What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(.19) On January 12, 1999, about 1050 Alaska standard time, a wheel equipped Cessna 207 airplane, N19TA, sustained substantial damage during landing the Chevak Airport, Chevak, Alaska. The airplane was being operated as a visual flight rules (VFR) on-demand cargo/U.S. Mail flight under title 14 CFR part 135, when the accident occurred. The airplane was registered to, and operated by, arctic transportation services, inc., anchorage, Alaska. The solo commercial pilot was not injured. Visual meteorological conditions prevailed, and VFR company flight following procedures were in effect. The flight originated a the bethel airport, bethel, Alaska, about 0947. During a telephone conversation with the national transportation safety board (NTSB) investigator-in-charge on January 12, the pilot reported that during his initial descent to the Chevak Airport,light snow with mixed rain was encountered throughtout the approach phase of the flight. He stated that while on a left base for landing on RUNWAY14, the airplane failed to responded to left control yoke movements. He said that he was able to turn the airplane slowly to the right, 270 degrees from his original heading, and align the airplane for landing on runway 14. He state that while on short final over the threshold of the runway,he again applied left control yoke movement to correct for a 10 to 12 knot, left touched down to the right of the runway, and nosed over. The pilot stated that a postaccident inspeciton revealed ice formation on the airplane's wings, struts, and fuselage. The airplane sustained substantial damage to the wings, and fuselage. The pilot reported the weather conditions at the accident airport as: sky condition and ceilings, indefinite; visibility, 4 statute miles; wind, from the northeast at 10 to 12 knots. Hooper bay, Alaska, is located 18 miles west of the accident site. At 1151, an unaugmented AWOS was reporting, in part: wind, 070 degrees (true) at 16 knots; visibility, 6 statute miles; clouds, 100 feet broken, 1,000 feet overcast; temperature, 19 degrees f; dew point, 15 degrees f; altimeter, 28.68 inhg. (.4) the certificated commercial pilot reported that during his initial descent to the Chevak Airport, the airplane became 'heavy to control' while flying through snow showers mixed with rain. He stated that while on a left base for landing on runway 14, the airplane fail ed to respond to left control yoke movements. He said that he was able to turn the airplane slowly to the right, 270 degrees from his original heading, and align the airplane for landing on runway 14. He stated that while on short final over the threshold of the runway, he again applied left control yoke movement to correct for a 12 to 15 knot, left crosswind. The control movement again failed to have any effect, and the airplane drifted to the right, touched down to the right of the runway, and nosed over. The pilot stated that a postaccident inspection revealed ice formation on the airplane's wings, struts, and fuselage. The airplane sustained substantial damage to the wings and fuselage.
As the FAA filed it
(.19) ON JANUARY 12, 1999, ABOUT 1050 ALASKA STANDARD TIME, A WHEEL EQUIPPED CESSNA 207 AIRPLANE, N19TA, SUSTAINED SUBSTANTIAL DAMAGE DURING LANDING THE CHEVAK AIRPORT, CHEVAK, ALASKA. THE AIRPLANE WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) ON-DEMAND CARGO/U.S. MAIL FLIGHT UNDER TITLE 14 CFR PART 135, WHEN THE ACCIDENT OCCURRED. THE AIRPLANE WAS REGISTERED TO, AND OPERATED BY, ARCTIC TRANSPORTATION SERVICES, INC., ANCHORAGE, ALASKA. THE SOLO COMMERCIAL PILOT WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND VFR COMPANY FLIGHT FOLLOWING PROCEDURES WERE IN EFFECT. THE FLIGHT ORIGINATED A THE BETHEL AIRPORT, BETHEL, ALASKA, ABOUT 0947. DURING A TELEPHONE CONVERSATION WITH THE NATIONAL TRANSPORTATION SAFETY BOARD (NTSB) INVESTIGATOR-IN-CHARGE ON JANUARY 12, THE PILOT REPORTED THAT DURING HIS INITIAL DESCENT TO THE CHEVAK AIRPORT,LIGHT SNOW WITH MIXED RAIN WAS ENCOUNTERED THROUGHTOUT THE APPROACH PHASE OF THE FLIGHT. HE STATED THAT WHILE ON A LEFT BASE FOR LANDING ON RUNWAY14, THE AIRPLANE FAILED TO RESPONDED TO LEFT CONTROL YOKE MOVEMENTS. HE SAID THAT HE WAS ABLE TO TURN THE AIRPLANE SLOWLY TO THE RIGHT, 270 DEGREES FROM HIS ORIGINAL HEADING, AND ALIGN THE AIRPLANE FOR LANDING ON RUNWAY 14. HE STATE THAT WHILE ON SHORT FINAL OVER THE THRESHOLD OF THE RUNWAY,HE AGAIN APPLIED LEFT CONTROL YOKE MOVEMENT TO CORRECT FOR A 10 TO 12 KNOT, LEFT TOUCHED DOWN TO THE RIGHT OF THE RUNWAY, AND NOSED OVER. THE PILOT STATED THAT A POSTACCIDENT INSPECITON REVEALED ICE FORMATION ON THE AIRPLANE'S WINGS, STRUTS, AND FUSELAGE. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE TO THE WINGS, AND FUSELAGE. THE PILOT REPORTED THE WEATHER CONDITIONS AT THE ACCIDENT AIRPORT AS: SKY CONDITION AND CEILINGS, INDEFINITE; VISIBILITY, 4 STATUTE MILES; WIND, FROM THE NORTHEAST AT 10 TO 12 KNOTS. HOOPER BAY, ALASKA, IS LOCATED 18 MILES WEST OF THE ACCIDENT SITE. AT 1151, AN UNAUGMENTED AWOS WAS REPORTING, IN PART: WIND, 070 DEGREES (TRUE) AT 16 KNOTS; VISIBILITY, 6 STATUTE MILES; CLOUDS, 100 FEET BROKEN, 1,000 FEET OVERCAST; TEMPERATURE, 19 DEGREES F; DEW POINT, 15 DEGREES F; ALTIMETER, 28.68 INHG. (.4) THE CERTIFICATED COMMERCIAL PILOT REPORTED THAT DURING HIS INITIAL DESCENT TO THE CHEVAK AIRPORT, THE AIRPLANE BECAME 'HEAVY TO CONTROL' WHILE FLYING THROUGH SNOW SHOWERS MIXED WITH RAIN. HE STATED THAT WHILE ON A LEFT BASE FOR LANDING ON RUNWAY 14, THE AIRPLANE FAIL ED TO RESPOND TO LEFT CONTROL YOKE MOVEMENTS. HE SAID THAT HE WAS ABLE TO TURN THE AIRPLANE SLOWLY TO THE RIGHT, 270 DEGREES FROM HIS ORIGINAL HEADING, AND ALIGN THE AIRPLANE FOR LANDING ON RUNWAY 14. HE STATED THAT WHILE ON SHORT FINAL OVER THE THRESHOLD OF THE RUNWAY, HE AGAIN APPLIED LEFT CONTROL YOKE MOVEMENT TO CORRECT FOR A 12 TO 15 KNOT, LEFT CROSSWIND. THE CONTROL MOVEMENT AGAIN FAILED TO HAVE ANY EFFECT, AND THE AIRPLANE DRIFTED TO THE RIGHT, TOUCHED DOWN TO THE RIGHT OF THE RUNWAY, AND NOSED OVER. THE PILOT STATED THAT A POSTACCIDENT INSPECTION REVEALED ICE FORMATION ON THE AIRPLANE'S WINGS, STRUTS, AND FUSELAGE. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE TO THE WINGS AND FUSELAGE.
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 N19TA · 1
Matched to the same aircraft by N-number and date.