Twin Falls - Truckee - Carlsbad - Monterrey

The airplane collided with the ground during a low altitude, steep banked, base-to-final left turn toward the landing runway during a circling instrument approach. The airplane impacted terrain 1/3-mile from the approach end of runway 28, and north of its extended centerline. A witness, located in the airport's administration building, made the following statement regarding his observations: "I saw the aircraft in and out of the clouds in a close base for [runway] 28. I then saw the aircraft emerge from a cloud in a base to final turn [and] it appeared to be approximately 300-400 feet above the ground. The left wing was down nearly 90 degrees. The aircraft appeared north of the [runway 28] centerline. The aircraft pitched nose down approximately 30-40 degrees and appeared to do a 1/2 cartwheel on the ground before exploding." ATC controllers had cleared the airplane to perform a GPS-A (circling) approach. The published weather minimums for category C and D airplanes at the 5,900-foot mean sea level airport was 3 miles visibility, and the minimum descent altitude was 8,200 feet mean sea level (msl). Airport weather observers noted that when the accident occurred, the visibility was between 1 1/2 and 5 miles. Scattered clouds existed at 1,200 feet above ground level (7,100 feet msl), a broken ceiling existed at 1,500 feet agl (7,400 feet msl) and an overcast condition existed at 2,400 feet agl (8,300 feet msl). During the approach, the first officer acknowledged to the controller that he had received the airport's weather. The airplane overflew the airport in a southerly direction, turned east, and entered a left downwind pattern toward runway 28. A 20- to 30-knot gusty surface wind existed from 220 degrees, and the pilot inadequately compensated for the wind during his base leg-to-final approach turning maneuver. The airplane was equipped with Digital Electronic Engine Controls (DEEC) that recorded specific data bits relating to, for example, engine speed, power lever position and time. During the last 4 seconds of recorded data (flight), both of the power levers were positioned from a mid range point to apply takeoff power, and the engines responded accordingly. No evidence was found of any preimpact mechanical malfunction. The operator's flight training program emphasized that during approaches consideration of wind drift is essential, and a circling approach should not be attempted in marginal conditions.

Flight / Schedule

Twin Falls - Truckee - Carlsbad - Monterrey

Aircraft

Learjet 35

Registration

N781RS

MSN

35-218

Year of Manufacture

1978

Date

December 28, 2005 at 02:06 PM

Type

CRASH

Flight Type

Positioning

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Truckee California

Region

North America • United States of America

Coordinates

39.3275°, -120.1858°

Crash Cause

Human factor

Narrative Report

On December 28, 2005 at 02:06 PM, Twin Falls - Truckee - Carlsbad - Monterrey experienced a crash involving Learjet 35, operated by Skyward Aviation - USA, with the event recorded near Truckee California.

The flight was categorized as positioning and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

2 people were known to be on board, 2 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.

Crew on board: 2, crew fatalities: 2, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. The airplane collided with the ground during a low altitude, steep banked, base-to-final left turn toward the landing runway during a circling instrument approach. The airplane impacted terrain 1/3-mile from the approach end of runway 28, and north of its extended centerline. A witness, located in the airport's administration building, made the following statement regarding his observations: "I saw the aircraft in and out of the clouds in a close base for [runway] 28. I then saw the aircraft emerge from a cloud in a base to final turn [and] it appeared to be approximately 300-400 feet above the ground. The left wing was down nearly 90 degrees. The aircraft appeared north of the [runway 28] centerline. The aircraft pitched nose down approximately 30-40 degrees and appeared to do a 1/2 cartwheel on the ground before exploding." ATC controllers had cleared the airplane to perform a GPS-A (circling) approach. The published weather minimums for category C and D airplanes at the 5,900-foot mean sea level airport was 3 miles visibility, and the minimum descent altitude was 8,200 feet mean sea level (msl). Airport weather observers noted that when the accident occurred, the visibility was between 1 1/2 and 5 miles. Scattered clouds existed at 1,200 feet above ground level (7,100 feet msl), a broken ceiling existed at 1,500 feet agl (7,400 feet msl) and an overcast condition existed at 2,400 feet agl (8,300 feet msl). During the approach, the first officer acknowledged to the controller that he had received the airport's weather. The airplane overflew the airport in a southerly direction, turned east, and entered a left downwind pattern toward runway 28. A 20- to 30-knot gusty surface wind existed from 220 degrees, and the pilot inadequately compensated for the wind during his base leg-to-final approach turning maneuver. The airplane was equipped with Digital Electronic Engine Controls (DEEC) that recorded specific data bits relating to, for example, engine speed, power lever position and time. During the last 4 seconds of recorded data (flight), both of the power levers were positioned from a mid range point to apply takeoff power, and the engines responded accordingly. No evidence was found of any preimpact mechanical malfunction. The operator's flight training program emphasized that during approaches consideration of wind drift is essential, and a circling approach should not be attempted in marginal conditions.

Aircraft reference details include registration N781RS, MSN 35-218, year of manufacture 1978.

Geospatial coordinates for this crash are approximately 39.3275°, -120.1858°.

Fatalities

Total

2

Crew

2

Passengers

0

Other

0

Crash Summary

The airplane collided with the ground during a low altitude, steep banked, base-to-final left turn toward the landing runway during a circling instrument approach. The airplane impacted terrain 1/3-mile from the approach end of runway 28, and north of its extended centerline. A witness, located in the airport's administration building, made the following statement regarding his observations: "I saw the aircraft in and out of the clouds in a close base for [runway] 28. I then saw the aircraft emerge from a cloud in a base to final turn [and] it appeared to be approximately 300-400 feet above the ground. The left wing was down nearly 90 degrees. The aircraft appeared north of the [runway 28] centerline. The aircraft pitched nose down approximately 30-40 degrees and appeared to do a 1/2 cartwheel on the ground before exploding." ATC controllers had cleared the airplane to perform a GPS-A (circling) approach. The published weather minimums for category C and D airplanes at the 5,900-foot mean sea level airport was 3 miles visibility, and the minimum descent altitude was 8,200 feet mean sea level (msl). Airport weather observers noted that when the accident occurred, the visibility was between 1 1/2 and 5 miles. Scattered clouds existed at 1,200 feet above ground level (7,100 feet msl), a broken ceiling existed at 1,500 feet agl (7,400 feet msl) and an overcast condition existed at 2,400 feet agl (8,300 feet msl). During the approach, the first officer acknowledged to the controller that he had received the airport's weather. The airplane overflew the airport in a southerly direction, turned east, and entered a left downwind pattern toward runway 28. A 20- to 30-knot gusty surface wind existed from 220 degrees, and the pilot inadequately compensated for the wind during his base leg-to-final approach turning maneuver. The airplane was equipped with Digital Electronic Engine Controls (DEEC) that recorded specific data bits relating to, for example, engine speed, power lever position and time. During the last 4 seconds of recorded data (flight), both of the power levers were positioned from a mid range point to apply takeoff power, and the engines responded accordingly. No evidence was found of any preimpact mechanical malfunction. The operator's flight training program emphasized that during approaches consideration of wind drift is essential, and a circling approach should not be attempted in marginal conditions.

Cause: Human factor

Occupants & Outcome

Crew On Board

2

Passengers On Board

0

Estimated Survivors

0

Fatality Rate

100.0%

Known people on board: 2

Operational Details

Schedule / Flight

Twin Falls - Truckee - Carlsbad - Monterrey

Flight Type

Positioning

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Aircraft

Learjet 35

Registration

N781RS

MSN

35-218

Year of Manufacture

1978