N841AB

ATA 3040

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 16,433 hrs

MBJ/HAV - FLT JM 061 - AIRCRAFT EN ROUTE WHEN IT WAS DIVERTED DUE TO A CRACKED LEFT WINDSHIELD AND A LEFT FORWARD WINDSHIELD WINDOW HEAT FAILURE. MAINTENANCE CHANGED THE LEFT WINDSHIELD AND THE LEFT HEAT CONTROLLER. OPERATIONAL CHECKS CARRIED OUT ON BOTH ITEMS WHICH WERE FOUND SERVICEABLE. TO-DATE, THERE HAS BEEN NO RECURRENCE OF THE REPORTED FAULT. LANDINGS: 6,733. (X)

ATA 5610

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,433 hrs

MBJ/HAV - FLT JM 061 - AIRCRAFT EN ROUTE WHEN IT WAS DIVERTED DUE TO A CRACKED LEFT WINDSHIELD AND A LEFT FORWARD WINDSHIELD WINDOW HEAT FAILURE. MAINTENANCE CHANGED THE LEFT WINDSHIELD AND THE LEFT HEAT CONTROLLER. OPERATIONAL CHECKS CARRIED OUT ON BOTH ITEMS WHICH WERE FOUND SERVICEABLE. TO-DATE, THERE HAS BEEN NO RECURRENCE OF THE REPORTED FAULT. LANDINGS: 6,733. (X)

ATA 7230

Part: STATOR — FAILED (HP COMPRESSOR)

KIN/JFK - FLT JM 017 - EN ROUTE, FLIGHT DIVERTED DUE BAD WEATHER. AFTER TAKEOFF AND DURING CLIMB PHASE AT 17,000 FEET, A LOUD BANG WAS HEARD FOLLOWED BY THE NR 1 ENGINE EGT GOING OVER ITS LIMIT. ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED. INSPECTION PERFORMED SHOWING NO SIGN OF FOREIGN OBJECT INGESTION, HOWEVER, SMALL METAL PARTICLES OBSERVED IN EXHAUST NOZZLE. DETERMINED THE ENGINE HAD SURGED AND WAS REPLACED. A STATOR 6 VARIABLE VANE FAILED CAUSING DAMAGE TO HP COMPRESSOR. AIRCRAFT RETURNED TO SERVICE. (X)

ATA 2913

Part: PUMP — FAILED (HYDRAULIC) · airframe 14,980 hrs · 6,062 cycles

JFK/KIN - FLT JM 010 - GREEN PUMP LOW PRESSURE LIGHT CAME ON IN-FLIGHT, AND COULD NOT BE RECOVERED. GREEN PUMP, PN 65066-06, SN 273874, IS AN ABEX UNIT WHICH WAS INSTALLED ON 12-13-99. THIS WAS A LOANER UNIT AND INSTALLED UNDER THE AUTHORITY OF A ''NO TECHNICAL OBJECTION'', REF: 997.0554/99. THE APPROVED EDP FOR THIS AIRCRAFT IS MFG BY VICKERS WITH P/N 887673. AFTER RE-INSTALLATION OF CORRECT TYPE PUMP ON 12-17-99, THERE HAS SINCE BEEN NO REPORTED DISCREPANCY ON THIS SYSTEM. (X)

ATA 2913

Part: PUMP — LEAKING (HYDRAULIC SYSTEM) · airframe 14,960 hrs · 6,053 cycles

KIN/MBJ - FLT JM 019 - AIRCRAFT LOST GREEN SYSTEM HYDRAULIC FLUID RESULTING IN MANUAL EXTENSION OF GEARS FOR LANDING. A FAILED PACKING WAS IDENTIFIED AS THE CAUSE. AFTER REPLACEMENT AND RE-SERVICING, AIRCRAFT WAS RETURNED TO SERVICE. NEXT FLIGHT, GREEN SYSTEM LOW LEVEL OCCURRED AFTER GEAR RETRACTION, RESULTED IN AIRCRAFT RETURNING. A LEAK CONFIRMED FROM THE NR 2 ENGINE GREEN SYSTEM ENGINE DRIVEN PUMP. THE AIRCRAFT HAS BEEN REMOVED PENDING PUMP REPLACEMENT. ALL GREEN SYSTEM HYDRAULIC PUMP CASE DRAIN FILTERS CHECKED FOR CONTAMINATION DUE SUSPECTED CAVITATION AND FOUND OK. PRESENTLY AWAITING STRIP REPORT AFTER REPAIR OF DAMAGED PUMP TO ESTABLISH REASON FOR FAILURE. (X)

ATA 2913

Part: PUMP — OVERHEATED (HYDRAULIC SYSTEM)

JFK/KIN - FLT JM 016 - NR 2 ENGINE YELLOW HYD PUMPS OVERHEAT WARNING CAME ON 2.50 HRS INTO FLIGHT. REPORT FROM O/H AGENCY REVEALED THE PUMP WAS BURNT. QUANTITY TRANSMITTERS INSTALLED ON THIS ACFT WERE FOUND TO BE MODIFIED PER TFU 29.31.00.002. REGARDING CHAFING WIRES TO SHUTOFF VALVE, ONCE ONLY INSP A310/052 ISSUED. WIRES TO ALL VALVES ON THIS ACFT CHECKED, FOUND MINOR NICKS ON OUTERMOST INSULATIONS. ALL NICKS RECTIFIED. REF: TFU 24.92-00-018. (X)

ATA 2913

Part: PUMP — OVERHEATED (HYDRAULIC SYSTEM)

DURING CRUISE, YELLOW HYD PUMP LOW PRESS LIGHT ILLUMINATED WITH ECAM WARNING. 10 MINUTES LATER, YELLOW HYD RESERVOIR LOW LIGHT ILLUMINATED. REPORT FOR HYD PUMP REVEALED PUMP OVERHEATED, INTERNAL PARTS DAMAGED. SKYDROL BURNED INSIDE PUMP SCRAPPED.

ATA 7830

Part: SWITCH MODULE — INTERMITTENT (NR 2 ENGINE)

REVERSE UNLOCK ECAM WARNING ACCOMPANIED BY REV (GREEN) AT FL 350, NR 2 ENGINE. FLIGHT DIVERTED TO MIA. NO BUFFET OR BANK EXPERIENCED. ECAM WARN DISAPPEARS AND RECURS A FEW TIMES DURING DIVERSION. LOCKED OUT NR 2 T/R PER MEL 78-30-01. REPLACED RVDT/STOW SWITCH MODULE S301. OPS CHECK GOOD.