N9629H

Part: VALVE — DEFECTIVE (FUEL SYSTEM) · airframe 55,549 hrs · 27,830 cycles

DURING CLIMB OUT, CENTER FUEL PRESSURE LOW ILLUMINATE WITH APROXIMATELLY 2000 LBS, IN THE CENTER TANK. WHILE EXECUTING THE QHR PROCEDURE THE CENTER FUEL QUANTITY INITIALLY INCREASED TO 2500 LBS , AT THE POINT THE LOW PRESS LIGHT EXTINGUISHED AND FUEL RETURNED NORMALLY FOR SEVERAL MINUTES. AT THAT POINT THE LIGHT REILLUMINATED. AN EMERGENCY WAS DECLAED AND THE FLIGHT AIR INTERRUPTED BACK TO ORD FOR LANDING WITH NO FURDER INCIDENT. NOTE: WHILE CENTER FUEL QUANTITY WAS INCREASING BOTH MAIN TANK QUANTITIES WERE DECREASING. REPLACED CENTER TANK EXTRACTOR CHECK VALVE PER AMM 28-20-26. NO DISCREPANCIES NOTED. AFTER CLOSE CLEARANCE, PANEL 1436C SEALED AT 2230. OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.

Part: SEAL — LEAKING (WINDSHIELD) · airframe 55,414 hrs · 27,744 cycles

WEATHER SEAL DAMAGED ON THE FIRST OFFICIERS WINDSHIELD. MOISTURE INGRESS WAS VISIBLE. THE AIRCRAFT WAS GROUNDED. REPLACED FIRST OFFICIERS WINDSHIELD IAW AMM 56-10-02.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 55,414 hrs · 27,744 cycles

DELAMINATION FOUND ON THE LOWER INBOARD CORNER OF THE CAPTAIN`S WINDSHIELD. EXTENDS APPROXIMATELY 2.5 INCHES FROM THE CLEAR VIEW EDGE INTO THE CRITICAL VISION AREA, ZONE 1. THE AIRCRAFT WAS GROUNDED. REPLACED THE WINDSHIELD IAW AMM 52-10-02.

Part: GUST LOCK — OUT OF ADJUST (L1 DOOR) · airframe 55,037 hrs · 27,499 cycles

L1 DOOR WOULD NOT ENGAGE GUST LOCK WITHOUT EXCESSIVE EFFORT. THE AIRCRAFT WAS GROUNDED. INSTALLED NEW GUST LOCK DOOR HOLD OPEN PER MM 52-11-04.

Part: LANYARD — DISCONNECTED (TAILCONE SLIDE) · airframe 54,829 hrs · 27,372 cycles

SLIDE TETHER DISCONNECTED AT TAILCONE. RECONNECTED TETHER IAW AMM 25-62-01.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 53,691 hrs · 26,648 cycles

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

Part: COVER — LOOSE (R1 DOOR) · airframe 52,292 hrs · 25,753 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE RAFT COVER IS LOOSE AND CABLE IS OUT OF POSITION. REATTACHED SLIDE COVER AND SECURED CABLE PER AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: HINGE — LACK OF LUBE (L1 DOOR) · airframe 52,267 hrs · 25,739 cycles

L1 DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBRICATED HINGES AND FITTINGS IAW AMM 12-21-01. OPS CHECKED GOOD IAW AMM 52-11-00. AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,639 hrs · 25,333 cycles

MAINT ENTRY REF MIC 33286216 FOR RED INDICATOR ON FWD FLASHLIGHT NOT FLASHING. REPLACED EXPIRED BATTERY GRND CK GOOD PER MM 256000. THE AIRCRAFT WAS NOT GROUNDED.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 51,503 hrs · 25,247 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE LIGHT IN CEILING BY L2 DOOR IS DISCONNECTED. RECONNECTED LIGHT IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: FITTING — LEAKING (APU) · airframe 51,497 hrs · 25,242 cycles

AIRCRAFT WAS GROUNDED. OIL ODOR IN CABIN FROM TAKEOFF UNTIL 20,000 FEET. AUXILIARY POWER UNIT LEAKING OIL FROM OIL PUMP FITTING ON BOTTOM OF PUMP. REMOVED AND REPLACED APU IAW AMM 49-96-91 AND ACCOMPLISHED PACK BURNOUT IAW AMM 21-92-12. OPERATIONAL CHECK GOOD..

Part: OIL TANK — LEAKING (APU) · airframe 51,493 hrs · 25,238 cycles

STRONG ODOR OF OIL IN THE COCKPIT AND LESSER ODOR IN CABIN. CONFIRMED OIL LEAK ABOVE OIL TANK. REMOVED AND REPLACED AUXILIARY POWER UNIT ASSEMBLY IAW WORK CARD 49-98-83. OPERATONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: APU — FAULTY (ZONE 100) · airframe 51,227 hrs · 25,063 cycles

AIRCRAFT WAS GROUNDED. ODOR OF OIL IN CABIN AND COCKPIT AFTER APU START. ODOR DISSIPATES AFTER SEVERAL MINUTES. REMOVED AND REPLACED AUXILIARY POWER UNIT. OPERATIONAL CHECK GOOD.

Part: ENGINE — SMOKE (LEFT) · airframe 51,197 hrs · 25,038 cycles

AFTER GATE ARRIVAL, MAINTENANCE PULLED FIRE HANDLE DUE TO SMOKE AND FUEL FROM THE LT ENGINE. AIRCRAFT WAS GROUNDED. ACCOMPLISHED VISUAL CHECKS. STARTED AND SHUTDOWN ENGINE TWICE. RESET ENGINE GENERATOR. ALL PARAMETERS NORMAL. OPS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,629 hrs · 24,669 cycles

AIRCRAFT IN BASE MAINTENANCE. FUSELAGE SKIN CRACK WAS FOUND AT STATION 1437 BETWEEN STRINGERS 2R AND 3R. REPAIRED IAW EA 264374.

Part: FITTING — CRACKED (LT SPOILER) · airframe 50,629 hrs · 24,669 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT GROUND SPOILER FITTING IS CRACKED ON THE INBOARD FLANGE OF THE OUTBOARD LEG. REMOVED AND REPLACED FITTING IAW SRM 51-30-05, SR09570010 AND AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (BS 370) · airframe 50,629 hrs · 24,669 cycles

FORWARD CARGO DOOR STOP FITTING CRACKED. REMOVED AND REPLACED FITTING IAW ESO80174 PAGE 602.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,629 hrs · 24,669 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHTS INOPERATIVE BETWEEN STATIONS 243 AND 1332. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,629 hrs · 24,669 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHTS INOPERATIVE BETWEEN STATIONS 243 AND 1332. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,629 hrs · 24,669 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHTS INOPERATIVE BETWEEN STATIONS 243 AND 1332. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,629 hrs · 24,669 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHTS INOPERATIVE BETWEEN STATIONS 243 AND 1332. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,629 hrs · 24,669 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHTS INOPERATIVE BETWEEN STATIONS 243 AND 1332. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECK GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,311 hrs · 24,475 cycles

AIRCRAFT WAS GROUNDED. IN ACCESSORY COMPARTMENT, RT STR AFT OF FIRE BOTTLES IS CRACKED. R & R STR IAW AARD 51-00-00-1.

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 50,014 hrs · 24,315 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY NOT DECLARED, LANDING UNEVENTFUL, AIRCRAFT OVERWEIGHT. DURING CLIMB F/A`S REPORTED A BURNING ODOR. R & R THE RT PRSOV IAW AMM 21-31-12. ACCOMPLISHED PACK BURN OUT IAW CARD 21-92-12. NO ODORS NOTED. SYSTEM CHECKS NORMAL.

Part: TRANSMITTER — STICKING (NR 2 ENGINE) · airframe 49,553 hrs · 24,050 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL NR 2 ENG WOULD NOT ATTAIN TAKEOFF THRUST. ABORTED TAKEOFF AT APPROX 120 KNOTS. FOUND RT EPR TRANSMITTER STICKING. R & R TRANSMITTER IAW AMM 77-11-02 & ACCOMPLISHED OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,299 hrs · 23,254 cycles

L1 DOOR PORTABLE EMER LIGHT, AMBER CHARGE LIGHT IS INOPERATIVE & BATTERIES ARE DEAD. REPLACED L1 DOOR PORTABLE EMER LIGHT ASSEMBLY IAW AMM 33-53-00. TESTED OK.

Part: OIL COOLER — FAILED (LT ENGINE) · airframe 48,225 hrs · 23,206 cycles

EMERGENCY DECLARED, INBD ACCOUNT LT ENG GEN FAIL. APU FAILED TO LIGHT OFF AT ALTITUDE. AT LOWER ALTITUDE, SUBSEQUENT APU START ATTEMPT WAS ACCOMPLISHED WITH SUCCESSFUL APU START. LANDED WITHOUT FURTHER INCIDENT. R & R CSD OIL COOLER IAW MM 24-10-03. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 47,483 hrs · 22,740 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE CTR TANK PUMP FAILED. UNABLE TO TRANSFER FUEL OUT OF CTR TANK. RESET APPLICABLE CENTER UFI IAW AMM 28-20-28. PERFORMED OPERATIONAL CHECK. SYSTEM CHECKED NORMAL.

Part: RIB — CRACKED (RT WING) · airframe 47,102 hrs · 22,525 cycles

RIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER IAW MCM CARD 5798-06 & EA 250469.

Part: CASTING — CRACKED (SPOILER ACTUATOR) · airframe 47,102 hrs · 22,525 cycles

CRACK IN FWD END RT SIDE OF RT GND SPOILER ACTUATOR CASTING. REPLACED ACTUATOR CASTING IAW AMM 27-62-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,102 hrs · 22,525 cycles

CABIN SEAT TRACK NR 6 CORRODED OUT OF LIMITS BETWEEN STATION 216 & 588. REMOVED & INSTALLED NEW SEAT TRACK IAW AMM 53-40-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,102 hrs · 22,525 cycles

CORROSION ON UNDERSIDE OF CUSP ANGLE AT STATION 213 - 217 RT. INSTALLED REPAIR DOUBLER IAW EA 250200 DATED 04 16 2015.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 47,102 hrs · 22,525 cycles

VERTICAL STABILIZER LE FAIRING FUSELAGE LT ATTACH ANGLE AT BS 1401 - 1429 CRACKED. REPLACED ANGLE IAW AARD 55-30-00-7.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 47,102 hrs · 22,525 cycles

STIFFENER ON AFT SIDE OF FRAME 1338 AT LONGERON 1 IS CRACKED. R & R STIFFENER IAW DWG 5930760, DWG 9915562 & AARD 51-00-05-1.

Part: CARGO TRACK — CORRODED (BS 1130-1212) · corrosion level 2 · airframe 47,102 hrs · 22,525 cycles

LEFT CTR CARGO TIE DOWN TRACK CORRODED. INSTALLED NEW TRACK IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (BS 1024-1030) · airframe 47,102 hrs · 22,525 cycles

CORROSION FOUND ON BOTTOM SIDE OF CUSP FROM STATION 1024 - 1030 AROUND LIGHTNING HOLES. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: FRAME — CRACKED (BS 1418) · airframe 47,102 hrs · 22,525 cycles

FRAME CRACKED AT AFT SIDE OF STATION 1418 L2-R. INSTALLED DOUBLER IAW SRM 53-03-00-001, 53-01-00-001 & AARD 53-10-00-15.

Part: FRAME — CRACKED (BS 1401) · airframe 47,102 hrs · 22,525 cycles

FRAME CRACKED AT STATION 1401 L1. CUT OUT DAMAGED AREA, INSTALLED FILLER & DOUBLER IAW AARD 53-10-00-17.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 47,102 hrs · 22,525 cycles

RIGHT CUSP WEB CORRODED BETWEEN STATION 200 & 218. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: WEB — CORRODED (BS 160-190) · airframe 47,102 hrs · 22,525 cycles

FORWARD GALLEY SILL AREA HAS CORROSION ON FLOOR WEB OTBD OF J CHANNEL BETWEEN STATION 160 & 190. INSTALLED WEB DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 1231-1250) · airframe 47,102 hrs · 22,525 cycles

LEFT CUSP CORRODED BETWEEN STATION 1231 - 1250. INSTALLED CUSP DOUBLER SECTION IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 370-389) · airframe 47,102 hrs · 22,525 cycles

CORROSION FOUND ON CUSP AT STATION 370 RT. INSTALLED CUSP DOUBLER REPAIR IAW SRM 53-05-00 FIG 131A SHEET 1.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 47,102 hrs · 22,525 cycles

AFT RT CARGO TIE DOWN TRACK FOUND CORRODED. NEW TRACK INSTALLED IAW SRM 51-30-01.

Part: SKIN — WORN (ZONE 100) · airframe 47,102 hrs · 22,525 cycles

WORN AREA ON INTERIOR FWD SKIN OF APU ENCLOSURE. REPAIRED & INSTALLED DOUBLER IAW AARD 53-20-00-11 REPAIR 11.

Part: CUSP WEB — CORRODED (BS 370) · corrosion level 2 · airframe 47,102 hrs · 22,525 cycles

RIGHT CUSP WEB CORRODED AT BS 370. INSTALLED DOUBLER & SPLICE STRAP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 641-646) · corrosion level 2 · airframe 47,102 hrs · 22,525 cycles

MID CARGO CORROSION ON RT CUSP SHEET, BOTTOM SIDE, EMITTING FROM UNDER FIBER GLASS THROUGH STATION 641 - 646. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: FORMER — CRACKED (SLAT TRACK) · airframe 47,102 hrs · 22,525 cycles

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

Part: SKIN — CRACKED (ZONE 100) · airframe 47,102 hrs · 22,525 cycles

CRACK IN FS 1474 APPROX 13" ABOVE RT AIR STAIR DOOR. STOP DRILLED CRACK IAW SRM 51-01-00 & INSTALLED DOUBLER IAW SRM 53-01-00-001.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 47,102 hrs · 22,525 cycles

CABIN GUSSET CRACKED AT BS 207, BL 12L. REMOVED DAMAGED MATERIAL & REPAIRED WITH FILLER & DOUBLER IAW SRM 53-05-00-001.

Part: FORMER — CRACKED (SLAT TRACK) · airframe 47,102 hrs · 22,525 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED DOUBLER & HAT BUSHING IAW WC 57-98-05.

Part: CUSP WEB — CORRODED (BS 1174-1178) · corrosion level 2 · airframe 47,102 hrs · 22,525 cycles

CORROSION ON SUBFLOOR, INBD SIDE OF SEAT TRACK NR 1, STATION 1174 - 1178. INSTALLED DOUBLER ON LT CUSP SHEET AT STATION 1174 - 1178 IAW AARD 53-20-00-16.

Part: ELECTRONIC UNIT — FAULTY (CARGO BAY) · airframe 43,178 hrs · 20,462 cycles

MAF INFLIGHT DFW-TUS. CARGO FIRE INDICATION WARNING. FIRE BOTTLE WAS DISCHARGED. EMERGENCY DECLARED FLIGHT DIVERTED MAF LANDED WITHOUT INCIDENT. NO EVIDENCE OF CARGO FIRE OR OVERHEAT DETECTED. AIRCRAFT REMOVED FROM SERVICE. REPLACED AFT CARGO ELECTRONIC UNIT & NR 1 FIRE EXTINGUISHING BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: FIRE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 40,473 hrs · 19,029 cycles

DFW - CREW REPORTED AFT CARGO FIRE INDICATION. CREW DISCHARGED FORWARD AND AFT FIRE BOTTLES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NO INDICATION OF FIRE. REPLACED ALL THREE AFT CARGO FIRE DETECTORS AND FORWARD AND AFT FIRE BOTTLES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CIRCUIT BREAKER — FAILED (COCKPIT) · airframe 37,039 hrs · 17,283 cycles

DEN - INFLIGHT PDX-DFW. CREW REPORTED AFT CENTER BOOST PUMP, FORWARD LEFT WING FUEL BOOST PUMPS AND FUEL QUANTITY INDICATION FAILED. FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. REPLACED AC BUS CONTROLLER AND RT BUS "B" PHASE CIRCUIT BREAKER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN) · airframe 36,744 hrs · 17,129 cycles

FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED AB5-1 MODULE AND BATTERY PACK. FOUND PINCHED WIRE TO AL2-2. INTEGRITY OF WIRE FOUND GOOD AND REROUTED WIRE TO ILLUMINATE PINCHING. OPS CHECK NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 36,304 hrs · 16,925 cycles

LONGERON 2 RIGHT IS CRACKED AFT OF STATION 1418. REMOVED CRACKED SECTION OF LONGERON AND INSTALLED REPAIR PER SRM 53-02-00 FIGURE 18 AND EA MD80-53-016588.

Part: STIFFENER — CRACKED (BS 1338 BULKHEAD) · airframe 36,304 hrs · 16,925 cycles

CRACKED STIFFENER TOP CENTER FORWARD SIDE OF STATION 1338 BULKHEAD. INSTALLED DOUBLER PER EA MD80-53-016535.

Part: PAN — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

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

Part: FRAME — CRACKED (BS 1463) · airframe 36,304 hrs · 16,925 cycles

FRAME CRACKED AT CANT 1463. REMOVED AND REPLACED CRACKED FRAME PER AARD 51-10-00-5.

Part: PAN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

CARGO FORWARD CARGO CORROSION ALONG DOOR CUTOUT DOOR PAN, STATIONS 370 TO 427, LONGERON 28 RIGHT. REMOVED DAMAGED AREA OF DOOR PAN AND INSTALLED SERVICEABLE FORWARD CARGO DOOR PAN STATIONS 370 TO 427 PER SRM 53-05-00 AND EA MD80-53-016572.

Part: SKIN — DENTED (CARGO DOOR) · airframe 36,304 hrs · 16,925 cycles

AFT CARGO DOOR SKIN HAS A DEEP DENT BETWEEN OUTER HANDLE AND AFT ACCESS PLATE HAS AN ADL STICKER. INSTALLED NEW OUTER SKIN.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,304 hrs · 16,925 cycles

CRACKS ON TOP LIP OF INTERCOSTAL, CENTER LINE, BETWEEN FLOORBEAMS, STATIONS 1271 TO 1287. INSTALLED INTERCOSTAL BETWEEN STATIONS 1271 TO 1287 PER AARD 51-10-00-5.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

CORROSION ON DOOR CUTOUT BEAM STATIONS 1160 TO 1206. REMOVED CORROSION AND INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: GUSSET — GOUGED (CARGO BAY) · airframe 36,304 hrs · 16,925 cycles

FORWARD CARGO HAS GOUGES BELOW INBOARD EDGE OF RIGHT TIE DOWN TRACK BETWEEN STATIONS 362 TO 370. COMPLETED INSTALLATION OF GUSSET PER SRM 51-30-05, 51-30-01 AND SRM 51-30-02 AND AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

CORROSION OUT OF LIMITS ON SEAT TRACK NUMBER 6 AT STATIONS 229 TO 235. INSTALLED REPAIR STRAP ON SEAT TRACK NUMBER 6 STATION 235 PER AARD 53-20-00-13 FIGURE 1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,304 hrs · 16,925 cycles

TOP LIP OF INTERCOSTAL CRACKED SEVERAL PLACES CENTERLINE BETWEEN FLOORBEAMS STATIONS 1287 TO 1309. INSTALLED NEW INTERCOSTAL BETWEEN STATIONS 1287 TO 1309 PER AARD 51-10-00-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,304 hrs · 16,925 cycles

FORWARD LEFT AFT NOSE LANDING GEAR STRUT DOOR, AFT HINGE CUTOUT, SKIN IS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 53-05-00 FIGURE 62.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

SEAT TRACK NUMBER 1 STATION 694 OUT OF LIMITS. INSTALLED PLUG AT NUMBER 1 SEAT TRACK PER SRM 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

CORROSION REMOVAL OUT OF LIMITS ON LEFT CUSP STATIONS 589 TO 788. INSTALLED NEW CUSP SHEET PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

CORROSION ON RIGHT CUSP AT STASIONS 218 TO 222. REMOVED CORROSION AND INSTALLED NEW CUSP SHEET PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

LEFT CUSP SHEET FROM STATIONS 845 TO 905 TO BE OUT OF LIMITS. INSTALLED NEW CUSP SHEET LEFT STATIONS 845 TO 905 PER AARD 51-10-00-5.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 36,304 hrs · 16,925 cycles

NUMBER 2 SEAT TRACK GOUGED STATIONS 427 TO 430. PERFORMED PLUG REPAIR ON NUMBER 2 SEAT TRACK AT STATIONS 427 TO 430 AS PER SRM 53-0-05 FIGURE 4A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

CORROSION ON FRAME 110 LONGERON 30. REPAIRED PER SRM 53-02-00 FIGURE 1B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,304 hrs · 16,925 cycles

LEFT CUSP STATIONS 836 TO 845 CORRODED. REPLACED LEFT CUSP STATIONS 807 TO 845 PER AARD 53-20-00-16.

Part: DUCT — DAMAGED (CABIN PRESSURE) · airframe 36,170 hrs · 16,862 cycles

DFW - CREW REPORTED LEFT PACK WOULD NOT MAINTAIN CABIN PRESSURIZATION AND RIGHT PACK INOPERATIVE PER MEL. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED Y-DUCT THAT HAD A HOLE IN IT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT) · airframe 34,935 hrs · 16,287 cycles

DFW - DURING TAKEOFF OTHER AIRCRAFT AND TOWER REPORTED SMOKE COMING FROM ENGINE. CREW REPORTED NO ABNORMAL ENGINE INDICATIONS. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. DECLARED LEFT ENGINE CHANGE DUE TO BREATHER PRESSURE TEST FAILURE. REPLACED LEFT ENGINE AT DFW ON 10/10/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,705 hrs · 16,171 cycles

FIRST CLASS EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED EGRESS BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,705 hrs · 16,171 cycles

EGRESS LIGHTS INOPERATIVE BETWEEN ROWS 7 AND 20. REMOVED AND REPLACED EGRESS BATTERY PACK. OPS CHECKED NORMAL.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,900 hrs · 15,347 cycles

FORWARD LOWER LEFT SIDE OF RADOME BULKHEAD HAS CRACK AT STOP PAD ALIGNMENT PIN. DOUBLER WAS INSTALLED PER AARD 53-10-00-19.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,900 hrs · 15,347 cycles

LONGERON 2 LEFT CRACKED AT STATION 1418. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER EA MD80-53-009159.

Part: GENERATOR — FAILED (NR 2 ENGINE) · airframe 31,569 hrs · 14,764 cycles

IN FLIGHT, NUMBER TWO ENGINE GENERATOR FAILED AND WOULD NOT RESET. APU WOULD NOT START IN FLIGHT. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE GENERATOR AND RIGHT CONSTANT SPEED DRIVE.

Part: TIRE — OUT OF ROUND (ZONE 700) · airframe 29,397 hrs

DFW INFLIGHT - CREW REPORTED NOSE WHEEL VIBRATION AFTER TAKEOFF. LANDED DFW WITHOUT INCIDENT AND TAXIED TO GATE. FOUND RIGHT NOSE TIRE OUT OF ROUND. REPLACED BOTH NOSE TIRE ASSEMBLIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · 28,572 cycles

LGA EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: TRANSDUCER — INOPERATIVE (MLG) · airframe 28,424 hrs

DFW INFLIGHT T1115/05AUG. CREW REPORTED LT HAND ANTI SKID LIGHT ILLUMINATED ON APPROACH. LANDED DFW WITHOUT INCIDENT. REPLACED NR 2 WHEEL SPEED TRANSDUCER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - FOUND EMERGENCY LIGHT AT SEAT ROW 22 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - OVERHEAD EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — UNSERVICEABLE (PAX DOOR)

MSY - ENTRY DOOR SLIDE FOUND WITH NO PRESSURE. REPLACED ENTRY DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PAD — INOPERATIVE (GEAR DOOR)

ORD - DURING APPROACH EXTENDED LANDING GEAR AND GEAR DOOR OPEN REMAINED ILLUMINATED. TOWER ADVISED GEAR DOORS MAIN WRE OPEN. WENT AROUND AND ACCOMPLISHED GEAR DOOR OPEN LIGHT QRH, NO HELP. REPLACED BOTH MAIN LANDING GEAR DOOR PADS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOWNLOCK SENSOR — INOPERATIVE (MLG)

LAX - INFLIGHT ON APPROACH NOSE LANDING GEAR GREEN LIGHT DID NOT COME ON. ON SECOND APPROACH THE NOSE LANDING GEAR EXTENDED NORMALLY. NOSE LANDING LIGHT TESTED GOOD. NOSE LANDING LIGHT FLICKERED ON LANDING. REPLACED DOWNLOCK SENSOR FOR NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RDU - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT POSITION B5103 FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,448 hrs · 20,799 cycles

DURING CHECK-C CRACK AT LEFT HAND MAIN GEAR DOOR CUTOUT FORWARD 11B CORNER FORWARD OF DOOR ACTUATOR ASSEMBLY RUNNING OUTBOARD FROM CORNER TURNING UPWARD. ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER IAW SRM 51-20-5.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,448 hrs · 20,799 cycles

DURING CHECK-C 4 EACH CRACKS AROUND BOLT HEAD LE HORIZONTAL STABILIZER 1-8 INCH APPROXIMATELY 19 INCHES FROM LE LEFT HAND HORIZONTAL STABILIZER. REPAIR COMPLETED PER SRM 51-70-4.

Part: BULB · airframe 11,247 hrs · 5,750 cycles

A CABIN EGRESS LIGHT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 1-5-02 STL. --CLOSED--

Part: PANEL — FAILED (BUSS PROTECTION) · airframe 5,150 hrs · 2,501 cycles

DURING CLIMB BOTH AC ELECTRICAL BUSSES TRIPPED OFF LINE AT THE SAME TIME. EMERGENCY POWER WAS USED UNTIL THE BUSSES WERE RESET. FLIGHT RETURNED TO STL. REPLACED THE BUS PROTECTION PANEL. CHECK-C 1-19-00 STL.