N760AF

Part: FILTER — MELTED (ZONE 100) · airframe 6,913 hrs

EMI FILTER / RELAY FAILED CAUSING PLASTIC COVER TO MELT

Part: DISPLAY — FAILED (COCKPIT) · airframe 6,688 hrs

CO-PILOT IAD SCREEN WENT BLACK DURING FLIGHT AND WOULD NOT POWER UP.

Part: DISPLAY — FAILED (COCKPIT) · airframe 6,685 hrs

CO-PILOT IAD FAILED IN FLIGHT.

Part: GENERATOR — WORN (ZONE 200) · airframe 5,489 hrs

AC GEN BEARING LIGHT ILLUMINATED IN FLIGHT.

Part: HARNESS — INTERMITTENT (ZONE 700) · airframe 4,420 hrs

DURING LANDING GEAR RETRACTION, #2 SERVO BYPASS LIGHT ILLUMINATED. AIRCRAFT ABORT TRIP AND RECOVERED TO KLIT

Part: HYDRAULIC SYSTEM — INTERMITTENT (ZONE 200) · airframe 4,715 hrs

UPON SHUTDOWN A EXCEEDANCE WAS NOTED FOR HIGH HYDRAULIC PRESSURE. AFTER TROUBLESHOOTING / HUMS DOWNLOAD IT WAS NOTED THAT HYDRAULIC PRESSURE HAD REACHED 3340 PSI. CONDUCTING RUNUPS RESULTED IN #2 HYDRAULIC PRESSURE NOT BEING VERY STEADY / VERY WEAK REGULATION. REPLACED #2 HYDRAULIC PUMP. AIRCRAFT RETURNED TO SERVICE.

Part: TAB — MISSING (TRIM SYS) · airframe 3,999 hrs · 7,909 cycles

ONE INBOARD TRIM TAB MISSING DURING PREFLIGHT

Part: TRANSDUCER — OUT OF LIMITS (NR 1 AUTOPILOT) · airframe 1,617 hrs

NR 1 AUTOPILOT DISENGAGED DURING CRUISE FLIGHT. FOUND THE TRANSDUCER OUT OF LIMITS.

Part: TRANSDUCER — OUT OF LIMITS (NR 1 AUTOPILOT) · airframe 1,617 hrs

NR 1 AUTOPILOT DISENGAGED DURING CRUISE FLIGHT. ROLL TRANSDUCER OUT OF LIMITS.

Part: BLADE — DEBONDED (TAIL ROTOR) · airframe 1,559 hrs

DURING SPECIAL 25 HOUR TAIL ROTOR BLADE INSPECTION, OUTBOARD BLADE WAS NOTED TO BE DEBONDED FROM TAIL ROTOR PITCH HORN.

Part: DISPLAY — FAILED (NR 1) · airframe 1,536 hrs

DURING FLIGHT #1 SIDE MFD PRODUCED FAIL MESSAGE. WOULD NOT REBOOT.

Part: WIRE HARNESS — INOPERATIVE (MLG DOWNLOCK) · airframe 1,379 hrs

RIGHT MAIN LANDING GEAR DOWN LOCK LIGHT WOULD NOT ILLUMINATE ON GEAR PANEL. APPROACH TO HOSPITAL ABORTED AND AIRCRAFT RETURNED TO HANGAR. MAIN GEAR TESTED TO ENSURE DOWN AND LOCKED. TESTING REVEAL RIGHT MAIN GEAR WIRE HARNESS DOWN SENSOR INOPERATIVE. THE WIRE HARNESS REPLACED AND AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN · airframe 1,265 hrs

NR 2 MCDU FAILURE LIGHT ON POWER UP. LOCATED BROKEN WIRE AT CONNECTOR PLUG P180R PIN 39, MCDU HEALTH DISCREET TO VMM P100R B H05 PIN. WIRE WAS TOO SHORT UPON ORIGINAL INSTALL, REULT CAUSED BREAKAGE

Part: WIRE HARNESS — DAMAGED (RT MLG) · airframe 1,263 hrs

RIGHT MLG HARNESS CAUSING LANDING GEAR POSITION INDICATION FAULTS. ABORTED APPROACHED. RETURNED TO BASE. GEAR CONFIRMED DOWN PRIOR TO LANDING. INSTALLED SEGMENT (S26 LEG) REMOVED FROM REPLACEMENT HARNESS AND INSTALLED.

Part: AHRS — FAILED (NR 2) · airframe 1,257 hrs

NR 2 AHRS FAILED ON RUN UP.

Part: SERVO — LEAKING (MLG) · airframe 1,257 hrs

NR 2 SERVO BYPASS WHEN GEAR UP SELECTED. HYDRAULIC LEAK.

Part: MOTOR — FAILED (BLOWER) · airframe 1,247 hrs

FAILED, EVAPERATION BLOWER.

Part: COVER — SPLIT (GLARESHIELD) · airframe 1,185 hrs

GLARESHIELD COVER IS CRACKING AND SPLITTING.

Part: TRANSDUCER — INTERMITTENT (ZONE 200) · airframe 10,063 hrs

MINOR DECU FAULT, COLLECTIVE POSITION FAULT.

Part: ENGINE — POWER LOSS · airframe 4,967 hrs · 8,528 cycles

DURING CLIMB OUT FROM CONFINED AREA, ENGINE AND ROTOR RPM FLUCTUATED. ROTOR RPM DROOPED, COLLECTIVE APPLIED, ACTIVATED NR 2 ENGINE OEI LIGHT.

Part: BEARING SUPPORT — LOOSE (NR 2 DRIVESHAFT) · airframe 3,632 hrs

NR 2 DRIVESHAFT SUPPORT BEARING EXTREMELY LOOSE IN HOUSING. EXCESSIVE GREASE PURGED OUT.

Part: RELAY — NO TEST (ATTITUDE) · airframe 3,232 hrs

STANDBY ATTITUDE IND WILL NOT TEST.

Part: HEATER — INOPERATIVE (NR 1 NACELLE) · airframe 3,232 hrs

NR 1 ENGINE HEATED FIREWALL INOP, WILL NOT HEAT. TEMP SENSOR BAD.

Part: BOLT — DAMAGED (M/R BLADE) · airframe 3,232 hrs

1 M/R BLADE RETENTION BOLT HAS 1 PULLED THREAD.

Part: HEATER — INOPERATIVE (STATIC PORT) · airframe 3,232 hrs

LT UPPER HEATED STATIC PORT WILL NOT HEATUP.

Part: PRESSURE SWITCH — STICKING (INLET ANTI ICE) · airframe 3,232 hrs

NR 1 ENGINE INLET ANTI-ICE LIGHTS INTERMITTENTLY.

Part: TRANSPONDER — INOPERATIVE (ATC) · airframe 3,005 hrs

ATC UNABLE TO TRACK AIRCRAFT TRANSPONDER INFLIGHT.

Part: MOTOR — INOPERATIVE (BLOWER) · airframe 2,991 hrs

AIRCONDITIONING EVAP BLOWER INOPERATIVE.

Part: MOTOR — INOPERATIVE (BLOWER) · airframe 2,991 hrs

VENT BLOWER INOPERATIVE.

Part: WIRE HARNESS — INTERMITTENT (ELECTRICAL) · airframe 2,951 hrs

MULTIPLE T5 SIGNAL FAULTS DURING STARTING. NO AUTOSTART AVAILABLE. HARNESS LOSES CONTINUITY AT PLUG P528 AT DECU ASSY.

Part: WIRE — CHAFED (AC GENERATOR) · airframe 2,367 hrs

AC GENERATOR WILL NOT COME ON LINE DURING TEST, WIRES CHAFED IN BOX ASSY. REPLACED WITH OVERHAULED ITEM (P/N 90320-1, S/N 010) RETURNED TO SERVICE.

Part: AUTOPILOT SYS — INTERMITTENT (NR 2) · airframe 2,122 hrs

NR 2 ROLL CHANNEL ROCKING BACK AND FORTH ON AUTOPILOT SYSTEM

Part: TURBINE — CRACKED (RT ENGINE) · airframe 2,070 hrs · 3,501 cycles

CONTAINMENT SHIELD CRACKED. REPLACED ITEM I/A/W TURBOMECA S/B 292722022 TU 22.

Part: SHIELD — CRACKED (LEFT ENGINE) · airframe 2,070 hrs · 3,501 cycles

CONTAINMENT SHIELD CRACKED. REPLACED ITEM IAW TURBOMECA S/B 292722022 TU 22.

Part: TORQUE BOX — INTERMITTENT (ENGINE) · airframe 1,889 hrs

REPLACED TORQUE TRIM CONFORMATION BOX. NO FURTHER DEFECTS

Part: SCREW — CORRODED (M/R TIP CAP) · airframe 881 hrs

HAD ONE SCREW BREAK ON REMOVAL. NR 1 BOTTOM POSITION LEADING EDGE. CORROSION AND EXCESSIVE BREAKING, TORQUE NOTED ON ALL MAIN ROTOR BLADES. ALL ATTACHMENT REPLACED AS PRE-CAUTION.(K)

Part: SCREW — CRACKED (BLADE TIP CAP) · airframe 459 hrs

ONE (1) SCREW CRACKED NR 1 BOTTOM POSITION FROM LEADING EDGES.

Part: SCREW — CRACKED (BLADE TIP CAP)

MAIN ROTOR TIP CAP SCREWS/ MAIN ROTOR BLADE. HAD ONE (1) SCREW CRACKED, NR 1 UPPER POSITION LEADING EDGE. REPLACED AT 292.2 A/C HOURS. HAD ONE (1) SCREW CRACKED NR 1 BOTTION POSITION LEADING EDGE.

Part: SCREW — CRACKED (BLADE TIP CAP) · airframe 714 hrs

ONE SCREW CRACKED NR 1 BOTTOM POSITION LEADING EDGES.

Part: WIRE — CHAFED (NR 2 ENGINE)

NR 2 ENGINE DECU FAULT, T 1 FAILURE IN FLIGHT, ENROUTE. FOUND CHAFED WIRE. REPLACED HARNESS.