19961020033101A

Accident · Substantial damage

FAA accident report · Cessna 210K · Tampa, FL · October 20, 1996

Date
October 20, 1996 · 10:30 local
Place
Tampa, FL
Airport
Vandenberg Airport
Phase of flight
In Traffic Pattern-Circling
Operating rules
General operating rules (Part 91)
Collision
Midair collision, first aircraft
Damage
Substantial damage
Aircraft
N81SC
NTSB investigation
NTSBMIA97LA008
Reported as
Cessna 210K
Reported engine
Continental IO520L
People aboard
3
Fatal injuries
0
Pilot’s flight hours
2,681 total150 in this make and model40 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.

(.4)The Cessna 210, N81SC, was planning on departing the traffic pattern on the downwind leg and reportedly announced his takeoff, crosswind and downwind turns. The Beech 23, N4021T, was inbound from the north and announced his intention of a 'long' 2 mile downwind, which was reportedly heard by an employee at the airport. The Cessna was just completing the turn to downwind at 900 feet when the collision occurred. The pilots of both airplanes were able to land at the airport. A witness observed the collision and reported that it occurred about 1/4 mile north and 1/3 mile west of the departure end of runway 36. A component from the Cessna was found in a field located about 1 nautical mile and 322 degrees from the departure end of the runway. The aim recommends that aircraft depart the traffic pattern either on the upwind leg or turn 45 degrees to the left while in the upwind leg. The recommended downwind entry is at a 45 degree angle abeam the midpoint of the downwind leg.

As the FAA filed it

(.4)THE CESSNA 210, N81SC, WAS PLANNING ON DEPARTING THE TRAFFIC PATTERN ON THE DOWNWIND LEG AND REPORTEDLY ANNOUNCED HIS TAKEOFF, CROSSWIND AND DOWNWIND TURNS. THE BEECH 23, N4021T, WAS INBOUND FROM THE NORTH AND ANNOUNCED HIS INTENTION OF A 'LONG' 2 MILE DOWNWIND, WHICH WAS REPORTEDLY HEARD BY AN EMPLOYEE AT THE AIRPORT. THE CESSNA WAS JUST COMPLETING THE TURN TO DOWNWIND AT 900 FEET WHEN THE COLLISION OCCURRED. THE PILOTS OF BOTH AIRPLANES WERE ABLE TO LAND AT THE AIRPORT. A WITNESS OBSERVED THE COLLISION AND REPORTED THAT IT OCCURRED ABOUT 1/4 MILE NORTH AND 1/3 MILE WEST OF THE DEPARTURE END OF RUNWAY 36. A COMPONENT FROM THE CESSNA WAS FOUND IN A FIELD LOCATED ABOUT 1 NAUTICAL MILE AND 322 DEGREES FROM THE DEPARTURE END OF THE RUNWAY. THE AIM RECOMMENDS THAT AIRCRAFT DEPART THE TRAFFIC PATTERN EITHER ON THE UPWIND LEG OR TURN 45 DEGREES TO THE LEFT WHILE IN THE UPWIND LEG. THE RECOMMENDED DOWNWIND ENTRY IS AT A 45 DEGREE ANGLE ABEAM THE MIDPOINT OF THE DOWNWIND LEG.

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.

Other reports on N81SC · 1

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