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Accidents · NTSB LAX03FA072 · Final report

Cirrus Design Corp. SR 20 accident near San Jose, California, January 24, 2003

On January 24, 2003, a Cirrus Design Corp. SR 20, registered N893MK, was destroyed in an accident near San Jose, California (Reid-Hillview Of Santa Clara C airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

The pilot's failure to maintain the course for the published approach procedure due to his diverted attention. The distraction responsible for the pilot's diverted attention was the erroneous frequency assignment provided by ATC and the resultant task overload induced by this problem and the confusion surrounding the ATC clearances to get established on the final approach course, which likely involved repeated reprogramming of the navigation system. Factors in the accident include the failure of ATC to provide the pilot with a timely and effective safety alert concerning the deviation from the proper course, which was influenced in part by the features of the radar display at both facilities which made the deviation more difficult to detect, and the nature of radar as a secondary tool for a VFR tower controller. An additional factor was the nonstandard method of providing approach clearance, which likely may have exacerbated pilot task overload.

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

What the record shows

Date
January 24, 2003
Place
San Jose, California · Reid-Hillview Of Santa Clara C · map
Type
Accident
Injuries
1 person was killed.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Cirrus Design Corp. SR 20
Registration
N893MK · no longer on the register · serial 1038
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The airplane collided with high-tension power lines in a mountainous area after deviating from the GPS approach procedure in instrument conditions. The airplane was equipped with a GPS navigation system incorporating a moving map feature. During the initial portions of the flight after departure, the TRACON sector controller working the flight initially believed the airplane was destined to another airport and issued a clearance accordingly, but corrected the clearance after the pilot questioned the controller. Shortly after this discussion, the pilot significantly deviated from his cleared course for unknown reasons in the general direction of the mistaken airport. The controller noticed the deviation and corrected the pilot's course. A second controller in the next sector the airplane would be worked by overheard the course correction, and inferred the pilot was somewhat confused. After handoff by the first controller, the second sector controller attempted to provide what he believed was a helpful method of handling the airplane in the transition to the GPS approach; however, these methods of clearing the pilot for the GPS approach were not in strict accordance with FAA Order 7110.65, and included an intercept angle with the final approach course that was greater than allowed. The airplane was on a modified downwind and proceeding to the initial approach fix (IAF) when the controller cleared the pilot to turn toward an intermediate fix between the IAF and the final approach fix (FAF) with the idea in mind that this course would be the same as a radar vector to the FAF. The pilot questioned the clearance, and then acknowledged it, and the airplane turned left toward the FAF, which was directly behind the airplane. The controller noticed that the left turn put the airplane heading toward high terrain and advised the pilot to turn right to go to the intermediate fix. After some additional confusion the airplane's track stabilized on the approach course after passing the intermediate fix. As the airplane passed the FAF the controller told the pilot to contact the tower, but gave him the frequency for the wrong airport. The pilot questioned the controller, who insisted the frequency was correct. The pilot then contacted the second airport tower and was told he was on the wrong frequency. Almost 1 minute elapsed between the pilot's acknowledgement of the erroneous frequency, and his initial contact to the correct tower. During this period the airplane's heading diverged approximately 90 degrees from the published final approach course toward rising terrain and the accident site. The Minimum Safe Altitude Warning alarms went off in the TRACON and in the tower, and the tower controller provided a low altitude safety alert based on the alarm by saying "check your altitude immediately;" however, at the time of the low altitude alert, the airplane was about 500 feet above the Minimum Descent Altitude (the accident site elevation was about 200 feet above the MDA.) and the alert was activated not because the airplane's altitude was below the segment minimums but due to the course and altitude being projected to come in contact with terrain in the near future. This may have confused the pilot and decreased the perceived urgency. The limitations of the radar display effectively masked the initial portions of the course deviation and the controller did not see the deviation for some 30 seconds; however, the controller did advise the pilot that he was off course as soon as he was aware of it. The pilot's unintelligible response was about the time the radar target return went into coast mode.

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: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 461 hours in all; 334 in this make and model; 84 in the last 90 days; 31 in the last 30 days; 98 as pilot in command
  • Last flight review: January 6, 2003
  • Medical certificate: Class 3 (valid medical--w/ waivers/lim.)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 369.3 hours
  • Last inspection: annual inspection, February 20, 2002; 301.5 hours since
  • Maximum gross weight: 3,000 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Teledyne Continental IO-360-ES 6B (piston); 0 hours total

The flight

  • Departed from: KAPC Napa CA
  • Destination: KRHV San Jose CA
  • Flight plan: IFR
  • Runway 31R, 3,101 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 280° at 12 knots
  • Visibility: 4 statute miles
  • Sky: overcast at 8,000 ft
  • Temperature: 61°F (16°C), dew point 59°F (15°C)
  • Altimeter: 30.23 inHg

Injuries

FatalSeriousMinorNone
Crew1

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.

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.