NYC84MA151

NTSB accident investigation · Piper PA-60-601P · Cockeysville, MD · April 28, 1984

Accident · FatalMajor investigationFinal report
Date
April 28, 1984, 15:07 local (20:07 UTC)
Place
Cockeysville, MD
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N6079RPiper PA-60-601P
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Safety recommendations
Yes
Case key
35781

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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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.

Loss of engine power(total) - nonmechanicalClimb - to cruise
Flight manuals - not followedPilot in commandCause
Fluid,fuel - starvationCause
Fuel boost pump selector position - improperPilot in commandCause
Lack of total experience in type of aircraftPilot in commandFactor
Loss of control - in flightClimb - to cruise
Aircraft performance,two or more engines - inoperativeFactor
Aircraft handling - uncontrolledPilot in commandCause
Spatial disorientationPilot in commandCause
Inadequate recurrent trainingPilot in commandFactor
Airframe/component/system failure/malfunctionDescent - uncontrolled
Flight control,aileron - overloadCause
Design stress limits of aircraft - exceededPilot in commandCause
Flight control,aileron - separation
In flight collision with terrain/waterDescent - uncontrolled

Analysis

On the day of departure the plt had received a 30 min familiarization flt upon completion of the superstar conversion. Emphasis was directed to eng gages, fuel flow & counter, & power settings. The flt was flown at 5,500 ft. the plt then obtained a wx briefing & filed a flt plan. About 15 min after departure, while climbing thru FL 170, the plt radioed that he had lost both engs. The acft was subsequently observed descending uncontrolled out of the overcast. At about 1,000 ft AGL the right aileron separated. The fuel boost pumps were found in the 'off' position. The AFM states that theboost pumps should be on during climb above 10,000 ft. the plt had been enrolled in an Aerostar transition school the previous month during which a 2-HR combined demonstration/flt evaluation flt was conducted. The instructor plt recommended further multi-eng training.

Aircraft

Registration
N6079R
Reported as
Piper PA-60-601P
Category
Airplane
Serial number
0735-8063359
Engine
Lycoming IO-540-S1A5MM, 325 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
G And J Leasing
Airworthiness certificate
Standard, Normal
Departed
Lancaster, PA
Destination
Gainesville, FL
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
58
Certificate
Private
Airplane ratings
Single-engine land, Single-engine sea, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Toxicology
Performed
Flight hours
2,500 total · 105 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
20 statute miles
Lowest ceiling
4,200 ft overcast
Temperature
63 °F, dew point 45 °F
Altimeter
30.00 inHg
Observed at
BWI

Other investigations on N6079R · 1

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