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ANC82DA031 · Cessna A185E

5 Apr 1982 · Juneau, AK, United States

Cessna A185E · Accident: total loss of engine power (mechanical failure) on approach

From AUKE BAY, AK to Farmerville, LA

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Event

NTSB case
ANC82DA031
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 A185E

Aircraft type
Cessna 185
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
N4745Q
Operator
Brian A. Emerich · private individual
Onboard fatalities
Unknown
Route
From AUKE BAY, AKTo Farmerville, LA
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 final
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
Substantial

Cause areas

  • Fuel system, pump › Loose
  • Fuel system, pump › Worn

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

NTSB narrative

DURING AN APPROACH TO LAND, THE PILOT OF THE AMPHIBIOUS AIRCRAFT EXTENDED THE GEAR AND PERFORMED HIS PRELANDING CHECKS. HE STATED THAT WHILE HE WAS DESCENDING, HE NOTICED AN EXCESSIVE LOSS OF ALTITUDE AND BEGAN TO ADD POWER. HOWEVER, THE ENGINE DID NOT RESPOND AND HE WAS UNABLE TO OBTAIN A RESTART. SUBSEQUENTLY, THE AIRCRAFT TOUCHED DOWN ON IN THE LIGHTING SYSTEM SHORT OF THE RUNWAY AND NOSED OVER. AN EXAMINATION REVEALED THAT THE LOW PRESSURE RELIEF VALVE ADJUSTING SCREW ON THE FUEL PUMP, PN 638154-1, WAS WORN AND RECESSED IN THE HOUSING. THE SCREW WOULD ROTATE AND VARY THE LOW PRESSURE FUEL SETTING.

Verbatim NTSB analysis from the NTSB dataset

Sources

NTSB record ANC82DA031
Event ID
20020917X01640
Case number
ANC82DA031
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: local date, investigation status. Values present in the bulk record are kept.
  • The date is the local date; the NTSB stores the UTC date 1982-04-06.
  • API snapshot SHA-256: 393cf6455b119234b0178a80478e7faa749564c1988c648f20020845ae5500c3; retrieved 2026-09-22T03:08:07.871Z.