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Airborne Express Douglas DC8-62 incident

30 Dec 1996 · Orlando, FL, United States

Douglas DC8-62 · Incident: loss of control on ground/water during takeoff

From Orlando International Airport (MCO) to Wilmington Airpark (ILN)

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Event

NTSB case
MIA97IA050
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Incident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
Airline
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Douglas DC8-62

Aircraft type
Douglas DC8
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N804AX
Onboard fatalities
Unknown
Route
From Orlando International Airport (MCO)To Wilmington Airpark (ILN), Wilmington, OH
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 121: Air Carrier
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Takeoff · roll/run
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of control on ground/water
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Minor

Cause areas

  • Pilot in command › Nosewheel steering, improper use of
  • Pilot in command › Throttle/power control, improper use of

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

As the first officer began the takeoff roll the aircraft began to drift to the left. Attempts to correct the drift by application of full right nose wheel steering through the rudder pedals was unsuccessful. The captain took control of the aircraft and aborted the takeoff. As engine power was reduced the aircraft turned sharply to the right and went off the right side of the runway where it came to rest on soft terrain. The aircraft center of gravity was near the aft limit. After the incident the nose landing gear was found to be over serviced and extended 2.35 inches higher than normal. DFDR data showed that as engine power was added for takeoff the nose of the aircraft pitched up extending the nose gear further. This allowed the centering cam to restrict nose gear steering to +/- 4 degrees. As the captain aborted the takeoff the nose pitched down and normal nose steering returned at which time the aircraft responded to the full right rudder input. DFDR and CVR data also show that as the captain aborted the takeoff he did not fully close throttles 1 and 2 and the asymmetric thrust contributed to the uncontrolled right turn.

Probable cause

The failure of the captain to center the rudder and close all engine throttles during an aborted takeoff resulting in an uncontrolled turn to the right due to nose wheel steering through the rudder pedals and asymmetric engine thrust. A factor in the incident was failure of operator maintenance personnel to properly service the nose landing gear strut resulting in an over extended strut and the flight crews loss of directional control to the left during takeoff requiring them to abort the takeoff.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record MIA97IA050
Event ID
20001208X07207
Case number
MIA97IA050
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (5)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: local date, investigation status. Values present in the bulk record are kept.
  • The date is the local date; the NTSB stores the UTC date 1996-12-31.
  • API snapshot SHA-256: a478fb24f78aab9b46cae9bc77c9bdc8fdf253e62c1af33986c36f4aeacafb66; retrieved 2026-09-18T17:43:42.523Z.
  • The NTSB's operator name is blank for N804AX; the operator shown is the name the NTSB records it doing business as.