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October 3, 1982 · Grumman AA-5B · N28820

Denver, NC

Overview

Report Status
Preliminary report
Event Type
Accident
Date
October 3, 1982
Injury Outcomes
No injuries (3 uninjured)
Location
Denver, NC
Aircraft
Grumman AA-5B
Tail Number
N28820
Operator
William T Jay
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ATL83LA002

While cruising at 3500 ft MSL, the pilot heard a loud noise (like an explosion) and saw the engine cowling come open. Simultaneously, the engine lost power and would not respond to throttle movement. During a forced landing in a pasture, the aircraft collided with a fence, and at that time, the engine separated from the aircraft. Witnesses, who saw the plane land, stated that the engine was just hanging on and dropping down during the approach. An investigation revealed that one blade of the McCauley, 1A170 propeller had failed and separated in flight. A metallurgical examination revealed the blade had failed from high cycle, low stress fatigue cracking. The crack initiated from an area adjacent to an attachment bolt hole. AD 80-04-05 had previously identified a cracking problem on this model/propeller. It called for a one-time dye penetrant inspection which had been accomplished on the failed propeller. After this accident, AD 82-27-01 was issued to inspect this make and model every 200 hours.

Full Narrative

WHILE CRUISING AT 3500 FT MSL, THE PILOT HEARD A LOUD NOISE (LIKE AN EXPLOSION) AND SAW THE ENGINE COWLING COME OPEN. SIMULTANEOUSLY, THE ENGINE LOST POWER AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. DURING A FORCED LANDING IN A PASTURE, THE AIRCRAFT COLLIDED WITH A FENCE, AND AT THAT TIME, THE ENGINE SEPARATED FROM THE AIRCRAFT. WITNESSES, WHO SAW THE PLANE LAND, STATED THAT THE ENGINE WAS JUST HANGING ON AND DROPPING DOWN DURING THE APPROACH. AN INVESTIGATION REVEALED THAT 1 BLADE OF THE MCCAULEY, 1A170 PROPELLER HAD FAILED AND SEPARATED IN FLIGHT. A A METALLURGICAL EXAMINATION REVEALED THE BLADE HAD FAILED FROM HIGH CYCLE, LOW STRESS FATIGUE CRACKING. THE CRACK INITIATED FROM AN AREA ADJACENT TO AN ATTACHMENT BOLT HOLE. AD 80-04-05 HAD PREVIOUSLY IDENTIFIED A CRACKING PROBLEM ON THIS MODEL/PROPELLER. IT CALLED FOR A ONE TIME DYE PENETRANT INSPECTION WHICH HAD BEEN ACCOMPLISHED ON THE FAILED PROPELLER. AFTER THIS ACCIDENT, AD 82-27-01 WAS ISSUED TO INSPECT THIS MAKE AND MODEL EVERY 200 HRS.

Flight

Event TypeAccident
Event Time18:45 EDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGrumman AA-5B
Tail NumberN28820
Aircraft CategoryAir
DamageSubstantial
OperatorWilliam T Jay
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A4K · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 31 · Third Class

Conditions

ConditionsVMC
LightDusk
WindCalm
Visibility3 sm
CeilingNone
Temperature / Dew Point17 C / 0 C
Altimeter30.00 inHg

Appendix: Source Data