ERA22LA411

NTSB accident investigation · Cessna 172 · Clearfield, PA · September 3, 2022

Accident · No injuriesClass 3 · LimitedFinal report
Date
September 3, 2022, 16:35 local (20:35 UTC)
Place
Clearfield, PA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N9619HCessna 172
Defining event
Initial climb: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Eastern Region Aviation
Parties
Lycoming Engines, FAA/FSDO
Case key
105921

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

A sudden partial loss of engine power for undetermined reasons, which resulted in an off-airport landing.

Findings · 2

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.

Power plantAircraft › Aircraft power plant · Unknown/Not determinedCessna 172M: 1 caseAll aircraft: 198 casesProbable cause

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

During initial climb, about 300 ft above ground level, the airplane’s engine began shaking and lost partial power. The pilot lowered the nose and saw that the airplane was still over the runway but too close to the end to land on the remaining runway. He made a “hard” left turn in an attempt to land on the runway in the opposite direction. He also turned the fuel selector to off in preparation for an off-airport impact. The engine subsequently lost all power (due to the fuel being turned off), and the airplane impacted a field, coming to rest upright in a wooded area at the edge of the field. A postaccident compression check performed when the engine was cold revealed no compression on the No. 1 cylinder and low compression on the No. 3 cylinder; however, the engine was subsequently started and run at idle power, with no anomalies noted. After shutdown, removal of the Nos. 1 and 3 cylinders revealed scoring on the No. 1 piston skirt and cylinder wall. The scoring was consistent with material entering the cylinder as a result of tappet to camshaft wearing, which also would have affected the intake and exhaust valves opening and closing properly. While this condition may have reduced the engine’s ability to produce full takeoff power; it would not have resulted in the sudden loss of engine performance described by the pilot. Given the engine’s subsequent normal operation postaccident, the reason for the partial loss of engine power could not be determined.

Factual narrative

On September 3, 2022, about 1635 eastern daylight time, a Cessna 172M, N9619H, was substantially damaged when it was involved in an accident near Clearfield, Pennsylvania. The private pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. In a written statement provided to the National Transportation Safety Board, the pilot reported that the airplane had 42 gallons of fuel onboard. He completed a preflight inspection, and the engine run-up was normal. During initial climb, about 300 ft above ground level, the engine began shaking and lost all power. The pilot lowered the nose and saw that the airplane was still over the runway but too close to the end to land on the remaining runway. He then made a “hard” left turn in an attempt to land on the runway in the opposite direction; however, the airplane impacted a field. According to a Federal Aviation Administration (FAA) inspector, the pilot reported that the engine lost partial power, and during the 180° left turn back to the airport, he moved the fuel selector to off in preparation for an off-airport impact. The engine subsequently lost all power, and the airplane impacted a field, coming to rest upright in a wooded area at the edge of the field. The inspector examined the wreckage and observed substantial damage to both wings and the fuselage. After the wreckage was recovered, the FAA inspector further examined the engine and noted no compression on the No. 1 cylinder and 24/80 psi compression on the No. 3 cylinder; however, the compression test was done when the engine was cold. The inspector further stated that he was able to start the engine and run it at idle power, but he did not attempt to increase engine power due to a bent propeller. He subsequently removed the Nos. 1 and 3 cylinders and noted scoring on the No. 1 piston skirt and cylinder wall. The inspector and a representative from the engine manufacturer (who viewed the FAA inspector’s photographs) stated that the scoring was consistent with tappet to camshaft wearing. Review of maintenance records revealed that the most recent annual inspection was completed on August 4, 2022. At that time, the engine had accumulated 1,718 hours since its most recent major overhaul, which was performed in December 2009.

Aircraft

Registration
N9619H
Reported as
Cessna 172 (M)
Category
Airplane
Serial number
17266269
Built
1975
Airframe hours
18,338
Engine
Lycoming O-320-E2D, 150 hp, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · August 4, 2022 · 10 hours before
Destination
HNZ · Henderson, NC
Airport
FIG · Clearfield-Lawrence Airport, runway 30, 4,499 × 75 ft, asphalt
Equipment
Stall warning system, ADS-B

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
56
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Without waivers/limitations
Last flight review
March 6, 2022
Seat
Left
Restraint
3-point
Flight hours
604 total · 91 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 3 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 61 °F
Altimeter
30.22 inHg
Observed at
FIG
METAR
METAR KFIG 022054Z AUTO VRB03KT 10SM CLR 25/16 A3022 RMK AO2 SLP230 T02500156 58006=

Docket · 5

The files NTSB released with the investigation on March 7, 2024, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.6 MB in all.