Israel Aircraft Industries 1124 accident near Yukon, Oklahoma, March 18, 2019
On March 18, 2019 at about 8:31 pm local time, a 1978 Israel Aircraft Industries 1124, registered N4MH, was destroyed in an accident during initial climb near Yukon, Oklahoma (Sundance Airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The airplane’s unairworthy thrust reverser (T/R) system due to inadequate maintenance that resulted in an asymmetric T/R deployment during an approach to the airport and the subsequent loss of airplane control.
Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- March 18, 2019 · about 8:31 pm local time · cases in 2019
- Place
- Yukon, Oklahoma · Sundance Airport · cases near this airport · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Israel Aircraft Industries 1124, built 1978 · all 1124s on the register
- Registration
- N4MH · registry record · serial 232
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The two commercial pilots were conducting a personal, cross-country flight. A video surveillance camera at the airport captured their airplane’s approach. Review of the video revealed that, as the airplane approached the approach end of the landing runway, it began to climb, rolled left, became inverted, and then impacted terrain. The left thrust reverser (T/R) was found open and unlatched at the accident site. An asymmetric deployment of the left T/R would have resulted in a left roll/yaw. The lack of an airworthy and operable cockpit voice recorder, which was required for the flight, precluded identifying which pilot was performing pilot flying duties, as well as other crew actions and background noises, that would have facilitated the investigation. Postaccident examination of the airplane revealed that it was not equipped, nor was required to be equipped, with a nose landing gear (NLG) ground contact switch intended to preclude in-flight operation of the thrust reverser (T/R). The left T/R door was found unlatched and open, and the right T/R door was found closed and latched. Further, electrical testing of the T/R left and right stow microswitches within the cockpit throttle quadrant revealed that the left stow microswitch did not operate within design specifications. Disassembly of the left and right stow microswitches revealed evidence of arc wear due to aging. Based on this information, it is likely that the airplane’s lack of an NLG ground contact switch and the age-related failure of the stow microswitches resulted in an asymmetric T/R deployment while on approach and a subsequent loss of airplane control. Also, there were additional T/R system components that were found to unairworthy that would have affected the control of the T/R system. Operational testing of the T/R system could not be performed due to the damage the airplane incurred during the accident. Toxicology testing results of the pilot’s specimens indicated that the pilot had taken diazepam, which is considered impairing at certain levels. However, the detected amounts of both diazepam and its metabolite nordiazepam were at subtherapeutic levels, and given the long half-life of these compounds, it appears that the medication was taken several days before the accident; therefore, it is unlikely that the pilot was impaired at the time of the accident and thus that his use of diazepam was a not factor in the accident.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Loss of control in flight during initial climb defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- Aircraft › Aircraft systems › (general) › (general) › Failure other cases naming the other and general
- Aircraft › Aircraft systems › (general) › (general) › Not installed/available other cases naming the other and general
Pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane; rotorcraft: glider
- Flight time: 5,872 hours in all
- Last flight review: March 9, 2019
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: left
- Injury: fatal
Co-pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 5,259 hours in all; 3,869 on instruments
- Medical certificate: Class 1
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 11,030.1 hours
- Last inspection: continuous airworthiness programme, February 4, 2019
- Maximum gross weight: 23,500 lb
- Seats: 9
- Landing gear: retractable
- Engine 1: Garrett Airesearch TFE731-3D-1G (turbofan); 14,425 hours total
- Engine 2: Garrett Airesearch TFE731-3D-1G (turbofan); 14,054 hours total
- Operator: Sundance Airport FBO LLC
The flight
- Departed from: ECP Panama City FL at 6:33 pm
- Destination: HSD Oklahoma City OK
- Flight plan: IFR
- Runway 18, 5,001 ft by 100 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 180° at 7 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 68°F (20°C), dew point 28°F (-2°C)
- Altimeter: 30.25 inHg
- Observation at 8:25 pm from HSD
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
Photographs from the investigation 3 pictures from the NTSB's docket, as the NTSB released them
Photo 1: Aircraft Wreckage
Photo 2: Left Thrust Reverser
Photo 3: Video Surveillance Image of AircraftThe NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
21 documents, released by the NTSB on April 5, 2021. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
Connections how this case links to the rest of the register
- N4MH on the register today · the tail number may have moved to another aircraft since
- Israel Aircraft Industries 1124 73 registered today · the model family and its accident history
- Israel Aircraft Industries 305 aircraft on the register
- Engine: Garrett Airesearch TFE731-3D-1G 25 aircraft carry this series today · as the NTSB recorded it
- Engine: Garrett Airesearch TFE731-3D-1G 25 aircraft carry this series today · as the NTSB recorded it
- Sundance Airport · nearest airport
- Northwest Florida Beaches International · departed from
- Accidents and incidents in Oklahoma 1,300 since 1982 · 181 in the last ten years
- Oklahoma 5,643 aircraft registered
The whole map of how records connect · these connections as data: /graph/accident/CEN19FA104.json.
The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
