Premium research interface

The modern interface for aviation safety intelligence.

Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.

63k+
Reports indexed
1940-2026
Coverage
Recent
Last data refresh
Featured Report

Loading…

Loading featured report…

Loading…
Open Report

Safety trends by operating rule

Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.

Loading trend charts…

Browse the aviation graph

Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.

Last Data Update

By Decade

By Month

Aircraft Manufacturer

More manufacturers

Airports

More airports

Operators

More operators

About

Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.

The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.

FAQs

NTSB Report

September 27, 1998 · Piper PA-28-140 · N7353J

Iowa City, IA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 27, 1998
Injury Outcomes
2 injuries (2 minor injuries)
Location
Iowa City, IA
Aircraft
Piper PA-28-140
Tail Number
N7353J
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
CHI98LA362

The pilot departed runway 30. He reported that immediately after liftoff, the engine 'seemed to lose a lot of its power.' The residential area offered no open area to do an emergency landing, so he landed the airplane in a small opening between two houses. The airplane fuselage went between two apple trees. The propeller exhibited minimal damage and chordwise scratching on one blade. The engine was run and it developed 2,450 RPM's and the magnetos, carburetor heat, and fuel selector operated normally. The fuel from the wing tanks could not be examined for contamination since the fuel had spilled out of the tanks when wings separated from the fuselage. The pilot reported that just prior to takeoff he had switched the fuel selector to the fullest tank after the engine run up.

NTSB Probable Cause

A loss of engine power for undetermined reasons.

Full Narrative

On September 27, 1998, at 1205 central daylight time, a Piper PA-28-140, N7353J, was substantially damaged during takeoff. The 14 CFR Part 91 flight was departing Iowa City, Iowa, en route to Maquoketa, Iowa. The pilot reported a loss of power during takeoff. The airplane descended into trees and impacted the ground. The private pilot and passenger received minor injuries. Visual meteorological conditions prevailed and no flight plan had been filed. The pilot reported he had conducted his normal preflight and run-up checks. He departed runway 30. He reported that immediately after liftoff, the engine "seemed to lose a lot of its power." He reported that he applied carburetor heat and cycled the throttle to full power, but the engine did not regain power. He reported the residential area offered no open area to do an emergency landing, so he flew the airplane to a small opening between two houses. The airplane fuselage went between two apple trees. The wings were separated from the fuselage by the impact with the apple trees. An Airworthiness Inspector from the Federal Aviation Administration inspected the airplane. The propeller exhibited minimal damage and chordwise scratching on one blade. The engine exhibited continuity to the accessory gearbox. The valve train operated normally and there was thumb compression on all cylinders. The carburetor evidenced no anomalies. The fuel from the wing tanks could not be examined for contamination since the fuel had spilled out of the tanks when wings separated from the fuselage. The inspector reported that no cause of the power loss could be found. The engine run was conducted with the engine still on the airframe. The mechanic who performed the engine run reported the engine made full power at 2,450 RPM. He reported, "... the engine accelerated good. Both magnetos checked OK. Carburetor heat checked OK. I ran the engine with fuel selector on LH tank and that checked OK. I checked fuel selector on RH with air pressure and that checked OK." The pilot reported that he switched the fuel selector to the fullest tank after he accomplished the engine run up prior to takeoff.

Flight

Event TypeAccident
Event Time12:05 CDT
Nearest AirportIowa City Municipal (0nm)
Runway30
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-140
Tail NumberN7353J
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-E2A · Reciprocating · 140
Seats4

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 31 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind320° @ 11 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F
Altimeter30.00 inHg
Observation Time12:05
Weather SourceWFAC

Appendix: Source Data