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LAX90LA035 · Cessna 177RG

17 Nov 1989 · Van Nuys, CA, United States

Cessna 177RG · Accident: total loss of engine power (mechanical failure) on approach

From Van Nuys Airport (VNY) to an unrecorded destination

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Event

NTSB case
LAX90LA035
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

Cessna 177RG

Aircraft type
Cessna 177
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
N2069Q
Operator
William A. Ryan · private individual
Onboard fatalities
Unknown
Route
From Van Nuys Airport (VNY)To not recorded
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 pattern downwind
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)
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
Substantial

Cause areas

  • Cooling system, baffle › Incorrect
  • Cooling system, cowling › Incorrect
  • Engine assembly, crankcase › Failure, total
  • Engine assembly, cylinder › Distorted
  • Engine assembly, cylinder › Overtemperature
  • Fluid, oil › Failure, total
  • Fluid, oil › Leak
  • Other maintenance personnel › Maintenance, installation, improper

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

NTSB narrative

NEAR THE END OF THE FIRST FLIGHT FOLLOWING INSTALLATION OF AN OVERHAULED ENGINE, THE ENGINE SIEZED AFTER THE PILOT NOTICED A RAPID DROP IN OIL PRESSURE. AFTER THE ACCIDENT, THE LEFT SIDE LOWER EXTERIOR FUSELAGE WAS FOUND TO BE COVERED WITH FRESH OIL, WITH THE OIL SMEAR ORIGINATING NEAR THE OIL BREATHER LINE. THE ENGINE COWL BAFFLE SEALS WERE FOUND INSTALLED INCORRECTLY. LESS THAN 1 QUART OF OIL WAS FOUND IN THE ENGINE SUMP. ON THE EXTERNAL REAR SIDES OF THE #3 & #4 CYLINDER BARRELS, AN OVAL AREA OF HEAT DISTRESS WAS NOTED. THE CRANKSHAFT & PISTON RODS EXHIBITED PROGRESSIVE HEAT DISTRESS ON ALL ROD BEARINGS AND CRANKSHAFT JOURNALS, WITH THE #1 ROD EXHIBITING THE LEAST HEAT SIGNATURES & THE #4 THE MOST SEVERE. THE #3 ROD CAP WAS FOUND LOOSE IN THE ENGINE; EXAMINATION OF THE CAP BOLTS REVEALED SEVERE NECKING SIGNATURES AT THE POINT OF TENSION FAILURE. A MICROMETER WAS USED TO MEASURE THE CYLINDER BARRELS FOR ROUNDNESS. THE #3 CYL WAS FOUND TO BE OUTSIDE THE FACTORY SPEC BY .002 INCHES.

Probable cause

THE INCORRECT INSTALLATION OF THE ENGINE COWL AND BAFFLE SEALS DURING THE INSTALLATION OF THE ENGINE FOLLOWING AN OVERHAUL.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX90LA035
Event ID
20001213X29825
Case number
LAX90LA035
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: ace39a09d5746eaa21e3ffb3b95b879aa24af6de927ef75815529ef1baf7abca; retrieved 2026-09-21T15:47:12.073Z.