CESSNA 172M near New Castle, VA — 2013-04-07
- Date
- 2013-04-07
- Location
- New Castle, VA, USA
- Airport
- VA85
- Aircraft
- CESSNA 172M
- Registration
- N92804
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Takeoff roll
Probable cause
The pilot's failure to abort the takeoff after recognizing that the airplane was not accelerating properly, which led to an aerodynamic stall. The reason for the lack of acceleration could not be determined because postaccident examinations did not reveal any anomalies that would have precluded normal operation.
NTSB narrative
The pilot reported that, before departure, he performed an engine run-up and then initiated takeoff from the 2,400-foot-long upsloping grass runway in accordance with soft-field takeoff procedures. The airplane was slow to produce speed; but, it lifted off the ground. Although the pilot attempted to fly in ground effect to produce more speed, he soon realized that he did not have enough speed or altitude to clear trees beyond the runway, so he maneuvered the airplane toward a clearing where he intended to land the airplane. However, the airplane then stalled, the left wing tip contacted the ground, and the airplane cart-wheeled. The pilot further reported that he should have recognized the "sluggish speed sooner and [aborted the] takeoff." Examinations revealed that the magnetos were slightly out of timing and that both of the No. 2 cylinder's spark plugs contained lead and carbon deposits; however, it could not be determined how this affected engine power or whether these conditions would have been noticeable to the pilot during the engine run-up before departure or during the takeoff. Examinations revealed no anomalies that could have precluded normal operation. Postaccident performance calculations indicate that, based on the airplane's weight, the reported headwind component, and takeoff from a grass runway, the total distance to clear a 50-foot obstacle was 914 feet; therefore, the pilot should have been able to clear the trees.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot should have aborted takeoff due to sluggish speed sooner.
NTSB coding
Evidence available
- Photos
- 17 docket documents
Docket documents17
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15, and Evidence Control Formform
- E-mail Statement from NTSB Chemist Nancy McAtee Regarding Inspection of the Upper and Lower Spark Plugs from the No. 2 Cylinder.interview
- FAA Inspector Statement Concerning Engine Examinationinterview
- Statement from Mechanic Concerning Inspection of the No. 2 Cylinder Assembly.interview
- Statement from Pilot who Flew the Accident Airplane Lastinterview
- Excerpts from Engine Logbookother
- Excerpts from Owner's Manualother
- Photo 1: Digital Photograph Provided by FAA. Captioning Provided by Unknown Source. View Taken South of the Departure End of Runway 18, Looking North.photos
- Photo 2: Digital Photograph Provided by FAA. View Taken Following Recovery. Note the Damage at Each Wingtip, and the Separated Nose Landing Gear.photos
- Photo 3: Digital Photograph Provided by FAA. View Taken Following Recovery. Note the Structural Damage Aft of the Engine Firewall.photos
- Photo 4: Digital Photograph Provided by FAA. View Taken Following Recovery. Note the Structural Damage to Both Wings.photos
- Photo 5: Digital Photograph Provided by FAA. View of the Lower Spark Plug of the No. 2 Cylinder.photos
- Photo 6: Digital Photograph Provided by FAA. View of the Upper Spark Plug of the No. 2 Cylinder.photos
- Photo 7: Digital Photograph Provided by the Airplane Operator. View of the No. 2 Cylinder Piston Following Removal of the Cylinder.photos
- Photo 8: Digital Photograph Provided by the Airplane Operator. View of the Interior of the No. 2 Cylinder.photos
- Weather Reports and Recordsreport
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