N857CA

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,054 hrs · 39,645 cycles

FWD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACKS OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,987 hrs · 39,566 cycles

MAIN CABIN DOOR AND RT EMERGENCY EXIT LIGHT INOPERATIVE. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 35,671 hrs · 39,180 cycles

EMERGENCY LIGHT AT ROW 1 IS INOPERATIVE. PERFORMED OPS CHECKED AND LIGHT IS WORKING AS REQUIRED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,495 hrs · 38,963 cycles

FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY UNIT AT POSITION NR 2, OPS CHECK SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,491 hrs · 38,957 cycles

1 OVERHEAD AND 2 SIDEWALL EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY PS2 OPS CHECK SATISFACTORY. R & R POWER SUPPLY UNIT 60-3844-3, OFF SN 3571.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,156 hrs · 38,564 cycles

LEFT AFT EXTERIOR EMER EGRESS LIGHT INOPERATIVE. DEFERRED IAW MEL. R & R NR 7 POWER SUPPLY UNIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,089 hrs · 38,497 cycles

AFT EMER LIGHT OUT. R & R LT AFT EMER EGRESS LIGHT BULB.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,936 hrs · 38,331 cycles

LEFT AFT EMER EGRESS LIGHT INOPERATIVE. R & R SET OF BATTERIES & EMER LIGHT SWITCH IN COCKPIT, PN 61-0478-11 & 61-0478-9.

Part: HANDLE — BROKEN (EMERGENCY EXIT) · airframe 34,794 hrs · 38,178 cycles

TYPE 1 EMER EXIT DOOR HANDLE BROKEN. R & R TYPE 1 EMER DOOR ASSIST HANDLE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,610 hrs · 37,984 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R 6 EMER LIGHT BATTERIES. PERFORMED OPERATIONS CHECK. THE RESULTS OF THE OPERATIONS CHECK WAS SATISFACTORY.

Part: PROPELLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 34,529 hrs · 37,899 cycles

NUMBER 1 ENG UN-COMMANDED FEATHER ON CLIMB. R & R PROPELLER ASSEMBLY, OPERATIONS CHECK & LEAK CHECK SATISFACTORY.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 34,384 hrs · 37,747 cycles

APU FIRE DETECTION LOOP FAULT LIGHT, FIRE DETECTION WARNING LIGHT ILLUMINATED. DEFERRED IAW MEL.

Part: SOLENOID VALVE — TRIPPED (TE FLAPS) · airframe 33,215 hrs · 36,453 cycles

FLAPS WOULD NOT EXTEND ON LANDING. FLAP CONT L7 POPPED & WOULD NOT RESET. R & R FLAP POWER UNIT SOLENOID VALVE.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 33,172 hrs · 36,408 cycles

DURING CRUISE ENCOUNTERED SEVERE ICE, PITOT HEAT 1 & 2 FAILED. LOST ALL AIRSPEED INDICATION. AUTOPILOT KICKED OFF. AIRSPEED DID NOT RETURN UNTIL OUT OF ICE CONDITIONS. RESET BREAKER LHDC H6, RH DC N4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,310 hrs · 35,490 cycles

RED EMER FLOOR STRIP INOPERABLE. R & R RED EMER FLOOR LIGHT STRIP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,497 hrs · 34,663 cycles

SEVERAL EMER LIGHTS INOPERABLE. CHARGED BATTERIES.

Part: DITCHING DAM — LOW PRESSURE (CABIN) · airframe 30,976 hrs · 34,115 cycles

PRESSURE OF LT SIDE DITCHING DAM NITROGEN IS LOW. SERVICED LT DITCHING DAM NITROGEN.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 30,646 hrs · 33,735 cycles

AFT CEILING EMERGENCY EXIT SIGN FASTEN SEAT BELT INDICATES ON WHEN SELECTED OFF & NO SMOKING SIGN DOES NOT ILLUMINATE UNLESS SELECTED ON. TURNED EMERGENCY EXIT SIGN 180 DEGREES, OPERATIONS CHECKED SATISFACTORY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,420 hrs · 33,466 cycles

FWD EMERGENCY CEILING LIGHT INOPERATIVE. R & R FWD EMERGENCY CEILING LIGHT BULB.

Part: COMPUTER — FAILED (RADIO ALTIMETER) · airframe 29,414 hrs · 32,301 cycles

ON LANDING, THE THE NR 1 & NR 2 ECU MANUAL LIGHTS ILLUMINATED. THE NR 1 RADIO ALTIMETER COMPUTER WAS REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,382 hrs · 32,266 cycles

THE EMERGENCY LIGHT FROM SEATS 1D TO 2D WAS INOPERATIVE. LIGHT REPLACED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 29,260 hrs · 32,125 cycles

DURING CRUISE FLIGHT, CREW RECEIVED A PASSENGER DOOR CAUTION LIGHT. THE CREW DECLARED AND EMERGENCY AND LANDED SAFELY. NO LOSS OF PRESSURIZATION WAS EXPERIENCED. MX ADJUSTED THE OVER CENTER PROXIMITY SENSOR.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,919 hrs · 31,726 cycles

DURING PREFLIGHT, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TESTING. THE CREW RAN THE ACFT TO CHARGE THE BATTERIES. AFTER THE BATTERIES WERE CHARGED ALL OPS TEST PRODUCED SATISFACTORY RESULTS.

Part: PRESSURE SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 28,813 hrs · 31,604 cycles

DURING CRUISE FLIGHT, THE CREW REPORTED THAT THE CABIN PRESS WARNING LIGHT ILLUMINATED IN FLIGHT. NEITHER MANUAL OR AUTO MODES OF PRESSURIZATION WERE INOPERATIVE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. R & R THE CABIN PRESSURE WARNING SWITCH. ALL OPS TEST PRODUCED SATISFACTORY RESULTS.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 28,366 hrs · 31,071 cycles

CREW REPORTED THAT THE PASSENGER DOOR WARNING LIGHT ILLUMINATED DURING CRUISE FLIGHT. CREW DECLARED AN EMERGENCY AND THE ACFT LANDED WITHOUT FURTHER INCIDENT. GROUND MX CREW WAS UNABLE TO DUPLICATE THE ERROR. ALL OPS CHECKS PRODUCED SATISFACTORY RESULTS AND THE ACFT WAS RETURNED TO SERVICE.

Part: CHECK VALVE — FAILED (HYD SYSTEM) · airframe 28,317 hrs · 31,007 cycles

DURING APPROACH, CREW EXPERIENCED SEVERAL WARNING AND CAUTION LIGHTS RELATED TO THE HYDRAULIC SYSTEM. NR 2 SYS WAS INDICATING A ZERO QUANTITY. ABORTED APPROACH AND DECLARED AN EMERGENCY AND PERFORMED EMERGENCY PROCEDURES. ACFT LANDED WITHOUT INCIDENT. GROUND MX CREW TRACED THE ISSUE TO A BAD HYD CHECK VALVE PN 3-1582-2-3.

Part: SKIN — DAMAGED (TAIL) · airframe 27,930 hrs · 30,544 cycles

ON LANDING, CREW OBSERVED THE TOUCHED RUNWAY LIGHT ILLUMINATE. CREW NOTIFIED MX OF THE ILLUMINATED LIGHT. GROUND MX CREW INSPECTED THE ACFT AND FOUND DAMAGE TO THE TAIL BUMPER AREA. ACFT REMOVED FROM SERVICE. PERFORMED A HARD LANDING INSPECTION, A TOUCHED RUNWAY INSPECTION, AND MADE SKIN REPAIRS TO THE TAIL BUMPER SECTION OF THE ACFT. ONCE ALL INSPECTIONS AND REPAIRS WERE SATISFACTORY THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,774 hrs · 30,376 cycles

DURING PRE-FLIGHT, CREW NOTICED EMERGENCY LIGHTS WERE INOPERATIVE. GROUND MX CREW R & R THE EMERGENCY LIGHTS AND ESCAPE PATH POWER SUPPLY UNITS. OPS CHECKED SATISFACTORY. ACFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (CARGO BAY) · airframe 26,646 hrs · 29,112 cycles

FLIGHT REPORTED THAT THE BAGGAGE SMOKE WARRING INTERMITTENT IN FLIGHT, FLIGHT DIVERTED. MX REMOVED AND REPLACED NR 2 SMOKE DETECTOR. OPS CHECKED SATISFACTORY.

Part: BLEED AIR SYS — ODOR (APU) · airframe 26,570 hrs · 29,029 cycles

FLIGHT CREW REPORTED ON LOG THAT THE LAVATORY SMOKE DETECTOR FLICKERED INTERMITTENTLY. MX CREW INSPECTED SMOKE DETECTOR FOUND OIL ODOR TO BE COMING FROM APU WHILE RUNNING BLEEDS. APU WAS PLACED ON THE MEL LIST AND NO OTHER DEFECTS WERE NOTED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 26,548 hrs · 29,003 cycles

FLIGHT CREW REPORTED ON THAT THE LAVATORY SMOKE DETECTOR IS ACTIVATING INTERMITTENTLY. MX CREW R & R THE LAVATORY SMOKE DETECTOR PERFORMED. OPS CHECK SATISFACTORY.

Part: LIGHT — BROKEN (CABIN) · airframe 26,294 hrs · 28,729 cycles

MX FOUND THAT THE FWD 2 RED LIGHTS ON SECOND EMERGENCY FLOOR LIGHT STRIP ARE NOT WORKING. R & R LIGHT STRIP PERFORMED. OPS CHECKED SATISFACTORY.

Part: DOOR — LEAKING (EMERGENCY EXIT) · airframe 26,262 hrs · 28,695 cycles

FLIGHT CREW REPORTED THAT THE TYPE 1 EMERGENCY EXIT DOOR WAS MAKING A LOUD NOISE AND WATER WAS COMING INTO THE CABIN. MX R & R THE EMERGENCY EXIT DOOR WITH A SERVICEABLE DOOR. PERFORMED OPS CHECK WAS SATISFACTORY.

Part: SMOKE DETECTOR — INTERMITTENT · airframe 26,074 hrs · 28,487 cycles

FLIGHT CREW REPORTED INTERMITTENT SMOKE WARNING LIGHT IN FLIGHT. MX CREW R & R 1 AND 2 SMOKE DETECTORS AND OPS CHECK WAS SATISFACTORY.

Part: PROPELLER — MALFUNCTIONED (FEATHERING SYS) · airframe 25,909 hrs · 28,299 cycles

FLIGHT CREW REPORTED THAT THEY HAD AN UNSCHEDULED FEATHER AT 2000 FEET. ECU FLICKERED 3 TIMES THEN TORQUE WENT TO 125 FOR 3 TO 5 SECONDS. MX CREW R & R THE ECU AND TSCU AND PERFORMED ALL GROUND RUNS AND TEST FLIGHT WERE SATISFACTORY FDR WILL BE DOWN LOADED AT NEXT EARLIEST CONVENIENCE FOR POSSIBLE OVERTORQUE. FDR WAS READ THEN NR 1 TSCU WAS CHANGED FOR UNSCHEDULED FEATHER. PERFORMED ALL NECESSARY OPS, CHECKS WERE SATISFACTORY ACFT WAS RETURNED TO SERVICE.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 25,751 hrs · 28,132 cycles

FLIGHT CREW REPORTED THAT THE FLIGHT DECK EMERGENCY OVERHEAD LIGHT WOULD NOT TEST. MX RESECURED BULB AND OPS CHECK WAS SATISFACTORY.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 25,736 hrs · 28,118 cycles

FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 1 ARE NOT WORKING. MX CREW RECONNECTED WIRING AT SECOND FLOOR STRIP. OPS CHECK WAS SATISFACTORY.

Part: GEAR — SLIPPED (ELEVATOR TRIM) · airframe 5,662 hrs · 7,618 cycles

WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TRIM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSED ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT.

Part: ACTUATOR — DEFECTIVE (RT MLG)

RIGHT MAIN LANDING GEAR ACTUATOR INDICATOR SLOW TO ILLUMINATE DOWN AND LOCKED. TROUBLESHOOTING FOUND DEFECTIVE DOWN AND LOCKED SWITCH INSIDE ACTUATOR. REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. (M)

Part: GOVERNOR — FAILED (RT ENGINE)

RIGHT ENGINE SURGING IN TORQUE. RIGHT PROPELLER GOVERNOR FAILURE. REPLACED RT PROPELLER GOVERNOR. (M)

Part: SELECTOR — FAILED (COCKPIT)

LANDING GEAR RETRACT CIRCUIT BREAKER OPENS. LANDING GEAR HANDLE FAILURE. REPLACED LANDING GEAR HANDLE IAW BEECH MAINTENANCE MANUAL. (M)

Part: GOVERNOR — MALFUNCTIONED (RT ENGINE)

TAKEOFF ABORTED, RIGHT PROP BEGAN TO FEATHER DURING APPLICATION OF T/O POWER. REPLACED GOVERNOR. (M)

Part: SELECTOR — FAILED (LANDING GEAR)

LANDING GEAR FAILS TO EXTEND NORMALLY.

Part: BLOWER — FAILED (COCKPIT)

INVESTIGATION FOR SMOKE IN COCKPIT FROM ENVIRONMENT BLOWERS. FOUND FORWARD VENT BLOWER FAILED.

Part: RT UNIT — SHORTED (FWD FUSELAGE)

RADAR INOPERATIVE.

Part: DISPLAY — SHORTED (LT COCKPIT)

CAPTAINS EHSI INOPERATIVE.

Part: FUEL PUMP — LEAKING (LT ENGINE)

LEFT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED. FOUND FUEL PUMP LEAKING, LEFT ENGINE.

Part: INVERTER — SHORTED (LT NACELLE)

LEFT AC BUS FAILURE.

Part: CIRCUIT BREAKER — CORRODED (COCKPIT)

CAPTAINS HSI AND CO-PILOTS AND RMI STUCK AT 360 DEGREES. FOUND CIRCUIT BREAKER CORRODED. (M)

Part: WHEEL — CRACKED (NLG)

DURING ROUTINE INSPECTION, NOSE WHEEL WAS DISCOVERED CRACK AROUND VALVE STEM HOLE. REMOVED AND REPLACED COMPLETE WHEEL ASSEMBLY P/N 114-8001-3.

Part: ELT — WET (AFT FUSELAGE)

ELT TRANSMITS CONTINUOUSLY. INVESTIGATION REVEALED THAT REMOTE SW WAS SHORTED DUE TO BEING WET. REMOVED AND REPLACED REMOTE SW P/N 118-34002-1 AND ELT BATTERY PACK P/N 452-0130. (M)