N803WA

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 47,937 hrs · 35,518 cycles

FLIGHT ATTENDANTS & PAXS REPORTED SMELLING SMOKE, PRECAUTIONARY DIVERSION. PERFORMED E & E VISUAL INSPECTION, NO DEFECT NOTED IAW 05-21-01 601. PERFORMED TAIL CONE AREA VISUAL INSPECTION, NO DEFECT NOTED IAW 05-21-01 501. PERFORMED BOTH ACM VISUAL INSPECTIONS FOR LEAK, NO DEFECT NOTED IAW 12-12-03. PERFORMED APU VISUAL INSPECTION, FOUND APU OIL SYS TANK OVER SERVICED, DRAINED TO CORRECT QTY IAW 12-12-01. PERFORMED APU OPERATIONAL TEST, NO DEFECT NOTED, NO SMELLING SMOKE IAW 49-00-00 201 & 501.

Part: SWITCH — UNKNOWN (EMERGENCY LIGHTS)

DURING SERVICE CHECK, FOUND FWD F/A STATION, EMERGENCY LIGHT SWITCH INOPERATIVE. PERFORMED OPS CHECK, EMERGENCY LIGHT SYSTEM F/A LIGHTS SWITCH FOUND NORMAL IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DURING SERVICE CHECK, FOUND OVERWING EMERGENCY LIGHTS LT & RT INOPERATIVE. R & R THE BATTERY PACK & OPS CHECKED NORMAL IAW AMM 33-53-00.

Part: WING — HANDLER ERROR (ZONE 500) · airframe 47,423 hrs · 35,031 cycles

DE-ICING TRUCK HIT LT WING TIP DURING DE-ICING. REMOVED LT WING TIP EXTENSION T/E PANEL IAW MM 57-20-02. CLEANED AND INSPECTED AREA FOR DAMAGES IAW WO 2701, ITEM NR 2. REPLACED DAMAGED LT WING TIP EXTENSION PANEL IAW MM 57-20-02. PERFORMED INTERIM REPAIR AT LT WING T/E PANEL IAW MESSAGE CSW-15-0005-03B/07B. REMOVED AND REINSTALLED FLUX VALVE IAW MM 34-21-06 TO FOM, FUNCTIONAL CHECK NORMAL IAW MM 34-21-00. INSPECTED WIRES FOR WING TIP LIGHTING AND FLUX VALVE AREA IAW MM 20-50-00, NO DEFECTS NOTED. PERFORMED OPS CHECK OF LT WING TIP LIGHTING, AFT STROBE, FWD STROBE, LANDING LIGHT AND COMPASS IAW MM 34-21-06 AND 33-40-00 FUNCTIONAL CHECK NORMAL. NOTE: OPS RESTRICTION, AVOID SEVERE TURBULENCE, REPAIR APPROVED FOR 20 FLIGHT HOURS, INSPECT REPAIR PRIOR TO EACH FLIGHT IAW MESSAGE CSA-15-0005-07B. TRANSFERRED TO WATCH ITEM 2875 BASED ON INFO FROM CSW-15-0005-07B AND SRM 51-02. 20 HOURS REVENUE FLIGHT ONLY. INSPECT TAPE FOR SECURITY BEFORE EACH FLIGHT. DOC FROM MFG IN LOG BOOK FOR CREW REFERENCE. PLACARD INSTALLED. REF TO WI 2875: ACCOMPLISHED REPAIR ON LT WING T/E IAW MFG MESSAGE CSW-15-0005-07B AND SRM 57-03, FIG 10 FOR T/E S3913181. THIS CLEARS WI 2875. PLACARD REMOVED.

Part: SOCKET — DAMAGED (CABIN LIGHTS) · airframe 47,241 hrs · 34,863 cycles

DURING DESCENT, AFT ROW 20 ELECTRICAL ODOR. INSPECTED AREA FOUND LAMP HOLDER DAMAGED. R & R HOLDER IAW AMM 33-21-03. OPS CHECKED NORMAL IAW AMM 33-21-03, NO DEFECTS NOTED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 47,087 hrs · 4,060 cycles

FLASHLIGHT FWD F/A BULKHEAD INOPERATIVE IN TEST MODE. PERFORMED EMERGENCY LIGHT TEST IAW AMM 33-53-00. OPS CHECKED NORMAL. FWD EMERGENCY FLASHLIGHT CRADLE BROKEN. ADJUSTED FWD EMERGENCY FLASHLIGHT CRADLE IAW AMM 25-60-00.

Part: ACTUATOR — DEFECTIVE (OUTFLOW VALVE) · airframe 46,972 hrs · 34,662 cycles

RAPID DEPRESSURATION ABLE TO MAINTAIN 6,000 FT, CABIN ALT AT 15,000 FT PRESSURE ALT. R & R OUTFLOW VALVE ACTUATOR IAW AMM 21-35-05. OPS CHECKED NORMAL.

Part: ENGINE — POWER LOSS (LEFT) · airframe 46,884 hrs · 34,584 cycles

LOST THRUST ON LT ENGINE AFTER TAKEOFF. RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED NORMAL. ACCOMPLISHED NR 1 ENGINE DFGC INTERMIX WIRING IAW MM 71-02-00 PARA (F) PAGE 203. OPS CHECKED NORMAL.

Part: FLASHLIGHT — DAMAGED (FWD CABIN) · airframe 46,660 hrs · 3,445 cycles

L-1 DOOR PORTABLE FLASHLIGHT DAMAGED. REMOVED AND INSTALLED FLASHLIGHT IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — LOOSE (FLASHLIGHT) · airframe 46,530 hrs · 34,339 cycles

PORTABLE FLASHLIGHT AT L1 DOOR DOES NOT COME ON WHEN SELECTED. INSPECTED FLASHLIGHT, FOUND LOOSE BATTERY, SECURED THE BATTERY IAW MM 33-53-00. OPS CHECKED NORMAL.

Part: BOLT — MISSING (MLG WHEEL) · airframe 46,128 hrs · 34,008 cycles

MAIN WHEEL ASSY TIE BOLT MISSING, FOUND DURING WALKING AROUND PREFLIGHT. R & R MAIN WHEEL ASSY IAW 32-40-01.

Part: DUCT — SEPARATED (AC BAY) · airframe 44,887 hrs · 32,843 cycles

DURING CRUISE RIGHT LAVATORY SMOKE DETECTOR WENT OFF AND THE FLIGHT ATTENDANT REPORTED SMELL OF SMOKE. INSPECTED AREA OF AFT VENTRAL AIRSTAIRS AND FOUND THE DUCT BETWEEN THE RT ACM AND PRIMARY HEAT EXCHANGER HAD BECOME SEPARATED. RECONNECTED RT ACM TO PRIMARY HEAT EXCHANGER PER MD80 AMM21-51-01, 21-51-04 AND OPS CHECKED THE AIR CONDITIONING SYSTEM PER MD80 AMM 21-00-00. NO LEAKS OR DEFECTS NOTED. OPS CHECKED ALL LAV SMOKE DETECTOR PER MD80 AMM 26-14-00. OPERATED A/C PACKS, LT & RT, PER 21-00-00, FOR 30 MINUTES, NO SMOKE DETECTOR ALARMS SOUNDED AND NO SMOKE ODORS WERE DETECTED DURING TEST.