Fuel exhaustion Accident Cessna T337D Turbo Super Skymaster N337J,
ASN logo
ASN Wikibase Occurrence # 196563
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Friday 7 July 2017
Time:07:35
Type:Silhouette image of generic C337 model; specific model in this crash may look slightly different    
Cessna T337D Turbo Super Skymaster
Owner/operator:Private
Registration: N337J
MSN: 337-1017
Year of manufacture:1968
Total airframe hrs:2591 hours
Engine model:Continental IO-360
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Greenwood County Airport (KGRD), Greenwood, SC -   United States of America
Phase: Landing
Nature:Training
Departure airport:Greenwood, SC (GRD)
Destination airport:Greenwood, SC (GRD)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The flight instructor and private pilot, who did not have a multiengine rating, were conducting a familiarization flight in the centerline thrust, multiengine airplane. Following the preflight inspection, the instructor and the pilot believed that both fuel tanks were about 1/2 to 3/4 full. After practicing maneuvers uneventfully for about 30 minutes, the front engine lost all power. The instructor told the pilot to return to the departure airport; the rear engine was operating at this time. However, before reaching the airport, the rear engine lost all power. With insufficient altitude remaining to reach a runway, the pilot transferred control to the instructor, who then conducted a forced landing into trees.

Postaccident examination of the accident site revealed no smell of fuel, and only about 6 gallons of fuel (of a possible 131 gallons with all fuel tanks filled to capacity, 3 gallons of which were unusable) were recovered from both wing fuel tanks. Examination of both engines revealed no evidence of any preaccident mechanical malfunctions or failures that would have precluded normal operation. The four fuel quantity sender units (two for each main fuel tank) were removed and tested with an ohm meter. In the empty position, the left outboard fuel sender unit displayed a resistance value equal to an approximate 1/2-tank reading. The left and right inboard fuel sender units displayed a resistance value equal to an approximate full-tank reading. The right outboard fuel sender unit displayed inconsistent resistance readings throughout its range of travel.

The airplane manufacturer published a mandatory service bulletin (SB) about 18 years before the accident, which required inspection of the fuel quantity indicating system to verify that each fuel gauge indicated the accurate fuel amount. The SB also required that an initial inspection of the system be completed within 100 hours of operation and subsequent recurring inspections every 12 months. Examination of the airplane's maintenance logbooks revealed no evidence of compliance with the SB.

Given the lack of fuel found at the accident site and that postaccident examination of the engines revealed no mechanical issues, it is likely that the pilots did not adequately verify the quantity of fuel during the preflight inspection, in part due to erroneous fuel quantity indications provided by the fuel quantity indicating system, which resulted in fuel exhaustion and a subsequent loss of all engine power to both engines. The airplane operator's failure to comply with the SB precluded the pilots from being able to identify the fuel quantity in flight.

Probable Cause: The pilots' inadequate preflight inspection, during which they failed to adequately verify the quantity of fuel, which resulted in fuel exhaustion, a subsequent total loss of power to both engines, and a forced landing into trees. Contributing to the accident were the erroneous fuel quantity displayed by the fuel quantity indicating system fuel sender units and the operator's failure to comply with a mandatory service bulletin addressing inaccuracies in the fuel quantity indicating system.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA17LA235
Status: Investigation completed
Duration: 2 years and 9 months
Download report: Final report

Sources:

NTSB

FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=337J

Location

Media:

Revision history:

Date/timeContributorUpdates
07-Jul-2017 14:09 Geno Added
07-Jul-2017 16:38 Iceman 29 Updated [Time, Total occupants, Source, Embed code, Damage, Narrative]
22-Apr-2020 17:04 ASN Update Bot Updated [Time, Operator, Nature, Departure airport, Destination airport, Source, Embed code, Damage, Narrative, Accident report, ]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org