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Inspection Detail

Inspection: 15193428 - Key Airlines

Inspection Information - Office: Utah Division Of Occupational Safety And Health

 

Inspection Nr: 15193428
Report ID: 0854910
Date Opened: 03/20/1984

Site Address:
Key Airlines
Salt Lake City International Airport
Salt Lake City, UT 84122

Mailing Address:
Po Box A M F 22065, Salt Lake City, UT 84122

Union Status: NonUnion

SIC:4581

NAICS: 0 


Inspection Type: Accident

Scope: Partial

Advanced Notice: N

Ownership: Private

Safety/Health: Safety

Close Conference: 04/03/1984

Planning Guide: Safety-Manufacturing

Emphasis:

Case Closed: 04/03/1984


Related Activity
Type Activity Nr Safety Health
Accident 360601504

Investigation Summary

Investigation Nr: 14456016
Event: 03/19/1984
MULTIPIECE WHEEL RIM ON AIRCRAFT LANDING GEAR EXPLODED

EMPLOYEE #1 WAS INFLATING AN UNDERINFLATED NOSE GEAR TIRE ON A LOCKHEED JETSTAR, USING COMPRESSED NITROGEN GAS. HE HEARD A HISSING NOISE. SHORTLY THEREAFTER, THE WHEEL EXPLODED, SENDING WHEEL FRAGMENTS FLYING INTO EMPLOYEE #1 WHO WAS STANDING DIRECTLY IN FRONT OF THE WHEEL. IT APPEARS THAT THE O RING INSIDE THE TWO PIECE ALUMINUM ALLOY WHEEL WAS DEFECTIVE, ALLOWING NITROGEN TO LEAK INTO THE WHEEL. PRESSURE BUILT UP INSIDE THE WHEEL, CAUSING IT TO EXPLODE. THE WEIGHT OF THE AIRCRAFT WAS ON THE TIRES AT THE TIME OF THE MISHAP. THE WHEEL IS COMPOSED OF TWO PARTS HELD TOGETHER BY EIGHT TNRV BOLTS. THE TORQUE ON THE BOLTS WAS CHECKED ON THE UNDAMAGED NOSE GEAR WHEEL (DUAL). THREE BOLTS WERE 30-50 INCH LBS OVER TORQUED, SIX WERE 30-70 INCH LBS UNDER TORQUED. THE PROPER TORQUE IS 100-120 INCH LBS. THE WHEEL WAS A B.F. GOODRICH TYPE VII, SERIES #693, MANUFACTURED JANUARY 1967. THE STATIC LOAD WAS 3,300 POUNDS. THE TIRE PRESSURE WAS 220 POUNDS. IT ALSO APPEARED FROM A FRAGMENT THAT THERE MAY HAVE BEEN A HAIRLINE CRACK IN THE WHEEL PRIOR TO THE MISHAP.

Keywords: WHEEL, EXPLOSION, INFLATING, MULTIPIECE RIM WHEEL

Investigated Inspection
# Inspection Age Sex Degree of Injury Nature of Injury Occupation
1 15193428 Hospitalized injury Fracture Aircraft engine mechanics
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