NYC89FA093

NTSB accident investigation · Piper PA-31-350 · Toms River, NJ · March 2, 1989

Accident · No injuriesField investigationFinal report
Date
March 1, 1989, 19:51 local (Mar 2, 1989, 00:51 UTC)
Place
Toms River, NJ
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N40978Piper PA-31-350
Weather
Visual (VMC) · Night/dark
Status
Completed · report September 30, 1991
Report
Approved by Office Director
FAA report
19890301002899A
Case key
36274

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

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Probable cause

Failure of the pilot to maintain airspeed and control of the aircraft, and his exceeding the design stress limits of the aircraft. Factors related to the accident were: autoplt malfunction due to improper installation by maintenance personnel and the pilot's failure to preflight the autopilot before using it in flight.

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.

Altitude deviation,uncontrolledCruise
Autopilot/flight director - erraticFactor
Maintenance,installation - improperOther maintenance personnelFactor
Aircraft preflight - inadequatePilot in commandFactor
Autopilot - improper use ofPilot in commandFactor
Loss of control - in flightCruise
Airspeed - not maintainedPilot in commandCause
Aircraft control - not maintainedPilot in commandCause
Airframe/component/system failure/malfunctionManeuvering
Flight control,elevator - overload
Design stress limits of aircraft - exceededPilot in commandCause

Analysis

The acft was cruising at 8500 ft when it experienced an inflt loss of control. The plt said the autopilot pitch trim ran away nose down & he was unable to disconnect the autopilot prior to the loss of control. Exam of the acft showed the left elevator horn was bent down & the right elevator horn was broken off. The autopilot was examined & all disconnects except for the accelerometer test functioned properly. The pitch trim board was found improperly installed in the auto pilot & did not make connection. With the altitude hold engaged, the autopilot would hold the elevator position at time of engagement & trim to keep the forces neutral. If the aircraft slowed, it would lose altitude & trim nose up. Radar data showed the acft started to slow, then descended from 8500 to 8300 ft, then climbed to 8900 ft. the acft then came down very rapidly to 1700 ft prior to a recovery. Rprtdly, the plt did not test the autoplt before takeoff. .

Aircraft

Registration
N40978
Reported as
Piper PA-31-350
Category
Airplane
Serial number
31-8152199
Airframe hours
4,131
Engine
Lycoming IO-540-J2B2, 350 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Operator
Falcon Flight Center
Registered owner
Ranger Air Inc
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 25, 1989 · 5 hours before
Departed
HFD · Hartford, CT
Destination
ACY · Atlantic City, NJ

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
26
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
Left
Toxicology
Performed
Flight hours
2,300 total · 300 in this make and model · 2,000 as pilot in command · 120 in the last 90 days · 40 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Visibility
20 statute miles
Lowest ceiling
None

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 N40978 · 1

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