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Accidents · NTSB WPR18LA250 · Final report

Amateur-built GLASAIR SUPER IIS accident near Yuma, Arizona, August 27, 2018

On August 27, 2018 at about 5:36 pm local time, a 1995 amateur-built GLASAIR SUPER IIS, registered N8162H, was substantially damaged in an accident during enroute (cruise) near Yuma, Arizona (Yuma Mcas/Yuma Intl airport). It was a personal flight under general aviation rules (Part 91). 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

A total loss of engine power as a result of the detachment of the throttle linkage from the throttle arm of the fuel injector servo due to an insufficiently tightened and secured bolt and the subsequent inadequate maintenance inspection.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
August 27, 2018 · about 5:36 pm local time
Place
Yuma, Arizona · Yuma Mcas/Yuma Intl · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Amateur-built GLASAIR SUPER IIS RG, built 1995
Registration
N8162H · registry record · serial 2224
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The private pilot reported that, about 35 minutes into the personal cross-country flight, the experimental, amateur-built airplane's alternator field toggle switch/circuit breaker tripped. He reset the switch, and all systems appeared normal. About 5 minutes later, the switch tripped again, and the pilot cycled the switch. About 2 minutes later, the pilot noticed that the engine manifold pressure was dropping, along with the airplane's airspeed, consistent with a partial loss of engine power. The engine then experienced a total loss of power when he was maneuvering for an emergency landing to a nearby airport. The airplane subsequently landed short of the runway and sustained substantial damage to the aft fuselage. The engine had been installed about 91 flight hours and 5 months before the accident flight, and a condition inspection was completed the same month of installation. Maintenance records indicated that during the period between the engine installation and the accident, maintenance was limited to routine oil changes, magneto timing adjustments, the replacement of exhaust gas temperature and cylinder head temperature probes, and the installation of a replacement alternator. Postaccident examination of the engine revealed that the throttle linkage had detached from the throttle arm of the fuel injection servo. The rod end bearing for the linkage and the throttle arm were intact and undamaged, but the connecting bolt and its associated washers, castellated nut, and cotter pin were missing. The butterfly valve within the throttle body was in the closed position, and the throttle lever in the cabin was in the full forward (open) position. It is likely that the bolt securing the linkage had not been sufficiently tightened and secured with a cotter pin during the installation and that the error was not detected during the subsequent condition inspection. The investigation determined that the electrical system malfunction was unrelated to the loss of engine power.

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

  1. Loss of engine power (partial) during enroute (cruise) defining event
  2. Loss of engine power (total) during emergency descent
  3. Off-field or emergency landing during emergency descent
  4. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine fuel and control › Fuel control/carburetor › Incorrect service/maintenance
  • cause Aircraft › Aircraft power plant › Engine fuel and control › Fuel control/carburetor › Inadequate inspection
  • cause Personnel issues › Task performance › Maintenance › Installation › Maintenance personnel

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 1,598.4 hours in all; 298.3 in this make and model; 74.4 in the last 90 days; 13.5 in the last 30 days; 1,598.4 as pilot in command
  • Last flight review: October 2, 2017
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 2,020.5 hours
  • Last inspection: condition inspection, April 24, 2018; 91 hours since
  • Maximum gross weight: 2,200 lb
  • Seats: 4
  • Landing gear: retractable
  • Engine: Superior Air Parts IO-361-J1HD2 (piston); 91 hours total

The flight

  • Departed from: MYF San Diego CA at 4:42 pm
  • Destination: AVQ Marana AZ
  • Flight plan: none
  • Runway 21L, 9,240 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: at 4 knots
  • Visibility: 7 statute miles
  • Sky: scat at 20,000 ft
  • Temperature: 97°F (36°C), dew point 57°F (14°C)
  • Altimeter: 29.80 inHg
  • Observation at 5:57 pm from KNYL, 2 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

5 documents, released by the NTSB on December 6, 2018. 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.

#DocumentWhat it is
1 Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 PDF, 9 pages View Download
2 Dynon "Sky View Touch" Multifunction Display Data data file Download
3 Maintenance Logbook Excerpts PDF, 9 pages View Download
4 Statement of Party Representatives to NTSB Investigation PDF, 1 page View Download
5 Photographs PDF, 3 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.