Piper PA-31-350 accident near Scottsdale, Arizona, December 11, 1999
On December 11, 1999 at about 1:00 am local time, a Piper PA-31-350, registered N27181, was substantially damaged in an accident near Scottsdale, Arizona. It was a flight of an unrecorded kind under charter and air-taxi rules (Part 135). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to follow the manufacturer's published emergency procedures for engine loss of power resulting in a forced landing in an open construction area where the airplane collided with a berm. A related factor was the loss of engine power in the left engine due to fuel starvation.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 11, 1999 · about 1:00 am local time
- Place
- Scottsdale, Arizona · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA-31-350 · all PA-31-350s on the register
- Registration
- N27181 · no longer on the register · serial 31-7752068
- Damage
- Substantial damage
- Flight
- Flight of an unrecorded kind · charter and air-taxi rules (Part 135)
The NTSB's narrative final · quoted from the NTSB record
The airplane collided with a berm in a construction area after making an emergency landing. Following a flight of about 1.5 hours and after starting a descent, the pilot felt the left engine surge, and saw the left boost pump warning light flashing. The left engine continued to surge and the boost pump light remained fully illuminated. He chose not to feather the left propeller. He engaged both emergency fuel boost pumps and advanced the throttles and propellers for both engines. In this configuration the engines did not produce enough power to sustain flight. ATC identified two nearby airports for the pilot; one airport was 6 miles away and the other was 2 miles away. At 4,000 feet agl, the pilot felt he would not make either airport. According to the manufacturer's published emergency procedures, once an inoperative engine has been identified and an unsuccessful engine restart attempt is made, the pilot should feather the propeller. During the recovery, personnel noted that the inboard fuel tanks were full of fuel. Both outboard tanks were empty; however, fuel was found on the ground by one of the outboard fuel tanks. According to the operator, once a month the pilot's are encouraged to burn out the fuel in the outboard fuel tanks in VFR conditions. Following the accident, a functional check was conducted of the continuous duty fuel boost pumps and emergency fuel boost pumps. No discrepancies were noted. According to the pilot's operating handbook (POH), the continuous duty fuel boost pump warning lights will illuminate when pressure to the system drops below 3 PSI or the boost pumps have failed. Engagement of the emergency fuel boost pumps provides steady fuel pressure. The POH further reports that the fuel system has right and left fuel warning lights. The fuel flow warning lights illuminate to warn the pilot of an impending fuel flow interruption. These lights are located underneath the fuel boost pump warning lights. If the fuel level near the tank outlet drops to a point where a fuel flow interruption and power loss could occur, a sensing probe will illuminate its corresponding warning light. An inspection of the fuel system revealed that the system was intact and operated normally. The cross feed valves were operated and fuel was observed to flow to each engine from the opposite side wing fuel tank. No mechanical anomalies were noted.
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
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 4,000 hours in all; 26 in this make and model
- Medical certificate: Class 1 (valid medical--w/ waivers/lim.)
- Seat: left
The aircraft
- Airframe total time: 8,659 hours
- Last inspection: approved inspection programme, November 18, 1999
- Maximum gross weight: 7,000 lb
- Seats: 2
- Landing gear: retractable
- Engine: Lycoming L/TI0-540 (piston); 0 hours total
- Operator: Union Flights INC
The flight
- Departed from: FLG Flagstaff AZ
- Destination: PHX Phoenix AZ
- Flight plan: VFR
- Runway 0
Weather at the time
- Light: dusk
- Wind: from 260° at 4 knots
- Visibility: 30 statute miles
- Sky: broken clouds at 20,000 ft; clear
- Temperature: 57°F (14°C), dew point 18°F (-8°C)
- Altimeter: 29.00 inHg
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
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.