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

February 21, 1990 · Piper PA-31-350 · N3554P

Greeley, CO

Overview

Report Status
Probable Cause
Event Type
Accident
Date
February 21, 1990
Injury Outcomes
2 injuries (2 serious injuries)
Location
Greeley, CO
Aircraft
Piper PA-31-350
Tail Number
N3554P
Operator
Beegles Aircraft Services
Injuries
Serious
Aircraft Damage
Destroyed
NTSB Number
DEN90FA066

N3554P WAS ON A MAINTENANCE TEST FLIGHT AFTER THE RIGHT WING WAS REPAIRED. THE PILOT LOST CONTROL OF THE AIRPLANE SHORTLY AFTER LIFTOFF AND WAS UNABLE TO REGAIN CONTROL PRIOR TO THE GROUND IMPACT. THE A&P MECHANIC WHO PERFORMED THE REPAIRS, RE ASSEMBLED THE RIGHT WING AILERON CONTROL CABLES PER THE PIPER SERVICE MANUAL. POST ACCIDENT EXAMINATION OF THE AILERON CONTROL SYSTEM REVEALED THE RIGHT WING CONTROL CABLES WERE REVERSED ON THE AILERON BELLCRANK, RESULTING IN BOTH AILERONS MOVING THE SAME DIRECTION (EITHER UP OR DOWN) WHEN THE CONTROL WHEEL WAS TURNED LEFT OR RIGHT.

NTSB Probable Cause

THE IMPROPER IDENTIFICATION OF PARTS IN THE PIPER PA-31-350 SERVICE MANUAL PERTAINING TO THE AILERON CABLES. THIS DISCREPANCY RESULTED IN THE IMPROPER INSTALLATION OF THE AILERON CABLES ON THE RIGHT AILERON BELLCRANK BY A MECHANIC DURING THE RECONSTRUCTION OF THE RIGHT WING. THE IMPROPER CONNECTION RESULTED IN A LOSS OF AIRCRAFT CONTROL BY THE PILOT IMMEDIATELY AFTER TAKEOFF. ALSO CAUSAL TO THE ACCIDENT WERE THE INADEQUATE INSPECTION OF THE FLIGHT CONTROL SYSTEM BY A SECOND MECHANIC WITH INSPECTION AUTHORIZATION, AND THE INADEQUATE PREFLIGHT INSPECTION OF THE FLIGHT CONTROL SYSTEM BY THE PILOT PRIOR TO TAKEOFF.

Full Narrative

N3554P WAS ON A MAINTENANCE TEST FLIGHT AFTER THE RIGHT WING WAS REPAIRED. THE PILOT LOST CONTROL OF THE AIRPLANE SHORTLY AFTER LIFTOFF AND WAS UNABLE TO REGAIN CONTROL PRIOR TO THE GROUND IMPACT. THE A&P MECHANIC WHO PERFORMED THE REPAIRS, RE ASSEMBLED THE RIGHT WING AILERON CONTROL CABLES PER THE PIPER SERVICE MANUAL. POST ACCIDENT EXAMINATION OF THE AILERON CONTROL SYSTEM REVEALED THE RIGHT WING CONTROL CABLES WERE REVERSED ON THE AILERON BELLCRANK, RESULTING IN BOTH AILERONS MOVING THE SAME DIRECTION (EITHER UP OR DOWN) WHEN THE CONTROL WHEEL WAS TURNED LEFT OR RIGHT.

Flight

Event TypeAccident
Event Time08:15 MST
Nearest AirportGreeley/Weld Cty (0nm N)
Runway27
Runway Length6210 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionGrd

Aircraft

AircraftPiper PA-31-350
Tail NumberN3554P
Aircraft CategoryAir
DamageDestroyed
OperatorBeegles Aircraft Services
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsLycoming · TIO-540-J28D · Reciprocating · 350
Seats10

People & Injuries

Injury Summary2 injuries (2 serious injuries)
Fatal0
Serious2
Minor0
Uninjured0
Total2
Crew 1Age 53 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind350° @ 15 kt
Visibility15 sm
CeilingOvercast 5000 ft
Temperature / Dew Point32 C / 0 C
Altimeter0
Weather SourceWIT

Appendix: Source Data