N9618A

Part: CABLE — BROKEN (L2 DOOR SLIDE) · airframe 58,382 hrs · 29,091 cycles

L2 SERVICE DOOR HAD A STEEL CABLE BROKEN AND IS EXPOSED AT BOTTOM OF THE SLIDE. THE AIRCRAFT WAS GROUNDED. REPLACED L2 DOOR EVACUATION SLIDE IAW MM 25-62-00.

Part: SLIDE — DISLODGED (GALLEY DOOR) · airframe 58,369 hrs · 29,082 cycles

AIRCRAFT WAS NOT GROUNDED. CREW REPORT AFT GALLEY DOOR SLIDE PACK DISLODGED. MAINTENANCE REPLACED SLIDE PACK ASSEMBLY PER AAMM 25-62-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,271 hrs · 29,003 cycles

EMERGENCY LIGHT AT THE L1 DOOR WAS INOPERATIVE. REPLACED THE EMERGENCY LIGHT IAW AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,871 hrs · 28,759 cycles

EMERGENCY LIGHTS FOR THE TAILCONE SLIDE WERE INOPERATIVE. REPLACED B5-27 BATTERY PACKS IAW AMM 33-53-00, AND WDM 33-51-13. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,871 hrs · 28,759 cycles

EMERGENCY LIGHTS IN TAIL COMPARTMENT OVERHEAD WERE INOPERATIVE. REPLACED THE B5-27 BATTERY PACKS IAW AMM 33-53-00 AND WDM 33-51-13. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,871 hrs · 28,759 cycles

EMERGENCY LIGHTS IN THE TAIL COMPARTMENT OVERHEAD WERE INOPERATIVE. REPLACED THE B5-28 BATTERY PACKS IAW AMM 33-53-00, AND WDM 33-51-13. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,871 hrs · 28,759 cycles

EMERGENCY LIGHTS TAIL CONE SLIDE EMERGENCY LIGHTS WERE INOPERABLE. REPLACED THE B5-28 BATTERY PACKS IAW AMM 33-53-00 AND WDM 33-51-13. OPS CHECKED GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 57,871 hrs · 28,759 cycles

EMERGENCY LIGHTS IN THE MID CABIN OVERHEAD AREA WILL NOT SHUT OFF. REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: BUSTLE — OUT OF ADJUST (DOOR SLIDE) · airframe 57,595 hrs · 28,579 cycles

AFT DOOR SLIDE BUSSLE OUT OF ADJUSTEMT. MAINTENANCE ADJUSTED THE DOOR SLIDE BUSSLE IAW 25-62-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PANEL — DISTORTED (AFT GALLEY DOOR) · airframe 57,399 hrs · 28,445 cycles

LEFT AFT SERVICE/GALLEY DOOR LINER PANEL FOR DOOR SLIDE IS PREVENTING DOOR FROM OPENING, RUBBING ON DOOR FRAME. THE DOOR PANEL WAS TWISTED AND DISTORTED. ADJUSTED AFT SERVICE DOOR SLIDE COVER TO OBTAIN CLEARANCE IAW AMM 52-12-00. AIRCRAFT WAS GROUNDED.

Part: PIN — BROKEN (L2 DOOR SLIDE) · airframe 57,342 hrs · 28,400 cycles

L2 DOOR SLIDE PIN BROKEN AND PULLED OUT. MAINTENANCE REPLACED THE SLIDE IAW MCM 25-94-17 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOOT — SEPARATED (ACM) · airframe 57,318 hrs · 28,386 cycles

DURING CRUISE AT 36000 FT, RIGHT PACK PRESSURE DROPPED, TURNED ON WING ANTI- ICE AND PACK PRESSURE RETURNED TO NORMAL. DURING DESCENT, OUT OF 36000 FT, BOTH PACK PRESSURES DROPPED, PRESSURE FLOW LIGHT ILLUMINATED, CABIN ALTITUDE LIGHT ILLUMINATED. DESCENDED TO 10000 FT. OXYGEN MASKS DID NOT DROP, NO INDICATION IN CABIN EXCEPT TEMP GOT COLD. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO GATE. AIRCRAFT WAS GROUNDED. INSPECTED THE LEFT & RIGHT PACKS, FOUND THE RIGHT BOOT TO AIR CYCLE MACHINE SEPARATED. SECURED THE BOOT IAW MM 21-51-01.

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

FIRST OFFICER`S INBOARD AFT SEAT TRACK HAS CORROSION. REPLACED SEAT TRACK IAW 51-00-05, AND DRAWING 9957871.

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

CAPTAIN`S INBOARD SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW 51-00-05, AND DRAWING 9957871.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION ON CUSP AT AFT GIRT BAR FITTING TO AFT END OF CUSP AT AFT SERVICE DOOR STATION 1174 AREA. INSTALLED NEW SECTION OF CUSP AND REPAIR DOUBLER PER 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 1175) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

CORROSION ON THE CUSP WEB AT THE END OF THE NR 1 SEAT TRACK AT BS 1175. REPAIRED THE CUSP WEB IAW SRM 53-05-00-001.

Part: SKIN — CRACKED (NEAR NLG DOOR) · airframe 57,176 hrs · 28,312 cycles

CRACK FOUND ON FUSELAGE SKIN AT THE NOSE LANDING GEAR AFT LEFT DOOR.HINGE CUTOUT. REPAIRED THE SKIN IAW SRM 53-05-00, FIGURE 158.

Part: SKIN — CRACKED (NEAR NLG DOOR) · airframe 57,176 hrs · 28,312 cycles

CRACK FOUND ON FUSELAGE SKIN AT THE NOSE LANDING GEAR AFT RIGHT DOOR.HINGE CUTOUT. REPAIRED THE SKIN IAW SRM 53-05-00, FIGURE 158.

Part: WINDOW FRAME — CRACKED (BS 1041) · airframe 57,176 hrs · 28,312 cycles

CRACKED CABIN WINDOW FRAME AT BS 1041. INSTALLED A DOUBLER IAW 53-10-00-25.

Part: CUSP WEB — CORRODED (BS 1140-1145) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

CUSP WEB UNDERNEATH FORWARD GIRT BAR BRACKET ATTACH POINT AT THE AFT SERVICE DOOR IS CORRODED. REPAIRED THE CUSP WEB IAW 53-20-00-16.

Part: WINDOW FRAME — CRACKED (BS 465) · airframe 57,176 hrs · 28,312 cycles

CRACKED WINDOW FRAME, BOTTOM AFT LEFT TANG AT BS 465. INSTALLED A DOUBLER IAW 53-10-00-25.

Part: WINDOW FRAME — CRACKED (BS 1060) · airframe 57,176 hrs · 28,312 cycles

CRACKED RIGHT CABIN WINDOW FRAME AT BS 1060. INSTALLED A DOUBLER IAW 53-10-00-25.

Part: SEAT TRACK — OUT OF LIMITS (BS 795-1136) · airframe 57,176 hrs · 28,312 cycles

SEAT TRACK, BS 795-1136, IS OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 25-23-00.

Part: FLOOR SUPPORT — CORRODED (BS 160-218) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

WEAR AND CORROSION FOUND ON THE FLOOR SUPPORT AT BS 218, CENTERLINE. INSTALLED A NEW FLOOR SUPPORT IAW DRAWING 9936535, AND 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,176 hrs · 28,312 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED CABIN FLOOR INTERCOSTAL CENTERLINE IN CARGO CEILING BETWEEN STA 769 TO STA 786. INSTALLED INTERCOSTAL IN CEILING PER PRINT 9936580 AND AARD 51-00-05-1.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

RIGHT WING FLAP CENTER HINGE UPPER AND LOWER STUDS AND FITTING CORRODED. INSTALLED A NEW CENTER HINGE STUDS AND FITTING IAW AMM 57-40-01.

Part: HINGE FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 57,176 hrs · 28,312 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. LEFT HAND WING ONBOARD FLAP CENTER HINGE UPPER AND LOWER STUDS AND FITTING CORRODED. INSTALLED NEW STUDS AND FITTING PER AMM 57-40-01.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,779 hrs · 28,057 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN SEAT PATH EMERGENCY LIGHTS INOPERABLE ON AFT BATTERY PACK. REPLACED AFT BATTERY PACK PER AMM 33-60-98.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,779 hrs · 28,057 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN SEAT PATH EMERGENCY LIGHTS INOPERABLE ON FOWARD BATTERY PACK. REPLACED FOWARD BATTERY PACK PER AMM 33-60-98.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 55,198 hrs · 27,059 cycles

FLIGHT ATTENDANT AFT EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 26-60-00. OPS CHECKED GOOD.

Part: BALLAST — ODOR (COCKPIT) · airframe 55,071 hrs · 26,976 cycles

AIRCRAFT WAS GROUNDED. DURING CRUISE, FAINT ELECTRICAL ODOR EMITTED FROM FIRST OFFICER INSTRUMENT PANEL. REMOVED AND REPLACED B6-1 INSTRUMENT PANEL FLUORESCENT LIGHTING BALLAST IAW AMM 33-10-00 AND WDM 33-14-00. OPERATIONAL CHECK GOOD.

Part: CIRCUIT BREAKER — FAILED (LT BUSS) · airframe 54,994 hrs · 26,928 cycles

LEFT ELECTRICAL BUSS FAILURE. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT AC BUSS CIRCUIT BREAKER B1-273 IAW WDM 24-50-01. OPERATIONAL CHECKED GOOD.

Part: LANYARD — DETACHED (L1 DOOR SLIDE) · airframe 54,866 hrs · 26,843 cycles

L1 DOOR EMERGENCY SLIDE GIRT BAR LANYARD IS DETACHED FROM SLIDE PACK. ATTACHED THE LANYARD IAW AMM 25-62-00. OPS CHECKED GOOD.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 54,856 hrs · 26,837 cycles

AIRCRAFT NOT GROUNDED. L2 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR IS DIFFICULT TO ARM AND DISARM. CLEANED AND LUBRICATED GIRT BAR ATTACHMENT IAW AMM 25-61-01. OPERATIONAL CHECK GOOD.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 54,586 hrs · 26,660 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24D HAS A CRACKED LENS COVER. REMOVED AND REPLACED LENS COVER IAW AMM 33-60-98. OPS CHECKED GOOD.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 54,586 hrs · 26,660 cycles

EMERGENCY EXIT SIGN RIGHT FORWARD OVERWING DOOR IS BRITTLE AND CRACKED. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 54,586 hrs · 26,660 cycles

EMERGENCY PORTABLE LIGHT ASSEMBLY HAS A BROKEN TIP ON THE BASE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (EXIT SIGN) · airframe 54,494 hrs · 26,606 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EXIT SIGN LENS COVER BROKEN. REPLACED LENS COVER IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — LACK OF LUBE (GLY DOOR SLIDE) · airframe 54,379 hrs · 26,541 cycles

AFT GALLEY DOOR EMERGENCY SLIDE GIRT BAR DIFFICULT TO ARM & DISARM. CLEANED AND LUBED GIRT BAR LATCH PLATE ASSEMBLY IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,334 hrs · 26,513 cycles

AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IN AFT GALLEY INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00-901-801. OPERATIONAL CHECK GOOD.

Part: BEAM — CRACKED (BS 180-181) · airframe 53,882 hrs · 26,231 cycles

CRACK IN CENTER SECTION OF NR 6 BEAM, FROM BOLT HEAD, IN FWD ENTRY DOOR. INSTALLED DOUBLER IAW AARD 52-10-00-3.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 53,855 hrs · 26,215 cycles

DURING ACCOMPLSIHEMENT OF WORK CARD 5403, POWER SUPPLY AB5-3 FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY BATTERY IAW AMM 33-60-98. OPS TESTED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 53,855 hrs · 26,215 cycles

DURING ACCOMPLSIHEMENT OF WORK CARD 0801, POWER SUPPLY B5-107 FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY BATTERY IAW AMM 33-53-00. OPERATIONAL TEST NORMAL.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 53,842 hrs · 26,201 cycles

DURING CLIMB, THE CENTER FUEL PRESSURE LOW LIGHT ILLUMINATED AND THE CENTER BOOST PUMP CIRCUIT BREAKER TRIPPED. R & R CENTER AFT BOOST PUMP IAW AMM 28-20-07.

Part: SEAL — LEAKING (APU GENERATOR) · airframe 53,139 hrs · 25,782 cycles

AIRCRAFT WAS GNDED. BURNING OIL SMELL IN CABIN & COCKPIT WHEN PACKS ARE ON APU AIR ACCOMPANIED BY HAZE IN CABIN. FOUND APU INGESTING OIL. MAINTENANCE FOUND MAIN GENERATOR SEAL LEAKING AND REPLACED AUXILIARY POWER UNIT PER MCM CARD 49-96-01.

Part: WIRE — BROKEN (ZONE 400) · airframe 50,554 hrs · 24,207 cycles

AIR INTERRUPT, ENG SHUTDOWN & EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB LT OIL TEMP HIGH, 199 DEG C. DESCENDED & OIL TEMP ERRATIC BUT STILL READING ABOVE 165 DEG C. OCCASIONALLY BLANKED OUT. FOUND BROKEN WIRE AT PIN A ON P1-812. R & R PIN. PERFORMED OPERATIONAL CHECK OF LT ENG OIL TEMP INDICATION SYS IAW AMM 79-32-01 & 72-00-00. SYS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,266 hrs · 24,042 cycles

MID CARGO DOOR FWD TOP STOP FITTING IS CRACKED. R & R STOP FITTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: FORMER — CRACKED (RT WING) · airframe 50,038 hrs · 23,918 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING, NR 4 SLAT REPAIR DOUBLER & HAT BUSHING IAW WC 57-98-06.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,810 hrs · 23,799 cycles

RIGHT FUSELAGE OVERWING EVACUATION LIGHT L2-662 INOPERATIVE. R & R LAMP. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00. SYS CHECKED NORMAL.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 49,154 hrs · 23,433 cycles

WHILE BOARDING, ELEC SMELL WAS NOTICED. LIGHT BALLAST LOCATED ABOVE ROW 7AB WAS BURNING. CHARRING OCCURRED ON THE OVERHEAD CEILING PANEL & INSULATION BAGS AROUND THE BALLAST ALSO BURNED UP. ACFT REMOVED FROM SERVICE. REPLACED LAMP & BALLAST. OPERATIONS CHECKED NORMAL.

Part: SPRING — BROKEN (TE FLAP) · airframe 48,139 hrs · 22,886 cycles

TUS CREW REPORTED FLAPS WOULD NOT EXTEND BEYOND 23 DEGREES ON APPROACH. EMERGENCY DECLARED FLIGHT LANDED TUS WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND SEQUENCE MECHANISM SPRING BROKEN. REPLACED SPRING & FLAP CONTROL VLV. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 46,856 hrs · 22,232 cycles

CLT CREW REPORTED CNTR TANK BOOST PUMP CIRCUIT BREAKER POPPED. FLIGHT RETURNED CLT LANDED WITHOUT INCIDENT. PLACARDED CNTR TANK BOOST PUMP INOPERATIVE IAW MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED AFT CNTR FUEL BOOST PUMP AT DFW ON A2/02/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SPAR — DAMAGED (LT WING) · airframe 46,850 hrs · 22,226 cycles

LT HAND WING REAR SPAR HAS IMPACT DAMAGE TO WEB & UPPER SPAR "T", FORWARD OF OTBD FLIGHT SPOILER ACTUATOR. ACCOMPLISHED REPAIR IAW EA MD80-57-032542.

Part: STOP FITTING — CRACKED (CABIN DOOR) · airframe 46,850 hrs · 22,226 cycles

CABIN AFT ENTRY DOOR CENTER STOP FITTING CRACKED. R & R STOP FITTING IAW AARD 51-00-05-1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

SEAT TRACK NR 1 AT STATION 793 OTBD DAMAGED. REPACKED STRAP IAW AARD51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CRACK IN RT HAND CUSP AT STATION 805, OTBD OF NR 6 SEAT TRACK. INSTALLED NEW CUSP SHEET IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

SEAT TRACK NR 4 CORROSION FROM STATIONS 237 & 262. INSTALLED NEW SEAT TRACK IAW AMM 53-40-01-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CORROSION ON RT CUSP FROM STATIONS 218 TO 237. INSTALLED NEW CUSP SHEET FROM STATIONS 218 TO 237 IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CORROSION ON CUSP MEMBRANE JUST INSIDE FWD ENTRY DOOR AT STATION 195. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CRACKS IN SUBFLOOR MEMBRANE. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CORROSION IN RT CUSP SHEET AT STATION 500. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

RT CUSP SHEET CORRODED AT STATION 602. INSTALLED NEW CUSP DOUBLER IAW AARD 53-20-00-16.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,850 hrs · 22,226 cycles

LONGERON 29 RT CORRODED AT STATION 1315. INSTALLED DOUBLER IAW SRM 53-02-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,850 hrs · 22,226 cycles

AFT CARGO DOOR BEAM CORRODED. INSTALLED DOUBLER IAW AARD 53-10-00-3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CRACK IN RT CUSP, STATION 843, AT FASTENER HOLE FOR HORSESHOE COLLAR. ACCOMPLISHED INSTALLATION OF CUSP REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

STATION 1418 & LONGERON 2 RT IS CRACKED IN RADIUS OF FRAME. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-15.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CRACK IN RT CUSP AT STATION 1165. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

RT WINDOW RING PAN CRACKED AT STATION 1079. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

PUNCTURE IN SUBFLOOR JUST INBD OF FWD SERVICE DOOR AT STATION 185 RT. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,850 hrs · 22,226 cycles

LT HAND TIE DOWN TRACK SPLICE CORRODED AT STATION 1213. REPLACED SPLICE IAW AARD 51-00-05-1.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,850 hrs · 22,226 cycles

CORROSION ON SUBFLOOR AT STATION 217 RT. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,850 hrs · 22,226 cycles

PUNCTURE & CORROSION ON SUBFLOOR FROM STATIONS 180 TO 200 RT. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CORROSION ON SUBFLOOR UNDER G1 GALLEY DRAIN PAN. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

CORROSION ON RT SUBFLOOR UNDER NR 6 SEAT TRACK AT STATION 217. FABRICATED & INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

RT HAND WINDOW PAN CRACKED AT STATION 946. INSTALLED DOUBLER ANGLE IAW AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

RT CUSP CORRODED AT STATION 389. CUSP DOUBLER INSTALLED IAW AARD 53-20-00-16.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

RT HAND CUSP PUNCTURED AT STATION 429 UNDER SEAT TRACK NR 6. ACCOMPLISHED REPAIR IAW SRM 53-01-00 FIGURE 2.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

RT HAND WINDOW PAN CRACKED AT STATION 1174. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: CUSP WEB — MISMANUFACTURED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

HOLE FOR HORSE SHOE COLLAR AT STATION 886 LT SIDE DOES NOT HAVE MINIMUM EDGE DISTANCE. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

SKIN PANEL AT STATION 224 DAMAGED. INSTALLED EXTERNAL DOUBLER.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

RT WINDOW RING PAN CRACKED AT STATION 1193. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 46,850 hrs · 22,226 cycles

AFT SERVICE DOOR SLIDE AFT GIRT BAR MOUNT HAS CORROSION, INSTALLED AFT GIRT BAR MOUNT IAW AARD 51-00-05-1.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

LT WINDOW RING PAN CRACKED AT STATION 598. INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,850 hrs · 22,226 cycles

SHEAR TIE CRACKED INBD OF LONGERON 3 RT & STATION 1437. INSTALLED NEW SHEAR TIE.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,850 hrs · 22,226 cycles

CORROSION ON RT CUSP AT STATION 472 OTBD OF NR 6 SEAT TRACK. CUT OUT CORRODED AREA & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

AFT RIGHT OVERWING EXIT DOOR EXIT ILLUMINATION SIGN IS INOPERATIVE. REPLACED EMERGENCY BATTERY PACK AT ROW 21DEF OVERHEAD. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

AFT LEFT OVERWING EXIT DOOR OVERHEAD EMERGENCY EXIT ILLUMINATION SIGN INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 20DEF CENTER OVERHEAD. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

OVERHEAD EMERGENCY LIGHTS OVER ROWS 26 TO 28 INOPERATIVE. REPLACED BATTERY PACK AT ROW 29DEF OVERHEAD. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

SEAT MOUNTED EMERGENCY EGRESS LIGHT AT 24D INOPERATIVE. REPLACED BATTERY PACK AT SEAT 25DEF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

ROWS 23 TO 26 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-106. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 42,453 hrs · 19,958 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. RESEATED BATTERY PACK AT 7DEF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

ROWS 27 THROUGH 29 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5 107. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

ROW 21 EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B5-105. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,453 hrs · 19,958 cycles

ROW 20 EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B5-104. OPS CHECK NORMAL.

Part: CONNECTOR — BROKEN (CABIN) · airframe 41,709 hrs · 19,556 cycles

SEAT ROW 17 EMERGENCY LIGHT INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY LIGHT AT ROW 17.

Part: CONNECTOR — BROKEN (CABIN) · airframe 41,709 hrs · 19,556 cycles

SEAT ROW 15 EMERGENCY LIGHT INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY LIGHT AT ROW 15.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 39,600 hrs · 18,485 cycles

EMERGENCY ESCAPE PATH LIGHT AT SEAT 18D INOPERATIVE. REPINNED EMERGENCY LIGHT CONNECTOR AT SEAT 18D. OPS CHECK NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 38,995 hrs · 18,190 cycles

LONGERON 2 RIGHT CRACKED AFT OF 1418. INSTALLED LONGERON 2 RIGHT REPAIR PER SRM 53-14-04, SRM 53 02-00 AND EA MD80-53-015113 DATED 1/31/11.

Part: FLAP — DAMAGED (LT WING) · airframe 38,995 hrs · 18,190 cycles

INBOARD FLAP LEADING EDGE HAS DAMAGE ABOVE INBOARD HINGE. INSTALLED HOT BOND REPAIR PER SRM 51-70-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 38,995 hrs · 18,190 cycles

CRACK IN RADIUS OF LONGERON 20 LEFT ABOVE INBOARD FLAP ACTUATOR. INSTALLED DOUBLER PER AARD 53-10-00-18.

Part: ACTUATOR — FAULTED (OUTFLOW VALVE) · airframe 34,712 hrs · 16,308 cycles

DFW - CREW REPORTED AMBER AUTO INOPERATIVE AND AIRCRAFT HAVING PRESSURIZATION ISSUES. RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND THE OUTFLOW VALVE ACTUATOR HAD FAULTED. REPLACED OUTFLOW VALVE ACTUATOR AND BOTH OUTFLOW/BUTTERFLY MOTORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

CORROSION ON ANTENNA DOUBLER CUTOUT AT STATION 643. INSTALLED NEW ANTENNA DOUBLER AS UNDER SRM 53-30-05.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

AFT CARGO CORROSION ON SKIN STATION 1310 AT FORWARD LOWER CORNER OF LAVATORY SERVICE PANEL. SKIN DOUBLER INSTALLED AT STATION 1310 LOWER FORWARD CORNER OF AFT LAVATORY SERVICE PANEL UNDER EA MD80-53-006933.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

CANT FRAME CRACKED ABOVE LEFT UPPER TAIL CONE LATCH AT STATION 1510. INSTALLED NEW SECTION OF FRAME WITH SPLICE UNDER SRM 51-70-5 FIGURE 1 SHEET 2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

CORROSION OF AFT SIDE FRAME STATION 1309 L28L-L29R. ACCOMPLISHED SPLICE REPAIR UNDER SRM 51-30-02.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

CORROSION OUT OF LIMITS RIGHT HAND TIE DOWN TRACK. INSTALLED NEW TIE DOWN TRACK FROM 1212 TO 1322 UNDER SRM 53-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

CORROSION ON ALTIMETER DOUBLER. REMOVED AND REPLACED DOUBLER UNDER SRM 51-30-05 AND 51-30-02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

TUL - LEFT 1380 FRAME WEB HAS HOLE WORN THRU WEB BY CONTROL TEMPERATURE VALVE. REPLACED DOUBLER ON WEB UNDER AARD 53-10-00-28.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

TUL - RIGHT CUSP OUT OF LIMIT STATION 1184 - 1185. INSTALLED DOUBLER AT RIGHT CUSP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

TUL - FUSELAGE SKIN CRACKED AT FASTENERS STATION 1380 BETWEEN LONGERONS 13 & 14 RIGHT. INSTALLED REPAIR DOUBLER AT STATION 1380 BETWEEN L13 AND L14 UNDER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

TUL - SHEAR TIE CRACKED. REPLACED SHEAR TIE UNDER SRM 51-30-05.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

TUL - CORROSION IN ANTENNA DOUBLER. INSTALLED DOUBLER UNDER SRM 51-30-05.

Part: STOP FITTING — CRACKED (DOOR) · airframe 34,701 hrs · 16,303 cycles

TUL - NUMBER FOUR AFT STOP PAD FITTING CRACKED. REMOVED AND REPLACED NUMBER FOUR BEAM AFT STOP PAD FITTING PER ESO-80174.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

TUL - TWO DENTS IN FUSELAGE SKIN. DENTS WERE COLD WORKED AND DOUBLER INSTALLED UNDER SRM 53-04 FIGURE 38 VIEW P.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

TUL - CORROSION IN NUMBER SIX SEAT TRACK GALLEY MOUNT. REMOVED AND REPLACED GALLEY MOUNT UNDER SRM 51-30-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

TUL - RIGHT CUSP OUT OF LIMITS STATION 484-503. INSTALLED DOUBLER AT RIGHT CUSP STATION 484-503.

Part: STOP FITTING — CRACKED (DOOR) · airframe 34,701 hrs · 16,303 cycles

TUL - NUMBER ONE BEAM FORWARD STOP PAD FITTING CRACKED. REMOVED AND REPLACED NUMBER ONE BEAM FORWARD STOP PAD FITTING PER ESO-80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,701 hrs · 16,303 cycles

TUL - AFT CARGO DOOR STOP-PAD FITTING CRACKED AT FORWARD NUMBER FIVE BEAM. REPLACED STOP-PAD FITTING PER ESO-80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 34,701 hrs · 16,303 cycles

TUL - FORWARD STOP-PAD FITTING CRACKED AT NUMBER ONE BEAM ASSEMBLY. REPLACED STOP-PAD FITTING PER ESO-80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 34,701 hrs · 16,303 cycles

TUL - NUMBER FOUR BEAM FORWARD STOP PAD FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO-80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,701 hrs · 16,303 cycles

TUL - AFT CARGO DOOR FORWARD STOP-PAD FITTING AT NUMBER THREE BEAM CRACKED. REPLACED STOP-PAD FITTING PER ESO-80174.

Part: SHEAR TIE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

TUL - CORROSION IN SHEAR TIE IN MID CARGO. REPAIRED UNDER SRM 51-30-05 AND SRM 51-30-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

TUL - CORROSION IN AFT CARGO TIE DOWN TRACK. INSTALLED NEW TRACK UNDER AARD 51-00-00-012.

Part: STOP FITTING — CRACKED (DOOR) · airframe 34,701 hrs · 16,303 cycles

AFT STOP PAD FITTING CRACKED AT NUMBER 5 BEAM ASSEMBLY. REMOVED AND REPLACED AFT DOOR STOP PAD FITTING PER ESO80174.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

TUL - LOWER LEFT VAULT DOOR STOP STIFFENER CRACKED. INSTALLED NEW STIFFENER PER 51-01.

Part: STOP FITTING — CRACKED (DOOR) · airframe 34,701 hrs · 16,303 cycles

NUMBER ONE FORWARD BEAM STOP FITTING CRACKED. REPLACED NUMBER ONE BEAM FORWARD STOP PAD FITTING UNDER ESO-80174.

Part: PAN — DAMAGED (SERVICE DOOR) · airframe 34,701 hrs · 16,303 cycles

AFT SERVICE DOOR HANDLE PAN DAMAGED ON HANDLE PAN TOWERS. REPLACED HOUSING UNDER ESO-80175.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

WINDOW PAN CRACKED AT STATION1060L. INSTALLED DOUBLER AS PER AARD 53-10-00-75.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,701 hrs · 16,303 cycles

TUL - CORROSION ON CUSP RIGHT STATION 988-991. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

WINDOW PAN CRACKED AT STATION 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,701 hrs · 16,303 cycles

CRACK IN WINDOW PAN AT STATION 1022L. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: DUCT — RUPTURED (ZONE 200) · airframe 34,385 hrs · 16,139 cycles

STL - AIRCRAFT STARTED TO VIBRATE ON TAKEOFF. RETURNED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RUPTURED DUCT IN TAIL. REPLACED BOOT AND DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY) · 32,157 cycles

STL INFLIGHT T1419/22AUG. FIRST CLASS GALLEY OVEN SMOKING AFTER TAKE OFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. FOUND RESIDUE IN OVEN. REPLACED FIRST CLASS GALLEY OVEN AND OVEN CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SHROUD — DAMAGED (CABIN) · airframe 31,979 hrs

DFW EMERGENCY LIGHT SHROUD AT SEAT 22D DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: ELECTRONIC UNIT — SHORTED (CARGO FIRE)

LAX INFLIGHT T1943/18DEC - RECEIVED AFT CARGO FIRE INDICATION. DISCHARGED FIRE BOTTLE AND AIR INTERRUPTED TO BFL. LANDED WITHOUT INCIDENT. NO SIGN OF FIRE IN CARGO AREA. FOUND CARGO ELECTRONIC UNIT WET AND DRIPPING WATER AND SHORTING. CHECKED FOR WATER LEAK AND REPLACED CARGO ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FILTER — DIRTY (NR 2 ENGINE OIL) · airframe 29,949 hrs

DFW INFLIGHT T1874/30NOV - NUMBER TWO ENGINE OIL FILTER CLOG LIGHT ILLUMINATED IN FLIGHT. CAPTAIN SHUT DOWN NUMBER TWO ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 48 MINUTES. FOUND NUMBER TWO ENGINE OIL FILTER DIRTY WITH CARBON. REPLACED OIL FILTER AND SERVICED NUMBER TWO ENGINE OIL TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY FLASH LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASH LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (ANTI-ICE SYSTEM)

RIGHT ENGINE ANTI-ICE VALVE INDICATION ILLUMINATED WITH SWITCH ON. RECYCLED SWITCH AND CIRCUIT BREAKER WITH NO HELP. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED RIGHT ENGINE ANTI-ICE VALVE NOSE COWL AND PERFORMED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY SEAT PATH LIGHTING IN CABIN AT AB5 4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT PATH LIGHTING IN CABIN AT AB5 4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN)

LGA - EMERGENCY CEILING LIGHT FROM ROWS 21 TO AFT OF CABIN DOOR INOPERATIVE. RESEATED BATTERY PACK AT ROW 21 FOR EMERGENCY CEILING LIGHT FROM ROWS 21 TO AFT OF CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ELECTRONIC UNIT — INOPERATIVE (CARGO BAY)

PSP - INFLIGHT DURING DESCENT WARNING SOUNDED INDICATING FIRE IN AFT CARGO. BOTTLES DISCHARGED. LANDED PSP WITHOUT INCIDENT. NO FIRE. FOUND CARGO ELECTRONIC UNIT IN AFT CARGO COMPARTMENT CAUSING FIRE WARNING. REPLACED CARGO ELECTRONIC UNIT AND REPLACED CARGO SUPPRESSION SYSTEM FIRE BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

TPA - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD COACH OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN FORWARD COACH OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK · airframe 13,686 hrs · 6,596 cycles

THE EGRESS LIGHTS ROW 21 THRU 26 WOULD NOT SHUT OFF. REPLACED THE BATTERY PACK. CHECK-C 11-9-01 MCI. --CLOSED--

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,925 hrs · 6,115 cycles

DURING CHECK-C MAINT FOUND CRACKED INTERCOSTAL AT CANT LINE 1510, 2 O'CLOCK POSITION, AFTER BODY. REMOVED CRACKED INTERCOSTAL AT CANT LINE 1510, 2 O'CLOCK POSITION AND INSTALLED NEW INTERCOSTAL PER TWA SPM 6-70-01, AND DRAWING 9911875, SRM 51-30-01, SRM 51-30-02, AND SRM 51-30-5.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 12,925 hrs · 6,115 cycles

DURING CHECK-C MAINT THE LT CARGO TIE DOWN TRACK HAD CORROSION IN SCREW HOLES AND EDGES AT STA 1123 TO 1287. INSTALLED NEW TRACK USING FASTENERS PER SRM 51-30-1 AND SPM 6-70-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 12,925 hrs · 6,115 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, BETWEEN STA 1250 TO 1271, THE RT CARGO TIE DOWN TRACK SCREW HOLES HAD CORROSION. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30-1 AND 51-30-2, PER SPM 6-70-01 AND DRAWING 5936663.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,925 hrs · 6,115 cycles

DURING CHECK-C MAINT, THE RT MAIN LANDING GEAR WHEEL WELL RT GEAR DOOR CUTOUT WAS CRACKED ON THE AFT OUTBOARD END. ACCOMP INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLERS PER SRM 53-01, PAGE 10.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,925 hrs · 6,115 cycles

DURING CHECK-C MAINT FOUND LT MAIN LANDING GEAR WHEEL WELL AFT INBOARD LOWER CORNER HAD CRACK IN AFT FACE. ACCOMPLISHED HIGH FREQ EDDY CURRENT AND CONFIRMED CRACK PER 51-00-03, PART 6. INSTALLED NEW PART PER SPM 6-70-01.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 12,925 hrs · 6,115 cycles

DURING CHECK-C MAINT THE SKIN STANDOFF WAS DAMAGED AT BELT RING STA 1443, BETWEEN LONGERON 16L AND 17L. REPAIRED PER SRM 53-03, PAGE 7 AND PAINTED PER SRM 51-10-3.

Part: WEB — CRACKED (FUSELAGE) · airframe 12,925 hrs · 6,115 cycles

DURING CHECK-C MAINT THE LT VENT BOX AREA, SHIELD WEB WAS CRACKED AT UPPER AFT CORNER INSIDE THE VENT BOX. STOP DRILLED CRACK PER SRM 51-01 PAGE 6. INSTALLED DOUBLER PER SRM 51-70-4.

Part: LENS — MISSING (CABIN) · airframe 11,536 hrs · 5,472 cycles

THE EGRESS LIGHT RED LENS WAS MISSING AT ROW 21. REPLACED THE RED LENS. CHECK-C 10-12-00 STL.

Part: WIRE — BROKEN (EGRESS LIGHT) · airframe 10,687 hrs · 5,095 cycles

THE EGRESS LIGHTING WAS INOPERATIVE FROM THE FORWARD GALLEY TO ROW 3. SPLICED BROKEN WIRES AT SEAT ROW 3. CHECK-C 12-12-00 STL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,487 hrs · 4,046 cycles

DURING OVERNIGHT INSPECTION FOUND EGRESS LIGHTS INOP AT ROWS 22 - 23. REPLACED 2 BATTERIES AND OPERATIONAL CHECKED PER M33-59-00. AC09 04-16-00 JFK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,913 hrs · 3,824 cycles

THE PORTABLE EMERGENCY LIGHT AT THE LEFT SIDE NUMBER 1 CABIN DOOR WAS INOPERATIVE. THE SWITCH HAD BEEN LEFT ON. REPLACED THE BATTERIES. CHECK-C 9-9-99 STL.

Part: POWER SUPPLY — INOP (ROW 12)

THE EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN ROWS 4 AND 12. REPLACED THE POWER SUPPLY. CHECK-C 9-3-99 STL.