FTW84FA126

NTSB accident investigation · Piper PA-30B · Hugo, OK · February 6, 1984

Accident · FatalField investigationFinal report
Date
February 6, 1984, 12:00 local (17:00 UTC)
Place
Hugo, OK
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N1VEPiper PA-30B
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19840206059289A
Case key
21104

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

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.

Loss of engine power(total) - nonmechanicalTakeoff - initial climb
Procedures/directives - not followedPilot in commandFactor
QualificationPilot in commandFactor
Inadequate trainingPilot in commandFactor
Overconfidence in personal abilityPilot in commandFactor
Maintenance,annual inspection - not performed
Improper use of equipment/aircraftPilot in command
Fluid,fuel - starvationCause
Fuel system - improper use ofPilot in commandCause
Loss of control - in flightTakeoff - initial climb
Gear retraction - not performedPilot in commandFactor
Propeller feathering - not performedPilot in commandFactor
Airspeed(vmc) - not maintainedPilot in commandCause
Aircraft handling - not maintainedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

According to witnesses, the acft was having some kind of problem after takeoff. It entered a nose high attitude, went to the right & crashed. An exam revealed that it had impacted in a nose down attitude. The landing gear was found in a down & locked position. The left prop was twisted & curled, opposite to the direction of rotation & its blades had chordwise scratches from ground impact. The right prop had no signs of rotational damage & it was not feathered. About 40 gals of fuel were found in the left tanks. The right fuel tanks contained virtually no fuel: they were not ruptured. The plt had no multi-engine rating. His logbook had no entries to show dual multi-engine instruction nor compliance with a biennial flt review. The acft was equipped with a robertson stol kit, STC SA-2313-WE, which increased its gross wt to 3800 lbs. The last annual inspection was on 1/10/83.

Aircraft

Registration
N1VE
Reported as
Piper PA-30B
Category
Airplane
Serial number
30-1260
Airframe hours
2,623
Engine
Lycoming IO-320-C1A, 160 horsepower, reciprocating
Damage
Destroyed
Flight
Business · Part 91
Registered owner
James R. Lee
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 10, 1983 · 86 hours before
Departed
F53 · Hugo, OK
Destination
ADH · Ada, OK

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
40
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
2,581 total

Weather

Conditions
Visual (VMC) · Day
Wind
185° at 5 knots
Visibility
10 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 N1VE · 1

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