N566AA

Part: BATTERY — FAULTY (CABIN) · airframe 89,803 hrs · 41,357 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY LIGHTS BETWEEN ROW 12 AND 18 ILLUMINATE WHEN POWER IS TURNED OFF. REMOVED AND REPLACED BATTERY ASSEMBLY AT ROW 13D IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL IAW AMM 33-53-00.

Part: BATTERY — FAULTY (CABIN) · airframe 89,803 hrs · 41,357 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY LIGHTS BETWEEN ROW 12 AND 18 ILLUMINATE WHEN POWER IS TURNED OFF. REMOVED AND REPLACED BATTERY ASSEMBLY AT ROW 20D IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 89,803 hrs · 41,357 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY LIGHTS BETWEEN ROW 28 AND 31 ILLUMINATE WHEN POWER IS TURNED OFF. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL IAW AMM 33-53-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 89,546 hrs · 41,186 cycles

EMERGENCY LIGHTS ROW 27-32 FAILED TO TEST. REPLACED THE POWER SUPPLY IAW AMM 33-53-00. TESTED OK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 89,546 hrs · 41,186 cycles

EMERGENCY LIGHTS ROW 11-17 FAILED TO TEST. REPLACED THE POWER SUPPLY IAW AMM 33-53-00. TESTED OK.

Part: POWER SUPPLY — NO TEST (EMEGENCY LIGHTS) · airframe 89,546 hrs · 41,186 cycles

FORWARD INTERIOR EMERGENCY EXIT LIGHTS FAIL TO TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-53-00. TEST OK.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 89,324 hrs · 41,065 cycles

DURING CLIMB THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE ADJUSTED THE RIGHT MAIN LANDING GEAR PROXIMITY SENSOR IAW AMM 32-60-05. OPS CHECKED NORMAL.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 88,354 hrs · 40,478 cycles

AIRCRAFT WAS GNDED. CABIN FLOOR PANEL BETWEEN SEATS 20B & 20D REPORTED TO BE SOFT. FOUND FLOOR PANEL SUPPORTS, 2 EACH, CRACKED. R & R SUPPORTS. SEE ALSO AALA 20160317006.

Part: FLOOR SUPPORT — DAMAGED (CABIN) · airframe 88,354 hrs · 40,478 cycles

AIRCRAFT WAS GNDED. CABIN FLOOR PANEL, BETWEEN SEATS 20B & 20D, REPORTED TO BE SOFT. MX FOUND FLOOR PANEL SUPPORTS, TWO EACH, CRACKED. R & R SUPPORTS. SEE ALSO AALA 20160330009.

Part: WIRE — BURNED (COCKPIT) · airframe 87,113 hrs · 39,769 cycles

FLIGHT 1010, WHILE AT CRUISE ALTITUDE, EXPERIENCED SMOKE IN THE COCKPIT EMANATING FROM THE THROTTLE QUADRANT. SEVERAL CBS WERE POPPED. DECLARED EMER, DIVERTED & PERFORMED CHECKLISTS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. REPLACED BURNED WIRING TO CONNECTOR P1-430, CONNECTOR P1-430 & SWITCH S1-4.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 85,424 hrs · 38,828 cycles

DURING CRUISE, LT HYD SYS LOST PRESS & QTY. FOUND 2 HYD LINES CHAFED & LEAKING IN THE 48 SECTION LT SIDE NEAR THE HYD FILTER MODULE. R & R HYD LINES. PERFORMED LEAK CHECK IAW MM 20-12-01. SYS CHECKED NORMAL. SUBMITTED IN CONJUNCTION WITH SUPPLEMENTAL FOR AALA20150123001 TO DOCUMENT 2ND TUBE PART NR.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 85,423 hrs · 38,827 cycles

DURING CRUISE, THE LT HYD SYS LOST PRESSURE & QTY. EMERGENCY DECLARED, AND LANDING UNEVENTFUL. FOUND TWO HYD LINES CHAFED & LEAKING IN THE 48 SECTION LT SIDE NEAR THE HYD FILTER MODULE. REMOVED AND REPLACED HYDRAULIC LINES AND PERFORMED LEAK CHECK PER MM 20-12-01. SYSTEM CHECKED NORMAL.

Part: ENGINE — FIRE (RIGHT) · airframe 85,280 hrs · 38,756 cycles

DURING THE SECOND ABORT OF A RT ENGINE EXTERNAL AIR START FIRE WAS REPORTED BY GND CREW. FUEL LEVER WAS ALREADY IN OFF POSITION ENG WAS SPOOLED IN AN ATTEMPT TO EXTINGUISH FIRE. GND CREW REPORTED FLAMES STILL PRESENT. RT ENGINE FIRE HANDLE PULLED & WHILE GROUND CREW USED THEIR FIRE BOTTLE. R & R RT ENGINE IAW AMM 71-91-99 & 71-91-03. OPS CHECKS PERFORMED. SYS CHECKED NORMAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 84,781 hrs · 38,482 cycles

CRACKED SHEAR TIE AT STATION 1437 BETWEEN LONGERONS 12 & 13 RT. REPLACED SLIP IAW AARD 51-00-05-1 & DWG 9911840.

Part: FORMER — CRACKED (LE SLAT) · airframe 84,711 hrs · 38,444 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 (LE SLAT) · airframe 84,711 hrs · 38,444 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: CASTING — CRACKED (LE SLAT) · airframe 82,277 hrs · 37,167 cycles

RT WING INBD NR 4 SLAT CASTING CRACKED. REPAIR DOUBLER INSTALLED IAW EA MD80-57-032266.

Part: CASTING — CRACKED (LE SLAT) · airframe 82,277 hrs · 37,167 cycles

LT WING INBD NR 4 SLAT TRACK CASTING CRACKED. REPAIR DOUBLER INSTALLED IAW EA MD80-57-032266.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 82,269 hrs · 37,159 cycles

DFW CREW REPORTED LT ENG MADE A LOUD THUD & ROLLED BACK TO IDLE WITH ALL INDICATIONS NORMAL FOR IDLE. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT HAND ENGINE AT DFW ON 11/07/2013. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: CONTROL VALVE — INOPERATIVE (CABIN TEMP) · airframe 82,210 hrs · 37,129 cycles

DFW BOTH CABIN TEMPERATURE CONTROLS INOPERATIVE. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT TEMPERATURE CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CSD — FAILED (LT ENGINE) · airframe 81,980 hrs · 37,001 cycles

DFW CREW REPORTED LT GENERATOR FAILED DURING CRUISE. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONSTANT SPEED DRIVE TRANSMISSION. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 81,801 hrs · 36,889 cycles

EMERGENCY LIGHTS IN THE TAIL CONE AREA INOPERATIVE. REPLACED B5-28 POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 81,801 hrs · 36,889 cycles

EMERGENCY LIGHT ABOVE AFT FLIGHT ATTENDANT SEAT & IN TAIL CONE AREA INOPERATIVE. REPLACED 5-27 POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: FITTING — CRACKED (FUSELAGE) · airframe 81,230 hrs · 36,567 cycles

CRACK NEXT TO SEAT TRACK SUPPORT VERTICAL FITTING BELOW NR 3 SEAT TRACK AT STA 830 ON WEBBING. INSTALLED DOUBLER IAW SRM 51-70-04.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,230 hrs · 36,567 cycles

LEFT CUSP CORRODED AT STATION 1155 AROUND HOLE 12" FROM DOOR JAMB. INSTALLED LT CUSP DOUBLER REPAIR AND FILLER AT STATION 1155 IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,230 hrs · 36,567 cycles

CORROSION UNDER AFT GIRT BAR SUPPORT, ON CUSP, AT AFT SERVICE DOOR. INSTALLED CUSP DOUBLER, FILLER AND AFT GIRT BAR ANGLE SUPPORT AT AFT SERVICE DOOR, UNDER AFT GIRT BAR SUPPORT IAW AARD 53-20-00-16 AND AARD 51-00-05-01.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

LONGERON 3 LEFT CRACKED AT STATION 160. REPLACED LONGERON 3 LEFT AND SPLICE FROM STATIONS 148 TO 200 PER SRM 53-02-00 FIGURE 18 AND BOEING AAL-AAL-13-0838-07C.

Part: FRAME — CRACKED (ZONE 200) · airframe 80,835 hrs · 36,371 cycles

FRAME CRACKED AT THE LOWER END BELOW VENTRAL STAIR ACTUATOR. ACCOMPLISHED SPLICE REPAIR IAW 53-10-00-33, FIG 2.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,835 hrs · 36,371 cycles

CORROSION ON FORWARD CARGO DOOR OPENING FROM STATIONS 636 TO 693. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,835 hrs · 36,371 cycles

CORROSION BELOW DOOR STOP ON BOTTOM OF FRAME (AFT CARGO DOOR CUTOUT LOWER THRESHOLD). INSTALLED BEAM DOUBLER PER AARD 53-10-00-3.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

AFT CARGO, LOWER DOOR FRAME BRACKET CRACKED AT STATION 1212. REPLACED BRACKET.

Part: SPAR — CRACKED (RT WING) · airframe 80,835 hrs · 36,371 cycles

RIGHT WING SPAR CRACKED AT OUTBOARD FLAP HINGE, LOWER INBOARD HOLE AT WING STATION XRS 164. ACCOMPLISHED REAR SPAR REPAIR PER EA MD80-57029767 AND BOEING DWG J060165.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,835 hrs · 36,371 cycles

CORROSION ON LONGERON 22 LEFT AT STATION 1285. INSTALLED NEW LONGERON AND SPLICES PER SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

LONGERON 2 RIGHT IS CRACKED AT THE OUTBOARD LEG AFT OF STATION 1418. INSTALLED LONGERON AND SPLICE REPAIR PER SRM 53-02-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

FRAME AFT SIDE OF STATION 1418 AT LONGERON 2 RIGHT CRACKED. INSTALLED DOUBLER AND FILLER PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,230 hrs · 36,567 cycles

CUSP SHEET AFT OF STA 1174 RT CORRODED ON OTBD EDGE ABOVE AIR VENT. INSTALLED DOUBLER FROM RT STA 1174 TO 1189 IAW AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

LONGERON 4 LEFT CRACKED AT STATION 160. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

CENTER STIFFENER ABOVE VAULT DOOR CRACKED AT STATION 1338. INSTALLED NEW SERVICABLE VERTICAL STIFFENER ABOVE VAULT DOOR AT STATION 1338 PER AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

STATION 807, LEFT CUSP MEMBRANE CRACKED/FASTENER SHEARED AT HORSE COLLAR FASTNER HOLE. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

RIGHT CUSP SHEET CRACK AT STATION 843 HORSE COLLAR FASTENER HOLE. INSTALLED DOUBLER FROM STATIONS 841 TO 845 PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,835 hrs · 36,371 cycles

CABIN, LONGERON 4 LEFT CRACKED, JUST FORWARD OF STATION 541. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18 SHEET 1.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 78,383 hrs · 35,108 cycles

ATL - FLIGHT ATTENDANTS REPORTED ELECTRICAL BURNING SMELL AND SMOKE IN AFT CABIN. EMERGENCY DECLARED FLIGHT RETURNED ATL LANDED WITHOUT INCIDENT. REPLACED BALLAST AT SEAT 26AB THAT WAS BAD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COALESCER BAG — DIRTY (ZONE 100) · airframe 78,133 hrs · 34,993 cycles

CREW REPORTED A BURNING ELECTRIC ODOR CAME THROUGH ENTIRE AIRCRAFT. PASSENGER REPORTED A BLUE FLASH OUTSIDE OF AIRCRAFT. EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED GROUND INSPECTION PRECAUTIONARY LIGHTNING STRIKE STATIC DISCHARGE CARD 05-91-25. NO DAMAGE FOUND. ACCOMPLISHED PACK BURN AND REPLACED RIGHT AND LEFT COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,902 hrs · 34,878 cycles

SHEAR TIE CRACKED AT STATION 1418 BETWEEN LONGERON 1 AND 2 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-20 AND EA MD80-53-021383.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,510 hrs · 34,175 cycles

CEILING EMERGENCY LIGHT AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,510 hrs · 34,175 cycles

EXIT SIGN BY AFT GALLEY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EXIT SIGN BY AFT GALLEY DOOR. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,673 hrs · 32,740 cycles

CRACK STATION 1510 FRAME LOWER RIGHT SIDE AT ALIGNMENT PIN. INSTALLED DOUBLER PER SRM 53-01.

Part: STRUT — LOW PRESSURE (NLG) · airframe 72,640 hrs · 32,242 cycles

ORD - INFLIGHT DAY-DFW. CREW REPORTED AFTER TAKEOFF THE NOSE LANDING GEAR WOULD NOT RETRACT. EMERGENCY DECLARED FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED NOSE GEAR STRUT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OXYGEN BOTTLE — LOW PRESSURE (OXYGEN SYSTEM) · airframe 71,203 hrs · 31,599 cycles

INFLIGHT ORD TO SFO. CREW OXYGEN BOTTLE PRESSURE DROPPED TO ZERO DURING FLIGHT. FLIGHT DIVERTED TO DEN DUE TO PART AVAILABILITY. LANDED DEN WITHOUT INCIDENT. REPLACED CREW OXYGEN BOTTLE. NO LEAKS NOTED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

CORROSION ON AFT CARGO LEFT TIE DOWN TRACK AT MOUNT SCREW HOLES AND FLOORBOARD ATTACH HOLES, REMOVED CORRODED SECTION OF TRACK AND INSTALLED NEW TRACK AND SPLICE AT STATION 1117 PER SRM 53-05-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,237 hrs · 30,677 cycles

INTERCOSTAL ANGLE CRACKED ABOVE CENTER FUEL TANK BETWEEN STATION 826 AND 845 ON RIGHT SIDE OF COMPARTMENT. REPAIRED PER EA MD80-53-005456.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

LEFT TIE DOWN TRACK HAS CORROSION ON FLANGE FROM STATION 1211 TO 1271. INSTALLED SERVICEABLE TIE DOWN TRACK PER SRM 51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

NR 6 SEAT TRACK CORRODED STATION 216 TO 229, REMOVED AND REPLACED SEAT TRACK PER SRM 53-40-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,237 hrs · 30,677 cycles

CORROSION ON FLOORBOARD SUPPORT STATION 1150-1155 INBOARD OF RIGHT TIEDOWN TRACK. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

FRAME LOWER FLANGE HAS CORROSION AT STATION 1309 ABOVE LONGERON 30, INSTALLED NEW LOWER CHANNEL L28L TO L28R PER SRM 53-03 FIGURE 2A.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 69,237 hrs · 30,677 cycles

ANGLE CRACKED AT FORWARD LOWER CLIP FITTING AREA. REMOVED AND REPLACED ANGLE ON BOTTOM OF DOOR PER ESO 80174.

Part: ANGLE — CRACKED (DOOR) · airframe 69,237 hrs · 30,677 cycles

ANGLE INSIDE LOWER AFT DOORSTOP STRAP IS CRACKED. REPLACED ANGLE UNDER LOWER AFT STRAP PER ESO 80174.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,237 hrs · 30,677 cycles

GOUGE AND DENT IN SKIN AT STATION 1466 ABOVE L6L. INSTALLED DOUBLER PER SRM 53-01.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

FUSELAGE SKIN BULGED AT LONGERON 29R FROM STATION 725 TO 730, CUT OUT CORROSION. INSTALLED CLASS II DOUBLER REPAIR PER SRM 53-04-00 FIGURE 12B, AND ESO 80559 DATED 2/11/09.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

CORROSION ON RIGHT CUSP AT STATION 219. INSTALLED NEW CUSP SHEET FROM STATION 218 TO STATION 237 PER SRM 51-30-05 AND 51-30-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,237 hrs · 30,677 cycles

DENT IN SKIN AT CANT STATION 1417 BELOW L6L. INSTALLED DOUBLER PER SRM 51-50-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,237 hrs · 30,677 cycles

LEFT CUSP STATION 218, LONGERON 18 LEFT IS CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

CORROSION ON FORWARD GIRT BAR ATTACH CHANNEL AT STATION 1140. INSTALLED NEW FORWARD GIRT BAR ATTACH CHANNEL PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

CORROSION ON BOTTOM OF CUSP STATION 522 TO 541 RIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 69,237 hrs · 30,677 cycles

VERTICAL SUPPORT FOR FLOORBEAM AT STATION 927 RIGHT ABOVE CENTER FUEL TANK CRACKED. INSTALLED NEW VERTICAL SUPPORT PER SRM 51-01.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

CORROSION ON AFT GIRT BAR ATTACH FITTING CHANNEL AT STATION 1170. INSTALLED NEW GIRT BAR ATTACH FITTING CHANNEL PER SRM 51-01-00.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 69,237 hrs · 30,677 cycles

NR 3 SEAT TRACK LUG EAR AT STATION 579 IS BROKEN OFF, INSTALLED REPAIR PLUG PER SRM 53-05 FIGURE 4A.

Part: FITTING — CRACKED (LE SLAT) · airframe 69,237 hrs · 30,677 cycles

LEFT NR 5 SLAT, SECOND FROM OUTBOARD SLAT RIB FITTING IS CRACKED AT NR 14 SLAT TRACK ATTACH. REMOVED AND REPLACED ATTACH FITTING PER ESO 80117.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,237 hrs · 30,677 cycles

CORROSION ON WEBBING FROM STATION 1212 TO 1218, L26R TO L28R, REMOVED CORRODED SECTION AND INSTALLED NEW WEB PER SRM 51-01-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,237 hrs · 30,677 cycles

DENT IN FUSELAGE SKIN AT STATION 1303 BELOW LONGERON 18R FROM COWL DRAIN MAST DAMAGE. INSTALLED TWO ROW INTERNAL DOUBLER PER SRM 53-04 FIGURE 38.

Part: FITTING — CRACKED (LE SLAT) · airframe 69,237 hrs · 30,677 cycles

LEFT NR 5 SLAT OUTBOARD RIB FITTING CRACKED AT NR 15 SLAT TRACK ATTACH POINT. REMOVED AND REPLACED OUTBOARD ATTACH FITTING PER ESO 80117.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — MALFUNCTIONED (RIGHT)

DFW INFLIGHT DURING CLIMB AT 4000 FEET AIRCRAFT ENCOUNTERED A COMPRESSOR STALL FROM NUMBER 2 ENGINE. SUBSEQUENT POWER APPLICATIONS CAUSED REPEATED SURGES. SHUT RIGHT HAND ENGINE DOWN AND PULLED FIRE HANDLE AS PRECAUTION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CONFIRMED NO FIRE. ACCOMPLISHED FLIGHT DATA RECORDER DOWNLOAD. ENGINE GAS TEMPERATURE 777 DEGREES AND SURGE TO POWER. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NLG)

SEA - INFLIGHT LANDING GEAR HANDLE STUCK HALF WAY UP ON GEAR RETRACTION ON TAKEOFF. FOUND NOSE STRUT BINDING. SERVICED NOSE STRUT WITH OIL AND NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CABLE — OVERHEATED

TUL - GENERATOR WIRE FEEDER CABLE (APU) LEFT HAND AUXILIARY RELAY FEEDER CABLE NUMBER 3X1C2A AND 3X1D2A SHOW SIGNS OF OVERHEATING. REPLACED FEEDER CABLES MADE FROM ESO 81249. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - OVERHEAD EMERGENCY LIGHTS AT ROWS 25 TO 29 INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 25 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

AUS - EMERGENCY LIGHT BATTERY PACK AT AFT RIGHT LAVATORY FORWARD POSITION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT LAVATORY FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COUPLING — DISCONNECTED (RT WING)

FSD - FLT 1887 - EN ROUTE ORD-SEA, CENTER TANK AT 12,500 LBS, LT MAIN TANK AT 9,400 LBS AND BOOST PUMPS ON, CROSSFEED CLOSED. THE RT MAIN FUEL QUANTITY WAS DECREASING FROM 9,400 LBS. RT MAIN QUANTITY DECREASED 3,000 LBS IN 30 MIN. AILERON TRIM WAS INCREASING CONFIRMING FUEL IMBALANCE. INSPECTION OF THE RT WING INFLIGHT DID NOT INDICATE LEAK. RT ENGINE WAS SHUT DOWN. LANDED FSD WITHOUT INCIDENT. NO EXTERNAL FUEL LEAKS NOTED. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FOR UNWANTED FUEL TRANSFER RT WING TANK TO CENTER TANK. RECONNECTED GAMMA COUPLING AND SECURED. FILLED RT WING TANK, FOUND NO TRANSFER BACK TO CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LONGERON — CRACKED (FS 160)

TUL - FOUND LONGERON NR 4 LEFT CRACKED AT STATION 160. REPAIRED PER SRM 53-02 WITH LONGERON SPLICE. (M)

Part: BEAM — CORRODED (FS 1174/1192)

TUL - FOUND CORROSION UNDER DOOR STOPS AT AFT CARGO DOOR LOWER CUTOUT. COMPLETED DOOR JAMB REPAIR PER AARD 53-10-00-3 AND SRM 51-10-3. (M)

Part: LONGERON — CRACKED (FS 160)

TUL - FOUND LONGERON NR 3 LEFT CRACKED AT STATION 160. ERPAIRED PER SRM 53-02 WITH LONGERON SPLICE. (M)

Part: SKIN — CORRODED (FS 579)

TUL - FOUND DENT IN SKIN NEXT TO DOUBLER STATION 579 BETWEEN LONGERON 29L-30R. REMOVED REPAIRED DOUBLER NEXT OT DENT. INSTALLED LARGER DOUBLER OVER DENT PER ESO-80559, DATED 6/1/2001. (M)

Part: CAP — CORRODED (FUSELAGE)

TUL - FOUND CORROSION 2 INCHES BY 4 INCHES AROUND FASTENERS ON LONGERON 23R AT STATION 1220. REMOVED AND INSTALLED NEW END CAP ON LONGERON PER SRM 51-01. (M)

Part: WEB — DAMAGED (FS 693)

TUL - FOUND WEB UNDER RIGHT FLOORBOARD SUPPORT DAMAGED AT STATION 693. REPAIRED WEB PER AARD 53-10-00-24. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT CARGO RIGHT TIE DOWN STRAP AROUND FASTENER HOLES FROM STATION 1211 TO STATION 1255 IN UPPER AND LOWER SURFACES. INSTALLED NEW RIGHT TIE DOWN STRAP PER SRM 53-20-00-3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND LEFT CUSP CRACKED AT LIGHTENING HOLE BETWEEN STATION 218 AND STATION 229. INSTALLED DOUBLER PER SRM 53-01 PAGE 18 FIG 4. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, LOWER RIGHT OVER WING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LOWER RIGHT OVER WING EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: DUCT — LEAKING (A/C BAY)

DFW - FLT 1507 - EN ROUTE DFW-YVR - ON TAKEOFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURE, DECLARED EMERGENCY AND LANDED DFW WITHOUT FURTHER INCIDENT. INSTALLED NEW DUCT ASSEMBLY IN AFT ACCESSORY COMPARTMENT, PERFORMED HIGH PRESSURE DUCT LEAK CHECK. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT PORTABLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS FROM ROWS 21 TO AFT, INOPERATIVE. REPAIRED WIRE AT SEAT 30. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SUPPORT — BROKEN (RT MLG)

SJC - FLT 1157 - DURING APPROACH SJC, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. GEAR WAS CYCLED WITH NO CHANGE. AIRCRAFT LANDED WITHOUT AND STOPPED ON TAXI WAY FOR LANDING GEAR DOOR INSPECTION. GEAR DOORS WERE FOUND IN THE UP AND LOCKED POSITION AND AIRCRAFT TAXIED TO GATE. MAINTENANCE FOUND R IGHT MAIN LANDING GEAR DOOR TARGET BRACKET BROKEN. REPLACED RIGHT MAIN LANDING GEAR DOOR TARGET BRACKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: B NUT — LOOSE (APU)

ORD - FLT 0447 - AFTER TAKEOFF, FLIGHT CREW SMELLED AND SAW SMOKE IN COCKPIT. FLIGHT ATTENDANT CONFIRMED THE SAME IN THE FORWARD CABIN. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED APU AND FOUND A LOOSE B-NUT AT TEE FITTING. TIGHTENED B-NUT AT TEE FITTING WITH NO FURTHER LEAK NOTED. RAN PACKS AND ACCOMPLISHED BURN-OUT WITH NO SMOKE NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

ATL - DURING OVERNIGHT CHECK, EMERGENCY LIGHT AT FORWARD GALLEY DOOR INOPERATIVE. REPAIRED BROKEN WIRE AT FORWARD GALLEY DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUT SEALS — WORN (NLG)

TUL - FLT 1917 - AFTER TAKEOFF TUL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO TUL AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SEALS. REPLACED NOSE GEAR STEERING BYPASS VALVE. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECK NORMAL. (M)

Part: BEAM — CORRODED (BS 1155-1211)

TUL - DOOR CUTOUT, LOWER BEAM CORRODED BETWEEN STATION 1155-1211. REMOVED CORROSION, BEYOND MANUAL LIMITS. INSTALLED DOUBLER PER SRM 53-10-00-3. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 3-6 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)