19980319003921A

Accident · Destroyed

FAA accident report · Cessna 310H · Corona, CA · March 19, 1998

Date
March 19, 1998 · 16:59 local
Place
Corona, CA
Airport
Corona Municipal Airport
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Collision
Midair collision, first aircraft
Damage
Destroyed
Aircraft
N310RR
NTSB investigation
NTSBLAX98FA118
Reported as
Cessna 310H
Reported engine
Continental IO520E
People aboard
2
Fatal injuries
2
Pilot’s flight hours
1,150 total800 in this make and model

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.

Collided with N6575L a 152 at entry point for downwind at L66. 152 was in pattern. 310 pilot possible sun problem. (.4) a Cessna 310 and a Cessna 152 collided in-flight about 2 miles south of the Corona airport at 2,600 feet mean sea level (about 2,000 above ground level). The Cessna 310, with two pilots aboard, was descending toward another nearby area airport, and the Cessna 152, flown by a certified flight instructor (the sole occupant) from the right seat, was orbiting south of the airport awaiting the reopening of the runway following construction. Radar data showed that in the 1 minute 18 seconds prior to the collision, the Cessna 310 descended from 4,000 feet to the collision point on a southeast bound ground track at a rate of about 1,200 feet per minute. Nine seconds prior to the collision, the Cessna 152, which had been on a westbound track, began a right turn toward a northwest bound ground track. Over the 1 minute 18 second period, the horizontal separation decreased from 6.01 nautical miles to zero as the vertical separation decreased 1,400 feet. Reconstruction of the two airplanes revealed that at the point of collision, the Cessna 310'S lateral axis was about 80 degrees to the Cessna 152'S vertical axis as the 310'S outer right wing and tip tank contacted the 152'S left main gear strut, lift strut, and inboard left wing. In the one minute prior to the collision, the relative horizontal bearing from the Cessna 310 ground track to the Cessna 152 was between 8 and 10 degrees left of the track. During this same period, the relative horizontal bearing from the Cessna 152 ground track to the Cessna 310 varied between 25 degrees and 40 degrees right of the Cessna 152 ground track as it maneuvered prior to the right turn. Trigonometric calculation of altitude difference between the targets yielded a 2 degree 10 minute relative vertical angle between the target positions.

As the FAA filed it

COLLIDED WITH N6575L A 152 AT ENTRY POINT FOR DOWNWIND AT L66. 152 WAS IN PATTERN. 310 PILOT POSSIBLE SUN PROBLEM. (.4) A CESSNA 310 AND A CESSNA 152 COLLIDED IN-FLIGHT ABOUT 2 MILES SOUTH OF THE CORONA AIRPORT AT 2,600 FEET MEAN SEA LEVEL (ABOUT 2,000 ABOVE GROUND LEVEL). THE CESSNA 310, WITH TWO PILOTS ABOARD, WAS DESCENDING TOWARD ANOTHER NEARBY AREA AIRPORT, AND THE CESSNA 152, FLOWN BY A CERTIFIED FLIGHT INSTRUCTOR (THE SOLE OCCUPANT) FROM THE RIGHT SEAT, WAS ORBITING SOUTH OF THE AIRPORT AWAITING THE REOPENING OF THE RUNWAY FOLLOWING CONSTRUCTION. RADAR DATA SHOWED THAT IN THE 1 MINUTE 18 SECONDS PRIOR TO THE COLLISION, THE CESSNA 310 DESCENDED FROM 4,000 FEET TO THE COLLISION POINT ON A SOUTHEAST BOUND GROUND TRACK AT A RATE OF ABOUT 1,200 FEET PER MINUTE. NINE SECONDS PRIOR TO THE COLLISION, THE CESSNA 152, WHICH HAD BEEN ON A WESTBOUND TRACK, BEGAN A RIGHT TURN TOWARD A NORTHWEST BOUND GROUND TRACK. OVER THE 1 MINUTE 18 SECOND PERIOD, THE HORIZONTAL SEPARATION DECREASED FROM 6.01 NAUTICAL MILES TO ZERO AS THE VERTICAL SEPARATION DECREASED 1,400 FEET. RECONSTRUCTION OF THE TWO AIRPLANES REVEALED THAT AT THE POINT OF COLLISION, THE CESSNA 310'S LATERAL AXIS WAS ABOUT 80 DEGREES TO THE CESSNA 152'S VERTICAL AXIS AS THE 310'S OUTER RIGHT WING AND TIP TANK CONTACTED THE 152'S LEFT MAIN GEAR STRUT, LIFT STRUT, AND INBOARD LEFT WING. IN THE ONE MINUTE PRIOR TO THE COLLISION, THE RELATIVE HORIZONTAL BEARING FROM THE CESSNA 310 GROUND TRACK TO THE CESSNA 152 WAS BETWEEN 8 AND 10 DEGREES LEFT OF THE TRACK. DURING THIS SAME PERIOD, THE RELATIVE HORIZONTAL BEARING FROM THE CESSNA 152 GROUND TRACK TO THE CESSNA 310 VARIED BETWEEN 25 DEGREES AND 40 DEGREES RIGHT OF THE CESSNA 152 GROUND TRACK AS IT MANEUVERED PRIOR TO THE RIGHT TURN. TRIGONOMETRIC CALCULATION OF ALTITUDE DIFFERENCE BETWEEN THE TARGETS YIELDED A 2 DEGREE 10 MINUTE RELATIVE VERTICAL ANGLE BETWEEN THE TARGET POSITIONS.

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 aircraft in the event · 1

Each aircraft in a collision has its own report.