20010601013119I

Incident · Substantial damage

FAA incident report · Beech D55 · Stockton, CA · June 1, 2001

Date
June 1, 2001 · 21:07 local
Place
Stockton, CA
Airport
Stockton Metropolitan
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2296V
Reported as
Beech D55
Reported engine
Continental IO520C
Pilot’s flight hours
1,961 total46 in this make and model90 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry 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.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23)Pilot states: departed alto morning of 06/01/01 for oxnard, CA. Flight normal. On return flight from oxnard that evening, he began experiencing electrical system failures, beginning with interior light and instrument light failures. At approximately 50NM from sck, he contacted Stockton tower to report situation, and began turning systems off to conserve power for radios. On approach to sck, he attempted normal extension of the landing gear, but normal mode would not function. Manual extension was executed after opening landing gear circuit breaker. He asked tower whether they could see position of landing gear. In dark conditions, no determination could be made. Pilot indicated he had "down arrow" in view. As the circuit breaker was "pulled", he did not have indicator light available for landing gear position indication. Landing was executed. Pilot reported as weight on wheels increased, he sensed the right wing settling closer to the ground. He feather the propellers, and was able to maintain directional control of aircraft, as all three landing gear collapsed. Pilot evacuated the aircraft with no injuries. Substantial damage to underside resulted. Investigation of electrical system to follow.

As the FAA filed it

(-23)PILOT STATES: DEPARTED ALTO MORNING OF 06/01/01 FOR OXNARD, CA. FLIGHT NORMAL. ON RETURN FLIGHT FROM OXNARD THAT EVENING, HE BEGAN EXPERIENCING ELECTRICAL SYSTEM FAILURES, BEGINNING WITH INTERIOR LIGHT AND INSTRUMENT LIGHT FAILURES. AT APPROXIMATELY 50NM FROM SCK, HE CONTACTED STOCKTON TOWER TO REPORT SITUATION, AND BEGAN TURNING SYSTEMS OFF TO CONSERVE POWER FOR RADIOS. ON APPROACH TO SCK, HE ATTEMPTED NORMAL EXTENSION OF THE LANDING GEAR, BUT NORMAL MODE WOULD NOT FUNCTION. MANUAL EXTENSION WAS EXECUTED AFTER OPENING LANDING GEAR CIRCUIT BREAKER. HE ASKED TOWER WHETHER THEY COULD SEE POSITION OF LANDING GEAR. IN DARK CONDITIONS, NO DETERMINATION COULD BE MADE. PILOT INDICATED HE HAD "DOWN ARROW" IN VIEW. AS THE CIRCUIT BREAKER WAS "PULLED", HE DID NOT HAVE INDICATOR LIGHT AVAILABLE FOR LANDING GEAR POSITION INDICATION. LANDING WAS EXECUTED. PILOT REPORTED AS WEIGHT ON WHEELS INCREASED, HE SENSED THE RIGHT WING SETTLING CLOSER TO THE GROUND. HE FEATHER THE PROPELLERS, AND WAS ABLE TO MAINTAIN DIRECTIONAL CONTROL OF AIRCRAFT, AS ALL THREE LANDING GEAR COLLAPSED. PILOT EVACUATED THE AIRCRAFT WITH NO INJURIES. SUBSTANTIAL DAMAGE TO UNDERSIDE RESULTED. INVESTIGATION OF ELECTRICAL SYSTEM TO FOLLOW.

Other reports on N2296V · 1

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