WPR26LA245

NTSB accident investigation · Piper PA-28-140 · Salome, AZ · July 5, 2026

Accident · No injuriesClass 3 · LimitedPreliminary report
Date
July 5, 2026, 08:25 local (15:25 UTC)
Place
Salome, AZ
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N3995KPiper PA-28-140
Defining event
Initial climb: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Investigation ongoing
Investigation class
Class 3
NTSB office
Western Pacific Region
Parties
Lycoming Engines, Federal Aviation Administration
FAA report
20260705008529A
Case key
203329

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Preliminary report

What NTSB knew early in the investigation. It may change in the final report.

On July 5, 2026, at about 0825 Pacific daylight time, a Piper PA-28-140, N3995K, was substantially damaged when it was involved in an accident near Salome, Arizona. The pilot and passenger were uninjured. The airplane was operating as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the passenger, who was a rated pilot and mechanic, the purpose of the flight was to conduct an engine break-in flight following a recent engine overhaul. Before the flight, the pilot and passenger completed a preflight inspection and engine ground run, during which no anomalies were noted. The magneto checks were within specifications, with an approximate 100-rpm drop, and the passenger did not observe any abnormal engine temperature or oil pressure indications. The passenger reported that he had previously conducted ground runs on the engine following the overhaul, and they were normal. The airplane departed from runway 17 at Western Sky Airpark (OAZ2), Salome, Arizona. The passenger described the takeoff as normal and stated that the engine was producing about 2,400 rpm, with the throttle full forward and the mixture full rich. At about 800 to 900 ft above ground level, the pilot turned the airplane to the right and began reducing the throttle from full power. The passenger estimated the throttle reduction at about 200 rpm, though he did not recall the exact rpm amount. Immediately after the throttle was reduced, the engine lost all power. The passenger reported there were no indications of an impending engine failure, including no unusual vibration, smoke, sounds, or abnormal gauge readings. The pilot then searched for a forced landing area. The passenger estimated that about 20 to 30 seconds later the airplane impacted terrain. The airplane sustained substantial damage to the wings, fuselage, tail, and empennage. The wreckage was recovered to a secure location for further examination.

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.

Aircraft

Registration
N3995K
Reported as
Piper PA-28-140
Category
Airplane
Serial number
28-23887
Built
1967
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Kennedy Daniel P
Airworthiness certificate
Standard, Normal; Standard, Utility
Destination
Same as departure
Airport
0AZ2 · Western Sky Airpark
Equipment
Stall warning system

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.

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 5 knots
Visibility
9 statute miles
Lowest ceiling
None
Temperature
95 °F, dew point 36 °F
Altimeter
29.91 inHg
Observed at
KBXK, 53 nm away
METAR
METAR KBXK 051615Z AUTO 20005KT 9SM CLR 35/02 A2991 RMK AO2

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.