SEA88IA028

NTSB incident investigation · Canadair CL600-2A12 · Twentynine Plms, CA · December 6, 1987

Incident · No injuriesIncident investigationFinal report
Date
December 6, 1987, 13:23 local (21:23 UTC)
Place
Twentynine Plms, CA
Injuries
2 uninjured
Damage
No damage
Phase of flight
Enroute
Aircraft
N125PSCanadair CL600-2A12
Weather
Visual (VMC) · Day
Status
Completed · report July 10, 1989
Report
Approved by Office Director
FAA report
19871206075519I
Case key
40739

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the incident.

On this page

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionClimb - to cruise
Water and waste system - leakCause
Maintenance,installation - improperUnknownCause
Autopilot/flight director,amplifier and computer - corrodedFactor
Flt control syst,rudder control - erraticFactor
Loss of control - in flightClimb - to cruise
In-flight planning/decision - improperCopilot/second pilotCause
Operation with known deficiencies in equipment - attemptedCopilot/second pilotCause
Autopilot/flight director - engagedCause

Analysis

The water filter housing lower seal was mis-installed which allowed water to seep out and run down the housing case. Over time the water dropped onto a lavatory drain line, followed the line to a low point & collected on the stab aug computer box. The fluid accumulation resulted in corrosion on one of the circuit boards within the computer box causing a power imbalance within the yaw damper system and a subsequent uncommanded rudder signal. Drg the climb to cruise transition a mach trim failure occurred which would have necessitated the use of the autopilot for speeds in excess of 0.7 mach. Operation of the autopilot, however, resulted in operation of the yaw damper system which had been determined to have been producing uncommanded rudder inputs. As the acft was levelled at FL330 and the airspd was allowed to exceed mach 0.7 the coplt activated the autoplt which powered the malfunctioning damper system and a dutch roll maneuver ensued. PIC disconnected the autoplt, executed a descent and recovery.

Aircraft

Registration
N125PS
Reported as
Canadair CL600-2A12
Category
Airplane
Serial number
3058
Airframe hours
336
Engine
GE CF34-1A, 8,600 lbs thrust, turbo fan
Damage
No damage
Flight
Personal · Part 91 subpart F
Registered owner
Omni Restaurant Consulting Cor
Airworthiness certificate
Standard, Transport
Last inspection
100 hour · October 29, 1987 · 36 hours before
Departed
SNA · Santa Ana, CA
Destination
LAS · Las Vegas, NV
Flight plan
IFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
49
Certificates
Airline transport, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
10,510 total · 325 in this make and model · 10,195 as pilot in command · 150 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
260° at 65 knots
Visibility
100 statute miles
Lowest ceiling
None
Temperature
55 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N125PS · 1

Matched to the same aircraft by N-number and date.