# NTSB ANC95LA052: Cessna 205, N8312Z, Anchorage, AK, May 4, 1995 - Type: NTSB accident investigation - Classification: Accident · No injuries · Limited investigation · Final report - Date: May 3, 1995, 21:15 local (May 4, 1995, 05:15 UTC) - Place: Anchorage, AK - Coordinates: 61.159137, -149.990814 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=61.1591&lon=-149.9908&mi=10 - Phase of flight: [Maneuvering](https://openairdocs.org/ntsb-phases/450) (OpenAirDocs' grouping) - Highest injury: No injuries - Injuries: 4 uninjured - Status: Completed, report November 8, 1995 - Report: Approved by Office Director - NTSB office: Alaska Regional Office - NTSB case key (mKey): 2647 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=ANC95LA052 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/2647/pdf - Page: https://openairdocs.org/ntsb/ANC95LA052 ## Probable cause A FAILURE OF THE ENGINE DRIVEN FUEL PUMP. FACTORS IN THE ACCIDENT WERE THE PILOTS' INADEQUATE IN-FLIGHT PLANNING AND UNSUITABLE TERRAIN IN THE AREA OF THE FORCED LANDING. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of engine power(partial) - mech failure/malf, maneuvering - emergency procedure - simulated, pilot passenger - in-flight planning/decision - inadequate, pilot in command (contributing factor) - go-around - initiated, pilot in command - fuel system,pump - seized (cause) - In flight collision with object, maneuvering - terrain condition - none suitable (contributing factor) - object - tree(s) ## Analysis A CERTIFICATED COMMERCIAL/CFI PILOT WAS RECEIVING AN AIRPLANE CHECKOUT FROM THE OWNER/PILOT PRIOR TO RENTING THE AIRPLANE. THE OWNER REDUCED THE ENGINE POWER TO IDLE TO SIMULATE AN ENGINE FAILURE AND FORCED LANDING. THE AREA CONSISTED OF OPEN AREAS OF SOFT TUNDRA MUSKEG AND TALL SPRUCE TREES. THE PILOT MANEUVERED THE AIRPLANE TOWARD A PROSPECTIVE LANDING AREA AND DESCENDED TO ABOUT 300 TO 500 FEET AGL. THE PILOT INITIATED A GO-AROUND AND ADVANCED THE THROTTLE TO BEGIN A CLIMB, BUT THE ENGINE DID NOT RESPOND. EMERGENCY PROCEDURES BY BOTH PILOTS DID NOT RESTORE ENGINE POWER. THE AIRPLANE CONTINUED TO DESCEND AND COLLIDED WITH TREES. A POSTACCIDENT EXAMINATION OF ENGINE REVEALED THAT THE ENGINE DRIVEN FUEL PUMP HAD FAILED. ## Factual narrative On May 3, 1995, about 2115 hours Alaska daylight time, a wheel equipped Cessna 205, N8312Z, collided with trees during a simulated forced landing, about 10 miles north of Anchorage, Alaska. The airplane was being operated as a visual flight rules (VFR) local area flight when the accident occurred. The airplane, owned and operated by the second pilot, was destroyed. The certificated commercial pilot (first pilot), the second pilot, and two passengers were not injured. Visual meteorological conditions prevailed. The flight originated at Merrill Field, Anchorage, Alaska, about 2100 hours. The first pilot reported that he was receiving a check-out in the aircraft from the second pilot prior to renting the airplane. After a series of aerial maneuvers, the second pilot reduced the throttle to idle for a simulated engine failure. The terrain consisted of open areas of soft tundra muskeg, surrounded by tall spruce trees. The first pilot maneuvered the airplane toward a clearing and about 300 to 500 feet above the ground, advanced the throttle to full power. The engine did not respond with sufficient power to begin a climb. The second pilot began performing emergency checklist items while the first pilot continued to fly. The airplane struck several trees and came to rest about 1 1/2 miles south of the Goose Bay airstrip. A Federal Aviation Administration (FAA) airworthiness inspector, Anchorage Flight Standards District Office (FSDO), examined the airplane at the accident site. He reported that the left wing was torn off the airplane and the aircraft received damage to the right wing and fuselage. After recovery and removal from the airframe, the airplane's engine was examined at T and B Aircraft, Anchorage, Alaska. A mechanic noted that the mechanical fuel pump shaft was frozen and the drive shaft coupling was fractured. The engine had accrued a total time of 4,094.34 hours of operation. It had accrued 2,594.34 hours since a major overhaul on April 6, 1973. The engine manufacturer's recommended time between overhaul (TBO) is 1,500 hours. An annual inspection was performed on June 28, 1994, 74 hours prior to the accident. The fuel pump was last overhauled on June 30, 1988. The fuel pump's total time in service is unknown. There is no recommended TBO criteria for the fuel pump. The engine driven fuel pump was submitted to the National Transportation Safety Board's, Materials Laboratory Division for examination. The examination revealed rotational smearing and scoring on the internal face of the pump thrust plate. Scoring was noted on the internal surface of the pump housing, adjacent to the mating surface end of the 2 internal pump vanes. The vanes rest in 2 slots at the end of the rotating shaft and slide laterally within the slot. One vane was frozen within its shaft slot. A small particle of metal was found wedged between the edge of the immobile pump vane and its adjacent shaft slot surface. Additional flakes of metal were smeared over the top surface of the immobile vane, adjacent to the mating surface of the thrust plate. The examination of the shaft coupling revealed that the pressure side of each drive spline tooth was indented and plastically deformed. ## Aircraft - Registration: [N8312Z](https://openairdocs.org/deregistered/N8312Z-1997-03-19), registration cancelled 1997-03-19, S/N 2050312 (OpenAirDocs) - Reported make and model: CESSNA 205 - Registry model: [Cessna 210-5(205)](https://openairdocs.org/model/cessna-210-5-205) (registry code 2073202) (OpenAirDocs) - Category: Airplane - Serial number: 2050312 - Airframe hours: 4220 - Engines: CONTINENTAL IO-470-S 260 horsepower reciprocating - Damage: Destroyed - Flight: Personal, Part 91 - Registered owner: William H. Merrill Jr. - Airworthiness certificate: Standard, Normal - Last inspection: 100 hour, June 28, 1994, 74 hours before - Departed: MRI ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 34; commercial, flight instructor; airplane ratings: multi-engine land, single-engine land; instrument ratings: airplane; medical: class 2, valid medical--w/ waivers/lim; seat: left; flight hours: 1,900 total, 1,730 as pilot in command, 50 in the last 90 days, 15 in the last 30 days ## Weather - Conditions: Visual (VMC), Dusk - Wind: 60° at 8 knots - Visibility: 90 statute miles - Lowest ceiling: 5,000 ft overcast - Temperature: 61 °F - Altimeter: 29.00 inHg ## FAA reports on this event (1) The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs). - [Accident 19950503009239A](https://openairdocs.org/incident/19950503009239A), May 3, 1995: Cessna 2105, Anchorage, AK, Destroyed. Simulated forced landing during checkout. Engine failed on go around. Hit trees. Fuel pump siezed. Engine over tbo. 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. --- 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.