# Accident 19991116032169A: Cessna 207A, Dillingham, AK, November 16, 1999 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: November 16, 1999, 10:20 local time - Place: Dillingham, AK - Airport: Dillingham - Damage: Substantial damage - Phase of flight: Climb - Operating rules: Air taxi and commuter (Part 135) - Operator: YAAA - Location: 58.8197° N, 157.8608° W: From the FAA, an estimate near the named town, within about 3 miles - Nearby events: https://openairdocs.org/map.md?lat=58.8197&lon=-157.8608&mi=10 - Aircraft: N9933M, registered now (https://openairdocs.org/aircraft/N9933M) (OpenAirDocs) - Registry model: Cessna 207A (registry code 2073605, https://openairdocs.org/model/cessna-207a) (OpenAirDocs) - Registry engine: Continental IO-520-F (registry code 17237, https://openairdocs.org/engine/continental-io-520-f) (OpenAirDocs) - Reported make and model: CESSNA 207A - Reported engine: CONT IO520F - Fatal injuries: 0 - Pilot flight hours: 2,445 total, 1,296 in this make and model, 265 in the last 90 days - NTSB investigation: [NTSB ANC00LA015](https://openairdocs.org/ntsb/ANC00LA015) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/19991116032169A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (.19) ON NOVEMBER 16, 1999, AT 1020 ALASKA STANDARD TIME, A CESSNA 207A AIRPLANE, N9933M, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT IMPACTED TERRAIN WEST OF RUNWAY 01 DURING TAKEOFF FROM THE DILLINGHAM AIRPORT, DILLINGHAM, ALASKA. THE SOLO COMMERCIAL PILOT RECEIVED MINOR INJURIES. THE FLIGHT WAS OPERATED BY YUTE AIR ALASKA, INC., OF ANCHORAGE, ALASKA, UNDER 14 CFR PART 135 AS A CARGO AND MAIL FLIGHT TO NEW STUYAHOK, ALASKA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT, AND A COMPANY VFR FLIGHT PLAN WAS IN EFFECT. DURING A TELEPHONE INTERVIEW WITH THE NTSB IIC ON NOVEMBER 17, THE PILOT STATED THAT HE TAXIED TO THE END OF THE 6,404 FEET LONG BY 150 FEET WIDE RUNWAY, AND MADE A FULL LENGTH TAKEOFF. HE SAID THE PRETAKEOFF ENGINE RUNUP WAS NORMAL, AS WAS THE TAKEOFF RUN AND LIFTOFF. HE INDICATED THAT ABOUT 30 FEET ABOVE THE GROUND, THE ENGINE "MISSED, QUIVERED, AND LOST POWER." HE SAID THE AIRPLANE DRIFTED TO THE LEFT OF THE RUNWAY, HE WAS NOT ABLE TO GET BACK OVER THE ASPHALT BEFORE CONTACTING THE GROUND, SO HE LEVELED THE WINGS AND LANDED. THE NOSE LANDING GEAR BROKE OFF, AND THE AIRPLANE NOSED OVER. HE TOLD THE NTSB IIC THAT THE CARGO LOAD WAS 1,100 POUN DS, AND THE AIRPLANE CONTAINED ABOUT 1/2 OF A FULL FUEL LOAD. THE NTSB IIC ESTIMATED THE TAKEOFF WEIGHT BETWEEN 3,700 POUNDS AND 3,800 POUNDS. THE MAXIMUM ALLOWABLE TAKEOFF WEIGHT FOR THE CESSNA 207A IS 3,800 POUNDS. THE ACCIDENT FLIGHT WAS THE FIRST FLIGHT SINCE THE ENGINE AND PROPELLER ASSEMBLY WAS REPLACED. THE ENGINE HAD BEEN GROUND RUN, BUT NOT FLOWN SINCE INSTALLATION ON THIS AIRPLANE. THE ENGINE HAD ABOUT 800 HOURS SINCE OVERHAUL, AND ABOUT 5 HOURS IN OPERATION ON A DIFFERENT AIRPLANE SINCE A TEARDOWN INSPECTION FOR A PROPELLER STRIKE. THE WEATHER OBSERVATION FOR DILLINGHAM AT 0950 WAS, WIND FROM 040 DEGREES AT 5 KNOTS, 20 MILES VISIBILITY, A CEILING OF 1,000 FEET OVERCAST, A TEMPERATURE OF 7 DEGREES FAHRENHEIT, AND A DEW POINT OF 3 DEGREES FAHRENHEIT. (-23) DURING TAKEOFF THE PILOT REPORTED THAT ABOUT 30 FEET ABOVE THE GROUND THE ENGINE MISSED, QUIVERED, AND LOST POWER, UPON LANDING THE NOSE GEAR BROKE OFF AND THE AIRCRAFT FLIPPED OVER. WAITING SHIPMENT TO ANCHORAGE TO RUN ENGINE. (.4) AFTER TAKEOFF THE AIRPLANE DID NOT CLIMB ABOVE 30 FEET, DRIFTED LEFT OF THE RUNWAY, AND SETTLED ONTO THE GROUND. THE PILOT STATED THE ENGINE 'MISSED, QUIVERED, AND LOST POWER.' HE ALSO STATED THERE WAS LIGHT FROST ON THE AIRPLANE, BUT THAT OTHER SMALL AIRPLANES HAD DEPARTED WITH SIMILAR FROST. THE ENGINE HAD BEEN INSTALLED ON THE AIRPLANE THE DAY PRIOR TO THE ACCIDENT, AND HAD BEEN OPERATED ON THE GROUND, BUT NOT FLOWN. AFTER THE ACCIDENT, AN UNDAMAGED PROPELLER WAS INSTALLED, AND THE ENGINE WAS OPERATED AT 1,000 RPM FOR 4 MINUTES. THE ENGINE-DRIVEN FUEL PUMP, FUEL CONTROLLER, AND FUEL DISTRIBUTOR AND NOZZLES WERE TESTED. THESE COMPONENTS ALL PRODUCED THE NORMAL FUEL FLOWS AND PRESSURES SPECIFIED BY THE MANUFACTURER. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ANC00LA015](https://openairdocs.org/ntsb/ANC00LA015), Nov 16, 1999: Cessna 207A (N9933M), Dillingham, AK, substantial damage. Probable cause: Failure of the pilot to remove frost from the wings prior to flight, and the resulting inadvertent stall/mush. From the FAA Accident/Incident Data System. Reports are matched to registry aircraft 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. For accidents, the NTSB's own investigation is the fuller record. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.