Mcdonnell Douglas Helicopter 369E accident near Mesa, Arizona, June 8, 2014
On June 8, 2014 at about 7:56 am local time, a 1995 Mcdonnell Douglas Helicopter 369E, registered N504MP, was substantially damaged in an accident during enroute (cruise) near Mesa, Arizona (Falcon Fld airport). It was a public-use flight (local) under public-use (government) rules. 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 loss of engine power during cruise flight due to the decoupling of the engine’s turbine and compressor sections. Contributing to the decoupling was the excessive wear of the turbine-to-compressor coupling components due maintenance personnel’s placement of an incorrect shim during a compressor section overhaul and a latent misalignment within the exhaust collector.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 8, 2014 · about 7:56 am local time
- Place
- Mesa, Arizona · Falcon Fld · map
- Type
- Accident
- Injuries
- No one was hurt; 2 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Mcdonnell Douglas Helicopter 369E, built 1995 · all 369Es on the register
- Registration
- N504MP · registry record · serial 0523E
- Damage
- Substantial damage
- Flight
- Public-use flight (local) · public-use (government) rules
The NTSB's narrative final · quoted from the NTSB record
The commercial pilot was conducting a nighttime law enforcement patrol flight in the helicopter. The pilot reported that, about 1.4 hours into the flight, the engine lost all power, and he subsequently performed an autorotation to an unlit empty field. The helicopter landed hard, and the main rotor blades subsequently struck and severed the tailboom. Postaccident examination of the engine revealed excessive wear in the turbine-to-compressor coupling components. The turbine-to-compressor coupling had moved, which caused its forward splines to contact the spur adapter gear shoulder and its rear splines to disengage from the turbine-splined adapter. The disengagement caused the decoupling of the turbine section from the compressor section and the subsequent loss of engine power. The excessive wear was determined to be the result of a misalignment of the engine's centerline shafting components. Two areas of misalignment were found. The first misalignment was caused by the incorrect placement of two shims at the interface between the rear diffuser and gearbox. A review of the engine maintenance logbooks revealed that maintenance personnel had placed these shims during the last compressor section overhaul, about 2 years or 1,432.1 flight hours before the accident. The second misalignment was found between the forward and rear pilot diameter bores of the exhaust collector assembly, which exhibited excessive runout when compared to engineering drawings. The maintenance records showed that, about 9 months before the accident, the exhaust collector assembly was reworked in accordance with the engine manufacturer's maintenance manual, which did not call for a runout check of the forward-to-rear pilot diameters but rather a runout check of both pilot diameters independently with reference to the bearing bore. At the time of rework, the runout-to-bearing bore values were within tolerance. Therefore, it is likely that the discrepancy was latent, predating the accident by a long period of time, and was not significant enough to cause previous shafting misalignment. Although neither of the misalignments individually were likely significant, cumulatively, they produced sufficient misalignment to cause the observed wear.
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 engine power (total) during enroute (cruise) defining event
- Autorotation Off-field or emergency landing
- Autorotation Loss of visual reference
- Hard landing during landing (flare/touchdown)
The NTSB's findings
- cause Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Compressor section › Fatigue/wear/corrosion
- cause Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Turbine section › Fatigue/wear/corrosion
- factor Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Compressor section › Incorrect service/maintenance
- factor Personnel issues › Task performance › Maintenance › Scheduled/routine maintenance › Maintenance personnel
- factor Aircraft › Aircraft power plant › Engine exhaust › Collector/nozzle › Damaged/degraded
Pilot
- Certificate: commercial pilot
- Ratings: rotorcraft: helicopter
- Flight time: 826 hours in all; 826 in this make and model; 125 in the last 90 days; 61 in the last 30 days; 701 as pilot in command
- Last flight review: June 5, 2013
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: left
- Injury: no injuries
Other crew
- Certificate: flight instructor, commercial pilot
- Ratings: single-engine land; instructor: airplane single-engine; instructor: helicopter; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
- Flight time: 4,582.2 hours in all; 3,760.8 in this make and model; 101.4 in the last 90 days; 39.5 in the last 30 days; 4,466.2 as pilot in command; 130.6 on instruments
- Last flight review: September 20, 2012
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: no injuries
The aircraft
- Airframe total time: 19,921 hours
- Last inspection: continuous airworthiness programme, June 5, 2014; 8 hours since
- Maximum gross weight: 3,000 lb
- Seats: 4
- Landing gear: fixed
- Engine: Rolls-Royce 250-C20 (turboshaft); 15,350 hours total
- Operator: City Of Mesa
The flight
- Departed from: FFZ Mesa AZ at 11:15 pm
- Destination: FFZ Mesa AZ
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: night
- Wind: from 310° at 5 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 90°F (32°C), dew point 32°F (0°C)
- Altimeter: 29.67 inHg
- Observation at 7:55 am from KPHX, 13 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
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.
