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

May 30, 1984 · Lockheed L-188 · N5523

Chalkhill, PA

Overview

Report Status
Preliminary report
Event Type
Accident
Date
May 30, 1984
Injury Outcomes
4 injuries (4 fatalities)
Location
Chalkhill, PA
Aircraft
Lockheed L-188
Tail Number
N5523
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
DCA84AA024

After departing the Baltimore-Washington Airport, the aircraft had climbed to FL 220. According to information on the cockpit voice recorder (CVR), the crew experienced gyro problems during the climb. They selected the #1 vertical gyro to drive both approach horizons (attitude indicators), since there was an indication of a malfunction in the #2 vertical gyro system. About 7 minutes after leveling at FL 220, the flight was cleared to the Dryer VOR. Shortly after that, there were indications of confusion in the cockpit which included the statements, "What's happening here," "You got it?" and "No." The aircraft entered a right descending spiral; the indicated airspeed increased from approximately 205 to 317 knots; then an in-flight breakup occurred. The wreckage was found scattered over an area approximately 2 miles long by 1 mile wide. An examination of the wreckage revealed that the in-flight structural failure had occurred due to overload, then a fire ignited in the right wing after it had failed. The aircraft was not equipped with an independent standby attitude indicator.

Full Narrative

AFTER DEPARTING THE BALTIMORE-WASHINGTON ARPT, THE ACFT HAD CLIMBED TO FL 220. ACCORDING TO INFO ON THE COCKPIT VOICE RECORDER (VCR), THE CREW EXPERIENCED GYRO PROBLEMS DURING THE CLIMB. THEY SELECTED THE #1 VERTICAL GYRO TO DRIVE BOTH APPROACH HORIZONS (ATTITUDE INDICATORS), SINCE THERE WAS AN INDICATION OF A MALFUNCTION IN THE #2 VERTICAL GYRO SYS. ABOUT 7 MIN AFTER LEVELING AT FL 220, THE FLT WAS CLEARED TO THE DRYER VOR. SHORTLY AFTER THAT, THERE WERE INDICATIONS OF CONFUSION IN THE COCKPIT WHICH INCLUDED THE STATEMENTS, 'WHAT'S HAPPENING HERE,' 'YOU GOT IT?' & 'NO.' THE ACFT ENTERED A RIGHT DESCENDING SPIRAL; THE INDICATED AIRSPEED INCREASED FROM APRX 205 TO 317 KTS; THEN AN IN-FLT BREAKUP OCCURRED. THE WRECKAGE WAS FOUND SCATTERED OVER AN AREA APRX 2 MI LONG BY 1 MI WIDE. AN EXAM OF THE WRECKAGE REVEALED THAT THE IN-FLT STRUCTURAL FAILURE HAD OCCURRED DUE TO OVERLOAD, THEN A FIRE IGNITED IN THE RIGHT WING AFTER IT HAD FAILED. THE ACFT WAS NOT EQUIPPED WITH AN INDEPENDENT STANDBY ATTITUDE INDICATOR.

Flight

Event TypeAccident
Event Time01:44 EDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledIFR
Aircraft FireIflt
Aircraft ExplosionIflt

Aircraft

AircraftLockheed L-188
Tail NumberN5523
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 121
Engines4
Engine TypeTurboprop
Engine DetailsAllison · 501-D13 · Turboprop · 3750
Seats6

People & Injuries

Injury Summary4 injuries (4 fatalities)
Fatal4
Serious0
Minor0
Uninjured0
Total4
Crew 1Age 37 · First Class

Conditions

ConditionsUnknown
LightDark Night
Wind240° @ 5 kt
Visibility7 sm
CeilingOvercast 3600 ft
Temperature / Dew Point45 C / 43 C
Altimeter30.00 inHg
Observation Time05:58
Weather SourceWFAC

Appendix: Source Data