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CHI89DEC02 · Piper PA-28R-201

21 Jan 1989 · Brighton, MI, United States

Piper PA-28R-201 · Accident: total loss of engine power (mechanical failure) en route

From Oakland County International Airport (PTK) to Jackson County Airport/Reynolds Field (JXN)

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Event

NTSB case
CHI89DEC02
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
0 · 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-28R-201

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
N3536M
Operator
Unknown
Onboard fatalities
Unknown
Route
From Oakland County International Airport (PTK), Pontiac, MITo Jackson County Airport/Reynolds Field (JXN), Jackson, MI
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
En route · cruise
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
Total loss of engine power (mechanical failure)
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

  • Fluid, oil › Exhaustion
  • Fluid, oil › Leak
  • Lubricating system, oil quickdrain/drain plug › Improper
  • Lubricating system, oil quickdrain/drain plug › Open
  • Other maintenance personnel › Maintenance, compliance with ad, not followed
  • Other maintenance personnel › Maintenance, installation, improper

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

NTSB narrative

THE PLT WAS ON A X-COUNTRY FLT WHEN HE NOTICED THE OIL PRESSURE WAS DECREASING RAPIDLY. HE ELECTED TO MAKE AN OFF-AIRPORT LANDING, BUT THE ENGINE SEIZED BEFORE HE COULD REACH THE SELECTED AREA. SUBSEQUENTLY, THE AIRCRAFT WAS DAMAGED DURING A WHEELS UP LANDING. INITIAL TOUCHDOWN WAS ON A GRAVEL ROAD AND THE ACFT HIT A BERM BEFORE SLOWING TO A STOP. AN EXAM OF THE AIRCRAFT AND ENGINE REVEALED AN OIL (QUICK) DRAIN VALVE (AEROQUIP PN: AE80664H) HAD BEEN INSTALLED ON 7/10/87. IT WAS INSTALLED WITH A 4-3/8 INCH HOSE THAT EXTENDED BELOW THE ENGINE RESERVOIR, IN THE VICINITY OF THE LANDING GEAR. SUBSEQUENTLY, THE DRAIN VALVE WAS PUSHED OPEN BY MOVEMENT OF THE LANDING GEAR AS IT WAS BEING RETRACTED. THIS RESULTED IN LOSS OF OIL & SUBSEQUENT ENGINE SEIZURE. THIS DRAIN VALVE WAS NOT APPROVED FOR INSTALLATION ON THIS MODEL OF AIRCRAFT. PIPER SERVICE LETTER 910 & AD 81-11-02/R1 SPECIFIED USE OF ANOTHER VALVE (PIPER PN: 492-172V).

Probable cause

INSTALLATION OF AN IMPROPER OIL DRAIN VALVE BY OTHER MAINTENANCE PERSONNEL AND THEIR FAILURE TO FOLLOW THE APPLICABLE AIRWORTHINESS DIRECTIVE (AD 81-11-02/R1), RESULTING IN SUBSEQUENT INTERFERENCE BETWEEN THE LANDING GEAR AND OIL DRAIN VALVE. THIS CAUSED THE VALVE TO MOVE OPEN & LEAK, WHICH RESULTED IN THE LOSS OF ALL ENGINE OIL.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CHI89DEC02
Event ID
20001213X27548
Case number
CHI89DEC02
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: 18bec2a908d43960f4f87112b66db2e3fa171fdf1bc74f5d088e12aecdf6e711; retrieved 2026-09-21T15:58:53.777Z.