# Accident 20051125027719A: Cessna 195A, Heber, UT, November 25, 2005

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: November 25, 2005, 12:10 local time
- Place: Heber, UT
- Airport: Heber Valley Airport
- Damage: Substantial damage
- Phase of flight: Roll-Out (Fixed Wing)
- Operating rules: General operating rules (Part 91)
- Location: 40.4819° N, 111.4289° W: From the FAA
- Nearby events: https://openairdocs.org/map.md?lat=40.4819&lon=-111.4289&mi=10
- Aircraft: N1528D, registered now (https://openairdocs.org/aircraft/N1528D) (OpenAirDocs)
- Registry model: Cessna 195A (registry code 2073110, https://openairdocs.org/model/cessna-195a) (OpenAirDocs)
- Registry engine: Jacobs L4 /R755-7 (registry code 35003, https://openairdocs.org/engine/jacobs-l4-r755-7) (OpenAirDocs)
- Reported make and model: CESSNA 195A
- Reported engine: JACOBS R7557
- People aboard: 2
- Fatal injuries: 0
- Pilot flight hours: 2,164 total, 116 in this make and model, 10 in the last 90 days
- NTSB investigation: [NTSB SEA06CA020](https://openairdocs.org/ntsb/SEA06CA020) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20051125027719A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) 32. AFTER DISASSEMBLY OF THE BRAKE CYLINDER THERE MAY BE A DETERMINATION OF THE PART AND CAUSE OF THE FAILURE. AT THAT TIME AN AMENDMENT WILL BE SUBMITTED WITH A RECOMMENDATION AS TO AN APPROPRIATE CORRECTIVE ACTION. AT THE CONCLUSION OF A RELATIVELY SHORT LOCAL FLIGHT CONDUCTED IN ACCORDANCE WITH TITLE 14 CODE OF FEDERAL REGULATIONS PART 91, THE PILOT MADE A LANDING TO RUNWAY 21 AT 36U (HEBER CITY, UT). DURING THE ROLLOUT THE PILOT APPLIED APPROXIMATELY EQUAL PRESSURE TO BOTH MAIN BRAKES. AT ABOUT 40 KTS THE RIGHT BRAKE COMPLETELY FAILED. WITH PRESSURE ON THE LEFT THE AIRCRAFT MADE AN ABRUPT SWERVE TO THE LEFT, BECAME UNCONTROLLABLE, WENT SOMEWHAT SIDEWISE TO THE RIGHT, THE RIGHT WING WENT DOWN AND STRUCK THE RUNWAY. THE AIRCRAFT CAME TO REST WITH THE LEFT WING IN THE AIR. SEVERAL FEET OF THE OUTBOARD PORTION OF THE RIGHT WING WAS SUBSTANTIALLY DAMAGED AND BENT UP AT APPROXIMATELY A 45 DEGREE ANGLE. THE RIGHT MAIN GEAR STRUT WAS BENT INBOARD TO SOME DEGREE. THERE WAS NO FINDING OF PILOT INCOMPETENCE OR MAINTENANCE IRREGULARITY.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA06CA020](https://openairdocs.org/ntsb/SEA06CA020), Nov 25, 2005: Cessna 195A (N1528D), Heber City, UT, substantial damage. Probable cause: The failure of the right brake, which resulted in a loss of directional control during the landing roll and a nose down.

## Other reports on N1528D (1)

Matched to the same aircraft by N-number and date.

- [Accident 19730719022279A](https://openairdocs.org/incident/19730719022279A), Jul 19, 1973: Cessna 195A (N1528D), Heart Butte, MT, Substantial damage. 3300FT strip,apch end rough. Lndd past midfield,ran off end.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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