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MIA07IA080 · Beech E-55

31 Mar 2007 · Key West, FL, United States

Beech E-55 · Incident: nose gear collapsed during landing

From Sarasota Bradenton International Airport (SRQ) to Key West International Airport (EYW)

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Event

NTSB case
MIA07IA080
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
Unknown
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
General aviation
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

Beech E-55

Aircraft type
Beechcraft E-55
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
N25612
Operator
Unknown
Onboard fatalities
Unknown
Route
From Sarasota Bradenton International Airport (SRQ), Sarasota, FLTo Key West International Airport (EYW), Key West, FL
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 91: General Aviation
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
Landing · landing roll
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
Nose gear collapsed
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

  • Reason for occurrence undetermined

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The pilot stated that when he extended the landing gear on final approach he received a green gear down light. During landing rollout the nose landing gear collapsed. Examination of the airplane after the incident by a Federal Aviation Administration (FAA) inspectors showed the nose landing gear torque link had failed, causing the nose landing gear to collapse. Metallurgical examination of the nose landing gear drag brace was performed at the National Transportation Safety Board Materials Laboratory. The examination showed the drag brace had fractured in the tubing; at a point just forward of the right attach point. The fracture faces displayed surfaces that were inclined at approximately 45-degrees to the axis of the separated portion of the tubing, consistent with an overload event. The incident airplane was manufactured in January 1973. A representative from Hawker-Beechcraft stated that beginning in model year 1978, an improved nose landing gear drag brace was incorporated into new production airplanes. Beech also issued service kit 35-4012-1 S, which allowed for upgrade of earlier model E-55 airplanes with the improved nose landing gear drag brace. The representative stated that pictures of the failed drag brace from the accident airplane shows it was not the improved drag brace. Maintenance personnel for the incident airplane owner stated that a review of airplane logbook records show no evidence that the drag brace had been changed in the life of the airplane and that the failed drag brace appeared to be the original supplied with the airplane from the factory.

Probable cause

Failure of the nose landing gear drag brace due to overload during landing rollout for undetermined reasons. Contributing to the accident was the airplane had not been modified with an improved nose landing gear drag brace.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record MIA07IA080
Event ID
20070420X00443
Case number
MIA07IA080
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • 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: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: f5df5db10ba3cff64942d0f294fd749b83e3c9a65ef3e55ef8bf00b16b4ac9bc; retrieved 2026-09-22T03:56:26.102Z.