N9619V

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,312 hrs · 29,201 cycles

OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE IN THE CABIN FROM ROWS 29 - 31. REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,312 hrs · 29,201 cycles

OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE IN THE CABIN FROM ROWS 8 - 10. REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 57,948 hrs · 28,973 cycles

EMERGENCY LIGHTS AT SEATS 3E AND 3F WERE NOT WORKING. FOUND THE EMERGENCY LIGHTS WIRE HARNESS FOR SEATS 3E AND 3F WAS BROKEN AT THE CONNECTOR AND AT THE SPLICE. REPLACED THE WIRE HARNESS SPLICE IAW AMM 20S. OPS CHECKED GOOD.

Part: TARGET — OUT OF ADJUST (CARGO DOOR) · airframe 57,733 hrs · 28,840 cycles

AFTER TAKEOFF AFT CARGO DOOR LIGHT CAME ON AND AIRCRAFT WAS NOT PRESSURIZED. CARGO TEMPERATURE HIGH WARNING. EMERGENCY WAS DECLARED AND RETURNED TO DEPARTURE. ADJUSTED AFT CARGO DOOR TARGET DUE TO OUT OF TOLERANCE IAW AMM 52-70-02. OPS CHECKED GOOD.

Part: CONTROLLER — FAULTY · airframe 57,733 hrs · 28,840 cycles

AFTER TAKEOFF AFT CARGO DOOR LIGHT CAME ON AND AIRCRAFT WAS NOT PRESSURIZED. ACCOMPLISHED ATBT WIRES CHECK GOOD. AIRCRAFT WAS GROUNDED. REPLACED NR 2 CONTROLLER IAW AMM 21-32-00, OPS CHECKED GOOD.

Part: ANGLE — CRACKED (BS 826) · airframe 57,094 hrs · 28,424 cycles

CRACK IN ANGLE AT BS 826 IN BOTTOM FORWARD CORNER OF WEB BELOW CABIN FLOOR INBOARD AND BELOW THE NR 5 SEAT TRACK. REPAIRED THE ANGLE IAW EA 279212.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,094 hrs · 28,424 cycles

AIRCRAFT IN BASE MAINTENANCE: FUSELAGE SKIN CRACKED AT NOSE LANDING GEAR WELL WELL, RIGHT HAND DOOR AFT HINGE CUTOUT BETWEEN STATION 89.05 TO STATION 101.55. REPAIRED SKIN PER SRM 53-05-00-001.

Part: SKIN — CRACKED (BS 89-101) · airframe 57,094 hrs · 28,424 cycles

NOSE WHEEL WELL, LEFT STRUT DOOR AFT HINGE CUTOUT SKIN CRACKED. INSTALLED A DOUBLER IAW SRM 53-05-00-001, FIGURE 158.

Part: LONGERON — CRACKED (BS 993) · airframe 57,094 hrs · 28,424 cycles

LONGERON 20L FOUND CRACKED FROM EDGE TO FASTENER HOLE AT BS 993. INSTALLED A REPAIR ANGLE IAW 53-10-00-18.

Part: FRAME — CRACKED (BS 1484) · airframe 57,094 hrs · 28,424 cycles

FRAME CRACKED AT LOWER END BELOW AFT STAIR DOOR ACTUATOR RIGHT SIDE AT BS 1485. REPAIRED THE FRAME IAW 53-10-00-33.

Part: LONGERON — CRACKED (BS 1418) · airframe 57,094 hrs · 28,424 cycles

LONGERON 2R CRACKED AT BS 1418. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: LATCH — BENT (L1 DOOR HOLDOPEN) · airframe 56,977 hrs · 28,353 cycles

L1 DOOR HOLD-OPEN LATCH, DOES NOT ALIGN, FOUND BENT. REPLACED THE HOLD OPEN IAW AMM 52-11-04.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,978 hrs · 28,353 cycles

EMERGENCY LIGHT DIM AND INOPERATIVE WHEN TESTED. REPLACED THE EMERGENCY LIGHT BATTERY PACKS IN THE FWD AND AFT GALLEY AREAS. OPS CHECKED GOOD IAW AMM 33-60-98.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,978 hrs · 28,353 cycles

EMERGENCY LIGHT DIM AND INOPERATIVE WHEN TESTED. REPLACED THE BATTERY PACKS IN FWD AND AFT GALLEY AREAS. OPS CHECKED GOOD IAW AMM 33-60-98.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,978 hrs · 28,353 cycles

EMERGENCY LIGHTS DIM THEN INOPERATIVE. REPLACED THE EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33-60-98.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,978 hrs · 28,353 cycles

EMERGENCY LIGHTS DIM THEN INOPERATIVE. REPLACED THE BATTERY PACKS ABOVE ROW 21, IAW AMM 33-60-98. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,978 hrs · 28,353 cycles

AFT OVERWING EMERGENCY EXIT LIGHTS FOUND INOPERATIVE DURING AN A CHECK. REPLACED THE BATTERY PACK B5-105 IAW WDM 31-51-11. EMERGENCY EXIT LIGHT OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,978 hrs · 28,353 cycles

EMERGENCY LIGHTS DIM THEN INOPERATIVE. REPLACED THE BATTERY PACKS ABOVE ROW 21, IAW AMM 33-60-98. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,978 hrs · 28,353 cycles

AIRCRAFT WAS NOT GROUNDED: ESCAPE PATH LIGHT DIM THEN INOPERABLE. MAINTENANCE REPLACED ESCAPE PATH LIGHT BATTERY PACK PER AMM 33-60-98 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,890 hrs · 28,296 cycles

SEAT ROW 23D EMERGEMCY LIGHT SHROUD BROKEN. REPLACED THE EMERGENCY LIGHT LENS IAW AMM 33-60-98.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,890 hrs · 28,296 cycles

SEAT ROW 30D EMERGENCY LIGHT SHROUD BROKEN. REPLACED THE EMERGENCY LIGHT LENS IAW AMM 33-60-98.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,890 hrs · 28,296 cycles

SEAT ROW 21D EMERGENCY LIGHT AFT SHROUD BROKEN. REPLACED THE EMERGENCY LIGHT LENS IAW AMM 33-60-98.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,890 hrs · 28,296 cycles

EMERGENCY LIGHT LENS BROKEN AT SEAT ROW 20D. MAINTENANCE REPLACED THE LENS IAW AMM 33-60-98 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — DETACHED (L1 DOOR) · airframe 56,290 hrs · 27,910 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR GIRT BAR IS UNATTACHED. RESECURED GIRT BAR CABLE PER AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,860 hrs · 27,632 cycles

EMERGENCY PORTABLE LIGHT BY THE FORWARD ENTRY DOOR IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,860 hrs · 27,632 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS ON RIGHT SIDE OF AIRCRAFT, ROW 20 BELOW ESCAPE DOOR ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY CONTROL MODULE (AALA201709069009) PER AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: TIRE — SEPARATED (MLG) · airframe 55,797 hrs · 27,590 cycles

AIRCRAFT WAS GROUNDED. NR 4 MAIN TIRE TREAD SEPARATED ON LANDING CAUSING DAMAGE TO THE FLAP. REMOVED AND REPLACED NR 4 MAIN LANDING GEAR WHEEL AND TIRE ASSEMBLY IAW AMM 32-40-01-201.

Part: SLIDE — DEFECTIVE (ZONE 800) · airframe 55,564 hrs · 27,445 cycles

THE AIRCRAFT WAS NOT GROUNDED. FWD GALLEY GIRT BAR CABLE IS DETACHED. REMOVED AND REPLACED FWD GALLEY SLIDE ASSY PER MM 25-62-00. OK FOR SERVICE.

Part: LANYARD — FRAYED (R1 DOOR SLIDE) · airframe 55,175 hrs · 27,214 cycles

R1 DOOR SLIDE GIRT BAR CABLE IS FRAYING. REPLACED LANYARD ON R1 DOOR. CHECKED OK IAW AMM 25-62-00. THE AIRCRAFT WAS GROUNDED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 54,927 hrs · 27,055 cycles

FORWARD GALLEY EMERGENCY LIGHT LENS FELL OFF. REPLACED EMERGENCY EXIT LENS IAW AMM 33-53-01.

Part: GUST LOCK — OUT OF ADJUST (L1 DOOR) · airframe 54,820 hrs · 26,988 cycles

L1 DOOR GUST LOCK WILL NOT ENGAGE WHEN DOOR OPENED. ADJUSTED L1 DOOR GUST LOCK AS PER AMM 52-11-00-501. OPS CHECKED GOOD. THE AIRCRAFT WAS NOT GROUNDED.

Part: LIGHT — BROKEN (CABIN) · airframe 54,802 hrs · 26,977 cycles

FWD DETACHABLE EMERGENCY LIGHT TOP LATCH BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-53-00. THE AIRCRAFT WAS NOT GROUNDED.

Part: FITTING — DETACHED (ZONE 800) · airframe 54,561 hrs · 26,827 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR CLIP IS DETACHED. REINSTALLED CLIP. OPERATIONAL CHECK GOOD.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 54,410 hrs · 26,732 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE PARTIALLY DISLODGED FROM COVER. SECURED SLIDE IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: NOT REPORTED — MALFUNCTIONED (BRAKE SYSTEM) · airframe 54,354 hrs · 26,691 cycles

AIRCRAFT WAS GROUNDED. AFTER PUSHBACK, AFTER BRAKE SET LEFT HYDRAULIC BRAKE PRESSURE WENT TO ZERO PRESSURE. AFTER PUMPS ARE TURNED ON AND OFF AGAIN, LEFT HYDRAULIC BRAKE PRESSURE BLEEDS DOWN QUICKLY. ACCOMPLISHED TASK IAW AMM 32-40-00-101. LEAK AND OPERATIONAL CHECK GOOD.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 54,354 hrs · 26,689 cycles

AIRCRAFT WAS GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE LANYARD WAS ATTACHED TO THE SLIDE COVER WHEN DOOR WAS OPENED RESULTING IN DAMAGE TO THE COVER AND SLIDE DEPLOYMENT. REMOVED AND REPLACED SLIDE IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (TEMP SENSOR) · airframe 53,262 hrs · 26,017 cycles

DURING CRUISE, THE NR 1 ENGINE OIL TEMPERATURE REACHED 184 DEGREEES. IAW THE APPLICABLE CHECKLIST. NR 1 ENGINE WAS SHUT DOWN. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND A WIRE PULLED FROM THE P1-812 CONNECTOR FOR THE OIL TEMPERATURE SENSOR. REPAIRED CONNECTOR IAW WDM 79-33-01. ACCOMPLISHED ENGINE RUN. SYSTEM CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,560 hrs · 25,583 cycles

AIRCRAFT WAS NOT GNDED. FWD EXTERIOR OVERWING EMER EXIT LIGHT FAILED TO TEST. R & R EMER BATTERY ASSEMBLY B5-103 IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,560 hrs · 25,583 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS BETWEEN ROWS 27 AND 32 FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY ASSEMBLY B5-107 IAW AMM 33-53-00.

Part: FUEL CONTROL — LEAKING (APU) · airframe 51,911 hrs · 25,162 cycles

AIRCRAFT WAS GNDED. DISTINCT JET FUEL ODOR IN COCKPIT & CABIN WHEN APU BLEED AIR IS SELECTED TO ON. ACCOMPLISHED TROUBLESHOOTING IAW WC 21-96-01. FOUND FUEL LEAK AT APU FUEL CONTROL DRAIN SHROUD. R & R APU FUEL CONTROL UNIT IAW AMM 49-30-01. OPERATIONAL & LEAK CHECKED GOOD.

Part: MODULE — FAULTY (FUEL SYSTEM) · airframe 51,503 hrs · 24,903 cycles

CENTER FUEL TANK NO FEED, QRH FOLLOWED. FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. CTR TANK AFT BOOST PUMP WAS DEFERRED IAW MEL PROCEDURES. REPLACED RAM FOR AFT CTR FUEL PUMP. OPERATIONS CHECKED NORMAL IAW AMM 28-20-28. THE ACFT WAS NOT GNDED. SEE ALSO SDR AALA 20151118001.

Part: UFI — FAULTY (FUEL SYSTEM) · airframe 51,503 hrs · 24,903 cycles

CENTER FUEL TANK NO FEED. QRH FOLLOWED, FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. CTR TANK AFT BOOST PUMP WAS DEFERRED IAW MEL PROCEDURES. REPLACED UFI FOR AFT CTR FUEL PUMP. OPERATIONS CHECKED NORMAL IAW AMM 28-20-28. THE ACFT WAS GNDED. SEE ALSO SDR AALA 20160505005.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 51,479 hrs · 24,882 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB CTR TANK LOW FUEL PRESS LIGHT ILLUMINATED. CREW CONFIRMED CTR TANK NOT FEEDING. FOUND UFI FAULTED AFT CTR PUMP, TROUBLE SHOT IAW AMM 28-20-28. PLACARD APPLIED. FURTHER TROUBLESHOOTING FOUND NO FAULTS ON UFIS. PERFORMED OPERATIONAL TEST OF CTR TANK LOW PRESS INDICATION IAW AMM 28-41-00-501. SYS CHECKED NORMAL.

Part: RELAY — FAULTY (FUEL SYSTEM) · airframe 50,373 hrs · 24,247 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, CTR FUEL TANK BOOST PUMP BECAME INOPERATIVE. R & R UNIVERSAL FAULT INTERRUPTER RELAY TOP ASSEMBLY FOR CTR FUEL PUMP IAW AMM 28-20-28. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,117 hrs · 24,096 cycles

AFT CARGO DOOR, FWD LOWER DOOR STOP FITTING IS CRACKED. INSTALLED NEW STOP PAD FITTING IAW AARD 51-00-05-1, DWG 5910141 & CDK 2345.

Part: PAN — CORRODED (BS 390-393) · airframe 50,117 hrs · 24,096 cycles

FORWARD CARGO DOOR CUT OUT CORRODED BETWEEN LOWER PAN & SKIN BETWEEN BS 390 - 393. R & R LOWER PAN IAW SRM 53-05-00-001.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 50,117 hrs · 24,096 cycles

CRACKED SUPPORT ON FWD CARGO DOOR. INSTALLED NEW STOP PAD FITTING IAW AARD 51-00-05-1, AMM 52-31-00-5 & DWG 5910141.

Part: PUMP — FAULTY (FUEL BOOST) · airframe 50,086 hrs · 24,076 cycles

DURING CLIMB CREW NOTED THE FUEL FROM THE CTR TANK WAS NOT BEING USED & THE WING TANKS WERE IN USE. EMERGENCY DECLARED, RETURNED TO DEPARTURE, AND LANDED UNEVENTFULLY. R & R CTR AFT BOOST PUMP IAW AMM 28-20-07-201. SYS CHECKED NORMAL IAW AMM 28-20-07.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 50,036 hrs · 24,046 cycles

FOUND CRACK AT INSPECTION HOLE 3430A RT SIDE ON HORIZONTAL STABILIZER. INSTALLED REPAIR DOUBLER IAW EA COMP-55-039328 DATED 04 07 15.

Part: FORMER — CRACKED (RT WING) · airframe 50,036 hrs · 24,046 cycles

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

Part: CONNECTOR — DAMAGED (RADIO ALTIMETER) · airframe 49,305 hrs · 23,650 cycles

AIR INTERRUPT, RETURNED, DURING DESCENT RADAR ALTIMETER FAILED. DUE TO WEATHER MINIMUMS CREW RETURNED. REMOVED NR 1 RADIO ALTIMETER RECEIVER ANTENNA & FOUND CONNECTOR DAMAGED. R & R CONNECTOR IAW SWPM 20-32-02 & REPLACED ANTENNA IAW AMM 34-42-01. PERFORMED CHECK OF NR 1 RADIO ALTIMETER IAW AMM 34-42-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — WEAK (CABIN) · airframe 49,128 hrs · 23,542 cycles

LEFT OVERWING EXIT IDENTIFIER DIM ON TEST. R & R BATTERY PACK. SYS CHECKED NORMAL.

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 48,332 hrs · 23,110 cycles

LEFT AFT SERVICE DOOR SKIN AT GUST LOCK CRACKED. INSTALLED DOUBLER IAW SRM 52-05-00.

Part: PUMP — SEIZED (FUEL SYSTEM) · airframe 46,817 hrs · 22,343 cycles

TUL INFLIGHT OMA-DFW. CREW REPORTED AFT CTR TANK FUEL BOOST PUMP CIRCUIT BREAKER J21 POPPED OUT ON CLIMB OUT. FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PUMP IMPELLER SEIZED. REPLACED CTR AFT FUEL BOOST PUMP. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

CUSP SHEET CRACKED OTBD NR 2 SEAT TRACK FORWARD OF STATION 905 LT. INSTALLED DOUBLER AT STATION 905 IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CABIN NR 5 SEAT TRACK CORRODED FROM STATIONS 200 TO 246. INSTALLED SEAT TRACK SPLICE REPAIR IAW SRM 53-05-00 FIGURE 4F.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

SEAT TRACK SUPPORT CRACKED BELOW NR 2 SEAT TRACK AT STATION 886. INSTALLED NEW SERVICEABLE TRACK SUPPORT.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

CABIN SEAT TRACK SUPPORT BRACKET BELOW SEAT TRACK NR 2 AT STATION 905 CRACKED. INSTALLED NEW SERVICEABLE SEAT TRACK BRACKET BELOW NR 2 SEAT TRACK AT STATION 905 IAW AARD 51-00-05-1.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

CABIN CTR TANK TO FLOOR BEAM SUPPORT T CRACKED AT STATION 905 UNDER SEAT TRACK NR 2. INSTALLED NEW SERVICEABLE FLOORBOARD SUPPORT BRACKET IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON RT HAND CUSP SHEET FROM STATIONS 920 TO 921. INSTALLED NEW CUSP SHEET FROM STATIONS 905 TO 946 IAW AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON CUSP T ANGLE. INSTALLED REPAIR DOUBLER.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

RT CUSP IS CRACKED FROM STATIONS 218 TO 237 BELOW NR 6 SEAT TRACK. INSTALLED NEW CUSP SHEET FROM STATIONS 218 TO 237 RT.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

DAMAGE TO SUBFLOOR FROM STATIONS 200 TO 218. INSTALLED DOUBLER.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

CABIN SEAT TRACK SUPPORT BRACKET CRACKED BELOW SEAT TRACK NR 3 AT STATION 826. INSTALLED CABIN SEAT TRACK SUPPORT BRACKET IAW AARD 51-00-05-1, BOEING PRINT 5930561-505 & DRAWING 9936634-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON SUBFLOOR FROM STATIONS 200 TO 218. REPLACE SECTION ON SUBFLOOR.

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

EE BAY, STATION 180 & LONGERON 29 RT HAS DAMAGED GUSSET. INSTALLED NEW GUSSET IAW AARD 51-00-00-1, DRAWING PL2913044 & SRM 51-01-00.

Part: ATTACH ANGLE — DAMAGED (VERTICAL STAB) · airframe 46,807 hrs · 22,334 cycles

RT HAND INTERNAL VERTICAL STAB ATTACH ANGLE CRACKED AT 1427. INSTALLED NEW ANGLE IAW SRM 55-02-00 & AARD 51-00-05-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

FUSELAGE SKIN CRACKED AT FASTENER STATION 1418 BETWEEN LONGERONS 2 & 3 RT. INSTALLED FILLER INTERNAL & EXTERNAL DOUBLER IAW SRM 53-04-00 FIGURE 40 SHEET 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

SEAT TRACK NR 6 AT STATION 1214 CORRODED. INSTALLED PLUG IAW SRM 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON LT HAND CUSP FROM STATIONS 474 TO 478. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

GALLEY MOUNT FWD END OF NR 6 SEAT TRACK CORRODED. REPLACED GALLEY MOUNT IAW AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

CANT 1510 CRACKED AT TAIL CONE ALIGNMENT PIN AT THE 3 O CLOCK POSITION. INSTALLED REPAIR DOUBLER IAW EA MD80-53-032880.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

FUSELAGE SKIN CRACKED AT FASTENER STATION 1418 BETWEEN LONGERONS 2 & 3 LT. INSTALLED FILLER, INTERNAL DOUBLER & EXTERNAL DOUBLER IAW SRM 53-04-00 FIGURE 40 SHEET 1.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

HEAVY CABIN SEAT TRACK SUPPORT BRACKET CRACKED BELOW SEAT TRACK NR 2 AT STATION 927. INSTALLED SEAT TRACK SUPPORT FITTING IAW AARD 51-00-05-1 & DRAWING 9936637.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

SEAT TRACK AT STATION 80 CORRODED. REPLACED SEAT TRACK IAW AARD 53-20-00-10.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

CRACK IN FUSELAGE SKIN AT STATION 1474 & LONGERON 23 RT. INSTALLED REPAIR DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET 3.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

INTERCOSTAL CRACKED AT CTR LINE FROM STATIONS 1287 TO 1309. INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 46,807 hrs · 22,334 cycles

NR 3 SEAT TRACK CORRODED FROM STATIONS 200 TO 265. SPLICE IN NEW SECTION IAW SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON SEAT TRACK NR 4 FROM STATIONS 200 TO 265. INSTALLED SPLICE REPAIR IAW SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON NR 3 SEAT TRACK FROM STATIONS 1098 TO 1103. CORROSION WAS ROUTED OUT & PLUG REPAIR INSTALLED IAW SRA 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

LT HAND CUSP FROM STATIONS 474 TO 478 CORRODED. CORROSION WAS CUT OUT & DOUBLER INSTALLED IAW AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

SUBFLOOR CORRODED UNDER G 1 GALLEY DRAIN PAN FROM STATIONS 148 TO 160. CORROSION WAS CUT OUT & DOUBLER WAS INSTALLED IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

SEAT TRACK NR 6 CORRODED AT STATION 1214. CORROSION WAS ROUTED OUT & PLUG REPAIR INSTALLED IAW SRM 53-05-00 FIGURE 4A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON LT HAND CUSP SUBFLOOR UNDER AFT SERVICE DOOR GIRT BAR SUPPORT FITTING. CORROSION WAS CUT OUT & DOUBLER INSTALLED IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

G 2 GALLEY FWD INBD TIE DOWN MOUNT CORRODED AT STATION 210. DAMAGED MOUNT WAS R & R WITH NEW SERVICEABLE MOUNT IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

CORROSION ON RT HAND CUSP FROM STATIONS 500 TO 503. DAMAGE WAS REMOVED & DOUBLER INSTALLED IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON NR 1 SEAT TRACK AT STATION 380. CORRODED AREA ROUTED OUT & SEAT TRACK PLUG INSTALLED IAW AARD 53-20-00-10.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,807 hrs · 22,334 cycles

RT HAND WINDOW RING PAN BETWEEN STATIONS 886 TO 905 CRACKED IN TOP FWD CORNER. DAMAGE WAS REMOVED & DOUBLER WAS INSTALLED IAW AARD 53-10-00-25.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON LT HAND TIE DOWN TRACK FROM STATIONS 1187 TO 1212. REPLACED TIE DOWN TRACK IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CUSP WAS CORRODED AT STATION 378. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON RT HAND AFT CARGO TIE DOWN TRACK FROM STATIONS 1212 TO 1322. INSTALLED NEW TIE DOWN TRACK IAW AARD 51-00-05-1.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,807 hrs · 22,334 cycles

CORROSION ON LT HAND AFT CARGO TIE DOWN TRACK FROM STATIONS 1212 TO 1322. REPLACED TIE DOWN TRACK IAW AARD 51-00-05-1.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 43,629 hrs · 20,629 cycles

EMERGENCY ESCAPE PATH MARKING LIGHT ON SEAT 22D INOPERATIVE. RECONNECTED SEAT CONNECTOR. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,399 hrs · 19,505 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK AT ROW 28. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,399 hrs · 19,505 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK AT ROW 08. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,688 hrs · 19,183 cycles

DAMAGE FOUND AT FORWARD PASSENGER DOOR FUSELAGE SKIN DOOR HOLD OPEN CUTOUT. ACCOMPLISHED DOUBLER REPAIR EA MD80-019392 AND MD80 SRM 53-04-00 FIGURE 24 REF TO BOW FMR/002 S/N 1678214 DATED 9-23-11.

Part: AUGMENT VALVE — INOPERATIVE (ZONE 400) · airframe 40,453 hrs · 19,053 cycles

ABQ - INFLIGHT PHX-DFW. CREW REPORTED WHILE IN CRUISE, SELECTED ENGINE ANTI ICE ON AND ELECTRICAL ODOR WAS NOTICED IN THE COCKPIT AND CABIN. ENGINE ANTI ICE WAS TURNED OFF AND THE ODOR DISSIPATED. SHORTLY THERE AFTER, COMPRESSOR STALLS WERE EXPERIENCED ON BOTH RIGHT AND LEFT ENGINES. EMERGENCY DECLARED FLIGHT DIVERTED ABQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AUGMENTATION VALVE AND THERMAL SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — BROKEN (CABIN) · airframe 39,575 hrs · 18,624 cycles

SEAT 12DEF EMERGENCY LIGHT SHROUD BROKEN. REPLACED SEAT 12DEF EMERGENCY LIGHT SHROUD. OPS CHECK NORMAL.

Part: FRAME — WORN (FUSELAGE) · airframe 39,146 hrs · 18,413 cycles

TEMP CONTROL VALVE WEARING INTO FRAME 1380. INSTALLED DOUBLER PER AARD 53-10-00-28.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,375 hrs · 16,673 cycles

EMERGENCY LIGHT AT OVER WING INOPERATIVE. REPLACED BATTERY PACK.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,909 hrs · 16,487 cycles

AFT DOOR BEAM AT STATION 1155 TO 1212, STRINGER 28 RIGHT CORRODED. REPAIRED DOUBLER UNDER AARD 53-10-00-3.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,909 hrs · 16,487 cycles

AFT CARGO DOOR BEAM CORRODED. REPAIRED UNDER AARD 53-10-00-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

AFT ACCESSORY 1418 FRAME CRACKED AT LONGERON 2 LEFT TO 2 RIGHT. INSTALLED DOUBLER IAW 53-11-04.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

FUEL LEAKING FROM RIGHT BATH TUB FITTING BOTTOM OF CENTER TANK STATION 890. INSTALLED 2 EACH BATH TUB FITTINGS UNDER SRM 51-30-05.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

AFT CARGO DOOR OPENING AFT SIDE HAS DAMAGE. INSTALLED EXTERNAL DOUBLER REPAIR UNDER AARD 53-30-00.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,909 hrs · 16,487 cycles

CORROSION ON FUSELAGE SKIN AT LONGERON 28 RIGHT. REMOVED AND INSTALLED DOUBLER IAW SRM 53-04-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,909 hrs · 16,487 cycles

CORROSION ON SEAT TRACK NUMBER 6 STATION 792 BEYOND LIMITS. INSTALLED SPLICE UNDER SRM 51-30-01.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

STATIC PORT MOUNT HOLES FOR DOUBLER ARE NOT SYMMETRICAL. INSTALLED DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

DENT ON FUSELAGE SKIN STATION 222. INSTALLED REPAIR UNDER SRM 53-04-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

CRACK IN FRAME 1418 AT LONGERON 2 RIGHT. REPAIR DOUBLER INSTALLED UNDER SRM 53-03-00.

Part: BRACKET — CRACKED (DOOR) · airframe 34,909 hrs · 16,487 cycles

AFT VAULT DOOR UPPER BAYONET LATCH BRACKET CRACKED. REMOVED AND REPLACED BAYONET LATCH BRACKET PER ESO80186.

Part: FLAP — DAMAGED (TE FLAP) · airframe 34,909 hrs · 16,487 cycles

SMMR TUL 9457 - AN INTERIM REPAIR WAS MADE ON A STATIC DISCHARGE HOLE ON THE EXTENDED EDGE LIMIT OF THE LEFT INBOARD FLAP PER SMMR TUL9457. ATBT 15JAN/TUL AT NEXT HEAVY C CHECK MAKE PERMANENT REPAIR OF LEFT INBOARD FLAP. REMOVED AND REPLACED TRAILING EDGE UNDER ESO 80095.

Part: SKIN — DAMAGED (TE FLAP) · airframe 34,909 hrs · 16,487 cycles

STATIC DISCHARGE DAMAGE ON LOWER SKIN 14.5 INCHES FROM TRAILING EDGE. DAMAGE WAS REMOVED AND DOUBLER WAS INSTALLED PER SRM 57-01-00 FIG 5 SHEET 1.

Part: ANGLE — CRACKED (CARGO DOOOR) · airframe 34,909 hrs · 16,487 cycles

MID CARGO DOOR, AFT LOWER STOP FITTING T-ANGLE CRACKED BETWEEN HI-LOKS. REPLACED FORMER.

Part: SKIN — DAMAGED (TE FLAP) · airframe 34,909 hrs · 16,487 cycles

STATIC DISCHARGE DAMAGE LOCATED 25 INCHES FROM INBOARD END AND 4.5 INCHES FROM TRAILING EDGE. INSTALLED PERMANENT REPAIR DOUBLER PER SRM 57-01-00 FIGURE 5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

DENT ON FUSELAGE 20 INCHES AFT OF FORWARD LAVATORY SERVICE PANEL. INSTALLED INTERNAL DOUBLER REPAIR UNDER SRM 53-04-02.

Part: HOUSING — GOUGED (SERVICE DOOR) · airframe 34,909 hrs · 16,487 cycles

AFT SERVICE DOOR OUTER HANDLE PAN HAS DEEP GOUGE. REMOVED AND REPLACED HANDLE PAN (HOUSING) PER ESO 80175.

Part: SKIN — DENTED (ENTRY DOOR) · airframe 34,909 hrs · 16,487 cycles

FORWARD ENTRY DOOR SKIN HAS IMPROPERLY INSTALLED RIVETS AND DEEP SKIN DENTS AT NUMBER 1 BEAM AFT END. REMOVED RIVETS, REWORKED SKIN, INSTALLED INTERNAL DOUBLER, AND REPLACED FASTENERS UNDER SRM 53-04-00 FIG 31.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 34,909 hrs · 16,487 cycles

MID CARGO DOOR FORWARD UPPER STOP FITTING T-ANGLE NEXT TO OUTER SKIN CRACKED IN RADIUS. REPLACED CRACKED T-ANGLE AT FORWARD UPPER STOP FITTING UNDER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

CRACK IN WINDOW PAN AT STATION 1211 LONGERON 12 RIGHT. INSTALLED WINDOW PAN DOUBLER UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

CRACK IN WINDOW PAN STATION 947 LONGERON 12 RIGHT. INSTALLED DOUBLER UNDER AARD 53-10-00-75.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

WINDOW PAN IS CRACKED AT STATION 1098 RIGHT. REPAIRED UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

WINDOW PAN IS CRACKED AT STATION 1021 RIGHT. REPAIRED UNDER AARD 53-10-00-25.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,909 hrs · 16,487 cycles

MID CARGO DOOR BEAM CORRODED ON VERTICAL LEG. REMOVED CORROSION AND INSTALLED DOUBLER IAW AARD 53-10-00-3.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

WINDOW PAN IS CRACKED AT STATION 1060. INSTALLED DOUBLER UNDER AARD 53-10-00-28.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

WINDOW PAN IS CRACKED AT STATION 1021 LEFT. REPAIRED UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

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

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

WINDOW PAN IS CRACKED AT STATION 947 LEFT. REPAIRED UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

WINDOW PAN CRACKED AT STATION 1060 RIGHT. INSTALLED REPAIR DOUBLER UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,909 hrs · 16,487 cycles

WINDOW PAN CRACKED AT STATION 1022 LEFT. INSTALLED DOUBLER UNDER AARD 53-40-00-25.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 32,617 hrs

DFW INFLIGHT - RIGHT MAIN LANDING GEAR RED LIGHT ON WITH GEAR UP. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC FLEX LINE FOR RIGHT MAIN LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL- EMERGENCY LIGHTS AT CABIN OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK AT STATION 875 FOR EMERGENCY LIGHTS AT CABIN OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - FORWARD RIGHT HAND EMERGENCY EXIT DOOR SIGN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD RIGHT HAND EMERGENCY EXIT DOOR SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS FROM THE FRONT OF THE AIRCRAFT TO ROW 19 INOPERATIVE. REPLACED BATTERY PACK 2 EACH AND CHARGING MODULES 2 EA IN RIGHT HAND OVERHEAD BIN AT ROW 20 AND REPAIRED CHAFED WIRE IN RIGHT HAND SIDEWALL GRILL FOR SEAT MOUNTED EMERGENCY LIGHTS FROM THE FRONT OF THE AIRCRAFT TO ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY)

AUS - INFLIGHT CREW REPORTED SMOKE IN FIRST CLASS GALLEY. FOUND NUMBER ONE OVEN DIRTY AND SMOKING AROUND HEATER ELEMENT. STEAM CLEANED NUMBER ONE OVEN. RAN OVEN ONE HOUR AND CLEANED ELEMENTS AND INTERIOR OF OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACTOR — DEFECTIVE (CABIN)

DFW - EMERGENCY DIRECTIONAL LIGHT MOUNTED ON FORWARD GALLEY WALL INOPERATIVE. REPINNED QUICK DISCONNECT CONTACT FOR EMERGENCY LIGHT MOUNTED ON FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RDU - EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW EMERGENCY ESCAPE PATH LIGHT MARKER AT FORWARD GALLEY WALL EXIT INOPERATIVE. RECONNECTED THE CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHT AT THE FORWARD GALLEY WALL EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER B5 23 FOR COCKPIT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROW 12DEF. RECONNECTED CONNECTOR AT SEAT 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, FORWARD TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 15,695 hrs · 8,048 cycles

THE EGRESS LIGHT WAS INOPERATIVE AT ROW 12, 13, 21 AND ROWS 27 TO 30. REPLACED THE LAMP (P/N 7732) AT ROW 12, 13, AND 21. RECONNECTED LOOSE CONNECTOR AT ROW 31 FOR ROW 27 TO 30. CHECK-C 10-30-02 STL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,594 hrs · 7,997 cycles

BOTH AFT OVERWING EXIT LIGHTS AND THE EGRESS LIGHT AT ROW 15 WERE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK 60-1177-9LB, AND THE LAMP FOR THE EGRESS LIGHT P/N 7732. CHECK-C 10-30-02 STL.

Part: HARNESS · airframe 15,381 hrs · 7,873 cycles

DURING OVERNIGHT INSPECTION SIX WHITE AND ONE RED EGRESS FLOOR LIGHT INOP ON CABIN FLOOR. REPLACED BROKEN HARNESS 105606-003 CPN 4096971 BETWEEN ROW 24 AND 25 ALSO SEATED BULBS INTO SOCKETS AS REQUIRED. OPS CHEK NORMAL PER MD80 MM33-53-01. CHECK-C MCI 10-30-02. --CLOSED--

Part: LAMP — BURNED OUT · airframe 14,904 hrs · 7,577 cycles

EGRESS LIGHTING INOP BETWEEN ROWS 21 AND 28. RELAMPED SECTION OF LIGHTS. LAST CHECK C PERFORMED IN STL 10/30/2002 --CLOSED--

Part: TEE CHORD — DAMAGED (FUSELAGE) · airframe 14,070 hrs · 7,048 cycles

DURING CHECK-C BULKHEAD CHORD DAMAGED FUSELAGE STATION 110 LONGERON 27R AND 28R AND TEE CHANNEL AFT SIDE OF BULKHEAD. COLD WORKED TEE CHORD NDT INSPECTED PER ARA 18213 ITEM 3 SHOT PEENED, NO CRACK FOUND PER 6-51-00-03.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 14,070 hrs · 7,048 cycles

DURING CHECK-C TEE CHANNEL BELOW LONGERON 28R FUSELAGE STATION 110 TO APPROX FUSELAGE STATION 129 DAMAGED. REPLACED TEE CHANNEL 9911597-502 AND SEAL PER ARA18213.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 14,070 hrs · 7,048 cycles

DURING CHECK-C, SKIN DAMAGED FUSELAGE STATION 110 TO APPROX FUSELAGE STATION 129 LONGERON 28 RIGHT TO LONGERON 27 RIGHT. REPAIRED SKIN DAMAGE FS 110 TO APPROX FS 129 L28R-L27R PER ARA18213 AND SRM 53-02. NO CRACKS FOUND PER PART 6-51-00-03.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 14,070 hrs · 7,048 cycles

DURING CHECK-C LONGERON 28R DAMAGED AT FUSELAGE STATION 110 TO FUSELAGE STATION 129. REPAIRED LONGERON 28A FUSELAGE STATION 110 TO FUSELAGE STATION 129 PER SRM 53-02 FIG 18. NO CRACKS FOUND PART 6-51-00-03.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 12,477 hrs · 6,069 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1221 TO 1332, THE LT FLOOR TRACK HAD CORROSION AROUND NUT PLATE HOLES IN SEVERAL LOCATIONS. INSTALLED NEW TRACK AND FASTENERS PER PRINT 5936663-503, AND SRM 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 12,477 hrs · 6,069 cycles

DURING CHECK-C MAINT THE AFT CARGO BIN, LT FLOOR TRACK HAD CORROSION AROUND NUT PLATE HOLES IN SEVERAL LOCATIONS, STA 1218 TO 1221. INSTALLED NEW TRACK AND FASTENERS PER PRINT 5936663-503, AND SRM 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 12,477 hrs · 6,069 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT FLOOR TRACK WAS CORRODED AROUND NUT PLATE HOLES IN SEVERAL LOCATIONS, STA 1211 TO 1322. MADE AND INSTALLED NEW CARGO TRACK PER SPM 6-70-01, PAGE 3, AND DOUGLAS PRINT 5936663.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 12,477 hrs · 6,069 cycles

DURING CHECK-C MAINT, THE LT WHEEL WELL, AFT FRAME FOR GEAR DOOR INBOARD SUPPORT BRACKET HAD CRACKED. REPLACED SUPPORT ANGLE PER DOUGLAS DRAWING 5936395.

Part: LIGHT — MISSING (CABIN) · airframe 10,476 hrs · 5,118 cycles

THE EGRESS LIGHTING SYSTEM WAS MISSING A PIECE AT ROW 23. INSTALLED LIGHT, (P/N 81000-22701ATS), AND REPLACED BATTERY CELL, (P/N 408822-101). CHECK-C 1-8-01 JFK.

Part: ACM — FAILED (LEFT)

ON TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT FROM THE LEFT AIR CONDITIONING PACK. PLACARDED THE PACK INOPERATIVE PER MEL. THE LT AIR CYCLE MACHINE WAS LATER REPLACED DUE TO LEAKAGE. CHECK-C 10-13-98 STL.

Part: COALESCER BAG — DIRTY (CABIN)

ON TAKEOFF CABIN FILLED WITH SMOKE. FLIGHT RETURNED TO DTW. FOUND SMOKE COMING FROM APU AIR SYSTEM. PLACARD THE APU AIR INOPERATIVE PER MEL. CHECK-C 10-31-98 STL. *S/D* NO APU OIL LEAKS WERE FOUND. REPLACED THE WATER SEPARATOR BAGS AND ACCOMPLISHED DUCT BURN OUT PROCEDURES.

Part: SOCKET — FAILED (CABIN)

STL - FLT 572 - ELECTRICAL FUMES AND SMOKE CAME FROM SIDE WALL LIGHT AREA ABOVE CABIN ROW 5, RT SEATS. ON LANDING SIDE WALL LIGHTS FLICKERED THEN WENT OUT. REPLACED LIGHT SOCKET AT FWD FLOURESCENT LAMP, AFT POSITION, AND REPLACED LIGHT BALLAST. BALLAST MFG B6-15. (M)

Part: BALLAST — FAILED (CABIN)

STL - FLT 572 - ELECTRICAL FUMES AND SMOKE CAME FROM SIDE WALL LIGHT AREA ABOVE CABIN ROW 5, RT SEATS. ON LANDING SIDE WALL LIGHTS FLICKERED THEN WENT OUT. REPLACED LIGHT SOCKET AT FWD FLOURESCENT LAMP, AFT POSITION, AND REPLACED LIGHT BALLAST. BALLAST MFG B6-15. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

ABQ - FLT 649 - STRONG ELECTRICAL BURNING SMELL IN AREA OF CABIN ROW 5, ABOVE RT SEATS. REMOVED PANELS AND THOROUGHLY INSPECTED AREA FROM ROW 1 THROUGH 8. NO DEFECT NOTED. (M)

Part: MOTOR — WORN (HORIZ STAB)

STL - FLT 263 - PRIMARY LONGITUDINAL TRIM FAILED. FLIGHT RETURNED TO STL. REPLACED PRIMARY TRIM MOTOR. (X)