N467AA

Part: CHIP DETECTOR — LEAKING (APU) · airframe 78,575 hrs · 41,959 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL. & ACFT NOT OVERWEIGHT. DURING CLIMB, THE FLIGHT ATTENDANTS REPORTED SMOKE & FUMES IN THE CABIN. FUMES DISSIPATED DURING RETURN TO FIELD. ACCOMPLISHED CAR MCM 21-96-01 & FOUND APU OIL INGESTION. APU OIL GEARBOX CHIP DETECTOR WAS FOUND TO BE LEAKING. R & R APU MAGNETIC DRAIN PLUG IAW AMM 40-90-12. LEAK CHECK GOOD.

Part: BATTERY PACK — FAILED (CABIN) · airframe 78,295 hrs · 41,789 cycles

WHEN REMOVING POWER FROM ACFT, SECTION OF EMER LIGHTS ILLUMINATED. UNABLE TO TURN OFF EVEN AFTER RESTORING POWER & RECYCLING SYS. REPLACED EMER LIGHT BATTERY PACK. ACFT IN BASE MX.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,075 hrs · 41,647 cycles

SEAT ROW 21AB & 21DEF EXIT HATCH LIGHT COMES ON & IMMEDIATELY GOES OUT. R & R EMER EXIT HATCH BATTERY PACK IAW AMM 33-53-00. OPERATIONALLY CHECKED GOOD. THE ACFT WAS NOT GNDED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 77,920 hrs · 41,552 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS IN ROWS 22 - 27 FAILED TO TEST. R & R POWER SUPPLY B5-106 IAW AMM 33-53-00. OPERATIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 77,920 hrs · 41,552 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS IN ROWS 3 - 7 FAILED TO TEST. R & R POWER SUPPLY B5-100 IAW AMM 33-53-00. OPERATIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 77,920 hrs · 41,552 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS IN ROWS 12 - 17 FAILED TO TEST. R & R POWER SUPPLY B5-102 IAW AMM 33-53-00. OPERATIONAL CHECKED NORMAL.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 77,920 hrs · 41,552 cycles

AIRCRAFT WAS NOT GNDED. EGRESS POWER SUPPLY AB5-3 FAILS TO TEST. R & R POWER SUPPLY IAW AMM 33-60-98. TESTED NORMAL.

Part: PORTABLE LIGHT — DEFECTIVE (CABIN) · airframe 77,312 hrs · 41,181 cycles

L1 DOOR PORTABLE EMER LIGHT LOCKING TAB MISSING. REPLACED L1 DOOR PORTABLE EMER LIGHT IAW AMM 33-53-00. OPERATIONALLY CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,506 hrs · 40,149 cycles

EMERGENCY LIGHT WILL NOT TEST. R & R BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,506 hrs · 40,149 cycles

EMERGENCY PORTABLE BATTERY PACK LIGHT INOPERATIVE, WILL NOT TEST. REPLACED EMER PORTABLE BATTERY PACK LIGHT ASSEMBLY IAW AMM 33-53-00.

Part: SERVO — FAILED (ELEVATOR) · airframe 75,215 hrs · 39,976 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT EXPERIENCED ALTERNATE TRIM MALFUNCTION. WHEN NR 2 AUTOPILOT WAS DISCONNECTED THE PITCH UP STOPPED. R & R DUPLEX ELEVATOR SERVO DRIVE IAW AMM 22-12-01 & NR 2 DFGC IAW AMM 22-01-01. ACCOMPLISHED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: CASTING — CRACKED (FUSELAGE) · airframe 74,937 hrs · 39,817 cycles

FORWARD CARGO DOOR TOP FWD DOOR STOP CASTING IS CRACKED. R & R CASTING IAW SRM 51-30-05.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 74,861 hrs · 39,771 cycles

PORTABLE EMER LIGHT AT L1 DOOR IS INOPERATIVE. R & R PORTABLE EMER LIGHT. SYS CHECKED NORMAL.

Part: RIB — CRACKED (LT WING) · airframe 74,743 hrs · 39,698 cycles

LEFT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED LT REPAIR DOUBLER IAW SRM 51-00 & EA MD80-57-037139.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 71,631 hrs · 37,834 cycles

DFW CREW REPORTED STRONG OIL ODOR IN THE CABIN FOLLOWED BY A STRONG VIBRATION IN THE TAIL DURING CLIMB OUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. FOUND EVIDENCE OF BIRD STRIKE TO LT ENGINE WITH TWO BLADES BENT & NR 1 BEARING LEAKING. REPLACED LT ENGINE AT DFW ON 08/11/2013. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,499 hrs · 37,749 cycles

CRACK IN AFT WHEEL WALL FRAME AT TOP OTBD END ABOVE FLAP BUS CABLE PULLEYS. INSTALLED REPAIR DOUBLER & -5 JAMB SECTION IAW SRM 51-70-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,499 hrs · 37,749 cycles

RT HAND SIDE FUSELAGE SKIN CRACKED AT STATION 1437, BETWEEN LONGERONS 3 & 4 RT. CUT OUT DAMAGE & INSTALLED DOUBLER & FILLER IAW SRM 53-04-00 FIGURE 27.

Part: COVER — MISSING (CABIN) · airframe 70,530 hrs · 37,179 cycles

EMERGENCY EXIT LIGHT COVER AT FORWARD GALLEY DOOR MISSING. REPLACED EMERGENCY EXIT LIGHT COVER AT FORWARD GALLEY DOOR. OPS CHECKS NORMAL.

Part: GUARD — MISSING (FUEL PANEL) · airframe 70,530 hrs · 37,179 cycles

ELP - INFLIGHT DFW-PHX. CREW REPORTED FUEL IMBALANCE DURING CLIMBOUT. FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FUEL PANEL REFUELING POWER SWITCH GUARD DOWN AND CENTER AND RIGHT TANK SWITCHES IN THE OPEN POSITION. FOUND FUEL PANELS SWITCH RESTRICTOR GUARD MISSING. REPLACED GUARDED POWER COVER ON FUEL PANEL AND CLOSED APPLICABLE TANK SWITCHES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PUMP — INOPERATIVE (CENTER TANK) · airframe 70,530 hrs · 37,179 cycles

MSY - INFLIGHT MCO-DFW. CREW REPORTED CENTER TANK FUEL WILL NOT FEED. FLIGHT DIVERTED MSY LANDED WITHOUT INCIDENT. REPLACED CENTER TANK FUEL BOOST PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN) · airframe 70,138 hrs · 36,981 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERY. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 70,138 hrs · 36,981 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE WALK WAY INOPERATIVE. RESEATED BATTERY PACK, OPS CHECK NORMAL.

Part: CUSP WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 67,774 hrs · 35,628 cycles

RIGHT CUSP AT STATION 1202 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,774 hrs · 35,628 cycles

RIGHT HAND CUSP AT STATION 665 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,774 hrs · 35,628 cycles

LEFT CUSP SHEET FROM STATIONS 922 TO 952 CORRODED. ACCOMPLISHED DOUBLER REPAIR AT STATION 926 PER AARD 53-20-00-16. INSTALLED HORSECOLLAR AT STATION 946 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,774 hrs · 35,628 cycles

CORROSION ON SUBFLOOR OUTBOARD OF SEAT TRACK NUMBER 2, STATIONS 1140 TO 1168. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,774 hrs · 35,628 cycles

FORWARD ACCY STATION 168, LONGERON 18 RIGHT HAS CORROSION ON BOTTOM OF CUSP AT FRAME. INSTALLED SUBFLOOR DOUBLER AND DOUBLER/OVERLAY PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

CORROSION ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED SUBFLOOR DOUBLER UNDER G-1 GALLEY DRAIN PAN STATIONS 148 TO 160 RIGHT PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

CABIN HAS A CRACK IN LONGERON 2 LEFT AT STATION 160. INSTALLED NEW LONGERON SECTION AND SPLICE FROM STATIONS 148 TO 168 PER SRM 53-02-00 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

CABIN HAS A CRACK IN LONGERON 3 LEFT AT STATION 160. INSTALLED NEW LONGERON AT STATIONS 160 TO 200 PER SRM 53-02-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,774 hrs · 35,628 cycles

CORROSION ON MID CARGO DOOR BEAM STATIONS 636 TO 693. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

AFT ACCS- 1485 CANT FRAME CRACKED BELOW STAIR RET ACTUATOR. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-33.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

FUSELAGE SKIN AT STATION 444 BETWEEN LONGERONS 19 TO 20 LEFT CRACKED. INSTALLED DOUBLER REPAIR PER SRM 53-04-02 VIEW S.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

MID CARGO, STATION 693 CORROSION ON ANGLE IN LOWER INBOARD ANGLE IN DOOR CUTOUT (FRAME TO BEAM). INSTALLED T ANGLE AT STATION 693 PER AARD 51-10-00-5 AND SRM 51-30-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,774 hrs · 35,628 cycles

CORROSION ON T-ANGLE LOWER DOOR BEAM MID CARGO. REPLACED T-ANGLE PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

RIGHT CUSP STATION 1202, CORROSION IS OUT OF LIMITS. INSTALLED NEW DOUBLER AT STATION 1202 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,774 hrs · 35,628 cycles

CABIN HAS CORROSION ON SUB FLOOR WEBBING BETWEEN STATIONS 200 TO 218 OUTBOARD OF NUMBER 5 SEAT TRACK. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,774 hrs · 35,628 cycles

FORWARD CARGO DOOR HAS DENT WITH GOUGES, BETWEEN NUMBER 2 AND 3 BEAMS. REMOVED AND REPLACED OUTER DOOR SKIN PER ESO 80174.

Part: CONNECTOR — NOT SEATED (CABIN PRESSURE) · airframe 67,768 hrs · 35,626 cycles

DFW - CREW REPORTED PRESSURIZATION FAILED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESEATED LOOSE CONNECTOR ON PRESSURE CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UNKNOWN — UNKNOWN (AUTOPILOT SYS) · airframe 67,619 hrs · 35,549 cycles

LAX - CREW REPORTED AIRCRAFT BECAME DIFFICULT TO CONTROL. AUTOPILOT AND AUTOTHROTTLES BOTH POPPED OFF. DURING THIS TIME THE MACH TRIM INOP LIGHT WAS FLASHING OFF. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE DIGITAL FLIGHT GUIDANCE SWITCH CIRCUIT BREAKER AT POSITION C-18 THAT WAS FOUND TRIPPED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,804 hrs · 33,986 cycles

CEILING BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AT CEILING.

Part: SKIN — DENTED (CARGO DOOR) · airframe 64,184 hrs · 33,631 cycles

DENT IN EXTERIOR OF FORWARD CARGO DOOR. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 30 VIEW P.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,184 hrs · 33,631 cycles

AFT ACC RIGHT SIDE CRACK IN FRAME 1497 AT INSTRUMENT SENSE LINE BRACKET 12 INCHES BELOW RIGHT LOUVER BOX. INSTALLED DOUBLER PER EA MD80-53-012097 AND SRM 51-70-05.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,184 hrs · 33,631 cycles

CORROSION ON DOOR WAY WEB STATION 1173. BLENDED AND REMOVED CORROSION PER SRM 51-10-03 FOUND TO BE OUT OF LIMITS PER SRM 53-01-00. INSTALLED REPAIR DOUBLER PER SRM 53-01-00 FIGURE 2 AND SRM 51-30-05 TREATED AND PRIMED PER SRM 51-10-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,184 hrs · 33,631 cycles

FUSE SKIN HAS CRACK AT STATION 1380 ABOVE LONGERON 13 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-30-00-02 AND SRM 53-01-00 FIGURE 2 SHEET 3.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,996 hrs · 32,435 cycles

OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 4 TO 6 INOPERATIVE. REPLACED BATTERY PACK.

Part: GYRO — INOPERATIVE (AUTOPILOT SYS) · airframe 61,557 hrs · 32,207 cycles

DFW - WHEN AIRCRAFT WAS MAKING A TURN OF FIFTEEN DEGREES THE CAPTAINS ATTITUDE INDICATOR FLUCTUATED WILDLY CAUSING THE AUTO PILOT AND AUTO THROTTLES TO DISENGAGE. RETURNED DFW WITHOUT INCIDENT. REMOVED AND REPLACED ALL THREE GYROS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — DAMAGED (AC BAY) · airframe 61,344 hrs · 32,087 cycles

DFW - ON CLIMBOUT CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND DAMAGED CLAMP ON RIGHT SIDE AIR CYCLE MACHINE. REPLACED DAMAGED CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,217 hrs · 31,453 cycles

RIVET BULGING ON SKIN. CORROSION AT LONGERON 26 LEFT AT STATION 686. INSTALLED SPLICE FOR LONGERON 26 LEFT AT STATION 686 AFTER CORROSION REMOVAL IN ACCORDANCE WITH SRM 53- 34-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,145 hrs

LGA - EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACE BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING.

Part: PISTON — FAILED (MLG) · airframe 59,891 hrs

SDF - CREW REPORTED NOSE LANDING GEAR DID NOT RETRACT. RETURNED TO SDF AND LANDED WITHOUT INCIDENT. REPLACED PISTON AND SERVICED STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACM — LEAKING (A/C BAY) · airframe 58,478 hrs

DFW INFLIGHT T2312/15JUN. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. LIGHT EXTINGUISHED PRIOR TO LANDING. FOUND RUBBER BOOT ON RT AIR CYCLE MACHINE LEAKING BETWEEN HEAT EXCHANGER AND PACK CONTROL VALVE. REPLACED AIR CYCLE MACHINE AND TEMPERATURE TABS ON BOTH SIDES. SYSTEM GROUND CHECKED NORMAL OPERAION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,570 hrs

LGA EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,199 hrs

LGA - EMERGENCY LIGHT AT OVERWING EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT SEAT ROWS 18 TO 29 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR EMERGENCY LIGHTS AT SEAT ROWS 18 TO 29 SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

PHX - EMERGENCY LIGHTS AT STATION 909 RIGHT AT AFT OVERWING EXIT SIGNS ABOVE SEAT 21DEF INOPERATIVE. REPLACED CHARGER FOR EMERGENCY LIGHTS AT STATION 909 RIGHT AT AFT OVERWING EXIT SIGNS ABOVE SEAT 21DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

PHX - EMERGENCY LIGHTS AT AFT TAIL COMPARTMENT AT STATION 1322 INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGHTS AT AFT TAIL COMPARTMENT AT STATION 1322. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

PHX - EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT STATION AND TAIL COMPARTMENT AT STATION 1330 INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT STATION AND TAIL COMPARTMENT AT STATION 1330. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

PHX - EMERGENCY LIGHTS AT DROP DOWN PANEL OUTSIDE FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK AT STATION 211 FOR EMERGENCY LIGHTS AT DROP DOWN PANEL OUTSIDE FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

PHX - EMERGENCY LIGHTS ABOVE SEAT ROW 25DEF INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGHTS ABOVE SEAT ROW 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT CEILING FROM SEATS 7D TO 11D INOPERATIVE. REPLACED BATTERY PACK AT 8D FOR EMERGENCY LIGHTS AT CEILING FROM SEATS 7D TO 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - EMERGENCY LIGHTS AT AFT GALLEY DOOR AND ALL LIGHTS FROM SEAT 21D AFT INOPERATIVE. REPLACED BATTERY PACK ABOVE AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DTW - EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EXTERIOR EMREGENCY LIGHTS, LEFT AND RIGHT, INOPERATIVE. REPLACED BATTERY IN AFT CARGO COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERAITON. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT CEILING EMERGENCY EXIT LIGHTS AND EVACUATION SLIDE LIGHTS INOPERATIVE. REPLACED AFT RIGHT LAV EMERGENCY EXIT LIGHT BATTERY PACK AND CHARGERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — FAILED (FUEL BOOST)

EN ROUTE AUS-ORD DURING CRUISE, WAS UNABLE TO BURN FUEL OUT OF CENTER TANK. RAN APPROPRIATE CHECKLIST TO NO AVAIL. AIR INTERRUPTED AND LANDED DFW WITHOUT INCIDENT. REPLACED CENTER AFT FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT OVERHEAD EMERGENCY CEILING EXIT LIGHTS FADE FROM DIM TO INOPERATIVE. REPLACED LEFT OVERHEAD EMERGENCY CEILING EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (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: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS AND TAIL CONE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK FOR AIRSTAIRS AND TAILCONE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, TWO OVERHEAD EMERGENCY EXIT LIGHTS ON CATWALK, RIGHT EMERGENCY EXIT LIGHT HANDHOLD ON CATWALK, AND TAIL CONE EMERGENCY EXIT LIGHTS ON JETTISON HANDLE INOPERATIVE. REWIRED FORWARD EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN TAIL COMPARTMENT INOPERATIVE. REPAIRED BROKEN WIRE LEAD ON BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: VALVE — LEAKING (TAIL)

ORD - FLT 1626 - TAIL COMPARTMENT TEMP HIGHT LIGHT CAME ON DURING CLIMBING. THE LIGHT WENT OUT AFTER ABOUT 5 MINUTES. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT SIDE PNEUMATIC SYSTEM AUGMENTATION VALVE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (M)

Part: VALVE — LEAKING (PNEUMATIC SYSTEM)

DFW - FLT 1357 - TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON DURING CLIMB-OUT. WENT OUT WHEN PACKS PUT TO MP BLEED OFF. THEN CAME BACK ON IN APPROXIMATELY 30 SECONDS. WENT OUT AFTER LEFT ENGINE BROUGHT TO IDLE BUT CAME BACK ON IN LESS THAN 1 MINUTE. BOTH ENGINES BROUGHT TO IDLE FOR DESCENT AND LIGHT WENT OUT. STAYED OUT DURING APPROACH AND LANDING. REPLACED RIGHT PNEUMATIC SYSTEM AUGMENTATION VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SEAT TRACK — CORRODED (BS 218-237)

TUL - FOUND CORROSION ON SEAT TRACK NR 5 BETWEEN STATION 218 AND STATION 237. INSTALLED NEWS TRACK PER SRM 51-10 PAGE 1. (M)

Part: SEAT TRACK — CORRODED (BS 965)

TUL - FOUND SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK SECTION STATION 795 THROUGH STATION 1030 PER SRM 51-01 PAGE 1. (M)

Part: SEAT TRACK — CORRODED (BS 826)

TUL - SEAT TRACK CORRODED NR 6 STATION 826. REMOVED AND REPLACED SEAT TRACK SECTION STATION 795 THROUGH STATION 1030 PER SRM 51-10 PAGE 1. (M)

Part: SEAT TRACK — CORRODED (BS 475-795)

TUL - FOUND SEAT TRACK CORRODED, RIGHT OUTBOARD TRACK.. REMOVED AND REPLACED SEAT TRACK SECTION STATION 475-795 PER SRM 51-01 PAGE 1. (M)

Part: LIGHT — DAMAGED (ROW 15)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT SEAT ROW 15 FOUND DAMAGED. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS BY FIRST CLASS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP BY FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (NLG)

DFW - FLT 694 - AFTER TAKEOFF AUS WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR UPLOCK SENSOR. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DIRTY (NLG)

DFW - FLT 1344 - AFTER TAKEOFF SAN WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. ACCOMPLISHED TEST OF PSEU WITH NO DEFECTS FOUND. CHECKED NOSE LANDING GEAR AND RETRACTION LINKAGE WITH NO DEFECTS FOUND. REMOVED EXCESS GREASE FROM NOSE LANDING GEAR LOCKED AND GEAR UP SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEPARATOR — OVERSERVICED (ACM BAY)

DFW - FLT 0311 - DURING CRUISE EN ROUTE DFW-PDX SMOKE IN CABIN, AIR INTERRUPTED BACK TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. NR 2 AIR CYCLE MACHINE OVERSERVICED. SERVICED TO PROPER LEVEL, PRECAUTIONARY REPLACED BOTH WATER SEPARATOR PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FCF, NO SMOKE NOTED AND SYSTEM CHECKED NORMAL OPERATION. (W)