21-51-01. ACCOMPLISHED PRESSURIZATION DECAY AND RIGHT PACK OPERATIONAL CHECK IAW AMM 21-00-00. SYSTEM CHECKS NORMAL.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 89,468 hrs · 42,372 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS BETWEEN ROWS 7 AND 11 FAIL TO TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY B5-101 IAW AMM 33-53-00. SYSTEM TEST NORMAL.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 89,468 hrs · 42,372 cycles

AIRCRAFT WAS NOT GROUNDED. AFT INTERIOR OVERWING EMERGENCY EXIT LIGHTS FAIL TO TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY B5-105 IAW AMM 33-53-00. SYSTEM TEST NORMAL.

Part: SIGN — BROKEN (CABIN) · airframe 89,338 hrs · 42,295 cycles

AIRCRAFT WAS NOT GROUNDED. AFT LEFT SIDE EXIT MARKER NEXT TO JUMP SEAT IS BROKEN. REMOVED AND REPLACED MARKER IAW AMM 33-53-01. OPERATIONAL CHECK NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 88,379 hrs · 41,693 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD MIDDLE CARGO DOOR STOP IS CRACKED. R & R DOOR STOP FITTING IAW SRM 51-30-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 88,379 hrs · 41,693 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. WEB L20R IS CRACKED JUST AFT OF FUSELAGE STATION 1474. R & R WEB IAW SRM 51-01-00.

Part: TRANSFORMER — FAILED (ZONE 100) · airframe 86,823 hrs · 40,783 cycles

FLIGHT ATTENDANT REPORTED SLIGHT ELEC SMELL BY ROW 5AB AFTER TAKEOFF, THEN DISSIPATED. PILOT REPORTS WING & NACELLE FLOODLIGHT CB TRIPPED IN FLIGHT. TROUBLESHOOTING FOUND T1-10 RT WING NACELLE FLOODLIGHT TRANSFORMER BURNED UP IN THE FWD CARGO BIN EQUIPMENT PANEL. R & R TRANSFORMER T1-10 & PERFORMED OPERATIONAL CHECK IAW AMM 33-45-00. INSPECTED AREA WITH NO DAMAGE NOTED.

Part: PRESSURE SWITCH — FAULTY (RT ENGINE) · airframe 86,063 hrs · 40,343 cycles

RIGHT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED DURING TAKEOFF. TAKEOFF ABORTED AT APPROXIMATELY 50 KNOTS. R & R RIGHT ENGINE DIFFERENTIAL PRESSURE SWITCH. PERFORMED LEAK & OPERATIONAL CHECKS IAW AMM 73-34-01. SYSTEM CHECKED GOOD.

Part: FORMER — CRACKED (LE SLAT) · airframe 84,728 hrs · 39,614 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER REPAIR DOUBLER & HAT BUSHING IAW WC 57-98-05.

Part: CASTING — CRACKED (LT SPOILER) · airframe 84,728 hrs · 39,614 cycles

LEFT GND SPOILER CASTING LUG CRACKED AT OTBD AFT REAR. R & R CASTING IAW SRM 57-01-00, IPC 27-60-02-02, IPC 27-60-04-05 & AARD 51-00-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 84,728 hrs · 39,614 cycles

FORWARD CARGO DOOR FWD STOP 3RD FROM BOTTOM IS CRACKED. R & R DOOR STOP IAW AARD 51-00-05-01 & DWG 5910141.

Part: TIRE — SEPARATED (RT MLG) · airframe 84,198 hrs · 39,348 cycles

RIGHT ENG COMPRESSOR STALLED AFTER TAKEOFF. AT 3000 FEET FLIGHT ATTENDANTS REPORTED SMELL OF RUBBER & POSSIBLE STRANGE VIBRATION. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND THE NR 4 MLG TIRE EXPERIENCED A CAP SEPARATION WHICH WAS INGESTED INTO THE NR 2 ENG. REPLACED RT ENG ON 10/23/14, OPEN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 83,189 hrs · 38,824 cycles

AFT ESCAPE PATH LIGHTING FAILED CHECK. REPLACED AB5-3 BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: FUEL CONTROL — INOPERATIVE (APU) · airframe 82,917 hrs · 38,683 cycles

TUS CREW REPORTED AUXILIARY POWER UNIT FAULTED WITH RT GEN ON PLACARD. EMER DECLARED FLIGHT RETURNED TUS LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED APU FUEL CONTROL & ELEC CONTROL UNIT REPLACED. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 81,898 hrs · 38,196 cycles

DFW CREW REPORTED RT ENG WAS STRUCK BY LIGHTING & CAUSED A COMPRESSOR STALL & FLAME OUT. ENG STARTED ON ITS OWN AS ENGINE FAILURE CHECKLIST WAS STARTED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT ENG AT DFW ON 12/23/2013. SYSTEM GND CHECKED NORMAL OPERATION OPEN.

Part: CLAMP — UNSECURE (AC BAY) · airframe 81,657 hrs · 38,067 cycles

PDX AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED PDX LANDED WITHOUT INCIDENT. RE-SECURED CLAMP FOR DUCT TO RT HAND AIR CYCLE MACHINE. ACCOMPLISHED DEFERRAL OF RT HAND AIR CONDITIONING PACK SYSTEM IAW MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED TEMPERATURE CONTROL VALVE AT RT HAND AIR CONDITIONING PACK AT ORD ON 10/18/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,592 hrs · 38,033 cycles

OVERHEAD EMERGENCY EXIT LIGHTS FROM ROWS 8 TO 11 REMAIN ON AFTER POWER HAS BEEN REMOVED. REPLACED BATTERY PACK ST ROW 8E/F BIN. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,471 hrs · 37,969 cycles

AFT EMERGENCY CEILING LIGHTS CAME ON WHEN ALL POWER WAS REMOVED FROM AIRCRAFT & BATTERY SWITCH SELECTED TO OFF. REPLACED B5-27 EMERGENCY LIGHT BATTERY PACK IN CEILING OF RT AFT LAVATORY. OPERATIONS CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 4 SEAT TRACK FROM STATIONS 263 TO 266. INSTALLED PLUG REPAIR IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 2 SEAT TRACK FROM STATIONS 1200 TO 1202. INSTALLED SPLICE REPAIR IAW SRM 53-05-00 FIGURE 4F & SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

CABIN FLOOR INTERCOSTAL CRACKED AT STATION 787 & BL 0. INSTALLED SERVICEABLE INTERCOSTAL IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 4 SEAT TRACK FROM STATIONS 283 TO 287. INSTALLED PLUG REPAIR IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 6 SEAT TRACK AT STATION 1122. ACCOMPLISHED PLUG REPAIR IAW SRM 53-05-00 FIGURE 4A.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

CRACK ON WINDOW PAN, LT SIDE AT STATION 332 UPPER FWD CORNER. INSTALLED ANGLE DOUBLER IAW AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 1 SEAT TRACK FROM STATIONS 484 TO 486. INSTALLED REPAIR PLUG IAW AARD 53-20-00-10.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

RT WINDOW RING PAN CRACKED AT UPPER TAB, STATION 1021. INSTALLED ANGLE DOUBLER IAW AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 6 SEAT TRACK AT STATION 1091. ACCOMPLISHED PLUG REPAIR IAW SRM 53-05-00 FIGURE 4.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

RT WINDOW RING PAN CRACKED AT UPPER TAB, STATION 1059. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 5 SEAT TRACK FROM STATIONS 203 TO 246. INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 53-05-00 FIGURE 4F.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON RT TIE DOWN TRACK IN AFT CARGO FROM STATIONS 1231 TO 1250. INSTALLED DOUBLER STRAP IAW AARD 53-20-00-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 1 SEAT TRACK AT STATIONS 469 TO 472. INSTALLED REPAIR PLUG IAW AARD 53-20-00-10.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

RT WINDOW RING PAN CRACKED AT UPPER TAB, STATION 1097. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,407 hrs · 37,935 cycles

CORROSION ON NR 6 SEAT TRACK FROM STATIONS 266 TO 796. ACCOMPLISHED SPLICE REPAIR IAW AARD 53-20-00-01 & AMM 53-40-01-201.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

LT WINDOW RINGPAN CRACKED AT UPPER AFT TAB, STATION 1060. INSTALLED ANGLE DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

RT WINDOW RING PAN CRACKED AT UPPER TAB, STATION 1040. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

RT WINDOW RING PAN CRACKED AT UPPER TAB, STATION 846. INSTALLED ANGLE DOUBLER IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,407 hrs · 37,935 cycles

LT WINDOW RING PAN CRACKED AT UPPER AFT TAB, STATION 1089. INSTALLED ANGLE DOUBLER IAW AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,406 hrs · 37,933 cycles

LT CUSP CORRODED AT STATION 1079. INSTALLED DOUBLER AT STATION 1079 IAW AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

FS FRAME CRACKED AT FWD SIDE OF STATION 1322 & LONGERON 17 RT. ACCOMPLISHED NESTED ANGLE REPAIR IAW SRM 53-03-00 FIGURE 51.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

FS FRAME FWD SIDE IS CRACKED AT STATION 1322 & LONGERON 17 LT. ACCOMPLISHED NESTED ANGLE REPAIR IAW SRM 53-03-00 FIGURE 51.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

RT CUSP AT STATION 863 HAS A CRACK NEAR THE HOLE. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 81,406 hrs · 37,933 cycles

CORROSION ON LT CUSP FROM STATIONS 256 TO 259. INSTALLED DOUBLER IAW SRM 53-05-00 FIGURE 131A-21.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 81,406 hrs · 37,933 cycles

RT CUSP SHEET CORRODED FROM STATIONS 237 TO 313. INSTALLED RT CUSP SHEET FROM STATIONS 237 TO 313 IAW AARD 51-00-05-1, SRM 51-30-02 & SRM 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

FS FRAME FWD SIDE IS CRACKED AT STATION 1322 & LONGERON 17 LT. INSTALLED FRAME CRACK CUTOUT REPAIR IAW SRM 53-03-00, FIGURE 51.

Part: CASTING — CRACKED (LE SLAT) · airframe 81,406 hrs · 37,933 cycles

RT WING INBD SIDE OF NR 4 SLAT TRACK CUTOUT CASTING IS CRACKED AT THE INBD AFT SIDE AT THE LOWER AFT CABLE BRACKET MOUNT BOSS LOWER SIDE. REPLACED CASTING IAW AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

FRAME CRACKED ON AFT SIDE OF STATION 1418 & LONGERON 2 RT. INSTALLED FRAME DOUBLER ON AFT SIDE OF FRAME IAW SRM 53-03-00, DRAWING PL591359, SRM 53-10-00-15, SRM 53-01-00, & AARD 53-10-00-15.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

AFT ACCY, LONGERON 2 LT AT STATION 1418 IS CRACKED. INSTALLED NEW SERVICEABLE LONGERON & LONGERON SPLICE AT STATION 1418 IAW 53-02-00 AND 53-00-00-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

FRAME CRACKED ON AFT SIDE OF STATION 1418 & LONGERON 2 LT. INSTALLED FRAME DOUBLER ON AFT SIDE OF FRAME 1418 & LONGERON 2 LT IAW 53-03-00, DRAWING PL591358, & SRM 53-01-00, AARD 53-10-00-15, SRM 53-03-00, SRM 53-01-00, & AARD 53-10-00-15.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

AFT ACCY LONGERON 2 RT & STATION 1418 IS CRACKED. INSTALLED NEW SERVICEABLE LONGERON & LONGERON SPLICE AT STATION 1418 & LONGERON 2 RT IAW SRM 53-02-00 & AARD 53-00-00-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

CORROSION ON SEAT TRACK FROM STATIONS 741 TO 797. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,406 hrs · 37,933 cycles

LT CUSP SHEET FROM STATIONS 256 TO 259 CORRODED. INSTALLED NEW CUSP SECTION & DOUBLER IAW ISRM 53-05-00 FIGURE 131A-21 SHEET 1 WIP 6 & 12.

Part: ANGLE — CORRODED (LT MLG WW) · corrosion level 2 · airframe 81,406 hrs · 37,933 cycles

LT WW SLANT PANEL AT OTBD ATTACHMENT ANGLE HAS CORROSION. REPLACED ANGLE IAW AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

CRACK IN LT CABIN CUSP FROM STATIONS 804 TO 805. REMOVED DAMAGE & INSTALLED NEW CUSP SHEET IAW 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,406 hrs · 37,933 cycles

LT CUSP FROM STATIONS 709 TO 712 CORRODED. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

RT CUSP CORRODED FROM STATIONS 1031 TO 1033. INSTALLED DOUBLER CUSP IAW AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

AFT ACCY CANT FRAME 1463 & LONGERON 18 LT CRACKED. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-15 REPAIR 15, PAGE 1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

LT CUSP SHEET AT STATION 693 CRACKED. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,406 hrs · 37,933 cycles

RT CUSP CORRODED FROM STATIONS 503 TO 598. INSTALLED NEW RT CUSP SHEET FROM STATIONS 503 TO 598 IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,406 hrs · 37,933 cycles

CORROSION ON CUSP FROM STATIONS 303 TO 305 OTBD OF NR 1 SEAT TRACK. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 81,406 hrs · 37,933 cycles

RT WINDOW RINGPAN CRACKED AT UPPER TAB STATION 1192. COMPLETED RINGPAN DOUBLER REPAIR IAW AARD 53-10-00 REPAIR 25.

Part: PLACARD — FADED (EXTERIOR) · airframe 79,040 hrs · 36,719 cycles

EMERGENCY EXIT PLACARDS ON EXTERIOR OF RIGHT OVERWING EXIT DOOR FADED AND UNREADABLE. REPLACED PLACARDS.

Part: PLACARD — FADED (EXTERIOR) · airframe 79,040 hrs · 36,719 cycles

EMERGENCY EXIT PLACARD ON EXTERIOR AFT LEFT OVERWING EXIT DOOR FADED AND UNREADABLE. REPLACED PLACARD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,768 hrs · 33,958 cycles

RIGHT FRAME 905 FASTENERS THROUGH SKIN WRONG SIZE. REMOVED CAD PLATED FASTENERS, REAMED HOLES TO OVERSIZE AND INSTALLED HLT141 FASTENERS PER EA MD80-53-012612.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,768 hrs · 33,958 cycles

RIGHT FRAME 886 FASTENERS THROUGH SKIN WRONG SIZE. REMOVED CAD PLATED FASTENERS, REAMED HOLES TO 0.1975 AND INSTALLED HLT141-6 LOCK FASTENERS PER EA MD80-53-014612.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,215 hrs · 33,694 cycles

CANT FRAME 1463 WEB CRACKED INBOARD OF LONGERON 9 LEFT. INSTALLED DOUBLER REPAIR PER EA MD80-53-013390.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 72,574 hrs · 33,386 cycles

LEFT NUMBER 1 DOOR EMERGENCY FLASHLIGHT DOES NOT TEST. REPLACED FLASHLIGHT ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,656 hrs · 32,098 cycles

CEILING EMERGENCY LIGHTS AT 17DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SEAT 17. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,656 hrs · 32,098 cycles

AFT STAIRWAY EMERGENCY LIGHTS INOP. RESEATED BATTERY PACK IN AFT LAVATORY CEILING. EMERGENCY LIGHTS OPS CHECK NORMAL.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 69,656 hrs · 32,098 cycles

FORWARD LOWER FLASHLIGHT STRAP BROKEN. REPLACED STRAP.

Part: BATTERY — NOT SEATED (CABIN) · airframe 69,656 hrs · 32,098 cycles

CEILING EMERGENCY LIGHTS AT 11DEF-10DEF INOPERATIVE. RESEATED BATTERIES AT BIN 9DEF. OPS CHECK GOOD.

Part: FUSE — INOPERATIVE (BRAKE SYS) · airframe 69,088 hrs · 31,837 cycles

LAX REPORT OF WHEEL NOT TURNING LIGHT ILLUMINATED AT 70K IAS. ABORTED TAKE-OFF RETURNED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LIMITER BRAKE FUSE. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

SEAT TRACK NR 3 AT STA 645 HAS BROKEN LUG, FWD FOOT PLACEMENT FOR SEAT 13AB. COMPLETED SEAT TRACK PLUG REPAIR PER SRM 53-05-00 FIG 4A.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

AFT PRESSURE BULKHEAD FWD SIDE VERTICAL STIFFENER CRACKED BELOW LONGERON ONE. INSTALLED ALL FASTENERS IN DOUBLER PER SRM 51-30-05. DOUBLER REPAIR MADE PER SRM 53-01-00.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

TIE DOWN TRACK HAS CORROSION. REPLACED TIE DOWN TRACK PER EA MD-80-53-006057 DATED 4-17-09.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

SEAT TRACK NR 5 HAS DEEP CORROSION AT STA 204. REPLACED SEAT TRACK NR 5 FROM STA 200 - STA 247 PER SRM 51-30 AND SRM 53-05-00 FIG 4.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

CRACK ON RT CUSP AT STA 218 JUST OTBD OF NR 5 S/T. INSTALLED REPLACEMENT CUSP SHEET PER AARD 53-20-00-16 SRM 51-30.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

LT TIEDOWN TRACK IS CORRODED. REPLACED TIE DOWN TRACK PER AARD 51-00-00-012.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

AFT CARGO AFT RIGHT TIE DOWN TRACK CORRODED BETWEEN STA 1211-1309. REPLACED TRACK PER SRM 51-10-1.

Part: LONGERON — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

CORROSION ON L29R BETWEEN STA 1313-1315. INSTALLED NESTED U CHANNEL REPAIR PER SRM 53-02-00. CORRECTED CONTROL NUMBER DUE TO DUPLICATES ORIGINAL NR AALA20090424TUL33

Part: STRAP — GOUGED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

WEB STRAP STA 1150 HAS SCREW GOUGE L28R. INSTALLED NEW STRAP BS 1150 PER SRM 51-30-3.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

FACTORY LONGERON SPLICE IS CRACKED AT STATION 234, LONGERON 27R. REPLACED SPLICE FITTING WITH NEW FITTING PER SRM 51-30-5, 51-30-2 AND DAC DRAWING NR 5913508.

Part: LONGERON — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

CORROSION ON L29R BETWEEN STA 1313-1315. INSTALLED NESTED U CHANNEL REPAIR PER SRM 53-02-00

Part: LONGERON — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

CORROSION ON LONGERON 29L BETWEEN STA 1311-1313. INSTALLED NESTED U CHANNEL REPAIR PER SRM 53-02-00.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LT CUSP CORRODED STA 1174-1176. SPLICED NEW SECTION OF CUSP PER AARD 53-20-00-16.

Part: FITTING — CORRODED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

CORROSION ON GALLEY T/D FITTING NR 1 OTBD STA 162 2ND INBD OF FWD SERVICE DOOR. INSTALLED TWO (2) NEW G1 GALLEY TIE-DOWN FITTINGS AT BS 160 RBL-43 PER SRM 51-01.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

CORROSION ON BOTTOM OF CUSP RT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

OVERWING FRAME CRACKED RIGHT SIDE AT STATION 886. REPLACED FRAME PER DRAWING SRO9530282.

Part: ANGLE — CRACKED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

AFT OF STA 826 ABOVE CENTER FUEL TANK RT SIDE HAS CRACK IN ANGLE THAT INTERCOSTAL ATTACHES TO AT FWD END. INSTALLED REPAIR DOUBLER PER EA 57-006020.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

AFT CARGO FWD RIGHT TIEDOWN TRACK IS CORRODED BTWN STA 1005-1155. REMOVED AND REPLACED TIE DOWN TRACK.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LONGERON 4L CRACKED AT STATION 160. REMOVED CRACKED LONGERON AND INSTALLED NEW LONGERON AND SPLICE PER SRM 53-02-00.

Part: LONGERON — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION ON LONGERON 28R BETWEEN STATION 1290 AND 1295. REMOVED CORROSION, TREATED, PRIMED, AND INSTALLED NESTED "U" CHANNEL REPAIR PER SRM 53-02-00.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION ON RIGHT CUSP STATION 1173-1174. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

SHEAR TIE CRACKED ON AFT SIDE OF FRAME 1418 BETWEEN LONGERON 1 AND LONGERON 2R. INSTALLED REPAIR ANGLE PER EA MD80-53-006009 AND AARD 53-10-00-20.

Part: LONGERON — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION ON LONGERON 28R BETWEEN STATION 1290 AND 1295. REMOVED CORROSION, TREATED, PRIMED, AND INSTALLED NESTED "U" CHANNEL REPAIR PER SRM 53-02-00. CORRECTED DUE TO DUPLICATE CONTROL NUMBER. ORIGINAL AALA20090424TUL45.

Part: CUSHION — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LEFT CUSP IS CRACKED AT STATION 226. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION ON RIGHT CUSP AFT OF STATION 237. DOUBLER REPAIR ACCOMPLISHED PER AARD 53-20-00-16.

Part: LONGERON — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION ON LONGERON 29R FROM STATION 1287-1295. REMOVED CORROSION, PRIMED, TREATED AND INSTALLED NESTED "U" CHANNEL REPAIR PER SRM 53-02-00.

Part: BEAM — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

CORROSION ON MID CARGO DOOR BEAM DOUBLER. REMOVED CARGO DOOR BEAM DOUBLER AND REPLACED WITH NEW DOUBLER.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

CUSP CRACKED AT STATION 1176 LEFT SIDE, OUTBOARD OF SEAT TRACK NR 1. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

FWD SERVICE DOOR NR 1 BEAM CRACKED, FWD END. INSTALLED DOUBLER PER SRM 52-05 FIG 25.

Part: SKIN — CRACKED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 1474, APPROX 1 INCH UP FROM VENTRAL STAIR CUTOUT. DOUBLER INSTALLED PER SRM 53-01 FIGURE 2.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION ON LEFT HAND CUSP STATION 1079-1098. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CORRODED (ZONE 100) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION ON LOWER ANGLE OF LOWER FORWARD CORNER OF AFT CARGO DOORWAY OPENING. REPLACED DAMAGED ANGLE WITH SERVICEABLE PART PER SRM 51-30-05.

Part: STRINGER — CRACKED (ZONE 600) · airframe 69,114 hrs · 31,850 cycles

CRACK IN STRINGER. REMOVED AND REPLACED STRINGER PER DRAWING NR 5930502 AND SRM 51-10-04.

Part: SKIN — DAMAGED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

DENT ON FUSELAGE JUST FORWARD OF AFT SERVICE DOOR ABOVE LONGERON 14L. INSTALLED DOUBLER PER SRM 53-04 FIGURE 38 SHEET 20, VIEW E.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LEFT CUSP IS CRACKED AT STATION 226. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

FASTENER HOLE ELONGATED IN RIGHT CUSP AT STATION 549. INSTALLED FREEZE PLUG AND STRAP PER EA MD80-53-005994.

Part: STRINGER — CRACKED (ZONE 600) · airframe 69,027 hrs · 31,809 cycles

CRACK IN STRINGER IN RIGHT WING VENT BOX. REMOVED AND REPLACED STRINGER PER BOEING DRAWING 5930502 AND SRM 51-10-04.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,027 hrs · 31,809 cycles

LEVEL 1 CORROSION FOUND ON RIGHT CUSP FROM STATION 579-598. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (BS 218 S19-20L) · airframe 69,027 hrs · 31,809 cycles

FUSELAGE DENT APPROX 4 INCH IN DIAMETER BY .187 INCH DEEP AND 14 INCHES AFT OF FORWARD AIRSTAIR DOOR STATION 218, BETWEEN LONGERON 19L AND 20L. INSTALLED EXTERNAL DOUBLER PER SRM 53-04-00 SHEET 34 FIGURE 12B.

Part: TARGET — BROKEN (MLG DOOR)

SLC INFLIGHT T416/27OCT - GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RETURNED TO SLC AND LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR PROXIMITY TARGET ASSEMBLY BROKEN OFF. REPLACED LEFT MAIN LANDING GEAR PROXIMITY TARGET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

SFO - EMERGENCY PATH LIGHT AT AFT STAIRWELL FORWARD SIDE HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY PATH LIGHT AT AFT STAIRWELL FORWARD SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - CEILING EMERGENCY LIGHT AT SEAT ROW 3 INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT AT SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT LIGHTS AT RIGHT AND LEFT AFT ESCAPE DOOR INOPERATIVE. REPLACED BATTERY PACK AT ROW 21 FOR EMERGENCY EXIT LIGHTS AT RIGHT AND LEFT AFT ESCAPE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — BACKED OUT (CONNECTOR)

DFW - WHILE LANDING LANDING GEAR DOWN INDICATION LIGHTS CYCLED ON AND OFF WITH ASSOCIATED WARNING HORN. INDICATOR PIN WAS UP. ACCOMPLISHED GO-AROUND. LANDED DFW WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. FOUND DOWN LOCK SENSOR CONNECTOR PIN PUSHED BACK. INSERTED AND LOCKED DOWN LOCK SENSOR CONNECTOR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OIL SYSTEM — LEAKING (APU)

DFW - AFTER TAKEOFF NOTICED ODOR AND SMOKE IN CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LARGE OIL LEAK ON APU COMPARTMENT AND BLEED DUCT WITH OIL CONTAMINATION. REMOVED APU ASSEMBLY AND CLEANED APU COMPARTMENT. REPLACED WATER SEPARATOR BAGS AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — LEAKING (SCHRADER VALVE)

STL INFLIGHT T0456/6JUL - NOSE GEAR WILL NOT RETRACT. RED LIGHT REMAINED ON AFTER GEAR RETRACTION. FOUND NOSE STRUT FLAT. SERVICED NOSE STRUT AFTER REPLACING SCHRADER VALVE O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROWS 2 THROUGH 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 2 THROUGH 7. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COALESCER BAG — CONTAMINATED (RT PACK)

SFO - INFLIGHT T1907 SMOKE IN CABIN REPORTED SOON AFTER TAKEOFF. TURNED RECIRCULATION FAN OFF AND NO SMOKE VISIBLE. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. FOUND RT PACK LEAKING OIL. REPLACED RIGHT HAND COALESCER BAG. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - CEILING EMERGENCY LIGHTS FROM ROWS 17-21 INOPERATIVE. REPLACED BATTERY PACK B5-104 FOR CEILING EMERGENCY LIGHTS FROM ROWS 17-21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — DEFECTIVE (A/C BAY)

DFW - FLT 1035 - EN ROUTE DFW-AUS - MASTER WARNING AND ASSOCIATED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. DID IMMEDIATE ACTION ITEMS AND LIGHT EXTINGUISHED WHEN AIR CONDITIONING SUPPLY SWITCHES MOVED TO HIGH PRESSURE BLEED OFF. RETURNED AND LANDED DFW WITHOUT INCIDENT. INSTALLED NEW HEAT EXCHANGER CLAMP. LEAK CHECKED GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — INOPERATIVE (EMERGENCY LIGHT)

AUS - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 17-21 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 12-17 AISLE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CANTED FRAME WEB CRACKED. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-32. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (AIRSTAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND CORROSION AND TWO CRACKS ON AFT CARGO DOOR JAMB BEAM AND WEB STATION 1155 TO 1220. INSTALLED DOUBLER ON DOOR BEAM. REPLACED WEB WITH NEW WEB AND INSTALLED NEW STRAP PER AARD 53-10-00-3. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION UNDER CARGO TRACK RIGHT CLIP NUT HOLES BETWEEN STATION 1231-1250. REPLACED RIGHT AFT CARGO TRACK STATION 1212 TO 1327 WITH NEW TRACK PER SRM 53-05. (M)

Part: PAN — CRACKED (FUSELAGE)

TUL - FOUND CRACK EMITTING FROM AND CORROSION FROM 373-377 ON LOWER CARGO DOOR PAN AREA. STOP DRILLED CRACK. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 80559 DATED 7/24/2001. (M)

Part: FRAME (FS 522)

TUL - FOUND TWO WEAR MARKS IN FRAME STATION 522 BETWEEN LONGERON 23L AND 24L 5 INCH APART. TRIMMED OUT DAMAGED AREAS TWO OUT OF LIMITS, J-ANGLE .010 INCH 17.7 CRS HEAT TREAT TO TH1050 ATTACH WITH HI-LOCKS, INSTALLED DOUBLER PER ESO 80554 DATED 7/19/2001. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND RIGHT CUSP CRACKED AT STATION 1270 AND STATION 1293. REMOVED AND REINSTALLED NEW CUSP RIGHT SIDE STATION 1250 TO STATION 1309 PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP CORRODED AT STATION 640-653. INSTALLED DOUBLER ON CUSP PER AARD 53-00-00-2. (M)

Part: SEAT TRACK — CORRODED (BS 219)

TUL - FOUND NR 2 SEAT TRACK HAS CORROSION IN CHANNEL, BS 219. CUT OUT DAMAGED SEAT TRACK FROM BS 200-246 PER SRM 53-05 FIG 4F. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP CORRODED BOTTOM SIDE STATION 560-572 OUTBOARD SIDE OF LIGHTENING HOLES OUTBOARD OF NR 6 SEAT TRACK. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-00-00-021 SRM 53-01. (M)

Part: LONGERON

TUL - FOUND LONGERON 17 LEFT BENT AT BLIND FASTENER REPAIR AREA STATION 250 SKIN ALSO DENTED SAME AREA. CUT OUT DAMAGED SECTION OF LONGERON SPLICED IN NEW SECTION OF LONGERON WITH 2 SPLICES PER SRM 53-02 FIG 18 SHEET 1. SKIN REPAIRED ON E-58-3 9069497. (M)

Part: SKIN — DENTED (FS 252)

TUL - FOUND LEFT FUSELAGE HAS DENT 1.5 INCHE BY 1.5 INCHE BY .0555 INCH ABOVE LAV SERVICE PANEL WITH POSSIBLE CRACK .8 INCH LONGERON. CUT OUT DAMAGED AREA OF SKIN, CUT TITANIUM DOUBLER, INSTALLED INTERNAL FINGER DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK (FS 256)

TUL - FOUND STATION 256 LEFT LOOSE HARDWARE UNDER SEAT TRACK FLANGE, FLANGE BENT/CRACKED, NR 1 SEAT TRACK. REPAIRED NR 1 SEAT TRACK AT STATION 256 LEFT WITH SPLICE REPAIR PER SRM 53-05. (M)

Part: SKIN — GOUGED (BS 1305)

TUL - FOUND DEEP GOUGE IN FUSELAGE SKIN AT STATION 1305 ABOVE LONGERON 19R. INSTALLED SCUFF PLATE PER AARD 53-30-00-8. (M)

Part: LONGERON (FS 160)

TUL - FOUND LONGERON 3L CRACKED AT OUTBOARD LEG AT FASTENER AFT SIDE OF STATION 160. INSTALLED SECTION OF LONGERON AND SPLICE PER SRM 53-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP CORRODED AT STATION 674-693. CUT OUT CORROSION AND INSTALLED DOUBLER STATION 684-687 PER AARD 53-00-02. (M)

Part: SEAT TRACK — CORRODED (BS 1200-1210)

TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1200-1210. REMOVED DAMAGED AREA ON NR 1 SEAT TRACK AT STATION 1200-1210. INSTALLED SEAT TRACK PLUG, TREATED AND PRIMED PER SRM 51-10-3 AND 53-05 PAGE 4A. (M)

Part: SEAT TRACK — CORRODED (BS 200-216)

TUL - FOUND CORROSION ON SEAT TRACKS NR 5 AT BS 200-216. INSTALLED STRAP PER AARD 53-20-00-13 AFTER REMOVAL OF CORROSION THEN TREATED, PRIMED AND PAINTED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ABOVE AFT STAIR DOOR INOPERATIVE. RECONNECTED QUICK DISCONNECT ON EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER — CONTAMINATED (CABIN)

SAN - FLT 1179 - EN ROUTE ORD/SAN DURING CRUISE, CREW NOTED BURNING SMELL IN CABIN. AIRCRAFT PROCEEDED TO LAND SAN WITHOUT INCIDENT. REPLACED RIGHT AIR CYCLE MACHINE COALESCER BAG. ACCOMPLISHED PACK BURN-OUT PROCEDURE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: TIE DOWN TRACK — CORRODED (BS 1126)

TUL - FOUND RIGHT TIE DOWN TRACK CORRODED. REPAIRED IAW ESO 80559, DATE 4-18-97, SRM 53-05 FIG 4G PAGE 10R. (M)

Part: CONNECTOR — BROKEN (CABIN)

EWR - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 12D INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANNUNCIATOR — DEFECTIVE (RT MLG)

MIA - FLT 0725 - DURING APPROACH TO MIA WHEN LANDING GEAR EXTENDED, RT MLG HAD NO INDICATION. ACCOMPLISHED TOWER FLY-BY AND VISUALLY CONFIRMED RT MLG EXTENDED. AIRCRAFT LANDED MIA WITHOUT INCIDENT. REPLACED LANDING GEAR ANNUNCIATOR PANEL. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)