19991121041129A

Accident · Destroyed

FAA accident report · Piper PA60600 · Avalon, CA · November 21, 1999

Date
November 21, 1999 · 10:15 local
Place
Avalon, CA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N97CC
NTSB investigation
NTSBLAX00LA038
Reported as
Piper PA60600
Reported engine
Lycoming TIO540*
People aboard
1
Fatal injuries
1
Pilot’s flight hours
1,710 total851 in this make and model100 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) The a/c departed fullerton, CA airport, was conducting "airwork" off the coast south of seal beach, CA. At 1015 PDT radar and radio contact was lost when the a/c was 20 miles south of seal beach (sli) VOR. The wreckage and remains of one person were located by the us coast guard. The body was recovered and taken to the USCG base in san pedro, CA. The a/c was destroyed on impact and sunk. (.4) on November 21, 1999, about 1015 hours pacific standard time, a smith Aerostar 600, N97CC, registered to the pilot, descended into the pacific ocean near Avalon, California. The airline transport rated pilot, the sole occupant, received fatal injuries. Visual meteorological conditions prevailed for the personal flight, which was operated by the pilot under the provisions of 14 CFR part 91. No flight plan was filed for the local area flight which originated at fullerton, California, about 0930. According to a family member, the airplane had maintenance performed and the pilot was accomplishing a post maintenance flight check. Review of information and radar data provided by the FAA disclosed that the pilot was receiving visual flight advisories from southern California terminal radar approach control. At 1015, radar contact was lost on the 200-degree radial of the seal beach VOR at 20 miles. Recorded radar data revealed that the mode c return was level at 4,900 feet mean sea level and exhibited a slowing ground speed. The secondary beacon returns then started a descending right spiral and radar contact was lost at 1,000 feet MSL. The pilot's body was recovered from the ocean and an autopsy was conducted by the los angeles county coroner's office. According to the autopsy report, the pilot had experienced sudden cardiac death secondary to an acute myocardial infarction due to atherosclerotic coronary artery disease. The attesting pathologist opinined that the event began from 30 minutes to several hours before the pilot's death. Tramadol, a painkiller not approved by the FAA for flight, was detected in blood and tissue samples submitted for toxicological tests. The pathologist stated that the drug may have masked the chest pain symptoms of the cardiac event. The a/c was not recovered. Review of the maintenance records disclosed that on novemer 5, 1999, the oil was changed on both engines. During engine run-up a "hot" or non-grounding magneto was found on the right engine. A loose "p" lead for grounding the magneto was discovered and reattached. At the same time, a broken exhaust flange was discovered on the no. 6 engine cylinder. Subsequently, the entire exhaust system and a gas temperature probe were replaced on the right engine. According to maintenance records, the last annual inspection occurred on July 16, 1999.

As the FAA filed it

(-23) THE A/C DEPARTED FULLERTON, CA AIRPORT, WAS CONDUCTING "AIRWORK" OFF THE COAST SOUTH OF SEAL BEACH, CA. AT 1015 PDT RADAR AND RADIO CONTACT WAS LOST WHEN THE A/C WAS 20 MILES SOUTH OF SEAL BEACH (SLI) VOR. THE WRECKAGE AND REMAINS OF ONE PERSON WERE LOCATED BY THE US COAST GUARD. THE BODY WAS RECOVERED AND TAKEN TO THE USCG BASE IN SAN PEDRO, CA. THE A/C WAS DESTROYED ON IMPACT AND SUNK. (.4) ON NOVEMBER 21, 1999, ABOUT 1015 HOURS PACIFIC STANDARD TIME, A SMITH AEROSTAR 600, N97CC, REGISTERED TO THE PILOT, DESCENDED INTO THE PACIFIC OCEAN NEAR AVALON, CALIFORNIA. THE AIRLINE TRANSPORT RATED PILOT, THE SOLE OCCUPANT, RECEIVED FATAL INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PERSONAL FLIGHT, WHICH WAS OPERATED BY THE PILOT UNDER THE PROVISIONS OF 14 CFR PART 91. NO FLIGHT PLAN WAS FILED FOR THE LOCAL AREA FLIGHT WHICH ORIGINATED AT FULLERTON, CALIFORNIA, ABOUT 0930. ACCORDING TO A FAMILY MEMBER, THE AIRPLANE HAD MAINTENANCE PERFORMED AND THE PILOT WAS ACCOMPLISHING A POST MAINTENANCE FLIGHT CHECK. REVIEW OF INFORMATION AND RADAR DATA PROVIDED BY THE FAA DISCLOSED THAT THE PILOT WAS RECEIVING VISUAL FLIGHT ADVISORIES FROM SOUTHERN CALIFORNIA TERMINAL RADAR APPROACH CONTROL. AT 1015, RADAR CONTACT WAS LOST ON THE 200-DEGREE RADIAL OF THE SEAL BEACH VOR AT 20 MILES. RECORDED RADAR DATA REVEALED THAT THE MODE C RETURN WAS LEVEL AT 4,900 FEET MEAN SEA LEVEL AND EXHIBITED A SLOWING GROUND SPEED. THE SECONDARY BEACON RETURNS THEN STARTED A DESCENDING RIGHT SPIRAL AND RADAR CONTACT WAS LOST AT 1,000 FEET MSL. THE PILOT'S BODY WAS RECOVERED FROM THE OCEAN AND AN AUTOPSY WAS CONDUCTED BY THE LOS ANGELES COUNTY CORONER'S OFFICE. ACCORDING TO THE AUTOPSY REPORT, THE PILOT HAD EXPERIENCED SUDDEN CARDIAC DEATH SECONDARY TO AN ACUTE MYOCARDIAL INFARCTION DUE TO ATHEROSCLEROTIC CORONARY ARTERY DISEASE. THE ATTESTING PATHOLOGIST OPININED THAT THE EVENT BEGAN FROM 30 MINUTES TO SEVERAL HOURS BEFORE THE PILOT'S DEATH. TRAMADOL, A PAINKILLER NOT APPROVED BY THE FAA FOR FLIGHT, WAS DETECTED IN BLOOD AND TISSUE SAMPLES SUBMITTED FOR TOXICOLOGICAL TESTS. THE PATHOLOGIST STATED THAT THE DRUG MAY HAVE MASKED THE CHEST PAIN SYMPTOMS OF THE CARDIAC EVENT. THE A/C WAS NOT RECOVERED. REVIEW OF THE MAINTENANCE RECORDS DISCLOSED THAT ON NOVEMER 5, 1999, THE OIL WAS CHANGED ON BOTH ENGINES. DURING ENGINE RUN-UP A "HOT" OR NON-GROUNDING MAGNETO WAS FOUND ON THE RIGHT ENGINE. A LOOSE "P" LEAD FOR GROUNDING THE MAGNETO WAS DISCOVERED AND REATTACHED. AT THE SAME TIME, A BROKEN EXHAUST FLANGE WAS DISCOVERED ON THE NO. 6 ENGINE CYLINDER. SUBSEQUENTLY, THE ENTIRE EXHAUST SYSTEM AND A GAS TEMPERATURE PROBE WERE REPLACED ON THE RIGHT ENGINE. ACCORDING TO MAINTENANCE RECORDS, THE LAST ANNUAL INSPECTION OCCURRED ON JULY 16, 1999.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N97CC · 1

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