No fatalities

Cessna 402C Landing Gear Collapse at Albuquerque International Sunport (N5802C)

Albuquerque, NM, United States

On February 3, 2011, a CESSNA 402 C (registration N5802C) operated by South Aero Inc was involved in an aviation accident near Albuquerque, NM. No fatalities were reported. Investigators recorded the probable cause as: The failure of the landing gear system for undetermined reasons. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

A Cessna 402C sustained substantial damage during landing at Albuquerque International Sunport after the right main landing gear collapsed due to a hydraulic malfunction. The pilot was not injured.

Incident Overview

On February 3, 2011, at 0840 mountain standard time, a Cessna 402C airplane, registration N5802C, was substantially damaged during landing at Albuquerque International Sunport Airport (ABQ), Albuquerque, New Mexico. The accident followed a hydraulic malfunction and subsequent collapse of the right main landing gear. The airline transport rated pilot was not injured.

Flight Details

The non-scheduled cargo flight was conducted under 14 Code of Federal Regulations Part 135 with a visual flight rules (VFR) flight plan. The flight originated at ABQ, with Las Vegas Municipal Airport (LVS), Las Vegas, New Mexico, as the intended destination. Visual meteorological conditions prevailed at the time of the accident.

Sequence of Events

The pilot reported that after gear retraction on initial takeoff from ABQ, the hydraulic pressure caution light illuminated and the nose landing gear failed to retract. The pilot performed the HYD PRESSURE LIGHT ILLUMINATED AFTER GEAR CYCLE and the LANDING GEAR WILL NOT EXTEND HYDRAULICALLY checklists, resulting in unsafe gear indications. He executed an approved flyover of the ABQ tower, and tower personnel reported the gear appeared to be down. During landing, the right main landing gear collapsed, causing substantial damage to the right aileron.

Post-Accident Examination

The day after the accident, the airplane was examined by Federal Aviation Administration inspectors and the operator. The aircraft was placed on jacks, and the landing gear was functionally tested. The system cycled with no anomalies noted. The hydraulic control valve and the landing gear hydraulic shuttle valve were removed for functional testing and contaminant checks. No anomalies were found with either unit.

Contributing factors

Causes

Gear extension and retract sys — Failure

Other contributing factors

Damaged/degraded