Piper PA-28-140 N5314S

Summary

On 7 March 1993 at about 19:30 local time, a Piper PA-28-140 registered N5314S, operated by Joseph V. Fera, was involved in an accident near Kissimmee, Florida, United States. 4 people were on board and one was seriously injured, 3 had minor injuries. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

7 March 1993 at 19:30

Classification

Accident

Location

Kissimmee, Florida, United States

Nearest airport

Kissimmee Municipal (ISM)

Coordinates

28.3010, -81.4101

Aircraft

Piper PA-28-140

Registration

N5314S

Category

Airplane

Engines

1

Operator

Joseph V. Fera

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Unknown → Lake Wales

Aircraft damage

Destroyed

Weather

VMC

Light

Day

NTSB number

MIA93FA082

1 person was seriously injured.

THE PILOT-IN-COMMAND'S ATTEMPT TO CLIMB AT A HIGH PITCH ATTITUDE AFTER TAKEOFF AND HIS FAILURE TO MAINTAIN AIRSPEED WHICH RESULTED IN A STALL MUSH CONDITION UNTIL THE AIRCRAFT DESCENDED TO THE GROUND. CONTRIBUTING TO THE ACCIDENT WAS THE PILOT-IN-COMMAND'S ATTEMPT TO TAKE OFF 150 POUNDS OVER MAXIMUM GROSS WEIGHT WITH A CENTER OF GRAVITY FORWARD OF THE FORWARD CENTER OF GRAVITY LIMIT. ADDITIONALLY, CONTRIBUTING TO THE ACCIDENT WAS THE PILOT-IN-COMMAND'S FAILURE TO SET STABILIZER TRIM FOR TAKEOFF AND HIS FAILURE TO RECOGNIZE THE STALLED CONDITION AND INITIATE STALL RECOVERY.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

AFTER TAKEOFF THE AIRCRAFT WAS OBSERVED BY WITNESSES TO BE IN AN UNUSUALLY HIGH PITCH ATTITUDE WHICH SOME WITNESSES DESCRIBED AS A STALLED CONDITION. THE PASSENGERS STATED THAT AFTER TAKEOFF THE AIRCRAFT BEGAN TO SHAKE BUT THAT THE ENGINE NOISE DID NOT CHANGE. THE AIRCRAFT DESCENDED IN THE HIGH PITCH ATTITUDE UNTIL GROUND IMPACT. EXAMINATION OF THE AIRCRAFT REVEALED NO EVIDENCE TO INDICATE PRECRASH FAILURE OR MALFUNCTION OF THE AIRCRAFT STRUCTURE, FLIGHT CONTROLS, OR ENGINE. CALCULATIONS INDICATED THE AIRCRAFT WAS ABOUT 150 OVER MAXIMUM ALLOWABLE GROSS WEIGHT AT THE TIME OF THE ACCIDENT. THE CENTER OF GRAVITY WAS 2.8 INCHES FORWARD OF THE FORWARD LIMIT FOR THE WEIGHT CONDITIONS. THE STABILATOR TRIM WAS FOUND AT THE 9-DEGREE TAB-DOWN OR NOSE-UP POSITION. THE AIRCRAFT FLIGHT MANUAL CALLS FOR TRIM NEAR NEUTRAL FOR TAKEOFF. ACCORDING TO THE PILOT'S LOGBOOK THE PILOT DID NOT HAVE THE REQUIRED THREE TAKEOFFS AND LANDINGS IN THE PAST 90 DAYS REQUIRED BY REGULATIONS TO ACT AS PILOT-IN-COMMAND CARRYING PASSENGERS.

Quoted verbatim from the NTSB record.