N591AA

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,636 hrs · 28,370 cycles

CRACK IN SKIN ABOVE RIGHT AFT NOSE LANDING GEAR DOOR HINGE. INSTALLED REPAIR DOUBLER PER SRM 53-05-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,636 hrs · 28,370 cycles

STATION 1510 CANT FRAME CRACKED AT LOWER LEFT TAIL CONE ALIGNMENT PIN. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-00 AND SRM 53-14-04.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,412 hrs · 28,252 cycles

OVERHEAD EMERGENCY LIGHTS AT ROWS 18, 20 AND 21 INOPERATIVE. REPLACED BATTERY PACK AT 20D. OPS CHECK NORMAL.

Part: OVEN — INOPERATIVE (GALLEY) · airframe 64,596 hrs · 27,791 cycles

TPA - FLIGHT ATTENDANTS REPORTED AN ELECTRICAL SMELL THROUGHOUT THE CABIN. EMERGENCY DECLARED FLIGHT RETURNED TPA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FIRST CLASS OVEN SMOKING. REPLACED FIRST CLASS GALLEY OVEN. REPLACED BOTH PACK COALESCER BAGS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,814 hrs · 26,396 cycles

AFT ACCESSORY 1418 FRAME CRACKED AT LONGERON 2 RIGHT. DOUBLER INSTALLED PER SRM 53-03-00.

Part: SLIDE — OUT OF POSITION (CABIN DOOR) · airframe 59,660 hrs · 25,353 cycles

AFTER LANDING WHEN FORWARD CABIN DOOR WAS OPEN EVACUATION SLIDE FELL OUT OF PACK BUT WAS NOT DEPLOYED. VERIFIED SLIDE WAS OK AND RE-INSTALLED.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 58,414 hrs · 24,761 cycles

GIRT BAR WAS NOT POSITIONED CORRECTLY RESULTING IN RIGHT NUMBER 1 DOOR SLIDE INADVERTANTLY DEPLOYING UNSUCCESSFULY WHEN DOOR OPENED FOR CATERING. REPLACED RIGHT NUMBER 1 DOOR SLIDE. OPS CHECK NORMAL.

Part: PAN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

FORWARD CARGO ALONG DOOR CUTOUT LOWER BEAM AT STATION 380 TO 420 CORRODED. REPAIRED FORWARD CARGO LOWER DOOR JAMB BEAM/PAN FROM STATION 370 TO 427 PER SRM 53-05-00 FIG 44.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

CORROSION ALONG TIE DOWN TRACK AT STATION 1220. INSTALLED NEW TIE DOWN TRACK AT STATION 1220 UNDER SRM 51-30-05.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

OUTBOARD GALLEY MOUNT FITTING AT STATION 160 CORRODED IN BORE. INSTALLED G1 GALLEY OUTBOARD MOUNT FITTING UNDER SRM 51-01 AND SRM 51-30.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

AT STATION 160, APPROXIMATELY 14 INCHES INBOARD OF OUTBOARD GALLEY MOUNT, CENTER MOUNT CORRODED IN BORE. INSTALLED G-1 GALLEY CENTER MOUNT FITTING UNDER SRM 51-01 AND SRM 51-30.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

G2 GALLEY AFT INBOARD FLOOR SUPPORT HAS CORROSION AT STATION 218. INSTALLED G2 GALLEY AFT INBOARD MOUNT FITTING PER SRM 51-01 AND SRM 51-30.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

CORROSION ON SUBFLOOR/MEMBRANE UNDER G2 GALLEY AFT INBOARD MOUNT AT STATION 217. FABRICATED AND INSTALLED SUBFLOOR DOUBLER UNDER G2 GALLEY AFT INBOARD TIE DOWN FITTING AT STATION 217, ACCOMPLISHED PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LARGE DENT IN SKIN FORWARD OF TAIL CONE RIGHT SIDE AT 3 O`CLOCK. DYE CHECKED DENT, NO CRACKS FOUND. INSTALLED DOUBLER PER AARD 53-30-00-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

CORROSION ON NUMBER 2 SEAT TRACK AT STATION 1240 LEFT BEYOND LIMITS. REPAIRED PER SRM 51-30-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

AFT CARGO CORROSION ON BOTTOM OF LEFT CUSP AT STATION 1300 INBOARD OF CUSP T-ANGLE. INSTALLED SERVICEABLE CUSP SHEET.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

RIGHT CUSP AT STATION 218 CORRODED AT ATTACH HOLES. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

CORROSION ON WEB UNDER RIGHT AFT TIE DOWN TRACK NUT PLATES. CORROSION WAS REMOVED BY CUTTING OUT DAMAGED SECTION. NEW SECTION OF WEB WAS SPLICED IN PER AARD 53-10-00-24.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

CORROSION ON NUMBER 2 SEAT TRACK AT STATION 1240 LEFT. INSTALLED NEW NUMBER 2 SEAT TRACK AT STATION 1220-1309.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

CORROSION AT MID CARGO THRESHOLD BEAM FROM STATION 636 TO 693. REPAIRED PER AARD 53-10-00-3 FIGURE 1.

Part: PAN — CRACKED (CARGO DOOR) · airframe 57,973 hrs · 24,566 cycles

FORWARD CARGO DOOR PAN CRACKED AT TOP AFT CORNER. STOPPED DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER UNDER ENGINEERING AUTHORIZATION COMPONENT 52 008494.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LEFT CUSP CRACKED AT STATION 807. INSTALLED NEW CUSP SHEET PER SRM 51-30.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

CORROSION ON AFT SIDE OF FRAME AT STATION 1271 BETWEEN LONGERON 29 RIGHT AND 30 RIGHT. REMOVED CORROSION AND PERFORMED REPAIR ON FRAME FROM LONGERON 28 RIGHT TO LONGERON 29 LEFT PER AARD 53-10-00-14 AND INSTALLED FASTENERS PER SRM 51-10-3, SRM 51-30-5.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

TAIL VERTICAL STABILIZER SKATE ANGLE IS CRACKED AT FASTENER RIGHT SIDE STATION 1463. INSTALLED PREVENTIVE DOUBLER AND FILLER PER AARD 53-10-00-2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

STATION 37 BULKHEAD FORWARD SIDE HAS A CRACK AT LOWER LEFT RADOME GUIDE PIN ATTACH RIVET. INSTALLED REPAIR DOUBLER, FILLER, AND SHIM IAW AARD 53-10-00-19.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

STATION 1418 FRAME CRACKED AT LONGERON 2 LEFT. INSTALLED DOUBLER PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

LEFT CUSP CORROSION OUT OF LIMITS. REMOVED CORRODED AREA. INSTALLED DOUBLER REPAIR TO CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CUSP MEMBRANE CRACKED BETWEEN STATION 222 AND 226 LEFT. REPLACED CUSP BETWEEN STATION 218 AND 237 PER AARD 53-20-00-16.

Part: FAIRING — CRACKED (ELEVATOR TAB) · airframe 57,973 hrs · 24,566 cycles

SMALL CRACK ON ELEVATOR TAB FAIRING 99 INCHES FROM INBOARD EDGE. INSTALLED DOUBLER ON ELEVATOR TAB PUSHROD FAIRING 2ND FROM INBOARD PER SRM 51-70-06.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

RIGHT CUSP FOUND CRACKED FROM STATION 803 TO 807. CUSP ALSO CRACKED AT AFT END OF LIGHTENING HOLE APPROXIMATELY .5 INCH. REPLACED CUSP SHEET FROM STATION 788 TO 807 PER AARD 53-20-00-16.

Part: KEELBEAM — DAMAGED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

FASTENER HOLE FOUND DAMAGED IN RIGHT KEEL BEAM ABOVE WHALE BONE. INSTALLED DOUBLER REPAIR PER SRM 53-01-00.

Part: SKIN — DENTED (ELEVATOR) · airframe 57,973 hrs · 24,566 cycles

DENT ON TOP OF LEFT ELEVATOR FROM HAIL. DEPTHS OF .085 INCH. DYE CHECKED AND NO CRACKS FOUND. REF SRM 51-50-02 P. 4B. INSTALLED REPAIR DOUBLER UNDER SRM 51-70-06 FIG 2. INSTALLED REPAIR DOUBLER REF SRM 51-70-06 FIG 2. INSTALLED BLIND FASTENERS UNDER ESO 80080.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 57,973 hrs · 24,566 cycles

MID CARGO DOOR "T" EXTRUSION UNDER FORWARD LOWER STEEL STOP STRAP CORRODED. REMOVED CORRODED "T" EXTRUSION AND INSTALLED NEW "T" EXTRUSION PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CRACK IN RIGHT SIDE WINDOW PAN FORWARD UPPER CORNER BETWEEN STATION 946 AND 965. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LEFT WINDOW PAN CRACKED AT LOWER FORWARD CORNER STATION 984. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CRACK IN RIGHT CUSP AT STATION 237 TO STATION 256. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

AFT CABIN ENTRY DOOR JAMB LEFT CENTER STOP PAD CRACKED. REMOVED AND REPLACED STOP PAD PER SRM 51-01.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CABIN AFT ENTRY DOOR JAMB, BOTTOM RIGHT STOP PAD FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER SRM 51-01.

Part: SKIN — DENTED (ELEVATOR) · airframe 57,973 hrs · 24,566 cycles

DENT ON TOP OF ELEVATOR FROM HAIL DEPTHS OF .085. TRIMMED OUT DENT AND FABRICATED DOUBLER PER SRM 51-70 06.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 57,973 hrs · 24,566 cycles

RIGHT ELEVATOR DENT. INSTALLED EXTERNAL DOUBLER PER SRM 51-70-06 PAGE 8.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CRACK IN RIGHT SIDE WINDOW PAN LOWER FORWARD CORNER BETWEEN STATION 1079 AND 1098. INSTALLED INTERNAL DOUBLER ON LOWER FORWARD CORNER OF WINDOW PAN PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LEFT WINDOW PAN CRACKED LOWER AFT CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CRACK IN RIGHT WINDOW PAN UPPER FORWARD CORNER AT STATION 946. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

RIGHT WINDOW PAN CRACKED UPPER AFT CORNER STATION 1136. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CRACK IN RIGHT SIDE WINDOW PAN UPPER AFT CORNER BETWEEN STATION 1136 AND 1155. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

RIGHT WINDOW PAN CRACKED AT UPPER AFT CORNER STATION 1041. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CRACK IN RIGHT WINDOW PAN UPPER FORWARD CORNER AT STATION 886. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LEFT WINDOW PAN CRACKED AT UPPER AFT CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LEFT WINDOW PAN CRACKED UPPER AFT CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LEFT WINDOW PAN CRACKED AT UPPER AFT CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

LEFT WINDOW PAN CRACKED UPPER FORWARD CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

WINDOW PAN CRACKED LOWER AFT CORNER AT STATION 908. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

TRIMMED OUT CRACK DAMAGE TO LEFT WINDOW PAN AT STATION 845 AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (LT WINDOW) · airframe 57,973 hrs · 24,566 cycles

LEFT WINDOW PAN CRACKED AT LOWER FORWARD CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,973 hrs · 24,566 cycles

CRACK IN WINDOW PAN UPPER AFT CORNER AT STATION 1193. REPAIRED PER AARD 53-10-00-25.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,032 hrs

SEA - EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK B5 28 FOR EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TAILPIPE — DEBONDED (LT ENGINE)

STL INFLIGHT T531/13NOV - NUMBER ONE ENGINE HAD MULTIPLE COMPRESSOR STALLS DURING CLIMB. RETURNED TO STL AND LANDED WITHOUT INCIDENT. DISCOVERED DISBONDED LINING IN TAIL PIPE. REPLACED NUMBER ONE ENGINE ON 14 NOV 2007 AT STL. REPLACED LEFT ENGINE ISOLATORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT SEATS 26D AND 29D INOPERATIVE. REPAIRED WIRING AT SEAT 26D FOR EMERGENCY LIGHTS AT SEATS 26D AND 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — DAMAGED (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT SEAT 26D NEEDS NEW LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT SEAT 26D NEEDS NEW SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

LGA - EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: RESERVOIR — EMPTY (APU OIL SYSTEM)

BUR - SMOKE IN CABIN AFTER LANDING AND THE APU AIR SWITCH WAS SELECTED ON. UPON REACHING THE GATE, THE APU WAS TURNED OFF AND SMOKE DISSIPATED RAPIDLY AFTER DOORS OPEN. REPLACED COALESCER BAGS FOR LEFT AND RIGHT AND PACKS. FOUND APU OIL RESERVOIR EMPTY AND LOWER FUSELAGE WET WITH OIL. CLEANED FUSELAGE AND SERVICED APU. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — STALLED (RT ENGINE)

RIGHT ENGINE HAD COMPRESSOR STALLS UPON TAKEOFF AT MAXIMUM POWER. STALLS CLEARED AT OR NEAR IDLE THRUST. REPLACED RIGHT ENGINE ON 07 JUL 2006. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - EMERGENCY LIGHTS AT RIGHT HAND FORWARD LOWER OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK IN CENTER AFT FOR EMERGENCY LIGHTS AT RIGHT HAND FORWARD LOWER OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 27 ARE INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ANTI-SKID SYS — INOPERATIVE (MLG)

DFW - DURING APPROACH TO DFW, LOWERED LANDING GEAR AND ALL FOUR ANTI SKID LIGHTS ILLUMINTATED ON OVERHEAD PANEL. CYCLED ANTI SKID SWITCH AND TWO LIGHTS WENT OUT. PERFORMED GO AROUND AND CYCLED GEAR, NO CHANGE. ON SECOND APPROACH ALL FOUR LIGHTS ILLUMINATED AGAIN. PULLED AND RESET CIRCUIT BREAKER AND ALL LIGHTS WENT OUT. LANDING AND ROLL OUT NORMAL. REPLACED ANTI SKID CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN)

ORD) OVERWING LOWER SIDE WALL EMERGENCY LIGHT AT ROW 2 INOPERATIVE. RESEATED BATTERY PACK FOR OVERWING LOWER SIDE WALL EMERGENCY LIGHT AT ROW 2. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - DURING OVERNIGHT MAINTENANCE, FOUND CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 18-20 INOPERATIVE. REPLACED BATTERY PACK AT B5-103. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

ORD - FLT 1251 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AFT OF ROW 22 RIGHT SIDE INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT LEFT OVERWING SIDE MARKER LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY EXIT LIGHTS AFT OF ROW 22 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT LEFT OVERWATER SIDE MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: GEARBOX — DAMAGED (NR 2 ENGINE)

MEM - FLT 814 - DFW-PHL, EN ROUTE AIRCRAFT LOST OIL PRESSURE IN NR 2 ENGINE. AIRCRAFT LANDED MEM WITHOUT INCIDENT. MAINTENANCE DISCOVERED PORT LP5 GEARBOX THREADS STRIPPED. AIRCRAFT BEING FERRIED TO TUL FOR ENGINE CHANGE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CONTACTOR — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 24 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 26 INOPERATIVE. CLEANED OVERHEAD EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 23 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

SAT - DURING OVERNIGHT MAINTENANCE, ALL SEAT PATH AND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BRACKET — CORRODED (GIRT BAR)

TUL - AFT GALLEY SERVICE DOOR AREA CUSP UPPER SURFACE UNDER GIRT BAR ATTACH BRACKET INBOARD AND OUTBOARD HOLES IN CUSP HAS CORROSION AROUND THEM. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND STATION 1175 LOWER SIDE OF CUSP CORRODED, LEFT SIDE OF CABIN. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP SHEET RIGHT SIDE, STATION 712 TO 719. INSTALLED NEW FABRICATED DOUBLER PER AARD 53-00-00-02. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND SKIN GOUGED AT STATION 312 BETWEEN L21 AND L22 RIGHT SIDE. CUT 1 INCH HOLE TO REMOVE DAMAGE. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED. REPLACED SHEAR TIE PER SRM 51-01. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - FOUND TWO SCRATCHES TWO FEET AFT OF FORWARD ENTRY DOOR ABOVE BLUE STRIPE. BLENDED, TREATED AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - FOUND SCRATCHES IN SKIN AND DENT LEFT STATION 219 AT L10L. BLENDED, TREATED AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND FORWARD LOWER FORWARD CORNER OF WINDOW FRAME CRACKED ON RIGHT SIDE OF AC AT STATION 985. INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 6 STATION 218 TO 222. REPLACED SEAT TRACK STATION 218-304 PER SRM 53-05-00. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN SKIN AND SKIN SCUFFED LEFT STATION 427 AT L20L. REWORKED SKIN AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LIGHT CORROSION RIGHT CUSP PREVIOUSLY REPAIRED. INSTALLED NEW CUSP SHEET FROM STATION 598-712 RIGHT. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND HEAVY CORROSION RIGHT CUSP PREVIOUSLY REPAIRED. INSTALLED NEW CUSP SHEET FROM STATION 598-712 RIGHT. (M)

Part: SEAT TRACK — CORRODED (FUSLEAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1233-1235. ROUTED OUT CORROSION BY ROUTER, TREATED AND PRIMED, INSTALLED PLUG REPAIR. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1205-1210. ROUTED OUT CORRODED AREA, TREATED AND PRIMED. INSTALLED PLUG REPAIR. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT CABIN SECTION DIM. REPLACED EMERGENCY EXIT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 22 THROUGH 28 INOPERATIVE. REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TURBINE BLADES — FAILED (LT ENGINE)

ORD - FLT 1477 - LEFT ENGINE FAILURE IN FLIGHT SHORTLY AFTER TAKEOFF N1 ROTATED AT 14 PERCENT N2 AT 15 PERCENT OIL QUANTITY DIMINISHED TO ZERO AND OIL PRESSURE TO 2 PSI. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED LEFT ENGINE, PERFORMED LEAK CHECK. INVESTIGATION REVEALED TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DETECTOR — DEFECTIVE (NR 2 ENGINE)

DFW - FLT 395 - EN ROUTE DFW-YVR - ON CLIMB-OUT, RIGHT SIDE FIRE WARNING LIGHT, BELL, AND AURAL CAME ON. ACCOMPLISHED ENGINE SHUTDOWN PROCEDURES. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FIRE LOOP ASSEMBLY AND CONNECTOR. ACCOMPLISHED FUNCTIONAL CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK TO EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK TO OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LANDING GEAR — DISCHARGED (NLG)

LAX - FLT 1056 - EN ROUTE LAX-ORD, NOSE LANDING GEAR WOULD NOT RETRACT. AIR INTERRUPTED, RETURNED LAX AND LANDED WITHOUT FURTHER INCIDENT. SERVICED NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (FUSELAGE)

DFW - FLT 433 - EN ROUTE DFW-MEX AT 7000 FEET, FLIGHT ATTENDANT NOTIFIED COCKPIT OF SMOKE IN CABIN. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU AND ACCOMPLISHED PACK BURNOUT PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — FAILED (A/C BAY)

STL - FLT 825 - EN ROUTE STL-LAX - IMMEDIATELY AFTER TAKEOFF CABIN FILLED WITH SMOKE. FLIGHT ATTENDANTS REPORTED AN ELECTRICAL SMELL. RETURNED STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE RECIRCULATION FAN. ACCOMPLISHED PACK BURNOUT PER MM. NO SMELL OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, AIRSTAIRS LEFT SIDE PANEL EMERGENCY LIGHT NOPERATIVE. REPLACED AIRSTAIRS LEFT SIDE PANEL EMERGENCY LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONDUCTOR — DEFECTIVE (CABIN FLOOR)

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