Thursday, October 16, 2025

Hawker 800XP, XA-JMR, fatal accident occurred on October 16, 2025, near Bath, Michigan

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.


- History of Flight:
On October 16, 2025, at about 1727 local time, a Mexican-registered Hawker 800XP jet, XA-JMR, registered to Aereo Lineas del Centro SA, was destroyed when it was involved in an accident near Bath Michigan. There are three reported fatalities at this point. The flight originated from the Kalamazoo Battle Creek International Airport (AZO/KAZO), 
Battle Creek, Michigan, at about 1708, and was destined to an unknown location. The purpose of the flight is unknown at the time of this writing.

The aircraft had not flown since last March.

According to preliminary Automatic Dependent Surveillance – Broadcast (ADS-B) data (figure 1), the airplane departed runway 23R at KBTL and entered a climbing left turn to an inflight cruising altitude of 14,750 ft. The airplane proceeded north with an average groundspeed between 240-270 knots and the flight appeared uneventful. At about 1724, the airplane entered a steady path on a magnetic 1° heading east of Lansing, Michigan, around the same time, the groundspeed values began to drop. At 1725:57, the airplane was at 14750 ft and 163 knots GS. Starting from this point, there were little altitude fluctuations noted while the groundspeed values continued to drop. At 1726:45, the airplane was at 14725 ft and 118 knots GS. At 1726:57, the airplane was at 14700 ft and 105 knots GS, with an average rate of 60 feet per minute (fpm), the next second, at 1726:58, the airplane was at 1726:58, the airplane began a 640 fpm climb. At 17:26:59, the airplane was at 14750 ft, 103 knots groundspeed, with an average rate of -6000 fpm, the next few seconds showed altitude and average rates fluctuations while the groundspeed stayed at 103 knots. At 1727:05, the airplane was seen in a -14000 feet per minute left hand descent. The airplane continued the descent, with extreme changes noted in the vertical speed. At about 1727:34, the airplane was now heading west at an altitude of 8,500 ft and a reported groundspeed of 74 knots and -18000 fpm rate, before it entered a second stall. At 1727:51, the airplane was observed heading east at an altitude of 4825 ft, 75 knots groundspeed, and -13300 fpm. At about 1727:57, the airplane was at 3525 ft, 89 knots GS, and -8700 fpm before it entered a final descending left hand spiral. The last ADS-B return was recorded at 1728:09, the airplane was at 1450 ft, 73 knots GS, with a reported vertical rate of -11000 feet per minute (check "additional information" section for additional figures).

Figure 1: ADS-B exchange track

Figure 2: End of track
- Pilot Information:
unknown

- Airplane Information:
The accident airplane, serial number 258530, was manufactured at an unknown date. The (mostly) 10 seat low-wing, retractable gear jet was powered by Honeywell TFE731-5BR engines.

According to the maintenance manual,  a stick shaker/stall warning test is conducted in Hawker jets when the wing leading edges are removed for maintenance. According to the airframe manufacturer’s requirements, the required altitude was above 10,000 ft above ground level, 10,000 ft above clouds and below 18,000 ft mean sea level. In addition, this check flight could only be conducted during day visual meteorological conditions with a good visual horizon, with the autopilot disengaged, an operative stall identification system, the external surfaces free of ice, the ventral tank empty and weather radar on standby.

According to the flight manual, the stall speed is about 92 kn (106 mph, 170 km/h) in landing configuration at typical landing weight.

- Wreckage and Impact Information:
No close-ups are available at the time of this writing.

- Weather:
(1) Brief:
A postaccident review of available meteorological data established that, at 1657, about 30 minutes before the accident, the KLAN automated surface observing system reported winds from 0 wind, 10 mile surface visibility, no cloud under 12,00 ft (CLR), temperature 17.2°C, dew point 2.8°C, and an altimeter setting of 30.16 inches of mercury.

(2) METARs:
nearby
METAR KLAN 162053Z 00000KT 10SM CLR 17/03 A3016 RMK AO2 SLP217 T01720028 56022 $
METAR KLAN 162153Z 00000KT 10SM CLR 17/03 A3015 RMK AO2 SLP211 T01670028 $

departure airport
METAR KAZO 162053Z VRB04KT 10SM CLR 18/05 A3016 RMK AO2 SLP215 T01780050 58019
METAR KAZO 162153Z 19004KT 10SM CLR 17/05 A3014 RMK AO2 SLP208 T01720050

(3) Area Forecast Discussion:
Area Forecast Discussion
National Weather Service Grand Rapids MI
343 PM EDT Thu Oct 16 2025

.KEY MESSAGES...

- Light rain tonight and tomorrow

- Wet and windy weather ahead

- More unsettled weather next week

&&

.DISCUSSION...
Issued at 330 PM EDT Thu Oct 16 2025


- Light rain tonight and tomorrow

An upper level ridge will continue to build and move over the
Great Lakes region through tomorrow. However, mid level moisture
stemming from an infiltrating low will bring a short save trough,
through the mid and lower levels. This will bring enough
instability that should allow for isolate showers along and north
or the I 96 corridor.
 Warm air advection will continue out ahead of the approaching
low. This will keep temperatures in the upper 60s to low 70s. That
is around 10 degrees above normal.
 There should be a break in precipitation Friday afternoon.
However that break in rain will be short lived.

- Wet and windy weather ahead

The trend is your friend and this case is not the exception to
the rule. Latest models continue to show a cold front approaching
from the west, moving slowly to the east. As it moves across the
Great Lakes it will drape across Michigan from the northeast to
the southwest beginning early Saturday morning. CAPE values remain
fairly low, but can`t rule out thunder along the leading edge of
the frontal boundary Saturday. The biggest area of moisture has
shifted to the east and south. The front should stall as the ridge
slowly shift eastward which will allow periods of showers
Saturday.
 The heaviest rain showers will move through the area Saturday
night into Sunday, especially through southern lower Michigan. The
low continues to track through the state, bringing wet and windy
weather through Sunday. Two day totals have QPF upwards of 1 to 2
inches, however that is over a 48 hour period. Heaviest rain is
most likely mainly along the lake shore and along a swath along
the I 69 corridor.
 While the moisture, temperature boundaries will allow for gusty
winds through this period. Saturday should have gusty upwards of
30 mph. Sunday should have a stronger gradient with wind gusts
upwards of 40 mph possible Sunday and Monday afternoon.

- More unsettled weather next week

 With the large upper level low moving slowly along the Upper
Great Lakes region, short waves and cold northwesterly flow should
bring periods of showers through the area through mid next week.
This will bring temperatures back to around normal, though lows
should remain above freezing.

&&

.AVIATION /18Z TAFS THROUGH 18Z FRIDAY/...
Issued at 145 PM EDT Thu Oct 16 2025

VFR is likely to continue into Friday morning. Light east winds
will become light from the southeast tonight, then a little
breezier with a few gusts over 16 knots from the south later
Friday morning. Clouds and some ceiling layers between 7,000 and
12,000 feet will stream in tonight... more so in the north. There
is about a 30 percent chance of light rain showers from 05 to 14 Z
at MKG, GRR, and LAN, though visibility is unlikely to be
affected.

- Additional Information:

Figure 3: Vertical Rate profile towards the end of track (Flysto)

Figure 4: Groundspeed (GS) profile towards the end of track (Flysto)

Cessna 750 Citation X, N769XJ, accident occurred on September 17, 2025, at San Diego International Airport (SAN/KSAN), San Diego, California

  • Location: San Diego, CA 
  • Accident Number: WPR25LA288 
  • Date & Time: September 17, 2025, 17:42 Local 
  • Registration: N769XJ 
  • Aircraft: Cessna 750
  •  njuries: 6 None 
  • Flight Conducted Under: Part 135: Air taxi & commuter - Non-scheduled
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201044/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N769XJ

On September 17, 2025, about 1742 Pacific daylight time, a Cessna 750, N769XJ, was substantially damaged when it was involved in an accident at San Diego International Airport (SAN), San Diego, California. The two pilots and four passengers sustained no injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 135 commuter flight.

The pilot reported that during the takeoff roll, he felt an intense vibration coming from the nosewheel as the airplane accelerated through 100 knots, so he elected to abort the takeoff. Subsequently, during the abort, the nose landing gear collapsed, and the nose of the airplane settled onto the runway. When the airplane came to a stop on the runway, the pilots executed an emergency shutdown and safely evacuated all occupants from the airplane.

Post accident examination revealed that the airplane’s fuselage sustained substantial damage.

The airplane was recovered and retained for further examination.

Cirrus SR22T GTS G5 Carbon, N218VB, fatal accident occurred on September 18, 2025, at Macon County Airport (1A5), Franklin, North Carolina

  • Location: Franklin, NC 
  • Accident Number: ERA25FA352 
  • Date & Time: September 18, 2025, 14:56 Local 
  • Registration: N218VB 
  • Aircraft: CIRRUS DESIGN CORP SR22T 
  • Injuries: 3 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201041/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N218VB

On September 18, 2025, at 1456 eastern daylight time, a Cirrus SR22T, N218VB, was substantially damaged when it was involved in an accident near Franklin, North Carolina. The private pilot and two passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Preliminary air traffic control information provided by the Federal Aviation Administration (FAA) indicated that the pilot was on an instrument flight rules flight from John C. Tune Airport (JWN), Nashville, Tennessee to Macon County Airport (1A5) Franklin, North Carolina. As the pilot approached 1A5, he requested a visual approach to runway 07 from air traffic control. The controller approved the request, and at 1448 the pilot reported the airport in sight. The controller then approved a frequency change to the common traffic advisory frequency. Shortly after, the pilot transmitted (while still tuned to the controller’s radio frequency) that he was at 6,800 ft and intended to perform a 360° turn to land on runway 07. The controller then advised the pilot that he was still on the frequency; there were no further transmissions received from the pilot.

Review of preliminary ADS-B data showed that shortly after, the airplane began a descending left turn from an altitude of about 6,300 ft mean sea level. It continued through a 360° left turn before it began to approach runway 7 at an altitude of about 3,300 ft (the airport elevation of 1A5 was 2,033 ft). The ADS-B data ended when the airplane was about 0.5 nautical miles from the runway threshold.

Surveillance video showed the airplane flying over the runway before initiating a descending left turn. The airplane continued descending in the left turn before entering a tightening spiral and impacting the ground.

Multiple witnesses near the accident site reported observing the airplane flying at a low altitude near the airport and over a nearby school playground. The airplane was described as rocking side-to-side, with its wingtips moving up and down, before rolling inverted and descending behind a tree line.

The airplane impacted a field about 0.25 miles east of 1A5. The airplane came to rest upright and all major components of the airframe were located at the accident site. All major flight control surfaces were observed and flight control continuity was traced throughout the flight control system.

The engine sustained impact damage but remained attached to all four engine mounts. The propeller flange, hub, and one blade remained attached to the engine. During the on-scene examination, the engine was lifted and its crankshaft was rotated, which confirmed crankshaft and camshaft continuity. Borescope examination of all cylinders revealed normal combustion and operating signatures on the piston faces, cylinder walls, and valve heads.

The airplane was recovered and retained for further examination.

Eurocopter EC 135T2+, N955AL, accident occurred on September 24, 2025, near Whittier, Washington

  • Location: Whittier, WA 
  • Accident Number: WPR25LA290 
  • Date & Time: September 23, 2025, 23:03 Local 
  • Registration: N955AL 
  • Aircraft: Eurocopter EC135 
  • Injuries: 4 Minor 
  • Flight Conducted Under: Part 135: Air taxi & commuter - Non-scheduled - Air Medical (Medical emergency)

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201708/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N955AL

On September 23, 2025, at 2303 Pacific daylight time, a Eurocopter EC-135 T2+, N955AL, was substantially damaged when it was involved in an accident near Whittier, Washington. The pilot and three medical crew members received minor injuries. The helicopter was operated by Air Methods, LLC as a Title 14 Code of Federal Regulations Part 135 air medical flight.

The pilot stated that while en route back to the helicopter’s base, he received a request to transport a medical patient. The pilot received the scene coordinates and proceeded to the location. Upon arrival, he determined the coordinates were incorrect by a few miles. After circling, he established communication with the landing zone (LZ) commander on the ground and was able to locate the scene. The LZ was located at an interstate highway exit adjacent to the highway, and the surface consisted of gravel and dirt. During his initial approach, he opted to perform a go-around maneuver and then establish an approach from another direction.

The pilot further stated that he communicated with the onboard crew throughout the approach about their view and obstructions. The helicopter passed surrounding treetops and light poles and continued to the LZ. As the helicopter descended, the crewmember positioned in the leftfront seat communicated that she observed dust accumulating in the air, which the pilot acknowledged. The helicopter continued to descend and, as it neared terrain, the crew’s visibility was reduced by dust/dirt, which the pilot described as “brown out.”

According to the pilot, he maintained visual reference to a light on a vehicle parked at the scene, but decided not to abort the landing due to the rising terrain and nearby obstacles surrounding the LZ. As he attempted to maintain the helicopter in a hover about two feet above the ground, the helicopter impacted a mound of gravel and rolled onto its right side. (See Figure 1). 

The pilot reported no pre impact mechanical failures or malfunctions that would have precluded normal operation.

Cessna 182N Skylane, N766EE, accident occurred on September 23, 2025, near Fallbrook Airpark (L18), Fallbrook, California

  • Location: Fallbrook, CA 
  • Accident Number: WPR25LA292 
  • Date & Time: September 23, 2025, 14:00 Local 
  • Registration: N766EE 
  • Aircraft: Cessna 182N 
  • Injuries: 1 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201727/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N766EE

On September 23, 2025, about 1400 Pacific daylight time, N766EE, a Cessna 182N, was substantially damaged when it was involved in an accident near Fallbrook, California. The pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, he purchased fuel at French Valley Airport (F70), Murrieta, California (F70), and departed about 1353. After takeoff, he flew southbound, toward Fallbrook Community Airpark (L18), Fallbrook, California, and flew a straight in approach to runway 18. As the airplane was less than one mile from runway 18, he attempted to increase engine power using the throttle, however, the engine power remained the same. He advanced the throttle position a second time and turned off the carburetor heat, with no change in engine power. The pilot realized that the airplane was too low to reach the runway and initiated an emergency landing on a divided highway, with partial engine power. The airplane landed on the southbound lanes and during the landing roll, the left wing impacted a tree, along the center divider. Subsequently, the airplane veered left, exited the roadway, nosed over, and came to rest inverted, on an embankment adjacent to the northbound lanes of the roadway.

Postaccident examination revealed that the fuselage, both wings, and empennage sustained substantial damage. The wreckage was recovered to a secure location for further examination.

Piper PA-28R-200 Arrow II, N999AD, accident occurred on October 1, 2025, near Colorado Springs, Colorado

  • Location: Colorado Springs, CO 
  • Accident Number: CEN26LA001 
  • Date & Time: October 1, 2025, 04:12 Local 
  • Registration: N999AD 
  • Aircraft: Piper PA-28R-200 
  • Injuries: 1 Minor, 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201763/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N999AD

Allison Aviation LLC opb Arapahoe Flight Club

On October 1, 2025, about 0412 mountain daylight time, a Piper PA-28R-200 airplane, N999AD, was substantially damaged during an accident near Colorado Springs, Colorado. The pilot sustained minor injuries, and the 2 passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that the airplane’s fuel tanks were topped off (48 gallons usable) before he departed on the cross country flight with the 2 passengers. The pilot reported that his weightand-balance calculations indicated that the airplane weighed about 2,477 lbs before engine start.

The pilot reported that he did not identify any anomalies with the airplane during his preflight inspection or the before takeoff engine runup. The tower controller issued a takeoff clearance for runway 35L from the taxiway A4 intersection. After taxiing onto runway 35L, the pilot held the airplane’s brakes as he increased the engine to takeoff power and leaned the mixture to yield maximum power. The pilot reported that he conducted a normal takeoff with the flaps retracted and that liftoff occurred shortly after the expected rotation speed.

The pilot reported that after liftoff the airplane’s climb was less than the 600 fpm he expected based on his preflight takeoff performance calculations. He stated that the airplane’s airspeed was about 80 mph, which was slower-than-normal for the initial climb after takeoff. The pilot confirmed that the engine throttle and propeller control were full-forward and then increased the mixture control to full rich. The pilot stated that despite the engine operating, he was unable to increase the airplane’s airspeed and/or climb rate sufficiently to maintain clearance from the rising terrain that was ahead of the airplane. Ultimately, the pilot attempted to land the airplane on a multi-lane highway below the airplane.

The pilot stated that shortly before landing the airplane suddenly rolled left and pitched down. In the moments before ground impact, the pilot pulled back on the yoke and used right rudder to reestablish a level flight attitude. The pilot stated that the airplane’s flight path crossed over the northbound lanes to the southbound lanes before the airplane landed on all 3 landing gear simultaneously. The airplane then impacted two power poles as it slid to a stop. The pilot reported that the engine continued to run after the accident and to secure the engine he pulled the mixture control to cutoff and turned off both engine magnetos. After the engine stopped, he placed the electrical master switch to off and exited the airplane with his two passengers.

According to the pilot, he normally retracts the airplane’s landing gear after the airplane accelerates to 90-100 mph and has climbed above 500 ft above ground level (agl). The pilot stated that he did not retract the landing gear at any point during the flight.

According to recorded FAA ADS-B track data, airplane’s flight path continued north after takeoff from runway 35L, as depicted in figure 1. At 0407:48, the airplane was 2,215 ft from the departure end of runway 35L and about 82 ft agl. At that time, the airplane’s calibrated airspeed and vertical speed were about 78.5 mph and 375 fpm, respectively. Airplane performance calculations based on the recorded ADS-B track data established that the airplane’s calibrated airspeed was less than airplane manufacturer’s specified best rate-ofclimb airspeed (95 mph) and best angle-of-climb airspeed (85 mph) with the landing gear extended for the entire flight, as shown in figure 2. The airplane made several climb and descents during the flight which yielded an average vertical speed of 110 fpm.

At 0412:31, the airplane’s calibrated airspeed was about 80 mph when it suddenly rolled left about 120 ft agl, as shown in figure 3. The final ADS-B track data, at 0412:41, showed the airplane was about 5.7 nautical miles (nm) north of the departure airport at about 6 ft agl. At that time, the airplane’s calibrated airspeed was about 72 mph.

According to the Piper PA-28R-200 Airplane Flight Manual (AFM), the airplane’s engine-off aerodynamic stall speed at maximum gross weight (2,650 lbs) with the wing flaps retracted and the landing gear extended is 71 mph. With an 8,000 ft density altitude, the airplane’s expected climb rate at maximum gross weight with the wings flaps and landing gear retracted is about 480 fpm. The AFM does not provide a climb performance chart for the airplane with the landing gear extended.

The airplane wreckage was recovered to a secured storage facility where it was examined by FAA airworthiness inspectors. The engine examination did not reveal any mechanical anomalies that would have prevented normal operation.

Cessna 172N Skyhawk, N80628, accident occurred on October 7, 2025, near Petersburg, Alaska

  • Location: Petersburg, AK 
  • Accident Number: ANC26LA001 
  • Date & Time: October 7, 2025, 14:56 Local 
  • Registration: N80628 
  • Aircraft: Cessna 172N 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Instructional

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201763/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N80628

On October 7, 2025, at 1456 Alaska daylight time, a Cessna 172 airplane, N80628, was substantially damaged when it was involved in an accident near Petersburg, Alaska. The student pilot and flight instructor were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 flight.

The student pilot purchased the airplane two weeks prior to the accident. The training flight included steep turns, turns around a point, and emergency procedures. The flight instructor stated that during the flight there was some mist in the area, so they had applied carburetor heat and left it on. After rolling out of a left turn, while in straight and level flight, the engine lost partial power. Engine power was briefly restored, then the engine lost all power.

In an attempt to restore engine power, the flight instructor and student pilot cycled the magnetos, turned on the electric fuel pump, ensured the fuel selector was in the BOTH position, and the mixture was full RICH. Unable to restart the engine, the flight instructor performed a forced landing to a road. During the landing roll the airplane struck a large rock that partially separated the right main landing gear, and it pivoted it into a ditch. The airplane came to rest inverted and sustained substantial damage to the right wing.

At 1456, the weather reported at Petersburg Airport (PAPG), about 14 miles southeast of the accident site, included a temperature of 9°C and a dew point of 7°C. The calculated relative humidity at this temperature and dewpoint was 87%. Review of the icing probability chart contained within Federal Aviation Administration Special Airworthiness Information Bulletin CE-09-35 revealed the atmospheric conditions at the time of the accident were “serious icing at cruise power settings, and also fell within the range specified for icing in pressure-type carburetors.”

A detailed examination is pending recovery of the airplane.