19980821021479A

Accident · Destroyed

FAA accident report · Cessna 182N · Painesville, OH · August 21, 1998

Date
August 21, 1998 · 16:45 local
Place
Painesville, OH
Airport
Casement Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9282G
NTSB investigation
NTSBIAD98FA097
Reported as
Cessna 182N
Reported engine
Continental O470R
People aboard
1
Fatal injuries
1
Pilot’s flight hours
970 total159 in this make and model5 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.

Acft crashed shortly after takeoff 1000 feet south east of the departure end of the runway. (.23) during investigation, evidence of oil was found on the left top surface of the engine, the uderside of the top cowl, and top surface of cowl, emitting from area of oil filler access door. The ingine oil filler cap was not on the oil filler tube. The cap was found on the engine compartment. The cap did not have the gasket installed. The cap would not lock into position onto the tube, nor fit tightly to the tube. (.4)according to a witness, the pilot departed runway 12. Shortly after takeoff, the pilot made a right turn, followed by a left turn. The airplane impacted the ground in a vertical descent 900 feet southeast of the airport. A second witness at the airport reported that the pilot refueled, started the airplane and departed with a tailwind without completing a preflight inspection or run-up. Examination of the wreckage revealed that the engine oil filler door was bent with the secure latch found pushed in. Upon removal of the engine cowling, there was evidence of oil on the inside. The oil filler cap had separated from the oil filler neck and it was found at the base of the engine. Examination of the oil filler cap revealed that the gasket was missing. When the oil filler cap was fitted to the filler neck, it rotated 360 degrees and would not fit securely. Search efforts did not locate the gasket in the wreckage or surrounding area. Some sections of separated windshield glass also showed evidence of oil deposits. Inside the airplane were five one-quart bottles of aeroshell 10W50. All except one bottle had burst open. The opened one was empty and the cap was intact with a broken seal. The reported winds at the time of the accident were from 330 degress at 7 knots. Examination of airplane and engine did not disclose any evidence of mechanical malfunction.

As the FAA filed it

ACFT CRASHED SHORTLY AFTER TAKEOFF 1000 FEET SOUTH EAST OF THE DEPARTURE END OF THE RUNWAY. (.23) DURING INVESTIGATION, EVIDENCE OF OIL WAS FOUND ON THE LEFT TOP SURFACE OF THE ENGINE, THE UDERSIDE OF THE TOP COWL, AND TOP SURFACE OF COWL, EMITTING FROM AREA OF OIL FILLER ACCESS DOOR. THE INGINE OIL FILLER CAP WAS NOT ON THE OIL FILLER TUBE. THE CAP WAS FOUND ON THE ENGINE COMPARTMENT. THE CAP DID NOT HAVE THE GASKET INSTALLED. THE CAP WOULD NOT LOCK INTO POSITION ONTO THE TUBE, NOR FIT TIGHTLY TO THE TUBE. (.4)ACCORDING TO A WITNESS, THE PILOT DEPARTED RUNWAY 12. SHORTLY AFTER TAKEOFF, THE PILOT MADE A RIGHT TURN, FOLLOWED BY A LEFT TURN. THE AIRPLANE IMPACTED THE GROUND IN A VERTICAL DESCENT 900 FEET SOUTHEAST OF THE AIRPORT. A SECOND WITNESS AT THE AIRPORT REPORTED THAT THE PILOT REFUELED, STARTED THE AIRPLANE AND DEPARTED WITH A TAILWIND WITHOUT COMPLETING A PREFLIGHT INSPECTION OR RUN-UP. EXAMINATION OF THE WRECKAGE REVEALED THAT THE ENGINE OIL FILLER DOOR WAS BENT WITH THE SECURE LATCH FOUND PUSHED IN. UPON REMOVAL OF THE ENGINE COWLING, THERE WAS EVIDENCE OF OIL ON THE INSIDE. THE OIL FILLER CAP HAD SEPARATED FROM THE OIL FILLER NECK AND IT WAS FOUND AT THE BASE OF THE ENGINE. EXAMINATION OF THE OIL FILLER CAP REVEALED THAT THE GASKET WAS MISSING. WHEN THE OIL FILLER CAP WAS FITTED TO THE FILLER NECK, IT ROTATED 360 DEGREES AND WOULD NOT FIT SECURELY. SEARCH EFFORTS DID NOT LOCATE THE GASKET IN THE WRECKAGE OR SURROUNDING AREA. SOME SECTIONS OF SEPARATED WINDSHIELD GLASS ALSO SHOWED EVIDENCE OF OIL DEPOSITS. INSIDE THE AIRPLANE WERE FIVE ONE-QUART BOTTLES OF AEROSHELL 10W50. ALL EXCEPT ONE BOTTLE HAD BURST OPEN. THE OPENED ONE WAS EMPTY AND THE CAP WAS INTACT WITH A BROKEN SEAL. THE REPORTED WINDS AT THE TIME OF THE ACCIDENT WERE FROM 330 DEGRESS AT 7 KNOTS. EXAMINATION OF AIRPLANE AND ENGINE DID NOT DISCLOSE ANY EVIDENCE OF MECHANICAL MALFUNCTION.

NTSB investigation

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