Mooney M20J accident near Palo Alto, California, September 4, 2018
On September 4, 2018 at about 6:00 pm local time, a 1992 Mooney M20J, registered N701JM, was substantially damaged in an accident during initial climb near Palo Alto, California (Palo Alto airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed, 1 person was seriously injured and 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to maintain aircraft control during a go-around due to his premature flap retraction, which resulted in an aerodynamic stall and subsequent loss of control.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- September 4, 2018 · about 6:00 pm local time
- Place
- Palo Alto, California · Palo Alto · map
- Type
- Accident
- Injuries
- 1 person was killed, 1 person was seriously injured and 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Mooney M20J No Series, built 1992 · all M20Js on the register
- Registration
- N701JM · no longer on the register · serial 24-3281
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot was flying two passengers on an Angel Flight. When the airplane was about 10 miles north of the destination, the pilot contacted the air traffic control tower (ATCT). He was given instructions to fly to a charted VFR checkpoint, but then reported that he was not familiar with it and asked for directions from the controller. The pilot navigated to that checkpoint after several communications, and was then instructed to overfly a second checkpoint, about 2.5 miles north of the runway, as his left base leg for the arrival. The pilot was unable to locate the airport and requested ATCT assistance to advise him when to turn final, which the controller did. The pilot saw the airport and continued the approach. Witnesses observed the airplane touch down about mid-field and began to porpoise, alternately bouncing between the main and nose landing gear. After 3 to 4 oscillations, the pilot initiated a go-around and reported to the controller of the go-around. In response, the controller instructed the pilot to make a left closed traffic and asked if he needed assistance, to which the pilot replied “negative, I just came in too fast." The airplane climbed a few hundred feet and was then observed to enter a very steep left bank. The nose pitched sharply down, and the airplane descended rapidly to the ground. Examinations of the airplane and engine did not reveal any evidence of any pre-impact mechanical deficiencies or failures. Physical examination of the engine and propeller, combined with review of recorded engine operating parameter data, indicated that the engine operated normally, and was producing power at impact. The pilot’s logbook indicated that he had flown into that airport at least 32 times before, and therefore he should have been familiar with both the physical location of the airport and the names and locations of the local navigation fixes. Even if he had never been into that airport before, proper preflight planning dictates that he should have become familiar with those aspects. Data downloaded from the onboard GPS device revealed the airplane was about 10 to 15 knots above the manufacturer's approach speed (75 knots for the calculated landing weight) during final approach. The data also indicated that for most of the final approach, the airplane remained below the runway's 4° PAPI approach slope path The pitch trim was found slightly airplane nose down from the normal takeoff setting, but the flaps were found fully retracted. The manufacturer's go-around procedures called for full power, liftoff, and retraction of the flaps from the landing position (full down) to the takeoff position (approximately half) once the climb was established. Then, in sequence, this was to be followed by re-trimming in pitch, acceleration to 76 knots, landing gear retraction, flap retraction to the full-up position, and acceleration to 86 knots. Witnesses reported that the landing gear was retracted very soon after liftoff, making it likely that the pilot did not comply with the manufacturer's retraction sequence. The flaps-retracted 0° bank stall speed for the calculated airplane weight was about 58 knots, and the stall speed for 30° bank was about 63 knots. Takeoff flaps reduce these speeds by about 2 knots. Both the short amount of time between liftoff and the stall, and the stall itself, indicate that the pilot had fully retracted the flaps prior to achieving the prescribed speed of 86 knots. Based on the available information, speed mismanagement by the pilot, and a reduced stall margin due to the pilot prematurely retracting the flaps, caused the airplane to stall during the early portion of its go-around climb out at an altitude too low for recovery.
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
- Abnormal runway contact during landing (flare/touchdown)
- Abnormal runway contact during landing (aborted after touchdown)
- Aerodynamic stall/spin during initial climb defining event
The NTSB's findings
- Personnel issues › Task performance › Use of equip/info › Use of equip/system › Pilot
- factor Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Personnel issues › Action/decision › Action › Incorrect action sequence › Pilot
- cause Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
- Aircraft › Aircraft systems › Flight control system › TE flap control system › Incorrect use/operation
Pilot
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Flight time: 1,265 hours in all; 38 in this make and model
- Medical certificate: BasicMed
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 1,063 hours
- Last inspection: annual inspection, April 24, 2018
- Maximum gross weight: 2,900 lb
- Seats: 4
- Landing gear: retractable
- Engine: Lycoming IO-360-B1E (piston); 1,063 hours total
The flight
- Departed from: RDD Redding CA at 4:30 pm
- Destination: PAO Palo Alto CA
- Flight plan: none
- Runway 13, 2,443 ft by 70 ft
Weather at the time
- Light: daylight
- Wind: from 090° at 7 knots
- Visibility: 7 statute miles
- Sky: scat at 1,300 ft
- Temperature: 66°F (19°C), dew point 59°F (15°C)
- Altimeter: 29.92 inHg
- Observation at 6:08 pm from PAO
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
25 documents, released by the NTSB on December 2, 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.
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.
