N454AA

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 71,865 hrs · 37,923 cycles

RED CABIN ALTITUDE LIGHT ILLUMINATED & AURAL CABIN ALTITUDE SOUNDED. CABIN ALTITUDE WAS INITIALLY ABOVE 10,000 FEET. REPLACED NR 1 & 2 AUTO CABIN PRESSURE CONTROLLERS. SYSTEM GROUND CHECKED NORMAL

Part: BATTERY — DIRTY (CABIN) · airframe 71,591 hrs · 37,776 cycles

EMERGENCY LIGHT IN AFT CABIN BY ROW 28 INOPERATIVE. CLEANED BATTERY. OPS CHECK NORMAL.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 66,158 hrs · 34,775 cycles

CREW REPORTED LEFT ENGINE COMPRESSOR STALLED DURING CLIMBOUT. ENGINE RETURNED TO IDLE WITH HIGH EGT. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. UPON INSPECTION FOUND TURBINE FAILURE. REPLACED LEFT ENGINE AT ELP ON 04/22/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

AFT CARGO DOOR BEAM, APPROXIMATE STATION 1192 SKIN AND DOOR BEAM HAVE AN EXTRA HOLE. INSTALLED STRAIGHT SHANK REPAIR BUSHINGS PER SRM 51-30-10 AND EA MD80-53-015817.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

LONGERON 3 LEFT CRACKED AT STATION 218. ACCOMPLISHED LONGERON 3 LEFT SPLICE REPAIR STATIONS 148 TO 228 PER SRM 53-02-00 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

LONGERON 3 LEFT CRACKED AT STATION 160. ACCOMPLISHED LONGERON 3 LEFT SPLICE REPAIR STATIONS 148 TO 228 PER SRM 53-02-00 FIGURE 18.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

CORROSION ON WEBBING STATIONS 1155 TO 1212 LONGERONS 29 TO 28 RIGHT. INSTALLED NEW WEB PER AARD 51-10-00-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

LONGERON 4 LEFT CRACKED AT STATION 200. ACCOMPLISHED LONGERON 4 LEFT REPAIR STATIONS 170 TO 228 PER SRM 53-02-00 FIGURE 18.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

AFT CARGO CORROSION ON THRESHOLD BEAM AND EMITTING FROM UNDER STAINLESS REPAIR DOUBLER STATIONS 1155 TO 1212. INSTALLED NEW DOOR BEAM PER AARD 51-10-00-5 AND EA MD80-53-015817.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

CRACK STATION 218 ON SUBFLOOR JUST INBOARD OF NUMBER 1 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

ANGLE CRACKED ON AFT SIDE OF STATION 875 ABOVE LEFT FORWARD OVERWING EXIT DOOR, VISIBLE THROUGH AFT LIGHTENING HOLE. INSTALLED NEW ANGLE ON AFT SIDE OF LEFT FORWARD OVERWING EXIT DOOR STATION 875 PER AARD57-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

CARGO AFT CORROSION ON BOTTOM OF CUSP LEFT SIDE AT STATIONS 1174 TO 1176. INSTALLED DOUBLER PER AARD 53-20-0016.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

HEAVY CABIN - CORROSION ON GIRT BAR ATTACH POINT AT CUSP AT AFT SERVICE DOOR AFT FITTING. INSTALLED DOUBLER ON CUSP AT AFT SERVICE DOOR AREA PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

HOLE IN RIGHT CUSP STATION 725. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

NUMBER 1 SEAT TRACK STATION 793 BLENDED OUT OF LIMITS. INSTALLED NUMBER 1 SEAT TRACK PLUG STATION 793 PER SRM 53-05-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

LEFT CUSP AT STATION 218 HAS A CRACK AT OUTBOARD FASTNER HOLE. INSTALLED SUBFLOOR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

FOUND CORROSION TO BE OUT OF LIMITS AT LEFT STATIONS 839 TO 843. INSTALLED DOUBLER AT LEFT STATIONS 839 TO 843 PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

SUB-FLOOR CORROSION UNDER NUMBER 2 GALLEY INBOARD TIE-DOWN FITTING AT STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED SUB-FLOOR DOUBLER AT NUMBER 2 GALLEY INBOARD TIE-DOWN FITTING PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

CUSP MEMBRANE AT FORWARD ENTRY AREA HAS CORROSION FROM STATIONS 170 TO 200. INSTALLED DOUBLER AS PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

CORROSION ON SEAT TRACK NUMBER 2 AT STATION 1195. INSTALLED NEW SECTION OF SEAT TRACK PER SRM 53-05-00 FIGURE 4.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

RIGHT CUSP SHEET IS OUT OF LIMITS AT STATIONS 1022 TO 1098. INSTALLED NEW CUSP SHEET AT STATIONS 1022 TO 1098 PER AARD 51-10-00-5 AND EA MD8051-015719.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

CUSP MEMBRANE AT FORWARD ENTRY AREA HAS CORROSION FROM STATIONS 170 TO 200. INSTALLED DOUBLER AS PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

RIGHT CUSP SHEET OUT OF LIMITS STATIONS 1022 TO 1098. COMPLETED INSTALLATION OF NEW CUSP SHEET BETWEEN STATIONS 1022 TO 1098 PER AARD 51-10-00-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

CRACK IN CUSP STATION 224. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

RIGHT CUSP SHEET IS OUT OF LIMITS FROM STATIONS 598 TO 712. INSTALLED NEW CUSP PER AARD 51-10-00-5 AND EA MD80-51-015719.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

LEFT CUSP CORROSION OUT OF LIMITS FROM STATIONS 1250 TO 1309. REMOVED AND REPLACED CUSP SHEET PER AARD 51-10-00-5.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

AFT ACCS SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 LEFT. INSTALLED NEW SERVICEABLE SHEAR TIE AT STATION 1451 LONGERON 2 LEFT PER SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

CORROSION REMOVAL BEYOND LIMITS ON SEAT TRACK NUMBER 2 FROM STATIONS 223 TO 224. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

NUMBER 6 SEAT TRACK STATION 1105 PLUG BLENDED OUT OF LIMITS. NUMBER 6 SEAT TRACK PLUG INSTALLED PER 53-20-00-10.

Part: SKIN — DENTED (TE FLAP) · airframe 65,995 hrs · 34,681 cycles

DENT IN BOTTOM OF SKIN APPROXIMATELY 6 FEET OUTBOARD OF ELEPHANT EAR FAIRING, LEFT HAND INBOARD FLAP. FABRICATED AND INSTALLED PERMANENT FLUSH REPAIR DOUBLER AND FILLER PER SRM 57-01-00, FIGURE 5 SHEET 2 AND AARD 51-60-00-05 AND SRM 51-30-02, PARAGRAPH 11.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

CABIN ABOVE CENTER TANK INTERCOSTAL LOWER SUPPORT ANGLE CRACKED AT STATION 826 BELOW NUMBER 2 SEAT TRACK. INSTALLED ANGLE DOUBLERS PER EA MD80-53-015688.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

CABIN ABOVE CENTER TANK VERTICAL SUPPORT ANGLE LOWER LEG CRACKED AT STATION 927 BELOW NUMBER 5 SEAT TRACK. INSTALLED REPAIR DOUBLER AND FILLER PER EA MD80-53-015690.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

RIGHT CUSP STATION 1004 CRACKED ON INBOARD EDGE. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

NUMBER 5 SEAT TRACK STATION 235 PLUG BLENDED OUT OF LIMITS. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

CABIN ABOVE CENTER TANK INTERCOSTAL LOWER SUPPORT ANGLE CRACKED AT STATION 826, BELOW NUMBER 5 SEAT TRACK. REPAIRED CENTER TANK INTERCOSTAL LOWER SUPPORT ANGLE AT STATION 826, BELOW NUMBER 5 SEAT TRACK PER EA MD80-53-015688.

Part: MOUNT — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 65,995 hrs · 34,681 cycles

NUMBER 1 GALLEY INBOARD TIE DOWN FITTING HAS CORROSION STATION 160. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

FUSELAGE LEFT SIDE DENT IN FUSELAGE SKIN AT STATION 370 APPROXIMATELY JUST BELOW LONGERON 27 LEFT. REPAIRED DAMAGE AT STATION 370 LONGERON 27 LEFT PER SRM 53-04-00 FIGURE 38 VIEW E.

Part: PAN — CRACKED (WINDOW) · airframe 65,995 hrs · 34,681 cycles

WINDOW PAN CRACKED AT LOWER FORWARD TAB LEFT STATION 1060. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: FITTING — CORRODED (FUSELAGE) · airframe 65,995 hrs · 34,681 cycles

NUMBER 2 GALLEY INBOARD TIE-DOWN FITTING HAS CORROSION STATION 218 INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED NEW NUMBER 2 GALLEY INBOARD TIE-DOWN FITTING PER AARD 51-10-00-5.

Part: PAN — CRACKED (WINDOW) · airframe 65,995 hrs · 34,681 cycles

RIGHT WINDOW PAN CRACKED, UPPER FORWARD SIDE AT STATION 946. REMOVED DAMAGE BY ROUTING PER AARD 53-10-00-25 AND INSTALLED REPAIR DOUBLER CDK 3488-2 PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 65,995 hrs · 34,681 cycles

RIGHT WINDOW PAN CRACKED AT UPPER FORWARD SIDE AT STATION 927. REMOVED CRACK BY ROUTING PER AARD 53-10-00-25 AND INSTALLED REPAIR DOUBLER CDK 3488-2 PER AARD 53-10-00-25.

Part: BATTERY — NOT SEATED (CABIN) · airframe 65,172 hrs · 34,247 cycles

FOUND CEILING EMERGENCY LIGHTS INOPERATIVE FROM SEATS 28 TO ROW 30. RESEATED THE EMERGENCY LIGHT BATTERY. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,449 hrs · 33,882 cycles

RIGHT AFT OVERWING EXIT DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. REPLACED BATTERY PACK FOR RIGHT AFT EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: RECEPTACLE — BROKEN (CABIN) · airframe 64,449 hrs · 33,882 cycles

SEAT 7D FORWARD EMERGENCY PATH LIGHT RECEPTACLE BROKEN. REPLACED SEAT 7D EMERGENCY PATH LIGHT RECEPTACLE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,780 hrs · 32,958 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK.

Part: CASTING — CRACKED (SPOILER) · airframe 62,780 hrs · 32,958 cycles

RIGHT GROUND SPOILER ACTUATOR CASTING CRACKED AT OUTBOARD FORWARD LEG. SPOILER CASTING REPLACED PER SRM 51-30.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,780 hrs · 32,958 cycles

RIGHT 1497 CANTON FRAME CRACKED AT LONGERON 15 RIGHT. REPAIRED DOUBLER INSTALLED PER ENGINEERING AUTHORIZATION MD80-53-007945 DATED 10/29/2009.

Part: SHROUD — MISSING (CABIN) · airframe 62,690 hrs · 32,904 cycles

EMERGENCY LIGHT AT SEAT 11D IS MISSING SHROUD. REPLACED SHROUD AT SEAT 11D.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 62,566 hrs · 32,837 cycles

CREW REPORTED THE RIGHT HYDRAULIC PRESSURE LOW AND THE RUDDER CONTROL MANUAL LIGHT ILLUMINATED IN FLIGHT. CREW RAN THE EMERGENCY GEAR EXTENSION CHECKLIST TO GET THREE GREEN LIGHTS. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC ENGINE DRIVEN PUMP AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BRACKET — DAMAGED (ZONE 700) · airframe 61,522 hrs · 32,275 cycles

JFK - INFLIGHT LGA-ORD. CAPTAIN REPORTED HE HAD GEAR LIGHT INDICATING GEAR DOWN WHEN IT SHOULD HAVE BEEN UP AND THERE WAS A BURNING RUBBER SMELL IN COCKPIT. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AND RIGHT AIR CONDITIONING REGULATE VALVE. REPLACED RIGHT MAIN LANDING GEAR DOOR TARGET AND BRACKET ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — BROKEN (CABIN)

MSP - EMERGENCY LIGHT AT SEAT 30D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: SHROUD — BROKEN (CABIN)

MSP - EMERGENCY LIGHT AT SEAT 32D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — DISCHARGED (CABIN)

MSP - EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT B5 103 FOR EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LINE — BROKEN (NR 1 ENG FUEL)

STL INFLIGHT T1400/28SEP - NR 1 ENGINE FIRE IN FLIGHT. LOST BOTH SYS HYDRAULICS. RETURNED TO STL AND LANDED WITHOUT INJURIES. FIRE TEAM MET FLT UPON LANDING AND FOAMED BOTH ENGINES. PASSENGERS DEPLANED VIA FORWARD LEFT DOOR USING STAIRS. SINGLE ENGINE TIME 20 MINUTES. 10-16-07 AIRCRAFT OUT OF SERVICE FOR EVALUATION. AIRCRAFT UNDER CONTROL OF NTSB. INITIAL FINDING IS MAIN FUEL LINE FLEX HOSE BROKE. BOTH ENGINES HAVE BEEN REMOVED. SIGNIFICANT PYLON DAMAGE. UNABLE TO DETERMINE COURSE OF ACTION FOR AIRCRAFT AT THIS TIME. (SUPP CLOSED)

Part: STRUT — INOPERATIVE (NLG)

AUS INFLIGHT T1560/27JUL - NOSE LANDING GEAR DID NOT RETRACT WHEN HANDLE WAS SELECTED UP. RETURNED TO AUS AND LANDED WITHOUT INCIDENT. DEFLATED STRUT COMPLETELY AND ACCOMPLISHED FULL OIL AND AIR SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR — DAMAGED (NLG)

DFW INFLIGHT T2055/19JUL - UNABLE TO EXTINGUISH RED NOSE GEAR LIGHT ON GEAR RETRACTION. CREW REPORTED LOUD AIR NOISE COMING FROM NOSE GEAR AREA. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPAIRED NOSE GEAR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE SWITCH — INOPERATIVE (A/C PACK)

DFW - AFTER TAKEOFF MASTER CAUTION LIGHT ILLUMINATED. PRESSURE FLOW FOR BOTH PACKS INDICATED ZERO POUNDS PER SQUARE INCH (PSI) AND BOTH PRESSURE LIGHTS ON THE CONTROLLER WERE ILLUMINATED. COULD NOT REINSTATE PACKS. RETURNED TO ELP AND LANDED WITHOUT INCIDENT. REPLACED PRESSURE SWITCHES FOR BOTH PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN BLADE — DAMAGED (NR 1 ENGINE)

INFLIGHT AFTER TAKEOFF LOUD VIBRATION REPORTED BY FLIGHT ATTENDANT. VIBRATION AT ROW 26 AND AFT. VERIFIED BY FIRST OFFICER. COULD NOT ISOLATE TO SPECIFIC ENGINE OR AIRFRAME. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND EVIDENCE OF BIRD STRIKE IN THE NUMBER 1 ENGINE INLET. PERFORMED BIRD STRIKE INSPECTION. REPLACED TWO EACH FAN BLADES IN NUMBER 1 ENGING PER WORK CARD 72-91-11. CONDUCTED PAST FAN BLADE REPLACEMENT ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY CEILING LIGHTS AT 8A-16 INOPERATIVE. REPLACED BATTERY PACKS AT 8DEF AND 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RDU - FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT LAVATORY ARE INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, OVERHEAD CEILING EMERGENCY EXIT LIGHT FORWARD OF AFT EXIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — FAILED (ACM BAY)

EN ROUTE DEN-DFW, ON TAKEOFF ROLL, HEAR A FAN TYPE NOISE SIMILAR TO INSTRUMENT COOLING FAN CYCLING ON/OFF SEVERAL TIMES. PAST V1 HAD BLAST OF AIR AND SAW SMOKE (GRAY) IN COCKPIT WITH PACK FLOW OFF. TURNED LEFT PACK OFF, SMOKE STOPPED IMMEDIATELY. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. INSPECTED COCKPIT, CABIN AND TAIL SECTION OF AIRCRAFT. NO SMOKE OR ODOR DETECTED. REPLACED LT PACK HEAT EXCHANGER COOLING FAN. SYSTEM GROND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT DOOR LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — MALFUNCTIONED (NLG)

DFW - FLT 2229 - DURING APPROACH DFW LANDING GEAR WARNING HORN CAME ON. INITIALLY HAD 3 GREEN LIGHTS THEN NOSE GEAR RED LIGHT ILLUMINATED. NOSE LANDING GEAR INDICATED UP POSITION. RECYCLED GEAR WITH SAME RESULTS, RAN QRH PROCEDURE WITH GEAR UP WITH NOSE GEAR INDICATING LIGHT STILL RED. GEAR LOWERED AND NOSE GEAR LIGHT REMAINED RED WITH NOSE LANDING GEAR INDICATING UP. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE GEAR LOCK SENSOR AND ACCOMPLISHED REQUIRED CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TURBINE — OVERSERVICED (NOSE SECTION)

ORD - FLT 0571 - DURING CLIMB FL 150, CABIN FILLED WITH SMOKE AND SMELL OF HOT DUCTING. CREW SELECTED RIGHT HI PRESSURE BLEED-OFF, RIGHT PNEUMATIC X-FEED CLOSED, AND AIRFOIL ANTI-ICE VALVES OFF. SMOKE AND HOT DUCTING SMELL DISSIPATED. AIRCRAFT CONTINUED TO ORD WITH RIGHT ACM ISOLATED AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAKEN OUT OF SERVICE. TROUBLESHOOTING FOUND RIGHT ACM'S HAD BEEN OVER SERVICED. DRAINED EXCESS OIL AND ACCOMPLISHED RIGHT PACK BURN-OUT PER MM PROCEDURES. REPLACED RIGHT HAND WATER SEPARATOR BAG. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: TURBINE — DEFECTIVE (NOSE SECTION)

DTW - FLT 1932 - DURING TAKEOFF DFW, FLIGHT CREW NOTED ACRID SMELL AND HAZE IN CABIN. CREW TURNED OFF RECIRCULATING FAN AND INCREASED TEMPERTURE, HAZE, AND SMELL DISSIPATED. AIRCRAFT COTNINUED TO DTW WITH NO FURTHER SMELL NOTED UNTIL DESCENT WHEN SMELL RETURNED. AIRCRAFT LANDED DTW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAKEN OUT OF SERVICE AND MAINTENANCE REPLACED BOTH AIR CYCLE MACHINES AND ACCOMPLISHED BURN-OUT PER MM PROCEDURES. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. REF: OPER CONTROL NR AALA980790.

Part: TURBINE — DEFECTIVE (NOSE SECTION)

DTW - FLT 1932 - DURING TAKEOFF DFW, FLIGHT CREW NOTED ACRID SMELL AND HAZE IN CABIN. CREW TURNED OFF RECIRCULATING FAN AND INCREASED TEMPERATURE, HAZE, AND SMELL DISSIPATED. AIRCRAFT CONTINUED TO DTW WITH NO FURTHER SMELL NOTED UNTIL DESCENT WHEN SMELL RETURNED. AIRCRAFT LANDED DTW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAKEN OUT OF SERVICE AND MAINTENANCE REPLACED BOTH AIR CYCLE MACHINES AND ACCOMPLISHED BURN-OUT PER MM PROCEDURES. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. REF: OPER CONTROL NR 98ZZZX1934. (X)

Part: WIRE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGH CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STATOR — FAILED (LT ENG 1ST STG)

MDT - FLT T035 - EN ROUTE ORD/LGA DURING CRUISE, LT ENG FAILED FOLLOWED BY SMOKE IN COCKPIT. ACCOMPLISHED LT ENG SHUT DOWN AND PRECAUTIONARY PULLED FIRE HANDLE FOR LT ENG. SMOKE CLEARED. AIRCRAFT DIVERTED TO MDT AND LANDED WITHOUT INCIDENT. REPLACED LT ENG. SHOP FINDINGS: RIVETS FROM THE 1ST STG COMP STATOR VANE FAILED AND NICKED A 1ST STG COMP FAN BLADE ON THE TRAILING EDGE 2 INCHES OTBD OF THE PLATFORM. A CRACK DEVELOPED OUT OF THIS NICK, LATER CAUSING THE FAN BLADE TO FAIL. THIS CAUSED AN ADJACENT FAN BLADE TO FAIL AT THE PLATFORM. THERE WAS VERY HEAVY DAMAGE THROUGHOUT THE LPC ABD HPC AS A RESULT OF THE FAILURE.

Part: COVER — CRACKED (LT ENGINE)

IAD - FLT 845 - WHILE EN-ROUTE EWR-DFW - DIVERTED TO IAD DUE TO FUMES IN CABIN. LEFT ENGINE HAD AN UNUSUAL NOISE DURING FLIGHT. LANDED OVERWEIGHT AT IAD WITHOUT INCIDENT. REPLACED N1 TACH ACCESSORY HOUSING ACCESS COVER AND AIR CONDITIONING PACK FILTERS. PERFORMED OVERWEIGHT LANDING AND PERFORMED ENGINE RUN UP. NO EXCESSIVE NOISE, VIBRATION, OR SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

LGA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRES AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)