N810AX

Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 89,694 hrs · 14,248 cycles

5:22 INTO FLIGHT, HEARD A LOUD THUMP WITH AN ASSOCIATED PITCH CHANGE WATER SYS, PRESS LOW LIGHTS ILLUMINATED AND SYS 2 QTY REDUCED TO 0. 7:22 INTO FLIGHT, HEARD 2ND LOUD THUMP WITH ASSOCIATED PITCH CHANGE. NO ADDITIONAL ABNORMAL INDICATIONS WERE NOT. FOUND DAMAGE AT LT NR 1 SLAT CRUISE AERODYNAMIC FILLET AND LT HORIZ STAB L/E; REMOVED AND REPLACED LT NR 1 SLAT IAW AMM 27-80 CKS GOOD AND INSTALLED INTERIM REPAIR IN LT HORIZ L/E IAW ERA NR 5530-711 ERA; DRAINED POTABLE WATER SYS 1, 2, AND 3.

Part: DOOR — UNLATCHED (E/E BAY) · airframe 89,604 hrs · 14,233 cycles

AFTER TAKEOFF LARGE AND STRONG BLAST OF AIR ENTERED FLIGHT DECK. ACFT WOULD NOT PRESSURIZE - OUT FLOW VALVE FULL CLOSED. NO LTSS ON FW ANNU PANELS. DURING WALKAROUND NOTED AVIONICS WHEEL WELL DOOR UNLATCHED. SECURED AND LATCHED DOOR PRESSURIZED A/C OPS CHECK NORMAL IAW AMM 21-30. A/C OK FOR CONTINUED SERVICE.

Part: SENSOR — FALSE INDICATION (OIL TEMP) · airframe 89,102 hrs · 14,136 cycles

AT 1330Z, FLT LEVEL 34, 000 FT, NR 2 ENG OIL TEMP BEGAN TO RISE. WENT INTO YELLOW BAND. ACCOMPLISHED QRM PROCEDURES AND SHUT ENG DOWN AFTER 15 MINUTES. REMOVED AND REPLACED NR 2 OIL TEMP BULB IAW MM 79-32. ENGINE OPS AND LK CK GOOD IAW JRH. REMOVED AND REPLACED NR 2 ENG OIL FILTER IAW MM CH 79-20 AND LEAK CK GOOD.

Part: FUEL — LEAKING (LT WING) · airframe 88,888 hrs · 14,091 cycles

TANK OVERFILL LIGHT CAME ON DURING CLIMB OUT FUEL WAS LEAKING OUT OF LT WING. COMPLIED WITH ALL QRH PROCEDURES ALL TANKS WERE LESS THAN FULL WHEN LIGHT CAME ON.

Part: WIRE — BURNED (EMERGENCY LIGHT)

ON PREFLIGHT FOUND FWD SECTION EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: EXTENSIVELY TROUBLESHOT SYSTEM R&R FAULTY BATTERY POWER SUPPLY AND BATTERY PACK. PERFORMED CONTINUITY POWER GROUNDED CHECKS OF ALL FUNCTIONS AND SWITCHES. REPLACED CHARRED WIRE BETWEEN PIN M&N OF POWER SUPPLY CONNECTOR. TIGHTENED LOOSE POWER WIRE OF R1 DOOR OVERHEAD LIGHT ASSY IAW DC10 M/M DC 10-30 WDM 33-52 SYSTEM OPERATES NORMAL AND DC 10-30 33-51.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 84,807 hrs · 13,282 cycles

EMERGENCY LIGHTS WILL NOT TEST FROM COCKPIT. REPLACED FWD POWER SUPPLY AT DOOR 1L IAW MM 33-51, SYSTEM OPS CHECK GOOD.

Part: RESISTOR — FAILED (CONTROL PANEL) · airframe 83,902 hrs · 13,095 cycles

DURING PAX LOADING SMOKE AND ELECTRICAL FUMES NOTED BY CREW, BY L-4 DOOR PA PNL. DE-PLANED ACFT, FIRE DEPT NOTIFIED. INSPECTED L-4 DOOR FLIGHT ATTENDANT PA PANEL WIRING IAW MM 20-30. FOUND WITH FIRE DEPARTMENT THAT THE L-4 DOOR RESISTOR R4-139 HAD OVERHEATED AND POPPED THE L-4 DOOR CONTROL CIRCUIT BREAKER. FOUND THAT NO WIRES WERE DAMAGED. WITH L-4 DOOR CONTROL C/B PULLED THERE IS NO POWER TO RESISTOR R4-139. DEFERRED L-4 DOOR ELECTRICAL OPERATION IAW MEL 52-1 CAT-C. L-4 DOOR ELECTRICALLY INOP DUE TO OVERHEATED RESISTOR R4-139 ON FLIGHT ATTENDANT PANEL (L-4 DOOR)

Part: SLIDE — DAMAGED (R3 DOOR) · airframe 110,878 hrs · 20,774 cycles

R-3 EVAC SLIDE DAMAGED (PARTIALLY DEPLOYED FOUND BY MAINTENANCE DURING CHECK). REMOVED AND REPLACED R-3 EVACUATION SLIDE IAW MM 25-61. REPAIR SHOP EVALUATION IS THAT THE ACTIVATION BOTTLE DISCHARGE FOR AN UNKNOWN REASON HOWEVER THE MAIN BOTTLE DID NOT DISCHARGE THE SLIDE WAS DETERMINED TO BE B.E.R.

Part: VALVE — MALFUNCTIONED (NR 2) · airframe 80,869 hrs · 12,517 cycles

NR 2 PNEUMATIC TEMP HI LIGHT ILLUMINATED. ASSOCIATED PNEUMATIC TEMP INDICATOR WAS IN THE RED ZONE. REMOVED AND REPLACED NR 2 ENGINE FAN AIR VALVE IAW 36-13. PERFORMED ENGINE RUN, NO DEFECTS NOTED.

Part: DECODER — FAULTY (CABIN) · airframe 80,696 hrs · 12,485 cycles

ABOUT 3+15 INTO THE FLIGHT FA'S NOTICED SMOKE COMING FROM LT SIDE OF AIRCRAFT UPPER SIDE WALL ROWS 15-16-17 RAN PROCEDURE 4-8-1-1 CABIN LIGHTING SMOKE, FIRE AND PULLED ALL C/B'S IN MID-GALLEY SERVICE AREA ALL BREAKERS PULLED TO HELP ISOLATE THE SOURCE OF SMOKE. FOUND PROBLEM WAS DECODER FAILURE ISOLATED TO THE FOLLOWING SEATS LT SIDE OB SEATS 12-14-15-16-17 ABC. REPLACED OVERHEAD DECODERS ROWS 12-14-15-16 IAW MM 23-33 P/N RD-AX5321 S/N 104079, 103990, 106855, 100376. INSPECTED WIRING NO DAMAGE NOTED IN OVERHEAD AREA. CHECKED O2 SYSTEM IAW MM 23-33.

Part: CLAMP — LOOSE (NR 1 ENGINE) · airframe 79,894 hrs · 12,347 cycles

DURING CLIMB AT APPROXIMATELY 240 FT, NR 1 ENGINE A-LOOP LIGHT ILLUMINATED ACCOMPLISHED QRH PROCEDURES ALL OTHER ENGINE INDICATIONS NORMAL. UPON LEVEL OFF AT FL 290 NR 1 ENG INDICATED ENG FIRE, ALL OTHER ENG INDICATIONS NORMAL. FOUND LOOSE PNEUMATIC DUCT CLAMP AT NR 1 ENG L/P RT RECOUP TUBE ASSY RESECURED AND INSPECTED FOR OTHER DAMAGE, NONE FOUND PERFORMED HIGH POWER ENGINE RUNS. NO DEFECTS NOTED.

Part: FIRE WARNING — ACTIVATED (NR 1 ENGINE) · airframe 77,675 hrs · 11,944 cycles

ON CLIMB-OUT, ENGINE FIRE INDICATION NR 1 ENGINE, AIR TURN BACK.