N578AA

Part: SIGN — BROKEN (CABIN) · airframe 64,021 hrs · 33,306 cycles

EMERGENCY EXIT SIGN ABOVE LT NR 1 SERVICE DOOR FOUND BROKEN. REPLACE EMERGENCY EXIT SIGN ABOVE LT NR 1 SERVICE DOOR. OPERATION CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,357 hrs · 32,371 cycles

EMERGENCY LIGHTS FROM ROW 20 FORWARD INOPERATIVE. REPLACED FORWARD OVERWING BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (AC BAY) · airframe 61,470 hrs · 31,832 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED AFT EMERGENCY BATTERY PACK. OPS CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,470 hrs · 31,832 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESET MID EMERGENCY BATTERY. OPS CHECKS NORMAL.

Part: HINGE — CRACKED (LT WING) · airframe 60,920 hrs · 31,506 cycles

LEFT WING PANEL 1503A BUTE DOOR FORWARD HINGE HAS A 1/2 INCH CRACK LOCATED APPROXIMATELY 3 FEET INBOARD OF THE 4TH FLAP HINGE FAIRING AND PANEL 1502C BUTE DOOR FORWARD HINGE HAS A 3/8 INCH CRACK LOCATED APPROXIMATELY 6 INCHES OUTBOARD OF THE 2ND FLAP HINGE FAIRING. INSTALLED DOUBLER STRAP PER EA AND SRM 57-01-00.

Part: HINGE — CRACKED (RT WING) · airframe 60,920 hrs · 31,506 cycles

RIGHT WING PANEL 1603A BUTE DOOR FORWARD HINGE HAS A 1/2 INCH CRACK LOCATED APPROXIMATELY 3 FEET INBOARD OF THE 4TH FLAP HINGE FAIRING. INSTALLED MIDDLE HINGE AND REPAIR STRAP PER EA.

Part: CASTING — CRACKED (SPOILER) · airframe 60,920 hrs · 31,506 cycles

GROUND SPOILER ACTUATOR FITTING ON LEFT WING TRAILING EDGE IS CRACKED ON THE INBOARD FORWARD CORNER. REPLACED CASTING PER AARD 51-00-05-1.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,257 hrs · 29,426 cycles

HEAVY CABIN CORROSION ON SUBFLOOR, APPROXIMATELY 6 INCHES INBOARD OF FORWARD SERVICE THRESHOLD ATTACH CHANNEL, STATIONS 180 TO 190. INSTALLED REPAIR DOUBLER AND OVERLAY DOUBLER AT STATIONS 160 TO 200 RIGHT BUTTLINES 41 TO 57 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

STATION 220, CRACK IN RIGHT CUSP BELOW NUMBER 6 SEAT TRACK. STATION 218, CRACK IN RIGHT CUSP OUTBOARD OF NUMBER 5 SEAT TRACK. REMOVED CRACKED CUSP SHEET AND INSTALLED SERVICEABLE CUSP SHEET AT STATIONS 218 TO 237 PER AARD 51-10-00-5.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,257 hrs · 29,426 cycles

CORROSION FOUND AT AFT LAV PAN. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIGURE 38.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,257 hrs · 29,426 cycles

STATION 1174 LONGERON 28 RIGHT, AFT CARGO DOOR CUTOUT, PLATE ON WEB HAS CORROSION. INSTALLED SERVICEABLE PLATE PER AARD 51-10-00-5 AND EA MD 80-51-015302.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

MIS-DRILLED HOLE RIGHT BUTTLINE 59 AND RIGHT STATION 229. INSTALLED DOUBLER PER EA MD80-53-015353.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

MISDRILLED HOLE STATION 200 RIGHT BUTTLINE 56 ON FLOORBEAM. INSTALLED FLOORBEAM REPAIR STRAP STATION 200 RIGHT BUTTLINE 56 PER EA MD80-53-015352.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

NOSE LANDING GEAR-LEFT AFT DOOR-AFT HINGE CUTOUT IS CRACKED. ROUTED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05-00 FIGURE 62.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

AFT CARGO HAS A CRACK IN INTERCOSTAL BETWEEN CEILING BEAMS AT BUTTLINE 0 BETWEEN STATIONS 1287 TO 1309. INSTALLED INTERCOSTAL BETWEEN CEILING BEAMS AT STATIONS 1287 TO 1309 PER AARD 51-10-00-05.

Part: SHELF — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,257 hrs · 29,426 cycles

AFT CARGO DOOR CUTOUT TOP SHELF INBOARD END HAS CORROSION FORWARD STATION 1212. REMOVED AND REPLACED CORRODED SHELF PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

RIGHT FUSELAGE CUSP SHEET CORRODED OUT OF LIMITS STATIONS 1250 TO 1308. REMOVED DAMAGED CUSP AND INSTALLED NEW PER AARD 51-10-00-5.

Part: SHELF — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,257 hrs · 29,426 cycles

AFT CARGO DOOR CUTOUT TOP SHELF INBOARD END HAS CORROSION AFT STATION 1155. REMOVED AND REPLACED DOOR CUTOUT FORWARD SHELF PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

CORROSION ON SUBFLOOR AT STATIONS 206 TO 218 AT FORWARD END OF NUMBER 6 SEAT TRACK. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

NOSE LANDING GEAR AFT GEAR DOOR HINGE CUTOUT IS CRACKED RIGHT SIDE. INSTALLED DOUBLER PER SRM 53-05-00 FIG 62.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,257 hrs · 29,426 cycles

RIGHT CUSP AT STATIONS 1220 TO 1231 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,257 hrs · 29,426 cycles

LEFT CUSP CRACKED AT STATION 493. REPAIRED CUSP AT LEFT STATION 493 BY INSTALLING DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 57,257 hrs · 29,426 cycles

WINDOW PAN CRACKED LEFT AT STATION 1249. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,257 hrs · 29,426 cycles

NUMBER 4 SEAT TRACK CORROSION REMOVAL IS OUT OF LIMITS AT STATION 1271. INSTALLED CHANNEL AND PLUG PER AARD 53-20-00-10 AND SRM 53-05-00 FIGURE 4A (SHEET 1).

Part: PAN — CRACKED (WINDOW) · airframe 57,257 hrs · 29,426 cycles

CABIN LEFT AFT WINDOW PAN CRACKED STATION 1211 (TOP AFT). CUT OUT CRACKED AREA OF RINGPAN, DRILLED UP DOUBLER AND INSTALLED ALL PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,257 hrs · 29,426 cycles

LEFT STATION 788 WINDOW RING PAN CRACKED UPPER FORWARD CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25 .

Part: PAN — CRACKED (WINDOW) · airframe 57,257 hrs · 29,426 cycles

RIGHT SIDE WINDOW PAN IS CRACKED AT STATION 845 UPPER FORWARD SIDE. INSTALLED REPAIR DOUBLER AT RIGHT WINDOW RING PAN STATION 845 PER AARD 53-10-00-25.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 57,257 hrs · 29,426 cycles

RIGHT NUMBER 5 SLAT, 2ND FROM OUTBOARD END CRACKED. REMOVED 2ND FROM OUTBOARD ATTACHED FITTING: LOCATED, DRILLED, AND INSTALLED NEW FITTING PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 57,257 hrs · 29,426 cycles

WINDOW RING PAN CRACKED UPPER AFT CORNER, STATION 1060 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,257 hrs · 29,426 cycles

WINDOW RING PAN CRACKED, UPPER AFT CORNER, STATION 1022 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 56,598 hrs · 29,059 cycles

FORWARD INBOARD G1 GALLEY MOUNT IS CORRODED. REMOVED AND REPLACED FORWARD INBOARD G1 GALLEY MOUNT PER SRM 51-30-05.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,161 hrs · 28,843 cycles

CEILING EGRESS LIGHTS AT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7 TO 11. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,161 hrs · 28,843 cycles

CEILING EGRESS LIGHTS AT ROWS 23 THROUGH 27 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EGRESS LIGHTS FROM ROWS 23 TO 27. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,161 hrs · 28,843 cycles

CEILING EGRESS LIGHTS INOP ROWS 18 TO 22. REPLACED EMERGENCY BATTERY PACK AT ROW 25 DEF. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,161 hrs · 28,843 cycles

SEAT EGRESS LIGHTS WEAK FROM ROWS 3 TO 20. REPLACED BATTERY PACK FOR SEAT EGRESS LIGHTST FROM ROWS 3 TO 20. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,161 hrs · 28,843 cycles

SEAT EGRESS LIGHTS FROM ROWS 21 TO 32 INOPERATIVE. REPLACED BATTERY PACK AT ROW 25 DEF. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,955 hrs · 28,186 cycles

FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE DURING ROUTINE TEST OF EMERGENCY LIGHTS. REMOVED AND REPLACED ASSOCIATED BATTERY PACK FOR AFFECTED EMERGENCY LIGHTS, OPS CHECKS NORMAL.

Part: SENSOR — FAILED (NLG) · airframe 53,724 hrs · 27,528 cycles

NOSE GEAR INDICATOR RED LIGHT REMAINED ON AFTER GEAR HANDLE PLACED IN UP POSITION. GEAR EXTENDED NORMALLY. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED D1-32 NOSE GEAR LOCK SENSOR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,721 hrs · 27,526 cycles

CORROSION ON CORNER FITTING. INSTALLED NEW FITTING PER SRM 51-30-00.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,721 hrs · 27,526 cycles

CORROSION ON CARGO DOOR FRAME. REPAIRED PER EA MD80-53-00=7585 AND SRM 51-70-5.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 53,721 hrs · 27,526 cycles

CARGO DOOR LOWER FORWARD STOP FITTING CRACKED. REPLACED STOP FITTING WITH NEW FITTING PER ESO 80174.

Part: FRAME — CRACKED (BS 1510) · airframe 53,721 hrs · 27,526 cycles

CRACK ON CANT FRAME 1510 AT GUIDE PIN, THIRD FROM TOP RIGHT. INSTALLED DOUBLER PER SRM 53-01, PARA 4.

Part: STOP FITTING — CRACKED (DOOR) · airframe 53,721 hrs · 27,526 cycles

STOP PAD FITTING CRACKED, FORWARD SIDE AT LOWER END OF DOOR. REMOVED AND REPLACED STOP FITTING PER ESO 80174.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,721 hrs · 27,526 cycles

LONGERON IS CRACKED. REPAIRED PER AARD 53-30-00-2.

Part: STOP FITTING — CRACKED (DOOR) · airframe 53,721 hrs · 27,526 cycles

DOOR STOP FITTING CRACKED, FORWARD SIDE OF DOOR TOWARDS UPPER END. REMOVED AND REPLACED DOOR STOP FITTING PER ESO 80174.

Part: VALVE — DEFECTIVE (AC PACK) · airframe 52,695 hrs · 26,973 cycles

EWR - CREW REPORTED STRONG BURNING SMELL THROUGHOUT CABIN. EMERGENCY DECLARED, RETURNED EWR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED MCM CARD 21-96-01 CABON ODOR TROUBLESHOOTING. REPLACED LEFT PILOT VALVE AND LEFT PACK PRESS REGULATING VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — INOPERATIVE (ZONE 100) · airframe 52,695 hrs · 26,973 cycles

CREW REPORTED STRONG BURNING ELECTRICAL ODOR. EMERGENCY DECLARED RETURNED EWR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT PACK PILOT VALVE AND LEFT PACK PRESS REGULATING VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 24D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 18D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 10D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 23D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY SEAT MOUNTED LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 15D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISINSTALLED (CABIN)

DFW - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 28DEF AND 29DEF OUT OF CONFIGURATION. CORRECTED CONFIGURATION FOR EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 28DEF AND 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT FORWARD GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: OIL SYSTEM — LOW PRESSURE (LEFT ENGINE)

ORD INFLIGHT - LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY OIL QUANTITY DEGRADING. CREW SHUTDOWN ENGINE. NO HIGH OIL TEMPERATURES OR ENGINE GAS TEMPERATURES OBSERVED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 20 MINUTES. REPLACED NUMBER ONE ENGINE ON 11 MARCH 2007 AT ORD DUE TO OIL PRESSURE OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - EMERGENCY LIGHTS AT AFT CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT CABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACCOUSTIC LINER — DAMAGED (THRUST REVERSER)

BNA - FOUND HOLE IN LEFT THRUST REVERSER ACCOUSTIC LINING 1.5 INCHES LONG BY .5 INCHES WIDE BY .5 INCH DEEP AT 1.00 POSITION 7.5 INCHES IN FROM TRAILING EDGE LOOKING UP AT TAIL PIPE. AIRCRAFT FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM BNA TO DFW FOR FURTHER EVALUATION OF DAMAGE.

Part: SLIDE — FAILED (GALLEY DOOR)

DFW - MAINTENANCE ARRIVED AT AIRCRAFT AND FOUND FORWARD GALLEY SERVICE DOOR SLIDE PACK HANGING OUTSIDE THE AIRCRAFT WITH THE GIRT BAR STILL HOOKED. THE SLIDE CAME OUT OF THE SLIDE PACK BUT DID NOT DEPLOY. REPLACED SLIDE FOR THE FORWARD GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — FAILED (CABIN PRESSURE)

TPA T1709/30 AIRCRAFT WOULD NOT PRESSURIZE. REPLACED CABIN PRESSURE OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO LOWER DOOR JAMB BEAM HAS HEAVY CORROSION. REMOVED AND REPLACED AFT CARGO DOOR BEAM PER SRM 51-01-00. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND SIDEWALL WEB CRACKED STATION 207 LONGERON 15L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-11. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1174. INSTALLED NEW SEAT TRACK STATION 1174 TO 1309 PER SRM 51-01. (M)

Part: BATTERY PACK — DISCHARGED (TAILCONE)

ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS FOR TAILCONE DROP HANDLE INOPERATIVE. REPLACED BATTERY PACK FOR TAILCONE DROP HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — SHORTED (SERVICE DOOR)

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

Part: CONNECTOR — DISCONNECTED (AFT AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIR STAIRS INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — INCORRECT (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH SEAT LIGHTS DIM. ONE WIRE HARNESS OF DUAL BATTERY POWERED SYSTEM NOT CONNECTED DUE TO INCORRECT HARNESS LENGTH. SPLICED ADDITINOAL WIRE INTO HARNESS BETWEEN SEATS 19 AND 20. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDE WALL MARKER LIGHT CONNECTORS ON AFT STAIRWAY BURNED. REPLACED CONNECTORS TO EMERGENCY EXIT SIDE WALL MARKER LIGHTS ON AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER — DIRTY (ACM BAY)

BFL - FLT 1768 - EN ROUTE BFL-DFW, AFTER TAKEOFF FLIGHT, ATTENDANTS REPORTED FUMES AND SMOKE IN AFT CABIN. SMELLED LIKE POSSIBLE BURNING OIL/HYDRAULIC FLUID. DECLARED AN EMERGENCY, RETURNED BFL, AND LANDED WITHOUT INCIDENT. AIRCRAFT HAS BEEN INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM BFL TO LAX FOR FURTHER EVALUATION OF AIR CONDITIONING SYSTEM. AT LAX, PERFORMED PAC BURNOUT PER MM. NO SMOKE OR FUMES NOTICED. GROUND CHECKED NORMAL OPERATION. (M)

Part: TURBINE BLADE — FAILED (LT ENGINE)

DFW - FLT 050 - DURING APPROACH TO DFW, LEFT ENGINE BEGAN VIBRATION WITH NO ABNORMAL COCKPIT INDICATIONS. REDUCED POWER TO LT ENGINE AND VIBRATION DIMINISHED. EMERGENCY DECLARED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED NR 1 ENGINE DUE TO TURBINE BLADE FAILURE. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (X)