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

August 14, 1994 · Rockwell 112A · N1315J

Eagle Lake, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 14, 1994
Injury Outcomes
2 injuries (2 minor injuries), 2 uninjured
Location
Eagle Lake, TX
Aircraft
Rockwell 112A
Tail Number
N1315J
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
FTW94LA269

EN ROUTE AT 3,500 FEET MSL, A TOTAL LOSS OF ENGINE POWER OCCURRED. THE PILOT ATTEMPTED AN ENGINE RESTART WITHOUT SUCCESS. DURING THE FORCED LANDING IN ROUGH AND UNEVEN TERRAIN, THE NOSE GEAR HIT A DIKE. THREE AND ONE GALLONS OF FUEL FROM THE RIGHT TANK AND 5 AND 1/2 GALLONS OF FUEL FROM THE LEFT TANK WAS MEASURED BY THE PILOT DURING THE AIRPLANE RECOVERY. THE PILOT ALSO REPORTED FUEL IN THE INJECTOR LINES.

NTSB Probable Cause

LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.

Full Narrative

On August 13, 1994, at 1920 central daylight time, a Rockwell International 112A, N1315J, was substantially damaged during a forced landing near Eagle Lake, Texas. The private pilot and one passenger were not injured. Two passengers received minor injuries. Visual meteorological conditions prevailed for the personal cross country flight. A review of Air Traffic Control data revealed the following information. At an altitude of 5,500 feet MSL en route at 50 miles from Eagle Lake VOR, the pilot contacted Houston Center for flight following to Clover Field, Houston, Texas. He was given an altimeter setting of 30.00 but radar contact was not established. The airplane descended to 4,000 feet MSL due to haze. The pilot was advised to contact Houston Approach for flight following. During a telephone interview, the pilot stated the following information. At 3,500 feet MSL a total loss of engine power occurred and the attempted restart was unsuccessful. The airplane was not in gliding distance of the Eagle Lake Airport. A rice field was selected for the forced landing. During the landing roll, the nose gear hit a dike. The pilot further stated that the firewall, engine mounts, and fuselage were damaged. Usable fuel during the recovery of the airplane was measured by the pilot as 3 and 1/2 gallons from the right fuel tank and 5 and 1/2 gallons from the left fuel tank. He also said fuel was found in the injector lines.

Flight

Event TypeAccident
Event Time19:20 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRockwell 112A
Tail NumberN1315J
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-360-C1D6 · Reciprocating · 200
Seats4

People & Injuries

Injury Summary2 injuries (2 minor injuries), 2 uninjured
Fatal0
Serious0
Minor2
Uninjured2
Total4
Crew 1Age 41 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind150° @ 6 kt
Visibility8 sm
CeilingNone
Altimeter30.00 inHg
Observation Time00:47
Weather SourceWFAC

Appendix: Source Data