N199CA
Registered owner: CAPITAL HOLDINGS 109 LLC, MD (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.
6 reports on file, 1996-07-03 – 2007-04-01.
Part: FITTING — LOOSE (FUEL LINE)
DURING THE INSPECTION FOR SB 07-71-01 THE FUEL RETURN LINE AT THE FIREWALL BULKHEAD FITTING WAS FOUND LOOSE. (K)
Part: CONNECTOR — CONTAMINATED (NR 2 ENGINE)
NR 2 FIRE WARNING SYSTEM CAME ON IN FLIGHT, ALL ENGINE INDICATIONS WERE NORMAL. THE PILOT CONTINUED THE FLIGHT AND MONITORED ENGINE, AND ENGINE INDICATORS. FLIGHT CONDITIONS WERE IN WET SNOW. MOISTURE CONTAMINATION OF ELECTRICAL CONNECTOR TO NR 2 ENGINE LOWER SENSOR CAUSED A FALSE FIRE WARNING. CLEANED AND DRIED CONNECTOR, REMOVED, AND REPLACED NR 2 LOWER FIRE LOOP. (M)
Part: ENGINE — SHUTDOWN (NR 2)
GTF - FLT 5031 - UNCOMMANDED NR 2 ENGINE SHUTDOWN DURING DESCENT INTO GTF AFTER POWER LEVER WAS RETARDED. UPON ARRIVAL INTO GTF, THE ENGINE, IGNITION, AND AUTO IGNITION SYSTEMS WERE INSPECTED, AND OPERATIONALLY CHECKED. THERE WERE NO DEFECTS NOTED THE AIRCRAFT WAS RETURNED TO SERVICE. THE FOLLOWING FLIGHT THE AIRCRAFT WAS PLACED IN THE SAME FLIGHT ATTITUDE, AND ALTITUDE IN AN ATTEMPT TO DUPLICATE THE PROBLEM. THE AIRCRAFT PERFORMED PROPERLY AND THERE HAVE BEEN NO OCCURRENCES SINCE THAT TIME. (M)
Part: TERMINAL — LOOSE (WINDSHIELD)
FLT 1713 - DEN - SMOKE AND FUMES IN THE COCKPIT REPORTED BY PILOT. LOOSE GROUND WIRE TERMINAL CONNECTION AT RIGHT FORWARD WINDSHIELD. RIGHT WINDSHIELD HEAT DEFERRED PER MEL 30-1-2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 1,800 hrs
CPR - FUSELAGE FRAME CRACKED .75 INCH IN LENGTH AT STA 409 JUST RIGHT OF CENTER BELLY OF AIRCRAFT. SUBMITTER SUSPECTED CAUSED BY FOD. PERFORMED DOUBLER REPAIR; STOP DRILLED THE CRACK, FABRICATED DOUBLER WITH .032 INCH 2024T3 ALUMINUM AND INSTALLED WITH MS20470AD4 RIVETS. COMPLETED FAA FORM 337. (X)
Part: TIRE — RECAP FAILED (LT MLG)
DEN - FLT 1825 - NO GEAR DOWN AND LOCKED INDICATION ON LT MLG ON DESCENT INTO DEN. PILOT PERFORMED TOWER FLYBY AND COMPLETED EMERGENCY GEAR EXTENSION PROCEDURES. ACFT LANDED WITHOUT FURTHER INCIDENT. ENGINES WERE SHUT DOWN AND PROPS WERE FEATHERED UPON LANDING AS PRECAUTIONARY MEASURE. NR 1 TIRE (LT OTBD) RECAP TREAD CAME OFF DURING TAKEOFF. THIS SEPARATED THE CANNON PLUG ON THE LOWER MLG DRAG LEG FOR THE DOWNLOCK SWITCH. TIRE MISSING TREAD. STILL HOLDING AIR, WAS DEFLATED BEFORE REMOVAL. REMOVED AND REPLACED NR 1 WHEEL ASSY, REPAIRED BROKEN CANNON PLUG AND INSPECTED AREA FOR FURTHER DAMAGE. NONE WAS NOTED. GEAR SWING PERFORMED WITH NO FURTHER DEFECTS NOTED.