19980206002389A

Accident · Destroyed

FAA accident report · Cessna T207 · Homer, AK · February 6, 1998

Date
February 6, 1998 · 12:45 local
Place
Homer, AK
Airport
Homer Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
Air taxi and commuter (Part 135)
Operator
SOCA
Damage
Destroyed
Aircraft
N91029
NTSB investigation
NTSBANC98FA019
Reported as
Cessna T207
Reported engine
Continental IO520F
People aboard
1
Fatal injuries
1
Pilot’s flight hours
1,358 total48 in this make and model191 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.

Aircraft climbed to 150 ft AGL on takeoff. Banked into steep turn and dove into snow covered ground. (.4)the certificated commercial pilot was departing on a 14 CFR 135 cargo flight. The airplane lifted off and climbed to about 200 feet. Instead of turning right toward the intended destination, the airplane began a left turn toward the runway. The angle of bank increased to about 45 degrees. The airplane then nosed down, and descended into snow covered terrain, about 200 yards north of the runway. Examination of the engine revaled the number six sylinder head was fractured, and slightly separated from the sylinder barrel. The area around the point of separation was blackened and oily. Wimilar discoloration was noted on the inside of the engine cowl. A metallurgical examination of the cylinder head revealed a fatigue fracture along a large segment of the thread root radius between the 5th and 6th threads. The engine's cylinder compression is part of the operator's approved airworthiness inspection program. The number six sylinder compression, recorded 121 hours before the accident, was noted as 60 PSI. The last engine inspection, 27 hours before the accident, did not in clude a record of the engine compression. (-23) no narrative.

As the FAA filed it

AIRCRAFT CLIMBED TO 150 FT AGL ON TAKEOFF. BANKED INTO STEEP TURN AND DOVE INTO SNOW COVERED GROUND. (.4)THE CERTIFICATED COMMERCIAL PILOT WAS DEPARTING ON A 14 CFR 135 CARGO FLIGHT. THE AIRPLANE LIFTED OFF AND CLIMBED TO ABOUT 200 FEET. INSTEAD OF TURNING RIGHT TOWARD THE INTENDED DESTINATION, THE AIRPLANE BEGAN A LEFT TURN TOWARD THE RUNWAY. THE ANGLE OF BANK INCREASED TO ABOUT 45 DEGREES. THE AIRPLANE THEN NOSED DOWN, AND DESCENDED INTO SNOW COVERED TERRAIN, ABOUT 200 YARDS NORTH OF THE RUNWAY. EXAMINATION OF THE ENGINE REVALED THE NUMBER SIX SYLINDER HEAD WAS FRACTURED, AND SLIGHTLY SEPARATED FROM THE SYLINDER BARREL. THE AREA AROUND THE POINT OF SEPARATION WAS BLACKENED AND OILY. WIMILAR DISCOLORATION WAS NOTED ON THE INSIDE OF THE ENGINE COWL. A METALLURGICAL EXAMINATION OF THE CYLINDER HEAD REVEALED A FATIGUE FRACTURE ALONG A LARGE SEGMENT OF THE THREAD ROOT RADIUS BETWEEN THE 5TH AND 6TH THREADS. THE ENGINE'S CYLINDER COMPRESSION IS PART OF THE OPERATOR'S APPROVED AIRWORTHINESS INSPECTION PROGRAM. THE NUMBER SIX SYLINDER COMPRESSION, RECORDED 121 HOURS BEFORE THE ACCIDENT, WAS NOTED AS 60 PSI. THE LAST ENGINE INSPECTION, 27 HOURS BEFORE THE ACCIDENT, DID NOT IN CLUDE A RECORD OF THE ENGINE COMPRESSION. (-23) NO NARRATIVE.

NTSB investigation

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

Other reports on N91029 · 4

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