Service difficulty report · Autopilot Sys · Braero BAE125800A

Difficulty date
October 24, 2005
Submitted
October 26, 2005
Operation
Air carrier
Aircraft
N861CW
Make and model
Braero BAE125800A
Aircraft serial
258061
Aircraft time
7,759 hours, 4,944 cycles
Engine
Garrtt TFE7315R
Part
Autopilot Sys
Condition
Malfunctioned
Stage of operation
DE
How discovered
O
Nature of condition
F
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

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.