Aviation Crash Map

Piper Aerostar 602P N61RG

9 May 2002 · Albuquerque, New Mexico, United States · No injuries

Summary

On 9 May 2002 at about 17:47 local time, a Piper Aerostar 602P registered N61RG was involved in an accident near Albuquerque, New Mexico, United States. 4 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 17:47
Classification
Accident
Location
Albuquerque, New Mexico, United States
Nearest airport
Albuquerque Intl. Sunport (ABQ)
Coordinates
35.0403, -106.6092
Aircraft
Piper Aerostar 602P
Registration
N61RG
Category
Airplane
Engines
2
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Wichita → Albuquerque
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
FTW02LA142

People

Nobody was injured.

On board Died Serious Minor Uninjured
4 0 0 0 4

Probable cause

The pilot's delayed extension of the main landing gear prior to the landing flare/touchdown, which resulted in a wheels-up landing. A contributing factor was the loss of engine power for an undetermined reason.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The airplane was on final approach for runway 3 at about 300-400 feet agl when the left engine lost power. The pilot performed a missed approach due to his inability to keep the airplane aligned with the runway with the loss of engine power and the crosswind conditions. The airplane was losing altitude and the pilot feathered the propeller. Subsequently, the pilot retracted the flaps and the landing gear. By this time, the airplane was at a low altitude, and the pilot delayed performing the landing gear extension procedure. The landing gear did not lock prior to touchdown on the runway, and the airplane landed wheels-up, and slid to a stop. The wind was from 140 degrees at 13 knots with gusts to 17 knots. The reason for the loss of engine power was not determined.

Quoted verbatim from the NTSB record.

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