# NTSB WPR21LA319: Piper PA-28-140, N1651J, Panguitch, UT, August 13, 2021

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Class 4 · Limited · Final report
- Date: August 12, 2021, 19:00 local (Aug 13, 2021, 01:00 UTC)
- Place: Panguitch, UT
- Coordinates: 37.855664, -112.388 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=37.8557&lon=-112.3880&mi=10
- Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping)
- Defining event: [Initial climb: Collision during takeoff/land](https://openairdocs.org/ntsb-events/490)
- Highest injury: No injuries
- Injuries: 3 uninjured
- Status: Completed
- Report: Approved by Office Director
- Investigation class: Class 4 - Basic report with no Prelim publish
- NTSB office: Western Pacific Region
- Parties: Federal Aviation Adminsitration
- NTSB case key (mKey): 103701
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=WPR21LA319
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/103701/pdf
- Page: https://openairdocs.org/ntsb/WPR21LA319

## Probable cause

The airplane’s inability to maintain altitude during the initial climb due to a degradation in the airplane’s performance due to high-density altitude conditions. Contributing to the accident was the pilot’s failure to conduct preflight performance planning calculations.

## Findings

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

- [Use of equip/info: use of equip/system](https://openairdocs.org/ntsb-findings/02063015): Personnel issues › Task performance · Pilot (probable cause); cases with it: [Piper PA-28-140, 16 cases](https://openairdocs.org/ntsb-findings/02063015/cases.md?model=7102802), [All aircraft, 1,391 cases](https://openairdocs.org/ntsb-findings/02063015/cases.md)
- [Planning/preparation: performance calculations](https://openairdocs.org/ntsb-findings/02061010): Personnel issues › Task performance · Pilot (probable cause); cases with it: [Piper PA-28-140, 8 cases](https://openairdocs.org/ntsb-findings/02061010/cases.md?model=7102802), [All aircraft, 114 cases](https://openairdocs.org/ntsb-findings/02061010/cases.md)
- [Temp/humidity/pressure: high density altitude](https://openairdocs.org/ntsb-findings/03031020): Environmental issues › Conditions/weather/phenomena · Effect on operation; cases with it: [Piper PA-28-140, 12 cases](https://openairdocs.org/ntsb-findings/03031020/cases.md?model=7102802), [All aircraft, 278 cases](https://openairdocs.org/ntsb-findings/03031020/cases.md)
- [Performance/control parameters: climb rate](https://openairdocs.org/ntsb-findings/01062035): Aircraft › Aircraft oper/perf/capability · Not attained/maintained (probable cause); cases with it: [Piper PA-28-140, 9 cases](https://openairdocs.org/ntsb-findings/01062035/cases.md?model=7102802), [All aircraft, 265 cases](https://openairdocs.org/ntsb-findings/01062035/cases.md)

## Sequence of events

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

- [Initial climb: Other weather encounter](https://openairdocs.org/ntsb-events/400); cases with it: [Piper PA-28-140, 11 cases](https://openairdocs.org/ntsb-events/400/sequence.md?model=7102802), [All aircraft, 1,127 cases](https://openairdocs.org/ntsb-events/400/sequence.md)
- [Initial climb: Collision during takeoff/land](https://openairdocs.org/ntsb-events/490) (defining event); cases with it: [Piper PA-28-140, 29 cases](https://openairdocs.org/ntsb-events/490/sequence.md?model=7102802), [All aircraft, 1,309 cases](https://openairdocs.org/ntsb-events/490/sequence.md)
- [Emergency descent: Off-field or emergency landing](https://openairdocs.org/ntsb-events/440); cases with it: [Piper PA-28-140, 56 cases](https://openairdocs.org/ntsb-events/440/sequence.md?model=7102802), [All aircraft, 3,365 cases](https://openairdocs.org/ntsb-events/440/sequence.md)

## Analysis

The pilot reported that, he conducted a maximum performance takeoff by adding full power and holding the brakes until engine RPM stabilized. The pilot released the brakes, and upon reaching rotation speed, the airplane drifted left. He maneuvered the airplane toward the runway centerline, and it touched down onto the runway briefly before it became airborne again. The airplane ascended to about 100 ft above ground level, before it began descending. The pilot stated that, there was no available runway remaining, so he initiated a forced landing to the uneven terrain ahead. During the landing roll, the airplane struck a fence and vegetation substantially damaging the fuselage. The pilot reported that prior to takeoff, he calculated the airplane’s weight with passengers and fuel, and determined it to be about 20 pounds under the maximum gross weight of the airplane. However, the pilot did not conduct preflight performance calculations prior to takeoff. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation and that if he took more time in preflight preparations, he would have noticed that the density altitude was too high to takeoff. The pilot operating handbook take-off distance vs. density altitude chart states “extrapolation of chart above 7,000 ft. [density altitude] is invalid. The calculated density altitude at the time of the accident was 9,000 ft mean sea level (msl).

## Aircraft

- Registration: [N1651J](https://openairdocs.org/deregistered/N1651J-2023-01-14), registration cancelled 2023-01-14, S/N 28-24044, built 1968 (OpenAirDocs)
- Reported make and model: PIPER PA-28-140
- Registry model: [Piper PA-28-140](https://openairdocs.org/model/piper-pa-28-140) (registry code 7102802) (OpenAirDocs)
- Registry engine: [Lycoming 0-320 series](https://openairdocs.org/engine/lycoming-0-320-series) (registry code 41508, reciprocating) (OpenAirDocs)
- Category: Airplane
- Serial number: 28-24044
- Year built: 1968
- Airframe hours: 6073.83
- Engines: Lycoming O-320 140 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Registered owner: Piper 140 LLC
- Airworthiness certificate: Standard, Normal
- Last inspection: Annual, December 1, 2020
- Airport: U55, Panguitch Muni, runway 36, 5,700 × 75 ft, asphalt
- Equipment: Stall warning system

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 38; injuries: none; airline transport; airplane ratings: multi-engine land, single-engine land; instrument ratings: airplane; medical: class 1, without waivers/limitations; last flight review October 1, 2020; seat: left; restraint: 3-point; flight hours: 9,429 total, 22 in this make and model, 7,106 as pilot in command, 171 in the last 90 days, 82 in the last 30 days

## Weather

- Conditions: Visual (VMC), Day
- Wind: 200° at 5 knots
- Visibility: 10 statute miles
- Temperature: 75 °F, dew point 43 °F
- Altimeter: 30.31 inHg
- Observed at: KBCE, 14 nm away
- METAR: KBCE 130053Z AUTO 20005KT 10SM FEW120 24/06 A3031 RMK AO2 SLP152 T02390061

## 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 20210812018579A](https://openairdocs.org/incident/20210812018579A), Aug 12, 2021: Piper PA-28-140, Panguitch, UT, Substantial damage. At 1600 MST the pilot in command (PIC) fueled N1651J to full capacity (50 gallons). The PIC and two passengers departed st. george regional airport (sgu) and…

## Other investigations on N1651J (1)

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.

- [NTSB LAX81DUJ68](https://openairdocs.org/ntsb/LAX81DUJ68), Jun 19, 1981: Piper PA-28 (N1651J), Elgin, AZ, substantial damage

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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