20050429006799A

Accident · Substantial damage

FAA accident report · Piper PA-25-235 · Houston, TX · April 29, 2005

Date
April 29, 2005 · 16:03 local
Place
Houston, TX
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4514Y
NTSB investigation
NTSBDFW05LA113
Reported as
Piper PA25235
Reported engine
Lycoming O540B2B5
Fatal injuries
0
Pilot’s flight hours
2,580 total1,200 in this make and model180 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) The PA-25-235 pawnee was at approximately 1,000 feet AGL and towing a 40' tall x 120' long, 4,800 square foot "billboard banner" over a congested area on the west side of Houston TX when the engine suddenly quit. The pilot said his only available forced landing area was the athletic grounds next to a high school. The pilot said he dropped his banner at 300 feet AGL and was at approximately 70 knots when he touched down on the left main gear, bounced once, and struck a 12 foot chain link fence surrounding the high school tennis courts. Total distance after initial touchdown was 280 feet. Only a superficial injury to the pilot, but there was substantial damage to the pawnee (both wing spars were damaged). FAA inspectors found water and solid contaminants in the gascolator and the carburetor bowl, and found an obvious "winged insect" trapped in the transparent in-line fuel filter. The operator's privately operated above ground fuel storage facility had no provisions for sumping the fuel, no provisions for a low point drain, no psid gauges, no water fuse, no record of filter change, no plan for quality sumping, and only a 2 lb dry chem fx, however the delivery pump sample passed a white bucket test.

As the FAA filed it

(-23) THE PA-25-235 PAWNEE WAS AT APPROXIMATELY 1,000 FEET AGL AND TOWING A 40' TALL X 120' LONG, 4,800 SQUARE FOOT "BILLBOARD BANNER" OVER A CONGESTED AREA ON THE WEST SIDE OF HOUSTON TX WHEN THE ENGINE SUDDENLY QUIT. THE PILOT SAID HIS ONLY AVAILABLE FORCED LANDING AREA WAS THE ATHLETIC GROUNDS NEXT TO A HIGH SCHOOL. THE PILOT SAID HE DROPPED HIS BANNER AT 300 FEET AGL AND WAS AT APPROXIMATELY 70 KNOTS WHEN HE TOUCHED DOWN ON THE LEFT MAIN GEAR, BOUNCED ONCE, AND STRUCK A 12 FOOT CHAIN LINK FENCE SURROUNDING THE HIGH SCHOOL TENNIS COURTS. TOTAL DISTANCE AFTER INITIAL TOUCHDOWN WAS 280 FEET. ONLY A SUPERFICIAL INJURY TO THE PILOT, BUT THERE WAS SUBSTANTIAL DAMAGE TO THE PAWNEE (BOTH WING SPARS WERE DAMAGED). FAA INSPECTORS FOUND WATER AND SOLID CONTAMINANTS IN THE GASCOLATOR AND THE CARBURETOR BOWL, AND FOUND AN OBVIOUS "WINGED INSECT" TRAPPED IN THE TRANSPARENT IN-LINE FUEL FILTER. THE OPERATOR'S PRIVATELY OPERATED ABOVE GROUND FUEL STORAGE FACILITY HAD NO PROVISIONS FOR SUMPING THE FUEL, NO PROVISIONS FOR A LOW POINT DRAIN, NO PSID GAUGES, NO WATER FUSE, NO RECORD OF FILTER CHANGE, NO PLAN FOR QUALITY SUMPING, AND ONLY A 2 LB DRY CHEM FX, HOWEVER THE DELIVERY PUMP SAMPLE PASSED A WHITE BUCKET TEST.

NTSB investigation

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