N205CA

Part: BLOWER MOTOR — FAILED (HEATER) · airframe 22,429 hrs · 38,240 cycles

PILOT REPORTED BURNING SMELL IN CABIN, THEY TURNED THE HEATER OFF AND SMELL DISSIPATED. MAINTENANCE INSPECTED AND FOUND THE COMBUSTION BLOWER INOPERATIVE. MAINTENANCE REPLACED THE COMBUSTION BLOWER WITH NO FURTHER DEFECTS NOTED.

Part: SEAL — LEAKING (FUEL PUMP) · airframe 19,989 hrs · 35,302 cycles

PILOT NOTED FUEL SMELL IN FLIGHT, DEACTIVATED THE HEATER AND THE SMELL WENT AWAY. MAINTENANCE INSPECTED AND FOUND FAILED SHAFT SEAL ON THE HEATER FUEL PUMP. FUEL PUMP WAS REPLACED WITH NO FURTHER DEFECTS NOTED.

Part: EXHAUST VALVE — DAMAGED (NR 5 CYLINDER) · airframe 32,333 hrs

CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.

Part: PUMP — LEAKING (FUEL SYSTEM) · airframe 16,526 hrs · 32,289 cycles

PILOT REPORTED STRONG FUEL ODOR IN CABIN. MAINTENANCE INSPECTED HEATER AND HEATER FUEL INLET, FOUND HEATER FUEL PUMP LEAKING AND REPLACED THE HEATER FUEL PUMP, OPERATIONAL AND LEAK CHECKED GOOD. ADDITIONAL DETAILS WILL BE MADE AVAILABLE UPON TEARDOWN REPORT RECEIPT.

Part: FUEL LINE — LEAKING (HEATER) · airframe 15,648 hrs · 31,094 cycles

PILOT REPORTED GAS SMELL FROM HEATER. RAN THE HEATER & FOUND FUEL LEAK COMING FROM HEATER FUEL PUMP LINE ON THE OUTLET SIDE AT FITTING. R & R HEATER FUEL LINE. PERFORMED LEAK & OPERATIONS CHECK, EVERYTHING OK IAW MM.

Part: WIRE — BROKEN (MLG C/B PANEL) · airframe 30,024 hrs · 44,905 cycles

DURING CLIMB OUT OF A FERRY FLIGHT, CREW ATTEMPTED TO RETRACT THE LANDING GEAR. GEAR LIGHTS REMAINED IN THE DOWN AND 3 GREEN POSITION. ELECTED TO RETURN TO DEPARTURE. CREW PERFORMED A FLY BY OF THE TOWER, WHO ADVISED IT APPEARED THE RT GEAR WAS NOT FULLY EXTENDED. PERFORMED THE MANUAL GEAR EXTENSION ITEMS IN THE ABNORMAL CHECKLIST, DECLARED AN EMERGENCY AND PERFORMED A SECOND FLY-BY, TOWER ADVISED ALL GEAR TO BE IN THE EXTENDED POSITION. ACFT LANDED WITH NO FURTHER INCIDENT AND SHUTDOWN ON THE NEAREST TAXIWAY. MX TROUBLESHOT ACFT AND FOUND BROKEN WIRE AT CIRCUIT BREAKER (CB107) ON THE LANDING GEAR PANEL. MX REPAIRED THE WIRE AND OPS GEAR SWINGS AND FUNCTIONAL CHECKS WERE GOOD. ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.

Part: DOOR — NOT LATCHED (FUEL SERVICE)

SERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR CLOSED AND AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — DIRTY (AUTO FEATHER SYS)

AUTOFEATHER SYSTEM INOPERABLE DURING TAKEOFF. CLEANED THE AUTOFEATHER ARMING SWITCHES IN POWER LEVER QUADRANT.

Part: SIGN — LOOSE (CABIN)

EXIT SIGN LOOSE AT ROW 5A. REPLACED EXIT SIGN.

Part: T/O WARNING — MALFUNCTION (E/E COMPT)

'TRIM' AURAL WARNING DURING TAKEOFF. REPLACED THE AUDIO WARNING UNIT.

Part: ACTUATOR — MALFUNCTUATING (RT TE FLAP)

OUTBOARD FLAP INDICATION IS FLUCTUATING BETWEEN 2 AND 7 UNITS. COULD NOT DUPLICATE DISCREPANCY. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR FOR TROUBLESHOOTING.

Part: CROSSBEAM — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.

Part: BUTTSTRAP — CORRODED (LAVATORY)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

2C TASK 532D-147-03I REVEALED RIGHT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CENTER BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

2C TASK 151-01Z REVEALED LEFT CROSSBEAM TO BE CORRODED AT FRAME 33. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES.

Part: SILL — CORRODED (LAVATORY)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CABIN SILL RIGHT TO BE HEAVILY CORRODED. REMOVED CORRODED SILL AND INSTALLED SERVICABLE SILL USING EMB 120 STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 23 TO BE CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

2C TASK 5320-147-03I REVEALED CROSSBEAM (RIGHT) AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

2C TASK 532D-147-03I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEBLE PART USING EMB 120 STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICABLE PART USING EMB 120 STANDARD PRACTICES.

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB 120 SRM STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (FUSELAGE)

2C INSPECTION TASK 5310-131-01I REVEALED THAT THE RIGHT CROSSBEAM AT FRAME 16 WAS CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES.

Part: FRAME T-SECTION — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT MIDDLE T-SECTION AT FRAME 16 TO BE HEAVILY CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICABLE T-SECTION USING EMB120 SRM STANDARD PRACTICES.

Part: SOLENOID — SHORTED (CABIN)

ON 1C TASK 35-09, THE OXYGEN MASKS AT ROW 9 FAILED TO DEPLOY. INVESTIGATION FOUND THE OXYGEN MASK DOOR SOLENOID TO BE SHORTED. THE SOLENOID WAS REPLACED WITH A NEW PART, OK FOR SERVICE.

Part: RELAY BOX — MALFUNCTIONED (E/E COMPT)

SMOKE IN COCKPIT AND CABIN AFTER PUSH BACK. FOUND GROUND COOLING FANS NOT OPERATING. REPLACED THE LANDING GEAR RELAY BOX.

Part: PCU — DAMAGED (PROP ASSY)

PCU ASSEMBLY REMOVED FROM AIRCRAFT FOR AD 95-22-12 COMPLIANCE. UPON INITIAL RECEIVING INSPECTION SEVERAL OF THE FORWARD PORTION OF THE SPLINES WERE FOUND TO BE GROUND DOWN. PCU WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER FOR FURTHER DISPOSITON.

Part: RADAR ANTENNA — FAILED (NOSE)

WEATHER RADAR DOES NOT WORK. REPLACED THE ANTENNA.

Part: ACTUATOR — MALFUNCTION (LT TE FLAP)

FLAP CONTROL FAULT WARNING WITH FLAPS RETRACTED. REPLACED THE LT OUTBOARD FLAP ACTUATOR.

Part: SKIN — BIRD STRIKE (FUSELAGE)

BIRD STRIKE ON LOWER FUSELAGE. INSPECTED EXTERIOR OF AIRCRAFT AND FOUND NO EVIDENCE OF BIRD STRIKE.

Part: FLAP CONTL UNIT — MALFUNCTIONED (E/E COMPT)

FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP CONTROL UNIT.

Part: DEICE BOOTS — WORN (LT/RT WING)

LT AND RT WING DEICE BOOTS AND LT AND RT ENGINE INLET DEICE BOOTS FAILED DURING FLIGHT. REPLACED WING AND ENGINE INLET DEICE BOOTS.

Part: SIGN — MISSING (CABIN)

EMERGENCY EXIT SIGN AT ROW 5 IS MISSING. REPLACED EMERGENCY EXIT SIGN.

Part: FLAP CONTL UNIT — MALFUNCTION (E/E COMPT)

FLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,052.

Part: PROPELLER — LEAKING (LT ENGINE)

LEFT ENGINE LEAKED A LARGE AMOUNT OF OIL DURING TAXI FROM HANGAR TO GATE. REPLACED THE LT PROPELLER ASSY.

Part: CONTROL VALVE — FAILED (LT ENGINE INLET)

LEFT INLET BOOT FAILED IN-FLIGHT. REPLACED LEFT INLET DEICE EJECTOR VALVE.

Part: WIRE — CHAFED (RT NACELLE)

RT HYDRAULIC RESERVOIR LOW PRESSURE INDICATOR ILLUMINATED. REPAIRED CHAFED WIRE AT PRESSURE SWITCH.

Part: CONTROL BOX — MALFUNCTION (LANDING GEAR)

LANDING GEAR INTRANSIT LIGHTS REMAINED ON WITH GEAR RETRACTED. REPLACED THE LANDING GEAR CONTROL BOX.

Part: FLAP TRACKS — DIRTY (TE FLAPS)

FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. CLEANED AND INSPECTED FLAP TRACKS AND OPERATIONAL CHECK NORMAL.

Part: ANNUNCIATOR — DEFECTIVE (INST PANEL)

TAKEOFF FLAPS AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE FLAP ANNUNCIATOR UNIT.

Part: IVA-81A AV — DEFECTIVE (LEFT)

THE PILOTS VSI IS COMPLETELY UNUSABLE IN ALL PHASES OF FLIGHT. REPLACED THE PILOTS TCASIVSI.

Part: TQ SIG COND — DEFECTIVE (LT PROP)

LEFT TORQUE INDICATION ERRATIC. LEFT PROPELLER AUTOFEATHERED. REPLACED THE TORQUE SIGNAL CONDITIONER.

Part: AHRS — DEFECTIVE (NR 1)

PILOTS ESHI SHOWS RED FLAG. REPLACED THE NR NR 1 AHRS.

Part: ENGINE — FAILED (LEFT)

LEFT ENGINE FAILED ABRUPTLY IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE.

Part: SKIN SUPPORT — CRACKED (LT/RT WING)

THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-013, 1 EA; 120-17057-005, 1 EA; 120-17059-017, 1 EA; 120-17059-015, 2 EA; 120-17059-019, 1 EA; 120-17063-009, 2 EA; 120-17057-006, 1 EA; 120-17062-005, 1 EA.

Part: SENSOR — DEFECTIVE (NLG)

NLG A SYSTEM INTRANSIT LIGHT IS ILLUMINATING INTERMITTENTLY. REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR.