N483A

Part: FITTING — STRIPPED (REGULATOR VALVE) · airframe 77,994 hrs · 41,363 cycles

DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R THE RT PNEUMATIC PILOT PRESS REGULATOR VLV, BROKEN SENSE LINE, CHAFED SENSE LINE, STRIPPED FITTING & CRACKED SUPPORT BRACKET IAW AMM 36-10-02. OPERATIONAL & LEAK CHECKS NORMAL IAW AMM 36-10-00.

Part: LINE — BROKEN (REGULATOR VALVE) · airframe 77,994 hrs · 41,363 cycles

DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R THE RT PNEUMATIC PILOT PRESSURE REGULATOR VALVE, BROKEN SENSE LINE, CHAFED SENSE LINE, STRIPPED FITTING & CRACKED SUPPORT BRACKET IAW AMM 36-10-02. OPS & LEAK CHECKED NORMAL IAW AMM 36-10-00.

Part: LINE — CHAFED (REGULATOR VALVE) · airframe 77,994 hrs · 41,363 cycles

DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R THE RT PNEUMATIC PILOT PRESS REGULATOR VALVE, BROKEN SENSE LINE, CHAFED SENSE LINE, STRIPPED FITTING & CRACKED SUPPORT BRACKET IAW AMM 36-10-02. OPERATIONAL & LEAK CHECKS NORMAL IAW AMM 36-10-00.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 77,994 hrs · 41,363 cycles

DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R THE RT PNEUMATIC PILOT PRESS REGULATOR VALVE, BROKEN SENSE LINE, CHAFED SENSE LINE, STRIPPED FITTING & CRACKED SUPPORT BRACKET IAW AMM 36-10-02. OPERATIONAL & LEAK CHECKS NORMAL IAW AMM 36-10-00.

Part: REGULATOR — FAULTY (ZONE 100) · airframe 77,994 hrs · 41,363 cycles

DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. R & R THE RT PNEUMATIC PILOT PRESS REGULATOR VLV, BROKEN SENSE LINE, CHAFED SENSE LINE, STRIPPED FITTING & CRACKED SUPPORT BRACKET IAW AMM 36-10-02. OPERATIONAL & LEAK CHECKS NORMAL IAW AMM 36-10-00.

Part: SWITCH — FAULTY (AC BAY) · airframe 77,967 hrs · 41,343 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED MCM 36-95-14 & MCM 0930. R & R LT & RT TEMPERATURE SWITCH. SYS CHECKED NORMAL IAW AMM 36-00-00. SEE ALSO AALA 20160526006.

Part: SWITCH — FAULTY (AC BAY) · airframe 77,967 hrs · 41,343 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED MCM 36-95-14 & MCM 0930. R & R LT & RT TEMPERATURE SWITCHED. SYS CHECKED NORMAL IAW AMM 36-00-00. SEE ALSO AALA 20160525003.

Part: DOOR — OPEN (NLG) · airframe 77,091 hrs · 40,829 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB AFTER GEAR RETRACTION A LOUD NOISE & VIBRATION OCCURRED FROM NOSE GEAR. NLG DOORS FOUND OPEN UPON ARRIVAL. CLOSED & INSPECTED DOORS & LINKAGE IAW 05-91-29. NO DAMAGE FOUND. DOORS MANUALLY CYCLE & CLOSE PROPERLY. OK FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (LT ENGINE) · airframe 76,641 hrs · 40,551 cycles

LEFT ENG OIL STRAINER LIGHT FLICKERED, THEN CAME ON CONTINUOUSLY AFTER TAKEOFF. THE LT ENG WAS BROUGHT BACK TO IDLE. OIL PRESS, TEMP, & QTY NORMAL. EMER WAS DECLARED & FLIGHT RETURNED WITHOUT FURTHER INCIDENT. LT ENG WAS SHUT DOWN ON TAXI IN. ACFT REMOVED FROM SERVICE. R & R OIL FILTER DIFFERENTIAL PRESS SWITCH IAW AMM 79-35-01, LEAK & OPERATIONALLY CHECKED GOOD.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,640 hrs · 40,549 cycles

FORWARD CARGO DOOR, FWD 2ND FROM BOTTOM STOP PAD FITTING CRACKED. INSTALLED NEW CARGO DOOR STOP FITTING IAW AARD 51-00-05-1, DWG 4920233 & DWG CDK2345.

Part: CASTING — CRACKED (LT SPOILER) · airframe 76,640 hrs · 40,549 cycles

LEFT WING, CRACK IN GND SPOILER CASTING INBD EDGE. R & R CRACKED CASTING IAW SRM 51-01-00 & OPERATIONALLY CHECKED SPOILER IAW AMM 27-62-01-2.

Part: STRUCTURE — CORRODED (BS 160-165) · corrosion level 2 · airframe 76,640 hrs · 40,549 cycles

CORROSION ON CABIN SUBFLOOR, FWD SIDE OF STATION 160, APPROX 14 INCHES LT OF CTR. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SCREW — LOOSE (ZONE 100) · airframe 76,346 hrs · 40,371 cycles

UNABLE TO CONTROL PRESSURIZATION EITHER AUTO OR MANUAL. FLIGHT DECLARED AN EMER. RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. CHECKED & FOUND OUTFLOW VLV CONTROL WHEEL MOUNT SCREWS CAME LOOSE, CAUSING WHEEL TO JAMB. SECURED MOUNT SCREWS. OPERATIONS CHECKED NORMAL IAW MM 21-32-00.

Part: TRIM MOTOR — INOPERATIVE (HORIZ STAB) · airframe 76,087 hrs · 40,213 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, PRIMARY STABILIZER TRIM INOPERATIVE ON BOTH CONTROL WHEEL TRIM SWITCHES. ALTERNATE TRIM IS OPERATIVE. R & R PRIMARY STABILIZER TRIM MOTOR IAW MCM 27-94-12.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,977 hrs · 39,594 cycles

LONGERON 23 LT IS CRACKED AT FS 200. PERFORMED SLICE REPAIR IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,977 hrs · 39,594 cycles

LONGERON 25 LT IS CRACKED AT FS 160. PERFORMED SPLICE REPAIR IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,977 hrs · 39,594 cycles

LONGERON 24 LT IS CRACKED AT FS 200. PERFORMED SPLICE REPAIR IAW SRM 53-02-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,723 hrs · 38,839 cycles

OVERWING EMER LIGHTS ILLUMINATED WITH THE COCKPIT EMER LIGHT SWITCH IN THE OFF POSITION. R & R THE BATTERY PACK.

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 73,480 hrs · 38,693 cycles

WORN FASTENER HOLES IN VERTICAL STABILIZER LE REMOVABLE PANEL. INSTALLED DOUBLER REPAIR STRAP IAW SRM 55-03-00 FIGURE 30.

Part: FORMER — CRACKED (LT WING) · airframe 72,917 hrs · 38,364 cycles

LEFT HAND 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 MD80-57-035192.

Part: FORMER — CRACKED (RT WING) · airframe 72,917 hrs · 38,364 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMED IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-05 & EA MD80-57-035192.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,917 hrs · 38,364 cycles

FORWARD CARGO DOOR STOP CRACKED. REPLACED FWD CARGO DOOR STOP IAW AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 72,917 hrs · 38,364 cycles

AFT ACCY, LT HAND SIDE LONGERON 2 CRACKED AT AFT END AFT OF 1418 FRAME. REPLACED SECTION OF LONGERON & INSTALLED LONGERON SPLICE IAW SRM 53-20-00 FIGURE 18.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 72,917 hrs · 38,364 cycles

2 CRACKS IN FASTENER HOLES AT STATION 1474 & LONGERON 19 LT. INSTALLED DOUBLER IAW SRM 53-01-00-001.

Part: LENS — BROKEN (CABIN) · airframe 70,404 hrs · 36,869 cycles

EMERGENCY LIGHT AT ROW 29 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT ROW 29. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,404 hrs · 36,869 cycles

EMERGENCY LIGHT AT ROW 29 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT ROW 29. OPERATION CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,745 hrs · 37,063 cycles

EMERGENCY CABIN & COCKPIT OVERHEAD LIGHTING WILL NOT SHUT-OFF. RECHARGED BATTERY. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,340 hrs · 36,281 cycles

LEFT NUMBER 2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK AT B5-4 POSITION FOR LEFT NUMBER 2 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 69,340 hrs · 36,281 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE CONNECTION ON BATTERY PACK B5-27 TERMINAL 5 FOR TAIL COMPARTMENT EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,340 hrs · 36,281 cycles

AFT GALLEY CEILING EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE CONNECTION ON BATTERY PACK B5-107, TERMINAL 5. OPS CHECK NORMAL.

Part: SOCKET — DIRTY (CABIN) · airframe 69,340 hrs · 36,281 cycles

CEILING CENTER EMERGENCY LIGHT JUST FORWARD OF AFT BULKHEAD DOOR INOPERATIVE. CLEANED LIGHT SOCKET CONTACT ON BASE. OPS CHECK NORMAL.

Part: ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 69,118 hrs · 36,162 cycles

ORD - CREW REPORTED SLAT DISAGREE LIGHT ILLUMINATED. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH AUTOSLAT ACTUATORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 68,912 hrs · 36,052 cycles

AFT CARGO STATION 1212 UPPER SIDE OF FRAME NUT PLATE ATTACH HOLE ELONGATED. INSTALLED REPAIR DOUBLER PER EA MD80-53-027356.

Part: DRAIN PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,912 hrs · 36,052 cycles

SUBFLOOR UNDER G-1 DRAIN PAN IS CORRODED. INSTALLED DOUBLER UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,912 hrs · 36,052 cycles

SKIN AT INBOARD CORNER OF LEFT RADOME HINGE IS CRACKED. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 77.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,912 hrs · 36,052 cycles

CORROSION ON LONGERON 27 LEFT FROM STATIONS 1286 TO 1288. INSTALLED LONGERON SPLICE PER SRM 53-02-00.

Part: SKIN — DAMAGED (TE FLAP) · airframe 68,912 hrs · 36,052 cycles

LEFT WING TRAILING EDGE: DAMAGE TO BOTTOM SIDE OF INBOARD FLAP, OUTBOARD WEDGE, INBOARD END. INSTALLED NEW SKIN REPAIR PER SRM 51-70-06.

Part: BEAM — CORRODED (FUSELAGE) · airframe 68,912 hrs · 36,052 cycles

MID CARGO DOOR BEAM CORRODED FROM STATIONS 645 TO 674, LONGERON 28 RIGHT. REMOVED CORROSION AND INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,912 hrs · 36,052 cycles

CORROSION BEYOND MANUAL LIMITS IN AFT CARGO AT STATION 1322 BETWEEN LONGERONS 29 LEFT AND 29 RIGHT. REMOVED AND REPLACED CORRODED J-ANGLE AT STATION 1322 BETWEEN LONGERONS 29 LEFT AND 29 RIGHT.

Part: DOOR — DAMAGED (CABIN) · airframe 68,912 hrs · 36,052 cycles

FORWARD ENTRY DOOR DAMAGED AT LOWER FORWARD CORNER. STRAIGHTENED LOWER EDGE OF FORWARD ENTRY DOOR, DYE CHECKED AND NO CRACKS FOUND. INSTALLED DOUBLER PER AARD 52-10-00-02 FIGURE 1.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,912 hrs · 36,052 cycles

SUB-FLOOR AT STATION 160, RIGHT BUTTLINE 11 CORRODED. INSTALLED SUB FLOOR DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,912 hrs · 36,052 cycles

SUBFLOOR UNDER G-1 DRAIN PAN IS CORRODED. REMOVED CORROSSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,912 hrs · 36,052 cycles

RIGHT WINDOW RING PAN CRACKED UPPER AFT CORNER AFT OF STATION 788. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SKIN — WORN (ENTRY DOOR) · airframe 68,912 hrs · 36,052 cycles

FORWARD ENTRY DOOR HAS WEAR ON OUTER SKIN AT HOLD OPEN HOOK CUTOUT. INSTALLED DOUBLER PER SRM 52-05-00 FIGURE 20A.

Part: BATTERY — DIRTY (CABIN) · airframe 68,589 hrs · 35,866 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 18 TO 27 INOPERATIVE. CLEANED CONTACTS ON BATTERY AND RESEATED. OPS CHECKED NORMAL.

Part: UPLOCK SWITCH — DEFECTIVE (STAIRWAY DOOR) · airframe 63,557 hrs · 33,038 cycles

DFW - CREW REPORTED AFT STAIRWAY DOOR LIGHT FLICKERED IN FLIGHT AND TOWARD THE END CAME ON STEADY. NO BUFFETING AND FUEL BURN NORMAL. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. REPLACED LEFT UPLOCK SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,419 hrs · 32,967 cycles

SEAT EGRESS LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AT AB5-1. OPS CHECKED NORMAL.

Part: RIB — WORN (LE SLAT) · airframe 63,308 hrs · 32,910 cycles

SLAT BRACKET ON OUTBOARD SKIN AT RIB NUMBER 15 WORN. REPLACED SLAT BRACKET AND NEW SKIN ON LEADING EDGE OUTBOARD PER ESO 80117

Part: VALVE — STICKING (FUEL HEAT) · airframe 62,568 hrs · 32,523 cycles

DFW - CREW REPORTED DURING CLIMB OUT THE RIGHT FUEL HEAT LIGHT ILLUMINATED WITH CORRESPONDING RISE IN OIL TEMPERATURE. ACCOMPLISHED QRH PROCEDURES AND LIGHT REMAINED ON. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. FOUND RIGHT ENGINE FUEL HEAT VALVE WAS STICKING PARTIALLY OPEN. REPLACED RIGHT ENGINE FUEL HEAT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PITOT TUBE — FAILED (PITOT/STATIC SYS) · airframe 62,109 hrs · 32,274 cycles

INFLIGHT BUR TO DFW. NUMBER 4 RUDDER LIMITER HEATER CURRENT INDICATED 10 BEFORE CIRCUIT BREAKER 30Z TRIPPED. LANDED LAS WITHOUT INCIDENT. REMOVED AND REPLACED RUDDER LIMITER PITOT TUBE PER MM 34-11-02.

Part: WEB — DAMAGED (FUSELAGE) · airframe 61,712 hrs · 32,047 cycles

DEEP GOUGE IN RIGHT WALL DUE TO CONTACT WITH RIGHT NOSE GEAR STEERING CYLINDER. INSTALLED DOUBLER REPAIR PER SRM 53-05-00.

Part: TAB — SPLIT (RT WING) · airframe 61,659 hrs · 32,016 cycles

RIGHT TAB TRIM TRAILING EDGE SPLIT OPEN. REPAIRED TRAILING EDGE UNDER SRM 51-70-01A.

Part: TRIM TAB — SPLIT (AILERON) · airframe 61,659 hrs · 32,016 cycles

RIGHT TAB TRIM TRAILING EDGE SPLIT OPEN. REPAIRED TRAILING EDGE UNDER SRM 51-70-01A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,282 hrs · 31,811 cycles

FORWARD CEILING EMERGENCY LIGHTS OUT. REPLACED FORWARD EMERGENCY BATTERY PACK. OPS CHECK NORMAL.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,282 hrs · 31,811 cycles

FLASHLIGHT STRAP BROKEN OFF FLASHLIGHT OUTSIDE FORWARD AFT RIGHT LAVATORY. REPLACED STRAP FOR FLASHLIGHT OUTSIDE AFT RIGHT LAVATORY.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,282 hrs · 31,811 cycles

FLASHLIGHT STRAP BROKEN OFF FLASHLIGHT BY FLIGHT ATTENDANT SEAT AFT GALLEY DOOR. REPLACED STRAP FOR FLASHLIGHT BY FLIGHT ATTENDANT SEAT AFT GALLEY DOOR.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,282 hrs · 31,811 cycles

FLASHLIGHT STRAP BROKEN OFF FLASHLIGHT BY FLIGHT ATTENDANT SEAT AFT GALLEY DOOR. REPLACED STRAP FOR FLASHLIGHT BY FLIGHT ATTENDANT SEAT AFT GALLEY DOOR.

Part: BATTERY — NOT SEATED (CABIN) · airframe 61,282 hrs · 31,811 cycles

CEILING EMERGENCY LIGHT BY AFT RIGHT LAVATORY INOPERATIVE. RESET AFT EMERGENCY BATTERIES. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 61,282 hrs · 31,811 cycles

CEILING EMERGENCY LIGHT ABOVE FLIGHT ATTENDANT SEAT BY AFT VENTRAL DOOR INOPERATIVE. RESET AFT EMERGENCY BATTERIES. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 57,701 hrs

LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERIES AT AFT RIGHT LAVATORY FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

MSP - EMERGENCY LIGHT AT FIRST CLASS GALLEY WALL BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT FORWARD FIRST CLASS GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT MOUNT)

LGA - AFT FORWARD EMERGENCY FLASHLIGHT STRAP BROKEN. REPLACED STRAP FOR AFT FORWARD EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

PHX - BATTERY PACKS FOR EMERGENCY LIGHTS IN FORWARD CABIN STATION 211 CENTER FAILED FUNCTIONAL TEST. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN FORWARD CABIN STATION 211 CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

PHX - BATTERY PACKS FOR EMERGENCY LIGHTS IN AFT CABIN STATION 1190 RIGHT FAILED FUNCTIONAL TEST. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN AFT CABIN STATION 1190 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

PHX - FOUND EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 902 RIGHT FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT TAIL CONE CEILING INOPERATIVE. REPLACED BATTERY PACK AT RIGHT HAND AFT LAVATORY CEILING FOR EMERGENCY LIGHTS AT TAIL CONE CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK AT FORWARD OVERHEAD BIN AT SEATS 20DEF FOR EMERGENCY LIGHTS AT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING TOW TO GATE, OVERWING EMERGENCY EXIT LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED BATTERY PACKS FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - FORWARD AISLE EMERGENCY LIGHTS NEAR FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD AISLE EMERGENCY LIGHTS NEAR FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BRAKE — DRAGGING (MLG)

NUMBER FOUR BRAKE OVER TEMPERATURE. REPLACED NUMBER FOUR WHEEL, BRAKE, AND AXLE SLEEVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — PINCHED (EMERGENCY LIGHT)

RDU EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN INOPERATIVE. FOUND PINCHED WIRE ON OUTBOARD SEAT TRACK. REPAIRED WIRE FOR EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DFW - TWO EACH OVERHEAD EMERGENCY LIGHTS AT AIRSTAIRS CATWALK AND ONE TAIL CONE EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR TWO EACH OVERHEAD EMERGENCY LIGHTS AT AIRSTAIRS CATWALK AND FOR ONE TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AUS - EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK IN AFT RIGHT LAVATORY FOR EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX EMERGENCY LIGHTS IN AFT CABIN DROP CEILING PANELS AND NR 1 EMERGENCY LIGHT FOR TAIL SLIDE INOPERATIVE. REPLACED B5-27 BATTERY PACK/CHARGER ASSEMBLY AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — DAMAGED (A/C BAY)

FLT 1719 - DFW-SEA - ON CLIMB-OUT AIRCRAFT HAD THE SMELL OF A PAK OVERHEAT FOLLOWED BY SMOKE IN THE CABIN. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FURTHER INVESTIGATION REVEALED A HOLE IN LEFT PACK HEAT EXCHANGER WATER SPRAY LINE. REMOED AND REPLACED LINE. PACK BURN ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DETACHED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REATTACHED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — MALFUNCTIONED (TAIL SECTION)

DFW - FLT 1039 - EN ROUTE DFW-PHX - AFTER TAKEOFF DFW TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. COMPLETED CHECKLIST AND LIGHT EXTINGUISHED THEN RE-ILLUMINATED AND FINALLY EXTINGUISHED. RETURNED AND LANDED DFW WITHOUT INCIDENT. INSPECTED TAIL COMPARTMENT AREA FOR LEAKS. NO LEAKS NOTED, PRECAUTIONARY REPLACED LEFT AND RIGHT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ARM/ON SWITCH AT ATTENDANT STATION INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ARM/ON SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT STAIRS SIDEWALL ON LEFT SIDE INOPERATIVE. REPAIRED LEFT SIDE EMERGENCY EXIT LIGHTS AT AFT STAIRS SIDEWALL WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUT — DEFLATED (NLG)

ORD - FLT 1460 - EN ROUTE ORD-BDL, NOSE LANDING GEAR WOULD NOT RETRACT. RED NOSE GEAR LIGHT REMAINED ILLUMINATED. RETURNED AND LANDED WITHOUT FURTHER INCIDENT. SERVICED NOSE LANDING GEAR WITH NITROGEN. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: CLAMP — LOOSE (TAIL BAY)

DFW - FLT 1890 - DURING CLIMB-OUT, BETWEEN 8000-10,000 FT, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY PROCEDURE CHECKLIST COMPLIED WITH AND LIGHT EXTINGUISHED. RETURNED DFW AND LANDED WITHOUT INCIDENT. RE-TORQUED AUGMENTATION VALVE CLAMPS, AND COMPLETED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY HANDLE RELEASE FLOOR LIGHT WOULD NOT ILLUMINATE. CLEANED CONTACTS ON LAMPS. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE IN FORWARD CABIN. REPAIRED EMERGENCY EXIT FLOOR PATH CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CUSP — CORRODED (BS 685)

TUL - CORORSION AT CUSP STA 685, RT. CUT OUT CORROSION, INSTALLED DOUBLER PER SRM 53-01, FIG 4, SHEET 3. TST: 23,817.05 HOURS. CYCLES, 13,327. (X)