N9622A

Part: LENS — MISSING (CABIN) · airframe 53,139 hrs · 26,058 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT CEILING LIGHT AT ROW 12 RIGHT SIDE HAS A MISSING LENS COVER. REPLACED LENS COVER PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 53,139 hrs · 26,058 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT CEILING LIGHT AT ROW 12 LEFT SIDE HAS A MISSING LENS COVER. REPLACED LENS COVER PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 53,139 hrs · 26,058 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT CEILING LIGHT AT ROW 14 LEFT SIDE HAS A MISSING LENS COVER. REPLACED LENS COVER PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 52,779 hrs · 25,812 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE DEPLOYED. ACCOMPLISHED EVACUATION SLIDE INSTALLATION PER AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: MECHANISM — FAULTY (SLIDING WINDOW) · airframe 52,659 hrs · 25,730 cycles

AIRCRAFT WAS GROUNDED. CAPTAINS CLEARVIEW SLIDING WINDOW WILL NOT OPEN. REMOVED AND REPLACED UPPER LOCK BAR (AALA201708219073) AND CAM FORWARD/AFT ADJUSTMENT LOCK ASSEMBLY PER AMM 56-10-03. OPERATIONAL AND LEAK CHECK GOOD.

Part: BAR — FAULTY (SLIDING WINDOW) · airframe 52,659 hrs · 25,730 cycles

AIRCRAFT WAS GROUNDED. CAPTAINS CLEARVIEW SLIDING WINDOW WILL NOT OPEN. REMOVED AND REPLACED UPPER LOCK BAR AND CAM FORWARD/AFT ADJUSTMENT LOCK ASSEMBLY (AALA201708229020) PER AMM 56-10-03. OPERATIONAL AND LEAK CHECK GOOD.

Part: MECHANISM — DAMAGED (COCKPIT) · airframe 52,539 hrs · 25,658 cycles

AIRCRAFT WAS NOT GROUNDED. FIRST OFFICER'S WINDOW CAME OUT OF WINDOW FRAME. REPLACED WINDOW FORWARD UPPER SLIDE HARDWARE PER AMM 56-10-03.

Part: TRANSMITTER — FAULTY (EPR SYSTEM) · airframe 52,361 hrs · 25,552 cycles

AIRCRAFT WAS GROUNDED. TUS-DFW FLIGHT ABORTED TAKEOFF AT 15 KNOTS ACCOUNT LEFT ENGINE PRESSURE RATIO INDICATION. REMOVED AND REPLACED LEFT ENGINE PRSSURE RATIO TRANSMITTER PER AMM 77-11-02 AND ENGINE DISPLAY PANEL PER AMM 77-42-00 (AALA201707129011). OPERATIONAL CHECK GOOD.

Part: WARN PANEL — FAULTY (COCKPIT) · airframe 52,361 hrs · 25,552 cycles

AIRCRAFT WAS GROUNDED. TUS-DFW FLIGHT ABORTED TAKEOFF AT 15 KNOTS ACCOUNT LEFT ENGINE PRESSURE RATIO INDICATION. REMOVED AND REPLACED LEFT ENGINE PRSSURE RATIO TRANSMITTER PER AMM 77-11-02 (AALA201707119013) AND ENGINE DISPLAY PANEL PER AMM 77-42-00. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 52,214 hrs · 25,470 cycles

FWD ENTRY DOOR FLASHLIGHTS ONE HAS RED FLASHING LED ONE HAS NO RED LED FLASHING. REMOVED AND REPLACED THE FLASHLIGHT. OPS CHECKED NORMAL IAW MM 25-60-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,199 hrs · 25,463 cycles

EMERGENCY EXIT SIGN ON THE RIGHT SIDE OF THE L2 DOOR IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 51,990 hrs · 25,329 cycles

FLIGHT ATTENDANT FLASHLIGHT AT THE L1 DOOR IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTTERY IAW AMM 25-60-00-901-801. OPS CHECKED GOOD.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 51,801 hrs · 25,222 cycles

PORTABLE EMERGENCY LIGHT FLASHLIGHT PORTION INOP. REMOVED AND REPLACED PORTABLE LIGHT ASSY. OPS CKED NORMAL PER MM 33-53-00. THE AIRCRAFT WAS NOT GROUNDED.

Part: PORTABLE LIGHT — FAULTY (CABIN) · airframe 51,440 hrs · 24,987 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY PORTABLE LIGHT AT L1 DOOR IS ON WHILE IN THE OFF POSITION. REMOVED AND REPLACED LIGHT IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 51,440 hrs · 24,987 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS AT SEAT 28D ARE INOPERATIVE. RECONNECTED SEAT LIGHT PLUG IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,257 hrs · 24,867 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM THE EXIT ROW BACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK AB5-3 AND BATTERY PACK AB5-4(AALA20170125022) IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,257 hrs · 24,867 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM THE EXIT ROW BACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK AB5-3(AALA20170125005) AND BATTERY PACK AB5-4 IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: NOZZLE — STICKING (OUTFLOW VALVE) · airframe 50,799 hrs · 24,570 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING DESCENT THE NR 1 PRESSURIZATION CONTROLLER FAILED WITH THE NR 2 PREVIOUSLY PLACARDED. DIFFERENTIAL PRESSURE WENT TO MAXIMUM AND CABIN ALTITUDE WENT BELOW SEA LEVEL. CREW REVERTED TO MANUAL PRESSURIZATION CONTROL. MAINTENANCE FOUND THE OUTFLOW VALVE NOZZLE STICKING IN THE CLOSED POSITION. CLEANED DIRT AND DEBRIS FROM NOZZLE AND ACCOMPLISHED OPERATIONAL CHECK IAW AMM 21-32-05. SYSTEM CHECKS NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 49,966 hrs · 24,067 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY WAS DECLARED, LANDING UNEVENTFUL. DURING CLIMB, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. MAINTENANCE ACCOMPLISHED MCM 36-95-14. REPAIRED ALL LEAKS.

Part: APU — CONTAMINATED (APU BAY) · airframe 49,797 hrs · 23,968 cycles

SMOKE & ODOR REPORTED IN THE CABIN. IDENTIFIED APU OIL INGESTION AS SOURCE. REMOVED AND REPLACED AUXILIARY POWER UNIT IAW MCM 49-96-83. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 49,776 hrs · 23,956 cycles

AIRCRAFT WAS IN BASE MX. FWD ENTRY DOOR INTERIOR BEAM NR 6 IS CRACKED. REPAIRED BEAM IAW AARD 52-10-00-3.

Part: FITTING — CRACKED (RT SPOILER) · airframe 49,776 hrs · 23,956 cycles

AIRCRAFT WAS IN BASE MX. RT WING GND SPOILER FITTING IS CRACKED AT THE INBD FWD CORNER. R & R FITTING IAW SRM 51-01-00-001.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,776 hrs · 23,956 cycles

AIRCRAFT WAS IN BASE MX. MID CARGO DOOR FWD STOP PAD FITTING, 2ND FROM TOP, IS CRACKED. R & R FITTING IAW AARD 51-00-05-1, DWG 5910141 & CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,776 hrs · 23,956 cycles

AIRCRAFT WAS IN BASE MX. FWD CARGO DOOR FWD STOP FITTING, 3RD FROM BOTTOM IS CRACKED. R & R STOP FITTING IAW AARD 51-00-05-1, DWG 5910141 & CDK-2345.

Part: ACTUATOR — FAULTY (OUTFLOW VALVE) · airframe 49,610 hrs · 23,845 cycles

AIRCRAFT WAS NOT GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH, AT 25,000 FEET, AUTO PRESSURIZATION CONTROLLER NR 1 BECAME INOPERATIVE. SWITCHED TO NR 2 & CABIN ALTITUDE WENT TO SEA LEVEL. R & R THE OUTFLOW ACTUATOR IAW AMM 32-21-05. ACCOMPLISHED BITE CHECK IAW AMM 21-32-00-201 WITH NO FAULTS FOUND.

Part: CASTING — CRACKED (LT SPOILER) · airframe 49,237 hrs · 23,600 cycles

FOUND 3 INCH CRACK IN LT WING INBD GND SPOILER CASTING. R & R LT GND SPOILER CASTING IAW AARD 51-00-05-1. ACFT IN BASE MX.

Part: FLOORBEAM — WORN (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

LOWER FLANGE OF FLOORBEAM WORN AT STATION 655 & RBL 12. REPAIRED FLOORBEAM IAW EA 53-037697 DATED 12/1/2014.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

FORWARD ENTRY AREA GUSSET CRACKED AT FS 210 & LONGERON 11 LT. REPAIRED GUSSET IAW 53-10-00-11 & SRM 51-30.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

FORWARD ENTRY AREA GUSSET CRACKED AT FS 210 & LONGERON 15 LT. REPAIRED GUSSET IAW 53-10-00-11 & SRM 51-30.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

NUMBER 6 SEAT TRACK IS CORRODED BETWEEN STATIONS 797 & 1088. REPAIRED SEAT TRACK IAW SRM 53-05-00 FIG 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

NUMBER 4 SEAT TRACK CORRODED BETWEEN FUSELAGE STATIONS 1240 & 1309. REPAIRED SEAT TRACK IAW SRM 53-05-00-001.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

AFT CARGO RT AFT TIE DOWN TRACK CORRODED BETWEEN FUSELAGE STATIONS 1212 & 1322 AT STRINGER 17 RT. R & R TRACK SECTION IAW SRM 51-30-05.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

AFT CARGO DOOR SILL BEAM WEB CORRODED AT FUSELAGE STATION 1195 & RBL 14. R & R WEB IAW SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

SEAT TRACK NR 6 IS CORRODED BETWEEN FUSELAGE STATIONS 212 & 588. R & R SEAT TRACK SECTION IAW AMM 53-40-01-2 & EA 53-037669 DATED 12/08/2014.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

RIGHT CARGO TIE DOWN TRACK CORRODED AT FUSELAGE STATIONS 1135. R & R TRACK SECTION IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

RIGHT CUSP CORRODED BETWEEN FUSELAGE STATIONS 218 & 238. R & R CUSP IAW AARD 53-20-00-16.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

FUSELAGE TO VERTICAL STABILIZER RT SKATE ANGLE IS CRACKED AT FUSELAGE STATION 1463. REPAIRED SKATE ANGLE IAW SRM 53-05-00-001 SHEET 3.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

HOLE IN LT CUSP AT FUSELAGE STATION 845. REPAIRED CUST IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

RIGHT CUSP CORRODED BETWEEN FUSELAGE STATIONS 160 & 198. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

RIGHT CUSP CORRODED BETWEEN FUSELAGE STATIONS 200 & 280. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

LEFT CUSP SHEET CORRODED BETWEEN FUSELAGE STATIONS 838 & 853. REPAIRED CUSP SHEET IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

LEFT CUSP AT FUSELAGE STATION 1297 IS CRACKED AT LIGHTNING HOLE. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

G4 GALLEY MOUNT AT FUSELAGE STATION 1174 IS CORRODED. R & R GALLEY MOUNT IAW DWG 5930566.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

LEFT CUSP CORRODED BETWEEN FUSELAGE STATIONS 1174 & 1177 OTBD OF NR 1 SEAT TRACK. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

RIGHT CUSP CORRODED AROUND VENT HOLE AT FUSELAGE STATION 380. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

SEAT TRACK NR 1 IS CORRODED BETWEEN FUSELAGE STATIONS 1174 & 1309. R & R SEAT TRACK IAW SRM 53-05-00-001 & AMM 53-40-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

RIGHT CUSP CRACKED BETWEEN FUSELAGE STATIONS 803 & 805 OTBD OF SEAT TRACK NR 6 AT STRINGER 18 RT. R & R CUSP IAW AARD 51-00-05-1, DWG 9910151 CONFIGURATION -514 & EA 53-037672 DATED 12/8/2014.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

NOSE LANDING GEAR RT AFT DOOR HINGE CUT OUT SKIN IS CRACKED AT FUSELAGE STATION 101.5. REPAIRED SKIN IAW SRM 53-05-00 FIG 62.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

AFT CARGO DOOR BEAM IS CORRODED BETWEEN FUSELAGE STATIONS 1155 & 1212 AT STRINGER 18 RT. REPAIRED BEAM IAW AARD 53-10-00-3.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 46,253 hrs · 21,895 cycles

FORWARD CARGO DOOR SKIN IS GOUGED & BENT ALONG THE LOWER AFT EDGE. R & R DOOR SKIN IAW ESO 80174 PAGE 601E DATED 07/28/2010 & ESO 80174 PAGE 601 2 C 1 DATED 09/15/2010.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

CORROSION ON AFT SIDE 1157 DOOR CORNER BRACKET AT RBL 18. R & R BRACKET IAW SRM 51-01-00-001 & DWG 5930483.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

SEAT TRACK NR 4 STATION 1060 HAS A GOUGED & WORN SPOT AT FUSELAGE STATION 1060. REPAIRED TRACK IAW AARD 53-20-00-10.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,253 hrs · 21,895 cycles

G2 GALLEY MOUNT AT NR 6 SEAT TRACK & FUSELAGE STATION 216 IS CORRODED. R & R GALLEY MOUNT IAW SRM 51-30-02.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

SUBFLOOR IS CRACKED AT FUSELAGE STATION 217 BELOW SEAT TRACK NR 4. REPAIRED SUBFLOOR IAW AARD 53-20-00-16.

Part: RIB — CRACKED (RT WING) · airframe 46,253 hrs · 21,895 cycles

RIGHT LE RIB CRACKED AT WING STATION XIS 134.546. REPAIRED RIB IAW EA 57-037704 DATED 12/10/2014.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

SUPPORT FITTING CRACKED AT LOWER END BELOW NR 5 SEAT TRACK AT FS 927. R & R FITTING IAW AARD 51-00-05 & DWG 9936637.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 46,253 hrs · 21,895 cycles

ELONGATED HOLE IN RT CUSP SHEET AT SEAT TRACK ATTACH HOLE AT FS 826. R & R SECTION OF CUSP FROM FS 807 - 845.

Part: RIB — CRACKED (LT WING) · airframe 46,253 hrs · 21,895 cycles

LEFT LE RIB CRACKED AT WING STATION XIS 134.546. REPAIRED RIB IAW EA 57-037704 DATED 12/10/2014.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,704 hrs · 21,585 cycles

CEILING EMER LIGHTS FROM ROWS 27 TO 32 FAILED TEST. REPLACED EMER LIGHT BATTERY PACK B5-107.

Part: PORTABLE LIGHT — FAILED (CABIN) · airframe 45,704 hrs · 21,585 cycles

LEFT NR 1 DOOR PORTABLE EMER LIGHT FAILED TEST. REPLACED LT NR 1 DOOR PORTABLE EMER LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 44,543 hrs · 20,977 cycles

PORTABLE EMERGENCY LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LT NR 1 DOOR. OPERATIONS CHECKED NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 44,543 hrs · 20,977 cycles

EMERGENCY EXIT SIGN BY FWD LAVATORY WALL INOPERATIVE. TERMINATED WIRES AT QUICK DISCONNECTS FOR EXIT LIGHT AT FWD LAVATORY WALL. OPERATIONS CHECKED NORMAL.

Part: WIRE HARNESS — CHAFED (STAB MOTOR) · airframe 43,445 hrs · 20,410 cycles

STL PILOT REPORTED 2 OF 3 PRIMARY TRIM CIRCUIT BREAKERS POPPED. AIRCRAFT REMOVED FROM SERVICE. UPON MAINTENANCE CHECK, FOUND WIRE BUNDLE FOR PRIMARY TRIM MOTOR ARCED AGAINST FRAME. REPAIRED WIRING AT P10-399 PR1 STAB MOTOR. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SHROUD — DAMAGED (CABIN) · airframe 42,197 hrs · 19,697 cycles

EMERGENCY PATH LIGHT AT SEAT 26D DAMAGED. REPLACED LIGHT SHROUD FOR SEAT 26D EMERGENCY PATH LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,197 hrs · 19,697 cycles

CEILING EMERGENCY LIGHT AT SEAT 8B INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT AT SEAT 8B. OPS CHECK NORMAL

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 42,197 hrs · 19,697 cycles

EMERGENCY PATH LIGHTING SIGN ACROSS FROM FIRST CLASS LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATH LIGHTING SIGN ACROSS FROM FIRST CLASS LAVATORY. OPS CHECK NORMAL

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 42,197 hrs · 19,697 cycles

FORWARD EMERGENCY PATH LIGHTING AT SEAT 21D INOPERATIVE. CONNECTED LOOSE CONNECTOR AT SEAT 21D. OPS CHECK NORMAL.

Part: PUMP — OVERHEATED (HYDRAULIC SYS) · airframe 40,881 hrs · 19,030 cycles

DFW - CREW REPORTED LEFT HAND HYDRAULIC TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: IRU — FAILED (ZONE 100) · airframe 38,514 hrs · 17,849 cycles

CREW REPORTED RIGHT INERTIAL REFERENCE UNIT FAILED. FLIGHT LANDED WITHOUT INCIDENT. REPLACED RIGHT INERTIAL REFERENCE UNIT. SYSTEM GROUND CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,542 hrs · 17,386 cycles

EMERGENCY LIGHTS FROM ROWS 23 TO 27 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN 25DEF. OPS CHECKS NORMAL.

Part: COALESCER BAG — MISSING (AC BAY) · airframe 36,281 hrs · 16,761 cycles

DFW - FLIGHT ATTENDANTS REPORTED SMOKE AND ODOR IN THE CABIN AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SOCK MISSING FROM LEFT WATER SEPARATORS. REPLACED RIGHT AND LEFT SEPARATORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 35,823 hrs · 16,546 cycles

WHILE PERFORMING FUNCTIONAL CHECK AND TEST OF EMERGENCY LIGHT SYSTEM FOUND EMERGENCY EGRESS LIGHTS IN AFT ACCESSORY COMPARTMENT INOPERATIVE. RE-SEATED BATTERY PACK IN AFT RIGHT LAVATORY. OPS CHECK NORMAL.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

STRUCTURE AROUND AUXILIARY POWER UNIT EXHAUST DUCT DISCOLORED. REPAIRED STRUCTURE PER MD80-53-012914.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

LONGERON 12 RIGHT FOUND TO HAVE HEAT DAMAGE AT AUXILIARY POWER UNIT EXHAUST EXIT CUTOUT AT STATION 1409 TO STATION 1418. REPAIRED LONGERON 12 RIGHT PER EA MD80-53-012914.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,601 hrs · 15,951 cycles

FORWARD LOWER ANGLE HAS CORROSION STATION 1287 LONGERON 26 LEFT TO LONGERON 28 RIGHT. INSTALLED J-ANGLE REPAIR AS PER AARD 53-10-00-14 AT STATION 1287.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

INTERCOSTAL AT STATIONS 1287 TO 1307 AND LEFT BUTTLINE 0 BELOW CABIN FLOORBOARD IS CRACKED AT FLOORBOARD ATTACH HOLE. INSTALLED INTERCOSTAL AT STATIONS 1287 TO 1307 AND LEFT BUTTLINE 0 BELOW CABIN FLOORBOARD PER SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

INTERCOSTAL JUST RIGHT HAND OF CENTER BETWEEN FLOOR BEAMS AT STATION 1271 AND 1287 IS CRACKED AFT END. INSTALLED NEW INTERCOSTAL PER SRM 51-30-05.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

CUSP SHEET DAMAGED STATIONS 389 TO 503. INSTALLED SERVICABLE CUSP SHEET PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

TEMPORARY CUSP REPAIR INSTALLED AT RIGHT STATION 370. INSTALLED PERMANENT REPAIR PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

CRACK IN FRAME FORWARD SIDE OF STATION 1418 LONGERON 2 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,601 hrs · 15,951 cycles

CORROSION ON LOWER SURFACE OF LEFT CUSP AT STATION 593. INSTALLED NEW CUSP SHEET, STATION 579-598, LEFT SIDE, PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

CRACK ON FRAME FORWARD SIDE OF STATION 1418 LONGERON 2 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,601 hrs · 15,951 cycles

CUSP SHEET RIGHT SIDE STATIONS 503 TO 598 HAS CORROSION. INSTALLED NEW CUSP SHEET RIGHT STATIONS 503 TO 598 PER EA MD80-53-012782, AARD 53-20-00-16, AND SRM 51-30-02 AND 51-30-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,601 hrs · 15,951 cycles

AFT CARGO - AFT LOWER ANGLE HAS CORROSION STATION 1271 LONGERON 27 LEFT TO LONGERON 29 RIGHT. REMOVED CORROSION AND INSTALLED J-ANGLE REPAIR PER EA MD80-53-012908.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

RIGHT CUSP SHEET HAS A HOLE AT STATION 711. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,601 hrs · 15,951 cycles

CORROSION ON LONGERON SPLICE FORWARD END STATION 1293 LONGERON 30. INSTALLED NEW SPLICE PER SRM 53-14-03.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

DAMAGE ON CUSP SHEET STATION 598 TO 617. INSTALLED SERVICEABLE CUSP SHEET PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

CORROSION ON CUSP RIGHT STATION 389. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

SEAT TRACK NUMBER 4 BLENDED OUT OF LIMITS AT STATION 757 TO 761. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR PLUG PER SRM 53-05-00 FIGURE 4A AND AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

SEAT TRACK NUMBER 4 BLENDED OUT OF LIMITS AT STATION 725 TO 730. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR PLUG PER SRM 53-05-00 FIGURE 4A AND AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,601 hrs · 15,951 cycles

CORROSION ON LEFT CUSP AT STATION 470 OUT OF LIMITS. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,601 hrs · 15,951 cycles

SUBFLOOR CORRODED AROUND POTABLE WATER LINE HOLE APPROXIMATE STATION 151 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 34,601 hrs · 15,951 cycles

WINDOW PAN CRACKED RIGHT STATION 1022 UPPER AFT CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 34,601 hrs · 15,951 cycles

WINDOW PAN CRACKED RIGHT STATION 946 UPPER FORWARD CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: CONTROL VALVE — DEFECTIVE (THRUST REVERSER) · airframe 32,905 hrs · 15,190 cycles

JFK - INFLIGHT ORD-LGA. CREW REPORTED ON APPROACH LEFT ENGINE THROTTLE WAS NOT ABLE TO MOVE OR ADJUST ENGINE POWER SETTING. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. UPON LANDING CREW SHUT DOWN ENGINE. AIRCRAFT REMOVED FROM SERVICE. REPLACED THRUST REVERSER CONTROL VALVE SECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIMIT SWITCH — OBSTRUCTED (THROTTLE) · airframe 32,875 hrs · 15,177 cycles

SJC - INFLIGHT DFW-SFO. CREW REPORTED LEFT ENGINE THROTTLE STUCK MID-RANGE. EMERGENCY DECLARED DIVERTED SJC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED DEBRIS THEN CLEANED AND LUBED THROTTLE LIMIT SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION (CLOSED) / MAINT: REMOVED DEBRIS. CLEANED AND LUBED THROTTLE LIMIT / SWITCHES. THROTTLES OPS CHECK NORMAL PER MM 76-11-00-5.

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW O2) · airframe 32,580 hrs · 15,048 cycles

CREW NOTED THAT CREW OXYGEN BOTTLE INDICATED LOW. LANDED SLC WITHOUT INCIDENT. REPLACED CREW OXYGEN BOTTLE.

Part: GENERATOR — FAILED (NR 2 ENGINE) · airframe 32,136 hrs · 14,855 cycles

INFLIGHT PHL TO DFW. CREW REPORTED RIGHT ENGINE GENERATOR ON FIRST OFFICER INSTRUMENTS BEGAN TO FLICKER AND WENT OFF FOLLOWED BY AC CROSS-TIE. THE APU WAS INOPERATIVE. LANDED CMH WITHOUT INCIDENT. REPLACED THE RIGHT CONSTANT SPEED DRIVE GENERATOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,370 hrs · 14,501 cycles

EMERGENCY LIGHT BATTERY PACK WILL NOT HOLD CHARGE. REPLACED BATTERY PACK.

Part: DOOR — OPEN (NLG) · airframe 30,511 hrs · 14,131 cycles

DFW - DURING CLIMB AS LANDING GEAR WAS RAISED, CREW REPORTED LOUD RUSHING NOISE AND FELT VIBRATIONS FROM THE NOSE GEAR AREA. EMERGENCY DECLARED, RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. UPON ARRIVAL FOUND NOSE GEAR DOOR OPEN. RESET DOOR CLOSED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 29,997 hrs · 13,917 cycles

ORD - CREW ADVISED, UNABLE TO FEED FUEL FROM THE LEFT TANK. THE CAPTAIN WAS CONNECTED TO TULSA TECH. NO SOLUTION WAS FOUND FOR THE PROBLEM. THE FLIGHT RETURNED TO ORD AND LANDED ORD WITHOUT INCIDENT. REPLACED CENTER FUEL BOOST PUMPS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LINK — INOPERATIVE (MLG) · airframe 28,397 hrs · 28,397 cycles

SFO - INFLIGHT T1544/16 JUL. CREW REPORTED VIBRATION AND NOISE DURING CLIMB. ACFT DID FLYBY AT SFO AND NOTICED RT FORWARD NOSE GEAR DOOR OPEN. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED RT FORWARD NOSE GEAR DOOR LINK. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: CONNECTOR — CORRODED (FIRE DETECTION) · airframe 27,863 hrs

AMA INFLIGHT T1661/17MAY DFW TO SEA. AFT CARGO FIRE INDICATION. FIRE BOTTLE DISCHARGED. LANDED AMA WITHOUT INCIDENT. NO EVIDENCE OF FIRE. FOUND CARGO ELECTRONICS UNIT CONNECTOR WITH CORROSION. REPLACED AFT CARGO ELECTRONICS UNTIL CONNECTOR AND FIRE BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: FIRE DETECTOR — FAULTY (CARGO BAY) · airframe 27,673 hrs

ABQ INFLIGHT T1178/24APR SFO TO DFW - CREW REPORTED B SYSTEM CARGO FIRE WARNING. CAPTAIN DECLARED EMERGENCY AND LANDED ABQ WITHOUT INCIDENT. NO INDICATION OF FIRE FOUND. REPLACED NUMBER ONE AND TWO FIRE EXTINGUISHER BOTTLES AND AFT FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN COCKPIT AT LOCATION 5 23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT SEAT ROWS 19 TO 22 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT SEAT ROWS 19 TO 22. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

STL - EMERGENCY LIGHT AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NLG)

ORD - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF, HAD RED NOSE GEAR LIGHT ON WITH HANDLE UP. GEAR EXTENDED OK. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND NOSE STRUT NEEDED SERVICE. SERVICED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

EMERGENCY LIGHT ABOVE CAT WALK IN TAIL COMPARTMENT INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT ABOVE CAT WALK IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - CEILING EMERGENCY LIGHT FROM ROW 15 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROWS 15-17. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR AFT CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BATTERY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 11,731 hrs · 5,873 cycles

DURING CHECK-C AFT CARGO, AFT CARGO COMPT FLOOR TRACK LT SIDE FROM STA 1211 TO STA 1322 HAS CORROSION IN NUT PLATE LUG HOLES. EVALUATED CORROSION WHICH REQUIRED PART REPLACEMENT, REMOVED OLD PART AND INSTALLED NEW PART PER SRM 51-10-4 AND SPM 6-70-01.

Part: BATTERY PACK (B5-23) · airframe 10,719 hrs · 5,272 cycles

THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-25-01 STL. --CLOSED--

Part: BATTERY PACK (FWD CABIN) · airframe 10,138 hrs · 4,932 cycles

THE EGRESS LIGHTING IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-25-01 STL. --CLOSED--

Part: BATTERY PACK · airframe 9,453 hrs · 4,592 cycles

DURING MAINTENANCE THE EXIT LIGHT OVER THE RIGHT AND LEFT OVER WING EXITS WERE INOP DUE TO WEAR.REPLACED BATTERY PACK P/N 60-0304-51LB.LAST CHECK C 07/25/01 STL ---CLOSED---

Part: POWER SUPPLY · airframe 9,453 hrs · 4,592 cycles

DURING MAINTENANCE THE EGRESS LIGHTS BETWEEN ROW 25 AND 26 WERE INOP. DUE TO WEAR. REPLACED POWER SUPPLY P/N 60-0304-51LB PER MM 33-51-00.LAST CHECK C 07/25/01 STL. ---CLOSED---

Part: POWER SUPPLY (B5-28) · airframe 9,341 hrs · 4,534 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 25 BACK. REPLACED THE POWER SUPPLY. CHECK-C 8-3-00 STL. --CLOSED--

Part: SWITCH — FAILED (COCKPIT)

COCKPIT, WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION THE LIGHTS ILLUMINATED. SECURED TERMINAL ON BACK OF COCKPIT SWITCH AND RESET THE CIRCUIT BREAKER. CHECK-C 8-4-9 STL.

Part: BATTERY PACK — INOPERATIVE (CABIN)

THE COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE WITH THE SWITCH IN THE ON POSITION. REPLACED THE BATTERY PACK. CHECK-C 8-4-99 STL.

Part: POWER SUPPLY — INOP (PAX DOOR)

THE EMERGENCY EXIT LIGHTS IN THE COCKPIT WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-4-99 STL.

Part: WIRE — LOOSE (ROW 15-20)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 15 TO 20, AND 24 TO 26. RECONNECTED LOOSE WIRING AT BOTH LOCATIONS.

Part: BULB — FAILED (LT/RT EXTERIOR)

BOTH LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED BULBS.