N7547A

Part: WIRE — SHORTED (ZONE 100) · airframe 75,452 hrs · 39,843 cycles

AIRCRAFT WAS GROUNDED. AUTO PILOT OFF, CLIMBING THRU 10,000 ADJUSTED RUDDER TRIM WHEN AIRCRAFT BEGAN ROLLING DUE TO RUDDER YAW. YAW DAMP OFF DFG APPEARED TO BE COMPLETED INOPERABLE DUE TO CONTROL ISSUES. DECLARED EMERGENCY, RETURNED TO OMA FOR LANDING AS AIRCRAFT SPEED DECREASED CONTROL IMPROVED ENOUGH FOR LANDING. MAINTENANCE FOUND SHORTED WIRE (2C610X22RD) AT RIGHT HAND SIDE, STATION 1431 CANT FRAME BETWEEN S30-5 AND RUDDER POSITION TRANSMITTER. REPAIRED WIRE PER AMM 22-01-05.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,434 hrs · 39,832 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD OVERHEAD EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSSEMBLY B5-23 PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LONGERON — CRACKED (BS 200) · airframe 74,991 hrs · 39,556 cycles

A CRACK INDICATION FOUND ON LONGERON 23L AT BS 200. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: STIFFENER — CRACKED (BS 218 BULKHEAD) · airframe 74,991 hrs · 39,556 cycles

CRACK INDICATION ON THE -7 STIFFENER, LOWER END AT BS 218 BULKHEAD BETWEEN LONGERONS 23L AND 24L. REPAIRED THE STIFFENER IAW SRM 53-01-00-001, SRM 53-14-01-001, AND DWG 53-10-00-15.

Part: LONGERON — CRACKED (BS 160-200) · airframe 74,991 hrs · 39,556 cycles

CRACK INDICATIONS ON LONGERON 24L AT BS 160 AND 200. REPAIRED THE LONGERON IAW SRM 53-02-00.

Part: LONGERON — CRACKED (BS 160) · airframe 74,991 hrs · 39,556 cycles

CRACK INDICATIONS ON TOP OF LONGERON 25L AT BS 160. REPAIRED THE LONGERON IAW SRM 53-02-00.

Part: ENGINE — SLOW (NR 1) · airframe 74,731 hrs · 39,392 cycles

AIRCRAFT WAS NOT GROUNDED. WHEN THROTTLES WERE ADVANCED FOR TAKE OFF THE NR 1 ENGINE WAS SLOW TO SPOOL. TAKE OFF ABORTED. CREW ACCOMPLISHED A PUSH-UP CHECK WITH ALL INDICATIONS NORMAL. SUBSEQUENT TAKE OFF WAS UNEVENTFUL.

Part: BEAM — CORRODED (BS 1155-1212) · airframe 74,285 hrs · 39,117 cycles

CORROSION ON AFT CARGO LOWER DOOR BEAM OUTBOARD EDGE. REMOVED AND REPLACED AFT CARGO DOOR BEAM IAW 51-00-05-1 AND DRAWING 5930483.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 74,284 hrs · 39,116 cycles

ON CLIMB OUT FROM 20,000 TAIL COMP TEMP HIGH LT ILLUMINATED AND AFTER DOING THE CHECKLIST LIGHT EXTINGUISHED AFTER 20 SECONDS. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE CLAMP ON THE RIGHT HAND AUGMENTATION VALVE. THE CLAMP WAS RESECURED, THE ENGINES WERE RUN AGAIN, AND NO LEAKS WERE FOUND. REFERENCE USED WAS AMM 36-10-01 AND MNM CARD 36-95-14. THE AIRCRAFT WAS GROUNDED.

Part: SEAL — LEAKING (ANTI ICE SYS) · airframe 74,253 hrs · 39,095 cycles

EMERGENCY DECLARED. DURING CLIMB RECEIVED A TAIL COMPARTMENT HIGH TEMPERATURE WARNING. RETURNED TO DEPARTURE. ACCOMPLISHED MCM 36-95-14 AND MCM 0930. REMOVED AND REPLACED ANTI-ICE SEALS. AIRCRAFT WAS GROUNDED.

Part: SENSOR — FAULTY (AC BAY) · airframe 74,246 hrs · 39,090 cycles

AFTER TAKE-OFF, THE TAIL COMP TEMP HIGH OVERHEAT LIGHT CAME ON. THE LIGHT WENT OUT AFTER MEMORY ITEMS. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LT TAIL COMP OVERTEMP SENSOR IAW AMM 36-20-02. OPS AND LEAK CHECKS PER AMM 36-10-01 AND AMM 36-10-05. THE AIRCRAFT WAS GROUNDED. (SEE ALSO AALA20170503001)

Part: CLAMP — LEAKING (BLEED AIR SYS) · airframe 74,246 hrs · 39,090 cycles

AFTER TAKE-OFF, THE TAIL COMP TEMP HIGH OVERHEAT LIGHT CAME ON. THE LIGHT WENT OUT AFTER MEMORY ITEMS. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. REPLACED CLAMPS ON LT AUGMENTATION VALVE, OPS AND LEAK CHECKS PER AMM 36-10-01 AND AMM 36-10-05. THE AIRCRAFT WAS GROUNDED. (SEE ALSO AALA20170502007)

Part: ACM — FAILED (RIGHT) · airframe 74,225 hrs · 39,073 cycles

AFTER TAKEOFF, A TAIL COMPARTMENT TEMP HIGH INDICATION ILLUMINATED. THE LIGHT EXTINGUISHED UPON COMPLETION OF MEMORY ITEMS. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT ACM IAW MCM CARD 21-94-02. THE AIRCRAFT WAS GROUNDED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,852 hrs · 38,845 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON FRAME AT STA 1401 LONGERON 1. REPAIRED FRAME PER SRM 53-01-00-001 AND AARD 53-10-00-15.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,525 hrs · 38,637 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH RED LIGHT AT SEAT 20D IS INOPERATIVE. REPAIRED IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: ATTACH FITTING — DIRTY (ZONE 800) · airframe 73,303 hrs · 38,502 cycles

AIRCRAFT NOT GROUNDED. L2 DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO ARM/DISARM. CLEANED GIRT BAR FLOOR ATTACH FITTINGS. OPERATIONAL CHECK GOOD.

Part: PLUG — FAULTY (ZONE 200) · airframe 73,267 hrs · 38,482 cycles

AIRCRAFT WAS NOT GROUNDED. DURING TAKEOFF ROLL THE RIGHT FUEL HEAT ANNUNCIATOR ILLUMINATED. TAKE OFF ABORTS AT APPROXIMATELY 10 KNOTS. REMOVED AND REPLACED RIGHT FUEL HEATER SHUTOFF VALVE IAW AMM 73-14-02, RIGHT FUEL DEICING VALVE RELAY R2-129 IAW AMM 24-00-00, AND FUEL HEAT CONTROL PLUG P1-806 IAW SWPM 20-31-15. SEE ALSO AALA20170123003.

Part: RELAY — FAULTY (ZONE 200) · airframe 73,267 hrs · 38,482 cycles

AIRCRAFT WAS NOT GROUNDED. DURING TAKEOFF ROLL THE RIGHT FUEL HEAT ANNUNCIATOR ILLUMINATED. TAKE OFF ABORTS AT APPROXIMATELY 10 KNOTS. REMOVED AND REPLACED RIGHT FUEL HEATER SHUTOFF VALVE IAW AMM 73-14-02, RIGHT FUEL DEICING VALVE RELAY R2-129 IAW AMM 24-00-00, AND FUEL HEAT CONTROL PLUG P1-806 IAW SWPM 20-31-15. SEE ALSO AALA20170123004.

Part: SHUTOFF VALVE — FAULTY (ZONE 500) · airframe 73,267 hrs · 38,482 cycles

AIRCRAFT WAS NOT GROUNDED. DURING TAKEOFF ROLL THE RIGHT FUEL HEAT ANNUNCIATOR ILLUMINATED. TAKE OFF ABORTS AT APPROXIMATELY 10 KNOTS. REMOVED AND REPLACED RIGHT FUEL HEATER SHUTOFF VALVE IAW AMM 73-14-02, RIGHT FUEL DEICING VALVE RELAY R2-129 IAW AMM 24-00-00, AND FUEL HEAT CONTROL PLUG P1-806 IAW SWPM 20-31-15. SEE ALSO AALA20170123003 AND AALA20170123004 (CLOSED)

Part: TARGET — OBSTRUCTED (NLG) · airframe 72,957 hrs · 38,296 cycles

DURING LANDING GEAR EXTENSION THE RED NOSE LANDING GEAR LIGHT ILLUMINATED. APPROACH ABORTED AND RECEIVED VISUAL GEAR DOWN CONFIRMATION FROM TOWER. LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED TROUBLESHOOTING IAW AMM 32-30-00. A FOREIGN OBJECT WAS FOUND BLOCKING THE NOSE LANDING GEAR SENSOR TARGET. OBJECT WAS REMOVED AND A SATISFACTORY NOSE LANDING GEAR SWING ACCOMPLISHED IAW 32-30-00. ALL CHECKS NORMAL . AIRCRAFT WAS GROUNDED.

Part: APU — ODOR (ZONE 100) · airframe 72,790 hrs · 38,193 cycles

FUEL ODOR AFTER LANDING IN COCKPIT AND CABIN SEEMS TO BE CONCENTRATED MORE IN COCKPIT. FOUND APU TO BE SOURCE OF FUEL ODOR. REMOVED AND REPLACED APU IAW MCM 49-96-82.

Part: FUEL CONTROL — FAULTY (APU) · airframe 72,790 hrs · 38,193 cycles

WHEN APU SUPPLYING PACK AFTER LANDING, FUEL SMELL NOTICED IN COCKPIT AND CABIN. ACCOMPLISHED MCM 21-96-01, REMOVED AND REPLACED APU FUEL CONTROL IAW AMM 49-30-01.

Part: HEATING ELEMENT — FAULTY (HEATER) · airframe 71,974 hrs · 37,702 cycles

AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE CREW REPORTED WHITE SMOKE IN FWD CABIN AT SEAT 3A LOWER VENT. FOUND FWD CARGO HEATER CB TRIPPED. AN INSPECTION OF THE FWD CARGO HEATER FOUND FAULTY HEATING ELEMENT. R & R FORWARD CARGO HEATER IAW AMM 21-41-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,091 hrs · 37,178 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN CRACKED FROM FASTENER HOLE AT STATION 189 & LONGERON 22L. ACCOMPLISHED DOUBLER REPAIR IAW DWG SR09530219 & SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

SHEAR TIE CRACKED AFT SIDE OF 1450 FRAME LT SIDE INBD OF LONGERON 3 LT. INSTALLED NEW SERVICEABLE SHEAR TIE AT STATION 1450 INBD OF LONGERON 3 LT IAW SRM 51-30-05.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

CRACKED SHEAR TIE AT STATION 1450 & LONGERON 2 LT. REPLACED SHEAR TIE.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

FASTENER PULLING THROUGH CUSP & TEE ANGLE AT STATION 1250 LT. INSTALLED FREEZE PLUG IN TEE ANGLE, FILLER & STRAP ON CUSP IAW EA MD80-53-036772.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

CUSP T ANGLE LOWER FLANGE OTBD FASTENER HOLE MATERIAL PUSHED DOWN & GOUGED ON LOWER SIDE AT STATION 1249 LT SIDE. INSTALLED REPAIR ON CUSP T & CUSP FILLER, WASHER & DOUBLER IAW EA MD80-53-036772.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,871 hrs · 35,279 cycles

STATION 1250 LT SIDE HAS CORROSION ON THE CUSP DOUBLER. REPLACED CUSP DOUBLER IAW 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

GALLEY MOUNT NR 2 CORRODED AT END OF SEAT TRACK NR 6. INSTALLED NEW GALLEY MOUNT IAW 51-00-05-1 & DWG 5930547.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

GALLEY MOUNT CORRODED AT STATION 218 & RBL 12. INSTALLED NEW GALLEY MOUNT IAW 51-00-00-012.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

SHEAR TIE AT STATION 1437 BETWEEN LONGERONS 2 & 4 RT IS CRACKED AT ATTACH HOLE. INSTALLED NEW SHEAR TIE IAW DWG 9911840 & SRM 53-05-00-001.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

GALLEY MOUNT CORRODED AT STATION 160 & RBL 45. INSTALLED NEW GALLEY MOUNT IAW SRM 51-30-05.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

GALLEY MOUNT CORRODED AT STATION 160 & RBL 51. INSTALLED NEW GALLEY MOUNT IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

LEFT CUSP CORRODED FROM STATION 811 TO 845. INSTALLED NEW CUSP SHEET IAW SRM 53-14-03-001 & DWG 9910151.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

SEAT TRACK NR 1 CORRODED FROM STATIONS 1174 TO 1309. INSTALLED NEW NR 1 SEAT TRACK IAW AMM 53-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,871 hrs · 35,279 cycles

NUMBER 6 SEAT TRACK FROM STATIONS 208 TO 759 CORRODED. REPLACED IAW SRM 53-05-00.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

CRACK EXISTS IN RT LOWER DOUBLER AT LONGERON 2 RT & STATION 1437. REPLACED INNER DOUBLER IAW SRM 51-30-05.

Part: CASTING — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

AFT ACCESSORY AFT FACE OF STATION 1437, VERTICAL STABILIZER SUPPORT CASTING LT SIDE BETWEEN LONGERONS 1 & 2 CRACKED. INSTALLED NEW VERTICAL SUPPORT CASTING IAW PRINT 9911840, 5918088 & SRM 51-30-5.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,871 hrs · 35,279 cycles

AFT CARGO Z ANGLE FROM STATIONS 1143 TO 1155 AT LONGERON 27 RT CORRODED. INSTALLED NEW ANGLE IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

LEFT CUSP FROM STATIONS 845 TO 905 CORRODED. INSTALLED NEW CUSP SHEET IAW 51-00-05-1 & DWG 9910151.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 67,871 hrs · 35,279 cycles

RIGHT FWD TIE DOWN TRACK IN AFT CARGO CORRODED. INSTALLED NEW TRACK IAW SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,871 hrs · 35,279 cycles

CORROSION ON SEAT TRACK NR FROM STATIONS 206 TO 231. INSTALLED SEAT TRACK SPLICE IAW SRM 53-05-00 FIGURE 4F.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

FOUND CRACKED SHEAR CLIP AFT SIDE OF FRAME 1437 BETWEEN LONGERONS 1 & 2 LT. INSTALLED NEW SHEAR CLIP IAW DWG 9911840 & SRM 51-30-05.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

AFT ACCESSORY, STATION 1437 & LONGERON 2 LT, SHEAR TIE CRACKED. INSTALLED NEW SHEAR TIE IAW DWG 9911840-165 & SRM 53-05-00-001.

Part: FORMER — CRACKED (LT WING) · airframe 67,871 hrs · 35,279 cycles

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

Part: FORMER — CRACKED (RT WING) · airframe 67,871 hrs · 35,279 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 67,871 hrs · 35,279 cycles

LEFT WING RIB CRACKED AT XIS 134.546. INSTALLED DOUBLER REPAIR AT XIS 134.546 IAW EA MD80-57-036732.

Part: RIB — CRACKED (RT WING) · airframe 67,871 hrs · 35,279 cycles

RIGHT WING RIB CRACKED AT STATION XIS 134.546. INSTALLED DOUBLER REPAIR IAW EA MD80-57-036732.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

VERTICAL WEB OF FRAME AT STATION 1437 & LONGERON 2 LT CRACKED. INSTALLED WEB REPAIR IAW EA MD80-53-036792.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

SUBFLOOR CORRODED UNDER G1 GALLEY MOUNT AT STATION 160 & RBL 51. CUT OUT CORROSION & INSTALLED DOUBLER IAW 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,871 hrs · 35,279 cycles

CRACK IN FRAME FLANGE AT STATION 1450 AB & LONGERON 3 RT. INSTALLED DOUBLER REPAIR IAW SRM 51-71-05-001 & EA MD80-53-036795.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 67,042 hrs · 34,767 cycles

LEFT NR 1 PORTABLE LIGHT INOPERATIVE. R & R LT NR 1 PORTABLE LIGHT. OPERATIONS CHECKED NORMAL.

Part: WIRE — PINCHED (CABIN) · airframe 65,630 hrs · 33,989 cycles

SEAT PATH EMERGENCY LIGHTS WERE INOPERATIVE IN ALL SEAT ROWS. FOUND PINCHED WIRING UNDER THE LAST SEAT ROW. CORRECTED WIRING ISSUES & REPAIRED PINCHED WIRE.

Part: BUNGEE CYLINDER — BROKEN (LT MLG) · airframe 65,409 hrs · 33,864 cycles

DURING GEAR RETRACTION ON TAKEOFF, LT MAIN GEAR RED LIGHT REMAINED ILLUMINATED AS WELL AS THE AMBER GEAR DOOR OPEN LIGHT. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MAIN GEAR BUNGEE CYLINDER THAT WAS BROKEN. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 64,837 hrs · 33,540 cycles

PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,684 hrs · 32,870 cycles

CANT FRAME 1510 IS CRACKED AT THE TAIL CONE ALIGNMENT PIN AT 11 O` CLOCK POSITION. INSTALLED DOUBLER REPAIR PER SRM 53-01-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,385 hrs · 32,709 cycles

EMERGENCY LIGHTS FROM ROWS 23 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 23 TO 26. OPS CHECK NORMAL.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 60,445 hrs · 31,045 cycles

EVIDENCE OF ARCING UNDER WASHER OF GROUND STUD BOLT. INSTALLED DOUBLER PER EA MD80-53-020594.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 60,386 hrs · 31,011 cycles

SHV - INFLIGHT DFW-EWR. CREW NOTICED ODOR IN THE COCKPIT ACCOMPANIED BY TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. EMERGENCY DECLARED AND ON DESCENT INTO SHV CABIN PRESSURIZATION WAS LOST. FLIGHT LANDED SHV WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DUCT 1701. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,264 hrs · 30,945 cycles

OVERHEAD EMERGENCY LIGHTS BETWEEN AFT LAVATORIES DO NOT ILLUMINATE. REPLACED BATTERY PACK IN RIGHT AFT LAVATORY. OPS CHECKS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 60,264 hrs · 30,945 cycles

ESCAPE PATH LIGHT AT SEAT 12D INOPERTAIVE. SECURED LOOSE CONNECTOR AT SEAT 12D. OPS CHECKS NORMAL.

Part: FLEX LINE — LEAKING (LT PYLON) · airframe 59,996 hrs · 30,780 cycles

DFW - CREW REPORTED LEFT ENGINE NO RESPONSE, 2 KNOB THROTTLE SPLIT, EGT IN AMBER AND N1 & N2 FLUCTUATIONS. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PT7 FLEX LINE GOING INTO PYLON THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSDUCER — INOPERATIVE (ANTI-SKID SYS) · airframe 59,976 hrs · 30,769 cycles

MCO - CREW REPORTED THE RIGHT OUTBOARD ANTI SKID LIGHT ILLUMINATED IN TAKEOFF ROLL. LIGHT CAME BACK ON WHEN GEAR LOWERED AND WENT OUT AND CAME ON SEVERAL TIMES ON APPROACH. EMERGENCY DECLARED FLIGHT LANDED MCO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 4 ANTI SKID TRANSDUCER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — FAULTY (AC BAY) · airframe 58,138 hrs · 29,721 cycles

TUS - CREW REPORTED TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED DURING CLIMBOUT. ACCOMPLISHED QRH PROCEDURES AND LIGHT WENT OUT. EMERGENCY DECLARED FLIGHT RETURNED TUS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RAM AIR VALVE AND THE FOLLWING WIRES - H362F22, H362H20 AND H362G20. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSE LINE — LOOSE (AC BAY) · airframe 58,053 hrs · 29,657 cycles

SJD - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMB OUT. EMERGENCY DECLARED FLIGHT RETURNED SJD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. TIGHTENED LEFT AND RIGHT AUGMENTATION VALVES SENSE LINES THAT WERE LOOSE. REPLACED LEFT TAIL COMPARTMENT HI SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — INOPERATIVE (ACM) · airframe 58,028 hrs · 29,644 cycles

TPA - CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED ON CLIMB. EMERGENCY DECLARED FLIGHT RETURNED TPA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT UPPER AIR CYCLE MACHINE CLAMP AND RIGHT OVERHEAT ELEMENT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,906 hrs · 29,023 cycles

COACH CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT ROW 9. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,906 hrs · 29,023 cycles

COACH CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 14. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,906 hrs · 29,023 cycles

COACH CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 21. OPS CHECKED NORMAL.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 56,739 hrs · 28,925 cycles

MSY - CREW REPORTED LEFT ENGINE GENERATOR CYCLING WITH MULTIPLE ELECTRICAL SYSTEM FAILURES. EMERGENCY DECLARED RETURNED MSY LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE GENERATOR AND CONSTANT SPEED DRIVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

AFT CARGO - CORROSION ON RIGHT TIE DOWN TRACK STATIONS 1212 TO 1287. REMOVED AND REPLACED AFT CARGO RIGHT TIE DOWN TRACK PER SRM 51-30-01 AND SRM 51-01-00-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

CORROSION ON G2 GALLEY TIE DOWN FITTING AT 210 RIGHT BUTTLINE 4. INSTALLED REPLACEMENT INBOARD G2 GALLEY MOUNT AS PER SRM 51-30-05.

Part: CUSP WEB — GOUGED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

CUSP DAMAGED DUE TO NUMBER 6 SEAT TRACK PLUG REPAIR STATION 1072. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: FINGER DOUBLER — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

FINGER DOUBLER UNDER THE RIGHT ALTERNATE PORT INTERNAL DOUBLER HAS MATERIAL MISSING OFF FINGERS. REPAIRED DAMAGED SECTION OF FINGER DOUBLER PER EA MD-80-53-010995.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

SEAT TRACK NUMBER 6 HAS LUG MISSING AT APPROXIMATE STATION 1072. INSTALLED SEAT TRACK PLUG SEAT TRACK NUMBER 6 STATIONS 1070 TO 1075 PER AARD 53-20-00-10.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

AFT CARGO CORROSION ON TIE DOWN TRACK STATIONS 1212 TO 1287 LEFT SIDE. REPLACED TRACK AND SPLICE PARTS DDK3057-1-3-5 AND SPACER 5936660-97 PER SRM 51-30-01.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

UPON REMOVAL OF SUPPORT FOUND HOLE IN CUSP UNDER FLOORBOARD SUPPORT STATION 175.5, INBOARD OF FORWARD ENTRY DOOR. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

INTERCOSTAL IS CRACKED BETWEEN STATION 1287 TO 1309 BETWEEN FLOORBEAMS AT APPROXIMATELY CENTERLINE. INSTALLED NEW INTERCOSTAL PER SRM 51-30-05.

Part: SKIN — BENT (ENTRY DOOR) · airframe 56,730 hrs · 28,918 cycles

FORWARD ENTRY DOOR SKIN BENT AT BOTTOM OF DOOR. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER ESO 80172 AND SRM 52-05-00.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

CORROSION ON SUBFLOOR RIGHT BUTTLINE 20 AT STATIONS 140 TO 146. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 56,730 hrs · 28,918 cycles

RIGHT STATION 788 FORWARD LOWER EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

CORROSION ON SUBFLOOR AT STATION 160 RIGHT BUTTLINE 44. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

CORROSION ON SUBFLOOR RIGHT BUTTLINE 0 TO RIGHT BUTTLINE 4 AT STATIONS 160 TO 166. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

RIGHT CUSP CRACKED AT STATION 243. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

CORROSION ON BOTTOM OF LEFT CUSP STATIONS 1136 TO 1155. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,154 hrs · 29,160 cycles

NUMBER 6 SEAT TRACK CORRODED BEYOND LIMITS AT STATION 546. REPAIRED DAMAGE BY INSTALLING PLUG REPAIR PER AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,154 hrs · 29,160 cycles

NUMBER 3 SEAT TRACK PLUG IS OUT OF LIMITS. REPAIRED CORROSION BY INSTALLING REPAIR PLUG PER AARD 53-20-00-10.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

HEAVY CORROSION ON CABIN SUBFLOOR LEFT BUTTLINE 0 TO LEFT BUTTLINE 12 AT STATIONS 160 TO 200. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME LEG CRACKED JUST FORWARD OF STATION 1041 UPPER AFT RIGHT MARKED. CUT OUT CRACKED AREA OF WINDOW RINGPAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME LEG CRACKED JUST FORWARD OF STATION 906 LEFT LOWER AFT - MARKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,730 hrs · 28,918 cycles

SUBFLOOR RIGHT BUTTLINE 50 AT STATIONS 200 TO 207 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

GUSSETT TO INTERCOSTAL CLIP CRACKED LEFT FUSE STATION 207. REMOVED CLIP FABRICATED AND INSTALLED NEW CLIP PER AARD 53-10-00-11.

Part: PAN — CRACKED (WINDOW) · airframe 56,730 hrs · 28,918 cycles

WINDOW PAN CRACKED AFT OF STATION 886 LEFT UPPER FORWARD CORNER. REPAIRED PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME CRACKED JUST AFT STATION 1022 LEFT LOWER FORWARD - MARKED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

RIGHT CUSP AT STATION 225 CRACKED. REPLACED CUSP SHEET PER AARD 53-20-00-16.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME CRACKED AT STATION 946 RIGHT UPPER FORWARD - MARKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME CRACKED JUST AFT OF STATION 1041 LEFT SIDE LOWER FORWARD CORNER. REMOVED DAMAGED CORNER AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME CRACKED STATION 1022 LEFT JUST FORWARD UPPER AFT LEG - MARKED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME LEG CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,730 hrs · 28,918 cycles

WINDOW FRAME LEG CRACKED AT STATION 1155 RIGHT LOWER AFT LEG. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,730 hrs · 28,918 cycles

WINDOW PAN CRACKED JUST FORWARD OF STATION 946 LEFT UPPER AFT CORNER. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 56,369 hrs · 28,733 cycles

DFW - CREW REPORTED AFTER CLIMB THE RIGHT ENGINE COMPRESSOR STALLED. CREW SHUT DOWN ENGINE (SINGLE ENGINE TIME 15 MINUTES) EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE RIGHT ENGINE AND ISOLATORS AT DFW ON 03/28/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,281 hrs · 28,679 cycles

SEAT EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED FORWARD BATTERY PACK AT ROW 20DEF, OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,281 hrs · 28,679 cycles

EMERGENCY LIGHTS FROM ROWS 9 TO 12 INOPERATIVE. REPLACED BATTERY PACK AT ROW 9 FOR EMERGENCY LIGHTS FROM ROWS 9 TO 12, OPS CHECKS NORMAL.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 55,244 hrs · 28,107 cycles

ON APPROACH RIGHT HYDRAULIC SYSTEM FAILED. LEFT MAIN LANDING GEAR DOOR DAMAGED ON LANDING. REVERSER UNLOCK LIGHT REMAINED ILLUMINATED. FLUID RETURNED TO 6 AFTER SHUTDOWN AND FLAPS RETRACTED. AIRCRAFT OUT OF SERVICE. REPLACED LEFT MAIN LANDING GEAR DOOR. DETERMINED HYDRAULIC LEAK AT RUDDER ACTUATOR. REPLACED RUDDER ACTUATOR.

Part: CUSP WEB — DAMAGED (ZONE 100) · airframe 52,630 hrs · 26,682 cycles

3/8 INCH HOLE IN CUSP LEFT SIDE, AFT OF FRAME 864, APPROXIMATE 10 INCH AFT AND INBOARD 6 3/4 INCH. INSTALLED DOUBLER PER SRM 53-01-00 IN CABIN FLOOR CUSP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 52,197 cycles

DFW EMERGENCY LIGHTS AT OVERHEAD AFT SERVICE DOOR AND TAIL CONE AREA INOPERATIVE. REPLACED BATTERY PACK AT AFT LAVATORY FOR EMERGENCY LIGHTS AT OVERHEAD AFT SERVICE DOOR AND TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — CORRODED (EMERGENCY LIGHT) · airframe 51,492 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 29 INOPERATIVE. CLEANED CORROSION ON BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,492 hrs

LGA - EXTERNAL EMERGENCY LIGHTS AT AFT FUSELADE INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL EMERGENCY LIGHTS AT AFT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT ROW 14DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - FOUND EMERGENCY PATH LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT SEAT ROW 25 INOPERATIVE. RESECURED CONNECTOR AT ROW 25 FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISLODGED (EMERGENCY LIGHT)

LGA - EMERGENCY EXIT SIGNS AT LEFT AND RIGHT HAND OVERWING INOPERATIVE. RESECURED BATTERY PACK FOR EMERGENCY EXIT SIGNS AT LEFT AND RIGHT HAND OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN)

SFO - RIGHT AND LEFT AFT OVERWING EMERGENCY EXIT LIGHTS AT SEAT ROW 21B AND 21D INOPERATIVE. RESEATED BATTERY PACK FOR INOPERATIVE RIGHT AND LEFT AFT OVERWING EMERGENCY EXIT LIGHTS AT SEAT ROW 21B AND 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT SEATS 12D AND 23D INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEATS 12D AND 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — INOPERATIVE (LEFT)

ABOUT 20 MINUTES INTO FLIGHT LEFT OIL PRESSURE LOW LIGHT ON. PRESSURE AND OIL QUANTITY DROPPED TO ZERO. SHUTDOWN LEFT ENGINE PER QRH. OIL TEMPERATURE 80, QUANTITY ZERO NUMBER TWO. 55 PERCENT ENGINE SHUTDOWN. AFTER OIL QUANTITY ZERO THREE MINUTES ENGINE WINDMILLED 23 MINUTES. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY — NOT SEATED (CABIN)

SFO - OVERHEAD EMERGENCY LIGHTS AT ROWS 8 TO 11 INOPERATIVE. RESEATED BATTERIES IN PACKS FOR OVERHEAD EMERGENCY LIGHTS FOR ROWS 8 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — LEAKING (APU)

SJC - CABIN BEGAN FILLING WITH SMOKE SHORTLY AFTER TAKEOFF. RETURNED TO SJC AND LANDED WITHOUT INCIDENT. FOUND APU OIL COOLER SEAL LEAKING. REPLACED APU OIL COOLER SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - OVERHEAD EMERGENCY LIGHTS AT SEATS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK M5107 FOR OVERHEAD EMERGENCY LIGHTS AT SEATS 27 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY SIDE WALL LIGHTS AT AFT STAIRWAY INOPERATIVE. REPAIRED BROKEN WIRE IN TAIL CONE AREA FOR STAIRWAY SIDE WALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ATL - OVERWING EMERGENCY LIGHTS AT ROW 20A AND 20F INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS FOR ROW 20A AND 20F. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY EXIT FLOOR LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN AT RED STRIPE ABOVE MIDDLE OF FORWARD CARGO DOOR. CUT OUT DAMAGE AND INSTALLED FILLER AND INTERNAL AND EXTERNAL DOUBLERS PER SRM 53-04. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

TUL - FOUND CRACK EMITTING FROM FASTENER HOLE STATION 1380 LONGERON 14R. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CABIN FLOOR WEB CRACKED STATION 1300 RIGHT SIDE 9 INCH INBOARD OF CUSP WEB. INSTALLED REPAIR PER ESO80559/6-12-02. (M)

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB)

TUL - FOUND VERTICAL FIN ATTACH ANGLE CRACKED STATION 1408 RIGHT. REPLACED CHORD ANGLE STATION 1408 PER AARD 55-30-00-7. (M)

Part: ATTACH ANGLE — CRACKED (VERTICA STAB)

TUL - FOUND VERTICAL FIN ATTACH ANGLE CRACKED STATION 1428 LEFT. REPLACED CHORD ATTACH ANGLE STATION 1428 PER AARD 55-30-00-1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP ABOVE DOOR CUTOUT STATION 1180. REPAIRED CUSP AS PER AARD 53-00-00-02. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - FOUND SEVERAL SMALL SCRATCHES AND SLIGHT DENT ON LEFT SIDE STATION 237 1 INCH ABOVE CUSP LINE. INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 12B AND AARD 53-30-00-9. (M)

Part: SILL — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON ENTRY PLATE AT FORWARD SERVICE DOOR. REMOVED AND REPLACED ENTRY PLATE SRM 51-01. (M)

Part: TAB — CRACKED (FUSELAGE)

TUL - FOUND TAB CRACKED ON DOOR JAMB BOX WEB AT INTERCOSTAL STATION 207 LONGERON 15L. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-11 PAGE 1 AND 2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND FLOOR SUPPORT CORRODED STATION 1211 ABOVE LONGERON 28L TO 29R. REPLACED FLOOR SUPPORT PER SRM 51-10-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP CORRODED AT STATION RIGHT 712. INSTALLED REPAIR DOUBLER PER AARD 53-00-00-02 PAGES 1-3. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - FOUND DEEP SCRATCHES IN FUSELAGE SKIN AT ANTENNA EDGES. BLENDED OUT SCRATCHES PER SRM 53-04 FIG 38 SHEET 3 CONDITION 2 ALODINED AREA. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

TUL - FOUND STATIC DISCHARGE AFT OF ANTENNA CUT OUT AT STATION 380 BETWEEN L29L-L30. DUE PENNED, NO CRACKS FOUND, POLISHED AREA, APPLIED ALODINE PER SRM 53-04-00 FIG 38 TABLE B SHEET 5 COND 1. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AROUND ANTENNA CUTOUT ON FUSELAGE SKIN AT STATION 380 BETWEEN L29L-L30. BLENDED CORROSION PER SRM 51-01 AND SRM 53-04 FIG 38 TREATED WITH ALODINE, TABLE A COND 2. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS CAME ON WITH POWER OFF. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT INOPERATIVE. REPAIRED OVERWING EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT R1 AND R2 DOOR INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INDICATOR — MALFUNCTIONED (MLG)

DFW - FLT 1764 - AFTER TAKEOFF DURING NOSE GEAR RETRACTION, THE NOSE GEAR POSITION RED INDICATOR REMAINED ILLUMINATED. RECYCLED AND RED LIGHT EXTINGUISHED. FLIGHT CONTINUED AND LANDED DFW WITHOUT INCIDENT. INSPECTED NOSE GEAR SENSORS AND ACCOMPLISHED GEAR SWING. UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: TIRE — FAILED (NR 2 MLG)

LAX - FLT 0889 - ON TAKEOFF, EXPERIENCED A LOUD NOISE OR BANG AT ROTATION. LANDING GEAR HANDLE RAISED AND NOSE GEAR FAILED TO RETRACT. LANDING GEAR HANDLE LOWERED AND NOSE AND RIGHT GEAR CAME DOWN NORMALLY. MAIN LEFT GEAR SHOWED UNSAFE. ACCOMPLISHED A MANUAL GEAR EXTENSION TO NO AVAIL. RETURNED AND LANDED LAX WITHOUT INCIDENT. NR 2 MAIN LANDING GEAR TIRE BLOWN AND WIRE BROKEN ON LT MLG PROXIMITY SWITCH. GREEN DOWN LOCK LIGHT INOPERATIVE. REMOVED AND REPLACED NR 2 MLG TIRE AND WHEEL ASSY. REPLACED WIRE ON LEFT MLG PROXIMITY SWITCH. ACCOMPLISHED GEAR SWING, SYSTEM GROUND CHECKED, NORMAL OPERATION. REPLACED NR 2 ENGINE FOR FOD DAMAGE. (X)

Part: WEB — CORRODED (BS 1155-1161)

TUL - FOUND CORROSION ON CUSP STATION 1155 TO 1161 ABOVE CARGO DOOR CUTOUT. INSTALLED DOUBLER PER AARD 53-00-00 AND CUTOUT DAMAGED AREA. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT FIRST CLASS GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGTH STRIP AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FAN — DEFECTIVE (ACM BAY)

ATL - FLT 0504 - EN ROUTE DFW/ATL. SHORTLY AFTER LEVELLING OFF AT 37,000 FEET, A BURNING SMELL WAS NOTICED IN THE CABIN AND COCKPIT. PULLED RE-CIRCULATION FAN CIRCUIT BREAKERS AND SMELL SEEMED TO DISSIPATE. LANDED ATL WITHOUT INCIDENT. INSPECTED CABIN, COCKPIT, CARGO COMPARTMENTS. NO DEFECTS OR BURNING SMELLS NOTED. REPLACED RE-CIRCULATION FAN AND GROUND SENSE RELAY R2-59. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)