N9414W

Part: FAN — DEFECTIVE (LAVATORY) · airframe 47,247 hrs · 22,965 cycles

IAD - CREW REPORTED ELECTRICAL ODOR IN BOTH AFT LAVATORIES. EMERGENCY DECLARED FLIGHT RETURNED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT LAVATORY SMOKE FAN THAT WAS DEFECTIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — LOOSE (ACM) · airframe 44,015 hrs · 21,348 cycles

DFW - CREW REPORTED TAIL COMPARTMENT HI LIGHT ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT AIR CONTROL MACHINE OUTFLOW MANIFOLD CLAMP LOOSE. TIGHTENED CLAMP NO DISCREPANCIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,779 hrs · 19,331 cycles

STIFFENER CRACKED AT STATION 1418 LONGERON 2R. INSTALLED STIFFENER DOUBLER ON FRAME PER EA MD80 53-005736.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 39,779 hrs · 19,331 cycles

LONGERON 2R CRACKED AT TOP AFT OF FRAME 1418. INSTALLED LONGERON SPLICE PER AARD 53-30-00-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,779 hrs · 19,331 cycles

STATION 1418 FRAME CRACKED AT LONGERON 2R. INSTALLED FRAME DOUBLER PER MD80-53-005736.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS)

LGA FLIGHT T1060/02OCT - AUXILIARY POWER UNIT AND EXTERNAL POWER FAILED AFTER PARKING. PASSENGERS REPORTED EMERGENCY LIGHTS IN CABIN INOPERATIVE. FLIGHT ATTENDANTS REPORTED EXIT LIGHTS ON. RESET CIRCUIT BREAKER FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GIRT BAR — WORN (EMERGENCY SLIDE)

MSP - EMERGENCY SLIDE GIRT BAR HANDLE HOLDER WORN OUT AT AFT GALLEY DOOR. REPLACED SLIDE FOR EMERGENCY SLIDE GIRT BAR HANDLE HOLDER AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 23 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — SHORTED (EMERGENCY LIGHTS)

TUL - EMERGENCY ESCAPE PATH LIGHTING SYSTEM FROM SEATS 3EF TO 20DEF INOPERATIVE. FOUND SHORTED WIRE AT SEAT 9DEF. REPAIRED WIRING FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM FROM SEATS 3EF TO 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

SFO - AFT ACCESSORY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT TAIL CONE FOR AFT ACCESSORY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT CONNECTOR AT SEAT 15D IN PINNED. REPAIRED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - EMERGENCY LIGHTS AT AFT CABIN ROWS 29, 30 AND 31 INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR EMERGENCY LIGHTS AT AFT CABIN ROWS 29, 30 AND 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - SECOND OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR SECOND OVERWING EXIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - COCKPIT ENTRY WAY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT ENTRY WAY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - EMERGENCY LIGHTS AT ROWS 24, 25 AND 26 INOPERATIVE. REPLACED BATTERY PACK B5-106 FOR EMERGENCY LIGHTS AT ROWS 24, 25 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT ON FORWARD GALLEY WELL INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT ON FORWARD GALLEY WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,047 hrs · 11,590 cycles

THE EGRESS LIGHTS WERE INOPERATIVE BETWEEN ROWS 3 AND 4, AND BETWEEN ROWS 7 TO 13. RESEATED LAMP AT ROW 3-4 AND RESEATED BATTERY IN POWER SUPPLY B5-206 FOR ROWS 7 TO 13. CHECK-C 11-6-02 STL.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 22,815 hrs · 11,459 cycles

TWO EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROW 4. REINSTALLED THE LAMPS INTO THE SOCKET AND OPERATED OK. CHECK-C 11-6-02 STL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 22,484 hrs · 11,268 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 1 TO 6. REPLACED THE POWER SUPPLY.

Part: LAMP · airframe 22,409 hrs · 11,221 cycles

THE EGRESS LIGHT AT CABIN ROW 31 WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 11-6-02 STL. --CLOSED--

Part: COMPUTER — FAILED (AHRS) · airframe 16,174 hrs · 7,733 cycles

ON DEPARTURE, NUMBER 1 AND 2 COMPASSES DIFFERED BY AT LEAST 45 DEGRESS. MAG COMPASS DIFFERED BY AT LEAST 40 DEGREES FROM KNOWN HEADING. MADE UNSCHEDULED LANDING AT JFK. REPLACED THE NUMBER 1 AHRS COMPUTER (P/N 460800-03-06M0D4), AND THE MAGNETIC COMPASS (P/N C4E). ALSO SWUNG THE MAG COMPASS. CHECK-C 10-14-99 MCI.

Part: CSD — FAILED (LT GENERATOR) · airframe 15,870 hrs · 7,580 cycles

THE LT CSD OIL TEMPERATURE ROSE INTO THE YELLOW BAND. THE APU WAS PREVIOUSLY DEFERRED INOPERATIVE PER MEL. MAKE AN UNSCHEDULED LANDING AT MCI. FOUND OIL TRANSFERRING FROM THE GEARBOX TO THE CSD. REPLACED THE CSD P/N 696233B. ALSO CORRECTED THE APU BY REPLACING THE OVERSPEED STOP RELAY, P/N 306366-2. CHECK-C 10-14-00.

Part: CIRCUIT BOARD — FAILED (PROX SWITCH) · airframe 15,316 hrs · 7,306 cycles

WHEN LANDING GEAR WAS EXTENDED THE LEFT MAIN GEAR GREEN LIGHT FAILED TO COME ON. NO RED LIGHT. ALL LIGHTS TESTED NORMAL. CREW ACCOMPLISHED VISUAL CHECK OF GEAR EXTENSION. LANDED NORMALLY. FOUND A BAD CARD IN THE PROXIMITY SWITCH CONTROL BOX. REPLACED THE BOX. CHECK-C 10-14-99 MCI.

Part: FLOORBEAM — CORRODED (BS 200)

DURING CHECK-C MAINT THE FORWARD GALLEY FLOOR FRAME WAS FOUND CORRODED AT STA 200, RBL 6 IN TO RBL 42 INCHES. REMOVED FLOORBEAM AND FABRICATED PART FROM TWA STOCK. ALODINED AND PAINTED. REINSTALLED FLOORBEAM WITH RIVETS AND ORIGINAL HI-LOKS PER SPM 6-70-01.

Part: FLOORBEAM — CORRODED (BS 180)

DURING CHECK-C MAINT, THE FORWARD GALLEY FLOORBEAM WAS FOUND CORRODED AT STA 180, RBL 6 IN TO RBL 40 INCHES. REPLACED THE PART PER SPM 6-70-01, PAGE 2.

Part: WIRE — BROKEN (CABIN)

STL - FLT 411 - DURING PRE-FLIGHT CHECK, FOUND EGRESS LIGHTING INOPERATIVE AT CABIN SEAT ROW 22. FOUND BROKEN WIRE. CUT OFF BROKEN CONNECTOR AND DAMAGED WIRE AND SPLICED ON NEW CONNECTOR AND WIRE. CHECK-C 10-26-97 MCI. (M)

Part: LIGHT — BROKEN (CABIN)

STL - FLT 202 - DURING OVERNIGHT INSPECTION EGRESS LIGHTING TRACK FOUND BROKEN WITH EXPOSED WIRING, MFG P/N 0105602-001, AT SEAT ROW 33. REPLACED LIGHT TRACK. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C - 10-5-95 - NEW AIRCRAFT.

Part: LENS — MISSING (CABIN)

STL - FLT 202 - DURING PRE-FLIGHT EGRESS LIGHTING RED LENS AT SEAT ROW 31 INOPERATIVE AND MISSING. REPAIRED RED LENS, MFG P/N 0105607-301, AND REPLACED COVER, MFG P/N 008PA57. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C - 10-5-95 - NEW AIRCRAFT.