Champion 7GC accident near Anchorage, Alaska, March 26, 2018
On March 26, 2018 at about 1:30 am local time, a 1959 Champion 7GC, registered N4844E, was substantially damaged in an accident during landing near Anchorage, Alaska (Merrill Field). It was a personal flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to maintain directional control during landing with a crosswind, which resulted in a loss of control and failure of the main landing gear. Contributing to the accident was the pilot's self-induced pressure to land.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- March 26, 2018 · about 1:30 am local time
- Place
- Anchorage, Alaska · Merrill Field · map
- Type
- Accident
- Injuries
- No one was hurt; 2 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Champion 7GC NO SERIES, built 1959 · all 7GCs on the register
- Registration
- N4844E · registry record · serial 7GC-44
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot was landing at the airport after a personal flight. After obtaining weather information for the destination airport, the pilot contacted the air traffic control (ATC) tower and requested to land on the runway that corresponded to the current wind condition. The pilot's intent was to land with a direct headwind. The controller responded that the requested runway was not available due to other airplanes landing and directed the pilot to land on another runway that would result in the airplane landing with a crosswind. The pilot reported that the approach was stable. Upon touchdown, the airplane began to ground loop to the left, so she applied rudder and brake inputs as a corrective action, with no success. Subsequently, the right main landing gear separated, and the right wing impacted the runway; the airplane sustained substantial damage to the right wing and right aileron. An examination of the main landing gear (right side) strut threaded sleeve and jam nut found that the oleo strut had fractured. Overstress fracture features were consistent with the sleeve fracturing from the end of the oleo strut assembly with the assembly loaded in tension. No evidence of progressive or long-term cracking was observed on the fracture surface, which indicates that no cracks developed in the braze due to the low-tension loads during flight or due to attachment loads from assembly of the cap onto the strut cylinder assembly. Although the brazed joint between the sleeve and the oleo strut tube did not conform to the engineering drawing and the strength would have been substantially less than a properly brazed joint, there was no evidence to indicate that the joint would have separated if loaded as designed; the joint appeared to be strong enough to perform under normal operation given that there was no evidence of progressive fracture. Therefore, the strut likely fractured due to abnormal side loading of the wheel with little or no loads in the upward direction as the airplane tipped to the right during the landing sequence involving the ground loop to the left. The pilot reported she should have "held firm" to her request to land with a headwind and not a direct crosswind or quartering tailwind. She further reported that in the "future I will be more firm in my requests as pilot in command for the runway that I feel comfortable with and will wait as necessary for tower permission to use my requested runway." It is likely that if the pilot had contacted the ATC tower again and waited to land to her original runway of choice, the landing would have had a direct headwind instead of a crosswind. The pilot's decision to land on a runway with a crosswind was likely due to self-induced pressure to land.
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
- Air traffic event during landing
- Other weather encounter during landing
- Loss of control on ground during landing defining event
- Attempted remediation/recovery during landing
- Landing gear collapse during landing
- Part(s) separation from AC during landing
- Collision with terrain or object (not controlled flight into terrain) during landing
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Not attained/maintained
- cause Environmental issues › Conditions/weather/phenomena › Wind › Crosswind › Effect on operation
- factor Personnel issues › Psychological › Personality/attitude › Motivation/respond to pressure › Pilot
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 156 hours in all; 49 in this make and model; 11 in the last 90 days; 8 in the last 30 days; 54 as pilot in command
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: frt
- Injury: no injuries
The aircraft
- Airframe total time: 2,464.7 hours
- Last inspection: annual inspection, January 20, 2018
- Maximum gross weight: 1,650 lb
- Seats: 2
- Landing gear: fixed
- Engine: Lycoming O-290-D2B (piston); 2,427 hours total
The flight
- Departed from: MRI Anchorage AK
- Destination: MRI Anchorage AK
- Flight plan: VFR
- Runway 25, 4,000 ft by 100 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 360° at 7 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 39°F (4°C), dew point 7°F (-14°C)
- Altimeter: 29.59 inHg
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
4 documents, released by the NTSB on April 28, 2020. 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.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Materials Laboratory Factual Report 18-106 | PDF, 5 pages | View Download |
| 2 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 3 | N4844E Airframe Maintenance Records | PDF, 5 pages | View Download |
| 4 | Accident Photographs | PDF, 4 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
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 never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
