N852CA
Registered owner: REBBENKYO ASSOCIATION LLC, DE (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
No NTSB accidents or incidents on file for this aircraft.
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.
14 reports on file, 1995-06-03 – 2001-09-08.
Part: HOSE — MISSING (FUEL SYSTEM)
DURING SCHEDULED MAINTENANCE, (FUEL TANK INSPECTION) FOUND RIGHT AFT TRANSFER PUMP FUEL STRAINER AND HOSE NOT INSTALLED ON AIRCRAFT. NOTE: NOT INSTALLED BY MFG.
Part: STRAINER — MISSING (FUEL SYSTEM)
DURING SCHEDULED MAINTENANCE, (FUEL TANK INSPECTION) FOUND RIGHT AFT TRANSFER PUMP FUEL STRAINER AND HOSE NOT INSTALLED ON AIRCRAFT. NOTE: NOT INSTALLED BY MFG.
Earlier reports · 1995–1999 · 12 reports
1999
Part: ENGINE — SEIZED (LEFT)
UPON A NORMAL ENGINE START AT GATE, LEFT ENGINE EMITTED AN ABNORMAL PITCH NOISE FOLLOWED BY A DROP IN N1 SPEED AND A RISE IN ITT INDICATION. OTHER ENGINE INDICATIONS ALSO, INDICATED ABNORMAL INDICATIONS. ENGINE WAS REPLACED. (M)
Part: WASHER — FAILED (NLG STEERING)
UNABLE TO STEER AIRCRAFT FROM RUNWAY AFTER LANDING. INSPECTION OF AIRCRAFT FOUND RIGHT MAIN LANDING GEAR TORQUE KNEE SEPARATED DUE TO WASHER FAILURE, CAUSING CENTER TORQUE KNEE BOLT TO PULL THROUGH TORQUE KNEE. RIGHT MAIN LANDING GEAR, WHEEL ASSEMBLIES, AND BRAKE ASSEMBLIES REPLACED. FLEET INSPECTION INITIATED. (M)
1998
Part: TEMP CONTROLLER — FAILED (CABIN)
FUMES REPORTED IN CABIN EN ROUTE FROM ELM TO BOS. AIRCRAFT DIVERTED TO ALB. UPON INSPECTION OF AIRCRAFT, THE PCB IN THE CABIN TEMPERATURE CONTROLLER HAD BURNED. ADDITIONAL INSPECTION, FOUND WIRES NR H177A22 AND NR H178A22, TO DUCT TEMP SENSOR SHORTED IN CABIN SIDE WALL. WIRING REPAIRED, TEMP CONTROLLER REPLACED. SYSTEM CHECKS TO SPEC, IAW CHAPTER 21 OF MM. (M)
Part: TEMP CONTROLLER — FAILED (CABIN)
DURING DESCENT AT APPROXIMATELY 14,000 FT, A SUDDEN AND STRONG BURNING SMELL WITH A HAZE OF SMOKE FILLED COCKPIT. INSPECTION OF AIRCRAFT FOUND CIRCUIT CARD FAILURE IN CABIN TEMPERATURE CONTROLLER IN CABIN CEILING. UNIT WAS REPLACED AND SYSTEM CHECKED SATISFACTORY IAW CHAPTER 21. (M)
Part: ACTUATOR — FAILED (LT MLG WW)
NO DOWNLOCK INDICATION ON LT MLG. SUSPECTED ACTUATOR ZIGGING. REPLACED LT MLG ACTUATOR.
Part: DOOR STRUT — BROKEN (PAX DOOR)
CABIN DOOR STRUT BROKEN. BROKEN STRUT. REPLACED STRUT. (M)
1997
Part: SWITCH — FAILED (LT FUEL PRESS)
LEFT LOW PRESSURE FUEL ANNUNCIATOR INOP. LEFT LOW PRESSURE FUEL SWITCH FAILED. REMOVED AND REPLACED LEFT LOW PRESSURE SWITCH IAW CHAP 28. (M)
Part: TACH GENERATOR — FAILED (LT ENGINE)
LEFT ENGINE TACHOMETER GENERATOR INOPERATIVE.
Part: PROPELLER — SEALS FAILED (RT ENGINE)
OIL LEAK FROM RT PROPELLER/ENGINE. REPLACED PROPELLER.
1995
Part: LIGHT BULB — FAILED (NLG)
NOSE LANDING GEAR ANNUNCIATOR MODULE BULBS FAILED TO ILLUMINATE ON EXTENSION. INSPECTION OF MODULE FOUND P/N 951-F04 BULBS FAILED. (M)
Part: DE-ICE BOOT — MISSING (RT PROP)
ON RIGHT PROP, THREE INCHES MISSING FROM DE-ICE BOOT ON ONE BLADE. A SECTION OF LEADING EDGE METAL ABRASION STRIP WAS ALSO FOUND DETACHED FROM THE COMPOSITE BLADE. PROP WAS REMOVED AND REPLACED WITH AN AIRWORTHY UNIT. APPARENT CAUSE IMPROPER BONDING. (M)
Part: ELT MOUNT — BROKEN (AFT FUSELAGE)
DURING DETAILED PHASE NR 6 INSPECTION, FOUND ELT MOUNT AND FACE PLATE BROKEN. REPLACED ELT WITH NEW UNIT.