20021013036009A

Accident · Substantial damage

FAA accident report · Cessna 172N · Pompano Beach, FL · October 13, 2002

Date
October 13, 2002 · 14:30 local
Place
Pompano Beach, FL
Airport
Pompano Beach Airpark Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6542J
NTSB investigation
NTSBATL03LA003
Reported as
Cessna 172N
Reported engine
Lycoming O320H2AD
People aboard
1
Fatal injuries
0
Pilot’s flight hours
76 total76 in this make and model30 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) Inspectors statement: on 10/13/02 at about 16:30 eastern daylight time, a Cessna 172N, N6542J, registered to American flyers flight school crashed into the airport property fence shortly after takeoff from runway 10 at Pompano air park (pmp) located in Pompano, Florida. Visual meteorological conditions prevailed and visual flight rules (VFR) flight plan was filed for the 14 CFR part 91 personal flight. There were no serious injuries reported but the aircraft sustained major damage. When the pilot was interviewed he stated that after a normal takeoff he noted a loss of engine performance. At this time the aircraft was about 75-90 feet in altitude and about 70% down the runway. The pilot said the aircraft began a descent and then he decided to try to land back on the runway. The pilot stated that upon touchdown, the aircraft bounced three times on the runway before exiting the end of the runway onto the grass and colliding with the airport property fence. The pilot was not injured but the aircraft received major damage to both wings, aircraft fuselage right side aft of engine firewall and to the aircraft crown area. Engine inspection disclosed damage to the engine mount and exhaust pipe. The propeller received only minor nicks and scrapes, prop spinner was destroyed. On October 16, 2002 the engine was tested on the aircraft at Pompano airport. Maintenance personnel from American flyers performed the engine run with me present inside the aircraft. The engine run disclosed a magneto drop of 100 RPM on left and right side at 1700 RPM, with a takeoff RPM of 2200 RPM, well within the green range. Oil press and oil temp. Were in the normal range. This test was performed several times with the same results. The engine attained takeoff power without any hesitation or roughness. Post engine inspection disclosed no oil leaks or further discrepancies.

As the FAA filed it

(-23) INSPECTORS STATEMENT: ON 10/13/02 AT ABOUT 16:30 EASTERN DAYLIGHT TIME, A CESSNA 172N, N6542J, REGISTERED TO AMERICAN FLYERS FLIGHT SCHOOL CRASHED INTO THE AIRPORT PROPERTY FENCE SHORTLY AFTER TAKEOFF FROM RUNWAY 10 AT POMPANO AIR PARK (PMP) LOCATED IN POMPANO, FLORIDA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND VISUAL FLIGHT RULES (VFR) FLIGHT PLAN WAS FILED FOR THE 14 CFR PART 91 PERSONAL FLIGHT. THERE WERE NO SERIOUS INJURIES REPORTED BUT THE AIRCRAFT SUSTAINED MAJOR DAMAGE. WHEN THE PILOT WAS INTERVIEWED HE STATED THAT AFTER A NORMAL TAKEOFF HE NOTED A LOSS OF ENGINE PERFORMANCE. AT THIS TIME THE AIRCRAFT WAS ABOUT 75-90 FEET IN ALTITUDE AND ABOUT 70% DOWN THE RUNWAY. THE PILOT SAID THE AIRCRAFT BEGAN A DESCENT AND THEN HE DECIDED TO TRY TO LAND BACK ON THE RUNWAY. THE PILOT STATED THAT UPON TOUCHDOWN, THE AIRCRAFT BOUNCED THREE TIMES ON THE RUNWAY BEFORE EXITING THE END OF THE RUNWAY ONTO THE GRASS AND COLLIDING WITH THE AIRPORT PROPERTY FENCE. THE PILOT WAS NOT INJURED BUT THE AIRCRAFT RECEIVED MAJOR DAMAGE TO BOTH WINGS, AIRCRAFT FUSELAGE RIGHT SIDE AFT OF ENGINE FIREWALL AND TO THE AIRCRAFT CROWN AREA. ENGINE INSPECTION DISCLOSED DAMAGE TO THE ENGINE MOUNT AND EXHAUST PIPE. THE PROPELLER RECEIVED ONLY MINOR NICKS AND SCRAPES, PROP SPINNER WAS DESTROYED. ON OCTOBER 16, 2002 THE ENGINE WAS TESTED ON THE AIRCRAFT AT POMPANO AIRPORT. MAINTENANCE PERSONNEL FROM AMERICAN FLYERS PERFORMED THE ENGINE RUN WITH ME PRESENT INSIDE THE AIRCRAFT. THE ENGINE RUN DISCLOSED A MAGNETO DROP OF 100 RPM ON LEFT AND RIGHT SIDE AT 1700 RPM, WITH A TAKEOFF RPM OF 2200 RPM, WELL WITHIN THE GREEN RANGE. OIL PRESS AND OIL TEMP. WERE IN THE NORMAL RANGE. THIS TEST WAS PERFORMED SEVERAL TIMES WITH THE SAME RESULTS. THE ENGINE ATTAINED TAKEOFF POWER WITHOUT ANY HESITATION OR ROUGHNESS. POST ENGINE INSPECTION DISCLOSED NO OIL LEAKS OR FURTHER DISCREPANCIES.

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 N6542J · 3

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