N9626F

Part: LANYARD — LOOSE (GIRT BAR) · airframe 54,923 hrs · 27,278 cycles

FORWARD SERVICE DOOR SLIDE DETACHED. FOUND GIRT BAR LANYARD LOOSE FROM COVER ACCOMPLISHED MONITOR AND CHALLENGE CARD 10151-3, REINSTALLED SLIDE PACK AND GIRT BAR LANYARD PER AMM 25-62-00, AT R-1 DOOR, CHECKS NORMAL.

Part: VALVE — FAULTED (PNEUMATIC SYS) · airframe 54,424 hrs · 26,959 cycles

AT APPROXIMATELYH 10,000 FT, THE TAIL COMP TEMP HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO DEPARTURE. LANDED NORMALLY. THE AIRCRAFT REMOVED FROM SERVICE. REPLACED THE LEFT PNEUMATIC AUGMENTATION VALVEIAW AMM 36-10-01.

Part: DUCT — FAULTY (PNEUMATIC SYS) · airframe 54,424 hrs · 26,859 cycles

AT APPROXIMATELYH 10,000FT, TAIL COMP TEMP HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO DEPARTURE. LANDED NORMALLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE DUCT ASSEMBELY IAW AMM 20-10-11.

Part: CONNECTOR — NOT REPORTED (AIR CON SYS) · airframe 54,422 hrs · 26,955 cycles

AT APPROXIMATELY 10,000 FT, THE TAIL COMP TEMP HIGH LIGHT ILLUMINATED. MEMORY ITEMS AND EXPANDED QRH CHECKLIST COMPLIED WITH. RETURNED TO DEPARTURE. ARFF SHOT TAIL WITH NORMAL TEMPERATURE. THE AIRCRAFT WAS GROUNDED. REPLACED GROUND AIR CONDITIONING CONNECTER IAW AMM 21-20-08.

Part: THERMOSTAT — FAULTY (A/C PACK) · airframe 54,422 hrs · 26,955 cycles

AT APPROXIMATELY 10,000 FT TAIL COMP TEMP HIGH LIGHT ILLUMINATED. MEMORY ITEMS AND EXPANDED QRH CHECKLIST COMPLIED WITH, RETURNED TO DEPARTURE. ARFF SHOT TAIL WITH NORMAL TEMPERATURE. REPLACED THE LEFT PNEUMATIC AIR CONDITIONING CONTROL THERMOSTAT IAW AMM 21-61-07. AIRCRAFT WAS GROUNDED.

Part: DUCT — LEAKING (RT A/C PACK) · airframe 54,422 hrs · 26,955 cycles

AT APPROXIMATELY 10,000 FT TAIL COMP TEMP HIGH LIGHT ILLUMINATED. MEMORY ITEMS AND EXPANDED QRH CHECKLIST COMPLIED WITH. RETURNED TO DEPARTURE FF SHOT TAIL WITH NORMAL TEMPERATURE. SUPPLY DUCT REPLACED. THE RIGHT PACK SUPPLY DUCT LEAKED CHECK GOOD IAW AMM 36-00-00. THE AIRCRAFT WAS GROUNDED.

Part: DUCT — LEAKING (RT A/C PACK) · airframe 54,422 hrs · 26,955 cycles

AT APPROXIMATELY 10,000 FT, TAIL COMP TEMP HIGH LIGHT ILLUMINATED. MEMORY ITEMS AND EXPANDED QRH CHECKLIST COMPLIED WITH. RETURNED TO DEPARTURE. ARFF SHOT TAIL WITH NORMAL TEMPERATURE. INSTALLED A SERVICABLE SUPPLY DUCT FOR THE RT A/C PACK BETWEEN FLOW CONTROL VALVE AND HEAT EXCHANGER IAW 21-00-00. THE AIRCRAFT WAS GROUNDED.

Part: SENSOR — FAULTY (DUCT TEMP) · airframe 54,422 hrs · 26,955 cycles

AT APPROXIMATELY 10,000 FT, TAIL COMP TEMP HIGH LIGHT ILLUMINATED. MEMORY ITEMS AND EXPANDED QRH CHECKLIST COMPLIED WITH - RETURNED TO DFW - ARFF SHOT TAIL WITH NORMAL TEMPERATURE. REPLACED LEFT SUPPLY TEMPERATURE SENSOR IN NEW DUCT IAW AMM 21-61-04. AIRCRAFT WAS GROUNDED.

Part: GASKET — BLOWN (BLEED AIR SYS) · airframe 54,370 hrs · 26,922 cycles

AIRCRAFT WAS GROUNDED. TAIL COMPRESSOR TEMPERATURE HIGH ILLUMINATED IN FLIGHT, JUST PRIOR TO 10,000 FT. NO EMERGENCY DECLARED. THE FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND PNEUMATIC SUPPLY TEMP SENSOR GASKET BLOWN OUT. REPLACED GASKET PER AMM 36-10-00.

Part: WINDOW — HAZE (EMERGENCY EXIT) · airframe 54,207 hrs · 26,817 cycles

RIGHT FORWARD EMERGENCY EXIT DOOR WINDOW FOGGED. THE AIRCRAFT WAS GROUNDED. REPAIRED IAW SRM 56-30-00, PRESSURIZED AIRCRAFT, AND PERFORMED SATISFACTORY OPERATIONAL CHECK. NO LEAKS FOUND.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 54,038 hrs · 26,711 cycles

TOP FORWARD EDGE DOOR STOP BRACKET ON MID CARGO DOOR IS CRACKED. INSTALLED A NEW STOP PAD FITTING IAW 51-00-05-1, AND DRAWING 5910141.

Part: ATTACH ANGLE — CRACKED (BS 1437) · airframe 54,038 hrs · 26,711 cycles

CRACK INDICATION ON THE RIGHT VERTICAL ATTACH (SKATE) ANGLE AT BS 1437. REPLACED ATTACH ANGLE IAW SRM 53-05-00 AND 53-10-00.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,824 hrs · 26,561 cycles

THE AIRCRAFT WAS NOT GROUNDED. TAILCONE SLIDE EMERGENCY LIGHTS 2 UPPER LAMPS ARE INOPERATIVE. REPLACED BATTERY & CHARGER ASSEMBLY IAW AMM 33-53-00. OPS CHECKED OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,824 hrs · 26,561 cycles

SEAT 29D CEILING EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS IAW AMM 33-53-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,824 hrs · 26,560 cycles

SEAT 29D CEILING EMERGENCY LIGHT LENS MISSING. MAINTENANCE REPLACED THE LENS IAW AMM 33-53-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 53,726 hrs · 26,496 cycles

FORWARD SEAT MOUNTED EMERGENCY LIGHT HAD A LOW BATTERY, BS 243 OVERHEAD DROP DOWN PANEL. REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: SPRING — BROKEN (EMERGENCY EXIT) · airframe 53,107 hrs · 26,071 cycles

AIRCRAFT WAS GROUNDED. AFT PRESSURE BULKHEAD DOOR EMERGENCY EXIT MECHANISM SPRING IS BROKEN. REMOVED AND REPLACED SPRING PER AMM 53-53-02-201. OPERATIONAL CHECK GOOD.

Part: TERMINAL — DEFECTIVE (EMERGENCY LIGHT) · airframe 52,353 hrs · 25,594 cycles

SEAT 15D EMERGENCY LIGHT ON ISLE INOPERATIVE. REPLACED THE TERMINAL . OPS CHECKED GOOD IAW MM 33-60-98.

Part: B-NUT — LOOSE (LT ENGINE) · airframe 52,167 hrs · 25,477 cycles

THE AIRCRAFT WAS GROUNDED. LEFT ENGINE SLOW TO ACCELERATE ON TAKE OFF. THE N1 EVENTUALLY ACHIEVED 90%, BUT EPR REMAINED AT 1.20% AND NEVER REACHED 1.92% TAKE OFF POWER. TAKE OFF ABORTED BELOW 80 KNOTS, BRAKE TEMP NORMAL. EXAMINED LEFT ENGINE EPR SYSTEM IAW AMM 77-11-01. DISCOVERED LOSE CONNECTION ON PT7 MANIFOLD AT 9 O’CLOCK. SECURED B NUT. NO LEAKS NOTED. ACCOMPLISHED TAKEOFF POWER ASSURANCE CHECK IAW AMM 71-00-00. CHECKS GOOD. OK FOR SVC.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,983 hrs · 25,355 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AFT CABIN RIGHT JUMPSEAT NEAR TAILCONE IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,364 hrs · 24,950 cycles

EMERGENCY PORTABLE LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: WINDOW — DEFECTIVE (L1 DOOR) · airframe 51,216 hrs · 24,854 cycles

AIRCRAFT NOT GROUNDED. L1 DOOR WINDOW FOGGED UP INSIDE PREVENTING VERIFICATION OF SLIDE STRAP STATUS. REMOVED AND REPLACED WINDOW IAW AMM 56-30-00. LEAK AND OPERATIONAL CHECK GOOD.

Part: CONTROL BOX — FAULTY (ANTI SKID SYS) · airframe 51,022 hrs · 24,735 cycles

DURING FLIGHT ALL ANTI SKID INOPERATIVE LIGHTS ILLUMINATED THEN EXTINGUISED. EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACE THE ANIT SKID SYSTEM CONTROL BOX IAW AMM 32-43-04. SYSYTEM CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,783 hrs · 24,583 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CEILING MOUNTED EMERGENCY LIGHTS BETWEEN ROWS 7 AND 9 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY AT STATION 500 AN ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-53-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,259 hrs · 24,256 cycles

DURING ACCOMPLISHMENT OF WORK CARD 5403 EMERGENCY POWER SUPPLY AB5-4 FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK IAW AMM 33-60-98. OPERATIONAL TEST NORMAL.

Part: WATER SEPARATOR — CLOGGED (AC BAY) · airframe 49,818 hrs · 24,007 cycles

AIRCRAFT WAS GROUNDED, AIR INTERRUPT. EMERGENCY DECLARED. LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. AFTER TURNING OFF ANTI-ICE THE PRESSURIZATION FLOW LIGHT ILLUMINATED. IN MANUAL MODE, CABIN ALTITUDE CONTINUED TO INCREASE. CABIN PRESSURIZATION BECAME UNCONTROLLABLE. MAINTENANCE FOUND LT WATER SEPARATOR FREEZING UP AND LEAKING. R & R WATER SEPARATOR IAW AMM 21-20-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,095 hrs · 23,567 cycles

EMER LIGHTS ROWS 27 - 32 FAIL TO TEST. REPLACED B5-107 EMER LIGHT BATTERY POWER SUPPLY IAW AMM 33-53-00. TESTED OK. THE ACFT WAS NOT GNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,095 hrs · 23,567 cycles

EMER LIGHTS ROWS 12 - 17 FAIL TO TEST. REPLACED B5-102 EMER LIGHT BATTERY POWER SUPPLY IAW AMM 33-53-00, TESTED OK. THE ACFT WAS NOT GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,593 hrs · 23,271 cycles

AIRCRAFT WAS NOT GNDED. DURING TAXI FROM HANGAR 2 TO HANGAR 1, TAXI CREW REPORTED THAT THE CEILING EMER EXIT LIGHT OVER THE OVERWING EMER EXIT WILL NOT EXTINGUISH. R & R EMER LIGHT BATTERY PACK B5-104. OPERATIONAL CHECKED NORMAL IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,890 hrs · 22,844 cycles

AFT EPL LIGHTS VERY DIM WITH BATTERY PACK AB5-3 IN USE. R & R BATTERY PACK. AFT EPL LIGHTS OPERATIONALLY CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

FUSELAGE SKIN CRACKED UNDER RAIN GUTTER AT CANT FRAME, STATION 1471 - 1477, ON LOWER RT SIDE. REPAIRED SKIN IAW SRM 53-01-00-001.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,261 hrs · 22,445 cycles

CORROSION ON BOTTOM OF RT CUSP, STATION 424 TO 432. REMOVED & INSTALLED NEW CUSP SHEET FROM STATION 389 TO 503 IAW RD51-00-05-1 & DWG 9930538-75.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

FUSELAGE SKIN CRACKED AT STATION 1380 ABOVE LONGERON 14R. REPAIRED SKIN IAW SRM 53-01-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,261 hrs · 22,445 cycles

SEAT TRACK NR 4 IS CORRODED BETWEEN FS 1273 TO 1279. INSTALLED SPLICE & NEW SECTION OF SEAT TRACK IAW SRM 53-05-00 FIG 4F.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

CRACKED ANGLE AT L2L, AFT SIDE OF FS 1451. R & R ANGLE IAW AARD 53-10-00-2 & DWG 9911860.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

SUPPORT BRACKET BELOW SEAT TRACK 3 BETWEEN STATION 927 & 928 IS CRACKED AT LOWER END. R & R SUPPORT BRACKET IAW AARD 51-00-05-1 & DWG 9936634.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

SUPPORT BRACKET BELOW SEAT TRACK 3 BETWEEN STATION 886 & 887 IS CRACKED AT LOWER END. R & R SUPPORT BRACKET IAW AARD 51-00-05-1 & DWG 9936634.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

SUPPORT BRACKET BELOW SEAT TRACK 3 BETWEEN STATION 826 & 827 IS CRACKED AT LOWER END. R & R SUPPORT BRACKET IAW AARD 51-00-05-1 & DWG 9936634.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

SUPPORT BRACKET BELOW SEAT TRACK 4 BETWEEN STATION 886 & 887 IS CRACKED AT LOWER END. R & R SUPPORT BRACKET IAW AARD 51-00-05-1 & DWG 9936634.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,261 hrs · 22,445 cycles

RIGHT CUSP CORRODED AT STATION 674 TO 693. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

CRACKED INTERCOSTAL BETWEEN CABIN FLOORBEAMS BETWEEN STATIONS 1287 - 1309 AT BL 0. REPLACED INTERCOSTAL IAW AARD 51-00-00-1 & DWG 9936580.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,261 hrs · 22,445 cycles

LEFT CUSP AT STATION 845 IS CRACKED UNDER NR 1 SEAT TRACK. INSTALLED LT CUSP DOUBLER REPAIR AT STATION 845 IAW AARD 53-20-00-16.

Part: CASTING — CRACKED (LT SPOILER) · airframe 47,261 hrs · 22,445 cycles

LEFT WING GND SPOILER CASTING CRACK. REPLACED PART.

Part: CASTING — CRACKED (RT SPOILER) · airframe 47,261 hrs · 22,445 cycles

RIGHT WING GND SPOILER CASTING CRACK. REPLACED CASTING.

Part: FORMER — CRACKED (LT WING) · airframe 47,261 hrs · 22,445 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. STOP DRILLED CRACK & INSTALLED FORMER DOUBLER IAW WC 57-98-03.

Part: FORMER — CRACKED (RT WING) · airframe 47,261 hrs · 22,445 cycles

RIGHT WING LE EDGE NR 4 SLAT TRACK INBD FORMED IS CRACKED. STOP DRILLED CRACK & INSTALLED FORMER DOUBLER IAW WC 57-98-04.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 46,016 hrs · 21,767 cycles

PORTABLE EMER LIGHT AT FWD CABIN DOOR INOPERATIVE. REPLACED PORTABLE EMER LIGHT IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,016 hrs · 21,767 cycles

AFT EMER PATH LIGHTING INOPERATIVE DURING DUAL FEED CHECK USING AB5-1 & AB5-4. R & R BATTERY IN PACK AB5-4 IAW 33-60-98. SYS CHECKED NORMAL.

Part: SKIN — DAMAGED (THRUST REVERSER) · airframe 44,873 hrs · 21,170 cycles

DAMAGE TO THE LT THRUST REVERSER LOWER DOOR LE SKIN. ACCOMPLISHED REPAIR TO LT LOWER THRUST REVERSER IAW FEA 17292.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,682 hrs · 20,617 cycles

CRACK IN WEB AT LOWER RT GUIDE PIN FOR RADOME. REMOVED DAMAGE FABRICATED FILLER & DOUBLER IAW AARD 53-10-00-19.

Part: DUCT — CRACKED (NR 1 ENGINE) · airframe 43,629 hrs · 20,589 cycles

STL INFLIGHT AUS-ORD. CREW REPORTED LEFT ENGINE OIL PRESSURE LOSS. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND 6 INCH BY 2 INCH SECTION OF FWD INTER DUCT SEGMENT CRACKED AT 9 O`CLOCK POSITION ON NR 1 ENG. REPLACED NR 1 ENG AT STL ON 01/06/2014. SYSTEM GND CHECKED NORMAL OPERATION OPEN.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 43,182 hrs · 20,366 cycles

ATL INFLIGHT TPA-ORD. RT GENERATOR FAILED & AUXILIARY POWER UNIT WOULD NOT START. EMERGENCY DECLARED FLIGHT DIVERTED ATL LANDED WITHOUT INCIDENT. PLACARDED RT ENG GENERATOR INOPERATIVE IAW MEL 24-1B AUTH 11-488DC-B. FLIGHT CONTINUED TO DESTINATION. REPLACED RT ENG GENERATOR AT DFW ON 11/09/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 41,028 hrs · 19,225 cycles

EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REMOVED AND REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,523 hrs · 17,009 cycles

MULTIPLE EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,523 hrs · 17,009 cycles

MULTIPLE EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK ON FOR MID CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

STATION 1463 FRAME WEB NEAR LONGERON 3 LEFT DAMAGED. DOUBLER INSTALLED PER EA MD80-53-15174.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

FRAME 1437 RIGHT SHEAR CLIP CRACKED AT LONGERON 1 RIGHT. INSTALLED NEW SHEAR CLIP PER AARD 51-10-00-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

AFT ACCY LONGERON 1 AT CANT FRAME 1401 IS CRACKED. ACCOMPLISHED DOUBLER REPAIR AT CANT FRAME 1401 PER AARD 53-10-00-15.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

AFT ACC - FRAME 1401 IS CRACKED AT LONGERON 1. (MKD) INSTALLED NEW SHEAR-TIE PER SRM 51-30-02 AND 51-30-05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

AFT CARGO CORROSION ON RIGHT TIE DOWN TRACK STATIONS 1212 TO 1220. REMOVED AND REPLACED RIGHT AFT TIE DOWN TRACK PER AARD 51-10-00-5 AND SRM 51-30-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

AFT ACCY RIGHT SIDE- FRAME 1418 IS CRACKED AT LONGERON 2 RIGHT. INSTALLED DOUBLER AT STATION 1418 PER SRM 53-03-00 FIGURE 31A.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

AFT CARGO CORROSION ON PLOW ANGLE STATION 1338 BETWEEN LONGERONS 28 LEFT AND 29 RIGHT. INSTALLED SERVICABLE NEW PLOW ANGLE PER AARD 51-10-00-5 AND BOEING DRAWING 9915561.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON CUSP AT RIGHT STATIONS 716 TO 720. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

FRAME 1418 CRACKED AT LONGERON 2 LEFT. INSTALLED DOUBLER AT STATION 1418 PER SRM 53-03-00 FIGURE 31A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON CUSP AT RIGHT STATIONS 661 TO 667. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CARGO, FORWARD, CORROSION ON BOTTOM OF CUSP RIGHT AT STATIONS 446 TO 465. INSTALLED DOUBLER FROM STATIONS 443 TO 459 RIGHT SIDE PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON LEFT CUSP STATIONS 1220 TO 1223 FOUND TO BE OUT OF LIMITS. INSTALLED CUSP DOUBLER FROM STATIONS 1187 TO 1232 LEFT HAND PER AARD 53-30-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

TWO DENTS FOUND ON EXTERNAL FUSELAGE SKIN AT STATION 237 LONGERON 17. DENT NUMBER 1 IS 1.5 X .5 X .015D, DENT NUMBER 2 IS 3 X 2 X .044D. INSTALLED REPAIR DOUBLER AND STRAP PER SRM 53-04-00 FIGURE 12-B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

INTERCOSTAL CRACKED BETWEEN FLOORBEAMS STATIONS 1287 TO 1309 BUTTLINE 0. INSTALLED INTERCOSTAL PER AARD 51-10-0-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON BOTTOM OF CUSP RIGHT STATIONS 446 TO 465. INSTALLED DOUBLER RIGHT STATIONS 443 TO 459 PER AARD 53-20-00-16.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

AFT CARGO - CORROSION ON FORWARD CORNER SUPPORT ANGLE AT THRESHOLD STATION 1155. INSTALLED CORNER SUPPORT ANGLE AT STATION 1155 PER SRM 51-30-05.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

AFT CARGO DOOR BEAM CORROSION AROUND FASTENERS FROM STATIONS 1155 TO 1212. REMOVED CORROSION AND INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

LIGHTNING STRIKE AT STATION 483 BELOW LONGERON 23 LEFT. REMOVED DAMAGED AREA, INSTALLED PLUG AND DOUBLER PER SRM 53-04-00 FIGURE 38, SHEET 23, VIEW H.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON LEFT CUSP STATIONS 708 TO 709. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

LIGHTNING STRIKE AT FUSELAGE STATION 454, BELOW LONGERON 23 LEFT. REMOVED DAMAGED AREA AND REPAIRED WITH PLUG AND DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 23 VIEW H.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

FORWARD ENTERY DOOR JAMB INNER WEB TONGUE CRACKED STATION 207 LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

CUSP CRACKED RIGHT BETWEEN STATIONS 984 TO 1003. INSTALL DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON SUB-FLOOR BELOW G-1 GALLEY PAN. INSTALLED DOUBLER ON SUB-FLOOR BELOW G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,303 hrs · 16,431 cycles

CORROSION ON SUB-FLOOR BELOW G-1 GALLEY PAN. INSTALLED DOUBLER ON SUB-FLOOR BELOW G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON LEFT CUSP STATIONS 511 TO 513 FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,303 hrs · 16,431 cycles

CORROSION ON BOTTOM OF CUSP RIGHT STATIONS 337 TO 341. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — DAMAGED (WINDOW) · airframe 35,303 hrs · 16,431 cycles

LEFT SIDE WINDOW PAN CRACKED UPPER AFT CORNER BETWEEN STATIONS 1003 TO 1022. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — DAMAGED (WINDOW) · airframe 35,303 hrs · 16,431 cycles

LEFT SIDE WINDOW PAN CRACKED LOWER FORWARD CORNER BETWEEN STATIONS 1079 TO 1098. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 35,303 hrs · 16,431 cycles

LEFT SIDE TOP FORWARD CORNER OF WINDOW PAN BETWEEN STATIONS 886 TO 905 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,003 hrs · 16,280 cycles

EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LAMP FOR CABIN EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,003 hrs · 16,280 cycles

EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LAMP FOR CABIN EMERGENCY LIGHT.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 33,971 hrs · 15,797 cycles

EWR - CREW REPORTED CABIN FILLED WITH GREY ELECTRICAL SMOKE. EMERGENCY DECLARED LANDED EWR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BURNT BALLAST AT ROW 8-9 AND DAMAGED POWER PORT CABLE AT SEAT 7-8. REPLACED BALLEST CONTROLLING SEATS 8-AB AND 9-AB OVERHEAD CEILING LIGHTS. REPLACED SEAT TO SEAT CABLE BETWEEN 7-DEF AND 8-DEF. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,995 hrs · 15,347 cycles

DURING TEST OF EMERGENCY LIGHT SYSTEM AS PER WORKCARD FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM ROW 13 TO ROW 16. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, SYSTEM OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,789 hrs · 14,838 cycles

PASSENGER SEAT EMERGENCY LIGHT PACK AB5-4 INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,789 hrs · 14,838 cycles

OVERWING EMERGENCY LIGHT DOES NOT COME ON. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,789 hrs · 14,838 cycles

PASSENGER SEAT EMERGENCY LIGHT PACK AB5-1 WEAK. REPLACED BATTERY PACK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,789 hrs · 14,838 cycles

CRACK IN FUSELAGE SKIN RIGHT SIDE AT CANT FRAME 1474 JUST AFT OF ACCUMULATOR ACCESS DOOR. INSTALLED DOUBLER REPAIR PER SRM 53-01-00 AND 53-30-00-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,784 hrs

DFW - RIGHT FORWARD OVERWING EXIT HATCH EMERGENCY EXIT MARKER LIGHT IS VERY DIM. REPLACED THE BATTERY PACK FOR CHARGING MODULE AB5-2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,784 hrs

DFW - THE TAIL COMPARTMENT CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK B5-28 FOR THE TAIL COMPARTMENT CEILING EMERGENCY LIGHTS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,784 hrs

DFW - EMERGENCY PATH LIGHTING AT SEAT 25D INOPERATIVE. RE-SECURED CONNECTOR NEAR SIDEWALL 24F.

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,784 hrs

DFW - EMERGENCY PATH LIGHTING AT SEAT 30D INOPERATIVE. RE-SECURED CONNECTOR NEAR SIDEWALL 30D.

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,784 hrs

DFW - EMERGENCY PATH LIGHTING AT SEAT 24D INOPERATIVE. RE-SECURED CONNECTOR NEAR SIDEWALL 24F.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 69,389 hrs · 36,909 cycles

AFT ACCESSORY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · 28,217 cycles

LAX EMERGENCY PORTABLE LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: TURBINE — DAMAGED (NR 1 ENGINE) · airframe 27,901 hrs

DFW INFLIGHT T2457/24JUL. CREW REPORTED NR 1 ENGINE MADE LOUD BANG FOLLOWED BY ENGINE GAS TEMPERATURE HIGH. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND TURBINE DAMAGE. REPLACED NR 1 ENGINE ON 24 JUL AT DFW. SYSTEM GROUND CHECKED NORMAL OPS. (OPEN)

Part: OVEN — DIRTY (GALLEY)

DFW - INFLIGHT FLIGHT ATTENDANT REPORTED SMOKE COMING FROM FORWARD GALLEY OVEN. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION. PLACARDED FIRST CLASS OVEN AND PULLED AND COLLARED CIRCUIT BREAKER. CLEANED HEATING ELEMENTS FOR FIRST CLASS OVEN ON 3 JULY AT LGA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 11,518 hrs · 5,920 cycles

DURING OVERNIGHT LS CHECK EMERGENCLY LIGHTS IN AFT TAIL STAIRWAY INOP. INSTALLED BATTERIES IN POWER PACK B5-28 AND B5-27 LAMP 7732 1315. OPS CK NORMAL. CHECK-C 11-11-02 MCI.

Part: LAVATORY — FIRE (RIGHT) · airframe 4,898 hrs · 2,404 cycles

SMOKE CAME FROM THE RT LAVATORY WASTE AREA. CREW EXTINGUISHED FIRE IN WASTE BASKET USING WATER FROM THE LAVATORY. SUSPECT CAUSED BY A CIGARETTE. THE FIRE DETECTION AND EXTINGUISHING SYSTEMS HAD NOT YET ACTIVATED BUT WERE OPERATIONALLY CHECKED NORMAL. CHECK-C 10-2-99 STL.

Part: SKIN — TORN (RT WING)

RT WING LE SKIN WAS TORN AND DENTED DUE TO GROUND DAMAGE BETWEEN 2 OTBD TRACKS FOR NUMBER 3 SLAT, RT WING, 37 IN LONG. REPLACED LE CAP PER DOUGLAS BLUE PRINT 5937513 SHEET 1.

Part: SKIN — SCRATCHED (RT WING)

RT WING LE CAP WAS SCUFFED ON LOWER SURFACE, 6 IN BY 4 INCHES OFF OF NUMBER 4 SLAT. REMOVED AND REINSTALLED SERVICEABLE NUMBER 4 LE CAP PER DOUGLAS BLUE PRINT 5937523, SHEET 1. CHECK-C 10-2-99 STL.

Part: SKIN — PUNCTURED (BS 218)

PUNCTURE IN FUSELAGE SKIN CAUSED BY GROUND EQUIPMENT 3.5 IN BY 3 IN AT STA 218, STR 21. CLASS 3 REPAIR INSTALLED. REMOVED CLASS 3 REPAIR AND INSTALLED CLASS 2 REPAIR PER DRM 53-04, FIG 12. CHECK-C 10-2-99 STL.

Part: FRAME — DAMAGED (BS 218)

THE RING FORMER SUPPORT ASSY WAS DAMAGED BY GROUND EQUIPMENT AT FUSESAGE STA 218, STR 21R. INSTALLED RING FORMER REPAIR PER SRM 53-03, FIG 3. CHECK-C 10-2-99 STL.

Part: FRAME — DAMAGED (BS 218)

THE FORMER SUPPORT ASSY RECEIVED GROUND DAMAGE AT FUSELAGE STA 218, STRINGER 21R. INSTALLED RING FORMER REPAIR PER SRM 53-03, FIG 3 CHECK-C 10-2-99 STL.

Part: SKIN — GOUGED (RT WING)

THE RT WING LOWER SURFACE SKIN HAD 3 GOUGES JUST AFT OF OTBD TRACK FOR NUMBER 3 SLAT, CAUSED BY GROUND EQUIPMENT DAMAGE. LENGTHS OF GOUGES 5 IN, 4.5 INCH, AND 2 INCH. DEEPEST DEPTH 0.050. BLENDED GOUGES PER SRM 57-01, FIG 1 SHEET 3. ALODINE AREA PER SRM 51-10-3, PARAGRAPH 30. EDDY CURRENT ACCOMP AND NO DEFECTS. AREAS ALSO COVERED BY ARA 16489 AND ARA 16488. CHECK-C 10-2-99 STL.

Part: SKIN — DAMAGED (BS 218)

THE RT FUSELAGE EXTERNAL DOUBLER WAS REMOVED TO GAIN ACCESS TO DAMAGE AT STA 218, LONGERON 21R. INSTALLED DOUBLER PER SRM 53-04, FIG 12B. CHECK-C 10-2-99 STL.