N965TW

Part: FRAME — WORN (BS 1380) · airframe 52,852 hrs · 26,838 cycles

WORN FRAME AT BS 1380, BETWEEN STRINGERS 4L AND 5L. REPAIRED THE FRAME IAW 53-10-00-28.

Part: FRAME — CRACKED (BS 1401) · airframe 52,852 hrs · 26,838 cycles

CRACKED FRAME AT BS 1401. LONGERON 1L. REPAIRED THE FRAME IAW SRM 53-01-00, FIGURE 2.

Part: LONGERON — CRACKED (BS 1418) · airframe 52,852 hrs · 26,838 cycles

CRACKED LONGERON 2R, BS 1418. REPAIRED THE LONGERON IAW SRM 53-03-001, AND 53-02-00-001.

Part: LONGERON — CRACKED (BS 1418) · airframe 52,852 hrs · 26,838 cycles

CRACKED LONGERON 2L, BS 418. REPAIRED THE LONGERON IAW SRM 53-02-00-001, AND 53-02-001.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,425 hrs · 26,571 cycles

EMERGENCY LIGHT FAILED A DUAL FEED CHECK. REPLACED THE BATTERY PACK IAW AMM 33-60-98.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,425 hrs · 26,571 cycles

THREE EMERGENCY LIGHTS AT THE AFT ENTRY WERE INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: SLIDE — FAILED (L1 DOOR) · airframe 52,381 hrs · 26,545 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR SLIDE FAILED PREFLIGHT INSPECTION. REPLACED L1 DOOR SLIDE PER 25-94-19.

Part: HINGE — LACK OF LUBE (SERVICE DOOR) · airframe 52,329 hrs · 26,512 cycles

AIRCRAFT WAS GROUNDED: AFT GALLEY SERVICE DOOR, EXTERIOR HANDLE, WOULD NOT RETRACT TO A FAIRED POSITION WHEN DOOR WAS CLOSED AND LOCKED. MAINTENANCE LUBRICATED AFT GALLEY SERVICE DOOR EXTERIOR HANDLE HINGE PER AMM 12-21-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FAN — FAULTY (RECIRCULATION) · airframe 52,215 hrs · 26,440 cycles

DURING CLIMB OUT, WITH CLIMB POWER PASSING 11,000 FT, ENTIRE ACFT HAD A FAINT ELECTRICAL BURNING ODOR, DISSIPATED AFTER TURNING OFF THE RECIRCULATION FAN. REPLACED CABIN RECIRCULATING FAN IAW AMM 21-20-12. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,159 hrs · 25,758 cycles

AIRCRAFT WAS NOT GROUNDED. 1L DOOR FLASHLIGHT LED DOES NOT FLASH. REMOVED AND REPLACED BATTERY IN EMERGENCY FLASHLIGHT BY L1 DOOR PER AMM 25-60-00. OPERATIONS CHECK GOOD.

Part: SLIDE — DAMAGED (AFT SERVICE DOOR) · airframe 51,058 hrs · 25,688 cycles

FOUND AFT LEFT SERVICE DOOR SLIDE DAMAGE AT GIRT BAR FLAP. REPLACED THE SLIDE IAW MCM 25-94-17.

Part: GIRT BAR — INADEQUATE (R1 DOOR) · airframe 51,045 hrs · 25,682 cycles

R1 DOOR GIRT BAR FLAP NOT INSTALLED CORRECTLY. R1 DOOR SLIDE WAS FOUND IN SERVICEABLE CONDITION WITH EXCESSIVE GIRT OUTSIDE OF PACK ENCLOSURE. RE-TUCKED EXCESSIVE GIRT INTO ENCLOSURE PER AMM 25-62-00.

Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 50,439 hrs · 25,275 cycles

EMERGENCY DECLARED. RIGHT MAIN LANDING GEAR DOWN GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR DOWN SELECTED. LANDING GEAR APPEARED TO BE NORMAL AS NOTED FROM TOWER FLY BY. LANDING UNEVENTFUL. REMOVED AND REPLACED BURNED OUT RIGHT GEAR DOWNLOCK BULBS. OPERATIONAL CHECK IAW AMM 32-60-03 GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 50,318 hrs · 25,196 cycles

AIRCRAFT WAS GROUNDED. UPON GEAR EXTENSION THE LEFT MAIN GEAR NEVER GOT A GREEN DOWN LIGHT. THE BULB DID NOT TEST GOOD, BUT AN EMERGENCY GEAR EXTENSION WAS MADE. A LOW PASS WAS DONE AND TOWER STATED THE GEAR APPEARED TO BE DOWN. UNEVENTFUL LANDING. AFTER LANDING THE GEAR WAS PINNED BEFORE TAXI IN. REMOVED AND REPLACED THE GREEN DOWN AND LOCKED LAMPS. PERFORMED PSEU BITE CHECK PER AMM 32-60-00 AND CHECKED MAIN GEAR INBOARD DOOR OPERATION. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,249 hrs · 25,157 cycles

THE AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS SEATS FIRST HALF WERE INOP. EMERGENCY LIGHT BATTERIES WERE FOUND DISCHARGED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES FORWARD AND MID, OPS OK.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 50,163 hrs · 25,102 cycles

THE AFT SERVICE DOOR SLIDE HAS LOW PRESSURE. R & R THE L2 DOOR SLIDE IAW MCM CARD 25-94-17.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 50,139 hrs · 25,090 cycles

THE AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS ON END OF SEATS INOP FROM ROW 3 TO ROW 19. REPLACED POWER SUPPLY, CHECKS NORMAL PER AMM 33-50-00. (SEE ALSO SDR AALA201707259018)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,139 hrs · 25,090 cycles

THE AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS ON END OF SEATS INOP FROM ROW 3 TO ROW 19. REPLACED BATTERY PACK, CHECKS NORMAL PER AMM 33-50-00. (SEE ALSO SDR AALA201707249056)

Part: SKIN — CRACKED (BS 1474) · airframe 49,852 hrs · 24,928 cycles

TWO SKIN CRACKS LOCATED AT BS 1474, MEASURING 1 INCH AND 1/2 INCH PREVIOUSLY INTERIM REPAIRED IAW 53-30-00-4. PERMANENT REPAIR IAW EA 270647A, SRM 53-01-00, DWG 53-30-00-02, AND DWG 51-60-00-04. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (BS 1474) · airframe 49,765 hrs · 24,872 cycles

FUSELAGE SKIN CRACKED LEFT, AFT TAIL SECTION BS 1474 IN TWO PLACES MEASURING 1 INCH AND 1/2 INCH. REPAIRED IAW EA 270647A, SRM 53-01-00, DWG 53-30-00-02, AND DWG 51-60-00-04.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,519 hrs · 24,713 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. MIDDLE CARGO DOOR STOP PAD FITTING IS CRACKED AT TOP AFT EDGE OF DOOR. INSTALLED NEW DOOR STOP FITTING IAW AARD 51-00-05-1 AND DRAWING 5910141.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,519 hrs · 24,713 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT ACCESSORY COMPARTMENT SHEAR TIE CRACKED FORWARD SIDE OF FUSELAGE STATION 1380 ABOVE LONGERON 13R. REPAIRED IAW AARD 53-10-10-20.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,519 hrs · 24,713 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT AFT NOSE LANDING GEAR DOOR HINGE CUTOUT CRACK AT FUSELAGE STATION 94.55. REPAIRED IAW SRM 53-05-00-001 PARAGRAPH 162 FIGURE 158.

Part: LIGHT — MISSING (CABIN) · airframe 49,519 hrs · 24,713 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. SEAT MOUNTED EMERGENCY ESCAPE PATH MARKING LIGHT ASSEMBLY AT SEAT 13D IS MISSING. INSTALLED LIGHT ASSEMBLY IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 49,519 hrs · 24,713 cycles

EMERGENCY EXIT LIGHTS BATTERY PACK AT B5-105 IS WEAK. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-53-00. OPERATIONAL CHECKED GOOD.

Part: LIGHT — MISSING (EMERGENCY LIGHT) · airframe 49,519 hrs · 24,713 cycles

EMERGENCY LIGHT MISSING AT 13D. INSTALLED MISSING EPM LIGHT ASSY AT SEAT 13D AND OPS CHECKED IAW AMM 33-60-98.

Part: LENS — MISSING (CABIN) · airframe 49,343 hrs · 24,595 cycles

EXIT LIGHT COVER AT R1 DOOR IS MISSING. REPLACED LENS COVER FWD GALLEY EMERGENCY EXIT SIGN PER MM 33-50-00. THE AIRCRAFT WAS NOT GROUNDED.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 49,132 hrs · 24,460 cycles

AIRCRAFT WAS GROUNDED. FUMES IN CABIN DUE TO AUXILIARY POWER UNIT INGESTION OF HYDRAULIC FLUID. TIGHTENED B-NUT ON LEFT THRUST REVERSER CONTROL VALVE. ACCOMPLISHED APU WASH AND PACK BURNOUT IAW MCM 49-97-11 AND 21-92-12. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 48,889 hrs · 24,309 cycles

AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR INBOARD SEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 48,838 hrs · 24,273 cycles

AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 46,584 hrs · 22,849 cycles

WITH AUTO CONTROLLER NR 1 INOPERATIVE ON MEL, NR 2 CONTROLLER FAILED AFTER TAKEOFF. THE CREW DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. THE ACFT WAS GNDED. R & R OUTFLOW VLV ACTUATOR IAW MM 21-32-05. PRESSURIZATION FUNCTIONS NORMAL IAW 21-32-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,230 hrs · 22,632 cycles

AIRCRAFT WAS NOT GNDED. FWD OVERWING EXIT EMER LIGHT WILL NOT TURN OFF. R & R BATTERY PACK B5-103 IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: SEAL — DEFECTIVE (FLASHLIGHT) · airframe 46,202 hrs · 22,618 cycles

AIRCRAFT WAS NOT GNDED. FLASHLIGHT AT NR 1 FLIGHT ATTENDANT JUMP SEAT IS NOT CHARGING. REPLACED TAMPER SEAL ON FLASHLIGHT AT NR 1 FLIGHT ATTENDANT JUMP SEAT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,989 hrs · 22,497 cycles

LEFT CANT FRAME 1474, JUST ABOVE LOUVER CUT OUT INNER ANGLE CRACKED. MANUFACTURED & INSTALLED NEW ANGLE IAW SRM 51-30-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,989 hrs · 22,497 cycles

FUSELAGE L20L IS CRACKED AT STATION 995. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-18.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,989 hrs · 22,497 cycles

CUSP CORRODED BEYOND LIMITS AT STATIONS 1148 - 1150 RT. REMOVED & INSTALLED NEW CUSP SHEET IAW SRM 51-01-00 & DWG 9930612.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,989 hrs · 22,497 cycles

RIGHT CANT FRAME 1474, JUST ABOVE LOUVER BOX, CUT OUT HAS DELAMINATION, CORROSION & A CRACKED ANGLE. MANUFACTURED NEW FRAME SPLICE & INSTALLED IAW SRM 51-70-05-001, SRM 51-01-00-001, SRM 51-30-05 & AARD 51-00-00-1. CORROSION LEVEL 2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,989 hrs · 22,497 cycles

AFT CARGO COMPARTMENT, CTR SECTION OF LT TIE DOWN TRACK AT L26L IS CORRODED, BETWEEN STATIONS 1136 - 1212. R & R TIE DOWN TRACK SECTION, BETWEEN STATION 1221 - 1108 IAW SRM 51-30-01 & SRM 51-30-05.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,989 hrs · 22,497 cycles

AFT CARGO FRAME 1268 IS CORRODED, BETWEEN LBL 4 & RBL 4. INSTALLED FRAME SPLICE REPAIR IAW SRM 53-03-00-001.

Part: FITTING — CRACKED (RT WING) · airframe 45,989 hrs · 22,497 cycles

RIGHT WING GND SPOILER ACTUATOR CASTING, WING SIDE, IS CRACKED IN RADIUS AT FWD OTBD SIDE. R & R SPOILER ACTUATOR FITTING IAW SRM 51-30-02 & SRM 51-30-05.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,989 hrs · 22,497 cycles

CRACK IN ANGLE, BOTTOM FWD END OF INTERCOSTAL AT STATION 826, BELOW SEAT TRACK 5. REPAIRED ANGLE IAW SRM 51-70-05 & EA 255879.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,989 hrs · 22,497 cycles

AFT CARGO COMPARTMENT, LT AFT TIE DOWN TRACK AT L26L IS CORRODED, BETWEEN STATIONS 1218 - 1271. R & R TRACK SECTION, BETWEEN STATIONS 1212 - 1322 IAW SRM 51-30-01 & SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,989 hrs · 22,497 cycles

NUMBER 6 SEAT TRACK, OTBD BOTTOM FLANGE IS CORRODED BEYOND LIMITS AT STATION 1153. R & R AFT SECTION OF NR 6 TRACK, BETWEEN STATIONS 10908 - 1307 IAW AMM 53-40-01-2.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,989 hrs · 22,497 cycles

CORROSION ON RT SIDE OF E & E CEILING, BETWEEN STATION 134 - 150. R & R SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: OIL COOLER — FAULTY (CSD) · airframe 45,289 hrs · 22,070 cycles

AT LEVEL OFF, DURING CLIMB LT CSD OIL PRESSURE LOW LIGHT ILLUMINATED ACCOMPANIED BY HIGH CSD TEMP INDICATION. DIVERTED, AND LANDING UNEVENTFUL. APU PREVIOUSLY PLACARDED OUT OF SERVICE. R & R LT CSD IAW AMM 24-10-01 & LT CSD OIL COOLER IAW AMM 24-10-03. PERFORMED LEAK CHECK IAW AMM 24-10-01. SYS CHECKED NORMAL.

Part: CSD — FAULTY (LEFT) · airframe 45,289 hrs · 22,070 cycles

AT LEVEL OFF DURING CLIMB, LT CSD OIL PRESSURE LOW LIGHT ILLUMINATED ACCOMPANIED BY HIGH CSD TEMP INDICATION. APU PREVIOUSLY PLACARDED OUT OF SERVICE. DIVERTED AND LANDING UNEVENTFUL. R & R LT CSD IAW AMM 24-10-01, LT CSD OIL COOLER IAW AMM 24-10-03. PERFORMED LEAK CHECK IAW AMM 24-10-01. SYS CHECKED NORMAL. SEE ALSO AALA20150727008.

Part: ENGINE — POWER LOSS (LEFT) · airframe 44,604 hrs · 21,670 cycles

ON SETTING TAKEOFF POWER LEFT EPR WENT TO 1.45 WOULD NOT ADVANCE. ALL OTHER ENG GAUGES INDICATED NORMAL. REJECTED TAKEOFF AT 75 KNOTS. CHECKED FLIGHT FAULT REVIEW, NO FAULTS FOUND. DRAINED MOISTURE TRAP. INSPECTED EPR TRANSMITTER LINES. RAN ENG, SYS CHECKED NORMAL.

Part: BLEED VALVE — FAULTY (RT ENGINE) · airframe 44,582 hrs · 21,653 cycles

RIGHT ENGINE COMPRESSOR STALL AFTER START UP. R & R RT ENGINE START BLEED VALV EIAW AMM 75-31-01. COMPLETED WC 72-93-11 ON RT ENGINE. PERFORMED ENG RUN WITH NO COMPRESSOR STALL NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,475 hrs · 21,588 cycles

FORWARD ENTRY DOOR EMER LIGHT INOPERATIVE. R & R LIGHT. SYS CHECKED NORMAL.

Part: TEE FITTING — LEAKING (HYD SYSTEM) · airframe 44,172 hrs · 21,406 cycles

AIRCRAFT LOST LT HYD SYS FLUID DURING FLIGHT. MAINTENANCE FOUND TEE FITTING OF LEFT THRUST REVERSER CONTROL VALVE LEAKING. TIGHTNED FITTING AND PERFORMED LEAK CHECK. SERVICED LEFT HYDRAULIC SYSTEM RESERVOIR PER AMM 29-00-00. SYSTEM CHECKS NORMAL.

Part: FORMER — CRACKED (LE SLAT) · airframe 43,161 hrs · 20,858 cycles

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

Part: FORMER — CRACKED (LE SLAT) · airframe 43,161 hrs · 20,858 cycles

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

Part: RELEASE PIN — PULLED (EVAC SLIDE) · airframe 40,233 hrs · 19,318 cycles

METAL SLIDE PACKING RELEASE PINS THAT RETAIN THE SLIDE WERE PULLED OUT OF THEIR FITTINGS ON THE SLIDE PACK. CAN NOT RE-INSTALL OR RE-ARM. REPLACED LT NR 1 DOOR SLIDE. OPERATIONS CHECKED NORMAL.

Part: TRIM MOTOR — FAILED (STABILIZER) · airframe 38,953 hrs · 18,598 cycles

DFE - CREW REPORTED PRIMARY STAB TRIM FAILED DURING CLIMBOUT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRIMARY STAB TRIM MOTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 38,953 hrs · 18,598 cycles

LIT - INFLIGHT MEM-DFW. CREW REPORTED ACCT UNABLE TO MAINTAIN CABIN PRESSURIZATION. FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRESSURIZATION SELECT PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FAN — INOPERATIVE (CABIN) · airframe 38,953 hrs · 18,598 cycles

RIC - CREW REPORTED ELECTRICAL ODOR THROUGHOUT CABIN. EMERGENCY DECLARED, FLIGHT RETURNED RIC LANDED WITHOUT INCIDENT. AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,953 hrs · 18,598 cycles

SMALL CRACK IN RIGHT SIDE OF FUSELAGE SKIN AT STATION 1380 JUST ABOVE LONGERON 14 RIGHT. INSTALLED DOUBLER PER SRM 53-01-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,953 hrs · 18,598 cycles

LARGE DENT AFT OF THE AFT CARGO DOOR AT STATION 1231 BETWEEN STRINGER 21 AND 22 RIGHT. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2 SHEET 13.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

CORROSION ON TOP OF WEB STATIONS 1212 TO 1215. ACCOMPLISHED SPLICE REPAIR PER AARD 53-10-00-24.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 35,404 hrs · 16,791 cycles

RIGHT CUSP T DAMAGED STATION 355 ON UPPER VERTICAL FLANGE. INSTALLED ANGLE PER EA MD80-53-020103.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

CORROSION ON TOP OF WEB STATIONS 1212 TO 1215 LONGERON 28 LEFT. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER AARD 53-10-00-24.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 35,404 hrs · 16,791 cycles

HOLE IN FORWARD SUBFLOOR STATION 198 LEFT BUTTLINE 44. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,404 hrs · 16,791 cycles

SKIN HAS DENT WITH SCRATCHES ON FRAME 229 ABOVE LONGERON 18 LEFT. REPAIRED SKIN PER SRM 53-04-5.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 35,404 hrs · 16,791 cycles

NUMBER 5 SEAT TRACK GOUGES IN RADIUS OF OUTBOARD LOWER FLANGE STATIONS 1174 TO 1212. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05-00 FIGURE 4F.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

AFT CARGO CORROSION ON DOOR BEAM STATIONS 1198 TO 1205. INSTALLED BEAM DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

RIGHT CUSP SHEET STATIONS 1174 TO 1250 CORRODED. REPLACED CUSP SHEET PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

NUMBER 5 SEAT TRACK, STATIONS 200 TO 218 CORRODED. SPLICED NEW SECTION OF TRACK STATIONS 200 TO 246 PER AARD 51-10-00-5.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

G2 GALLEY FORWARD OUTBOARD MOUNT, STATION 215, ATTACHED TO NUMBER 6 SEAT TRACK CORRODED. REPLACED MOUNT PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

NUMBER 6 SEAT TRACK STATIONS 265 TO 266 CORRODED. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 35,404 hrs · 16,791 cycles

CORROSION ON NUMBER 1 SEAT TRACK GALLEY MOUNT OUT OF LIMITS. INSTALLED NEW G-4 GALLEY MOUNT TO NUMBER 1 SEAT TRACK PER AARD 51-10-00-5.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

RIGHT STATION 237 CUSP DOUBLER CORRODED. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

RIGHT CUSP STATIONS 200 TO 218 CORRODED BETWEEN SEAT TRACKS 5 AND 6. REPAIRED PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

CORROSION ON G2 GALLEY FORWARD INBOARD MOUNT, STATION 211 RIGHT BUTTLINE 8. INSTALLED NEW MOUNT PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

NUMBER 6 SEAT TRACK STATIONS 321 TO 323 CORRODED. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

RIGHT CUSP SHEET STATIONS 313 TO 389 CORRODED. INSTALLED NEW CUSP SHEET PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

RIGHT CUSP SHEET STATIONS 218 TO 237 CORRODED. INSTALLED NEW RIGHT CUSP SHEET STATIONS 218 TO 237 PER AARD 51-10-00-5.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,404 hrs · 16,791 cycles

ANGLE CRACKED RIGHT SIDE OUTBOARD OF RUDDER ACTUATOR ROD END. REPAIRED ANGLE PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

NUMBER 6 SEAT TRACK STATIONS 284 TO 288 CORRODED. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

G4 GALLEY MOUNT, STATION 1176 ATTACHED TO NUMBER 1 SEAT TRACK IS CORRODED. REPLACED G4 GALLEY MOUNT PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

NUMBER 1 SEAT TRACK CORRODED AT STATION 1176. REPLACED NUMBER 1 SEAT TRACK STATIONS 1174 TO 1309 PER AARD 51-10-00-5.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 35,404 hrs · 16,791 cycles

LEFT VERTICAL STAB ATTACH ANGLE IS CRACKED AT FASTENER AT CANTED FRAME 1463. INSTALLED REPAIR ON FUSE TO VERTICAL STAB ANGLE PER AARD 53-10-00-2.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

FORWARD SUBFLOOR CORRODED BELOW G1 GALLEY DRAIN PAN. REPAIRED PER AARD 53-20-00-16

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,404 hrs · 16,791 cycles

LEFT CUSP CORRODED STATION 475. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: REPAIR — DENTED (LE SLAT) · airframe 35,404 hrs · 16,791 cycles

RIGHT WING NUMBER 4 SLAT HAD A INTERM REPAIR ACCOMPLISHED PER SRM 57-03-00. REPLACED TEMPERATURE REPAIR BY REWORKING THE DENTED AREA TO WITHIN LIMITS GIVEN IN THE SRM 57-03-00 FIGURE 18.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 35,404 hrs · 16,791 cycles

FORWARD PASSENGER DOOR JAMB INNER SKIN TONGUE CRACKED AT STATION 210 LONGERON 15 LEFT. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-11.

Part: PAN — CRACKED (WINDOW) · airframe 35,404 hrs · 16,791 cycles

CABIN WINDOW PAN LOWER AFT AREA HAS CRACK, STATION 788 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: ENGINE — FAILED (LEFT) · airframe 34,712 hrs · 16,437 cycles

DFW - CREW REPORTED LOUD BANG WAS HEARD AND LEFT ENGINE FAILED (SINGLE ENGINE TIME 7 MINS). EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT DFW ON 07/27/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — MALFUNCTIONED (RT ENGINE) · airframe 33,371 hrs · 15,755 cycles

DEN - CREW REPORTED NUMBEROUS MECHANICAL ISSUES - LOST RIGHT ENGINE PRESSURE RATIO, RIGHT GENERATOR DROPPED OFF LINE, MUTLIPLE CIRCUIT BREAKERS TRIPPED. FLIGHT RETURNED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE DRIVEN GENERATOR AND CONSTANT SPEED DRIVE (MPN 696233B). SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,121 hrs · 15,630 cycles

MID CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKS NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,311 hrs · 14,776 cycles

CRACK IN FUSELAGE SKIN AT RIGHT HAND STRUT DOOR AFT HINGE CUTOUT. REPAIRED PER SRM 53-05-00.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 31,311 hrs · 14,776 cycles

HOLE IN FORWARD TOP EDGE OF SKIN UNDER NUMBER 1 BEAM OF ENTRY DOOR. INSTALLED DOUBLER PER EA COMO 52-010631.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 31,311 hrs · 14,776 cycles

SHEAR TIE STATION 1451 CRACKED. REMOVED AND REPLACED SHEAR TIE.

Part: IDG — FAILED (RT ENGINE) · airframe 31,142 hrs · 14,699 cycles

BNA - INFLIGHT EWR-DFW. CREW REPORTED RIGHT ENGINE DRIVEN GENERATOR FAILED. EMERGENCY DECLARED, DIVERTED BNA LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE CONSTANT SPEED DRIVE AND RIGHT GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,577 hrs · 14,446 cycles

TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN RIGHT AFT LAVATORY. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,577 hrs · 14,446 cycles

EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK LOCATED IN CEILING OF AFT RIGHT LAVATORY FORWARD POSITION.

Part: BOOT — OUT OF POSITION (AC PACK) · airframe 30,433 hrs · 14,375 cycles

ORD - CREW REPORTED ELECTRICAL ODOR COMING FROM THE RIGHT AFT LAVATORY. EMERGENCY DECLARED RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RE-INSTALLED RIGHT PACK DUCT BOOT THAT HAD SLIPPED OUT OF POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,771 hrs

MCI - AFT EMERGENCY LIGHTS AT STATION 1296 AT RIGHT LAVATORY AND ENTRY AREA INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS AT STATION 1296 AT RIGHT LAVATORY AND ENTRY AREA.

Part: WEB — CRACKED (ZONE 200) · airframe 26,972 hrs · 12,878 cycles

CANT FRAME 1485 UPPER LEFT WEB CRACKED AFT OF LEFT LOUVER BOX. INSTALLED DOUBLER PER AARD 53-10-00-32.

Part: BLADES — DAMAGED (RT ENGINE)

DFW INFLIGHT T1157/15OCT - RIGHT ENGINE PRESSURE RATIO FLUCTUATION AND VIBRATION ON TAKEOFF ROLL ENGINE COMPRESSORS STALLED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 16 OCT 2007 AT DFW DUE TO FAN FOD DAMAGE DURING TAKEOFF. FAN BLADE BENT FORWARD AND SOME REPORTS STATE BIRD FOD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT 10EG HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10EG. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BROKEN (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT 10EG HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 10EG. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT 10EG HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10EG. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - FOUND EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 17 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 11 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 21 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - FOUND EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROW 7 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS IN FORWARD AND AFT CABIN INOPERATIVE. REPLACED TWO BATTERY PACKS AT AB52 AND AB53 FOR EMERGENCY LIGHTS IN FORWARD AND AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY EXIT LIGHTS ABOVE FORWARD ENTRY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS ABOVE FORWARD ENTRY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW EMERGENCY PATH LIGHT AT ROW 12 INOPERATIVE. FOUND CONNECTOR LOOSE AT ROW 12 LIGHT ASSEMBLY. RESECURED CONNECTOR FOR EMERGENCY PATH LIGHT ASSEMBLY AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL UNIT — FAULTY (ELECTRICAL SYS)

PDX T1010/01 EN ROUTE PDX-DFW RIGHT HAND BUS FAULT AND POPPING CIRCUIT BREAKERS. RETURNED PDX AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED AIRCRAFT BUS CONTROL UNIT AND R2-36 RELAY SYSTEM PER MM 24-20-08-4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CARGO TRACK — CORRODED (FUSELAGE)

FOUND AFT CARGO, LEFT TIE DOWN TRACK CORRODED FROM STATION 1220-1309. REMOVED AND REPLACD TRACK. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,109 hrs · 3,168 cycles

THE OVERWING EMERGENCY EXIT SIGN WAS MISSING AT SEAT 21A, THE FWD ENTRANCE DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE, AND THE THE RED EGRESS LIGHT WAS INOPERATIVE AT THE FWD GALLEY AND AFT LAVATORY. INSTALLED EXIT MARKER P/N 0105612-001, REPLACED 2 DISCHARGED BATTERIES P/N 408822-101 FOR THE PORTABLE LIGHT, AND REPLACED THE BURNED OUT LAMP P/N 7732 FOR EACH EGRESS LIGHT POSITIONS. CHECK-C 5-3-01 STL.

Part: AUDIO PANEL — FAILED (COCKPIT) · airframe 3,236 hrs · 1,747 cycles

CREW REPORTED A TOTAL RADIO COMMUNICATION FAILURE ENROUTE. FLIGHT RETURNED TO STL BUT WAS ABLE TO RE-ESTABLISH COMMUNICATION. REPLACED THE FIRST OFFICERS AUDIO SELECTOR PANEL. CHECK-C 6-1-00 STL. ---CLOSED---