N854CA
Registered owner: JUNIE THE FLYING DOG LLC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
17 reports on file, 1995-03-17 – 2003-08-27.
Part: BOLT — LOOSE (CONTROL HORN) · airframe 4,920 hrs · 6,913 cycles
DURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE.
Earlier reports · 1995–2001 · 16 reports
2001
Part: PANEL — SHORTED (COCKPIT)
SMELL OF SMOKE IN COCKPIT DURING FLIGHT, SMOKE COMING FROM LEFT SIDE OF INSTRUMENT PANEL. INSPECTED: FOUND SHORTED EL PANEL WIRE TO BUS BAR TERMINAL BEHIND FUEL QUANTITY INDICATOR PANEL. (WIRE X31F20) ALSO REPLACED WIRES: X30E20, 31E20, 30H20,31G20, 30J20, 31K20, 30K20, 30L20, 31L20, 31M20, 30F20, 31J20, 30A20, 30B20, 31A20, 63A22, 32A20N
1998
Part: LINE — CRACKED (RT ENGINE)
RT PROPELLER WENT INTO FEATHER ON APPROACH. CRACKED P3 DELIVERY LINE. REPLACED RT P3 DELIVERY LINE.
Part: BRACKET — BROKEN (NLG WW)
RED GEAR HANDLE, NO NOSE GEAR GREEN. BROKEN NOSE GEAR DOWN LOCK ACTUATOR BRACKET, REPLACED. (M)
Part: FUEL LINE — FAILED (RT ENGINE)
RIGHT ENGINE FUEL LEAK. FUEL LINE FAILURE. REPLACED FUEL LINE.
Part: TRANSDUCER — FAILED (LT WING)
STALL WARNING WILL NOT TEST. FAILED LIFT TRANSDUCER. REPLACED LIFT TRANSDUCER.
Part: CONVERTER — FAILED (FUSELAGE)
WINDSHIELD WIPERS INOPERABLE. COVERTER FAILURE. REPLACED WINDSHIELD WIPER CONVERTER AND FLEX DRIVES.
Part: ACTUATOR — FAILED (LT MLG)
GEAR WOULD NOT EXTEND. MLG ACTUATOR LEAKING. REMOVED AND REPLACED LT MLG ACTUATOR. (M)
1997
Part: WINDSHIELD — CRACKED (COCKPIT)
RIGHT WINDSHIELD, OUTER PLY CRACKED. REPLACED WINDSHIELD. (X)
Part: FIRE LOOP — FAILED (LT ENGINE)
LEFT FIRE PROTECTION AMP TEST INOPERATIVE. FOUND LT ENGINE FIRE LOOP FAILED.
Part: TACHOMETER GEN — FAILED (RT ENGINE)
RIGHT PROPELLER TACHOMETER INOPERATIVE.
Part: BRACKET — BENT (NOSE GEAR)
LANDING GEAR FAILED TO EXTEND ON FIRST TRY. SECOND ATTEMPT OK.
Part: CABLE — BROKEN (CO-PILOTS SEAT)
CO-PILOTS SEAT ADJUSTMENT CABLE BROKEN.
Part: ACTUATOR — FAILED (LT MLG)
PHL - FLT 4474 - GEAR WOULD NOT EXTEND. LT MLG ACTUATOR LEAKING. REMOVED AND REPLACED LT MLG ACTUATOR. GROUND OPS CHECK IAW CHAPTER 32.
1995
Part: DE-ICE BOOT — MISSING (LT PROPELLER)
LEFT PROP, BLADE S/N UNKNOWN, MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE. SUBMITTER STATES THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT INSTALLATION. (M)
Part: DE-ICE BOOT — MISSING (RT PROPELLER)
DE-ICE BOOT UNBONDED FROM ONE BLADE ON RIGHT PROPELLER. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL 361 HOURS AGO AT WHICH TIME BOOT WAS INSTALLED. SUBMITTER STATES UPON INSPECTION OF BOOT AREA ITS APPARENT THAT THE PAINT APPLIED TO THE BLADE PRIOR TO BOOT APPLICATION UNBONDED WITH BOOT END COULD BE THE CAUSE.
Part: DEICE BOOT — MISSING (RIGHT PROPELLER)
DE-ICE BOOT UNBONDED FROM ONE BLADE ON RIGHT PROPELLER. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL 198 HOURS AGO AT WHICH TIME THE BOOT WAS INSTALLED. UPON INSPECTION OF BOOT REMOVED, DISCOVERED THE PAINT APPLIED TO THE BLADE WAS STUCK TO GLUE ON THE BOOT.