ASN Wikibase Occurrence # 351337
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Date: | Sunday 29 May 2022 |
Time: | 16:27 LT |
Type: | Piper PA-28RT-201T |
Owner/operator: | |
Registration: | N2148J |
MSN: | 28R-7931012 |
Year of manufacture: | 1978 |
Total airframe hrs: | 3804 hours |
Engine model: | Continental TSIO 360FB |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Morgan, Texas -
United States of America
|
Phase: | En route |
Nature: | Private |
Departure airport: | Pampa-Perry Lefors Field, TX (PPA/KPPA) |
Destination airport: | Houston Southwest Airport, TX (KAXH) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:While in cruise flight, the pilot observed the manifold pressure drop, followed by a loud rattling engine noise with strong vibrations. The pilot shut down the engine and diverted toward a nearby airport. The pilot reported that he thought the airplane was too high on the downwind leg; however, after he turned the airplane onto the final leg, he realized that the headwind would prevent him from making it to the runway. The pilot performed a forced landing into rough terrain short of the runway, which resulted in substantial damage to the right wing.
Postaccident examination of the No. 3 cylinder revealed the cylinder barrel was fractured between the cooling fins and the threaded section used for mounting the cylinder head. A metallurgical examination revealed a fatigue crack that originated at a corrosion pit on the outer diameter surface of the cylinder barrel.
The inboard-facing side of the first cylinder cooling fin was tinted black for a 180° arc, with the center of the arc in line with the fatigue crack. Manufacturer guidance includes inspection of cylinder fins for any signs of oil or soot leakage that might indicate a cylinder or head-to-barrel junction structural integrity breach. The engine was operated about 30 hours since the last annual inspection.
Probable Cause: A partial loss of engine power due to a corrosion-related fatigue crack of the No. 3 cylinder barrel.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CEN22LA227 |
Status: | Investigation completed |
Duration: | 1 year and 8 months |
Download report: | Final report |
|
Sources:
NTSB CEN22LA227
History of this aircraft
Other occurrences involving this aircraft
27 July 2014 |
N2148J |
Private |
0 |
Houston, Texas |
|
sub |
Gear collapse |
Location
Revision history:
Date/time | Contributor | Updates |
01-Feb-2024 11:03 |
ASN Update Bot |
Added |
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