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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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June 24, 1993 · Grumman American AA5A · N9765U

Comet Mine, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 24, 1993
Injury Outcomes
No injuries (3 uninjured)
Location
Comet Mine, AK
Aircraft
Grumman American AA5A
Tail Number
N9765U
Operator
Dawson John B
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC93LA101

A POWERPLANT FAILURE FOR UNDETERMINED REASONS OCCURED OVER TERRAIN UNSUITABLE FOR AN EMERGENCY LANDING. THE PILOT DITCHED THE AIRPLANE AND IT SANK.

NTSB Probable Cause

LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. A FACTOR IN THE ACCIDENT WAS THE UNSUITABLE TERRAIN ON WHICH AN EMERGENCY LANDING COULD BE MADE SUCCESSFULLY.

Full Narrative

On June 23, 1993, at approximately 1605 Alaska daylight time, a wheel equipped Grumman American AASA airplane, N9765U, ditched in the Lynn Canal near Comet Mine, approximately 50 miles north of Juneau, Alaska. The flight was reportedly conducted under 14 CFR Part 91 for personal reasons, and had departed Juneau earlier on June 23 at an unknown time without a flight plan filed. Visual meteorological conditions existed. The Commercial pilot and the two passengers were not injured. The aircraft sank in shallow water and was substantially damaged. Information received from aircraft flying in the vicinity of the ditching indicated the pilot reported a loss of engine power at 2,500 feet while on a local sightseeing flight and elected to "land in the water" because of the unsuitability of the rocky shoreline. The sectional chart of the Lynn Canal, north of Juneau to Skagway and Haines, indicates no airports along the "fiord" type waterway for a distance of approximately 50 miles. The shoreline rises in most places from sea level to over 6000 feet in a distance of less than a mile. The pilot in command had selected a route of flight and an altitude within this fiord route. The airplane sank in shallow water and was recovered at low tide and on June 24, 1993, the airplane wreckage was transported by external-load helicopter to the road system connecting to Juneau. FAA inspectors from the FAA FSDO-S Juneau office told the NTSB that their efforts to see the airplane when it was recovered by external load helicopter were unsuccessful. The aircraft was reported lifted from the water ditching site to the road system north of Juneau. The operator told the NTSB that he "took the airplane apart and brought it to my garage." When asked if the NTSB could review his log books and maintenance records, the operator said that "I lost all of my log books." The pilot reported that the aircraft had 38 gallons of automobile gasoline in the airplane at takeoff from Juneau. The circumstances and events relating to the amount of fuel actually in the aircraft on departure and at the time of the power loss remain undetermined. Recent maintenance and annual inspection data could likewise not be verified, nor could the Supplementary Type Certificate (STC) for the use of automobile fuel. All records were reportedly lost at the time of the ditching, as the operator told investigators that they were aboard the aircraft in flight but not after the aircraft was salvaged. The pilot reported that airplane's carburetor, model MA-4 SPA (Marvel Schebler) malfunctioned, caused by "capscrews holding float chamber to throttle body were working loose." He also stated that "Safety lock tabs did not hold float body to throttle plate securely." Investigators could not verify the pilot's statement due to the removal of the airplane after the accident.

Flight

Event TypeAccident
Event Time16:05 AKDT
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGrumman American AA5A
Tail NumberN9765U
Aircraft CategoryAir
DamageSubstantial
OperatorDawson John B
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-E2G · Reciprocating · 150
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 71 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind210° @ 8 kt
Visibility50 sm
CeilingNone
Temperature / Dew Point57 / 0 C
Altimeter0
Observation Time16:05
Weather SourcePILO

Appendix: Source Data