DEN89FA155

NTSB accident investigation · Piper PA-16 · Minot, ND · July 5, 1989

Accident · Serious injuriesField investigationFinal report
Date
July 4, 1989, 21:01 local (Jul 5, 1989, 02:01 UTC)
Place
Minot, ND
Injuries
1 serious, 1 minor
Damage
Destroyed
Phase of flight
Approach
Aircraft
N5295HPiper PA-16
Weather
Visual (VMC) · Day
Status
Completed · report June 18, 1990
Report
Approved by Office Director
FAA report
19890704025519A
Case key
17596

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 airframe tubing (longeron) at the lower forward door frame due to corrosion. A contributing factor was failure of maintenance personnel to comply with service bulletin #819.

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/malfunctionApproach - vfr pattern - final approach
Fuselage,longeron - corrodedCause
Maintenance,service bulletin/letter - not followedOther maintenance personnelFactor
Fuselage,longeron - failure,totalCause
Aircraft control - not possible
Loss of control - in flightApproach - vfr pattern - final approach
In flight collision with terrain/waterDescent - uncontrolled

Analysis

As the plt turned on final apch to lnd, he heard a 'thud,' then the acft entered an uncontrolled left turn. After turning about 360 deg, it impacted the ground in a left wing low, nose low attitude. An investigation revealed a failureof the airframe tubing at the lower forward door frame. The failure was in the area of a conglomerate weld where the tubing was part of the door frame, fire wall/engine mount, & right forward lift strut support. An exam revealed the tubing had separated prior to impact. Aprx 3/4 of the fracture was the result of corrosion; the remaining fracture was from overload, but not due to impact. With this failure, the leading edge of the right wing would twist upward & the engine (with power) would move up & to the left. Piper service bulleting #819, subject: fuselage door frame tube corrosion, dated 2/28/86, addressed the hazard of corrosion in this area.

Aircraft

Registration
N5295H
Reported as
Piper PA-16
Category
Airplane
Serial number
16-99
Airframe hours
2,262
Engine
Lycoming O-235-C1, 108 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
William F. Martin
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 4, 1989 · 64 hours before
Departed
S25 · Watford City, ND
Destination
MOT
Airport
MOT · Minot Intl, runway 13, 7,493 × 150 ft, asphalt

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
53
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
2,600 total · 10 in this make and model · 1,520 as pilot in command · 34 in the last 90 days · 12 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 7 knots
Visibility
30 statute miles
Lowest ceiling
9,000 ft broken
Temperature
90 °F, dew point 63 °F
Altimeter
29.00 inHg
Observed at
MDT, 3 nm away

FAA reports on this event · 1

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