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DEN04LA082 · Lockheed TV-2

28 May 2004 · Calhan, CO, United States

Lockheed TV-2 · Accident: airframe, component or system failure during an emergency descent

From Salina Municipal Airport (SLN) to Centennial Airport (APA)

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Event

NTSB case
DEN04LA082
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
Accident
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

Lockheed TV-2

Aircraft type
Lockheed TV-2
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
N6617
Operator
Unknown
Onboard fatalities
Unknown
Route
From Salina Municipal Airport (SLN), Salina, KSTo Centennial Airport (APA), Denver, CO
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
Emergency descent
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
Airframe, component or system failure
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

No findings designated as a cause are recorded in the NTSB data yet.

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

NTSB narrative

According to the pilot, at approximately 45 nautical miles southeast of his intended destination, the wing tip tank low fuel light illuminated. He stated that this was planned, and he selected the 150-gallon wing tank. Approximately two minutes later, the low fuel light illuminated for the wing tank. A "drop," in the fuel quantity indication on the main fuselage tank gauge, confirmed the wing tanks low fuel condition. He then selected the 100-gallon leading edge tank, and within a few minutes, its low fuel light illuminated as well. Again, he noted a "drop" in the fuel quantity indication on the main fuselage tank gauge, confirming the leading edge tanks low fuel condition. The pilot immediately contacted the local Air Route Traffic Control Center (ARTCC), reported a "fuel emergency," and stated that he was going to make a precautionary landing at a nearby dirt strip. Upon landing, he retracted the flaps and applied full brakes; however, the airplane departed the end of the runway, struck a ditch, and slid approximately 400 feet, coming to a stop in an open field. The impact with the ditch collapsed and separated both main landing gear assemblies from the wing spar. The airplane sustained substantial damage to both wing spars and the lower aft fuselage. According to the pilot, the airplane departed with approximately 700 gallons of fuel. Prior to evacuating the airplane, he noted that the main fuselage tank gauge indicated approximately 68 gallons of fuel. During an examination of the wreckage, approximately 56 gallons of fuel was recovered. According to a maintenance representative, no aircraft anomalies were noted. However, a stuck fuel tank float valve would allow fuel to "drain out of the saber vents at approximately 30 gallons per minute." The representative also stated that, the calculated fuel loss, from the moment the fuel pumps were turned on to the moment the tanks indicated empty, correlated to the amount of unaccountable fuel.

Probable cause

the failure of the fuel tank float which resulted in the draining of fuel out the vents, and a low fuel supply. Contributing factors include the insufficient runway length, the ditch, and the rough, uneven terrain.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record DEN04LA082
Event ID
20040616X00804
Case number
DEN04LA082
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: local date, investigation status. Values present in the bulk record are kept.
  • The date is the local date; the NTSB stores the UTC date 2004-05-29.
  • API snapshot SHA-256: e0f9a02107fe0f902bfc7a9155100b10a725383a9e8996e5350b6938660da690; retrieved 2026-09-22T07:26:51.612Z.