N9402W

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 64,640 hrs · 31,491 cycles

CARGO MID CX DOOR FWD LOWER DOOR STOP CRACKED. INSTALLED NEW DOOR STOP FITTING.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 64,640 hrs · 31,491 cycles

CARGO AFT CX DOOR FWD MIDDLE DOOR STOP IS CRACKED. INSTALLED NEW DOOR STOP FITTING ASSEMBLY.

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 64,640 hrs · 31,491 cycles

CRACKED BRACKET IN FWD SERVICE DOOR UPPER AFT CORNER. R & R BRACKET.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,513 hrs · 31,414 cycles

AFT TAIL SLIDE EMER LIGHTS DO NOT TEST. R & R EMER LIGHT BATTERY PACK FOR TAIL SLIDE IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,513 hrs · 31,414 cycles

FORWARD OVERWING EMER EXIT LIGHTS DO NOT TEST. R & R BATTERY PACK FOR FWD OVERWING EMER LIGHTS IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,513 hrs · 31,414 cycles

OVERHEAD EMER LIGHTS AT ROW 22 - 26 DO NOT TEST. R & R BATTERY PACK FOR EMER LIGHTS AT ROWS 22 - 26 IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,826 hrs · 31,044 cycles

CRACKED INTERCOSTAL BETWEEN STATION 1271 - 1287. REPLACED INTERCOSTAL IAW AARD 51-00-05 & DWG 9936580.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,826 hrs · 31,044 cycles

INTERCOSTAL CRACKED 2 EACH BELOW CABIN FLOOR. REPLACED INTERCOSTAL IAW AARD 51-00-05 & DWG 9936580.

Part: FUEL CONTROL — DEFECTIVE (LT ENGINE) · airframe 63,034 hrs · 30,629 cycles

AIR INTERRUPT, ACFT EXPERIENCED AN UNCOMMANDED LT ENGINE ROLLBACK AT CRUISE ALTITUDE. ENGINE THRUST MOVED TO IDLE. POWER REGAINED IN DESCENT. DIVERTED, EMERGENCY DECLARED, LANDED UNEVENTFULLY . REMOVED AND REPLACED THE RIGHT ENGINE FUEL PUMP AND FUEL CONTROL UNIT IAW MCM 73-94-03, 73-94-04 AND 73-91-99, PERFORMED ADJUSTMENT TEST IAW 71-91-03. LEAK CHECKED GOOD. SYSTEM CHECKEDS NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,018 hrs · 29,587 cycles

CRACK IN FUSELAGE SKIN LT OF VERTICAL STABILIZER INLET DUCT. INSTALLED DOUBLER REPAIR IAW SRM 53-04-00 & EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,018 hrs · 29,587 cycles

SHEAR TIE FROM STATIONS 1437 TO 1438 & LONGERON 2 RT CRACKED. REPLACED SHEAR TIE IAW AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,018 hrs · 29,587 cycles

CANT FRAME 1510 CRACKED AT 9 O`CLOCK POSITION, AT TAIL CONE GUIDE PIN. REMOVED DAMAGE & INSTALLED DOUBLER IAW SRM 53-01-00.

Part: FORMER — CRACKED (LE SLAT) · airframe 61,018 hrs · 29,587 cycles

RT HAND WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED DOUBLER IAW EA MD80-57-033312.

Part: FORMER — CRACKED (LE SLAT) · airframe 61,018 hrs · 29,587 cycles

LT HAND WING LE NR 4 SLAT TRACK INBD FORMER, INSTALLED DOUBLER IAW EA MD80-57-033312.

Part: TRANSMITTER — INOPERATIVE (WEATHER RADAR) · airframe 59,281 hrs · 28,631 cycles

CREW REPORTED WEATHER RADAR FAILED IN FLIGHT. FLIGHT DIVERTED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR RECEIVER TRANSMITTER AND CONTROL PANEL. SYS GROUND CHECK NORMAL OPERATION (CLOSED)

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 57,702 hrs · 27,869 cycles

ONT - INFLIGHT SJD-LAX. CREW REPORTED BOTH AUTOPILOTS FAILED INFLIGHT. FLIGHT DIVERTED ONT LANDED WITHOUT INCIDENT. PLACARD BOTH AUTOPILOTS PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED NUMBER ONE DIGITAL FLIGHT GUIDANCE COMPUTER AND AILERON SERVO DRIVE AT LAX ON 11/23/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,802 hrs · 27,412 cycles

RIGHT CUSP TEE ANGLE IS CRACKED FORWARD OF FORWARD SERVICE DOOR AT APPROXIMATE STATION 150. INSTALLED CUSP ANGLE FILLER AND DOUBLERS PER SRM 53-05-00 FIGURE 55 SHEET 2.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,802 hrs · 27,412 cycles

CRACK IN CUSP SHEET AT FASTENER HOLE AT STATION 158. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 56,802 hrs · 27,412 cycles

AFT CARGO DOOR AFT FRAME CRACKED AT NUMBER 5 BEAM. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA COMP-52-024887.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,802 hrs · 27,412 cycles

CORROSION ON TIEDOWN TRACK RIGHT SIDE FROM STATIONS 1110 TO 1155. REMOVED AND REPLACED RIGHT TIE DOWN TRACK STATIONS 1110 TO 1155 PER AARD 51-00-05-1, SRM 51-30-05, SRM 51-30-01 AND BOEING DRAWING 5936663.

Part: SKIN — BENT (ENTRY DOOR) · airframe 56,802 hrs · 27,412 cycles

CABIN FORWARD ENTRY DOOR SKIN BENT AT LOWER AFT CORNER. STRAIGHTENED LOWER AFT SKIN AND INSTALLED DOUBLER PER AARD 52-10-00-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,802 hrs · 27,412 cycles

STATION 905 ABOVE CENTER FUEL TANK HAS VERTICAL ANGLE CRACKED JUST BELOW NUMBER 4 SEAT TRACK. INSTALLED SERVICEABLE VERTICAL ANGLE PER AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,802 hrs · 27,412 cycles

RIGHT CUSP FROM STATIONS 522 TO 541 CORRODED. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,802 hrs · 27,412 cycles

CRACK IN LEFT CUSP AT LIGHTNING HOLE OUTBOARD OF SEAT TRACK NUMBER 1 AT STATION 412. INSTALLED DOUBLER LEFT CUSP AT STATION 412 PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,802 hrs · 27,412 cycles

CUSP AT RIGHT STATION 886 HAS DAMAGED HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,802 hrs · 27,412 cycles

LEFT CUSP AT STATION 886, OUTBOARD AFT NUMBER 1 SEAT TRACK MOUNT BOLT HOLE IN CUSP IS CRACKED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,802 hrs · 27,412 cycles

RIGHT CUSP STATION 905 HAS DOUBLE DRILLED HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,802 hrs · 27,412 cycles

CORROSION ON SUBFLOOR UNDER NUMBER 2 GALLEY TIE DOWN STATION 218. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 55,113 hrs · 26,544 cycles

YYC - OTHER AIRLINE REPORTED SPARKS FROM LEFT ENGINE ON TAKEOFF ROTATION AND ON INITIAL CLIMBOUT. CREW REPORTED NO ABNORMAL INDICATIONS. EMERGENCY DECLARED FLIGHT RETURNED YYC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT YYC ON 11/20/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,836 hrs · 24,971 cycles

STATION 1418 FRAME CRACKED AT LONGERON 2 LEFT. REPAIRED PER EA MD80-53-013026.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,836 hrs · 24,971 cycles

LONGERON 2 LEFT CRACKED AT FRAME 1418. REPAIRED PER AARD 53-30-00-2 AND EA MD80-53-013074.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,836 hrs · 24,971 cycles

STATION 1510 CANT FRAME CRACKED LOWER LEFT TAIL CONE ALIGNMENT PIN. INSTALLED REPAIR DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: LONGERON — CRACKED (ZONE 200) · airframe 51,836 hrs · 24,971 cycles

LONGERON 2 RIGHT CRACKED AT STATION 1418. INSTALLED DOUBLER PER AARD 53-30-00-2.

Part: FRAME — CRACKED (BS 1510) · airframe 51,836 hrs · 24,971 cycles

STATION 1510 CANT FRAME CRACKED AT TAIL CONE ALIGNMENT PIN ABOVE MAIT LIGHT SWITCH. INSTALLED DOUBLER REPAIR PER SRM 53-01-00.

Part: SKIN — CRACKED (ZONE 100) · airframe 51,836 hrs · 24,971 cycles

RIGHT FORWARD FUSELAGE AT AFT STRUT GEAR DOOR FOR NOSE LANDING GEAR HAS AFT HINGE CUTOUT WITH CRACK IN SKIN. ROUTED OUT CRACKED SKIN AND INSTALLED REPAIR DOUBLER AS PER SRM 53-05-00.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,836 hrs · 24,971 cycles

STATION 1510 CANT FRAME CRACKED LOWER RIGHT TAIL CONE ALIGNMENT PIN. INSTALLED REPAIR DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SHUTOFF VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 50,680 hrs · 24,397 cycles

ORD - CREW REPORTED STRONG ACRID ODOR IN CABIN ON TAKEOFF THEN SAME ODOR DURING DESCENT. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH PRESSURE REGULATING SHUT-OFF VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,539 hrs · 24,335 cycles

FOUND FORWARD HALF OF SEAT EMERGENCY LIGHTS WEAK. REMOVED AND REPLACED BATTERY PACK AT FORWARD DROP CEILING PANEL SEAT EMERGENCY LIGHTS, OPS CHECKED NORMAL.

Part: PISTON — DEFECTIVE (NLG) · airframe 48,788 hrs · 23,587 cycles

SEA - AIRCRAFT UNABLE TO RETRACT NOSE LANDING GEAR. EMERGENCY DECLARED, RETURNED TO SEA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR SHOCK STRUT PISTON. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,578 hrs · 22,886 cycles

PASSENGER SEAT MOUNTED EMERGENCY LIGHT BATTERY PACK IS WEAK. REMOVED AND REPLACED BATTERY PACK.

Part: SEAL — LEAKING (NLG STRUT) · airframe 46,581 hrs

INFLIGHT CREW REPORTED NOSE LANDING GEAR RED INDICATION WITH AIR NOISE. SUSPECTED GEAR NOT FULLY RETRACTED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR STRUT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GENERATOR — FAILED (NR 1 ENGINE) · 46,064 cycles

INFLIGHT T1363/24SEP. LT ENGINE GENERATOR OFF LINE. AUXILIARY POWER UNIT (APU) WOULD NOT COME ON LINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LT CONSTANT SPEED DRIVE AND GENERATOR. APU REPLACED ON 24 SEP AT DFW. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,547 hrs

ORD EMERGENCY LIGHT AT RT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: GCU — FAILED (NR 2 ENGINE) · airframe 45,215 hrs

STL INFLIGHT T2361/17JUN ORD TO DFW. CREW REPORTED LOSS OF RT AC BUD POWER AND RT ENGINE DRIVEN GENERATOR WOULD NOT HOLD A LOAD. LANDED STL WITHOUT INCIDENT. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 17D TO 27D INOPERATIVE. REPLACED RESEATED BATTERIES IN BATTERY PACK AT SEAT ROW 20D FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 17D TO 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANYARD — FRAYED (R1 DOOR SLIDE)

LGA - RIGHT NUMBER ONE DOOR SLIDE LANYARD CABLE FRAYED. REPLACED RIGHT NUMBER ONE DOOR SLIDE LANYARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT SEAT ROWS 28ABC AND 30ABC INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROWS 28ABC AND 30ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

LGA SEAT MOUNTED EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BULBS FOR SEAT MOUNTED EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - EMERGENCY LIGHTS AT FORWARD AND AFT GALLEY AND LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD AND AFT GALLEY AND LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL UNIT — MALFUNCTIONED (ELECTRICAL SYS)

RDU - SEVERAL CIRCUIT BREAKERS POPPED AFTER TAKEOFF. LANDED RDU WITHOUT INCIDENT. SECURED SEVERAL LOOSE WIRES ON RELAY. REPLACED BUS CONTROL UNIT AND TWO A PHASE RIGHT BUS CIRCUIT BREAKERS AND ONE A PHASE GROUND SERVICE BUS POWER CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1 TO 20 INOPERATIVE. REPLACED BATTERY PACKS AT FORWARD ROW AND MID ROW FOR EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 8D AND 18D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEATS 8D AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHT BATTERY PACK ASSEMBLIES AT B523, B5104 AND L2694 INOPERATIVE. REPLACED BATTERY PACK FOR B523, B5104 AND L2694 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACTOR — LOOSE (BATTERY PACK)

OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. ADJUSTED AND CLEANED BATTERY CONTACTS FOR OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROW 14 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,286 hrs · 16,302 cycles

THE AFT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,286 hrs · 16,302 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 20 TO 26. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,983 hrs · 15,468 cycles

THE CEILING EMERGENCY LIGHT WAS INOPERATIVE ABOVE SEAT 18B, 19B, AND 20B. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 9-4-02 STL. --CLOSED--

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,892 hrs · 15,415 cycles

THE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 9-4-02 STL.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 30,548 hrs · 15,236 cycles

THE EMERGENCY FLOOR PATH LIGHTING HAD BROKEN WIRES AT ROW 16. REPLACED LIGHT HARNESS. CHECK-C 9-4-02. --CLOSED--

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 30,485 hrs · 15,200 cycles

THE EGRESS LIGHT WAS INOPERATIVE AT ROW 16 AND AT ROWS 20 TO 23. REPLACED THE LAMP P/N 79991-000 AT ROW 16, AND RESEATED THE CONNECTOR AT ROW 23. CHECK-C 9-4-02 STL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,266 hrs · 15,070 cycles

THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 27 TO 29. REPLACED BATTERIES FOR THE EMERGENCY LIGHTS.

Part: BATTERY — NOT SEATED (CABIN) · airframe 29,400 hrs · 14,577 cycles

THE EGRESS LIGHT STRIP IN THE FWD SECTION OF COACH WAS INOPERATIVE. OPERATED MEL ONE LEG AND THEN THE BATTERIES IN THE POWER SUPPLY WERE PROPERLY SEATED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 29,257 hrs · 14,484 cycles

DURING CHECK-C MAINT LONGERON 2L WAS CRACKED AT STA 1418, .25 INCH LONG. INSTALLED REPAIR SPLICE PER SRM 53-02, FIG 18.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,458 hrs · 12,354 cycles

THE OVERHEAD EMERGENCY LIGHTS IN THE COCKPIT AND FORWARD ENTRY WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 12-14-00 MCI.

Part: LINE — CRACKED (HYDRAULIC SYS) · airframe 24,517 hrs · 11,846 cycles

AN ACRID ELECTRICAL TYPE SMELL WAS NOTED IN THE COCKPIT AND CABIN WHEN ENGINE ANTI-ICE WAS TURNED ON. FOUND A PINHOLE CRACK IN A HYDRAULIC LINE, AND THE LEAK WAS GETTING INTO THE AIR CONDITIONING SYSTEM. FABRICATED AND REPLACED THE LINE ON THE RT SIDE OF THE TAIL COMPARTMENT AT THE RT ELEVATOR ACCUMULATOR. CHECK-C 9-19-99 STL.

Part: POWER SUPPLY — INOPERATIVE (RT & LT OVERWING) · airframe 24,223 hrs · 11,692 cycles

THE LT AND RT FWD OVERWING EMERGENCY EXIT LIGHTS, AND THE EGRESS LIGHT AT ROW 7, WERE INOPERATIVE. REPLACED THE POWER SUPPLY (P/N 60-0304-51LB) FOR THE EXIT LIGHTS, AND THE LIGHT SOCKET (P/N 0105606-003) FOR THE EGRESS MALFUNCTION. CHECK-C 9-19-99 STL.

Part: WIRE — EXPOSED (CABIN) · airframe 23,834 hrs · 11,499 cycles

THE EGRESS LIGHT WIRING WAS EXPOSED AND SEPARATED BETWEEN ROWS 16 AND 17 ON RT SIDE OF AISLE. SPLICED THE BREAK AND SECURED THE WIRES. CHECK-C 9-19-99 STL. ---CLOSED---

Part: LIGHT — INOPERATIVE (ROW 11 & 19) · airframe 23,113 hrs · 11,068 cycles

THE CABIN EGRESS LIGHTS WERE INOPERATIVE JUST AFT OF SEAT ROWS 11 AND 19. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 9-19-99 STL.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 23,113 hrs · 11,068 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AFT OF THE FORWARD GALLEY AND AFT OF SEAT ROW 10. REPLACED LIGHT ASSEMBLY. CHECK-C 9-19-99 STL.

Part: LAMP — FAILED (ROW 11 & 18)

CABIN EGRESS LIGHTS WERE FOUND INOPERATIVE AT ROWS 11 AND 18. REPLACED LAMPS AT BOTH POSITIONS. CHECK-C 10-25-98 STL.

Part: LIGHT — INOP (CABIN)

FOUND EGRESS LIGHTS INOPERATIVE AT FORWARD GALLEY AND AT ROWS 4, 5, 17, 22, 26, AND 33. REPLACED LIGHT MODULES, MFG 0105606-002 AND 0105606-003. CHECK-C 10-25-98 STL.

Part: WIRE — BROKEN (CABIN)

SEVERAL EGRESS LIGHTS WERE INOPERATIVE IN THE FWD CABIN. REPAIRED BROKEN WIRE AT THE END OF THE FIRST CLASS SECTION. CHECK-C 10-25-98 STL.

Part: STOPS — OUT OF POSITION (TAIL CONE)

TAIL CONE UNSAFE LIGHT CAME ON DURING DEPARTURE OUT OF BWI. MADE UNSCHEDULED LANDING AT DCA. FOUND CABLE BALL STOPS HAD BECOME UNSEATED. REINSTALLED CABLE BALL STOPS AT UNSAFE LIGHT SWITCH. CHECK-C 10-29-97 LAX.

Part: LIGHT — INOPERATIVE (CABIN)

STL - FLT 765 - DURING GROUND CHECK, FOUND ONE EGRESS LAMP INOPERATIVE AT ROW 14, AND EGRESS LIGHTING ROW 30 TO ROW 33 INOPERATIVE. REPLACED LAMP AT ROW 14, MFG P/N 7732. FOUND EXPOSED WIRES NEAR SEAT ROW 24, AND REPLACED LIGHT STRIP. CHECK-C 10-29-97 LAX. (X)

Part: LENS — INOPERATIVE (CABIN)

STL - FLT 467 - DURING PREFLIGHT, CREW REPORTED RED EGRESS LIGHT STRIP INOP AT ROW 22. REPLACED LENS. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

STL - SHORTLY AFTER TAKEOFF, STRONG FUMES WERE DETECTED IN THE AFT CABIN. A PACK BURNOUT WAS PERFORMED AND THE TAIL COMPARTMENT DUCTING WAS INSPECTED. SYSTEM OPERATIONAL CHECK NORMAL. (M)