N486AA

Part: STRAP — DISCONNECTED (EVAC SLIDE) · airframe 77,031 hrs · 40,754 cycles

TAIL CONE SLIDE COVER STRAP DISCONNECTED FROM BRACKET ON FLOOR. CONNECTED TAIL CONE SLIDE COVER STRAP IAW AMM-25-62-01.

Part: STOP FITTING — CRACKED (BS 427) · airframe 75,818 hrs · 40,053 cycles

FORWARD CARGO AFT LOWER DOOR STOP PAD CASTING IS CRACKED. R & R DOOR STOP PAD CASTING IAW AARD 51-00-05-01, DWG CDK2345 & 5910141.

Part: CUSP WEB — CORRODED (BS 234-240) · airframe 75,818 hrs · 40,053 cycles

RIGHT CUSP WEB CORRODED ON BOTTOM SURFACE BETWEEN BS 234 - 240. REPAIRED CUSP WEB IAW SRM 53-14-02 FIG 4.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 75,234 hrs · 39,714 cycles

DURING CLIMB RT ENG OIL PRESSURE INCREASED TO 60 PSI, OIL QTY DROPPED TO ZERO & ENG SHUTDOWN. RETURNED & EMERGENCY DECLARED. LANDING UNEVENTFUL. R & R RT ENG POWER PLANT ENGINEERING REPORTS INTRUSION OF HOT AIR INTO THE NUMBER 4 & 5 BEARING COMPARTMENT WHICH RESULTED IN SCAVENGE PUMP FAILURE LEADING TO OIL STARVATION & BEARING FAILURE.

Part: FORMER — CRACKED (LE SLAT) · airframe 75,142 hrs · 39,660 cycles

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

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 74,713 hrs · 39,401 cycles

FORWARD PORTABLE EMER LIGHT INOPERATIVE WHEN TESTED IAW CARD 0801. R & R L1 PORTABLE EMER LIGHT IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY — WEAK (CABIN) · airframe 74,713 hrs · 39,401 cycles

FORWARD EMER PATH LIGHTING IS WEAK WHEN TESTED IAW CARD 5403. R & R FWD EMER PATH LIGHTING BATTERY AT OVERWING AREA IAW 33-60-98. SYS CHECKED NORMAL.

Part: CASTING — CRACKED (CARGO DOOR) · airframe 72,430 hrs · 38,057 cycles

FWD CARGO DOOR TWO STOP CASTINGS CRACKED AFT UPPER & FWD UPPER. INSTALLED TWO NEW CASTINGS IAW SRM 51-30-05.

Part: CASTING — CRACKED (CARGO DOOR) · airframe 72,430 hrs · 38,057 cycles

AFT CARGO DOOR FWD LOWER DOOR STOP CASTING CRACKED. INSTALLED NEW CASTING IAW SRM 51-30-05.

Part: RIB — CRACKED (LT WING) · airframe 72,430 hrs · 38,057 cycles

LT HAND WING LE RIB CRACKED JUST INBD OF NR 4 SLAT TRACK. INSTALLED DOUBLER & SHIM IAW MD80-57-033080.

Part: DUCT — CRACKED (AC BAY) · airframe 70,080 hrs · 36,764 cycles

AUS - REPEAT ITEM CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED AUS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT CRACKED ON THE RIGHT SIDE OF AFT ACCESSORY COMPARTMENT. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — CRACKED (AC BAY) · airframe 70,080 hrs · 36,764 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINTED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED Y DUCT THAT WAS CRACKED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — OUT OF POSITION (AC BAY) · airframe 69,869 hrs · 36,649 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPOSITIONED Y DUCT BOOT AND CLAMP AND REPLACED BOTH TEMP SENSORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,695 hrs · 35,984 cycles

EMERGENCY EXIT LIGHTS IN THE CABIN CAME ON FOR NO APPARENT REASON AFTER TAKEOFF. LIGHTS STAYED ON FOR ABOUT 5 MINUTES AND THEN WENT OUT. REPLACED EMERGENCY LIGHT BATTERY PACK ABOVE SEAT 6F. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,607 hrs · 35,930 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SPLICE — DAMAGED (VERTICAL STAB) · airframe 68,444 hrs · 35,842 cycles

VERTICAL STABILIZER UPPER SPLICE SECTION HOLES DISTRESSED. REAMED OUT HOLES AND INSTALLED BUSHINGS AND DOUBLER PER SRM 55-03-00 FIGURE 30.

Part: SPAR CAP — CRACKED (LT WING) · airframe 68,444 hrs · 35,842 cycles

LEFT WING LEADING EDGE FITTING CRACKED INBOARD OF TRACK 8. SPAR CAP STRAP REPAIR COMPLETED PER EA MD80-57-024516.

Part: BEAM — CORRODED (FUSELAGE) · airframe 68,444 hrs · 35,842 cycles

CORROSION FOUND ON UPPER AFT DOOR BEAM SECTION, STATIONS 1193 TO 1202 ABOVE AFT CARGO DOOR. INSTALLED NEW SECTION OF AFT UPPER DOOR BEAM PER AARD 51-10-00-5 AND BOEING PRINT 5936072.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,444 hrs · 35,842 cycles

RIGHT CUSP IS CRACKED AT STATION 1275 AT LIGHTENING HOLE. INSTALLED RIGHT CUSP SHEET FROM 1250 TO 1309 PER AARD 53-20-00-16, SRM 51-30-01 AND SRM 51-30-02

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,444 hrs · 35,842 cycles

SUBFLOOR HAS CORROSION AT AFT G-2 GALLEY MOUNT AT APPROXIMATE RIGHT BUTTLINE 10, STATION 218. INSTALLED SUBFLOOR DOUBLER PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,444 hrs · 35,842 cycles

FORWARD CARGO LOWER DOOR JAMB PAN HAS CORROSION ON BOTTOM OF PAN AT LOWER DOOR STOP PADS. INSTALLED NEW LOWER DOOR JAMB PAN SECTION FROM STATIONS 370 TO 427 AND REPAIR SPLICE ANGLE/DOUBLERS PER SRM 53-05-00 FIGURE 44.

Part: CUSP WEB — TORN (FUSELAGE) · airframe 68,444 hrs · 35,842 cycles

CUSP TORN INBOARD OF NUMBER 2 SEAT TRACK STATION 218. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,444 hrs · 35,842 cycles

CUSP DAMAGED AT STATION 886 LEFT HORSE COLLAR FASTENER HOLE. ROUTED OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,444 hrs · 35,842 cycles

CUSP DAMAGED AT STATION 864 LEFT SIDE HORSE COLLAR FASTENER HOLE. INSTALLED DOUBLER AT LEFT STATION 864 PER AARD 53-20-00-16.

Part: DUCT — LEAKING (AC BAY) · airframe 67,523 hrs · 35,321 cycles

DFW - CREW REPORTED THE MASTER WARNING LIGHT AND TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON INTERMITTENTLY FOR 3 OR 4 CYCLES. RAN QRH CHECKLIST AND LIGHT WENT OUT AFTER 30 SECONDS AND STAYED OFF FOR REMAINDER OF FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DUCT ASSEMBLY THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 67,354 hrs · 35,221 cycles

CREW REPORTED TAIL COMPARTMENT HIGH LIGHT FLICKERED THEN CAME ON STEADY DURING CLIMBOUT. LIGHT EXTINGUISHED WITH REDUCED POWER. EMERGENCY DECLARED FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,839 hrs · 33,800 cycles

LONGERON 2 RIGHT CRACKED AFT OF FRAME STATION 1418. INSTALLED LONGERON SPLICE AND FILLER PER EA MD80-53-014831 DATED 01/14/11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,839 hrs · 33,800 cycles

AFT SIDE OF FRAME STATION 1418 CRACKED AT LONGERON 2 RIGHT. INSTALLED DOUBLER PER EA MD80-53-014820.

Part: STOP FITTING — CRACKED (DOOR) · airframe 60,877 hrs · 31,677 cycles

TUL - NUMBER FIVE BEAM FORWARD STOP-PAD FITTING CRACKED. REPLACED STOP-PAD FITTING PER ESO-80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 60,877 hrs · 31,677 cycles

TUL - NUMBER ONE BEAM FORWARD STOP-PAD BRACKET CRACKED. REPLACED STOP-PAD BRACKET UNDER ESO-80174.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,877 hrs · 31,677 cycles

TUL - CRACK IN FUSELAGE SKIN. REPAIR DOUBLER WAS INSTALLED UNDER SRM 53-30-00-02.

Part: DISPLAY — FAILED (PFD) · airframe 59,369 hrs

LGA INFLIGHT - AT 15000 FEET CAPTAINS PRIMARY FLIGHT DISPLAY WENT BLANK AND SMOKE STARTED COMING INTO COCKPIT. TURNED OFF PRIMARY FLIGHT DISPLAY AND ELECTRIC SMOKE FUMES CONTINUED. RETURNED TO LGA AND LANDED WITHOUT INCIDENT. REPLACED ELECTRONIC FLIGHT INSTRUMENT SYSTEM UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,858 hrs

LGA - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,518 hrs

LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: ENGINE — LEAKING (RIGHT)

TPA INFLIGHT - RSW TO DFW, DURING CRUISE RIGHT ENGINE OIL QUANTITY AND PRESSURE DROPPED. CREW PERFORMED RIGHT ENGINE SHUTDOWN AND DIVERTED TO TPA. LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 15 MINUTES. FOUND RIGHT ENGINE LEAKING OIL. PERFORMED FLIGHT DATA RECORDER DOWNLOAD. REPLACED NUMBER TWO ENGINE AT TPA ON 10 MAR 2007. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LGA - RIGHT HAND OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR RIGHT HAND OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (HYD SYSTEM)

INFLIGHT T1622/14 AFTER TWO HOURS OF FLIGHT LEFT HYDRAULIC PRESSURE DECREASED TO CA 500 PSI WITH LEFT ENGINE PUMP IN LOW. PERFORMED QRH PROCEDURE FOR RIGHT SYSTEM ENGINE PUMP HI TRANSFER PUMP ON. OPERATED NORMALLY FOR APPROXIMATELY 10 MINUTES AND RIGHT SYSTEM FAILED. RESTORED RIGHT SYSTEM LATER IN FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED HYDRAULIC TRANSFER PUMP. ALSO REPLACED LEFT HYDRAULIC PRESSURE TRANSMITTER AND RETURN FILTERS. SERVICED HYDRAULIC SYSTEM AS REQUIRED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE L1 DOOR EXIT. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP LOWER SURFACE, LEFT SIDE STATION 622. FABRICATED AND INSTALLED DOUBLER REPAIR TO CUSP PER SRM 53-01-06. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED. STOP DRILLED CRACK AT ENDS. INSTALLED DOUBLER PER SRM 53-01-00 AND 51-01-01. (M)

Part: VALVE — DEFECTIVE (ACM BAY)

IMMEDIATELY AFTER TAKE OFF THE CABIN FILLED WITH NOTICEABLE AMOUNT OF SMOKE. DISSIPATED AFTER 3-5 MINUTES. RETURNED AND LANDED WITHOUT INCIDENT. REPLACED LIGHT AND RIGHT AIR CONDITIONING PRESSURE REGULATOR VALVES. BOTH COALESCERS BAGS, AND LEAKING APU MAGNETIC DRAIN PLUG. ACCOMPLISHED PACK BURNOUT. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DEN - DURING OVERNIGHT MAINTENANCE, RAR CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - DURING OVERNIGHT MAINTENANCE, FIRST CLASS CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE HANDLE EMERGENCY LIGHT INOPERATIVE. REPLACED WIRING TO TAIL CONE HANDLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHTS AT FLIGHT DECK AND R1 DOOR FAILED TO STAY ILLUMINATED. REPLACED BATTERY ASSEMBLY TO OVERHEAD EMERGENCY LIGHTS AT FLIGHT DECK AND R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPLICE — DAMAGED (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE SIDEWALL EMERGENCY LIGHTS INOPERATIVE. REPLACED BAD SPLICE AT FEEDER WIRE FOR TAIL CONE SIDEWALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (TAIL)

LAX - FLT 2430 - AFTER TAKEOFF, FLIGHT CREW REPORTED SMOKE IN CABIN. RETURNED AND LANDED LAX WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DIAPHRAGM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION SUBFLOOR DIAPHRAGM AT FWD SERVICE DOOR THRESHOLD. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: SKIN — BULGED (FUSELAGE)

TUL - FOUND BULGE IN SKIN FROM BAG CART IMPACT, AFT OF OUTFLOW VALVE. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND 238 DEEP GOUGE IN FUSE SKIN LONGERON 18L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B AND ESO 80559 5/16/2000. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSE SKIN STATION 220 BELOW L18L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B AND ESO 80559 5/16/2000. (M)

Part: LONGERON — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LONGERON 23R FROM STATION 1309 TO 1322. REMOVED CORROSION AND INSTALLED SPLICE PER ESO 80559, DATED 5-12-2000. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON NR 6 SEAT TRACK FS 215-FS 275. SPLICED IN NEW SECTION OF SEAT TRACK NR 6 FS 215 TO FS 275 SRM 51-01 USED 16 NAS623-3-4 SUBSTITUTE FASTENERS FOR TRACK TO FLOOR BEAM ATTACHMENT SRM 53-40 ATTACH ANGLES PER 53-05 PART 1 FIG 4F. (M)

Part: BRACKET — CORRODED (GIRT BAR)

TUL - FOUND CORROSION ON CUSP UNDER GIRT BAR BRACKET AT STATION 1174. CUTOUT CORROSION, FABRICATED AND INSTALLED DOUBLER 53-01-00. (M)

Part: FLOORBEAM — CUT (CABIN)

TUL - FOUND FLOORBEAM HAS DAMAGE AT STATION 218 AND RBL 13 HAS CUT MARK. BLENDED DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-05 PART 1 FIG 20A. (M)

Part: WINDOW POST — CRACKED (FUSELAGE)

TUL - FOUND INNER WINDOW FRAME HAS VISUAL INDICATION OF CRACK AT LOWER FORWARD EDGE AT RADIUS RIGHT SIDE STATION 986. INSTALLED NEW DOUBLER PER SRM 53-10-00-25. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND STATION 160 LONGERON 4 LEFT CRACKED IN RADIUS AT OUTBOARD ATTACH FASTENER. REMOVED LONGERON FROM STATION 148.55 TO 176. INSTALLED NEW LONGERON WITH SPLICE PER SRM 53-02 FIG 18. (M)

Part: BEAM — CORRODED (THRESHOLD)

TUL - FOUND CORROSION ON LOWER DOOR SILL BEAM HORIZ AND VERT LEG. REMOVED CORROSION AND INSTALLED .040 TITANNIUM DOUBLER PER AARD 53-10-00-3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND STATION LONGERON 15L DOOR CUT OUT AFT SIDE WEB CRACKED AT ATTACH FASTENERS. INSTALLED 1 EACH, FABRICATED STRAP PER AARD 53-10-00-11. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP STATION 446-465 LEFT SEVERAL PLACES. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER STATION 446-465 PER SRM 51-10-B AND SRM 51-1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP STATION 446-465 LEFT SEVERAL PLACES. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER STATION 446-465 PER SRM 51-10-3 AND SRM 51-1. (M)

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT ROW 7 TO ROW 20 INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP AT ROW 7 TO ROW 20. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS IN AFT OF AIRCRAFT INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP IN AFT OF AIRCRAFT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIRS)

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

Part: COALESCER — DIRTY (AIR COND COMPT)

DFW - FLT 1478 - AFTER TAKEOFF DFW, FLIGHT ATTENDANT NOTED A STRONG ELECRICAL SMELL IN CABIN. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS AND BURNED PACKS OFF AFTER CHANGE. AIRCRAFT FLEW ON FUNCTIONAL CHECK FLIGHT AND NO ODOR WAS NOTED. SYSTEMS CHECKED NORMAL OPERATION AND AIRCRAFT RELEASED INTO SERVICE. (X)

Part: COALESCER — DIRTY (ACM BAYS)

LIT - FLT 1551 - EN ROUTE EWR/DFW - DURING CRUISE AT FL 310, REPEATED INSTANCES OF SMOKE NOTED IN MAIN CABIN WHICH WOULD LAST FOR APPROXIMATELY 5 MINUTES AND THEN DISSIPATE. AIRCRAFT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. CHECKED BOTH ENGINE INLETS WITH NO DEFECTS FOUND. CHECKED ALL INDIRECT LIGHT BALLASTS WITH NO DEFECTS FOUND. CHECKED LEFT AND RIGHT PACK FANS AND RECIRCULATION FAN WITH NO DEFECTS FOUND. REPLACED LEFT AND RIGHT COALESCER BAGS AND ACCOMPLISHED BURN OUT PROCEDURE OF PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE OR ODOR NOTED. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN THE FORWARD CABIN BY GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTS STRIP IN FORWARD CABIN BY GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — SHORTED (CABIN OVERHEAD)

ORD - FLT NR 0205 - UPON ARRIVAL AT THE GATE, OVERHEAD FLUORESCENT LIGHT NEAR PASSENGER SEAT ROW 6 ARCED CAUSING SMOKE IN THE CABIN. PASSENGER DEPLANED NORMALLY. REPLACED OVERHEAD FLUORESCENT LIGHT CONNECTOR PI2101 AND RECEPTACLE R52105 IN CABIN OVERHEAD BY PASSENGER SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)