N592AA

Part: ACTUATOR — INOPERATIVE (CABIN PRESSURE) · airframe 69,733 hrs · 30,195 cycles

STL CREW REPORTED BOTH TRANSFER LOCKOUT & STANDBY LIGHT ILLUMINATED WITH CABIN DIFFERENTIAL INCREASE & CABIN ALTITUDE DECREASING. CYCLED PRESSURIZATION SWITCH BUT HAD NO EFFECT. FLIGHT RETURNED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OUTFLOW VLV ACTUATOR. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 66,920 hrs · 28,722 cycles

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

Part: BATTERY — LOOSE (CABIN) · airframe 66,920 hrs · 28,722 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RE-SECURED LOOSE BATTERIES. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (RT WING) · airframe 65,359 hrs · 27,919 cycles

DELAMINATION ON TOP SKIN 48 INCHES OUT FROM INBOARD END AND 3.5 INCHES FROM LEADING EDGE. REMOVED DAMAGED SKIN AND CORE. PREPARED NEW FILLER AND CORE. HOT BONDED FILLER AND CORE PER SRM 51-70-02. FABRICATED DOUBLER AND HOT BONDED AND SEALED REPAIR DOUBLER PER SRM 51-70-02.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 63,487 hrs · 26,984 cycles

CORROSION SUBFLOOR MEMBRANE CORRODED. SPLICED IN NEW SUBFLOOR DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,487 hrs · 26,984 cycles

CRACK ON CANTED FRAME 1510. INSTALLED DOUBLER PER SRM 51-10-4.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,487 hrs · 26,984 cycles

CRACKED SHEAR TIE STATION 1401 LONGERONS 15 TO 16 LEFT. INSTALLED NESTLED ANGLE DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 4.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 60,816 hrs · 25,647 cycles

FOUND RIGHT AND CENTER OVERHEAD EMERGENCY LIGHTS INOPERATIVE JUST FORWARD OF AFT BULKHEAD CABIN DOOR. BATTERY PACK FOUND LOOSE IN AFT GALLEY. RE-SECURED AND RE-SEATED EMERGENCY LIGHT BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 60,816 hrs · 25,647 cycles

FOUND AFT ACCESSORY COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RE-SEATED AND RE-SECURED BATTERY PACK FOR ASSOCIATED EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,082 hrs · 24,818 cycles

BLENDED OUT INTERNAL SKIN CORROSION AROUND LEFT ALTERNATE STATIC PORT HOLE. INSTALLED REPAIR PER SRM 53-04-00 FIGURE 12C.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

GROOVE WORN INTO TOP OF LONGERON 11 LEFT AT STATION 1383. INSTALLED LONGERON SPLICE PLATE PER SRM 53-02 AND EA MD80-53-00917.

Part: TRACK — DAMAGED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

CORROSION ON LEFT AFT TIE-DOWN TRACK AROUND SEVERAL CLIP NUT HOLES AND AROUND SEVERAL MOUNT BOLTS. INSTALLED NEW LEFT AFT TRACK AND SPLICE PER SRM 51-30-01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

NUMBER 6 SEAT TRACK STATIONS 216 TO 218 TOP OUTBOARD OF TRACK BLENDED OUT OF LIMITS. SPLICE NEW SECTION OF NUMBER 6 SEAT TRACK FROM STATIONS 216 TO 267 PER SRM 53-05-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

SEAT TRACK NUMBER 5 STATIONS 203 TO 210 CORROSION REMOVAL IS BEYOND LIMITS. INSTALLED NEW SECTION OF SEAT TRACK FROM STATIONS 200 TO 246 AND A SPLICE AT STATION 246 PER SRM 53-05-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

CANTON FRAME CRACKED STATION 1418 LONGERON 2 RIGHT. REPAIR DOUBLER WAS INSTALLED PER SRM 53-03-00 FIGURE 31A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,082 hrs · 24,818 cycles

CORROSION ON AFT SIDE OF STATION 1309 FRAME BETWEEN LONGERON 27 LEFT AND LONGERON 28 LEFT. INSTALLED STATION 1309 FRAME REPAIR PER SRM 53-03-00.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,082 hrs · 24,818 cycles

CORROSION ON FORWARD GALLEY DRAINLINE PAN STATION 150. INSTALLED DOUBLER AT STATION 150 TO 160 RIGHT BUTTLINE 46 TO RIGHT BUTTLINE 57 PER AARD 53-20-00-16.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,082 hrs · 24,818 cycles

CORROSION ON GALLEY ATTACH FITTING STATION 160 RIGHT BUTTLINE 45. INSTALLED NEW FITTING PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

CORROSION ON CUSP AT STATION 200 BETWEEN NUMBER 5 AND NUMBER 6 SEAT TRACKS OUT OF LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

LEFT CUSP IS CRACKED JUST AFT OF STATION 218. INSTALLED CUSP AND DOUBLER STATION 218 TO 237 LEFT PER AARD 53-20-00-16.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,082 hrs · 24,818 cycles

CORROSION ON SUPPORT ANGLE AT STATION 210 BODY LINE 10 RIGHT. INSTALLED FITTING PER SRM 51-30-05.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,082 hrs · 24,818 cycles

CORROSION ON ATTACH FITTING AT STATION 218 BODY LINE 10 RIGHT. INSTALLED FITTING PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,082 hrs · 24,818 cycles

CORROSION OUT OF LIMITS AT STATION 440 TO 441 LEFT CUSP. INSTALLED DOUBLER AT STATIONS 440 TO 441 CUSP LEFT PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,082 hrs · 24,818 cycles

CABIN RIGHT CUSP CRACKED STATION 1265. INSTALLED DOUBLER OVER DAMAGED AREA AT STATION 1265 RIGHT CUSP AS PER AARD 53-20-00-16.

Part: VANE — GOUGED (TE FLAP) · airframe 59,082 hrs · 24,818 cycles

RIGHT WING, WEAR AREA INTO LEADING EDGE OF FLAP VANE, ABOVE INBOARD FLAP TRACK, FOR OUTBOARD FLAP. DID HOT BOND REPAIR PER SRM 51-70-02.

Part: PAN — CRACKED (WINDOW) · airframe 59,082 hrs · 24,818 cycles

CRACKED WINDOW PAN STATION 905 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,082 hrs · 24,818 cycles

WINDOW PAN RIGHT STATION 256 CRACKED AT LOWER AFT CORNER. REPAIRED WITH DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,082 hrs · 24,818 cycles

CRACKED WINDOW PAN AT STATION 886 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,082 hrs · 24,818 cycles

CRACKED WINDOW PAN STATION 927 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,082 hrs · 24,818 cycles

STATION 807 RIGHT WINDOW PAN CRACKED AT UPPER FORWARD CORNER. DAMAGED REMOVED AND DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,082 hrs · 24,818 cycles

UPPER AFT WINDOW PAN CORNER CRACKED STA 1079. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,082 hrs · 24,818 cycles

UPPER AFT WINDOW PAN CRACKED AT STATION 1041. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: STOP FITTING — WORN (L1 DOOR) · airframe 57,327 hrs · 24,058 cycles

SFO - CREW DESCRIBED POPPING SOUND COMING FROM THE FORWARD CABIN DOOR AREA. EMERGENCY DECLARED, RETURNED TO SFO WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO DUPLICATE SOUND AND FOUND POPPING SOUND COMING FROM FORWARD EDGE OF LEFT NUMBER ONE DOOR AREA JUST FORWARD OF WINDOW ON THE DOOR. FOUND THERE WAS A PROBLEM WITH HOW THE DOOR CLOSED. REPLACED 13 OF 16 DOOR STOPS DUE TO UNUSUAL WEAR AND REPLACED THE ROD FOR THE AIRSTAIR INTERLOCK DUE TO IT BEING BROKEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,655 hrs

LGA - COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERHEAD BATTERY PACK.

Part: GYRO — INOPERATIVE (COCKPIT) · airframe 56,014 hrs · 23,455 cycles

MCI - CREW REPORTED LOST ALL AUTOMATION INCLUDING AUTO-PILOT, AUTO THROTTLE, FLIGHT DIRECTOR, AUTO-COMPASS, ETC. EMERGENCY DECLARED, LANDED MCI WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DIRECTIONAL GYRO AND FIRST OFFICERS RADIO MAGNETIC INDICATOR.

Part: OIL SYSTEM — LOW PRESSURE (NR 1 ENGINE) · airframe 55,585 hrs · 23,282 cycles

EUG INFLIGHT PDX TO DFW - ABOUT TEN MINUTES AFTER TAKEOFF AT 25000 FEET OIL STRAINERS CLOG LIGHT ILLUMINATED. PRESSURE WAS DROPPING SLOWLY THROUGH 35 PSI AND OIL TEMPERATURE WAS RISING SLOWLY. CREW SHUT DOWN NR 1 ENGINE. OIL QUANTITY NORMAL. ENGINE WINDMILLED ABOUT 45 MINUTES WITH PRESSURE ABOUT 10 PSI. LANDED EUG WITHOUT INCIDENT. REPLACED NR 1 ENGINE ON 16 JUNE 2009 AT EUG DUE TO METAL FOUND IN SCREEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: INLET — CONTAMINATED (APU) · airframe 55,584 hrs · 23,281 cycles

PDX INFLIGHT - CREW REPORTED SMOKE IN CABIN AND COCKPIT FROM UNKNOWN SOURCE. SMOKE BEGAN TO DISSIPATE BUT SMELL AND VISIBLE SMOKE STILL PRESENT AFTER LANDING. RETURNED TO PDX AND LANDED WITHOUT INCIDENT. FOUND SMALL AMOUNT OF GLYCOL AT APU INLET. CLEANED APU INLET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — LOW PRESSURE (NR 2) · airframe 55,091 hrs

INFLIGHT - ABOUT 160 MILES OUT OF DFW NUMBER TWO ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ALONG WITH ZERO OIL PRESSURE READING. OIL TEMPERATURE AT 30C. CREW SHUT DOWN NR 2 ENGINE. LANDED DFW WITHOUT INCIDENT. REPLACED NR 2 ENGINE ON 4 NOV AT DFW DUE TO OIL PRESSURE OUT OF LIMITS AND REQUIRED OIL SYSTEM COMPONENT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TURBINE — FAILED (NR 2 ENGINE)

JFK INFLIGHT T2393/04AUG. LGA TO ATL. NR TWO ENGINE SEIZED ON TAKE OFF ROTATION. ALL INDICATIONS WENT TO ZERO. LANDED JFK WITHOUT INCIDENT. SINGLE ENGINE TIME 13 MINUTES. REPLACED NR TWO ENGINE DUE TO TURBINE FAILURE ON 05AUG AT JFK. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: VALVE — INOPERATIVE (A/C PACK) · airframe 53,287 hrs

SAV INFLIGHT T1914/05APR DFW TO JAX - CREW REPORTED LOSING LEFT AIR CONDITIONING PACK IN ICING CONDITIONS. FLIGHT WAS IN HOLDING PATTERN FOR JAX DUE TO THUNDERSTORMS. LANDED SAV WITHOUT INCIDENT. REPLACED LEFT AIR CONDITIONING PACK ANTI ICE VALVE AND REPLACED WATER SEPARATOR BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — FLAT (NLG) · airframe 52,722 hrs

PHL INFLIGHT T895/21JAN - NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO PHL AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT FLAT. REPACKED NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — OUT OF POSITION (CABIN)

DFW - EMERGENCY PATH LIGHTS ON SEATS 28D AND 29D NOT IN CORRECT POSITION. REPOSITIONED EMERGENCY PATH LIGHTS FOR SEATS 28D AND 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COALESCER BAG — DIRTY (AIR CONDITIONING)

ORD INFLIGHT T1184/15FEB - CREW REPORTED SMOKE IN CABIN AND COCKPIT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING AND CHANGED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (RT ENG HYDRAULIC)

RT ENGINE PUMP INOPERATIVE. RT HYDRAULIC PRESSURE LOW LIGHT ON. LANDED ORD WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC PUMP AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — UNDERSERVICED (NLG)

NLG WOULD NOT RETRACT. LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT WITH NITROGEN AND OIL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — STALLED (LEFT)

LT ENGINE COMPRESSOR STALLS DURING CLIMB-OUT AT 11,000 FT. ENGINE ACCELERATED FOR CLIMB NORMALLY BUT STARTED STALLS WHILE AT FULL CLIMB THRUST. ENGINE ANTI-ICE ON. ENGINE FAIL CHECKLIST ACCOMPLISHED. ENGINE LEFT AT IDLE. FOUIND NUMEROUS LEFT ENGINE FAN BLADES DAMAGED. REPLACED LEFT HAND ENGINE PER CARD 71 91 99. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — FOD (ZONE 500)

ORD - INFLIGHT LEFT ENGINE COMPRESSOR STALLS DURING CLIMBOUT AT 11,000 FT. ENGINE ACCELERATED FOR CLIMB NORMALLY BUT STARTED STALL WHILE AT FULL CLIMB THRUST. ENGINE ANTI-ICE ON. ENGINE FAIL CHECKLIST ACCOMPLISHED. ENGINE LEFT AT IDLE. FOUND INLET FOD. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COALESCER BAG — CONTAMINATED

ABQ INFLIGHT T1114/25 - AFTER TAKEOFF FLIGHT ATTENDANT REPORTED GREYISH SMOKE THROUGHOUT ENTIRE CABIN. SMELL WAS A HOT SMELL. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. FOUND APU INLET SOAKED WITH OIL. REMOVED AND REPLACED WATER SEPARATOR COALESCER. CLEANED AND REPLACED BAGS AND ACCOMPLISHED A PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — WORN (FUSELAGE)

TUL - FOUND SKIN AND FASTENER HEAD WORN STATION 1338 L5R. INSTALLED DOUBLER AND NEW FASTENERS PER SRM 53-04 FIG 12B SHEET 7. (M)

Part: HINGE — CORRODED (HORIZ STAB)

TUL - FOUND CORROSION IN LEFT STAB HINGE BORE OUTBOARD SIDE BETWEEN LUG AND BUSHING. REMOVED CORROSION PER ESO 80559 DATED 4-11-02 AND INSTALLED OVERSIZE BUSHING. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED AROUND FASTENER LONGERON 13L AT STATION 1380. REMOVED DAMAGE. DYE CHECK SKIN, INSTALLED DOUBLER PER SRM 53-01 FIGURE 2. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND LEFT AFT CABIN FLOOR CUSP CRACKED BETWEEN LIGHTENING HOLES, INBOARD OF PREVENTIVE DOUBLER, STATION 1300. ROUTED-OUT DAMAGED SECTION OF CUSP. INSTALLED INTERIM REPAIR FILLER AND DOUBLER PER ESO 80559. (M)

Part: SKIN — WORN (FUSELAGE)

TUL - FOUND FUSELAGE SKIN WORN AT LONGERON 7R PLUS 4 INCHES. INSTALLED DOUBLER AT STATION 599 L7R PLUS 4 INCHES PER SRM 53-04 FIG 38. (M)

Part: WINDOW FRAME — DAMAGED (FUSELAGE)

TUL - FOUND OVERSIZED HOLE LOCATED ON TOP LEFT CORNER OF CAPTAINS AFT WINDOW FRAME. OVERSIZED DAMAGED HOLE AND INSTALLED DOUBLER PER ENGINEERING ESO. (M)

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN J-ANGLE OF FRAME STATION 1271, AFT SIDE AT LONGERON 20. REMOVED CORROSION. TREATED AND PRIMED AREA. INSTALLED J-ANGLE REPAIR DOUBLER PER AARD 53-10-00-14, REPAIR 1. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN GOUGE AT STATION 237 LONGERON 18L, DENT IN SKIN STATION 241 LONGERON 18 AND 19L, DENT IN SKIN STATION 247 LONGERON 18 AND 19L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B SHEET 34/AARD 53-30-00-11. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND STATION 1300 LEFT CUSP CRACKED. INSTALLED DOUBLER PER SRM 53-01-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION STATION 1203 NR 1 TRACK. INSTALLED NEW TRACK STATION 1174 TO 1307 51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 2 STATION 1305-1307. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIG 4A. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND CABIN FLOORBOARD SUPPORT CORRODED AT STATION 200 RBL 62. REMOVED CORRODED SUPPORT ANGLE, INSTALLED NEW SUPPORT 51-01. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND WINDOW FRAME CRACKED STATION 947 LONGERON 12L. STOP DRILLED, CRACK AND INSTALLED DOUBLER PER 53-10-00-25 PAGE 2 FIG 1. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND WINDOW FRAME CRACKED STATION 1021 LONGERON 12L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-25 PAGE 2 FIG 1. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND LEFT WINDOW FRAME ANGLE CRACKED. STOP DRILLED END OF CRACK, CONFIRMATION WITH DYE CHECK. INSTALLED ANGLE DOUBLER PER AARD 53-10-00-25. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (MLG)

SEA - FLT 330 - DURING FLIGHT, RED NOSE GEAR LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP. DIVERTED AND LANDED SEA WITHOUT INCIDENT. REPLACED SCHRAEDER VALVE AD O-RING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: UNKNOWN — ODOR (CABIN)

MEX - FLT 1156 - AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED BURNING ODOR IN AFT CABIN. INSPECTED AIRCRAFT PACKS, COFFEEMAKERS, OVENS, CABIN ILLUMINATION SYSTEM, AND RAN ENGINES. COULD NOT DUPLICATE ODOR. ACCOMPLISHED PACK BURNOUT AND REPLACED COALESCER BAGS AS A PRECAUTION. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT TAIL CONE RELEASE FLOOR LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT TAIL CONE RELEASE FLOOR LIGHT CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: DUCT — CRACKED (WATER SEPARATOR)

DFW - FLT 819 - AFTER TAKEOFF DFW DURING CLIMB-OUT THROUGH FL190, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO DFW, LANDING WITHOUT INCIDENT. PLACARDED RT PACK DUE TO CRACK IN WATER SEPARATOR DUCT ASSEMBLY. SUBSEQUENTLY AT TUL/07 WELD REPAIRED RT PACK WATER SEPARATOR DUCT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION AND PLACARD REMOVED. (M)

Part: APU — LEAKING OIL (APU COMPARTMENT)

EWR - FLT 1223 - DURING TAKEOFF FROM EWR, SLIGHT SMOKE NOTED IN CABIN. TURNED OFF BOTH AIR CONDITIONING PACKS AND SMOKE CLEARED. AIRCRAFT RETURNED TO EWR AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED APU DUE TO OIL LEAKAGE. ACCOMPLISHED PNEUMATIC SYSTEM DUCT BURN-OUT PROCEDURE. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION WITH NO SMOKE OR SMELL NOTED. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (X)