# NTSB WPR11LA067: Piper PA 28-181, N4122F, Wittmann, AZ, December 1, 2010

- Type: NTSB accident investigation
- Classification: Accident · Minor injuries · Limited investigation · Final report
- Date: December 1, 2010, 10:45 local (17:45 UTC)
- Place: Wittmann, AZ
- Coordinates: 33.790279, -112.48278
- Nearby events: https://openairdocs.org/map.md?lat=33.7903&lon=-112.4828&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Defining event: [Enroute-cruise: Fuel starvation](https://openairdocs.org/ntsb-events/191)
- Highest injury: Minor injuries
- Injuries: 1 minor
- Status: Completed, report August 15, 2012
- Report: Approved by Office Director
- NTSB office: Western Pacific Region
- Parties: Piper Aircraft, Inc., Federal Aviation Administration, TransPac Aviation Academy
- NTSB case key (mKey): 77916
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=WPR11LA067
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/77916/pdf
- NTSB docket: https://data.ntsb.gov/Docket?ProjectID=77916
- Page: https://openairdocs.org/ntsb/WPR11LA067

## Probable cause

The pilot’s improper fuel management, which resulted in a total loss of engine power due to fuel starvation.

## Findings

NTSB's coded findings; those marked are part of the probable cause.

- [Fluids: fuel](https://openairdocs.org/ntsb-findings/01071010): Aircraft › Fluids/misc hardware · Fluid management (probable cause); cases with it: [All aircraft, 1,695 cases](https://openairdocs.org/ntsb-findings/01071010/cases.md)
- [Fluids: fuel](https://openairdocs.org/ntsb-findings/01071010): Aircraft › Fluids/misc hardware · Fluid level (probable cause); cases with it: [All aircraft, 1,695 cases](https://openairdocs.org/ntsb-findings/01071010/cases.md)
- [Use of equip/info: use of equip/system](https://openairdocs.org/ntsb-findings/02063015): Personnel issues › Task performance · Pilot (probable cause); cases with it: [All aircraft, 1,391 cases](https://openairdocs.org/ntsb-findings/02063015/cases.md)

## Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event best describes what happened.

- [Enroute-cruise: Fuel starvation](https://openairdocs.org/ntsb-events/191) (defining event); cases with it: [All aircraft, 733 cases](https://openairdocs.org/ntsb-events/191/sequence.md)
- [Enroute-cruise: Loss of engine power (total)](https://openairdocs.org/ntsb-events/341); cases with it: [All aircraft, 3,820 cases](https://openairdocs.org/ntsb-events/341/sequence.md)
- [Enroute-descent: Off-field or emergency landing](https://openairdocs.org/ntsb-events/440); cases with it: [All aircraft, 3,365 cases](https://openairdocs.org/ntsb-events/440/sequence.md)
- [Landing-landing roll: Collision with terr/obj (non-CFIT) ](https://openairdocs.org/ntsb-events/470); cases with it: [All aircraft, 10,189 cases](https://openairdocs.org/ntsb-events/470/sequence.md)

## Analysis

The student pilot was making a solo cross-country flight involving four flight legs. Before beginning the final return leg, he completed multiple full stop landings and touch-and-go landings that he had not included in his preflight planning. During the final leg, the engine began to lose power. The student pilot switched the fuel selector valve to the left tank, but then switched it back to the right tank after a short period of time. The engine subsequently lost all power, and the student pilot made a forced landing in rough terrain. Postaccident examination revealed that the right fuel tank was not breached and was empty of fuel. The left fuel tank was breached, and the soil beneath the tank was wet with fuel. After the wreckage was recovered, a fuel delivery system was rigged, and the engine was started and continued to run as the fuel selector was positioned to both the right and left fuel tank positions. According to the pilot operating handbook for the airplane, if the pilot allows a tank to run dry and the engine loses power, it may take up to 10 seconds for fuel to reach the engine after the other tank is selected. It is likely that, after running the right tank dry, the pilot did not leave the selector in the left tank position for long enough to allow fuel to reach the engine.

## Factual narrative

HISTORY OF FLIGHT On December 1, 2010, about 1045 mountain standard time (MST), a Piper PA 28-181, N4122F, experienced a loss of engine power, and the pilot made a forced landing near Wittmann, Arizona. TransPac Aviation Academy was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The student pilot sustained minor injuries; the airplane sustained substantial damage to the fuselage and right wing. The solo cross-country instructional flight departed Deer Valley Airport (DVT), Phoenix, Arizona, about 0700, with a planned route of flight to Wickenburg, Arizona (E25), to Gila Bend, Arizona, back to E25, and then back to DVT. Visual meteorological conditions prevailed, and no flight plan had been filed. The student pilot reported that during the solo cross-country flight, specifically the last leg from E25 to DVT, the engine started to run rough and he was unable to maintain altitude. He made a forced landing in the desert near Wittmann. A Federal Aviation Administration (FAA) accident coordinator responded to the scene, and documented the accident site. During the recovery it was noted that the right fuel tank was not breeched, but contained no fuel. The left fuel tank’s drain had been damaged during the crash sequence. No fuel was found in the tank; however, the ground below the damaged fuel drain smelled of fuel, and was wet for several inches down in the dirt, covering an area of at least a 12” diameter. The student pilot was interviewed by the (FAA) accident coordinator. The student pilot related that he had intended to only complete one full stop landing with a taxi back for takeoff. However, during the second time at E25 on his return, the student pilot made two additional full stop taxi backs and two touch-and-goes. The student pilot stated that he felt the engine vibrate during the final approach to E25. The FAA coordinator asked him why he did not land at E25 and call for maintenance. The student pilot said he “didn’t feel it was that bad.” The student pilot also stated that he needed to return to DVT. The student pilot attempted to return to DVT. However, while en route, the engine lost partial power. The student pilot said he switched to the left tank, but only for a short period of time. He then switched it back to the right tank. Prior to landing, the engine completely quit, and the airplane landed in a desert wash. The airplane sustained damage to the left wing, both main landing gear, and the nose gear. On December 8, 2010, investigators conducted an exam of the wreckage at Air Transport, Inc., Phoenix. During the examination, the airframe and engine were secured, and a temporary fuel delivery system was configured. The engine was started using both the left and right fuel selection positions. No abnormalities were noted that would have precluded normal operations. The Piper PA28-181 Pilot Operating Handbook addressed a loss of engine power. It states if the engine quits due to fuelexhaustion, it will take up to 10 seconds for fuel to reach the engine with the fuel pump on.

## Aircraft

- Registration: N4122F (not matched to a registry record)
- Reported make and model: PIPER PA 28-181
- Category: Airplane
- Serial number: 2843118
- Airframe hours: 8558
- Engines: Lycoming O-360-A4M 180 horsepower reciprocating
- Damage: Substantial damage
- Flight: Instructional, Part 91
- Operator: TransPac Aviation Academy
- Registered owner: Bird Acquisition LLC
- Airworthiness certificate: Standard, Normal
- Last inspection: Continuous airworthiness, November 28, 2010, 24 hours before
- Departed: E25, Wickenburg, AZ
- Destination: DVT, Phoenix, AZ

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Student pilot; age 21; injuries: minor; student; medical: class 3, without waivers/limitations; seat: left; flight hours: 61 total, 61 in this make and model, 7 as pilot in command, 61 in the last 90 days, 33 in the last 30 days, 3 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: variable at 1 knots
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 57 °F, dew point 18 °F
- Altimeter: 30.19 inHg
- Observed at: LUF, 16 nm away

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 20101201053399A](https://openairdocs.org/incident/20101201053399A), Dec 1, 2010: Piper PA-28-181, Surprise, AZ, Substantial damage. The aircraft made a forced landing in a field 15 miles n. luke afb. The accident site was on the abandoned chrysler proving grounds in Surprise AZ.. The first…

## Docket (3 files)

The files NTSB released with the investigation on June 22, 2012, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=77916. 1.5 MB in all.

- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1 (item 1, .PDF, 830 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40369783&FileExtension=.PDF&FileName=Pilot%2FOperator%20Aircraft%20Accident%20Report,%20NTSB%20Form%206120.1-Redacted.PDF
- NTSB Field Exam Report (item 2, .PDF, 444 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40369785&FileExtension=.PDF&FileName=NTSB%20Field%20Exam%20Report-Redacted.PDF
- Statement of Party Representatives to NTSB Investigation (item 3, .PDF, 274 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40369786&FileExtension=.PDF&FileName=Statement%20of%20Party%20Representatives%20to%20NTSB%20Investigation-Redacted.PDF

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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