N498AA

Part: DUCT — LOOSE (AC BAY) · airframe 60,223 hrs · 30,910 cycles

DFW - CREW REPORTED ON CLIMBOUT TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RE-INSTALLED LEFT PACK HI PRESS BLEED FLEX DUCT THAT WAS LOOSE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FUEL CONTROL — INOPERATIVE (NR 2 ENGINE) · airframe 59,665 hrs · 30,614 cycles

LIT - INFLIGHT LGA-DFW. CREW REPORTED NUMBER 2 ENGINE N1, N2 AND EPR HAD ROLLED BCAK. EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. REPLACED ENGINE FUEL CONTROL AND FUEL PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,732 hrs

LGA - CEILING EMERGENCY LIGHTS FROM ROWS 26 TO 29 INOPERATIVE. REPLACED BATTERY PACK AT AFT CABIN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,732 hrs

LGA - AFT LAVATORY DROP DOWN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT AFT LAVATORY.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,676 hrs · 29,579 cycles

LT CUSP CORRODED BENEATH FWD GIRT BAR FITTING AT AFT SERVICE DOOR. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,160 hrs

LGA - EMERGENCY LIGHT AT SEAT 7F INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 7F.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 57,047 hrs · 29,235 cycles

STL - DURING DESCENT CREW REPORTED SMOKE SMELL IN CABIN. EMERGENCY DECLARED, LANDED STL WITHOUT INCIDENT. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CABIN SUBFLOOR CORROSION, 8 INCH BY 16 INCH, INSTALLED NEW SUBFLOOR DOUBLER PER 53-20-00-16.

Part: STRUCTURE — CRACKED (ZONE 100)

CABIN SUBFLOOR CRACKED, 1/2 INCH IN LENGTH. INSTALLED NEW CUSP SECTION PER 51-30-02 AND 51-30-5, 8 INCH BY 16 INCH.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CABIN SUBFLOOR CORRODED, STATION 160-200 RIGHT. REMOVED AND REPLACED SUBFLOOR PER AARD 53-20-00-16.

Part: PAN — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CORROSION ON BOTTOM SIDE OF G1 GALLEY DRAIN PAN STATION 148-160 RIGHT SIDE OF CABIN. REMOVED CORROSION INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CORROSION ON RIGHT CUSP AT STATION 160-168. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CORRODED (ZONE 200) · airframe 55,971 hrs · 28,646 cycles

FWD CARGO DOOR PAN CORRODED, STATION 370-427. INSTALLED NEW DOOR PAN SECTION FROM STATION 370 TO 427 PER SRM 53-05-00 FIG 44 SHEET 14.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

RIGHT CUSP VERTICAL ANGLE CORRODED AT STATION 200. INSTALLED NEW VERTICAL ANGLE.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO, CORROSION ON OUTBOARD LEG AND CLIPNUT HOLES OF RIGHT TIE DOWN TRACK AT STATION 1211-1309. REMOVED AND REPLACED TIE DOWN TRACK PER SRM 51-30-1.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO SPLICE PLATE CORRODED ON LEFT TIE DOWN TRACK AT STATION 1213. INSTALLED NEW SPLICE PLATE PER AARD 51-00-012.

Part: FRAME — CRACKED (ZONE 200) · airframe 55,971 hrs · 28,646 cycles

CRACK AT LEFT OVERWING FRAME RADIUS STATION 905. REMOVED AND REPLACED FRAME PER BOEING SERVICE REWORK DRAWING SRO9530282-7013.

Part: CUSP WEB — CUT (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CUT IN LEFT CUSP SHEET AT STATION 895 TO 905. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

MID CARGO DOOR BEAM CORRODED AT STATION 636-693. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: WEB — CORRODED (CARGO DOOR) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO, CORROSION ON DOOR WEB AT STATION 1155-1174. INSTALLED WEB REPAIR PER AARD 53-10-00-24.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CUSP HAS CORROSION AT STATION 664. INSTALLED DOUBLER PER SRM 53-20-00-16.

Part: LONGERON — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO, CORROSION ON LONGERON 23L AT STATION 1287. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-10-1.

Part: BRACKET — CORRODED (CARGO DOOR) · airframe 55,971 hrs · 28,646 cycles

CORROSION ON BRACKET ON AFT CARGO DOOR, LOWER AFT CORNER AT STATION 1212. INSTALLED NEW BRACKET PER SRM 51-10-01.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO AREA, CORROSION AFT LOWER ANGLE STATION 1211 AT LONGERON 30R TO 29R. INSTALLED SERVICEABLE SHEAR TIE AT STATION 1211 PER SRM 51-10-1.

Part: BRACKET — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO AREA, TEE BRACKET CORRODED STATION 1155 LOWER FORWARD CORNER OF DOOR OPENING. REMOVED AND REPLACED TEE BRACKET AT STATION 1155 PER SRM 51-10-1.

Part: BRACKET — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO DOOR LOWER FORWARD CORNER CORROSION ON BRACKET AT STATION 1155. INSTALLED NEW BRACKET PER SRM 51-10-01.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

LEFT CUSP HAS CORROSION AT STATION 505 TO 509. REMOVED CORROSION, INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO DOOR BEAM CORRODED AT STATION 1155-1211. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO COMPARTMENT, INTERCOSTAL BETWEEN FLOORBEAMS AT STATION 1287-1309 UPPER LEG HAS CORROSION AFT END IS CRACKED. INSTALLED NEW INTERCOSTAL PER AARD 51-00-012 AT STATION 1287.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CORROSION ON RIGHT HAND CUSP AT STATION 1179-1189. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

AFT CARGO FLOORBOARD SUPPORT CORRODED STATION 1212 AT LONGERON 28L TO 29L. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-10-1.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CORROSION UNDER LEFT CUSP AT STATION 489. REMOVED CORROSION. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

RIGHT HAND CUSP CORRODED AT STATION 1155-1174 IN PASSENGER CABIN. REMOVED CORROSION PER SRM 51-10-3, INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CORROSION ON CUSP AT STATION 1136 TO 1174. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

LEFT CUSP CORRODED AT STATION 1155 TO 1174. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 55,971 hrs · 28,646 cycles

"J" ANGLE DOUBLER CRACKED. INSTALLED NEW J ANGLE DOUBLER.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,971 hrs · 28,646 cycles

FLOOR BOARD SUPPORT CRACKED AT LOWER FWD SIDE BELOW SEAT TRACK NR 5. INSTALLED NEW SUPPORT.

Part: ANGLE — CRACKED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

LEFT NOSE LANDING GEAR DOOR JAM BEAM J ANGLE DOUBLER CRACKED AT STA 47. INSTALLED NEW J ANGLE DOUBLER.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CORROSION ON DOUBLER LEFT CUSP AT STATION 664-668. INSTALLED NEW CUSP DOUBLER PER AARD 53-20-00-16.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

SUBFLOOR CRACKED OUTBOARD SIDE OF NUMBER 2 SEAT TRACK AT STATION 218. INSTALLED DOUBLER PER SRM 53-20-00-16.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CRACK AT FORWARD LOWER END OF FLOORBEAM SUPPORT, STATION 927 BELOW NR 2 SEAT TRACK. REPLACED FLOORBEAM SUPPORT PER SRM 51-01

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

FORWARD LOWER TANG CRACKED ON LT WINDOW PAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (ZONE 100) · airframe 55,971 hrs · 28,646 cycles

CRACK AT BELT BOTTOM CORNER ON WINDOW FRAME STATION 1098 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,971 hrs · 28,646 cycles

CORROSION ON RIGHT HAND CUSP STATION 1179 TO 1189. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: WIRE — BROKEN (TAILCONE)

DFW - EMERGENCY LIGHT AT OVERHEAD TAIL CONE HAS BROKEN TWIST LOCK TERMINAL WIRE L795ZD14. REPLACED TWIST LOCK TERMINAL WIRE AT OVERHEAD TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — DAMAGED (COCKPIT DOOR) · airframe 55,383 hrs

LGA EMERGENCY PLACARD AT COCKPIT DOOR UNREADABLE. REPLACED EMERGENCY PLACARD AT COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,383 hrs

LGA EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 23 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 25 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EXTERNAL EMERGENCY LIGHT AT RIGHT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT RIGHT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SCREW — MISSING (EMERGENCY LIGHTS)

DFW - EXTERNAL EMERGENCY EXIT LIGHT AT RIGHT HAS TWO SCREWS MISSING. REPLACED SCREWS FOR EXTERNAL EMERGENCY EXIT LIGHT AT RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — STALLED (RT ENGINE)

ORD - HEARD LOUD BANG AND RIGHT ENGINE EXHAUST GAS TEMPERATURE INCREASED TO 800C. CREW SHUT DOWN ENGINE. SINGLE ENGINE TIME TEN MINUTES. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 09 NOVEMBER AT ORD DUE TO COMPRESSOR STALLS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DIRTY (CABIN)

SFO - TWO EMERGENCY LIGHTS IN AFT CABIN OVERHEAD JUST FORWARD OF AFT AIRSTAIR DOOR INOPERATIVE. CLEANED BATTERY FOR INOPERATIVE EMERGENCY LIGHT IN AFT CABIN OVERHEAD FORWARD OF AFT AIRSTAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - OVERHEAD EMERGENCY LIGHT FROM ROW 28 TO FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT FORM ROW 28 TO FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — DAMAGED (NR 2)

MCI - INFLIGHT CLIMBING THROUGH FL20, FLIGHT CREW HEARD A BANG AND SAW NR 2 ENGINE EXHAUST GAS TEMPERATURE DOUBLED AND LOSS OF N1 AND N2. AIR RETURNED TO MCI AND LANDED WITHOUT INCIDENT. FOUND SEVERAL MISSING FAN BLADES. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — SHORTED (POWER PORT)

BNA - INFLIGHT ELECTRICAL SHORT IN POWER PORT SYSTEM AT SEAT 10B. LANDED BNA WITHOUT INCIDENT. REPLACED POWERPORT POWER SUPPLY SEAT TO SEAT CABLE BETWEEN SEAT ROW 10AB AND SEAT ROW 11AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO OVERHEAD EMERGENCY LIGHT FROM SEAT 28D AFT INOPERATIVE. REPLACED BATTERY PACK B5 27 AND B5 107 FOR OVERHEAD EMERGENCY LIGHT FORM SEAT 28D AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SFO EMERGENCY LIGHT ON SEAT 15D AND OVERHEAD EMERGENCY LIGHT I VENTRAL STAIRWELL INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT ON SEAT 15D AND OVERHEAD EMERGENCY LIGHT IN VENTRAL STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND MODULE AT FORWARD RIGHT OVERWING EXIT IDENTIFIER FOR OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

AUS - EMERGENCY LIGHT AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CABLE — BROKEN (MLG)

TUL - INFLIGHT T1215/14 COULD NOT RETRACT MAIN LANDING GEARS AFTER TAKEOFF. AIRCRAFT RETURNED TO TUL GATE. FOUND BROKEN ANTI RETRACTION CABLE SEGMENT 118A. INSTALLED AND ADJUSTED A SERVICEABLE CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT EXIT SIGN LOCATION. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. SECURED COCKPIT DOOR EMERGENCY EXIT LIGHT BATTERY WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT ABOVE FORWARD GALLEY SERVICE DOOR FLICKERS. REPLACED FORWARD GALLEY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANT EMERGENCY FLASH INOPERATIVE. REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

TUL - FOUND CRACK BS 1485R, UNDER RIGHT AIR STAIRS ACTUATOR APPROX 1 INCH LONG. INSTALLED SPLICE REPAIR PER ESO 80559 DATED 29 JAN 2001. (M)

Part: WEB — TORN (FUSELAGE)

TUL - FOUND CUSP TORN AROUND NUTPLATE AT 1307. FABRICATED AND INSTALLED FILLER PER ESO 80559 DATED 1/23/2001. (M)

Part: LONGERON — TOOL DAMAGE (FUSELAGE)

TUL - FOUND DEEP TOOLING MARKS IN LONGERON 11L TOP SIDE STATION 456 AND 461. INSTALLED DOUBLER PER SRM 53-02 AND SRM 51-10-1. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND INBOARD GALLEY TIE DOWN CORRODED STATION 218. REMOVED AND REPLACED GALLEY TIE DOWN PER SRM 53-01-00. (M)

Part: FLOORBOARD — CORRODED (CABIN)

TUL - FOUND 2 INCH BY 32 INCHES OF CORROSION ON FLOORBOARD SUPPORT AT STATION 200, RBL 10-42. REMOVED AND REPLACED FLOORBOARD SUPPORT PER MM 51-00-00-8. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND HOLE IN CUSP WEB UNDER SEAT TRACK NR 6 STATION 1086. INSTALLED DOUBLER AT STATION 1086 IN CUSP WEB PER AARD 25-00-00-02. (M)

Part: FLOORBOARD — CORRODED (CABIN)

TUL - FOUND 2 INCH BY 4 INCHES OF CORROSION ON TOP SKIN OF FLOORBOARD STATION 146 RBL 24 APPROX. REMOVED AND REPLACED FLOORBOARD PER MM 53-20-01-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 2 STATION 1201. INSTALLED NEW SECTION OF NR 2 SEAT TRACK FROM STATION 1164-1309 PER SRM 53-05 FIG 4F. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AROUND ANTENNA ATTACHMENT HOLE STATION 402, BELLY. CUT OUT CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 12B SHEET 2 AT STATION 402. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION 1 INCH BY 2 INCHES ON CUSP STATION 655-674 LEFT. INSTALLED DOUBLER FROM 661 TO 667 LEFT SIDE PER SRM 53-01 FIG 4-3. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND FORWARD GALLEY INBOARD TIEDOWN FITTING CORRODED 2 INCHES BY 8 INCHES, STATION 160. REMOVED AND REPLACED FORWARD INBOARD GALLEY TIE DOWN FITTING PER SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, STATION 946-965. CUT OUT AND BLENDED DAMAGED AREA. INSTALLED DOUBLER, STATION 956-962 PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CRACKED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK, BROKEN AND CRACKED AT STATION 313. INSTALLED 1 NEW SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, STATION 636-655, UPPER SURFACE. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, STATION 927-946. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER BETWEEN STATION 938-942 PER AARD 53-00-00-00. (M)

Part: STRAP — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN TIE STRAP AT STATION 200 FRAME TO LONGERON 11 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-11. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 6 HAS CORROSION AT STATION 274-275. INSTALLED NEW SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP LEFT STATION 450 AT LIGHTENING HOLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SERM 53-01-00. (M)

Part: SEAT TRACK — CORRODED (FUSLEAGE)

TUL - FOUND SEAT TRACK NR 6 HAS CORROSION AT STATION 597-580. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED AROUND FASTENER AT STATION 160. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02 FIG 18 AND 53-14-1 FIG 3. (M)

Part: ENGINE — VIBRATION (LT ENGINE)

DFW - FLT 1055 - AFTER TAKEOFF, LEFT ENGINE VIBRATING. VIBRATION GONE WHEN ENGINE PULLED BACK TO IDLE. LEFT ENGINE OIL TEMPERATURE 30 DEGREES HIGHER THAN RIGHT ENGINE OIL TEMPERATURE. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT ENGINE. GROUND CHECK NORMAL OPERATION. FOD DAMAGE TO TURBINE AND EXHAUST AREA ACOUSTICAL LINER. (M)

Part: WIRE — FAILED (CABIN)

ATL - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRING IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: MODULE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT R2 DOOR LOWER MARKER INOPERATIVE. REPLACED FORWARD MODULE AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN MID-CABIN WERE FOUND INOPERATIVE. RECONNECTED LOOSE EMERGENCY FLOOR PATH LIGHTING CONNECTOR AT MID-CABIN. SYSTEM GOUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 10 AND 12 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ARM ASSY — BROKEN (LT TE FLAP)

DCA - DURING OVERNIGHT CHECK, LEFT WING INBOARD FLAP ARM ASSEMBLY BROKEN. REPLACED LEFT WING INBOARD FLAP ARM ASSEMBLY. ALSO, REPLACED LEFT WING INBOARD FLAP DRIVE CYLINDER. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, FORWARD RIGHT DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY EXIT SIGN WIRE AT FORWARD RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)