- Date
- October 5, 2014, 10:30 local (17:30 UTC)
- Place
- Sedona, AZ
- Injuries
- 1 minor
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N2179LCessna 172S
- Defining event
- Landing-landing roll: Loss of control on ground
- Weather
- Visual (VMC) · Day
- Status
- Completed · report December 5, 2014
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- FAA report
- 20141005019399A
- Case key
- 90221
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The pilot's failure to maintain airplane control during the landing roll out.
Findings · 3
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot stated that he was on an extended final for landing. As he got closer to the runway, he noted that he was right of centerline, and made corrections to return to the runway centerline for landing. The pilot indicated that he was still making corrections as he initiated the flare to land. The flare was too high, and as a result, the airplane developed a greater than desired sink rate, which he corrected by adding power. The pilot stated that the landing was firmer than normal, and the airplane bounced before it settled back to the runway. The pilot looked inside the cockpit to retract the flaps and reduce the power to idle. When he looked back outside, the airplane was pointed off the runway. The pilot added right rudder to correct back to the runway. He did not want to add too much rudder and lose airplane control, and when he went to apply the brakes, he noted that his feet were too far down the rudder pedals, so there was no braking action. The airplane departed the runway surface, and traveled onto the grass, toward a ditch. As the airplane traversed through the ditch, the nose landing gear collapsed, the propeller struck the ground, and then the airplane came to rest inverted. The airplane sustained substantial damage to right wing, rudder, and vertical stabilizer. The pilot reported that there were no mechanical malfunctions with the airplane that would have precluded normal operation. In the Recommendation (how could this accident/incident have been prevented) section of the accident report, the pilot reported that the flight school has changed their policy, and no longer allows solo students to fly to the accident airport. He further reported that if he had ensured positive aircraft control prior to retracting the flaps, or taking his attention away from the landing, the airplane would not have yawed to the side of the runway.
Factual narrative
The pilot stated that he was on an extended final for landing. As he got closer to the runway, he noted that he was right of centerline, and made corrections to return to the runway centerline for landing. The pilot indicated that he was still making corrections as he initiated the flare to land. The flare was too high, and as a result, the airplane developed a greater than desired sink rate, which he corrected by adding power. The pilot stated that the landing was firmer than normal, and the airplane bounced before it settled back to the runway. The pilot looked inside the cockpit to retract the flaps and reduce the power to idle. When he looked back outside, the airplane was pointed off the runway. The pilot added right rudder to correct back to the runway. He did not want to add too much rudder and lose airplane control, and when he went to apply the brakes, he noted that his feet were too far down the rudder pedals, so there was no braking action. The airplane departed the runway surface, and traveled onto the grass, toward a ditch. As the airplane traversed through the ditch, the nose landing gear collapsed, the propeller struck the ground, and then the airplane came to rest inverted. The airplane sustained substantial damage to right wing, rudder, and vertical stabilizer. The pilot reported that there were no mechanical malfunctions with the airplane that would have precluded normal operation. In the Recommendation (how could this accident/incident have been prevented) section of the accident report, the pilot reported that the flight school has changed their policy, and no longer allows solo students to fly to the accident airport. He further reported that if he had ensured positive aircraft control prior to retracting the flaps, or taking his attention away from the landing, the airplane would not have yawed to the side of the runway.
Aircraft
- Registration
- N2179L
- Reported as
- Cessna 172S
- Category
- Airplane
- Serial number
- 172S9633
- Built
- 2004
- Airframe hours
- 7,558
- Engine
- Lycoming IO-360-L2A, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Operator
- Northern Arizona Investment Group LLC
- Registered owner
- Northern Arizona Investment Group LLC
- Airworthiness certificate
- Certificate of authorization or waiver (COA)
- Last inspection
- 100 hour · September 15, 2014 · 50 hours before
- Departed
- PRC · Prescott, AZ
- Destination
- SEZ · Sedona, AZ
- Airport
- SEZ · Sedona, runway 03, 5,132 × 100 ft, asphalt
- Equipment
- Electronic flight bag or handheld device, Data recorder, Auto-pilot, Angle of attack indicator, Airframe parachute, ADS-B, Video recording device, Stall warning system, Onboard weather, Heads up display, Electronic primary flight display, Handheld GPS
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 29
- Injuries
- Minor
- Certificates
- Flight instructor, Commercial
- Instrument ratings
- Helicopter
- Medical
- Class 2, Without waivers/limitations
- Last flight review
- April 15, 2014
- Seat
- Left
- Restraint
- 3-point
- Flight hours
- 403 total · 22 in this make and model
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- Variable at 5 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 64 °F, dew point 27 °F
- Altimeter
- 30.29 inHg
- Observed at
- KFLG, 19 nm away
Docket · 2
The files NTSB released with the investigation on November 20, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.3 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.
Other investigations on N2179L · 1
Matched to the same aircraft by N-number and date.