N861CW

No registry detail on file · not in current registry

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.

1 report on file, 2005-10-24.

FLT CONT AFFECTED · 2005-10-24 Matched by certificate designator
ATA 2210

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 7,759 hrs · 4,944 cycles

WHEN CREW SELECTED VERTICAL SPEED ON MODE CONTROL PANEL TO BEGIN DESCENT, AC BEGAN STEEP CLIMB, AIRSPEED INDICATOR WAS NEAR BARBER POLE. CONTROL COLUMN YOKE WAS PUSHED FWD TO REDUCE CLIMB. AC FOUGHT CREW BY TRIMMING AC FURTHER NOSE UP. CLIMB WAS REPORTED TO HAVE STEEPENED, AC WAS CLOSING IN TO BASE OF RVSM AIRSPACE. AC WAS THEN ROLLED BY CREW TO APPROX 100 DEGREES BANK IN ORDER TO VECTOR LIFT DOWNWARD AND MAINTAIN A POSITIVE LOAD ON WINGS. FOLLOWING MANEUVER, AC STOPPED CLIMB. NML LANDING WAS MADE W/O FURTHER INCIDENT. MAINT HAS ISSUED MEL FOR AUTO-PILOT SYS AND MEL DUE TO VERT SPEED IND ON CAPTAINS SIDE JUMPING ERRATICALLY + / - 100 TO 300 FT. AIRSPEED INDICATION HAD SPLIT BETWEEN LT, RT INDICATORS.

Source: SDR DJFA2005155