N7544A

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,491 hrs · 34,707 cycles

COCKPIT EMERGENCY LIGHTS FAILED TEST. REPLACED BATTERY PACK AT FWD DROP CEILING FOR COCKPIT EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL

Part: ANTENNA — INOPERATIVE (WEATHER RADAR) · airframe 65,537 hrs · 34,129 cycles

WEATHER RADAR FAILED. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR ANTENNA. SYSTEM GROUND CHECKED NORMAL.

Part: LIGHT — DIRTY (CATWALK) · airframe 65,320 hrs · 34,007 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. CLEANED TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK. OPS CHECK NORMAL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,306 hrs · 33,439 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 64,306 hrs · 33,439 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. RESEATED BATTERY FOR CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11. OPS CHECK NORMAL.

Part: ENGINE — FAILED (RIGHT) · airframe 63,279 hrs · 32,856 cycles

LBB - INFLIGHT DFW-SAN. CREW REPORTED RIGHT ENGINE OIL QUANTITY LOSS AND VIBRATIONS. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLARED FLIGHT DIVERETD LBB LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT LBB ON 09/10/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DISPLAY — DEFECTIVE (TCAS) · airframe 61,893 hrs · 32,078 cycles

DFW - (REPEAT ITEM) CREW NOTICED SMOKE AROUND THE HYDRAULIC CONTROL PANEL AND TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM WAS INOPERATIVE DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TCAS DISPLAY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACARS — DIRTY (COCKPIT) · airframe 61,893 hrs · 32,078 cycles

DFW - CREW REPORTED LIGHT SMOKE AND ODOR COMING FROM UNDER ACARS. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND A LOT OF DUST UNDER ACARS. CLEANED UNDER ACARS AND ACCOMPLISHED WORK CARD 21-96-01. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,854 hrs · 31,491 cycles

THE 1510 CANT FRAME CRACKED AT TAIL CONE ALIGNMENT PIN BELOW RIGHT LOWER TAIL CONE LATCH. INSTALLED DOUBLER PER EA MD80-53-020087 REVISION A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,854 hrs · 31,491 cycles

THE 1418 FRAME CRACKED AT LONGERON 2 LEFT. REPAIRED WITH REPAIR DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,854 hrs · 31,491 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 LONGERON 2 LEFT. INSTALLED NEW SHEAR TIE PER AARD 51-10-00-5 AND SRM 51-30-05.

Part: TUBE — BROKEN (AC BAY) · airframe 60,020 hrs · 31,001 cycles

SAN - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED SAN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLOW CONTROL VALVE LINE BROKEN AND BOOT FOR RIGHT TEMP CONTROL VALVE TORN. REPLACED TUBE FOR VALVE LINE AND BOOT FOR RIGHT TEMP CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

G2 GALLEY MOUNT FORWARD END OF NUMBER 6 SEAT TRACK CORRODED. INSTALLED NEW G2 GALLEY MOUNT ON FORWARD END OF NUMBER 6 SEAT TRACK AS PER SRM 51-30-02.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON TOP AND BOTTOM OF RIGHT CUSP ANGLE STATIONS 200 TO 218. INSTALLED NEW CUSP ANGLE STATION 180 TO STATION 229 PER SRM 53-05-00 FIGURE 55.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON SUBFLOOR STATIONS 200 TO 218. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 56,994 hrs · 29,332 cycles

CABIN RIGHT CUSP CRACKED AFT OF STATION 218. INSTALLED NEW CUSP SHEET STATION 218 TO 237 RIGHT PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

FOUND FORWARD END OF SEAT TRACK NUMBER 6 OUT OF LIMITS ON OUTBOARD FLANGE STATIONS 218 TO 226 AND OUT OF LIMITS AT CENTER OF TRACK FORWARD END BY GALLEY NUMBER 2 OUTBOARD MOUNT. INSTALLED SEAT TRACK SPLICE STATION 303 PER SRM 53-05-00 FIG 4F AND INSTALLED SEAT TRACK FROM 215 TO 303 PER MM 53-40-01-2.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

LIGHT CORROSION AROUND RIVNUT HOLES ON DOOR BEAM STATIONS 636 TO 655. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

DAMAGE TO CUSP SHEET AT STATION 295 TO 312. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

CABIN CUSP CRACKED RIGHT SIDE STATION 1212. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON TOP OF RIGHT OUTBOARD EDGE OF FORWARD SUBFLOOR STATIONS 200 TO 218. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16 PARAGRAPH 6.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON RIGHT CUSP. REMOVED AND REPLACED CUSP SHEET STATIONS 503 TO 541 PER AARD 53-20-00-16.

Part: FITTING — DAMAGED (CARGO BAY) · airframe 56,994 hrs · 29,332 cycles

AFT TIE DOWN RIGHT SIDE DAMAGED IN AFT CARGO. INSTALLED SERVICEABLE TIE DOWN PER SRM 51-30-00.

Part: CARGO TRACK — CORRODED (BS 1220) · airframe 56,994 hrs · 29,332 cycles

AFT CARGO LEFT TIE DOWN TRACK SPLICE CORRODED. REPLACED SPLICE PER SRM 51-30-05.

Part: BEAM — CORRODED (BS 1174-1193) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON DOOR CUTOUT BEAM STATIONS 1174 TO 1193. INSTALLED BEAM DOUBLER PER AARD 53-10-00-03.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON AFT CARGO DOOR CUTOUT BEAM WEB STRAP. REMOVED CORRODED STRAP INSTALLED MANUFACTURED STRAP PER EA MD80-51-010490.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

PUNCTURE IN CUSP STATION 190 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

DAMAGE TO CUSP SHEET AT FORWARD GIRT BAR AT LEFT NUMBER 2 DOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

FOUND LEFT LONGERON 29 END FITTING CRACKED AT STATION 1331 TO 1336. REPLACED FITTING PER SRM 51-30-00.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

CUSP DAMAGE AT STATION 564 BETWEEN TRACKS 1 AND 2. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

CUSP HAS DAMAGE AT STATION 1271 TO 1287 BETWEEN TRACKS 1 AND 2. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON BOTTOM OF LEFT CUSP, STATION 596. REMOVED CORROSION PER SRM 53-01-00 AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON LEFT CUSP, STATION 488. PERFORMED CUSP REPAIR PER AARD 53-20-00-16.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,994 hrs · 29,332 cycles

CORROSION ON TIE DOWN TRACK, RIGHT SIDE, STATION 1007 TO 1155. INSTALLED NEW TIE DOWN TRACK PER AARD 51-00-00-012.

Part: TRACK — CORRODED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

CORROSION ON TIE DOWN TRACK RIGHT SIDE STATIONS 1007 TO 1155. REPLACED TIEDOWN TRACK PER IPC 25-52-00-03L ITEM 450. PER SRM 51-30-05.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

CABIN AFT SIDE OF FORWARD ENTRY DOOR JAMB CRACK IN CLIP AT FASTENER, LONGERON 11 LEFT AT STATION 207. INSTALLED CLIP REPAIR PER AARD 53-10-00-11.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

RIGHT CUSP CRACKED BETWEEN LIGHTENING HOLES AT STATIONS 1260 TO 1265. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,994 hrs · 29,332 cycles

DENT IN FUSELAGE AFT OF MAIN ENTRY DOOR BELOW LONGERON 17 LEFT STATION 220. INSTALLED DOUBLER PER SRM 53-04-02.

Part: PAN — CRACKED (WINDOW) · airframe 56,994 hrs · 29,332 cycles

NUMBER 39 RIGHT WINDOW PAN CRACKED UPPER FORWARD CORNER AT STATION 946. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: FLAP — WORN (RT WING) · airframe 56,994 hrs · 29,332 cycles

RIGHT WING WORN AREA OUTBOARD FLAP INBOARD LEADING EDGE. INSTALLED DOUBLER WITH HOT BOND PER SRM 51-70-02.

Part: BATTERY PACK — SHORTED (CABIN) · airframe 56,964 hrs · 29,317 cycles

ELECTRICAL BURNING SMELL IN CABIN AFTER AIRCRAFT WAS TOWED TO THE GATE. FOUND EMERGENCY LIGHT BATTERY PACK SHORTED AND A BURNT LIGHT SOCKET ABOVE SEAT 8DEF. REPLACED BATTERY PACK AND LIGHT SOCKET AT 8DEF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,520 hrs · 29,070 cycles

ESCAPE PATH LIGHTING AB5-2 BATTERY LOW VOLTS. REMOVED AND REPLACED ESCAPED PATH LIGHT BATTERY AB5-2. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,520 hrs · 29,070 cycles

ESCAPE PATH LIGHT AB5-3 BATTERY LOW VOLTS. REPLACED ESCAPE PATH LIGHT BATTERY PACK AB5-3. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,520 hrs · 29,070 cycles

ESCAPE PATH LIGHT AB5-4 BATTERY LOW VOLTS. REPLACED BATTERY PACK AB5-4 FOR ESCAPE PATH LIGHT. OPS CHECKED NORMAL.

Part: WIRE — SHORTED (CABIN) · airframe 56,520 hrs · 29,070 cycles

ESCAPE PATH LIGHT DOES NOT WORK WITH AB5-4 AS SOLE POWER SOURCE. FOUND SHORT BY AFT SIDEWALL STAIRS EMERGENCY LIGHT PL2-8 REPAIRED AS REQUIRED. OPS CHECKED NORMAL.

Part: PLACARD — UNSERVICEABLE (TAILCONE)

DFW - TAIL CONE DROP HANDLE PULL PLACARD UNREADABLE. REPLACED DROP HANDLE PULL PLACARD.

Part: PLACARD — UNSERVICEABLE (TAILCONE)

DFW - TAIL CONE EXIT SIGN AT HANDLE UNREADABLE. REPLACED EXIT SIGN.

Part: CASTING — CORRODED (CARGO DOORWAY) · airframe 53,504 hrs · 27,386 cycles

CORROSION ON DOOR JAMB,FORWARD LOWER CASTING. REPLACED WITH NEW CASTING.

Part: FRAME — CRACKED (BS 1510) · airframe 53,504 hrs · 27,386 cycles

STATION 1510 CANT FRAME CRACKED AT TAIL CONE ALIGNMENT PIN, JUST ABOVE RIGHT LOWER TAIL CONE LATCH. INSTALLED REPAIR PER ESO 80559 DATED 01/12/09.

Part: FRAME — CRACKED (ZONE 100) · airframe 53,504 hrs · 27,386 cycles

1510 CANT FRAME CRACKED AT RIGHT LOWER TAIL CONE ALIGNMENT PIN. INSTALLED REPAIR PER ESO 80559 DATED 01/12/09.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 53,504 hrs · 27,386 cycles

CORROSION AROUND DOME NUT ON SUBFLOOR STATION 160. REPAIRED AREA PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,504 hrs · 27,386 cycles

LONGERON 2 RIGHT CRACKED AFT OF 1418 FRAME. INSTALLED A LONGERON REPAIR PER AARD 53-30-00-2.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 53,150 hrs

EMERGENCY LIGHT AT SEAT ROW 6EF INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 6EF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 51,388 hrs

LGA - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,388 hrs

LGA - EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 50,777 hrs

DFW INFLIGHT T1695/15FEB - NUMBER ONE ENGINE DRIVEN HYDRAULIC PUMP FAILED IN FLIGHT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — TORN (EMERGENCY EXIT) · airframe 50,192 hrs

LGA - EMERGENCY EXIT PLACARD AT AFT LEFT TAIL CONE TORN. REPLACED EMERGENCY EXIT PLACARD AT AFT LEFT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: INDICATOR — FAULTY (COCKPIT)

ORD INFLIGHT T2045/11NOV - RED NOSE GEAR UNSAFE LIGHT ILLUMINATED DURING CLIMB. CYCLED GEAR AND RED NOSE GEAR LIGHT REMAINED ILLUMINATED WITH GEAR DOWN. SECONDARY GEAR INDICATOR WAS NORMAL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED INDICATOR D1 32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SCHRADER VALVE — INOPERATIVE (NLG STRUT)

DFW INFLIGHT T744/25SEP - NOSE GEAR WOULD NOT RETRACT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED SCHRADER VALVE AND ACCOMPLISHED NOSE GEAR STRUT SERVICING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHTS FROM SEAT ROWS 9B TO 11B INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY EXIT LIGHTS FROM SEAT ROWS 9B TO 11B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHTS AT SEAT ROWS 21A AND 21F INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT SEAT ROWS 21A AND 21F. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

LGA - EMERGENCY FLASHLIGHT AT AFT ENTRY DOOR HAS BROKEN BAND. REPLACED BAND FOR EMERGENCY FLASHLIGHT AT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - EMERGENCY AISLE LIGHT AT SEAT 8D INOPERATIVE. RELAMPED EMERGENCY AISLE LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - OVERHEAD EMERGENCY LIGHT AT FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR EMERGENCY LIGHT AT FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — MISSING (CABIN)

LGA - EMERGENCY EXIT ROW RECLINE PLACARD MISSING. REPLACED RECLINE PLACARD FOR EMERGENCY EXIT ROW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BEZEL — MISSING (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 16D HAS MISSING BEZEL. REPLACED BEZEL FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 16D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — MISSING (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 16D HAS MISSING BULB. RELAMPED EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY AISLE LIGHTS IN AFT HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACK IN CEILING AFT GALLEY FOR INOPERATIVE EMERGENCY AISLE LIGHTS IN AFT HALF OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLADE — FAILED (LT ENGINE)

SJC INFLIGHT T1810/19OCT - DURING CLIMB CREW REPORTED LEFT ENGINE ROLLBACK TO TEN PERCENT N1 AT FLIGHT LEVEL 140. PERFORMED ENGINE SHUTDOWN. SINGLE ENGINE TIME TEN MINUTES. LANDED SJC WITHOUT INCIDENT. FOUND COMPRESSOR BLADE FAILURE. REPLACED NUMBER ONE ENGINE ON 21 OCT AT SJC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — LOW PRESSURE (L2 DOOR)

MSP - AFT SERVICE L2 DOOR SLIDE POUNDS PER SQUARE INCH WAS BELOW LIMIT. REPLACED SLIDE AT AFT SERVICE L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSDUCER — FAILED (LEFT)

TPA - ON TAKEOFF ROLL AT 40 KNOTS WHEEL NOT TURNING LIGHT ILLUMINATED STEADY. TAKEOFF ABORTED AND RETURNED TO GATE. LEFT INBOARD BRAKE TEMPERATURE TO 280 AL OTHER BRAKES AT 100 DEGREES. FOUND LEFT OUTBOARD ANTI SKID RELEASE LIGHT ON STEADY. UNABLE TO RESET. SWAPPED LEFT OUTBOARD TRANSDUCER TO LEFT INBOARD AND FAULT FOLLOWED TO LEFT INBOARD. VERIFIED AND REPLACED FAULTY TRANSDUCER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SAT - EMERGENCY CEILING LIGHTS AT ROWS 19, 20 AND 22 INOPERATIVE. REPLACED BATTERY PACK ON OVERHEAD BIN ON SEAT ROW 20 FOR EMERGENCY CEILING LIGHTS AT ROWS 19, 20, AND 22. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SUBFLOOR STRUCTURE AT FORWARD ENTRY DOOR FROM STATION 168 TO STATION 200. INSTALLED DOUBLER AFTER CUT OUT OF AFFECTED AREA PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP LONGERON 18 LEFT AT STATION 747. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: HANDLE — OUT OF POSITION (MLG)

BWI - FLT 539 - EN ROUTE BWI-ORD, MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED BWI AND LANDED WITHOUT FURTHER INCIDENT. RE-STOWED MAIN LANDING GEAR DOOR BYPASS HANDLE. INSPECTED MAIN LANDING GEAR AND DOORS. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT ON CATWALK NR 1 POSITION HAS BROKEN WIRE. REPAIRED WIRE FOR EMERGENCY EXIT LIGHT ON CATWALK NR 1 POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER — CONTAMINATED (ACM BAY)

DFW - FLT 797 - DURING CLIMB-OUT, A HEAVY ODOR ACCOMPANIED BY BLUE COLORED SMOKE WAS OBSERVED IN THE CABIN. AIRCRAFT AIR INTERRUPTED AND RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE WATER SEPARATOR BAGS SATURATED WITH DE-ICING FLUID. INSPECTED DUCTS FOR FLUID AND FOUND NO FLUID. REPLACED WATER SEPARATOR BAGS AND RAN APU AND ENGINES AT FULL POWER WITH PACKS ON. PACKS OPERATED NORMALLY AT ALL TEMPERATURE SETTINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, THE EMERGENCY EXIT FLOOR PATH LIGHTS AT 21D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FITTING — LOOSE (TAIL)

DFW - FLT 568 - AFTER TAKEOFF DFW PASSING 9,000 FT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. RAN ABNORMAL PROCEDURE CHECKLIST, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT FLICKERED A FEW MINUTES AND THAN EXTINGUISHED. A FEW MINUTES LATER, WHEN POWER INCREASED, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT FLICKERED ON/OFF. RETURNED DFW AND LANDED WITHOUT INCIDENT. TIGHTENED EXTERNAL START AIR FITTING AND RAN ENGINES AND ACCOMPLISHED LEAK CHECK. (M)

Part: WIRE — SHORTED (CABIN)

LAS - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPAIRED SHORTED WIRE IN RIGHT OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PSEU — MALFUNCTIONED (LANDING GEAR)

ORD - FLT 1774 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH 4 ANTI-SKID LIGHTS ON. CONFIRMED NOSE LANDING GEAR WAS FULLY EXTENDED AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. WHILE AIRCRFT WAS BEING TOWED TO GATE, NOSE LANDING GEAR LIGHT CHANGED TO GREEN INDICATION BUT ANTI-SKID WOULD NOT ARM. ACCOMPLISHED LANDING GEAR RETRACTION CHECK FOR SEVERAL CYCLED BUT UNABLE TO DUPLICATE PROBLEM. ALL LANDING GEAR INDICATIONS AND ANTI-SKID FUNCTION CHECKED NORMAL. PRECAUTIONRAY RESEATED LANDING GEAR PSEU AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT STRIP — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION.

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT CABIN BY EMERGENCY EXIT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN BY EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)