N806DE

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 455 hrs · 350 cycles

EMERGENCY LIGHTS FLICKER ON AND OFF WITH SYSTEM IN ARM POSITION. REPLACED THE BATTERY PACK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 455 hrs · 350 cycles

EMERGENCY LIGHTS FLASH ON AND OFF WHEN SYSTEM IN ARM POSITION. REPLACED THE BATTERY PACK.

Part: ENGINE — FLAMED OUT (NR 1) · airframe 48,005 hrs · 5,623 cycles

AT 133 KNOTS THE NR 1 ENGINE SURGED WITH FLAME-OUT, THE FRONT AND BACK. INSPECTION IN THE FRONT AND BACK, LOOKS OK. DUE TO AD 2002-21-10, THIS IS A GROUP 3 TAKEOFF SURGE AND THE ENGINE WILL BE CHANGED.

Part: SOLENOID — INOPERATIVE (L2 DOOR) · airframe 47,920 hrs · 5,614 cycles

L2 DOOR SMELLS LIKE ELECTRICAL BURNING AND WILL NOT OPERATE ELECTRICALLY. REPLACED LOCK/RELEASE SOLENOID PER M/M. OPS GOOD. NO MORE BURNING SMELL.

Part: FAN — SEIZED (NR 1 PACK) · airframe 46,682 hrs · 5,442 cycles

STRONG ELECTRICAL BURNING ODOR DURING DESCENT, JUST AFTER WINDSHIELD HEAT WAS TURNED ON. CREW DEACTIVATED WINDSHIELD HEAT, TURNED ECON OFF AND ISOLATED THE NR 1 PACK. FUMES DISSAPATED. CREW COULD HEAR MOTOR FAN THAT SOUNDED AS IF IT WAS BINDING. FUMES SEEM STRONGEST AROUND C/B PANEL. FOUND AVIONICS COOLING FAN NR 3 WITH C/B POPPED. REPLACED FAN. FAN OPS NORMAL. C/B REMAINS CLOSED.

Part: ACTUATOR — LEAKING (MLG OVERCENTER) · airframe 46,427 hrs · 5,397 cycles

GEAR FAILED TO RETRACT ON FIRST ATTEMPT. SECOND ATTEMPT SUCCESSFULL. PERFORMED GEAR SWING TO DUPLICATE PROBLEM. SWUNG GEAR 4 TIMES. NO PROBLEMS NOTED. SYSTEM CHECKS GOOD. DURING GEAR SWING, FOUND LT GEAR OVERCENTER LOCK ACTUATOR LEAKING . R & R LT GEAR OVER CENTER LOCK ACTUATOR PER M/M.

Part: CHILLER — FAILED (AFT GALLEY) · airframe 44,656 hrs · 5,097 cycles

AT CRUISE FLT ATTDS INFORMED US THERE WAS A STRONG ELECTRICAL SMELL IN THE AFT GALLEY CHILLER #8 RED FAIL LIGHT WAS FLASHING. SHUT DOWN CHILLER #8 AND #7. GALLEY POWER WAS ALSO TURNED OFF. DIVERTED TO JFK. SMELL SEEMED TO DISSAPATE. CORR ACTION: FOUND NBR 7 CHILLER FAN GRINDING. CHECKED AREA OF CHILLERS NO EVIDENCE OF ELECT WIRING CHAFFED OR BURNT. CHECKED AFT COOLING FAN FOUND OK #8 CHILLER OPS NORMAL. RPLD #7 CHILLER. PERFORMED OVER WEIGHT LANDING INSPECTION PER M.M.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,039 hrs · 5,016 cycles

ON PREFLIGHT, EMERGENCY LIGHT TEST FAIL. EMERGENCY LIGHT BATTERY 6 LO MSG ON. REPLACED EMERGENCY LIGHT BATTERY 6 PER M/M. EMERGENCY LIGHT TEST PASS.

Part: OVEN — MALFUNCTIONED (AFT GALLEY) · airframe 41,316 hrs · 4,676 cycles

AFT GALLEY FWD OVEN GIVING OFF BURNING SMELL. REPLACED OVEN.

Part: TRANSDUCER — FAILED (ANTISKID SYS) · airframe 40,580 hrs · 4,580 cycles

NR 10 TIRE BLOWN ON LANDING. REPLACED NR 10 ANTISKID TRANSDUCER.

Part: BATTERY — MISSING (SMOKE DETECTOR) · airframe 38,330 hrs · 4,305 cycles

IR-1330/18DEC/LAX/ 060558 - FRC-261-02208 LAV 4R SMOKE. DETECTOR BATTERY MISSING. CA-REPLACED DETECTOR BATTERY AT 4R. SMOKE DETETOR TESTS NML. MALF-4T0 POS-CN CTL-C12180302 SKILL-02

Part: COMPUTER — MALFUNCTIONED (MANIFOLD FAIL) · airframe 37,448 hrs · 4,209 cycles

AT TOP OF CLIMB GOT NR 2 MANIFOLD FAILURE. SYSTEM RESOLVED ITSELF. FOUND MANIFOLD FAIL COMPUTER BAD. REPLACED SAME.

Part: CAWS — INOP (E/E)

ATB AURAL WARNING WITH NO VISUAL CAUSE, UNABLE TO SILENCE HORN. REPLACED CAWS UNIT.

Part: WATER COMP — FAILED (NR 1)

PAX AT 3B NOTICED A HOT WIRE SMELL. THE CREW ALSO NOTICED THE SMELL. LATER F/A AND PASSENGER COMPLAINED OF HEADACHES INSPECTED CEILING FWD CABIN FOR BURNING WIRE CK OK. CHECKED SIDEWALL OF FWD CRAGO COMP FOUND NR 1 WATER COMP BEARING FAILURE. REPLACED NR 1 WATER COMP. CKS GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (RT LAVATORY)

THERE WAS A SMALL FIRE OR SMOLDER IN 4R LAV TRASH BIN, IT WAS PUT OUT PROMPTLY BY THE FLIGHT ATTENDANT. NO DAMAGE VISABLE IN CAN. THE SMOKE ALARM DID NOT GO OFF. TESTED SMOKE DETECTOR ON ARRIVAL, CHECKED OK. NO EVIDENCE OF FIRE OR BURNED MATERIAL. TRASH COMPARTMENT AND CONTAINER IN SERVICABLE CONDITION. REPLACED SMOKE DETECTOR PRECAUTIONARY.

Part: MONITOR — FAILED (ROW 40J)

ODOR DETECTED IN AREA OF MONITOR 40J. MONITOR HAD BEEN FLICKERING, NO PICTURE. POWER REMOVED FROM MONITOR, ODOR DISAPPEARED. REPLACED MONITOR AND POWER SUPPLY.

Part: BATTERY — DISCHARGED (CABIN)

FWD CABIN EMERGENCY LIGHT INOP. REMOVED AND REPLACED N01 BATTERY PACK IN THE NR 1 BATTERY POWER SUPPLY, GRD OPS CK OK.

Part: OXYGEN LINE — LEAKING (COCKPIT)

IN CRUISE, FOUND CREW 02 BOTTLE EMPTY. FOUND FLEX LINE TO OBSERVER 02 REGULATOR LEAKING BADLY. REPLACED LINE AND REPLACED 02 BOTTLE. LEAK CK GOOD.

Part: FIRE BOTTLE — LOW PRESS (4L DOOR)

FIRE EXTINGUISHER BOTTLE AT 4L LOW PRESS. REPL BOTTLE.

Part: SKIN — CORROSION (BS 1937/1959)

THE RT FUSELAGE SKIN SURROUNDING THE FWD AND AFT LAV VACUUM WASTE AIR EXHAUST PORTS WERE FOUND CORRODED ON THE OUTER SURFACE AROUND THE AFT EDGES OF THE PORT CUTOUTS AT FS 1937 AND 1959 RESPECTIVELY. THE CORROSION BLEND OUT ON THE FWD PORT HOLE REQUIRED A MAX DEPTH OF 0.016. THE AFT PORT HOLE REQUIRED THAT THE SKIN BE CUTOUT IN THE DAMAGED AREA. FS 1937 - 0.063 EXT 2024-T3 REPAIR DOUBLER; FS 1956 - 0.071 2024-T3 EXT DOUBLER; GENERAL - 2 INTERNAL FINGER DOUBLERS - SEAL AND TREAT.

Part: FAUCET — LEAKING (LAV M)

WITH A/P ON, WHEN FLIGHT SPOILERS WERE EXTENDED TO FULL, THE AIRCRAFT ROLLED LEFT TOWARD 30 DEGREE BANK. SPOILERS DON'T APPEAR TO EXTEND AT 1/3 AND 2/3 POSITION. AILERON TRIM WAS JAMMED DURING APPROACH, WILL NOT MOVE FROM ZERO POSITION. GROUND SPOILERS DID NOT EXTEND ON LANDING. FOUND ICE BUILDUP IN RIGHT WHEEL WELL IN AREA OF CONTROL CABLES. WATER LEAK FROM LAV -M ABOVE. REPLACED WATER FAUCET IN LAV-M.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT SYSTEM FAULTED BATTERY PACK NR 3 AND NR 6.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT SYSTEM FAULTS BATTERY PACK NR 3 AND NR 6.

Part: COMPRESSOR — FAILED (NR 1 ENGINE)

ON TAKEOFF LOUD BANG LEFT SIDE, VIBRATION, ABORTED T/O. A/C REPORTED SMOKE AND FIRE, FIRED NR 1 AGENT BOTTLE. SHUTDOWN PER CHECKLIST. FOUND COMPRESSOR HAD FAILED, METAL IN TAILPIPE AND BELOW 2.5 BLEED OPENING. MTC IN PROGRESS.

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE FAILED DURING T/O RUN. LOUD BANG FROM LEFT SIDE OF A/C HEARD, T/O ABORTED AT 50 KNOTS. A/C REPORTED SMOKE AND FIRE. BLEW NR 1 FIRE BOTTLE AND SHUT DOWN ENGINE. NO EVIDENCE OF FIRE FOUND DURING INSPECTION. CHANGED ENGINE, METAL FOUND IN BLEED VALVE.

Part: AUTOPILOT — INOPERATIVE (NR 1/2)

BOTH A/P INOP, NO CURRENT FAULTS. ACFT RETURNED ATL. PERFORMED RTS ON BOTH FCC, ALL NORMAL.

Part: ENGINE — FAILED (NR 2 ENGINE)

AFTER TAKEOFF AT 2,600 FT AND 270 KIAS, NR 2 ENGINE FAILED. A/C SHUDDERED, RPM ROLLED BACK AND TEMP WENT TO 754, FIRED EXT AGENT FOR NR 2 ENG. FLIGHT RETURNED TO LAX WHERE MAINTENANCE FOUND METAL IN TAIL PIPE. REPLACED ENGINE AND ROUTED TO SHOP.

Part: BATTERY PACK — DISCHARGED (CABIN)

FAILED EMER LIGHT TEST MSC EMER LIGHT BAT 2 LOW. REPLACED EMER LIGHT BAT 2, OPS CKS OK.