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LAX97FA272 · Piper PA-28RT-201 PA-28RT-20

5 Aug 1997 · Hesperia, CA, United States

Piper PA-28RT-201 PA-28RT-20 · Accident: partial loss of engine power (non-mechanical) on approach

From Monterey Regional Airport (MRY) to Hesperia Airport (L26)

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Event

NTSB case
LAX97FA272
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
3 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Piper PA-28RT-201 PA-28RT-20

Aircraft type
Piper PA-28
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N8227Q
Operator
Brett R. Allen · private individual
Onboard fatalities
Unknown
Route
From Monterey Regional Airport (MRY), San Jose, CATo Hesperia Airport (L26), CA
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Approach · VFR go-around
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Partial loss of engine power (non-mechanical)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Wire, transmission
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Pilot in command › Altitude/clearance, not maintained
  • Pilot in command › Visual lookout, inadequate

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

Following a go-around in high density altitude conditions, the airplane was observed to enter a shallow climb. It then turned approximately 20 degrees to the right and followed a wide depression in the surrounding terrain without any noticeable gain in altitude. While following this depression, three packages (luggage) were observed being thrown from the right side of the aircraft. After the third package was thrown, the aircraft flew into high voltage power lines, which ran perpendicular to the depression at an altitude of approximately 75 to 100 feet agl. The aircraft then impacted the ground and was destroyed by fire. There were no orange balls or other visually alerting devices attached to the power lines, as the power lines were not in a location normally used by low flying aircraft. A teardown inspection of the engine did not disclose any mechanical malfunction or abnormal wear; however, the exhaust muffler for the No. 2 and No. 4 cylinders had a partially collapsed internal baffle. Density altitude was about 7,200 feet. Aircraft performance charts indicated that at that altitude, the engine would have been developing only 72 percent of its rated power.

Probable cause

failure of the pilot to see-and-avoid high voltage power lines, while coping with a lack of engine power during a go-around in a high density altitude condition. Factors relating to the accident were: high density altitude that resulted in a normal reduction of engine power; partial obstruction in the exhaust system that resulted in an additional loss of power; and the encounter with power lines.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX97FA272
Event ID
20001208X08660
Case number
LAX97FA272
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: ac25402e642a1cadd47db0f26518f9713f76707a14c63da7f97ba777af2ce2b2; retrieved 2026-09-20T22:52:12.421Z.