EAGLE INTERNATIONAL
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EAGLE INTERNATIONAL 10 1984
FIRES FROM AN UNDETERMINED CAUSE HAVE OCCURRED IN THE AIR DRYER COMPARTMENT. THE DEICER SYSTEM IS SUSPECTED AND IS KNOWN TO CONTRIBUTE TO ITS INTENSITY. CONSEQUENCE OF DEFECT: OCCUPANTS COULD RECEIVE BURN INJURIES.
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EAGLE INTERNATIONAL 10S 1982
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 10 1980
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 10 1982
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 10 1981
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 10S 1983
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 10S 1980
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 10S 1981
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 10 1983
CRACKS MAY DEVELOP IN THE WELDS THAT JOIN THE POWER STEERING UNIT MOUNTING BRACKET TO THE BUS FRONT END FRAMING. EVENTUALLY, THE WELDS MAY FAIL, CAUSING THE STEERING UNIT TO SEPARATE FROM THE FRONT END FRAME.
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EAGLE INTERNATIONAL 05 1979
THE INVOLVED VEHICLES FAIL TO CONFORM TO FEDERAL MOTOR VEHICLE SAFETY STANDARD NO. 121, AIR BRAKE SYSTEMS. THE VEHICLES WERE EQUIPPED WITH 12 SQUARE INCH BRAKE CHAMBERS INSTEAD OF THE REQUIRED 16 SQUARE INCH BRAKE CHAMBERS. UNDER TEST CONDITIONS 12 SQUARE INCH BRAKE CHAMBERS WILL NOT PROVIDE ADEQUATE BRAKING POWER OR RECOVERY.