N535SA

Substantial
None

AERO COMMANDER 500 SS/N: 3138

Accident Details

Date
Tuesday, July 24, 2012
NTSB Number
WPR12TA323
Location
Elko, NV
Event ID
20120723X90207
Coordinates
40.760833, -115.687225
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A loss of power due to fuel exhaustion. Contributing to the accident were the pilot's failure to comply with required fueling procedures and the pilot's poor decision-making in not monitoring his fuel gauge and turning back when it reached minimum fuel.

Aircraft Information

Registration
N535SA
Make
AERO COMMANDER
Serial Number
3138
Engine Type
Reciprocating
Model / ICAO
500 SAC50
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Status
Deregistered
Country
United States

Analysis

HISTORY OF FLIGHT On July 23, 2012, about 1745 Pacific daylight time, an Aero Commander 500 S, N535SA, was substantially damaged during an off-airport forced landing near Elko, Nevada, due to the complete loss of power in both engines. Neither the pilot nor the Air Tactical Group Supervisor (ATGS) was injured. The public-use flight was performing an air-attack coordination mission for aerial fire suppression activity. The airplane was owned by Spur Aviation Services of Twin Falls, Idaho, and was being operated on an exclusive use contract by the United States Department of the Interior, Bureau of Land Management (DOI/BLM). No Federal Aviation Administration (FAA) flight plan was filed for the flight.

A Fire Traffic Area was established and aviation support was controlled by the ATGS. The flight departed Elko International airport (EKO), Elko, about 1315, and flew to the vicinity of the fire, located about 15 minutes east of EKO. Interagency Dispatch Center (IDC) records indicated that at 1319, the pilot radioed that they were airborne, with 4 hours 30 minutes of fuel on board. The airplane loitered in the vicinity of the fire to enable the ATGS to coordinate the air attacks. About 1730, the pilot notified the ATGS that they had to depart the fire locale for a return to EKO, and shortly thereafter, the airplane turned on course for EKO.

While en route back to EKO, at a point that the ATGS estimated was 4 to 5 minutes away from EKO, the engines started "surging," and soon thereafter, the engines ceased developing power. The pilot decided that due to distance and terrain considerations, he would land off-airport instead of attempting to return to EKO. Although the airplane was in the vicinity of a four-lane highway, the pilot opted to land on a two-lane highway due to significantly less vehicular traffic on that highway. About 1744, the flight radioed IDC that the pilot was planning to conduct an off-airport landing. About 1751, the flight radioed that they had landed on Nevada State Highway 228, and that the occupants were uninjured, but that the airplane was damaged.

PERSONNEL INFORMATION

Pilot

The pilot held multiple pilot certificates (including Airline Transport Pilot) and ratings, and was appropriately certificated and rated for the accident airplane make and model. The pilot's records indicated that he had a total flight experience of about 16,800 hours, including about 1,500 hours in the accident airplane make and model. His most recent FAA second-class medical certificate was issued in April 2012, and his most recent flight review was completed in May 2012. In addition, he was properly certificated ("carded") by the DOI Office of Aviation Services (OAS) for the mission.

The pilot was employed by Spur Aviation Services. He completed his company-provided fire-mission flight and ground training, which is conducted annually prior to the each fire season, on May 23, 2012. His ground training session was 8 classroom hours, and included company-created modules regarding the airplane fuel system, fuel handling and management, and flight planning.

The pilot had been stationed at Elko since July 9, 2012. Since that time, he operated within the applicable crew day and flight hour requirements. His records indicated that he had flown the accident airplane make and model 121 hours in the previous 30 days, and 22 hours in the previous 10 days. The pilot stated that, on the day of the accident, he began his day with a good breakfast, and that he was well rested.

Air Tactical Group Supervisor (ATGS)

The ATGS was employed by the BLM. The Interagency Aerial Supervision Guide (IASG) was a primary guidance document for the conduct of BLM fire suppression operations, and the ATGS was qualified and current to conduct fire suppression missions in accordance with the IASG. According to the then-current IASG, in addition to aerial supervision of the fire suppression efforts, the ATGS was to "assist the pilot as requested with crew duties." Although not required for ATGS certification, the Crew Resource Management (CRM) course was cited in the IASG as a training opportunity that "should be considered prior to initial certification or as a supplemental or refresher training (for) individuals currently certified as air tactical group supervisors." The ATGS completed the CRM course in April 2007. It was not determined whether the ATGS had obtained any pilot training, or held any pilot certificates.

AIRCRAFT INFORMATION

FAA information indicated that the airplane was manufactured in 1972, and was equipped with two Lycoming TIO-540 series piston engines. At the time of the accident, the airplane had accumulated a total time in service (TT) of 6,443 hours, and each engine had accumulated a TT since overhaul of 1,323 hours. The airplane was maintained under an FAA-approved inspection program, and its most recent inspection was completed on July 16, 2012.

The airplane was certificated ("carded") in accordance with DOI/OAS policies and procedures, and met all requirements of the applicable BLM exclusive-

+use contract.

METEOROLOGICAL INFORMATION

Recorded weather information at EKO indicated that between 1256 and 1656 inclusive, there was significant weather activity. That activity included strong winds, stronger gusts, heavy rain, and thunderstorms. During the attempted flight leg from the fire area back to EKO, the winds were recorded as gusting to about 20 mph from the north-northwest; that wind direction presented a headwind for the returning airplane.

WRECKAGE AND IMPACT INFORMATION

The airplane landed on a straight section of two-lane highway that was about 2,300 feet long, and located about 6 miles southeast of EKO. The landing site elevation was about 5,300 feet above mean sea level. IDC records indicated that the airplane was pushed clear of the road about 1830.

Personnel from the FAA, BLM,.032 and DOI examined the airplane 2 days after the event. The airplane sustained substantial damage to the outboard leading edges of the left and right wings due to impacts with highway signs located on each side of the road.

Electrical power was applied to the airplane, and the fuel quantity gauge registered "0," which indicated that the fuel tanks were devoid of usable fuel. Investigators opened the fuel sump drain line to determine the amount of fuel remaining in the fuel tanks. About 3/4 gallon of fuel was drained from the airplane, which was consistent with the fuel quantity gauge indication.

The airplane was examined to determine if the lack of fuel was due to a fuel leak. There was no evidence of discoloration or residue on the airplane that would indicate a fuel leak. The airplane was refueled, and a fuel leak check was conducted. Again, no evidence of a fuel leak was observed.

Temporary wing repairs were accomplished on the airplane, and it was flown successfully from the accident site to EKO, and subsequently to Oregon for permanent repairs. Both flights were uneventful, with no indications of any fuel- or engine-related abnormalities.

ADDITIONAL INFORMATION

Airplane Fuel System

The airplane had a usable fuel capacity of 156 gallons, distributed in five interconnected tanks. The fuel quantity indication system utilized a mechanical float located in the main fuel cell. The fuel quantity gauge indication was limited to 135 gallons, with index marks in 10 gallon increments from 0 to 120 gallons. The next index mark was also the uppermost, and indicated 135 gallons. Since the indicated quantity could not exceed 135 gallons, the only way to determine whether the actual fuel quantity was above that level or full was to open the wing refueling port, and visually check the fuel quantity.

Maintenance records indicated that the fuel quantity indication system was last calibrated in May 2011, about 14 months prior to the accident. Per the airplane maintenance manual, the "Indicator reading shall never read more than [the] usable fuel." In the period between the calibration and the accident, there were no maintenance write-ups or actions concerning the fuel quantity indication system.

Fueling Procedures

Spur Aviation Services' Operations Manual (OM) contained the following statements regarding the pilot-in-command's (PIC) responsibilities with regard to fuel:

- The PIC "is responsible for fueling...his aircraft...at all times."

- "…fueling of aircraft at any location shall be performed by the Pilot in Command or by any other company personnel under his supervision…"

- "It shall be the responsibility of the Pilot in Command to check the amount of fuel serviced at each station and correlate this amount with the total fuel as reported by the servicing agent and as indicated by the fuel gauges."

In addition, the Spur Aviation Services fuel system ground training presentation module contained the following two statements:

- "Pilots must be present during refueling"

- "At each refueling [the] pilot will remove and reinstall fuel cap themselves"

The pilot reported that he was present during the fueling of the airplane. However, the fixed base operator line personnel stated that the pilot left the airplane before refueling was completed. The investigation did not determine whether the pilot removed and reinstalled the fuel cap, or whether he cross-checked the serviced and indicated fuel quantities.

The ATGS reported that he had assisted in the refueling of the airplane, which was contrary to the BLM contract for the airplane. The contract stated that BLM "personnel are not involved with refueling of contract aircraft unless the pilot has determined that it is an absolute necessity due to an emergency situation." However, the BLM guidance (IASG) was in conflict with that contract, since it required the ATGS to "confirm the fuel supply and flight time available for the flight."

Flight Planning and Fuel Burn

Spur Aviation Services' OM stated that the PIC "Prepares or supervises preparation of a flight plan c...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR12TA323