19990612047299A

Accident · Substantial damage

FAA accident report · Piper PA-28-140 · Grandjunction, CO · June 12, 1999

Date
June 12, 1999 · 15:45 local
Place
Grandjunction, CO
Airport
Private
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7556R
NTSB investigation
NTSBDEN99LA101
Reported as
Piper PA28140
Reported engine
Lycoming O320*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
601 total1 in this make and model118 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) While on takeoff roll from a 2,250 foot long Private air strip the aircraft became airborne then settled back to the ground off the end of the departure runway. The runway was dirt surface and the pilot was making his takeoff to the east. Wind at the time was from 290 degrees at 10 knots with gusts to 17 knots. Aircraft performance data provided information that the aircraft was within 70 pounds of its maximum certificated gross weight and that the takeoff chart upper limit was 7,000 foot density altitude. The actual density altitude was 7,700 feet. According to the chart, which was based on a hard surface runway, no wind, and the aircraft at maximum certificated gross weight, the takeoff roll should have been 1,750 feet. The chart also stated that extending the curves above the 7,000 foot upper limit was not permissible. The pilot said he thought he encountered a wind shear during rotation. (-23) see narrative #DEN99LA101

As the FAA filed it

(.4) WHILE ON TAKEOFF ROLL FROM A 2,250 FOOT LONG PRIVATE AIR STRIP THE AIRCRAFT BECAME AIRBORNE THEN SETTLED BACK TO THE GROUND OFF THE END OF THE DEPARTURE RUNWAY. THE RUNWAY WAS DIRT SURFACE AND THE PILOT WAS MAKING HIS TAKEOFF TO THE EAST. WIND AT THE TIME WAS FROM 290 DEGREES AT 10 KNOTS WITH GUSTS TO 17 KNOTS. AIRCRAFT PERFORMANCE DATA PROVIDED INFORMATION THAT THE AIRCRAFT WAS WITHIN 70 POUNDS OF ITS MAXIMUM CERTIFICATED GROSS WEIGHT AND THAT THE TAKEOFF CHART UPPER LIMIT WAS 7,000 FOOT DENSITY ALTITUDE. THE ACTUAL DENSITY ALTITUDE WAS 7,700 FEET. ACCORDING TO THE CHART, WHICH WAS BASED ON A HARD SURFACE RUNWAY, NO WIND, AND THE AIRCRAFT AT MAXIMUM CERTIFICATED GROSS WEIGHT, THE TAKEOFF ROLL SHOULD HAVE BEEN 1,750 FEET. THE CHART ALSO STATED THAT EXTENDING THE CURVES ABOVE THE 7,000 FOOT UPPER LIMIT WAS NOT PERMISSIBLE. THE PILOT SAID HE THOUGHT HE ENCOUNTERED A WIND SHEAR DURING ROTATION. (-23) SEE NARRATIVE #DEN99LA101

NTSB investigation

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