# NTSB LAX05LA317: Cessna A185F, N8548Q, Tracy, CA, September 26, 2005 - Type: NTSB accident investigation - Classification: Accident · No injuries · Limited investigation · Final report - Date: September 26, 2005, 12:46 local (19:46 UTC) - Place: Tracy, CA - Coordinates: 37.693054, -121.447502 - Nearby events: https://openairdocs.org/map.md?lat=37.6931&lon=-121.4475&mi=10 - Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping) - Highest injury: No injuries - Injuries: 4 uninjured - Status: Completed, report February 26, 2007 - Report: Approved by Office Director - Parties: Federal Aviation Administration - NTSB case key (mKey): 62564 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=LAX05LA317 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/62564/pdf - Page: https://openairdocs.org/ntsb/LAX05LA317 ## Probable cause loss of engine power for undetermined reasons. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of engine power, takeoff - initial climb - reason for occurrence undetermined (cause) - Forced landing, emergency landing after takeoff - Dragged wing,rotor,pod,float or tail/skid, emergency landing - wing,wingtip - Hard landing, emergency landing - landing gear,main gear - collapsed ## Analysis During the takeoff initial climb the engine experienced a partial loss of power and the landing gear collapsed during an ensuing off-airport forced landing in an open field. Upon arriving at the airport, the pilot conducted a preflight inspection, which included checking the fuel tanks for contamination. No discrepancies were noted with the preflight inspection, start-up, taxi to the active runway, or run-up. Shortly after takeoff the pilot reduced the throttle and revolutions per minute (rpm) to 25 inches of manifold pressure (MAP) and 2,500 rpm for best rate of climb. Shortly after that the pilot noticed that the climb performance was substandard and decaying, and the engine seemed to have a reduced power output. Due to the marginal climb performance and decaying power state of the engine, the pilot decided to land in an open field. During a turn to remain over the intended landing site, the engine started to misfire. Engine power continued to decay even though the throttle was full forward, mixture set at rich, and the fuel selector was selected to BOTH. While on downwind he noted obstructions at the end of his intended landing site. At the current rate of descent, he believed that the airplane would overrun the field and impact the obstructions. He lowered the flaps to 20 degrees and initiated a left 90-degree turn for a clearer area in which to land. During the flare, the left wing tip impacted the ground first, the airplane bounced, and when it touched down again, the right main landing gear collapsed. A post accident inspection and ground run of the engine was conducted by a Federal Aviation Administration inspector with no preimpact mechanical anomalies identified that would have precluded normal operation. ## Factual narrative On September 26, 2005, at 1246 Pacific daylight time, a Cessna A185F, N8548Q, collapsed the landing gear during a forced landing in an open field near Tracy, California. The pilot/owner operated the airplane under the provisions of 14 CFR Part 91 as a personal cross-country flight. The airplane sustained substantial damage. The certificated airline transport pilot (ATP) and three passengers were not injured. The flight departed Tracy Municipal Airport (TCY), Tracy, about 1240, and was destined for Corvallis, Oregon. Visual meteorological conditions prevailed for the flight and no flight plan had been filed. According to the pilot, he conducted a preflight inspection of the accident airplane that included the sumping of all four fuel tanks, as well as the low points for water contamination. No discrepancies were noted. He checked the weather prior to departure and noted no significant weather anomalies. The startup and taxi to runway 30 were uneventful. He indicated that he had to wait to for the oil temperature to rise before conducting the engine run-up; there were no discrepancies noted with the engine run-up, the takeoff roll or initial climb performance. About 300 feet above ground level (agl), the pilot reduced the throttle and rpm's (revolutions per minute) to 25 inches of manifold pressure (MAP) and 2,500 rpm. The pilot reported that at that point climb performance "seemed to lag, despite checks and adjustments to ensure 25/25." He reported that the climb performance was marginal and he decided to land in an open field. He noted a maximum altitude gain of 400 feet above agl. The pilot reported that he made a left 180-degree turn to remain over a cropless field, and at that point the engine started to misfire. The pilot indicated that the airplane was configured with all power levers full forward, mixture was rich, fuel selector was selected to BOTH; however, the power began to decay. With only partial engine power, he setup for the emergency landing at an airspeed of 75 knots and no flaps. While on downwind he noted farm equipment and telephone lines, and believed at his current rate of descent he would overrun the field and impact those items. He lowered the flaps to 20 degrees and started a left 90-degree turn for a more clear area. The pilot believed that the airplane was level when it contacted the ground; however, while out in the field he noted that the left wing tip impacted first. The airplane bounced once, and on the second touchdown the right main landing gear collapsed, the nose skidded to the left, and the right wing and strut contacted the ground opening the right door. After coming to a stop, the pilot checked that the passengers were OK, and noted a fuel leak from the right main wing tank. Upon securing the airplane, the pilot and passengers exited the airplane. The Federal Aviation Administration (FAA) accident coordinator inspected the engine and noted no obvious mechanical malfunctions. He performed an engine ground run, which was normal, and could not reproduce the loss of engine power. ## Aircraft - Registration: [N8548Q](https://openairdocs.org/aircraft/N8548Q), registered now, S/N 18503730, built 1978 (OpenAirDocs) - Reported make and model: Cessna A185F - Registry model: [Cessna A185F](https://openairdocs.org/model/cessna-a185f) (registry code 2072821) (OpenAirDocs) - Registry engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 18503730 - Airframe hours: 3415 - Engines: Teledyne Continental IO-520-D 300 horsepower reciprocating - Damage: Substantial damage - Flight: Personal, Part 91 - Registered owner: John S. Wood - Airworthiness certificate: Standard, Normal - Last inspection: Annual, January 1, 2005, 55 hours before - Departed: TCY, Tracy, CA - Destination: CVO, Corvallis, OR - Airport: TCY, Tracy Municipal Airport, runway 30, 4,001 × 100 ft, asphalt ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 55; injuries: none; flight instructor, commercial, flight engineer, airline transport; airplane ratings: single-engine land, single-engine sea, multi-engine land; instrument ratings: airplane; medical: class 1; last flight review April 1, 2005; seat: left; flight hours: 18,505 total, 58 in this make and model, 14,711 as pilot in command, 245 in the last 90 days, 49 in the last 30 days, 1 in the last 24 hours ## Weather - Conditions: Visual (VMC), Day - Wind: 130° at 9 knots - Visibility: 10 statute miles - Lowest ceiling: none - Temperature: 86 °F, dew point 46 °F - Altimeter: 29.89 inHg - Observed at: SCK, 16 nm away ## 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 20050926022749A](https://openairdocs.org/incident/20050926022749A), Sep 26, 2005: Cessna A185F, Tracy, CA, Substantial damage. (-23) After take off from tcy, CA, runway 30, Cessna 185 pilot reported loss of engine power. Power loss occurred approximately 1 mile after take off, at 400… 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.