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NTSB Report

July 29, 1998 · Piper PA-28-140 · N32583

Salem, NJ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 29, 1998
Injury Outcomes
No injuries (2 uninjured)
Location
Salem, NJ
Aircraft
Piper PA-28-140
Tail Number
N32583
Injuries
None
Aircraft Damage
Substantial
NTSB Number
IAD98LA113

The airplane collided with 10 foot tall, dense swamp reeds, 100 feet beyond the departure end of the runway shortly after takeoff. The airplane rotated 180 degrees, struck tail first and ended up inverted in the swamp. According to the pilot, his airspeed during climb out was 'normal' at 70 knots. He said he cleared the end of the 2,300 foot long, grass runway, when a gust of wind (wind shear) caused the airplane to drop about 10 to 15 feet. He said there was no mechanical malfunction with the airplane or the engine.

NTSB Probable Cause

The pilot's failure to maintain adequate altitude/clearance from the reeds. A related factor was the wind gusts.

Full Narrative

On July 29, 1998, at 1252 eastern daylight time, N32583, a Piper PA-28-140, was substantially damaged when it collided with terrain shortly after takeoff from the Salem Airport, Salem, New Jersey. The certificated private pilot and passenger were not injured. Visual meteorological conditions prevailed and a visual flight rules flight plan was filed. The personal flight was conducted under 14 CFR Part 91. The intended destination was Troy, New York. According to the pilot, his airspeed during climb out was "normal" at 70 knots. He said he cleared the end of the 2,300 foot long, grass runway, when a gust of wind (wind shear) caused the airplane to drop about 10 to 15 feet. The airplane struck 10 foot tall, dense swamp reeds, 100 feet beyond the departure end of the runway. He said, "the airplane rotated 180 degrees, struck tail first and ended up inverted in swamp." Due to the inaccessibility of the wreckage, and lack of examination, a Federal Aviation Administration Inspector initially classified it as an incident; however, an aerial examination later revealed that the fuselage was broken in half, and it was then upgraded to an accident on October 5, 1998. According to a Piper PA-28-140 airplane flight manual, the takeoff distance Vs density altitude at a density altitude of 2,000 feet required a ground run of 900 feet. The distance to clear a 50 foot obstacle would be about 2,000 feet. The pilot reported over 1,210 hours of total flight experience. He said that there was no mechanical malfunction with the airplane or the engine. He said the reported winds at the time of the accident were from the southwest at 6 to 10 knots, with gusts to 12 knots.

Flight

Event TypeAccident
Event Time12:52 EDT
Nearest AirportSalem Airport (0nm)
Runway33
Runway Length2200 ft
Runway Width180 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-140
Tail NumberN32583
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-E2D · Reciprocating · 150
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 59 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind280° @ 10 kt
Visibility7 sm
CeilingBroken clouds 5500 ft
Temperature / Dew Point37 C
Altimeter29.00 inHg
Observation Time16:51
Weather SourceWFAC

Appendix: Source Data