N861CA

Cancelled 2006

Deregistered aircraft · 1995 Beech 1900D · Pratt & Whitney PT6A series

Cancelled
October 26, 2006
Exported to
Canada
Status when cancelled
Triennial form not returned
Serial number
UE-164
Year built
1995
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, commuter
Airworthiness date
September 1, 1995
Certificate issued
March 11, 2003
Last registry action
March 21, 2006
Mode S code
ABD2C1
Owner when cancelled
Raytheon Aircraft Credit Corp
Location
Wichita, KS
Owner type
Corporation

From the FAA registry file of November 5, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N861CA and the event date: up to this one’s cancellation.

Service difficulty reports · 9

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2001F00583Spar Cap · corrodedDURING FUEL TANK INSPECTION, CORROSION ON LEFT AND RIGHT WING LOWER SPAR CAP AT WING STATION 124.5 WAS NOTED. (M)Jun 15, 2001 · N861CA · Beech 1900D · Wing SparSDR 98ZZZM950Power Section · restrictedDURING PREFLIGHT INSPECTION, LEFT PROP FAILS TO TURN FREELY DUE TO APPARENT INTERNAL POWER SECTION RESTRICTION. LOOSE PT BAFFLE (AIR SEAL) SUSPECTED PROBLEM. REPLACED POWER SECTION MODULE WITH AIRWORTHY MODULE IAW PW AND RAYTHEON MM. LEAK CHECK AND OPERATIONov 24, 1998 · N861CA · Beech 1900D · Turbine SectionSDR 98ZZZX2514Control Cable · failedPARKING BRAKE INOPERATIVE. CONTROL CABLE FAILURE. REPLACED PARKING BRAKE CONTROL CABLE. OPS SATISFACTORY IAW CHAPTER 32. (X)Jun 26, 1998 · N861CA · Beech 1900D · Landing Gear Brake SystemSDR 98ZZZX1091Prop Governor · failedAFTER TAKEOFF, PROPELLER RPM WENT TO 1,800. CREW ABLE TO REDUCE RPM TO 1,450, AND RETURNED TO FIELD. PROPELLER GOVERNOR FAILURE. REMOVED AND REPLACED PROPELLER GOVERNOR.Feb 25, 1998 · N861CA · Beech 1900D · Propeller GovernorSDR 98ZZZM300Actuator · brokenFLAP SYSTEM INOPERATIVE. LEFT INBOARD FLAP ACTUATOR BROKEN. (M)Feb 6, 1998 · N861CA · Beech 1900D · Trailing Edge Flap ActuatorSDR 98ZZZM153Arm · loosePILOT REPORTED ABNORMAL RUDDER CONTROL MOVEMENTS. INVESTIGATION AND INSPECTION OF CONTROL SYSTEM DISCOVERED RUDDER ARM ATTACHMENTS TO TORQUE SHAFT. LOOSE DUE TO LOOSE AND WORN FASTENERS (RIVETS) UNIT WAS REPLACED WITH NEW TORQUE SHAFT ASSEMBLE.Jan 2, 1998 · N861CA · Beech 1900D · Rudder Control SystemSDR 97ZZZM1214Torque Gauge · failedLEFT TORQUE GAUGE INOPERATIVE ON TAKEOFF ROLL, TAKEOFF ABORTED. TORQUE GAUGE FAILURE. REMOVED AND REPLACED LEFT TORQUE GAUGE. (M)Oct 31, 1997 · N861CA · Beech 1900D · Engine BMEP/Torque IndicatingSDR 97ZZZM890Rt Unit · wetWX RADAR FAILED DUE TO MOISTURE IN RAYDOME.Aug 13, 1997 · N861CA · Beech 1900D · Weather Radar SystemSDR 97ZZZX3512Air Cycle Mach · seizedCABIN COOLING MALFUNCTION. FOUND ACM TURBINE SEIZED.Jun 19, 1997 · N861CA · Beech 1900D · Cabin Cooling System

Other aircraft with N861CA · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N861CA is registered now to the first aircraft listed.