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Accidents · NTSB FTW90LA025 · Final report

Beech 95 accident near Floydada, Texas, November 11, 1989

On November 11, 1989, a Beech 95, registered N17AT, was substantially damaged in an accident near Floydada, Texas (Floydada Municipal airport). It was an instructional flight under general aviation rules (Part 91). No one was hurt; 4 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

FAILURE OF THE PROPELLER ATTACHMENT BOLTS DUE TO FATIGUE IN FOUR OF THE BOLTS AND OVERLOAD IN ANOTHER. A CONTRIBUTING FACTOR WAS THE LOSS OF ELECTRICAL POWER AND THE DETERIORATED AIRPLANE CONTROL/PREFORMANCE.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
November 11, 1989
Place
Floydada, Texas · Floydada Municipal · map
Type
Accident
Injuries
No one was hurt; 4 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Beech 95 · all 95s on the register
Registration
N17AT · no longer on the register · serial TD107
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

WHILE THE AIRPLANE WAS AT CRUISE, THE RIGHT PROPELLER SPINNER FELL OFF. THREE OR FOUR MINUTES LATER, THE RIGHT PROPELLER CAME OFF AND CUT INTO THE NOSE OF THE AIRPLANE. WITH NO ELECTRICAL POWER, AND DETERIORATED AIRPLANE CONTROL, THE PILOT MADE A WHEELS-UP LANDING ON THE DESTINATION AIRPORT. THE RIGHT PROPELLER AND THE CENTER OF THE STARTER RING WERE NOT RECOVERED. FIVE OF THE PROPELLER ATTACHMENT BOLTS REMAINED IN THE ENGINE CRANKSHAFT FLANGE. LABORATORY VISUAL INSPECTION INDICATED FOUR OF THESE BOLTS FAILED FROM FATIGUE AND THE FIFTH FAILED FROM OVERLOAD.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
  • Flight time: 1,120 hours in all; 200 in this make and model; 345 in the last 90 days; 140 in the last 30 days; 995 as pilot in command; 550 on instruments
  • Medical certificate: Class 2 (valid medical--no waivers/lim.)
  • Seat: left

The aircraft

  • Last inspection: annual inspection, November 7, 1989
  • Maximum gross weight: 4,100 lb
  • Seats: 4
  • Landing gear: retractable
  • Engine: Lycoming O-360-A1A (piston); 0 hours total
  • Operator: B & H Aviation

The flight

  • Departed from: F67 Grand Prairie TX at 10:45 pm
  • Destination: Q41
  • Flight plan: none
  • Runway 17, 3,700 ft by 50 ft

Weather at the time

  • Light: night, bright
  • Wind: from 170° at 7 knots
  • Visibility: 15 statute miles
  • Sky: clear
  • Temperature: 61°F (16°C), dew point 16°F (-9°C)
  • Altimeter: 30.00 inHg

Injuries

FatalSeriousMinorNone
Crew2
Passengers2

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Other NTSB records under N17AT the same tail number, which may have belonged to a different aircraft at the time

1986-04-08MIA86LA116 · accident near Hollywood, FL · substantial damage · no injuries

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.