19940920029139A

Accident · Destroyed

FAA accident report · Piper PA-28R-200 · Oakland, MD · September 20, 1994

Date
September 20, 1994 · 19:00 local
Place
Oakland, MD
Airport
Garrett County Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N2815T
NTSB investigation
NTSBNYC94LA180
Reported as
Piper PA28R200
Reported engine
Lycoming IO360C1C
Fatal injuries
0

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.

Aircraft crashed on takeoff. (.4)the pilot/owner of the airplane and three other pilots were planning to fly to an aviation safety meeting. A preflight was completed and fuel samples were taken. After the run-up, flaps were set to 10 degrees and full power was applied during the takeoff roll. The airplane rotated near the end of the 3,000 foot runway, climbed about 40 feet and settled down into the trees. The pilot stated that no deficiencies were noted with the engine and airplane during the takeoff. Examination revealed that the airplane was about 175 pounds over the maximum gross weight at takeoff, the airport density altitude was 4,500 feet, and the takeoff runway had a 0.5% up-slope grade. The pilot's operating manual specifies a 25 degree flap setting, with full power applied before brake release, for an obstacle clearance takeoff.

As the FAA filed it

AIRCRAFT CRASHED ON TAKEOFF. (.4)THE PILOT/OWNER OF THE AIRPLANE AND THREE OTHER PILOTS WERE PLANNING TO FLY TO AN AVIATION SAFETY MEETING. A PREFLIGHT WAS COMPLETED AND FUEL SAMPLES WERE TAKEN. AFTER THE RUN-UP, FLAPS WERE SET TO 10 DEGREES AND FULL POWER WAS APPLIED DURING THE TAKEOFF ROLL. THE AIRPLANE ROTATED NEAR THE END OF THE 3,000 FOOT RUNWAY, CLIMBED ABOUT 40 FEET AND SETTLED DOWN INTO THE TREES. THE PILOT STATED THAT NO DEFICIENCIES WERE NOTED WITH THE ENGINE AND AIRPLANE DURING THE TAKEOFF. EXAMINATION REVEALED THAT THE AIRPLANE WAS ABOUT 175 POUNDS OVER THE MAXIMUM GROSS WEIGHT AT TAKEOFF, THE AIRPORT DENSITY ALTITUDE WAS 4,500 FEET, AND THE TAKEOFF RUNWAY HAD A 0.5% UP-SLOPE GRADE. THE PILOT'S OPERATING MANUAL SPECIFIES A 25 DEGREE FLAP SETTING, WITH FULL POWER APPLIED BEFORE BRAKE RELEASE, FOR AN OBSTACLE CLEARANCE TAKEOFF.

NTSB investigation

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