N7514A

Part: LENS — BROKEN (CABIN) · airframe 75,510 hrs · 40,079 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT LENS IN AFT STAIRWAY BROKEN ON RIGHT LOWER PANEL. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-53-01. OPERATIONAL CHECK GOOD.

Part: BOLT — LOOSE (FILTER COVER) · airframe 74,276 hrs · 39,301 cycles

AIRCRAFT WAS GNDED. A STRONG FUEL SMELL REPORTED THROUGHOUT CABIN WHEN APU SUPPLYING AIR CONDITIONING. INSPECTED APU & FOUND FUEL FILTER COVER LOOSE & WET. R & R FILTER COVER BOLTS IAW AMM 49-30-02. OPERATIONAL & LEAK CHECKED NORMAL. ACCOMPLISHED CARD 21-96-01 WITH NO ODORS NOTED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,147 hrs · 39,223 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN AT CANT FRAME STATION 1474 IS CRACKED BETWEEN RIVETS BELOW LONGERON 19L. REPAIRED SKIN IAW SRM 53-01-00-001 & AARD 51-60-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,147 hrs · 39,223 cycles

AIRCRAFT WAS IN BASE MX. LONGERON 23L IS CRACKED AT FS 160 AT UPPER FLANGE FASTENER. REPAIRED LONGERON IAW SRM 53-02-00-001.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,992 hrs · 39,129 cycles

AIRCRAFT WAS GNDED. SEAT MOUNTED EMER LIGHTS ARE INOPERATIVE FROM ROW 21 AFT. R & R EMER LIGHT BATTERY PACK B5-105, BUT FOUND REPLACEMENT PACK TO BE BAD FROM STOCK. THIS SDR IS FOR ORIGINALLY DISCREPANT PACK. SEE RELATED SDR AALA20160321008 FOR BAD FROM STOCK UNIT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,992 hrs · 39,129 cycles

AIRCRAFT WAS GNDED. SEAT MOUNTED EMER LIGHTS ARE INOPERATIVE FROM ROW 21 AFT. R & R EMER LIGHT BATTERY PACK B5-105, BUT FOUND REPLACEMENT PACK TO BE BAD FROM STOCK. THIS SDR IS FOR THE BAD FROM STOCK UNIT. SEE RELATED SDR AALA 20160319001 FOR ORIGINALLY DISCREPANT UNIT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,179 hrs · 38,658 cycles

REFERENCE WORK CARD 0801. EMER LIGHTS IN COCKPIT & FWD GALLEY DO NOT TEST. REPLACED BATTERY PACK B5-23 IAW AMM 33-53-00. TESTED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,981 hrs · 37,965 cycles

AFT OVERWING EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK. LIGHTS OPERATIONALLY CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,981 hrs · 37,965 cycles

FORWARD EMER POWER LIGHTS DIM WHEN POWERED BY BATTERY AB5-1. R & R BATTERY IN BATTERY PACK AB5-1. FWD EMER POWER LIGHTS OPERATIONALLY CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,762 hrs · 37,258 cycles

CANT FRAME AT FS 1510 IS CRACKED AT FIRST TAIL CONE GUIDE PIN BELOW RT UPPER LATCH. REPAIRED FRAME IAW SRM 53-01-00-001.

Part: CHARGER — DEFECTIVE (MAIN BATTERY) · airframe 69,578 hrs · 36,574 cycles

BATTERY CHARGER LIGHT ILLUMINATED DURING CRUISE. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED MAIN SHIP BATTERIES, CHARGER, RELAY R2-56 MPN ZCDZLX021 & CHARGER CB B1-146. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,076 hrs · 35,753 cycles

FUSELAGE SKIN DAMAGE AT STATION 218 JUST ABOVE STRINGER 18 LT. INSTALLED EXTERNAL DOUBLER IAW SRM 53-04-02.

Part: CASTING — CRACKED (LT WING) · airframe 67,017 hrs · 35,126 cycles

CASTING CRACKED INBD OF NR 4 SLAT TRACK INBD UPPER SIDE ON LT WING. INSTALLED NEW CASTING IAW AARD 51-00-05-1.

Part: CASTING — CRACKED (LE SLAT) · airframe 67,017 hrs · 35,126 cycles

RT WING LE CASTING CRACKED INBD OF SLAT TRACK 4. INSTALLED A NEW INBD CASTING FOR NR 4 SLAT TRACK IAW AARD 51-00-05-1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 67,017 hrs · 35,126 cycles

FRAME DAMAGED & DENTED AT STATION 39 AT LONGERON 19 LT. INSTALLED DOUBLER IAW AARD 53-30-00-02 & INSTALLED NEW FRAME IAW AARD 51-00-05-1 & DRAWING 9911501.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,017 hrs · 35,126 cycles

FS AFT CRACK IN SKIN AT STATION 1380 ABOVE LONGERON 14 RT. INSTALLED FILLER & DOUBLER IAW SRM 53-04-00 FIGURE 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,017 hrs · 35,126 cycles

MULTIPLE SPOTS OF CORROSION IN SEAT TRACK NR 5 FROM STATIONS 200 TO 246. INSTALLED NEW NR 5 SEAT TRACK IAW SRM 53-05-00-FG 4F.

Part: CASTING — CRACKED (FUSELAGE) · airframe 67,017 hrs · 35,126 cycles

STATION 927 BELOW NR 2 SEAT TRACK, SUPPORT CASTING IS CRACKED. REPLACED CASTING IAW AARD 51-00-05-1.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,017 hrs · 35,126 cycles

LIGHTING HOLE FROM FS 434 - 440 LT HAND CUSP DAMAGED. INSTALLED DOUBLER ON CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,017 hrs · 35,126 cycles

ENLARGED HOLE IN CUSP AT STATION 237 RT SIDE JUST INBD OF FRAME FITTING. CUT OUT DAMAGE & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,017 hrs · 35,126 cycles

AFT FS CRACKED IN SKIN, FS 1309 ABOVE LONGERON 7 LEFT. INSTALLED DOUBLER IAW SRM 53-04-00 FIGURE 32.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,017 hrs · 35,126 cycles

CORROSION ON UNDER SIDE OF CUSP BELOW AFT GIRT BAR FITTING AT AFT SERVICE DOOR. INSTALLED DOUBLER IAW AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,017 hrs · 35,126 cycles

CORROSION ON GALLEY G-2 TIE DOWN FITTING AT STATION 218, AT INBD FLOOR MOUNT. INSTALLED SUB FLOOR DOUBLER & SERVICEABLE GALLEY FLOOR MOUNT IAW AARD 53-20-00-16.

Part: ACTUATOR — MALFUNCTIONED (NLG STEERING) · airframe 65,741 hrs · 34,416 cycles

DFW - CREW REPORTED SHARP TUG TO THE LEFT ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH NOSE TIRES AND LUBRICATED SALAD BOWL AND NOSE STEARING ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RELAY — DEFECTIVE (ELECTRICAL SYS) · airframe 62,326 hrs · 32,448 cycles

"DC BUSS OFF" ANNUNCIATOR LIGHT ILLUMINATED DURING CLIMB. ALL DC LOADS CHECKED NORMAL, ALL ASSOCIATED CBS WERE NORMAL. CLOSED, FOUND DC EMERGENCY POWER TRANSFER RELAY BAD. REPLACED RELAY AND CHECKED OK.

Part: RELAY — INOPERATIVE (ELECTRICAL SYS) · airframe 62,326 hrs · 32,448 cycles

DFW - CREW REPORTED "DC BUS OFF" ANNUNCIATOR ILLUMINATED DURING CLIMBOUT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DIRECT CURRENT EMERGENCY POWER TRANSFER RELAY R2-326. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,585 hrs · 30,890 cycles

AFT ACCY STATION 1510 RIGHT LOWER FRAME CRACKED AT ALIGNMENT PIN. INSTALLED NEW SECTION OF FRAME AND DOUBLER PER SRM 53-01 FIGURE 2.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 59,585 hrs · 30,890 cycles

AFT CARGO DOOR FORWARD EDGE CENTER STOP PAD FITTING CRACKED. REPLACED STOP PER SRM 52-33-00 AND BOEING PRINT NUMBER 5910141 AND INSTALLED STOP FITTING PER SRM 51-01-00.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 59,585 hrs · 30,890 cycles

FORWARD CARGO DOOR TOP FORWARD DOOR STOP PAD FITTING CRACKED. INSTALLED NEW DOOR STOP FITTING PER SRM 51-30-00.

Part: SHROUD — CRACKED (CABIN) · airframe 58,744 hrs · 30,427 cycles

EMERGENCY ESCAPE PATH LIGHT SHROUD AT 11D IS CRACKED. REPLACED SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 11D. OPS CHECKED NORMAL.

Part: PORTABLE LIGHT — DEFECTIVE (CABIN) · airframe 58,744 hrs · 30,427 cycles

THE FORWARD CABIN PORTABLE EMERGENCY LIGHT IS DIM. REPLACED THE FORWARD CABIN PORTABLE EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: SHROUD — CRACKED (CABIN) · airframe 58,744 hrs · 30,427 cycles

EMERGENCY ESCAPE PATH LIGHT SHROUD AT 29D IS CRACKED. REPLACED SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 29D. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,744 hrs · 30,427 cycles

THE FORWARD CABIN EMERGENCY ESCAPE PATH LIGHTS ARE DIM FROM THE FRONT TO THE OVERWING EMERGENCY EXIT HATCHES. REPLACED THE BATTERY PACK FOR THE CHARGING MODULE AB5-1. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,744 hrs · 30,427 cycles

THE FORWARD EMERGENCY ESCAPE PATH LIGHT AT SEAT 3E IS INOPERATIVE. REPLACED LAMP FOR FORWARD EMERGENCY ESCAPE PATH LIGHT AT SEAT 3E. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,744 hrs · 30,427 cycles

THE TAIL COMPARTMENT CEILING LIGHTS L2-637, 12-638, 12-639 AND TWO EACH IN L2-694 ARE INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY B5-28. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,744 hrs · 30,427 cycles

THE RIGHT AND LEFT AFT OVERWING EXIT LIGHTS AL2-5 AND AL2-6 ARE DIM. REPLACED THE BATTERY PACK FOR THE AB5-3 CHARGING MODULE. OPS CHECKED NORMAL.

Part: SHROUD — CRACKED (CABIN) · airframe 58,744 hrs · 30,427 cycles

SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 16D IS CRACKED. REPLACED SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 16D. OPS CHECKED NORMAL.

Part: SHROUD — CRACKED (CABIN) · airframe 58,744 hrs · 30,427 cycles

EMERGENCY ESCAPE PATH LIGHT SHROUD AT 30D IS CRACKED. REPLACED SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 30D. OPS CHECKED NORMAL.

Part: SHROUD — CRACKED (CABIN) · airframe 58,744 hrs · 30,427 cycles

EMERGENCY ESCAPE PATH LIGHT SHROUD AT 22D IS CRACKED. REPLACED SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 22D. OPS CHECKED NORMAL.

Part: SHROUD — CRACKED (CABIN) · airframe 58,744 hrs · 30,427 cycles

EMERGENCY ESCAPE PATH LIGHT SHROUD AT 23D IS CRACKED. REPLACED SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 23D. OPS CHECKED NORMAL.

Part: PLATE — MISSING (CABIN) · airframe 58,744 hrs · 30,427 cycles

THE BACKING PLATE FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 13D IS MISSING. INSTALLED A BACKING PLATE FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 13D. OPS CHECKED NORMAL.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 58,559 hrs · 30,334 cycles

EMERGENCY LIGHTING AT SEAT 12DEF INOPERATIVE. FOUND VOLTAGE TO SEAT HARNESS BUT NO VOLTAGE OUT TO SEAT LIGHT. UPON FURTHER INSPECTION DISCOVERED THAT PIN IN CONNECTOR CLOSEST TO SIDEWALL PUSHED BACK. RE-SECURED PIN IN CONNECTOR. OPS CHECKED NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 58,470 hrs · 30,283 cycles

DURING EMERGENCY LIGHT TEST FOUND AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS BARELY ILLUMINATED WHEN SELECTED ON. RE-SEATED BATTERY PACK IN AFT FUSELAGE AND EMERGENCY LIGHTS OPS CHECKS NORMAL DURING RETEST.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,659 hrs · 29,315 cycles

FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER AT POSITION B5-23. OPS CHECK NORMAL.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

AFT UPPER WINDOW PAN TAB CRACKED AT FASTENER, STATION 1079 LEFT SIDE. CUT OUT CRACK AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

STATION 1510 CANT FRAME CRACKED ABOVE LEFT UPPER TAIL CONE LATCH. INSTALLED REPAIR DOUBLER PER EA MD80-53-005820.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

HEAVY CORROSION ON SUB FLOOR DOUBLER JUST INBOARD OF FORWARD SERVICE DOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

LONGERON 1L CRACKED AT STATION 160. REPLACED LONGERON PER SRM 53-02-00 FIGURE 8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

LONGERON 1L CRACKED AT STATION 200. REPLACED LONGERON PER SRM 53-02-00 FIGURE 8.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

AFT PRESSURE BULKHEAD, 1 INCH CRACK AT TOP OF STIFFENER LOCATED ABOVE CENTER OF VAULT DOOR OPENING ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. INSTALLED NEW STIFFENER PER SRM 51-01-00.

Part: PAN — CRACKED (CARGO DOOR) · airframe 55,498 hrs · 28,679 cycles

CRACK ON UPPER FORWARD CORNER OF PAN ON FORWARD CARGO DOOR. INSTALLED REPAIR DOUBLER PER SRM 52-03-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

AFT CARGO DOOR CORROSION ALONG DOOR BEAM STATION 1158-1160 AND 1203-1206. INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3.

Part: ANGLE — BROKEN (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

ATTACH ANGLE INSIDE DOOR BEAM, AFT END BROKEN. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-10-00-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

SHEAR TIE CRACKED AT STATION 1451, LONGERON 2R. REPLACED SHEAR TIE PER SRM 51-30-00.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

CORROSION ON CORNER ANGLE BRACKET STATION 1155, LONGERON 25R-27R. REPLACED BRACKET PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

CORROSION ON CUSP IN THE LEFT TUNNEL STATION 554. INSTALLED CUSP DOUBLER FROM STATION 541-560 PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

LONGERON 2L CRACKED AFT OF STATION 1418. REMOVED DAMAGED SECTION AND INSTALLED LONGERON AND SPLICE PER AARD 53-30-00-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

LONGERON 2R CRACKED AFT OF STATION 1418. INSTALLED NEW LONGERON WITH REPAIR SPLICE PER AARD 53-30-00-2.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

RIGHT CUSP HAS A CRACK JUST AFT OF STATION 218. INSTALLED NEW CUSP SHEET STATION 218-237 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

RIGHT CUSP CORRODED FROM STATION 1174-1193. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

SEAT TRACK NR 5 CORRODED BEYOND LIMITS FROM STATION 200-206. INSTALLED NEW TRACK SECTION PER SRM 53-05-00 FIGURE 4.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 54,498 hrs · 28,679 cycles

CRACK IN RIGHT CUSP AT STATION 218 OUTBOARD OF NR 5 SEAT TRACK. INSTALLED CUSP SHEET PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,498 hrs · 28,679 cycles

CORROSION FOUND UNDER AFT GIRT BAR SUPPORT BRACKET AT STATION 1170. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

CORROSION ON CUSP UNDER FORWARD GIRT BAR BRACKET AT AFT SERVICE DOOR. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

FORWARD GIRT BAR BRACKET CORRODED AT AFT SERVICE DOOR. REMOVED AND REPLACED GIRT BAR BRACKET PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

RIGHT WINDOW PAN CRACKED AT STATION 946 LOWER CORNER. REMOVED CRACKED TAB AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

SEAT TRACK NR 2 CORRODED FROM STATION 216-220. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

FRAME CRACKED OUT AT STATION 905 ABOVE CENTER FUEL TANK AT THE CENTER FLOORBOARD. REMOVED AND REPLACED CRACKED FRAME PER SRM 51-01-00 PARAGRAPH 2D.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,498 hrs · 28,679 cycles

LEFT CUSP CRACKED BETWEEN STATION 218-237. REMOVED AND REPLACED CUSP SHEET PER SRM 51-01-00.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,498 hrs · 28,679 cycles

CORROSION ON GALLEY TIE DOWN FITTING AT STATION 208, 12 INCHES INBOARD OF NR 4 SEAT TRACK. REMOVED AND REPLACED FITTING PER SRM 51-01.

Part: BATTERY — LOOSE (EMERGENCY LIGHTS) · airframe 55,262 hrs

LGA - TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY FOR TAIL COMPARTMENT EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 55,262 hrs

LGA - SEVERAL CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 32 INOPERATIVE. REPLACED BATTERY PACK AT FORWARD GALLEY AND ROW 25.

Part: WIRE HARNESS — BROKEN (ANNUN PANEL) · airframe 54,431 hrs

DFW INFLIGHT. LANDING GEAR INDICATIONS INOPERATIVE DURING APPROACH. PERFORMED GO-AROUND TO CONFIRM LANDING GEAR DOWN AND LOCKED. LANDED DFW WITHOUT INCIDENT. FOUND BROKEN WIRE ON ANNUNCIATOR PANEL IN COCKPIT FOR LANDING GEAR INDICATION. REPAIRED WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 52,760 hrs

TPA - EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT SEAT AT AFT GALLEY DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT SEAT AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOSE — LEAKING (HYD SYSTEM)

RIC INFLIGHT 1180/01DEC - RIGHT LOW HYDRAULIC PRESSURE LIGHT ILLUMINATED. RIGHT HYDRAULIC QUANTITY AND PRESSURE ZERO. LANDED RIC WITHOUT INCIDENT. FOUND HYDRAULIC PRESSURE LINE ON RIGHT WHEEL LOOSE. TIGHTENED RIGHT HYDRAULIC PRESSURE LINE AND REPLACED HYDRAULIC PUMP AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROWS 19 TO 21 AND BETWEEN AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 19 TO 21 AND BETWEEN AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - EMERGENCY LIGHTS ON CEILING FROM SEAT ROWS 17 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK AT B5-104 FOR EMERGENCY LIGHTS ON CEILING FROM SEAT ROWS 17 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

THREE EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK AT B5-27 AND B5-28 FOR THREE EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT LIGHTS COMMON TO EMERGENCY EXIT LIGHT BATTERY PACK B5 101 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 30D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY — NOT SEATED (CABIN)

DURING OVERNIGHT MAINTENANCE CEILING EMERGENCY EXIT LIGHTS AT ROWS 8, 10, AND 11, INOPERATIVE. RESEATED CEILING EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DURING OVERNIGHT MAINTENANCE FIRST CLASS CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. TIGHTENED CEILING EMERGENCY EXIT LIGHTS CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM L2-639-694 AND 176-246 INOPERATIVE. REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PRESSURE PANEL — DAMAGED (NLG WW)

TUL - FOUND STEERING CYLINDER CONTACTED RIGHT NOSE W/W SIDE WALL DUE TO TOW BAR OVER STEER. INSTALLED DOUBLER REPAIR PER ESO 80559 DATED 1-31-02. (M)

Part: HINGE FITTING — CORRODED (VERTICAL STAB)

TUL - FOUND TWO RIGHT OUTBOARD, TWO RIGHT INBOARD, TWO LEFT OUTBOARD, TWO LEFT INBOARD VERTICAL STABILIZER HINGE PLATES CORRODED. REMOVED AND REPLACED 2 RIGHT OUTBOARD, 2 RIGHT INBOARD, 2 LEFT OUTBOARD, 2 LEFT INBOARD VERTICAL STABILIZER HINGE PLATES PER SRM 51-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENTS IN FUSELAGE SKIN AT STATIONS 238, 234, AND 218 LONGERON 18L AND 20L THERE WERE 2 EXISTING DOUBLER REPAIRS AFT OF STATION 239, THEY WERE CUT OUT WITH OTHER DAMAGE IN AREA. REPAIRED PER ESO 80559 DATED 3-29-2001. INSTALLED DOUBLER AND SKIN PLUG. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK AT 1200-1203, 1293, 1305. REPLACED NR 2 SEAT TRACK FROM 1136-1309 PER SRM 53-05 AND ESO 80559 DATED 3/27/2001. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP FROM 1263-1305. INSTALLED NEW CUSP SHEET FROM 1250-1309 LEFT PER SRM 51-01 AND ESO 80559 DATED 3/27/01. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED JUST AFT OF RIVET AT 1474 CANTED FRAME RIGHT SIDE APPROX 14 INCHES ABOVE AIRSTAIRS CUTOUT. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN BLENDED DEEP AROUND FASTENER JUST BELOW WINDOW BELT LEFT SIDE OF FUSELAGE APPROX STATION 442. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND ANTENNA INSTALLATION POINT AT FS 380 AND 402, BETWEEN LONERON 29 AND 30 LEFT HAVE CRACKS 1.5 INCHES LONG. CUT OUT DAMAGED AREAS 4 BY 6 INCHES AND INSTALLED INNER AND OUTER DOUBLER PER SRM 53-04, FIG 12B. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FRAME 1485 IS CRACKED AT STAIR ACTUATOR CASTING, RIGHT SIDE. INSTALLED SPLICE PER ESO 80559 DATED 2-23-01, MRR WRITTEN. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP MEMBRANE FROM STATION 160-200, INBOARD OF FORWARD SERVICE DOOR. INSTALLED ONE DOUBLER PER SRM 53-01-00. (M)

Part: SKIN — DENTED (CARGO DOOR)

TUL - FOUND SEVERAL DENTS IN SKIN OF ''DOOR''. REMOVED OLD SKIN AND INSTALLED NEW SKIN PER ESO 80174 3-26-01 OF ENTIRE AFT CARGO DOOR. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN STATION 1125 LEFT SIDE BETWEEN LONGERON 22 AND 23L. COLD WORKED DENTED AREA. DYE CHECKED, NO CRACKS FOUND. INSTALLED REPAIR DOUBLER PER SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK FORWARD END CORRODED, FS 218. SPLICED IN NEW SECTION OF NR 6 SEAT TRACK FROM STATION 212-302 PER SRM 53-05 FIG 4F. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN DENTED BETWEEN LONGERONS 24R AND 25R STATION 472 TO 503, DENTED UP TO .050 INCH DEEP. REWORKED SKIN TO CONTOUR AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 SHEET 22 AND ESO 80559 DATED 6/2/2000. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND SMALL SPOT OF CORROSION ON RIGHT CUSP AT STATION 267. CUT OUT CORROSION PER SRM 51-10-3. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AROUND NUTPLATE HOLES AT STATION 1148 ABOVE LONGERON 26R COMMON TO WEB. FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED PER SRM 51-70-4. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION IN SEAT TRACK NR 1 AT 1208. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174 TO STATION 1309 PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1199-1202. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174 TO STATION 1309 PER SRM 53-05. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGES IN FUSELAGE SKIN AT STATION 534 AT LONGERON 27L. REMOVED DAMAGED AREA, DYE CHECKED, NO CRACKS FOUND. FABRICATED DOUBLER FROM GAL4V T1 .032 INCH FILLER FROM 2024T3 .050 INCH. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1236-1237. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174 TO 1309 PER SRM 53-05. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT CARGO DOOR BEAM OUTBOARD FACE FROM STATION 1160 TO 1208. INSTALLED DOUBLER PER AARD 53-10-00-3. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 5 STATION 230-237. REPLACED SEAT TRACK STATION 199-246 IAW SRM 53-05 FIG 4F SHEET 2. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 598 TO 712. INSTALLED NEW CUSP SHEET FROM STATION 598 TO 712 LEFT SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND SEAT TRACK NR 1 CORRODED STATION 522 PLUS 6. INSTALLED 1 NEW SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON L4 CRACKED AT STATION 160 AT FASTENER HOLE. CUTOUT DAMAGE SECTION AND INSTLALED SPLICE PER SRM 53-02 FIGURE 18. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED AROUND LIGHTENING HOLE STATION 507. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED ALONG OUTBOARD EDGE STATION 527-540. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP STATION 997. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT ROW 22 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP ROW 22. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE TRACK LIGHT AFT MOST EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT AISLE LIGHT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CUSP — CORRODED (BS 511-693)

TUL - FOUND CORROSION ON BOTH SIDES CUSP MEMBRANE FROM STATION 511 TO STATION 693 RT SIDE. REMOVED DAMAGED AREA AND INSTALLED NEW CUSP SECTION PER AARD 53-20-00-16 AND ADVANCED ACTION DATED 12-17-97 PER RFS NR 203419. (M)

Part: O-RING — DEFECTIVE (A/C BAY)

LAX - FLT 1234 - AFTER TAKEOFF LAX, SMOKE NOTED IN CABIN. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED APU OIL COOLER O-RINGS AND ALL COALESCER BAGS. ACCOMPLISHED LEAK CHECK AND PACK BURNOUT PROCEDURE WITH NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)