20010210002819I

Incident · Minor damage

FAA incident report · Cessna 182 · Etters, PA · February 10, 2001

Date
February 10, 2001 · 20:19 local
Place
Etters, PA
Airport
Fairview Township
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N3DZ
Reported as
Cessna 182
Reported engine
Continental O470L

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 subject aircraft was being returned to the owner based at (481) duanesburg, new york from skydiving operations at (glv) gainesville, Georgia. The commercial pilot had 338 hours in this model in the past three years. After topping off fuel tanks at (glv) the aircraft proceeded on a direct GPS course of 041 for the first 1.5 hours and then changed course to 038 degrees to plan a fuel stop at (cxy) new cumberland, PA. The VFR flight, which lasted 4 hours 7 minutes, ended with an off field landing in Fairview Township, PA. During the landing, the aircraft nose gear contacted a wooden fence in the backyard of a home in a sub-division. The aircraft flipped over as a result causing damage to the lawn and fence. The aircraft received damage to the propeller, cowling, wing tip, and both horizontal and vertical stabilizer leading edges. The pilot was not injured. The pilot reported to ATC that his engine began to sputter then quit while he was descending from 5500' AGL. A post crash reconstruction of the flight made with privacy data omittedCessna accident investigator, revealed the aircraft probably contained 8 to 10 gallons of remaining fuel, most of which was lost due to being inverted. The post crash inspection and subsequent engine test revealed a large quantity of water was present in the gascolator and carburetor. Folds in the fuel bladder floor resulted in water retention during tank sumping.

As the FAA filed it

(-23) THE SUBJECT AIRCRAFT WAS BEING RETURNED TO THE OWNER BASED AT (481) DUANESBURG, NEW YORK FROM SKYDIVING OPERATIONS AT (GLV) GAINESVILLE, GEORGIA. THE COMMERCIAL PILOT HAD 338 HOURS IN THIS MODEL IN THE PAST THREE YEARS. AFTER TOPPING OFF FUEL TANKS AT (GLV) THE AIRCRAFT PROCEEDED ON A DIRECT GPS COURSE OF 041 FOR THE FIRST 1.5 HOURS AND THEN CHANGED COURSE TO 038 DEGREES TO PLAN A FUEL STOP AT (CXY) NEW CUMBERLAND, PA. THE VFR FLIGHT, WHICH LASTED 4 HOURS 7 MINUTES, ENDED WITH AN OFF FIELD LANDING IN FAIRVIEW TOWNSHIP, PA. DURING THE LANDING, THE AIRCRAFT NOSE GEAR CONTACTED A WOODEN FENCE IN THE BACKYARD OF A HOME IN A SUB-DIVISION. THE AIRCRAFT FLIPPED OVER AS A RESULT CAUSING DAMAGE TO THE LAWN AND FENCE. THE AIRCRAFT RECEIVED DAMAGE TO THE PROPELLER, COWLING, WING TIP, AND BOTH HORIZONTAL AND VERTICAL STABILIZER LEADING EDGES. THE PILOT WAS NOT INJURED. THE PILOT REPORTED TO ATC THAT HIS ENGINE BEGAN TO SPUTTER THEN QUIT WHILE HE WAS DESCENDING FROM 5500' AGL. A POST CRASH RECONSTRUCTION OF THE FLIGHT MADE WITH ^PRIVACY DATA ^CESSNA ACCIDENT INVESTIGATOR, REVEALED THE AIRCRAFT PROBABLY CONTAINED 8 TO 10 GALLONS OF REMAINING FUEL, MOST OF WHICH WAS LOST DUE TO BEING INVERTED. THE POST CRASH INSPECTION AND SUBSEQUENT ENGINE TEST REVEALED A LARGE QUANTITY OF WATER WAS PRESENT IN THE GASCOLATOR AND CARBURETOR. FOLDS IN THE FUEL BLADDER FLOOR RESULTED IN WATER RETENTION DURING TANK SUMPING.

Other reports on N3DZ · 2

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