N466AA

Part: MODULE — DEFECTIVE (FUEL SYSTEM) · airframe 76,942 hrs · 41,073 cycles

AIR INTERRUPT, DIVERTED. EMER DECLARED, UNEVENTFUL LANDING & ACFT WAS NOT OVERWEIGHT. THE FLIGHT CREW NOTED A 2000 LP FUEL LOSS IN THE LT TANK & DETERMINED THAT THERE WAS A FUEL LEAK. RAN BOTH ENGS & ACCOMPLISHED CHECK FOR LEAKS WITH NO LEAKS BEING NOTED. REPLACED THE STANDARDIZED ELECTRONIC MODULE, SEM, IAW AMM 28-40-05. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 76,733 hrs · 40,954 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH, RECEIVED AN UNSAFE NLG INDICATION ON, WHEN GEAR PLACED DOWN. ACFT DID NOT GET SAFE NOSE GEAR DOWN INDICATION. FOUND GREEN NOSE GEAR BULBS BURNED OUT. R & R BULBS. LIGHT PRESS TO TEST NOSE GEAR INDICATION GOOD. OPERATIONAL CHECKED GOOD IAW AMM 32-60-00. SYS CHECKED NORMAL.

Part: CASTING — CRACKED (RT SPOILER) · airframe 75,129 hrs · 40,012 cycles

RIGHT WING GND SPOILER ACTUATOR CASTING IS CRACKED AT THE FWD INBD SIDE ABOVE THE ACTUATOR MOUNT BOLT. R & R CASTING IAW AARD 51-00-05-1, SRM 51-30--02-001 & EA MD80-57-037460 REV A DATED 11/20/2014.

Part: FORMER — CRACKED (LE SLAT) · airframe 75,053 hrs · 39,963 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.

Part: FORMER — CRACKED (LE SLAT) · airframe 75,053 hrs · 39,963 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,910 hrs · 39,882 cycles

FOUND EMER LIGHTS IN AFT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK IN RT AFT LAVATORY CEILING. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,910 hrs · 39,882 cycles

FORWARD CABIN OVERHEAD EMER LIGHTS FOUND DIM. REPLACED BATTERY PACK FOR FWD CABIN OVERHEAD EMER LIGHTS. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (LANDING GEAR) · airframe 72,483 hrs · 38,464 cycles

DFW CREW REPORTED NLG & RT MLG HAVE NO INDICATION. EMERGENCY DECLARED FLIGHT EXECUTED GO AROUND & LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND WIRE G200F24 BROKEN AT L2-632. REPAIRED WIRE, SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,402 hrs · 37,827 cycles

SKIN CRACKED AT STATION 1437 RT BETWEEN LONGERONS 3 AND 4. INSTALLED DOUBLER IAW SRM 53-04-00 AND 51-60-00.

Part: POSITION SENSOR — DEFECTIVE (MLG DOOR) · airframe 69,458 hrs · 36,785 cycles

DFW - CREW REPORTED MAIN LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MAIN LANDING GEAR DOOR POSITION SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTACT — DIRTY (BATTERY CHARGER) · airframe 68,893 hrs · 36,454 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. CLEANED BATTERY CHARGER CONTACTS. OPS CHECK NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

CORROSION UNDER FORWARD GIRT BAR BRACKET ON CUSP AT STATION 1142. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16 AND EA MD80-53-021407.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

CORROSION ON INTERNAL SKIN AT STATION 891 BELOW LONGERON 18 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 51-30-05 AND EA MD80-53-021427.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

CORROSION ON INTERNAL SKIN AT STATIONS 870 TO 870 BELOW LONGERON 18 RIGHT. INSTALLED REPAIR DOUBLER PER EA MD80-53-021427.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,716 hrs · 35,798 cycles

FIVE CRACKS EMANATING FROM FASTENER HOLES ALONG LONGERON 22 LEFT BETWEEN STATIONS 160 TO 200. INSTALLED DOUBLER REPAIR PER SRM DRAWING SR009530219.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

CORROSION UNDER AFT GIRT BAR BRACKET ON CUSP AT STATION 1170. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16 AND EA MD80-53-021407.

Part: FRAME — DAMAGED (ZONE 200) · airframe 67,716 hrs · 35,798 cycles

RIGHT CANT FRAME 1463 MISDRILLED. ACCOMPLISHED REPAIR PER EA MD80-53-021470.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,716 hrs · 35,798 cycles

AFT CARGO HAS CORROSION ON SHEAR TIE STATION 1287 BETWEEN LONGERON 28 RIGHT 28 LEFT. INSTALLED NEW SHEAR TIE PER SRM 51-10-00-5, 53-03-00 FIGURE 3, SHEET 1 AND DRAWINGS #9957739, AND EDK2742 REVISION A.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 67,716 hrs · 35,798 cycles

RIGHT INBOARD FLAP WEDGE HAS DAMAGE TO TOP INBOARD AND OUTBOARD EDGES. REPAIRED FLAP WEDGE PER SRM 51-70-06, AARD 51-00-00-014 AND EA MD80-57-021341.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

AFT CARGO HAS CORROSION ON LONGERON 29 LEFT BETWEEN STATIONS 1287 TO 1309. REMOVED DAMAGED SECTION OF LONGERON AND SPLICED IN NEW LONGERON SECTION FROM STATIONS 1280 TO 1300 PER SRM 53-02-00.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

CORROSION ON AFT DOORWAY WEB, STATION 1213 ABOVE LONGERON 26 RIGHT. BLENDED AND REMOVED CORROSION PER SRM 51-10-03. CUT OUT SECTION OF WEB AND SPLICED IN A NEW SECTION PER AARD 53-10-00-24.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,716 hrs · 35,798 cycles

AFT CARGO HAS A CRACK IN INTERCOSTAL BETWEEN CEILING BEAMS BETWEEN STATIONS 1271 TO 1287. INSTALLED INTERCOSTAL IN AFT CARGO BETWEEN CEILING BEAMS STATIONS 1271 TO 1287 PER AARD 51-10-00-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,716 hrs · 35,798 cycles

CORROSION ON FORWARD SIDE OF INTERCOSTAL STATION 1183 LONGERONS 28 TO 29 RIGHT. INSTALLED NEW INTERCOSTAL AT STATION 1183 LONGERONS 28 TO 29 RIGHT (AFT CARGO).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

SEAT TRACK NUMBER 5 FROM STATIONS 200 TO 246 CORRODED. INSTALLED NUMBER 5 SEAT TRACK SECTION FROM STATIONS 200 TO 248 RIGHT PER SRM 51-30-01, SRM 51-30-05 AND SRM 53-05-00 FIGURE 4F SHEET 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

CORROSION UNDER AFT GIRT BAR BRACKET ON CUSP AT STATION 1170 LEFT. INSTALLED DOUBLER LEFT SIDE STATION 1170 PER AARD 53-20-00-16 AND SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,716 hrs · 35,798 cycles

AFT CARGO HAS A CRACK IN INTERCOSTAL BETWEEN CEILING BEAMS FROM STATIONS 1287 TO 1309. INSTALLED INTERCOSTAL IN AFT CARGO BETWEEN CEILING BEAMS FROM STATIONS 1287 TO 1309 PER AARD 51-10-00-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,716 hrs · 35,798 cycles

CABIN - LONGERON 4 LEFT HAS CRACK INDICATIONS AT STATION 200 IN THE INBOARD AND OUTBOARD LEGS. INSTALLED NEW LONGERON PER SRM 53-02-00 FIGURE 18.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

G-1 GALLEY MOUNT HAS CORROSION ON THE SURFACE AND IN THE BORE AT STATION 160 OUTBOARD SIDE OF THE DRAIN PAN. INSTALLED OUTBOARD G-1 GALLEY SUPPORT FITTING PER SRM 51-30-02 AND SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

E AND E COMPARTMENT STATION 155, CORROSION ON LOWER SIDE OF LEFT CUSP AT GALLEY 1 DRAIN LINE. INSTALLED SUBFLOOR DOUBLER UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

STATION 1212 DOOR BEAM TEE BRACKET CORRODED. INSTALLED SERVICEABLE NEW TEE BRACKET PER AARD 51-10-00-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

CORROSION ON THE FLOORBOARD SUPPORT FROM THE NUMBER 5 SEAT TRACK OUTBOARD TO THE FORWARD SERVICE DOOR FRAME AT STATION 200. INSTALLED FLOORBOARD SUPPORT AT STATION 200 RIGHT PER SRM 51-30-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 67,716 hrs · 35,798 cycles

STIFFENER CRACKED AT STATION 1338 LNGERON 1 LEFT, JUST UNDER TOP FASTENER. INSTALLED DOUBLER AFT CABIN BULK HEAD STATION 1338 OVER AFT ENTRY DOOR PER AARD 53-10-00-15.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,716 hrs · 35,798 cycles

G-1 GALLEY MOUNT HAS CORROSION ON THE SURFACE AND IN THE BORE AT STATION 160 INBOARD SIDE OF THE DRAIN PAN. INSTALLED MIDDLE G-1 GALLEY MOUNT PER SRM 51-30-02 AND SRM 51-30-05.

Part: INDICATOR — ERRATIC (COCKPIT) · airframe 67,289 hrs · 35,563 cycles

ATL - INFLIGHT ORD-MCO. CREW REPORTED LEFT WING TANK FUEL INDICATION IN CRUISE MODE IN QUESTION TO AMOUNT OF FUEL QUANTITY AND FUEL BURNED BY FLIGHT CREW. FLIGHT DIVERTED ATL LANDED WITHOUT INCIDENT. PLACARD LEFT FUEL QUANTITY AND FUEL TOTALIZER PER AMM MEL 28-4B AND 28-5. VERIFIED NEW FUEL LOAD BY MEASURING FUEL STICK METHOD. FLIGHT CONTINUED TO MCO WITHOUT FURTHER INCIDENT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: INDICATOR — INOPERATIVE (FUEL SYSTEM) · airframe 66,948 hrs · 35,378 cycles

LIT - INFLIGHT BHM-DFW. CREW REPORTED LEFT MAIN TANK FUEL IMBALANCE. FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. PLACARD LEFT MAIN TANK INDICATION PER MEL. FLIGHT CONTINUED ON TO DFW WITH NO FURTHER ISSUES. REPLACED FUEL QUANTITY INDICATION AT DFW ON 09/22/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — DIRTY (CABIN) · airframe 65,236 hrs · 34,413 cycles

CEILING EMERGENCY LIGHTS FROM ROW 28 TO ROW 30 INOPERATIVE. REMOVED AND CLEANED BATTERIES. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 65,236 hrs · 34,413 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS, JUST FORWARD OF AFT BULKHEAD DOOR INOPERATIVE. RE-SEATED BATTERIES IN CHARGER, OPS CHECK NORMAL.

Part: APU — DIRTY (APU BAY) · airframe 63,568 hrs · 33,466 cycles

DFW - CREW REPORTED SMOKE ODOR IN AFT CABIN AFTER TAKEOFF. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED AUXILIARY POWER UNIT WASH AND PACK BURN. NO ODORS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHT) · airframe 61,943 hrs · 32,557 cycles

RIGHT FORWARD AND AFT OVERWING DOOR LOWER EXIT SIGNS INOPERATIVE. RESEATED BATTERY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 61,943 hrs · 32,557 cycles

EMERGENCY LIGHT IN AFT GALLEY AREA AFT LIGHT INOPERATIVE. RELAMPED LIGHT.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHT) · airframe 61,943 hrs · 32,557 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 59,939 hrs

LGA- EMERGENCY LIGHTS INOPERATIVE AT SEATS 16DEF. RESEATED CONNECTOR AT SEAT 16DEF.

Part: LENS — BROKEN (CABIN) · airframe 59,176 hrs

DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (LIGHT ASSEMBLY) · airframe 59,176 hrs

DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · 62,046 cycles

DFW EMERGENCY LIGHT AT SEAT 7D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SHROUD — MISSING (CABIN) · 62,046 cycles

DFW EMERGENCY LIGHT AT SEAT 7D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: ACTUATOR — FAILED (YAW DAMPER) · airframe 58,538 hrs · 58,538 cycles

DFW INFLIGHT T1767/09JUL. CREW REPORTED YAW DAMPER FAILED ON CLIMB. FLIGHT GUIDANCE CIRCUIT BREAKER POPPED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED YAW DAMPER ACTUATOR. REPLACED LT AILERON SENSOR, LT ELEVATOR SENSOR AND DIGITAL FLIGHT GUIDANCE CIRCUIT BREAKER C17 AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: LAMP — BROKEN (EMERGENCY LIGHTS) · airframe 56,936 hrs

TPA - EMERGENCY AISLE LIGHT AT SEAT 22E HAS BROKEN LAMPS. REPLACED LAMPS FOR EMERGENCY AISLE LIGHT AT SEAT 22E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 56,936 hrs

TPA - EMERGENCY AISLE LIGHT AT SEAT 22E HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY AISLE LIGHT AT SEAT 22E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 56,936 hrs

TPA - EMERGENCY AISLE LIGHT AT SEAT 12D INOPERATIVE. SECURED CONNECTOR PIN AT SEAT 12F FOR INOPERATIVE EMERGENCY AISLE LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

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

Part: ENGINE — STALLED (RIGHT)

AT FLIGHT LEVEL 240, RIGHT ENGINE COMPRESSOR STALLED. ENGINE GAS TEMPERATURE ROSE TO 750. UNCOMMANDED ENGINE SHUTDOWN. DUE TO INABILITY TO MAINTAIN RUDDER CONTROL MISSED APPROACH. WAS UNABLE TO CONTROL RUDDER UNTIL POWER PULL BACK ALL THE WAY. LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 50 MINUTES. FOUND METAL IN TAIL PIPE. REPLACED NUMBER TWO ENGINE ON 27 MAR 2007 AT IAD AND REPLACED ISOLATORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — INOPERATIVE (NLG STRUT)

ORD INFLIGHT - NOSE GEAR WOULD NOT RETRACT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE STRUT SEAL AND SERVICED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (FUEL BOOST)

RDU INFLIGHT T1827/18OCT - RIC TO DFW - DURING FLIGHT CIRCUIT BREAKER FOR THE AFT CENTER FUEL BOOST PUMP POPPED. LANDED RDU WITHOUT INCIDENT. REPLACED TRANSFER FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEVERAL AFT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190 FOR AFT CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 11D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN)

DFW - RIGHT AFT EMERGENCY OVERWING EXIT LIGHT AT KNEE LEVEL FORWARD OF AFT RIGHT HAND OVERWING EXIT DOOR IS DIM. REPLACED THE UPPER CONTROL MODULE AND BATTERY PACK AT STATION 850 FOR RIGHT AFT EMERGENCY OVERWING EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - EMERGENCY LIGHTS AT FORWARD OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK AT B5-103 FOR EMERGENCY LIGHTS AT FORWARD OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

PHX CEILING EMERGENCY LIGHT AT ROWS 24 THROUGH 27 INOPERATIVE. REPLACED B5-106 BATTERY PACK/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHT FOR ROWS 24 THROUGH 27 AT STATION 1057R. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS WERE INOPERATIVE IN THE TAILCONE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 24 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 7 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (LAVATORY)

RDU - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT IN AFT LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY PACK IN AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS FROM ROW 8-11 INOPERATIVE. SECURED EMERGENCY EXIT PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER BAG — CONTAMINATED (ACM BAY)

EN ROUTE, DAY-ORD UNKNOWN SMOKE IN CABIN AND IN COCKPIT DURING TAKEOFF. DISSIPATED AFTER APPROXIMATELY 5 MINUTES. RETURNED AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM DAY TO ORD. REPLACED BOTH COALESCER BAGS AND ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED FIRST OVERHEAD EMERGENCY EXIT LIGHT CONTACTS ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HEATER — CORRODED (LAVATORY)

LGA - FLT 1194 - EN ROUTE MIA-LGA - FLIGHT ATTENDANT REPORTED A BURNING SMELL AT FIRST CLASS LAVATORY. LANDED LGA WITHOUT FURTHER INCIDENT. REPLAED WATER HEATER AND CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — MALFUNCTIONED (RT WING)

MCI - FLT 851 - APPROX 35 MIN AFTER TAKEOFF, WHILE AT CRUISE AT FL260 DISCOVERED AT 900 LB FUEL IMBALANCE BETWEEN RIGHT MAIN AND LEFT MAIN FUEL TANKS. CENTER TANK HAD 10,000 LBS OF FUEL STILL REMAINING, LEFT TANK WAS STILL FULL 9100 LBS AND RIGHT TANK 8200 LBS AS PER PROCEDURES TURNED OFF BOTH RIGHT FUEL PUMPS. FUEL CONTINUED TO FEED OUT OF THE RIGHT TANK. DIVERTED TO MCI AND LANDED 30 MINUTES LATER WITH A 4700 LB FUEL IMBALANCE. REPLACED RIGHT WING FUEL VALVE. SYTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LINE — LEAKING (ACM BAY)

MIA - FLT 1495 - AFTER TAKEOFF, FLT ATTENDANT REPORTED SMOKE AND STRONG ODOR IN CABIN. TIGHTENED LOOSE HYDRAULIC LINE RIGHT SIDE OF AIR CONDITIONING BAY. ACCOMPLISHED PACK BURNOUT AND REPLACED COALESCER BAGS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: PAN — CORRODED (CARGO DOOR)

TUL - CARGO DOOR PAN CORRODED FORWARD CARGO. REMOVED AND REPLACED SECTION OF DOOR PAN PER SRM 53-05. TST: 33,663 HOURS. CYCLES: 18,069. (X)

Part: ACM — DEFECTIVE (LEFT ACM BAY)

MIA - FLT 2024 - EN ROUTE MIA-BOS, SMOKE NOTED IN CABIN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED LEFT ACM. ACCOMPLISHED PACK BURNOUT OF BOTH AIR CONDITIONING PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN CENTER INOPERATIVE. REPAIR EMERGENCY EXIT FLOOR PATH LIGHTING STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (ROW 24)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 24 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, LIGHT STRIP AT FORWARD GALLEY INOPERATIVE. REPLACED LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TIE DOWN TRACK — CORRODED (BS 1212-1231)

TUL - FOUND CORROSION ON LEFT SIDE OF LEFT TIEDOWN AT SPLICE, BETWEEN FS 1212 AND FS 1231. REPLACED LEFT TIE TRACK FROM SPLICE FS 1212 TO AFT BULKHEAD. (M)

Part: CONDUCTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — LOW PRESSURE (AFT FUSELAGE)

ATL - DURING OVERNIGHT CHECK, TAIL CONE EMERGENCY EVACUATION SLIDE PRESSURE GAUGE INDICATED IN RED (LOW) ZONE. REPLACED TAIL CONE EMERGENCY EVACUATION SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)