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Aviation safety reports, made easier to study

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October 1, 1988 · Grumman AA-5A · N26827

Ridgeland, SC

Overview

Report Status
Preliminary report
Event Type
Accident
Date
October 1, 1988
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Ridgeland, SC
Aircraft
Grumman AA-5A
Tail Number
N26827
Operator
Ceronnie Robinson
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
ATL89LA001

The pilot reported that the left brake failed to function during taxi when he attempted to reduce speed and turn 180 degrees into the takeoff position. The airplane began to track to the right. He released brake pressure on both pedals thinking that he might have been applying pressure to the rudder pedal instead of the brake pedal. He then reapplied pressure and experienced the same results. At that point, he reduced the power to idle. The airplane ran off the side of the runway, traveled down an embankment, and flipped over. Examination of the aircraft revealed a hole in the left brake-system pressure line behind the co-pilot brake pedals. The hole had resulted from chafing between a mounting clamp and the line. The line and clamp were properly installed. The hole was not visible until the clamp was removed. Corrosion was also noted on the line in the area of the hole. A search of FAA SDRs revealed no reports of similar failures.

Full Narrative

THE PLT REPORTED THAT THE LEFT BRAKE FAILED TO FUNCTION DURING TAXI WHEN HE ATTEMPTED TO REDUCE SPEED AND TURN 180 DEG INTO T/O POSITION. THE AIRPLANE BEGAN TO TRACK TO THE RIGHT. HE RELEASED BRAKE PRESSURE ON BOTH PEDALS THINKING THAT HE MIGHT HAVE BEEN APPLYING PRESSURE TO THE RUDDER PEDAL INSTEAD OF THE BRAKE PEDAL. HE THEN REAPPLIED PRESSURE AND EXPERIENCED THE SAME RESULTS. AT THAT POINT, HE REDUCED THE POWER TO IDLE. THE AIRPLANE RAN OFF THE SIDE OF THE RWY. TRAVELED DOWN AN EMBANKMENT, AND FLIPPED OVER. EXAM OF THE ACFT REVEALED A HOLE IN THE LEFT BRAKE-SYSTEM PRESSURE LINE BEHIND THE CO-PLT BRAKE PEDALS. THE HOLE HAD RESULTED FROM CHAFING BETWEEN A MOUNTING CLAMP & THE LINE. THE LINE & CLAMP WERE PROPERLY INSTALLED. THE HOLE WAS NOT VISIBLE UNTIL THE CLAMP WAS REMOVED. CORROSION WAS ALSO NOTED ON THE LINE IN THE AREA OF THE HOLE. A SEARCH OF FAA SDR'S REVEALED NO REPORTS OF SIMILAR FAILURES.

Flight

Event TypeAccident
Event Time11:15 EDT
Nearest AirportRidgeland (0nm N)
Runway21
Runway Length3100 ft
Runway Width70 ft
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGrumman AA-5A
Tail NumberN26827
Aircraft CategoryAir
DamageSubstantial
OperatorCeronnie Robinson
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-E2G · Reciprocating · 150
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 39 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind270° @ 5 kt
Visibility5 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data