Thursday, April 09, 2026

Quicksilver GT-400, N120LF, accident occurred on March 23, 2026, at John Nichol's Field Airport (0CL3), Chula Vista, California

  • Location: Chula Vista, CA 
  • Accident Number: WPR26LA148 
  • Date & Time: March 23, 2026, 15:30 Local 
  • Registration: N120LF 
  • Aircraft: Quicksilver GT-400 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202775/pdf

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?NNumberTxt=N120LF

- History of Flight:
On March 23, 2026, at about 1530 local time, a privately-registered Quicksilver GT-400, N120LF, sustained substantial damage when it was involved in an accident at John Nichol's Field Airport (0CL3), Chula Vista, California. The pilot was not injured.

The FAA reported: "Aircraft overshot landing on runway resulting in substantial damage."

Boeing 737-824 (WL), N27213, accident occurred on March 6, 2026, at Denver International Airport (DEN/KDEN), Denver, Colorado

  • Location: Denver, CO 
  • Accident Number: DCA26LA150 
  • Date & Time: March 6, 2026, 15:24 UTC 
  • Registration: N27213 
  • Aircraft: Boeing 737-824 
  • Injuries: 1 Minor, 136 None 
  • Flight Conducted Under: Part 121: Air carrier - Scheduled 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202612/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N27213

On March 6, 2026, about 1024 mountain standard time (MST), United Airlines (UAL) flight 605, a Boeing 737-824, N27213, collided with two Vestergaard Elephant Beta deice trucks, operated by Aeromag, while taxiing out of the deice pad at Denver International Airport (DEN), Denver, Colorado. There were no injuries to the two pilots, 4 flight attendants, and 130 passengers onboard the airplane. One deice agent sustained minor injuries during the event. The airplane sustained substantial damage. Flight 605 was a scheduled domestic passenger flight operating under the provisions of Title 14 Code of Federal Regulations Part 121 from DEN to Nashville International Airport (BNA), Nashville, Tennessee.

According to the flight crew statements, they were parked at deice pad C, spot C5, while deicing procedures occurred. The flight crew stated they were engaged in a conversation, when the first officer heard the deice team communicate their post-deice briefing. The captain was unsure if the clearance was for their flight, but the first officer acknowledged the postdeice brief and readback pertinent details, specifically that all deice vehicles were behind the clearance lines. The flight crew conducted the post-deice checks and received clearance to taxi from air traffic control. The flight crew began to taxi and felt the aircraft collide with something. The flight crew stopped the aircraft and contacted the deice team on the radio. At that time, the flight crew was informed that they had not been cleared to exit the deice pad and that they had collided with two deice trucks.

According to the Aeromag deice team, flight 605 was being sprayed with type 4 fluid from four of their trucks, MAG 94 and MAG 95 were forward of the wings and MAG 28 and MAG 30 were aft of the wings. The deice agents observed the airplane beginning to move forward and no one was able to stop the airplane movement. The airplane struck trucks MAG 94 (left wing) and MAG 95 (right wing), resulting in MAG 95 being pushed onto its side. 

A postaccident examination of the airplane revealed damage to the left winglet, the left wing lower skin, slats number 1, 5, 6, 7, and 8, the right wing lower skin, and the right aileron.

As part of the investigation process, the NTSB invited qualified parties to participate in the investigation, including the Federal Aviation Adminstration and United Airlines. In accordance with the provisions of Annex 13 to the Convention on International Civil Aviation, the Transporation Safety Board (TSB) of Canada was notified and Aeromag, a Canadian based ground service provider, was invited to participate in the investigation as a technical advisor. The following NTSB specialists were assigned to investigate the accident: Operations, Human Performance, Airport Operations, Cockpit Voice Recorder (CVR), and Flight Data Recorder (FDR) were assigned.

The investigaiton is ongoing.

Cessna 421B Golden Eagle II, N799TF, accident occurred on March 27, 2026, at Sedona Airport (SEZ/KSEZ), Sedona, Arizona

  • Location: Sedona, AZ 
  • Accident Number: WPR26LA145 
  • Date & Time: March 27, 2026, 16:30 Local 
  • Registration: N799TF 
  • Aircraft: Cessna 421B 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202719/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=799TF

On March 27, 2026, about 1630 Pacific daylight time, a Cessna 421B, N799TF, was substantially damaged when it was involved in an accident near Sedona, Arizona. The pilot and pilot rated passenger were not injured. The airplane was operated as a Code of Federal Regulations Part 91 personal flight.

According to the pilot, the preflight checks, flight from Los Alamos Airport (LAM), Los Alamos, New Mexico, and approach to landing at Sedona Airport (SEZ), Sedona, Arizona, were uneventful. During the pre-landing checks, the pilot observed three green lights, indicating that all three landing gear legs were locked in the down position. After touchdown on runway 21 the airplane began to yaw to the right and progressed to a “heavy pull.” The pilot applied full left rudder to counteract the right yaw, and the airplane remained on centerline, initially. As the airplane slowed during the landing roll, the right yaw resumed and the left rudder correction became ineffective. Subsequently, the airplane exited the right side of the runway and impacted two taxiway signs. All three landing gear collapsed, and the airplane continued through a ditch before it came to rest upright in a grassy area adjacent to the runway.

Postaccident examination of the airplane revealed that the right wing, left horizontal stabilizer, and fuselage were substantially damaged.

The wreckage was retained for further examination.

The Airplane Factory Sling LSA, N166TW, fatal accident occurred on April 9, 2026, in Avalon, California

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.

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N166TW

- History of Flight:
On April 9, 2026, at about 1230 local time, a privately-registered The Airplane Factory Sling LSA, N166TW, was destroyed when it was involved in an accident in Avalon, California. The pilot and passenger were killed. The flight originated from the Zamperini Field-Torrance Airport (TOA/KTOA), 
Torrance, California, at 1053 LT, and was destined to an unknown location.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, the airplane departed KTOA and proceeded south towards Catalina Island while cruising at 4,000 ft. At 1108 LT, the airplane initiated a descent towards 800 ft that last roughly 5 minutes. At this point, flightradar24 stopped tracking the airplane. At 1112:42, the airplane was observed 3 miles west of Catalina Airport (KAVX), it was at 800 ft, 92 knots groundspeed, and descending 200 feet per minute. At this point, flightaware stopped tracking the airplane, but ADS-B exchange recorded two additional points in south of the island, the airplane was at 500 ft, 98 knots, and descending 100 feet per minute along the shoreline about 6 miles from the airport. This was the last recorded data point.

According to law enforcement, the airplane crashed in the vicinity of Divine Road which is located west of Avalon, California. This road is located 5.70 miles from the airport (see figures).

Figure 1: ADS-B exchange data of entire flight.

Figure 2: ADS-B exchange data ran through Google Earth pro with Divine Road marked.

- Pilot Information:
Unknown.

- Aircraft Information:
The accident aircraft, serial number 161, was a two seat (side-by-side), single engine, tricycle undercarriage, aluminium aircraft with a conventional low wing design and is compliant with the requirements of the FAA Light Sport Aircraft (LSA) category according to ASTM Standards F2245, F2279 and F2295, and was powered by a Rotax 912 iS engine that drove a 3-blade DUC FLASH propellers.

The Sling LSA is primarily intended for recreational and cross-country flying. It is not intended for aerobatic operation. It is considered to be suitable for use as a trainer.

According to the Pilot Operating Handbook (POH), section 2.2 "Airspeed Limitations":

Vs Stall Speed 45 KIAS:

The aircraft will stall at this speed with flaps fully retracted, at MAUW in the most forward CG configuration and engine idling.

VS0 Stall Speed in Landing Configuration 40 KIAS :

The aircraft will stall at this speed with full flap, at maximum all up weight in the most forward CG configuration and engine idling.

According to the Pilot Operating Handbook (POH), section 2.13 "Kinds of Operation":

2.13.1 Normal VFR Operation 

The Sling LSA, in standard configuration, is approved only for day VFR operation with visual contact with terrain.

2.13.3 IFR Operation

Provided that the aircraft is appropriately equipped, the aircraft may be safely flown under IFR. Depending on the practical and legal requirements of the judicial region the aircraft will be operated, the aircraft may also be safely flown in IMC conditions, in accordance with IFR. It is the responsibility of the aircraft operator to ensure that all legal and safety requirements are met, along with the installation of the required systems and instrumentation for IFR (and IMC) flight. However, in the United States of America, all flights (VFR and IFR) are to be conducted in VMC, as per the applicable LSA standards.

- Wreckage and Impact Information:
The airplane crashed in remote mountainous terrain.

- Airport Information:
Santa Catalina Island is located about 20 miles offshore from the southern California mainland. The island terrain is extremely rugged. AVX was situated on a small mesa, at an elevation of about 1,600 feet above mean sea level (msl). According to the Catalina Conservancy, which is the steward agency for AVX, the airport mesa was man-made by removing the tops of two adjacent mountains, and using that material to fill in the lower-elevation region between the two.

The airport and runway topography are somewhat unusual. It is very common practice for flight schools and fixed base operators in that region to require airport-specific checkouts prior to allowing any pilot to fly there on his/her own.

The single concrete runway, designated 4/22, measured 3,000 by 75 feet. The threshold of runway 22 was situated at an elevation of 1,553 feet. Over the first 2,000 feet, the runway sloped evenly upward to an elevation of about 1,597 feet msl. This yielded a runway gradient of about 2.2 percent, or about 1.26ยบ. Beyond that point, the runway rose more gradually, to a maximum elevation of about 1,605 feet at the runway 4 threshold. The gradient profile made the runway appear "humped," and rendered aircraft positioned at opposite thresholds invisible to one another.

According to an additional airport remark, "Operations PROHIBITED AT NIGHT OR WHEN ARPT IS UNATNDD."

According to the Catalina Conservancy Web Site Information for Pilots...

"Be Aware:

1) There are no familiar visual cues for altitude reference. You MUST [emphasis original] rely on your Altimeter. [capitalization original]"

- Weather:
(1) Brief:

The recorded weather at KTOA at 1149 LT included: Winds 070 at 6 knots, 10 mile visibility, a scattered cloud layer at 1,500 ft AGL, temperature 21°C, dewpoint 15°C, and an altimeter setting of 29.97 inches of mercury.

The recorded weather at KNUC at 1156 LT included: Winds 270 at 9 knots, 10 mile visibility, a scattered cloud layer at 900 ft AGL, a broken cloud layer at 18,000 ft AGL and 25,000 ft AGL, temperature 20°C, dewpoint 17°C, and an altimeter setting of 30.00  inches of mercury.

(2) METARs

METAR KTOA 091747Z 11005KT 10SM FEW009 SCT015 21/15 A2997

METAR KTOA 091849Z 07006KT 10SM SCT015 21/15 A2997

METAR KTOA 091948Z COR 12007KT 10SM FEW018 SCT110 BKN180 22/16 A2995

METAR KNUC 091756Z 27010KT 10SM FEW009 SCT180 BKN250 20/17 A2999 RMK SLPNO T02000167 51012

METAR KNUC 091856Z 27009KT 10SM SCT009 BKN180 BKN250 20/17 A3000 RMK SLPNO T02000172

METAR KNUC 091956Z 27007KT 10SM FEW010 BKN180 BKN250 21/17 A2999 RMK SLPNO T02110172

(3) Area Forecast Discussion:

Area Forecast Discussion...UPDATED
National Weather Service Los Angeles/Oxnard CA
1101 AM PDT Thu Apr 9 2026

UPDATED AVIATION SECTION

.SYNOPSIS...09/836 AM.

A cooling trend will begin today and continue through the weekend.
A couple storms will move through the area late Friday through
Monday with showers and thunderstorms possible, especially
Sunday.

&&

.SHORT TERM (TDY-SAT)...09/853 AM.

***UPDATE***

An upper low is approaching northern California this morning
which will be followed by an even colder upper low late Saturday
into Sunday. For the short term the main impacts locally will be
cooler temperatures as onshore flow returns as well as increasing
morning low clouds and fog. As mentioned below, the first system
for late Friday into Saturday will have minimal impact as the
upper low remains mostly over northern California. A few showers
but amounts from a trace of rain to around a quarter inch, highest
north of Pt Conception.

The second system for late Saturday into Sunday will be the
stronger of the two and with the potential for heavy showers and
severe storms, especially north of Pt Conception.

***From Previous Discussion***

A series of late season storms is still on track to affect the
state Friday into the weekend. There is now a broad consensus that
the 1st storm will pull up to the north and will not bring as
much moisture and dynamics to the area as once thought. A weak
front will likely bring rain to SLO and most of SBA county on
Friday with just a chc of afternoon rain over VTA county. LA
county will likely be dry during the morning and afternoon hours.
SLO county will see the bulk of the weather action, since they
will be closest to the upper low. There is just enough dynamics
and instability there to warrant a slight chc of TSTMs. Rainfall
north of Pt Conception looks like it will be around a tenth of an
inch with up to a half inch over the far NW corner of SLO county
and anywhere a TSTM forms. A trace to a tenth of an inch is
possible across the SBA south coast and VTA county. Clouds, rain
and falling hgts will all contribute to a 3 to 6 locally 8 degree
cooling trend.

The weak front will move through the entire area Friday night into
Saturday morning. Most areas will see a 40 to 50 percent chc of
rain during this time. Rainfall amounts will not be too much at
all mostly around a tenth of an inch.

Right now it looks like Saturday will mostly be between storms. A
cold 535 dam system will work its way down the coast during the
day. During the morning there is about a 40 percent chc that rain
from this system will reach the Central Coast. A slight chc of
rain from the outgoing system will linger over SE LA county. Rain
will likely (70 percent chc) develop over SLO county in the
afternoon with a 50 to 60 percent chc for western SBA county.
There is a chc (30 to 40 percent) that rain will reach the rest of
SBA county and VTA county. Rainfall amounts during this time are
not looking impressive. Except for nrn SLO county most areas will
not see more than a tenth of an inch of rain during the day. Nrn
SLO county could see a quarter to a third of an inch. Another 3 to
6 degrees of cooling will bring all cst/vly temps into the 60s or
4 to 8 degrees blo normal.

.LONG TERM (SUN-WED)...09/220 AM.

On Saturday night a colder and more vigorous upper low will move
into nrn CA. It will bring a wetter and much more dynamic front
into the area. There is a greater than 80 percent chc that all
areas will see rain overnight. The front will likely produce a
number of TSTMs. It will have at least advisory level southerly
winds in the mtns and interior vlys and perhaps over the Central
Coast as well. The south winds will bring enhanced precip totals
and rates to the transverse ranges. Any TSTM that forms will also
bring enhanced precip totals and rates to areas they pass over.

At this point it looks like the flatter portions of the csts and
vlys will see a half to three quarters of an inch of rain
overnight with inch plus amounts on the across the foothills and
coastal slopes and any area affected by TSTMs. Most rainfall
rates will be between 0.25 to 0.75 in/hr but higher rates will be
possible under any TSTM that develops.

Snow levels will fall to about 5500 ft and accumulating snow will
fall above 6000 ft.

These rainfall and snowfall numbers are still preliminary and are
still subject to change. The most likely factor that would change
the numbers are the speed of the front (slower = more rain /
faster = less rain) and the trajectory of the parent upper low.
Still confidence in this forecast is higher than it has been.

The main front will exit LA county sometime between dawn and mid
morning on Sunday. There will be some shower activity behind the
front but additional rainfall amounts will not amount to much. It
will feel more like a rainy January day with max temps only in the
lower to mid 60s.

There is a 20 to 30 percent chc of lingering showers Sunday
night and a low by non zero chc Monday morning. These showers
should just be stray nuisance showers. By mid morning Monday dry
NW flow will set up over the area. Sunnier skies and rising hgts
will bring 2 to 4 locally 6 degrees of warming to the area. Max
temps, however, will be 8 to 12 degrees blo normal.

Tue and Wed will see a nice warming trend as the cold air moves
out of the area and high April sun angle combine to bring 4 to 8
degrees of warming Tuesday and 2 to 4 additional degrees on
Wednesday. Wednesday`s highs across the csts and vlys will almost
all be in the 70s.

&&

.AVIATION...09/1800Z.

At 1654Z at KLAX, the marine layer was 1600 ft deep. The top of
the inversion was at 2000 ft with a temperature of 17 C.

Overall, moderate confidence in 18Z TAF Package. Timing of flight
cat changes may be off +/- 2 hours and cig hgts by +/- 300 ft.
PROB30 -SHRA chances after 10/14Z for KPRB, KSBP, and KSMX.

KLAX...Moderate confidence in TAF. Low clouds could arrive as
early as 09Z or as late at 13Z. Cigs could range between 008 and
015. No significant east wind component expected.

KBUR...Moderate confidence in TAF. There is a 40% chc MVFR CIGs
(015) do NOT develop (remaining FEW-SCT) after 10/09Z.

&&

.MARINE...09/808 AM.

Current Small Craft Advisories are on track. Refer to MWWLOX and
CWFLOX for more details.

A weak Cold Front will move across the coastal waters Friday into
Saturday morning bringing showers and a slight chance for a
thunderstorm north of point conception.

A second system will arrive later on Saturday into Sunday with a
more traditional cold front. This stronger front will bring
numerous showers and a slight chance for thunderstorms across all
waters. Potential hazards include: heavy downpours, dangerous
cloud to ocean lightning, small hail, and erratic gusty winds.
Boaters, especially those with small vessels should avoid these
conditions.

- Additional Information:
This is the first fatal accident involving this aircraft type on US soil.

Wednesday, April 08, 2026

Airbus EC130 T2, N237SH, accident occurred on February 22, 2026, in Evergreen, Alabama

  • Location: Evergreen, AL 
  • Accident Number: ERA26FA120 
  • Date & Time: February 22, 2026, 15:10 Local 
  • Registration: N237SH 
  • Aircraft: Airbus Helicopters EC 130 T2 
  • Injuries: 3 Serious 
  • Flight Conducted Under: Part 135: Air taxi & commuter - Non-scheduled - Air Medical (Unspecified)

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202478/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N237SH

On February 22, 2026, at 1510 central standard time, an Airbus EC130 T2 helicopter, N237SH, was substantially damaged when it was involved in an accident near Evergreen, Alabama. The commercial pilot and two medical crewmembers were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 135 positioning flight.

According to the operator, following a patient transport, the pilot flew the helicopter to Pensacola International Airport (PNS), Pensacola, Florida and refueled. Following the refueling, the pilot departed PNS and began the flight back to the helicopter’s home base at Evergreen Medical Center helipad, Evergreen, Alabama. The pilot reported that while on approach to the helipad, the helicopter began an uncommanded yaw to the left. In response to the uncommanded yaw, the pilot lowered the collective, and pitched the nose forward in an attempt to gain airspeed to try to “fly out.” The pilot continued that, despite the attempted remediation, the yaw continued and that, when the helicopter was about 10 to 20 feet above the ground, it impacted an object.

Surveillance video captured a portion of the accident sequence. The helicopter entered the frame as it began its approach to the helipad. The helicopter then began to slow, and subsequently began to spin into a leftward yaw. The helicopter descended behind trees, and the impact could be heard.

The main wreckage site was located about 0.2 miles from the helipad. The first identified impact point was the roof of a residential home; there were two large dents in the roof’s ridge as well as a large gouge in a panel of the metal roof. The main wreckage came to rest in the home’s southern yard. The main wreckage site contained the helicopter’s fuselage, tail boom, main rotor blades, and portions of the fenestron. The furthest piece of wreckage was a portion of the fenestron rotor support and was located about 300 ft northwest of the main wreckage location. Three of the fenestron’s blades and other portions of the fenestron hub were located between the main wreckage location and the furthest piece of wreckage.

The airframe sustained substantial damage during the accident sequence to the fuselage, tail boom, fenestron, main rotor assembly, and both horizontal stabilizers. The fuselage displayed impact damage signatures with most of the damage occurring to the forward and left side. The tail boom was found separated from the fuselage.

The fenestron had mostly separated from the tail boom and portions of the composite vertical stabilizer and the fenestron shroud were found throughout the accident site. Most of the fenestron rotor assembly was found about 30 ft from the main wreckage location. It contained most of the fenestron rotor hub, gearbox, 5 complete rotor blades and a portion of a 6th rotor blade. The rest of the 6th rotor blade was found a few feet away. Three of the other rotor blades were found between the fenestron rotor assembly and the furthest piece of wreckage (which was also part of the fenestron rotor assembly). Only a small portion of the 10th rotor blade was found; the rest of the blade was unable to be located at the time of the on scene examination. Several of the fenestron stators had separated and were located within the accident site. The fenestron drive shaft had separated into multiple pieces, all of the fractures were consistent with impact damage. The drive shaft was rotated manually, and the fenestron rotor hub rotated without signs of binding. The anti-torque pedals remained attached to the airframe and were jammed, consistent with the observed impact damage. The anti-torque control cable rod end remained attached to the pedals, the cable was fractured and bent near the separated tail boom. The rod end at the fenestron end had separated from the cable and its attach point on the fenestron rotor hub control attach point. The rod end was not located at the time of the on scene examination.

All three main rotor blades were destroyed. There was a large trench in the dirt underneath the Starflex and mast area.

Control continuity from the cyclic and collective was observed from the cockpit to the rotor mast hydraulic actuators. All of the hydraulic servos and control link components sustained impact damage. The collective twist-grip was found in the "Flight" gate.

Some attenuation damage was observed on the pilot's seat, the middle rear seat, and the far right seat. All four seats were equipped with 4-point restraints; the center seat's lap belt showed fraying in the webbing.

The crash-resistant fuel system remained relatively undamaged with approximately 50 gallons of fuel on board.

The engine remained attached to the engine deck by its forward and rear mounts. The bellmouth was broken away, leaving the axial compressor visible. The gas generator could be rotated by hand, and there was no visible foreign object damage on the axial compressor blades. The free turbine could be rotated by hand, and continuity was confirmed from the free turbine to the main rotor head. Proper freewheel operation was also confirmed. All fuel, oil, air and electrical connections were found properly connected and saftied. The Module 1 and 5 magnetic plugs were found clean as well as the electric chip detector. The fuel filter delta P was found not activated (no bypass). The module 5 reduction gearbox was removed for input pinion slippage mark examination. The slippage mark was found to have moved by approximately 2mm. The emergency backup control ancillary unit was removed, and the key was in the 12 o’clock position.

The wreckage was recovered and retained for further examination.

Boeing 787-9 Dreamliner, N24972, incident occurred on March 2, 2026, at Los Angeles International Airport (LAX/KLAX), Los Angeles, California

  • Location: Los Angeles, CA 
  • Incident Number: ENG26LA014 
  • Date & Time: March 2, 2026, 11:00 Local 
  • Registration: N24972 
  • Aircraft: Boeing 787-9 
  • Injuries: 250 None 
  • Flight Conducted Under: Part 121: Air carrier - Scheduled

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202579/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N24972

On March 2, 2026, at 1100 Pacific Standard Time, United Airlines flight 2127, a Boeing 787-9, registration N24972, powered by two General Electric GEnx™-1B76A/P2 turbofan engines  experienced a No. 1 (left) engine surge during climb from Los Angeles International Airport (LAX), Los Angeles, California. There were no injuries to the 2 flight crew, 9 cabin crew, or 239 passengers on board. United Airlines operated the airplane as a Title 14 Code of Federal Regulations Part 121 domestic passenger flight destined for Newark Liberty International Airport (EWR), Newark, New Jersey.

According to the flight crew statements, the flight began with an uneventful pre-flight, taxi, and takeoff from runway 25R. The First Officer was the pilot flying and the Captain was the pilot monitoring. While climbing through 17,000 feet, they experienced strong vibrations in the controls and observed decreasing left engine N2 speed. A compressor stall and a L ENGINE FIRE message was displayed on the engine indicating and crew alerting system (EICAS) shortly after. The First Officer transferred controls to the Captain and began executing the engine fire checklist. One fire bottle was discharged and the engine fire warning extinguished after about 30 seconds. The warning returned on the EICAS, and the second fire bottle was discharged. The crew declared an emergency, advised ATC of a suspected engine fire, requested clearance for immediate return to LAX, and asked for airport crash and fire rescue (CFR) assistance. The crew continued receiving intermittent fire warnings during their return to LAX.

A single engine, ILS approach and landing on Runway 25L was accomplished without incident. After landing, the L ENGINE FIRE EICAS warning returned and the crew decided to stop taxi and evacuate while still on the taxiway. While the crew was performing the evacuation checklist and informing passengers, a flight attendant told them she saw fire coming from the left engine. Aircraft rescue and fire fighting (ARFF) personnel brought airstairs to right-side door R1 and slides were deployed for the remaining right-side doors R2 and R3. The Captain stayed onboard to assist firefighters sweeping the aircraft while the First Officer went outside to assist passenger evacuation.

Post-incident examination of the airplane found sooting and thermal damage concentrated around the engine core module’s external surfaces and extending up toward the pylon connection. Both left and right thrust reverser halves showed minimal thermal damage. Borescope inspection found damage in the high-pressure turbine.


The NTSB invited qualified parties to participate in the investigation, including the Federal Aviation Administration, the Boeing Company, United Airlines, and General Electric Aerospace. NTSB specialists supporting this investigation include Flight Data Recorders, Materials, and Powerplants.

The investigation is ongoing.

Cessna R172E Skyhawk, N39ND, accident occurred on April 7, 2026, at Sun Valley Airport (A20), Bullhead City, Arizona

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.

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N39ND

- History of Flight:
On April 7, 2026, at about 1140 local time, a privately-registered Cessna R172E Skyhawk, N39ND, sustained substantial damage when it was involved in an accident at Sun Valley Airport (A20), Bullhead City, Arizona. The pilot and passenger received minor injuries.

The FAA reported: "Aircraft veered left on takeoff roll and struck a garage."

According to ADS-B data, the airplane arrived at A20 at 1117 LT following a trip that originated from Kingman Airport (IGM), Kingman, Arizona, at 1034 LT. The accident flight was not captured on ADS-B data.

The reported weather at KIFP about 6 minutes after the accident included: Winds 240 at 8 knots, temperature: 29 °C, dewpoint: 0 °C, and an altimeter setting of 29.90 inches of mercury.

The airport sits at an elevation of 725 ft and features a single asphalt/good condition runway 18/36 that is 3700 x 42 ft.

- Weather:

METAR KIFP 071747Z 21006KT 10SM CLR 27/M00 A2992

METAR KIFP 071847Z 24008KT 10SM CLR 29/00 A2990