19980222001569A

Accident · Destroyed

FAA accident report · Piper PA-28-235 · Jackson, MS · February 22, 1998

Date
February 22, 1998 · 14:19 local
Place
Jackson, MS
Airport
Hawkins Field Airport
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9166W
NTSB investigation
NTSBATL98FA053
Reported as
Piper PA28235
Reported engine
Lycoming O540B4B5
People aboard
1
Fatal injuries
1
Pilot’s flight hours
552 total100 in this make and model17 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.

Departed under IFR into IMC. Failed hold heading and alitude. Lost control vertigo and spiral dive to impact. (.4)following a takeoff in low ceilings, rain, and carburetor icing conditions, the pilot failed to maintain the assigned heading, or climb to the assigned altitude. Radar data depicted the airplane executing a meandering flight path, and his radio communications with air traffic were sporadic and ineffectual. Even though the pilot reported reaching his assigned altitude of 4,000 feet, radar data indicated the highest altitude was 2,300 feet. A pilot who departed to search for the reported accident stated he encountered carburetor icing just after takeoff. The carburetor heat valve for the accident airplane was found locked in an intermediate position in the wreckage, and there was evidence of low engine power at impact. Disassembly of the carburetor airbox revealed scrape marks on the interior of the box indicating the carburetor heat valve had been forced toward the warm position by impact forces. The spark plugs exhibited light sooting. The pilot's flight records recorded on three hour instrument flight after he had obtained his instrument rating about seven year s prior to the accident. (-23) investigation continues.

As the FAA filed it

DEPARTED UNDER IFR INTO IMC. FAILED HOLD HEADING AND ALITUDE. LOST CONTROL VERTIGO AND SPIRAL DIVE TO IMPACT. (.4)FOLLOWING A TAKEOFF IN LOW CEILINGS, RAIN, AND CARBURETOR ICING CONDITIONS, THE PILOT FAILED TO MAINTAIN THE ASSIGNED HEADING, OR CLIMB TO THE ASSIGNED ALTITUDE. RADAR DATA DEPICTED THE AIRPLANE EXECUTING A MEANDERING FLIGHT PATH, AND HIS RADIO COMMUNICATIONS WITH AIR TRAFFIC WERE SPORADIC AND INEFFECTUAL. EVEN THOUGH THE PILOT REPORTED REACHING HIS ASSIGNED ALTITUDE OF 4,000 FEET, RADAR DATA INDICATED THE HIGHEST ALTITUDE WAS 2,300 FEET. A PILOT WHO DEPARTED TO SEARCH FOR THE REPORTED ACCIDENT STATED HE ENCOUNTERED CARBURETOR ICING JUST AFTER TAKEOFF. THE CARBURETOR HEAT VALVE FOR THE ACCIDENT AIRPLANE WAS FOUND LOCKED IN AN INTERMEDIATE POSITION IN THE WRECKAGE, AND THERE WAS EVIDENCE OF LOW ENGINE POWER AT IMPACT. DISASSEMBLY OF THE CARBURETOR AIRBOX REVEALED SCRAPE MARKS ON THE INTERIOR OF THE BOX INDICATING THE CARBURETOR HEAT VALVE HAD BEEN FORCED TOWARD THE WARM POSITION BY IMPACT FORCES. THE SPARK PLUGS EXHIBITED LIGHT SOOTING. THE PILOT'S FLIGHT RECORDS RECORDED ON THREE HOUR INSTRUMENT FLIGHT AFTER HE HAD OBTAINED HIS INSTRUMENT RATING ABOUT SEVEN YEAR S PRIOR TO THE ACCIDENT. (-23) INVESTIGATION CONTINUES.

NTSB investigation

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